flight operations training manual—part three

Transcription

EAST HORIZON AIRLINES
COMPANY OPERATIONS MANUAL PART D
Flight Operations Training Manual
Part Three—CASA 212
FOTM 3
PAGE:
1
DATE:
2 FEB 2011
REVISION:
0
FLIGHT OPERATIONS TRAINING MANUAL—PART THREE
(FOTM 3)
APPROVED COURSES
CASA 212
FOTM 3 contains all EHA courses approved by the Authority for the CASA 212 Aircraft Type.
Subpart A contains the General and Systems courses and any other aircraft type specific ground
training courses.
Subpart B contains all Flight Training modules.
The Appendix contains a copy of the approved Aircraft Operating Manual (AOM)
Security Sensitive Document. No part may be disclosed or copied except by those with ―need to know‖.
Property of East Horizon Airlines • PO Box 1916 • Kabul, Afghanistan
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FOTM 3 CASA 212 SUBPART A
GROUND TRAINING
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SUBPART ‘A’
CASA 212 GROUND TRAINING
General and Systems Courses
Table of Contents
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GROUND TRAINING
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COURSE: CASA 212 INITIAL GROUND SCHOOL
This manual is written in accordance with (I/A/W) Afghanistan Civil Aviation Regulation(s)
8.10.1.14(B), and IS 8.10.1.14(B) as well as utilizing sections of ICAO Doc 9376, ICAO Annex 6,
and appropriate portions of 14 CFR 121.
The enclosed syllabus shows a total training time of 40 hours, as approved by the Ministry of
Transportation – Civil Aviation (MoTCA), and allowed in Afghanistan CARIS 8.10.1.14(B)(d).
Each individual course/module section represents the minimum time of each section and
instruction may exceed each given class.
The enclosed syllabus incorporates all course requirements of Afghanistan C.A.R. 8.10.1.14(B),
Pgs. 8-19 through 8-26.
This ground (Airplane Systems) course incorporates references and study materials from:
CASA-212 Systems Training Manual
CASA-212 Airplane Flight Manual
Approved Quick Reference Handbook (QRH)
Approved Daily Checklist
CASA-212 Cargo Loading Manual
CASA-212 Training – Profiles & Tasks Manual
CASA-212 Operations Manual
INTENTIONALLY LEFT BLANK
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GROUND TRAINING
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CASA 212 -100
5 DAY (INITIAL) - GROUND SCHOOL COURSE
OVERVIEW OF SYLLABUS
Day 1 - Introductions & Company Organization/Structure
Aircraft General Information
Fuel
Hydraulics
Lunch Flight Controls
Environmental
Daily Review
Day 2 – Engines/Powerplant
Propellers
Lunch Fire Detection & Suppression
Annunciator Panel Lights
Daily Review
Day 3 – Checklists & Quick Reference Handbook (QRH)
Emergency Procedures
Emergency Equipment
Emergency Evacuation
Aircraft Limitations
Lunch De-icing/Anti-Icing
Weight & Balance/Performance
Daily Review
Day 4 – Flight Instruments
Lunch Electrical & Lighting
Blue Sky Tracker
Daily Review
Day 5 – CASA-212 Differences Training
Crew Duties & Responsibilities
Lunch Systems Written Exam & Scoring
(2.0 + 1.)
Daily Review
TOTAL of training:
Time Planned
1.0 hr(s)
1.0
1.5
1.5
1.0
1.0
1.0
2.0
2.0
1.0
2.0
1.0
1.0
2.0
1.0
1.0
2.0
1.0
4.0
2.0
1.0
1.0
1.0
3.0
3.0
1.0
40.0 Hours
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GROUND TRAINING
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COURSE: CASA 212 (INITIAL) GROUND SCHOOL
DAY 1
1.1
Day 1, Module 1
Topic: Introductions & Company Organization/Structure
Scheduled time: 1.0 Hr.
Training Aid(s): All present company personnel
1 printed handout of Company Organization/Structure
Computer & projector
Methodology: Individual introductions & group discussion – supervised by Instructor
Objective: For the student to become familiarized with:
Company personnel present during training
Fellow students
Company structure & Management individuals
1.2
Day 1, Module 2
Topic: Aircraft General Information
Schedule time: 1.0 Hr.
Training Aid(s): Printed handout of general CASA 212 information
Airplane Systems Manual – (electronic version)
Small ―Take home‖ exam
Methodology:
Instructor presented coverage of general CASA 212 specifications and
information
Group discussion
―Take home‖ exam
Objective: For the students to have a basic understanding of the general knowledge of
the CASA 212 airplane
1.3
Day 1, Module 3
Topic: Fuel system
Scheduled time: 1.5 Hrs.
Training Aid(s): Printed handout of the CASA 212 fuel system
Easel – for sketching diagram(s)
Methodology: Instructor presented coverage of CASA 212 fuel system
Group discussion
Objective: For the students to have a thorough understanding of the CASA 212 airplane
fuel system.
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GROUND TRAINING
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CASA 212 Initial Ground School Day 1 (cont)
1.4
Day 1, Module 4
Topic: Hydraulics system
Training Aid(s): Printed handout of the CASA 212 hydraulic system
Methodology: Instructor presented coverage of CASA 212 hydraulic system
Group discussion
Objective: For the students to have a thorough understanding of the CASA 212 airplane hydraulic
system
1.5
Day 1, Module 5
Topic: Flight Controls
Training Aid(s): Printed handout of the CASA 212 flight controls
Methodology: Instructor presented coverage of CASA 212 flight controls
Group discussion
Objective: For the students to have a thorough understanding of the CASA 212 airplane
flight controls
1.6
Day 1, Module 6
Topic: Environmental system
Training Aid(s): Printed handout of the CASA 212 environmental system
Methodology: Instructor presented coverage of CASA 212 environmental system
Group discussion
Objective: For the students to have a thorough understanding of the CASA 212 environmental
system.
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GROUND TRAINING
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COURSE: CASA 212 (INITIAL) GROUND SCHOOL
DAY 2
2.1
Day 2, Module 1
Topic: Engine/Powerplant
Training Aid(s): Printed handout of the CASA 212 engine/powerplant
Methodology: Instructor presented coverage of CASA 212 engine/powerplant
Group discussion
Objective: For the students to have a thorough understanding of the Garret TPE-331 engine.
2.2
Day 2, Module 2
Topic: Propeller system
Training Aid(s): Printed handout of the CASA 212 propeller system
Methodology: Instructor presented coverage of CASA 212 propeller system
Group discussion
Objective: For the students to have a thorough understanding of the CASA 212 propeller system
2.3
Day 2, Module 3
Topic: Fire Detection & Suppression systems
Training Aid(s): Printed handout of the CASA 212 fire detection & suppression systems
Methodology: Instructor presented coverage of CASA 212 fire detection & suppression systems
Group discussion
Objective: For the students to have a thorough understanding of the CASA 212 fire detection &
suppression systems
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GROUND TRAINING
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2.4
Day 2, Module 4
Topic: Annunciator Panel
Training Aid(s): Printed handout of the CASA 212 annunciator panel
Methodology: Instructor presented coverage of CASA 212 annunciator panel
Group discussion
Objective: For the students to have a thorough understanding of the CASA 212 annunciator
panel
__________________________________________________________________________________
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GROUND TRAINING
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DAY 3
3.1
Day 3, Module 1
Topic: Checklists/Quick Reference Handbook (QRH)
Training Aid(s): Printed handout of the CASA 212 checklists & Quick Reference Handbook (QRH)
Methodology: Instructor presented coverage of CASA 212 checklists & QRH
Group discussion
Personal copies of the checklists & QRH to study and practice from
Objective: For the students to have a thorough understanding of the CASA 212 checklists & QRH
for proper usage in flight operations
3.2
Day 3, Module 2
Topic: Emergency Procedures
Training Aid(s): Printed handout of the CASA 212 Emergency Procedures
Airplane Flight Manual (electronic version)
Easel – for notes
Methodology: Instructor presented coverage of CASA 212 Emergency Procedures
Group discussion
Objective: For the students to have a thorough understanding of the CASA 212 emergency
procedures.
3.3
Day 3, Module 3
Topic: Aircraft Limitations
Training Aid(s): Printed handout of the CASA 212 aircraft limitations
Easel – for notes
Methodology: Instructor presented coverage of CASA 212 aircraft limitations
Group discussion
Objective: For the students to have a thorough understanding of the CASA 212 aircraft
limitations
3.4
Day 3, Module 4
Topic: De-icing/Anti-icing systems
Training Aid(s): Printed handout of the CASA 212 de-icing/anti-icing systems
Easel – for notes
Methodology: Instructor presented coverage of CASA 212 de-icing/anti-icing systems
Group discussion
de-icing/anti-icing systems
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GROUND TRAINING
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3.5
Day 3, Module 5
Topic: Weight & Balance/Performance
Training Aid(s): Printed handout of the CASA 212 weight & balance charts
along with additional performance charts
Airplane Flight Manual – (electronic version)
Easel – for notes
Methodology: Instructor presented training of CASA 212 weight & balance computations as well
as additional performance charts for necessary reference
Group discussion
Objective: For the students to have a thorough understanding of the necessary computations &
applications for the CASA 212 weight & balance charts in addition to other performance charts
from the Airplane Flight Manual.
___________________________________________________________________________________
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GROUND TRAINING
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DAY 4
4.1
Day 4, Module 1
Topic: Flight Instruments
Training Aid(s): Printed handout of the CASA 212 Nav/Comm avionics systems
Manuals for particular avionics system(s)
Easel – for notes
Methodology: Instructor presented training of CASA 212 navigation & communication avionics
Group discussion
navigation & communication systems
4.2
Day 4, Module 2
Topic: Electrical & Lighting systems
Training Aid(s): Printed handout of the CASA 212 electrical & lighting systems
Easel – for notes
Methodology: Instructor presented coverage of CASA 212 electrical & lighting systems
Group discussion
Electrical & lighting systems
4.3
Day 4, Module 3
Topic: Blue Sky Tracker system
Training Aid(s): Printed handout of the Blue Sky Tracker operations
Methodology: Instructor presented coverage of Blue Sky Tracker operations
Group discussion
Objective: For the students to have a thorough understanding of the Blue Sky Tracker system
___________________________________________________________________________________
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GROUND TRAINING
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DAY 5
5.1
Day 5, Module 1
Topic: CASA 212 Differences Training
Training Aid(s): Printed handout of the CASA 212 Model differences
Easel – for notes
Methodology: Instructor presented training of the CASA 212 model differences
Group discussion
Objective: For the students to have a basic understanding of CASA 212 model differences and
how to determine differences from the appropriate manual(s)
5.2
Day 5, Module 2
Topic: Crew Duties & Responsibilities
Training Aid(s): Printed handout of procedures
Company Operations Manual - (electronic version)
Easel – for notes
Methodology: Instructor presented training of a normal day’s procedures
Group discussion
Objective: For the students to have a basic understanding of a normal day’s procedures and
operations
5.3
Day 5, Module 3
Topic: Final Written Exam & Scoring
Scheduled time: 3.0 Hrs. (2.0 + 1.0)
Training Aid(s): Printed handout of final written exam
Methodology: Instructor presented examination & monitoring
Group discussion of exam answers
Objective: For the students to complete their final written exams of the ground school training
as well as to understand any mistakes they may have made in their answers
_______________________________________________________________________________
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GROUND TRAINING EXAMS
APPENDIX
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1
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APPENDIX 1 A
CASA 212 SYSTEM WRITTEN EXAMINATIONS
Table of Contents
Sect.
E.1
E.2
E.3
E.4
E.5
E.6
E.7
E.8
E.9
E.10
E.11
E.12
E.13
E.14
E.15
E.16
E.17
E.18
E.19
E.20
E.21
E.22
E.23
Page
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
24
25
26
36
Subject
Flight Controls
Heating & Vent.
Fuel System
General
Hydraulics
Lndg Gear & Brakes
Oxygen
Annunciator
Fire Detection & Suppresion
Powerplant
Propellers
Emergency Equipment
Ice & Rain
Operations Limitations
Performance & Planning
Wt. & Balance
Electrical
Flight Instruments
Lighting
Final Exam
Systems Oral Exam
Page 1
E.1
CASA 212
APPENDIX
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1A
2
2 FEB 2011
0
FLIGHT CONTROLS EXAM
NAME:__________________________________EMP #________ DATE:_________
INSTRUCTOR:___________________________EMP #________ SCORE:_________
1.
How many flaps on the CASA 212?
___________
2.
Where are the flaps located? _______________________________________________
3.
Which aileron has the trim tab on it? _________________________________________
4.
Which tab on the rudder is the trim tab?
a. Upper
b. Lower
5.
Which tab on the elevator is the trim tab? ____________________________________
6.
The flaps are __________________________activated and ______________actuated.
7.
Which flight control has a single cable system?
a.
b.
c.
d.
Ailerons
Rudder
Flaps
Elevators
8.
Flaps are doubled slotted with maximum extension of ____________ degrees.
9.
Flaps should fully extend or retract within _____________ seconds.
10.
Speed limitation for approach flaps: _______________ KIAS.
__________________________________________________________________________________
Page 2
E.2
CASA 212
APPENDIX
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DATE:
REVISION:
1A
3
2 FEB 2011
0
HEATING & VENTILATION EXAM
NAME:__________________________________EMP #________ DATE:_________
INSTRUCTOR:___________________________EMP #________ SCORE:_________
1.
What is the source for cabin heating? ________________________________
2.
Why should the heating system be turned OFF for take-off and landing?
________________________________________________________________________
3.
Ram air (for ventilation) enters the aircraft through _____ intakes located on the fuselage.
4.
What areas of the airplane are cooled?
_______________________________
_______________________________
_______________________________
____________________________________________________________________________________
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E.3
CASA 212
APPENDIX
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DATE:
REVISION:
1A
4
2 FEB 2011
0
FUEL SYSTEM EXAM
NAME:__________________________________EMP #________ DATE:_________
INSTRUCTOR:___________________________EMP #________ SCORE:________
1.
Total tank capacity is: _______ gallons, ___________ gallons usable.
2.
Inboard total capacity is: _______ gallons, ________ gallons usable.
3.
Outboard total capacity is: _____ gallons, _______ gallons usable.
4.
How many fuel tanks in the CASA 212 and where are they located?
_____ tanks, in the ________
5.
What type of fuel tanks are they?
a. Composite
b. Bladder
c. Integral
6.
What is the normal single point refueling pressure on the 200/300/400 models?
___ +/ - ___ psi
7.
Which tanks should be fueled first? Why?
________ tanks, because of ______________________________
8.
How many fuel boost pumps are there? ______
9.
The Fuel Boost pumps are located in the __________ tanks inside each inboard tank.
10.
Clogging of the ejector filter can cause abnormal fuel transfer within the tanks.
a. True
b. False
___________________________________________________________________________________
Intentionally left blank
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E.4
CASA 212
APPENDIX
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DATE:
REVISION:
1A
5
2 FEB 2011
0
AIRCRAFT GENERAL EXAM
NAME:__________________________________EMP #________ DATE:_________
1.
The aircraft has the structural integrity to operate STOL:
True or False
2.
Total usable fuel capacity is __________ US gallons.
3.
Max Takeoff Weight is __________ lbs.
4.
Max Landing Weight is __________ lbs.
5.
Max Zero Fuel Weight is _________lbs.
6.
Max Allowable Gross Weight is _______ lbs.
7.
The aircraft will start from an on-board battery source:
8.
The High Wing design reduces Foreign Object Damage:
9.
The aircraft Wing Span is _____ ft and _____ inches.
10.
Aircraft power is provided by _____ onboard batteries and _____ generators.
11.
The highest point of a CASA 212 is _____ ft and _____ inches.
12.
Tire pressure for the CASA 212-100 is ____psi for the main gear
True or False
True or False
and _____ psi for the nose tire.
_________________________________________________________________________
Page 5
E.5
CASA 212
APPENDIX
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DATE:
REVISION:
1A
6
2 FEB 2011
0
HYDRAULICS EXAM
NAME:__________________________________EMP #________ DATE:_________
1.
The hydraulic system consists of which four subsystems?
a.
b.
c.
d.
________________________________
________________________________
________________________________
________________________________
2.
Hydraulic fluid type used is: ______________________________
3.
What is the normal hydraulic system pressure? ________________________
4.
What is the hydraulic pump duty cycle? ______ minutes ON and _____ minutes OFF.
5.
How do you check the hydraulic fluid level?
_________________________________, ____________________________________
_________________________________, ____________________________________
6.
If both hydraulic pumps fail, can braking be used?
7.
a. Yes
b. No
What should the emergency brake accumulator indicate in the nose section?
_________________________________________________________________
8.
Approximately how many braking applications will the normal brake system accumulator
give in the event of a hydraulic failure?
a.
b.
c.
d.
9.
10
20
30
40
Approximate hydraulic system capacity is ___________ liters and a reservoir capacity of
__________ liters.
10.
If the electric hydraulic pump fails, can you still operate all the subsystems simultaneously, and if
so, how?
YES -
NO
HOW: ______________________________________
Page 6
E.6
CASA 212
APPENDIX
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DATE:
REVISION:
1A
7
2 FEB 2011
0
LANDING GEAR AND BRAKES EXAM
NAME:__________________________________EMP #________ DATE:_________
1.
Nose wheel is steerable through _________________ degrees either side of center.
2.
CASA 212 has ________________ - _________________ type shock struts.
3.
When towing a CASA 212, what precautions should be taken with the nose gear?
____________________________________
4.
Can pilots determine the brake wear?
a. Yes
b. No
5.
The accumulator brake pressure is sufficient for approximately _________ applications.
____________________________________________________________________________________
Page 7
E.7
CASA 212
APPENDIX
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DATE:
REVISION:
1A
8
2 FEB 2011
0
OXYGEN EXAM
NAME:__________________________________EMP #________ DATE:_________
INSTRUCTOR:___________________________EMP #________ SCORE:_______
1.
A full main oxygen bottle will provide both pilots with approximately ___ hours
of oxygen supply at _______ feet with the masks on normal (diluter-demand).
2. Minimum oxygen cylinder pressure of _______ psi prevents condensation
in the bottle and lines.
3.
Why is the oxygen system so important in the CASA 212?
____________________________________
4.
During a cabin fire, why should the oxygen masks be placed at the 100% position?
________________________________________________
____________________________________________________________________________________
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E.8
CASA 212
APPENDIX
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DATE:
REVISION:
1A
9
2 FEB 2011
0
ANNUNCIATOR PANEL LIGHTS EXAM
NAME:__________________________________EMP #________ DATE:_________
1. The ―GENERATOR‖ Light comes on when the affected generator _____________.
2. Battery Temp Light is _________ (color) and comes on when the battery temp goes above
_________ degrees.
3. The Fuel Level light comes on when the fuel level in the collector tank goes below _______
pounds of fuel.
4. The ―CHIP DETECTOR‖ light is __________ (Color) and comes on when _______________ is
detected.
5. The ―UNSAFE DOOR‖ light is __________ colored.
6. ―ENGINE FIRE‖ light is ___________colored.
7. The ―BAGGAGE COMPARTMENT SMOKE‖ light is _______ colored.
___________________________________________________________________________________
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E.9
CASA 212
APPENDIX
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DATE:
REVISION:
1A
10
2 FEB 2011
0
FIRE DETECTION & SUPPRESSION EXAM
NAME:__________________________________EMP #________ DATE:_________
1.
Does the pilot have a cockpit indication showing that the extinguisher bottles electrically
discharged? If so, how?
Yes – No How: ______________________________________________________
2.
When depressing the far right fire button, which bottle do you discharge into which engine?
Bottle # _________, into ________________________________ engine.
3.
What indication do you have in the event of engine fire extinguishing agent bottle over
pressure?
_______________________________________________________________
4.
How many fire extinguishers are located inside the aircraft and where are they?
_______, located: ____________________________________________________
5.
The smoke detection spring loaded test switch located on the overhead warnings and test panel
checks the continuity of the circuit.
a. True
b. False
___________________________________________________________________________________
Page 10
E.10
CASA 212
APPENDIX
PAGE:
DATE:
REVISION:
1A
11
2 FEB 2011
0
POWERPLANT EXAM
NAME:__________________________________EMP #________ DATE:_________
1.
The Garrett TPE331-5 is rated at 776 SHP?
a. True
or
b. False
2.
The main rotating group of the TPE-331 engine consists of a _______ stage centrifugal
compressor section and a __________ stage axial turbine section.
3.
At what engine (P)pressure station is the highest pressure? ___________
4.
The pressure and temperature of the air, as it passes through the two stage compressor section
will _________________________.
5.
The purpose of the oil vent valve is to unload the oil pump during the engine start.
a. True
or
b. False
6.
Normal operation of the oil vent valve will be indicated by a sudden ride of ________
_______________ at 60% RPM.
7.
During normal start of the -5 engine fuel is supplied to the engine automatically at 10%
a. True or b. False
8.
ITT limit during start/acceleration is ___________ C / for ________ second.
9.
When opening the fuel switch, which sequences do the valves operate?
RPM.
______________________________, ___________________________________
______________________________.
10.
Ground start OAT Limit: MIN -_______ C, MAX +__________ C.
11.
MAX residual ITT for start is ___________ C.
12.
―Light Off‖ time from 10% RPM: GND Start: ______________seconds
13.
The Fuel Purge Accumulator is fully charged at: _____________% RPM.
____________________________________________________________________________________
Page 11
E.11
CASA 212
APPENDIX
PAGE:
DATE:
REVISION:
1A
12
2 FEB 2011
0
Propellers Exam
NAME:__________________________________EMP #________ DATE:_________
1.
Propeller Governor Mode (PG): The power lever is forward of Flight Idle,
the RPM range is 96 – 100%
a. True
2.
or
b. False
Beta Mode: In response to movement of the power lever aft of Flight Idle,
the RPM range 65 – 97%.
a. True
or
b. False
3.
At about ________ % RPM the Start Lock pins extend as their spring forces overcome the
decreasing centrifugal force.
4.
The locks are disengaged, ―prop off the locks‖, after engine start by moving the Power Lever to
__________________.
5.
The Power Lever is mechanically connected to the _____________________________ and the
___________________________________.
6.
The Speed Lever is mechanically connected to the _____________________________ and the
___________________________________.
7.
MAX reverse speed is: ____________ KIAS.
8.
Loss of propeller oil pressure during operation would: ___________________________.
9.
10.
Negative Torque Sensing is an __________________________ drag reduction system.
What is the unfeathering pump duty cycle?
____________ min. ON and _____________ min. OFF
___________________________________________________________________________________
Page 12
E.12
CASA 212
APPENDIX
PAGE:
DATE:
REVISION:
1A
13
2 FEB 2011
0
EMERGENCY EQUIPMENT EXAM
NAME:__________________________________EMP #________ DATE:_________
1.
Where the following emergency equipment items are located onboard the aircraft?
Crash Axe ________________________
First Aid Kit _____________________________
Fire Extinguisher(s) ________________________________
_______________________________
2.
In case of a fire – what part of the fire do you direct the extinguishing agent at?
______________________________________________
3.
What else might be regarded as Emergency Equipment? (Bonus Points)
______________________________________________
______________________________________________
______________________________________________
___________________________________________________________________________________
Page 13
APPENDIX
PAGE:
DATE:
REVISION:
1A
14
2 FEB 2011
0
E.13
CASA 212
EMERGENCY EVACUATION EXAM
1.
There are ______doors and ______ hatch that can be used as emergency exits.
2.
When departing the aircraft remember to stay away from the ________________.
3.
Always remember to take ______________________ & __________________ with you
as you exit the airplane in an emergency.
____________________________________________________________________________
Page 14
E.14
CASA 212
APPENDIX
PAGE:
DATE:
REVISION:
1A
15
2 FEB 2011
0
EMERGENCY PROCEDURES EXAM
NAME:__________________________________EMP #________ DATE:_________
1.
2.
The Memory items to ENGINE FIRE ON THE GROUND are:
____________________________
______
____________________________
______
____________________________
______
____________________________
______
The Memory items to
ENGINE FAILURE DURING TAKEOFF – ABORTED TAKEOFF are:
_______________________________
____________
_______________________________
____________
_______________________________
____________
____________________________ ____________
3.
4.
_______________________________
____________
_______________________________
____________
The Memory items to ELECTRICAL FIRE IN FLIGHT are:
_______________________________
________________
_______________________________
________________
_______________________________
________________
The Memory items for BATTERY OVERTEMP IN FLIGHT are:
_______________________________
________________
_______________________________
________________
Page 15
E.15
CASA 212
APPENDIX
PAGE:
DATE:
REVISION:
1A
16
2 FEB 2011
0
ICE & RAIN PROTECTION EXAM
NAME:__________________________________EMP #________ DATE:_________
1.
The pneumatic de-ice boots consist of ___________ pneumatically inflated boots molded
to leading edge of outer wings, vertical and horizontal stabilizers.
2.
The system will function with either engine shut down?
a. True
3.
or
b. False
Pneumatic air is ducted to _______ ejector valves. Where are they located?
___________________________________
___________________________________
4.
What heats the lower air intake surface? __________________________________
5.
What heats the upper air intake surface? __________________________________
6.
Is the P2 probe of the P2/T2 sensor heated?
7.
A cold soaked windshield should be warmed gradually by cycling the heater for
a. Yes
or
b. No
__________ seconds ON and ____________ seconds OFF for 1 minute.
8.
Pitot heat operation is limited to _________ minute with the aircraft stationary.
9.
Where are the propellers de-ice fuses located?
_____________________________________________________________________
Page 16
E.16
CASA 212
APPENDIX
PAGE:
DATE:
REVISION:
1A
17
2 FEB 2011
0
AIRCRAFT OPERATIONS LIMITATIONS EXAM
NAME:__________________________________EMP #________ DATE:_________
1.
MAX Ramp Weight: ________ lbs.
2.
MAX Taxi Weight: __________ lbs.
3.
MAX Takeoff Weight: __________ lbs.
4.
MAX Landing Weight: __________ lbs.
5.
Max. Zero Fuel Weight: __________ lbs.
6.
MAX Operating Speed (Vmo): _______ KIAS
7.
MAX Inflight Ramp/Cargo Door Speed: _______ KIAS
8.
Maneuvering Speed: _______ KIAS
9.
Flap Extension Speed (Approach): _______ KIAS
10.
Flap Extension Speed (Landing – Full): _______ KIAS
11.
MAX Reverse Speed: _______ KIAS
12.
MAX Demonstrated Crosswind: ________ KIAS
13.
MAX Tail Wind: ______KIAS
14.
MAX Operating Altitude: __________ Ft.
15.
Operating Temperature Range: ______ C, to _______ C.
16.
Landing Lights Use (on the ground): _______________________________________
17.
Maximum Allowable Torque: __________
18.
Never Exceed RPM Limit:
19.
PROHIBITED Range of Propeller: _____________
20.
Maximum Airport Elevation for Take Off: __________
_________
Page 17
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CASA 212
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PERFORMANCE & PLANNING EXAM
NAME:__________________________________EMP #________ DATE:_________
1.
At the airports from which we operate, which condition is the most limiting?
a. Takeoff Runway length
2.
or
b. Climb Gradient
Which segment of the takeoff flight path are we most weight limited?
_________________________
3.
In our performance planning _________________, ______________________,
and ____________________ are all factors in computing V1/Vr – V2 & Vref.
____________________________________________________________________________________
Page 18
E.18
CASA 212
1.
What is the usual forward & aft C.G. limits?
2.
MAX Taxi Weight? _________ lbs.
3.
MAX Takeoff Weight? _________ lbs.
4.
MAX Zero Fuel Weight? _________ lbs.
5.
MAX Landing Weight? __________ lbs.
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WEIGHT & BALANCE EXAM
____ to ____
6.
Each multi-engine aircraft operated by the Company will be weighed at intervals not to exceed
______ calendar months.
7.
As you burn fuel - the Center of Gravity of the airplane shifts ___________
___________________________________________________________________________________
Page 19
E.19
CASA-212
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DATE:
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2 FEB 2011
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ELECTRICAL SYSTEM EXAM
NAME:__________________________________EMP #________ DATE:_________
1.
What temperature will cause the battery overtemp light to come on?
a.
b.
c.
d.
54° C
66° C
25° C
65° C
2.
How many batteries does the C-212 have?
a. 1
a. 2
b. 3
c. 4
3.
What bus-bar is connected to the auxiliary battery?
a.
b.
c.
d.
4.
The starter-generators feed into parallel into which bus-bar?
a.
b.
c.
d.
5.
7.
Primary bus
Secondary bus
Essential bus
Start bus
Which bus-bar is fed by the No. 1 battery?
a.
b.
c.
d.
6.
Auxiliary or primary bus
Secondary bus
Essential bus
Start bus
Primary bus
Secondary bus
Essential bus
Start bus
What feature connects the secondary bus to the essential bus?
a. Essential master switch
b. Secondary master switch
c. Bus tie switch
d. Bus tie circuit breaker
When starting with the series/parallel switch in the series position, how many volts are
supplied to that first engine start?
a.
a.
b.
c.
24
28
30
48
Page 20
APPENDIX
PAGE:
DATE:
REVISION:
E.17
CASA-212
8.
Is it possible to do a manual 48-volt battery start?
9.
a. Yes
b. No
Can the battery switches be left on when doing an APU start?
1A
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2 FEB 2011
0
Electrical System Exam (cont)
a. Yes, they should always be on for an APU start.
b. No, they should never be on for an APU start.
10.
What is the voltage rating of the inverters?
a.
b.
c.
d.
28 VAC
115 VAC
400 VAC
None of the above.
11.
How many inverters are on the CASA 212?
12.
a. 1
b. 2
c. 3
d. 4
How can we determine if an inverter has failed?
a. Loss of all AC instruments
b. Turn of all the inverters and then turn them back on one at a time
c. Warning light on the warning panel
d. None of the above
13.
If a fault develops on the Essential bus bar will the generators automatically switch to
the Secondary bus bar?
14.
a. Yes
b. No
The capacity of the two starter generators on the CASA 212 is?
15.
a. 24 volts, 22 amps
b. 28 volts, 200 amps
c. 30 volts, 300 amps
Is it possible to start both engines with 48 volts (series) ?
a. Yes
b. No
Page 21
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E.17
CASA-212
APPENDIX
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DATE:
REVISION:
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0
16.
In flight or on the ground, where is the main DC volt indicator taking the voltage from
the switch is in the center position?
when
17.
a. Primary bus
b. Secondary bus
c. Essential bus
d. Start bus
The minimum battery voltage prior to start:
18.
a. 24 volts
b. 28 volts
c. 23 volts
d. 15 volts
The capacity of batteries 1 and 2 are:
19.
b. 26 volts, 22 amps
c. 24 volts, 40 amps
To use a ground power unit, it should supply a minimum of:
20.
a. 28 volts, 600 amps with 1200 amps overload capacity
b. 24 volts, 700 amps with 800 amps intermittent capability
c. 48 volts, 500 amps with no intermittent capability
d. 22 volts, 800 amps with 1000 overload capability
The power output of the aux battery is:
21.
b. 24 volts, 7 amps
c. 28 volts, 7 amps
d. 24 volts, 22 amps
The generator control (DC control panel) incorporates what forms of generator
22.
a. Over voltage, fault, synchronization of frequency
b. Ground fault, over voltage, reverse current protection
c. Over voltage from APU
d. Over temperature and ground fault protection
What percentage of RPM can the Starter-Generator function as a generator and be put on-line?
23.
a. 55%
b. 60%
c. 65%
d. 70%
Which statement is correct?
a.
b.
c.
d.
protection?
There is 1 DC ammeter and 1 DC voltmeter for each starter-generator.
There is 1 DC ammeter and 1 DC voltmeter on the aircraft.
There are 2 DC ammeters and 1 DC voltmeter on the aircraft.
There is 1 DC ammeter and 2 DC voltmeters on the aircraft.
Page 22
E.17
CASA-212
24.
The over voltage function on the generator test switch is:
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a. To provide an artificial over voltage in order to automatically disconnect the generator when
it reaches 31 volts.
b. To simulate an absence of the ground in the generators.
c. To provide an artificial over voltage in order to connect the generator.
d. To provide an over intensity in the generator.
25.
What is the purpose of the auxiliary battery?
a.
b.
c.
d.
To supply emergency power for emergency lighting in the cabin.
To help give more electrical power for initial engine starting.
To supply added power to critical primary flight instruments during an engine start.
To supply 24 VDC to critical engine instruments during an engine start.
___________________________________________________________________________________
Page 23
E.20
CASA 212
APPENDIX
PAGE:
DATE:
REVISION:
1A
24
2 FEB 2011
0
Flight Instruments Exam
NAME:__________________________________EMP #________ DATE:_________
1.
On the CASA 212, there are ____ static ports of which one on each side is integrated in the
______________.
2.
The overspeed sensor receives its pitot static information from the:
a. Captain’s side
3.
or
b. First Officer’s side pitot static system?
Pitot tube heating is electrical through what bus bar(s)?
_______________________, _________________________
4.
In the event that we lose static source, we can select a back-up source in the cockpit?
a. True or b. False
5.
The difference between IAS and CAS is negligible throughout the speed range of the
aircraft?
a. True
6.
or
b. False
What is the purpose of Pitot Heat in the CASA 212?
______________________________________________________
7.
If the #1 DG/Compass systems fails – a _______________________ switch will allow
copilot’s data to supply the pilots HSI.
the
8.
The CASA 212 is equipped with ___ identical, but independent remote sensing compass
system(s).
Page 24
E.21
CASA-212
APPENDIX
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DATE:
REVISION:
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2 FEB 2011
0
LIGHTING SYSTEM EXAM
NAME:__________________________________EMP #________ DATE:_________
1.
Position Lights, emergency lights, essential instrument lights, internal lights and one
light are powered through the circuit breakers on the ________________ bus bar.
2.
The Taxi light switch operates the ______ watts wide angle taxi light in the nose radome.
3.
The Landing light Left & Right operates the _____ watts dual lights in the nose radome.
4.
Max ground operating time: ______min. ON and _____ min. OFF prevents overheating.
5.
What two internal light switches are hot wired directly to the battery?
landing
__________________ and ___________________
_______________________________________________________________________________
Page 25
APPENDIX
PAGE:
DATE:
REVISION:
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2 FEB 2011
0
E.21
CASA 212 FINAL WRITTEN EXAM
NAME:__________________________________EMP #________ DATE:_________
AIRCRAFT GENERAL
1. The turning radius of this aircraft is __________
2. There are ______ emergency exits to this airplane (not counting windows or ramp)
3. Fuel capacity for this airplane is _________ gallons.
4. Maximum Landing Weight is _____________pounds.
5. Zero Fuel Weight means:__________________________________
6. The service ceiling of this airplane is _________’
7. The landing gear is steerable through _______ degrees either side of center.
8. Can Pilots determine the brake wear? ______
9. The accumulator brake pressure is good for approximately _______ applications.
10. Why is the oxygen system so important to pilots? ____________________________
11. The aircraft has the structural integrity to operate STOL:
True or False
12. Total usable fuel capacity is __________ US gallons.
13. Max Takeoff Weight is __________ lbs.
14. Max Landing Weight is __________ lbs.
15. Max Zero Fuel Weight is _________lbs.
16. Max Allowable Gross Weight is _______ lbs.
17. The aircraft will start from an on-board battery source:
True or False
18. The High Wing design reduces Foreign Object Damage:
True or False
19. The aircraft Wing Span is _____ ft and _____ inches.
20. Aircraft power is provided by _____ onboard batteries and _____ generators.
21. The highest point of a CASA 100 is _____ ft and _____ inches.
22. Tire pressure for the CASA 212-100 is ____psi for the main gear
and _____ psi for the nose tire.
POWERPLANTS/ENGINES
23. The engines powering the airplane are designated(Make & Model) _________________
24. These engines are rated at _________ Shaft Horse Power.
25. The basic concept of a turbo-prop system is:
_______________, __________________, ________________, _____________
26. Propeller Reverse (BETA Range) is activated by the _______________ levers.
27. Normal engine RPM operating limits are: _______ % to _______% rpm.
28. An overspeed condition exists when the engine rpm exceeds _________%
Page 26
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29. During normal start of the -5 engine fuel is supplied automatically at 10%? __T or F___
30. Max Residual ITT for start is ______ degrees
31. The main rotating group of the TPE-331 engine consists of a ______stage centrifugal compressor
and a _____ stage axial turbine section.
32. The highest pressure point/engine station is the ______ point?
FIRE DETECTION & SUPPRESSION
33. Engine Fire sensing uses a closed ____________________ loop system.
34. Engine fire extinguishers use _______Vdc (power) from the Essential Bus.
35. The LEFT Fire bottle may be used to combat a fire in the RIGHT engine nacelle
YES or
NO
36. In the event that a fire bottle has over pressurized the indication is
___________________________________________.
37. There are _______ hand held fire extinguishers on board the airplane.
FUEL
38. There are a total of _____ fuel tanks in this airplane?
39. What type of fuel tanks are they? _______________
40. How many fuel boost pumps are there? __________
41. Total usable fuel for this airplane is __________ gallons?
HYDRAULICS
42. There are _____ sources of hydraulic pressure. (Not counting the accumulators)
43. Three nitrogen charged accumulators provide backup for ______ systems.
44. The hydraulics system has _______ primary systems that it provides pressure for.
45. The foot pedals (brakes) work on the ______________ pressure concept.
46. The rear cargo door can be open up to _____ KIAS.
47. The hydraulic pressure indicator should show _____psi when in the green/normal range.
48. The hydraulic system consists of which four subsystems?
________________________________
________________________________
________________________________
________________________________
49. Hydraulic fluid type used is: ______________________________
50. What is the normal hydraulic system pressure? ________________________
51. What is the hydraulic pump duty cycle? ______ minutes ON and _____ minutes OFF.
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52. How do you check the hydraulic fluid level?
_________________________________, ____________________________________
_________________________________, ____________________________________
53. If both hydraulic pumps fail, can braking be used?
Yes No
54. What should the emergency brake accumulator indicate in the nose section?
_________________________________________________________________
55. Approximately how many braking applications will the normal brake system
accumulator give in the event of a hydraulic failure?
a. 10
b. 20
c. 30
d. 40
56. Approximate hydraulic system capacity is ___________ liters and a reservoir capacity of
__________ liters.
57. If the electric hydraulic pump fails, can you still operate all the subsystems simultaneously, and if
so, how?
YES -
NO
HOW: ______________________________________
FLIGHT CONTROLS
58. All controls are mechanical – except for the flaps which are _______________ activated and
_______________ actuated.
59. The flaps are double slotted and extend to a maximum of _____ degrees.
60. The flaps should extend completely within _____ seconds.
61. All of the systems have duplicate cables except for the __________ system.
ENVIRONMENTAL
62. The source for the cabin heating is ___________ air.
63.
64. What areas of the airplane are cooled?
________________, ____________________, ______________________
65. Ram air (for ventilation) enters thru _____ intakes along the fuselage.
PROPELLERS
66. In the Prop Governor Mode – the power lever is forward of the Flight idle stop and the RPM range
is ______________%.
67. The start Lock pins extend at _______% RPM as their spring forces overcome the decreasing
centrifugal force.
68. Max reverse speed is _______LIAS.
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APPENDIX
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REVISION:
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69. Los of oil pressure during operation would _______________________.
70. The Speed Lever is mechanically connected to the ______________________ and the
_________________________.
ANNUNCIATOR PANEL LIGHTS
71. The Red ―BATTERY OVERTEMP‖ light comes on when the battery reaches ____ degrees.
72. The ―CHIP DETECTOR‖ light is ________ colored.
73. The ―FUEL PRESSURE‖ light comes on when the fuel pressure goes below ______ psi and goes
back out when the pressure goes back above _____ psi.
74. The ―OVERLOAD START RELAY‖ light is ________ colored.
Landing Gear and Brakes
75. Nose wheel is steerable through _________________ degrees either side of center.
76. CASA 212 has ________________ - _________________ type shock struts.
77. When towing a CASA 212, what precautions should be taken with the nose gear?
____________________________________
78. Can pilots determine the brake wear?
a. Yesb.No
79. The accumulator brake pressure is sufficient for approximately _________ applications.
Oxygen
80.
A full main oxygen bottle will provide both pilots with approximately _______ hours
of oxygen supply at ___________ feet with the masks on normal (diluter-demand).
81.
Minimum oxygen cylinder pressure of _________________ psi prevents
Condensationin the bottle and lines.
82.
__________________________________________________
83.
Emergency Equipment & Evacuation
84. Where are the following emergency equipment items located onboard the aircraft?
Crash Axe ________________________
First Aid Kit _____________________________
Fire Extinguisher(s) ________________________________
_______________________________
85. In case of a fire – what part of the fire do you direct the extinguishing agent at?
______________________________________________
86. What else might be regarded as Emergency Equipment? (Bonus Points)
______________________________________________
Page 29
APPENDIX
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DATE:
REVISION:
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2 FEB 2011
0
______________________________________________
______________________________________________
87. There are ______doors and ______ hatch that can be used as emergency exits.
88. When departing the aircraft remember to stay away from the ________________.
89. Always remember to take ______________________ & __________________ with you
Limitations
90. MAX Ramp Weight: ________ lbs.
91. MAX Taxi Weight: __________ lbs.
92. MAX Takeoff Weight: __________ lbs.
93. MAX Landing Weight: __________ lbs.
94. Max. Zero Fuel Weight: __________ lbs.
95. MAX Operating Speed (Vmo): _______ KIAS
96. MAX Inflight Ramp/Cargo Door Speed: _______ KIAS
97. Maneuvering Speed: _______ KIAS
98. Flap Extension Speed (Approach): _______ KIAS
99. Flap Extension Speed (Landing – Full): _______ KIAS
100.
MAX Reverse Speed: _______ KIAS
101.
MAX Demonstrated Crosswind: ________ KIAS
102.
MAX Tail Wind: ______KIAS
103.
MAX Operating Altitude: __________ Ft.
104.
Operating Temperature Range: ______ C, to _______ C.
105.
Landing Lights Use (on the ground):
_______________________________________
106.
Maximum Allowable Torque: __________
107.
108.
PROHIBITED Range of Propeller: _____________
109.
Maximum Airport Elevation for Take Off: __________
_________
Page 30
APPENDIX
PAGE:
DATE:
REVISION:
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2 FEB 2011
0
Ice & Rain Protection
110.
The pneumatic de-ice boots consist of ___________ pneumatically inflated boots
moldedto leading edge of outer wings, vertical and horizontal stabilizers.
111.
a. True
112.
or
b. False
Pneumatic air is ducted to _______ ejector valves. Where are they located?
___________________________________
___________________________________
113.
What heats the lower air intake surface?
__________________________________
114.
What heats the upper air intake surface?
__________________________________
115.
a. Yes
or
b. No
116.
__________ seconds ON and ____________ seconds OFF for 1 minute.
117.
Pitot heat operation is limited to _________ minute with the aircraft stationary.
118.
Where are the propeller de-ice fuses located?
_____________________________________________________
Electrical
119.
120.
(a)
What temperature will cause the battery light to come on?
54° C
(b)
66° C
(c)
25° C
(d)
65° C
(a)
1
(b)
2
(c)
3
(d)
4
Page 31
121.
122.
123.
124.
1A
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2 FEB 2011
0
(a)
(b)
Secondary bus
(c)
Essential bus
(d)
Start bus
(a)
Primary bus
(b)
Secondary bus
(c)
Essential bus
(d)
Start bus
(a)
Primary bus
(b)
Secondary bus
(c)
Essential bus
(d)
Start bus
(a)
Essential master switch
(b)
Secondary master switch
(c)
Bus tie switch
(d)
Bus tie circuit breaker
(a)
When starting with the series/parallel switch in the series position, how many
volts are supplied to that first engine start?
24
(b)
28
(c)
30
(d)
48
125.
126.
127.
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DATE:
REVISION:
Yes No
(a)
Can the battery switches be left on when doing a GPU start?
Yes, they should always be on for a GPU start.
(b)
No, they should never be on for a GPU start.
Page 32
128
129
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(a)
28 VAC
(b)
115 VAC
(c)
400 VAC
(d)
None of the above.
(a) 1
(b)
2
(c)
3
(d)
4
130.
(a)
Loss of all AC instruments
(b)
Turn of all the inverters and then turn them back on one at a time
(c)
Warning light on the warning panel
(d)
None of the above
131.
(a)
If a fault develops on the Essential bus bar will the generators automatically
switch toconnect the Secondary bus bar?
Yes
(b)
No
132.
(a)
24 volts, 22 amps
(b)
28 volts, 200 amps
(c)
30 volts, 300 amps
(d)
None of the above
133.
Yes No
134.
In flight or on the ground, where is the main DC volt indicator taking the voltage From
when the switch is in the center position?
(a) Primary bus
(b)
Secondary bus
(c)
Essential bus
(d)
Start bus
Page 33
135.
(a)
24 volts
(b)
volts
(c)
volts
(d)
volts
136.
(a)
28 volts, 22 amps
(b)
26 volts, 22 amps
(c)
24 volts, 40 amps
(d)
None of the above
137.
(a)
28 volts, 600 amps with 1200 amps overload capacity
(b)
volts, 700 amps with 800 amps intermittent capability
(c)
volts, 500 amps with no intermittent capability
(d)
volts, 800 amps with 1000 overload capability
138.
(a)
28 volts, 22 amps
(b)
23 volts, 7 amps
(c)
28 volts, 7 amps
(d)
22 volts, 22 amps
139.
(a)
140
APPENDIX
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REVISION:
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The generator control (DC control panel) incorporates what forms of generator
protection?
Over voltage, fault, synchronization of frequency
(b)
Ground fault, over voltage, reverse current protection
(c)
Over voltage from APU
(d)
Over temperature and ground fault protection
What percentage of RPM can the Starter-Generator function as a generator and be put
(a)
55%
(b)
60%
(c)
65%
(d)
70%
Page 34
on-line?
141.
APPENDIX
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DATE:
REVISION:
(a)
(b)
(c)
(d)
142.
(a)
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2 FEB 2011
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To provide an artificial over voltage in order to automatically disconnect the generator when it reaches 31
volts.
(b)
To simulate an absence of the ground in the generators.
(c)
To provide an artificial over voltage in order to connect the generator.
(d)
143.
To provide an over intensity in the generator.
(a)
(b)
(c)
(d)
To supply 24 VDC to critical engine instruments during an engine start
Lighting
144.
Position Lights, emergency lights, essential instrument lights, internal lights and
onelanding light are powered through the circuit breakers on the
________________ bus bar.
145.
The Taxi light switch operates the ______ watts wide angle taxi light in the nose
radome.
146.
The Landing light Left & Right operates the _____ watts dual lights in the nose
radome.
147.
Max ground operating time: ______min. ON and _____ min. OFF prevents
overheating.
148.
__________________ and ___________________
Page 35
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CASA 212
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DATE:
REVISION:
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0
SYSTEMS ORAL EXAMINATION
GENERAL
1.
Describe the CASA-212 in general.
2.
3.
Total usable fuel capacity is 528 US gallons.
4.
Max Takeoff Weight is 14,300 lbs.
5.
Max Landing Weight is 13,750lbs.
6.
Max Zero Fuel Weight is 11,847lbs.
7.
Max Allowable Gross Weight is 14,410 lbs.
8.
9.
10.
The aircraft Wing Span is 62 ft and 4 inches.
11.
Aircraft power is provided by 3 onboard batteries and 2 generators.
12.
The highest point of a CASA 200 is 20 ft - 8 inches.
13.
Tire pressure for the CASA 212-100 is:56psi for the main gear and 53psi for the nose tire.
True
True
True
Passed_______ Failed_______
FUEL
1.
Total tank capacity is: 538 gallons, 528 gallons usable.
2.
Inboard total capacity is: 380 gallons, 370 gallons usable.
3.
Outboard total capacity is: 158 gallons, 158 gallons usable.
4.
5.
What type of fuel tanks are they? Integral
6.
4 tanks, in the WINGS
_50 +/ - 5_ psi
7.
Inboard tanks, because of Uneven weight distribution and tilting
8.
How many fuel boost pumps are there? 4
9.
The Fuel Boost pumps are located in the COLLECTOR tanks inside each inboard tank.
10.
True
11. Describe the fuel system & its operation – in general.
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HYDRAULICS
1.
a.BRAKES (Normal & Emergency)
b.NOSEWHEEL STEERING & SHIMMY DAMPENING
c.REAR LOADING DOOR/RAMP
d. FLAPS
2.
Hydraulic fluid type used is: MIL H 5606 B
3.
What is the normal hydraulic system pressure? 2000 psi
4.
What is the hydraulic pump duty cycle? 25 minutes ON and 15minutes OFF.
5.
Release all trapped fluid:
Parking Brake OFF, Flaps UP,
Rear Loading Door – CLOSED, Accumulator Discharged
6.
Yes
7.
The Pressure retained in the Accumulator
8.
Approximately how many braking applications will the normal brake system accumulator give in
the event of a hydraulic failure? 30
9.
Approximate hydraulic system capacity is 11 liters and a reservoir capacity of 7 liters.
10.
so, how?
YES – With Manual Hand pump
11. Describe the basic operations of the Hydraulic system.
FLIGHT CONTROLS
1.
How many flaps on the CASA 212-100?
4
2.
Where are the flaps located? Inboard Trailing Edge of Wings
3.
Which aileron has the trim tab on it? Left
4.
Which tab on the rudder is the trim tab? Lower
5.
Which tab on the elevator is the trim tab? Inboard Left
6.
The flaps are Hydraulically activated and Mechanically actuated.
7.
Which flight control has a single cable system? Rudder
8.
Flaps are doubled slotted with maximum extension of 40 degrees.
9.
Flaps should fully extend or retract within 15 seconds.
10.
Speed limitation for approach flaps: 135 KIAS.
Page 37
APPENDIX
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DATE:
REVISION:
1A
38
2 FEB 2011
0
11. Describe the basic systems and operations of the Flight Control systems.
Passed_______
Failed_______
ENVIRONMENTAL (Heating & Ventilation)
1.
What is the source for cabin heating? P-3 Bleed Air
2.
To insure MAX engine cooling air - and MAX engine power available
3.
Ram air (for ventilation) enters the aircraft through _5_ intakes located on the fuselage.
4.
What areas of the airplane are cooled? CABIN, COCKPIT, RADIO RACK
5. Describe the basic operations of the Environmental systems
Passed_______ Failed______
POWERPLANT
1.
The Garrett TPE331-5 is rated to 776 SHP? True
2.
The main rotating group of the TPE-331 engine consists of a __2__ stage centrifugal
compressor section and a __3__ stage axial turbine section.
3.
At what engine station is the highest pressure? P3
4.
The pressure and temperature of the air, as it passes through the two stage compressor
section will INCREASE.
5.
True
6.
Normal operation of the oil vent valve will be indicated by a sudden rise of _OIL_
PRESSURE at 60% RPM.
7.
During normal start of the -5 engine fuel is supplied to the engine automatically at 10% RPM.
False
8.
ITT limit during start/acceleration is 1149° F for 1 second.
10.
Shutoff Valve armed to open,
Fuel flow to primaries only solenoid valve,
Closes valve to secondary nozzels
11.
Ground start OAT: MIN - 40°C MAX + 55°C.
12.
MAX residual ITT for start is 300° C.
13.
―Light Off‖ time from 10% RPM: GND Start: 10 seconds
14.
The Fuel Purge Accumulator is fully charged at: 95% RPM.
15. Describe the Engine/Powerplant system(s) and its operation(s)
Page 38
Passed_______
APPENDIX
PAGE:
DATE:
REVISION:
1A
39
2 FEB 2011
0
Failed_______
FIRE DETECTION & SUPPRESSION
1.
discharged? If so, how? Yes - AMBER PTT Light
2.
Bottle #1, discharged into # 2 engine.
3.
pressure? Green Disc Cover on left side of engine nacelle is gone/blown out
4.
2, located: Behind the F/O & AFT Cabin near emergency door
5.
True
6. Describe the basic operation of the Fire Detection & Suppressions systems
Passed_______
Failed_______
PROPELLERS
1)
Propeller Governor (PG) Mode: The power lever is forward of Flight Idle.
The Normal RPM range is 96 – 100% True
2)
Beta Mode: In response to movement of the power lever aft of Flight Idle.
RPM range 65 – 97%. True
3)
At about 25 % RPM the Start Lock pins extend as their spring forces overcome
the decreasing centrifugal force.
4)
The locks are disengaged, ―prop off the locks‖, after engine start by moving the Power
Lever to REVERSE.
5)
The Power Lever is mechanically connected to the MANUAL FUEL VALVE
(Fuel Control Unit) and the PROP PITCH CONTROL
6)
The Speed Lever is mechanically connected to the UNDERSPEED GOVERNOR
and the PROP GOVERNOR
7)
MAX reverse speed is: 90 KIAS.
8)
Loss of propeller oil pressure during operation would: FEATHER THE PROPELLOR(S)
9)
NTS is an AUTOMATIC drag reduction system.
10)
What is the unfeathering pump duty cycle? 1 min. ON and 3 min. OFF
11. Describe the Propeller System in general.
Page 39
APPENDIX
PAGE:
DATE:
REVISION:
1A
40
2 FEB 2011
0
Passed_______ FAILED_______
ANNUNCIATOR PANEL LIGHTS
1.
The Red ―BATTERY OVERTEMP‖ light comes on when the battery reaches 66°..
2.
The ―CHIP DETECTOR‖ light is RED colored.
3.
The ―FUEL PRESSURE‖ light comes on when the fuel pressure goes below 3.5psi and goes
back out when the pressure goes above 7.0 psi.
4.
The ―OVERLOAD START RELAY‖ light is RED colored.
5. Describe the Annunciator Panel lights in general
LANDING GEAR AND BRAKES
1.
Nose wheel is steerable through 45° either side of center.
2.
The CASA-212 has oleo - pneumatic type shock struts.
3.
Disconnect the scissors linkage with the 2 pins
4.
Can pilots determine the brake wear? Yes
5.
The accumulator brake pressure is sufficient for approximately 30 applications.
6.
Describe the Landing Gears & Brakes in general
Passed_______
Failed_______
OXYGEN
1.
A full main oxygen bottle will provide both pilots with approximately 6 hours
of oxygen supply at 20,000’ feet with the masks on normal (diluter-demand)
2.
Minimum oxygen cylinder pressure of 280 psi prevents Condensation in the bottle and lines
3.
Why is the oxygen system so important in the CASA 212? The aircraft is unpressurized
4.
5.
Describe the Oxygen system in general
Passed_______
Failed_______
Page 40
APPENDIX
PAGE:
DATE:
REVISION:
1A
41
2 FEB 2011
0
EMERGENCY EQUIPMENT & EVACUATION
1.
Where are the following emergency equipment items located onboard the aircraft?
Crash Axe - lower right of the Captain
First Aid Kit - Left side of the Captain
Fire Extinguisher(s) Behind the First Officer & Right rear of the Cargo area
2. In case of a fire – what part of the fire do you direct the extinguishing agent at? The Base of the fire
3.
GPS, Iridium Sat-Com Phone, Map & Compass
4.
There are 4 doors and 1 hatch that can be used as emergency exits
5.
When departing the aircraft remember to stay away from the propellers
6.
Always remember to take Fellow Crew Members & Emergency Equipment with you
as you exit the airplane in an emergency
7. Describe the Emergency Equipment & Evacuation Procedures in general
Passed_______
Failed_______
LIMITATIONS
1.
MAX Ramp Weight: 14, 410 lbs.
2.
MAX Taxi Weight: 14,300 lbs.
3.
MAX Takeoff Weight: 14,300 lbs.
4.
MAX Landing Weight: 13,750 lbs.
5.
Max. Zero Fuel Weight:11,847 lbs.
6.
MAX Operating Speed (Vmo): 202 KIAS
7.
MAX Inflight Ramp/Cargo Door Speed: 170 KIAS
8.
Maneuvering Speed: 146 KIAS
9.
Flap Extension Speed (Approach): 135 KIAS
10.
Flap Extension Speed (Landing – Full): 115 KIAS
11.
MAX Reverse Speed: 90 KIAS
12.
MAX Demonstrated Crosswind: 20 KIAS
13.
MAX Tail Wind: 10 KIAS
14.
MAX Operating Altitude: 25,000 Ft.
15.
Operating Temperature Range: +54° C, to +40° C.
16.
Landing Lights Use (on the ground): 5 Min ON – 5 Min off
17.
Maximum Allowable Torque: 100.0%
18.
19.
PROHIBITED Range of Propeller: 18% - 28%
20.
Maximum Airport Elevation for Take Off: 8,000’
Passed_______
106%
Failed_______
Page 41
APPENDIX
PAGE:
DATE:
REVISION:
1A
42
2 FEB 2011
0
ICE & RAIN PROTECTION
1.
The pneumatic de-ice boots consist of 7 pneumatically inflated bootsmolded to leading edge
of outer wings, vertical and horizontal stabilizers.
2.
True
3.
Pneumatic air is ducted to 5 ejector valves. Where are they located? 2 in each wing
and 1 in the tail group
4.
What heats the lower air intake surface? Hot Bleed Air
5.
What heats the upper air intake surface? Warm Engine Gearbox Oil
6.
7.
Yes
10 seconds ON and 10seconds OFF for 1 minute.
8.
Pitot heat operation is limited to 1 minute with the aircraft stationary.
9.
Where are the propeller de-ice fuses locate?
Inside the crew access door – upper right hand side of the bulkhead
10. Describe the Ice & Rain Protection system in general
Passed_______
Failed_______
Page 42
APPENDIX
PAGE:
DATE:
REVISION:
1A
43
2 FEB 2011
0
ELECTRICAL
1.
What temperature will cause the battery Overtemp light to come on?
66° C
2.
3.
What bus-bar is connected to the auxiliary battery? Auxiliary or primary bus
4.
The starter-generators feed into parallel into which bus-bar? Secondary bus
5.
Which bus-bar is fed by the No. 1 battery? Essential bus
6.
7.
3
Bus Tie Switch
supplied to that first engine start? 48 volts in series
8.
Yes
9.
Can the battery switches be left on when doing a GPU start?
No, they should never be on for a GPU start
10.
What is the voltage rating of the inverters? 115 VAC
11.
How many inverters are on the CASA 212? 3
12.
How can we determine if an inverter has failed? Warning light on the warning panel
13.
If a fault develops on the Essential bus bar will the generators automatically switch to connect the
Secondary bus bar?
No
14.
The capacity of the two starter generators on the CASA 212 is? 30 volts & 300 amps
15.
Is it possible to start both engines with 48 volts (series)? Yes
16.
In flight or on the ground, where is the main DC volt indicator taking the voltage from when the
switch is in the center position? Essential bus
17.
The minimum battery voltage prior to start: 23 volts
18.
The capacity of batteries 1 and 2 are: 24 volts, 40 amps
19.
28 volts, 600 amps with 1200 amps overload capacity
20.
The power output of the aux battery is: 24 volts, 7 amps
21.
The generator control (DC control panel) incorporates what forms of generator protection?
22.
What percentage of RPM can the Starter-Generator function as a generator and be put on-line?
65%
23.
24.
To provide an artificial over voltage in order to automatically disconnect the generator
when it reaches 31 volts.
Page 43
25.
APPENDIX
PAGE:
DATE:
REVISION:
1A
44
2 FEB 2011
0
To supply 24 VDC to critical engine instruments during an engine start
26.
Describe the electrical system in general
LIGHTING
1.
Position Lights, emergency lights, essential instrument lights, internal lights and one landing
light are powered through the circuit breakers on the28 VDC ESSential bus bar.
2.
The Taxi light switch operates the 150 watts wide angle taxi light in the nose radome.
3.
The Landing light Left & Right operates the 250 watts dual lights in the nose radome.
4.
Max ground operating time: 5 Min. ON and 5 Min. OFF prevents overheating.
5.
COCKPIT and HALL
6. Describe the basic operations of the aircraft lighting system(s)
Passed________
Failed_______
AVIONICS & FLIGHT INSTRUMENTS
1. On the CASA-212, there are 6 static ports. One from each side of the aircraft is integrated
into the respective side Pitot Tube
2. The overspeed sensor receives its pitot static information from the First Officer’s side pitot
static system
3. Pitot Tube heating is supplied by the #1 ESS Bus Bar & the #2 Secondary Bus Bar
4. In the event that we lose the primary static source can we select an alternate or back-up source?
YES
5. In this aircraft the difference between IAS & CAS is negligible. TRUE
6. If the #1 DG/Compass systems fails – a Compass Selector switch will allow the Co-Pilot’s
data to supply the Captain’s HIS info
7. Explain the basics of the _________GPS System
8. Explain the basics of the Blue Sky Tracking System
9. Describe the basics of the Avionics Systems of the CASA-212.
Passed_______
Failed_______
Page 44
APPENDIX
PAGE:
DATE:
REVISION:
1A
45
2 FEB 2011
0
WEIGHT & BALANCE & PERFORMANCE
1. What are the usual fore and aft limits of the center of Gravity? 16 to 30
2. As you burn fuel the center of gravity shifts FORWARD
3. What are the usual factors in computing a day’s flight performance statistics of V1/Vr& V2
Altitude, Temperature, Weight
4. The day of the flight check ride - Given a weight & balance sheet and the day’s particular
information – determine the C.G.s of the airplane before takeoff and at the expected landing time.
5. The day of the flight check ride – Given the days particular information – determine specific
information from the appropriate charts regarding aircraft performance for that flight and fill out a
Take Off or Landing Data card (TOLD).
Final Grade: Passed_______ Failed_______
Instructor: ____________________________
Page 45
GROUND TRAINING EXAM ANSWERS
APPENDIX
PAGE:
DATE:
REVISION:
1B
1
2 FEB 2011
0
Appendix 1 B
ANSWERS TO THE CASA 212 WRITTEN EXAMINATION
Table of Contents
Subject
Sect. Page
EA.1
2
Flight Controls
EA.2
3
Heating & Vent.
EA.3
4
Fuel System
EA.4
5
General
EA.5
6
Hydraulics
EA.6
7
Lndg Gear & Brakes
EA.7
8
Oxygen
EA.8
9
Annunciator
EA.9
10 Fire Detection & Suppresion
EA.10 11 Powerplant
EA.11 12 Propellers
EA.12 13 Emergency Equipment
EA.13 14 Emergency Evacuation
EA.14 15 Emergency Procedures
EA.15 16 Ice & Rain
EA.16 17 Operations Limitations
EA.17 18 Performance & Planning
EA.18 19 Wt. & Balance
EA.19 20 Electrical
EA.20 24 Flight Instruments
EA.21 25 Lighting
Page 1
APPENDIX
PAGE:
DATE:
REVISION:
EA.1
Flight Controls Exam Answers
1.
How many flaps on the CASA 212?
2.
Where are the flaps located? Inboard Trailing Edge of Wings
3.
Which aileron has the trim tab on it? Left
4.
Which tab on the rudder is the trim tab?
a.
Upper
b.
Lower
4
5.
Which tab on the elevator is the trim tab? Inboard Left
6.
The flaps are Hydraulically activated and Mechanically actuated.
7.
Which flight control has a single cable system?
e.
f.
g.
h.
1B
2
2 FEB 2011
0
Ailerons
Rudder
Flaps
Elevators
8.
Flaps are doubled slotted with maximum extension of 40 degrees.
9.
Flaps should fully extend or retract within 15 seconds.
10.
Speed limitation for approach flaps: 135 KIAS.
Page 2
APPENDIX
PAGE:
DATE:
REVISION:
EA.2
CASA 212
1.
What is the source for cabin heating? Bleed Air
2.
1B
3
2 FEB 2011
0
HEATING & VENTILATION EXAM ANSWERS
TO insure MAX engine cooling air - and MAX engine power available
3.
Ram air (for ventilation) enters the aircraft through _5_ intakes located on the fuselage.
4.
What areas of the airplane are cooled?
__CABIN, COCKPIT, RADIO RACK__
Page 3
APPENDIX
PAGE:
DATE:
REVISION:
EA.3
CASA 212
1.
Total tank capacity is: ___538___ gallons, ___528_____ gallons usable.
2.
Inboard total capacity is: ___380__ gallons, ___370____ gallons usable.
3.
Outboard total capacity is: __158__ gallons, ___158___ gallons usable.
4.
1B
4
2 FEB 2011
0
FUEL SYSTEM EXAM ANSWERS
___4__ tanks, in the ___WINGS__
5.
What type of fuel tanks are they?
d. Composite
e. Bladder
f. Integral
6.
_50 +/ - 5_ psi
7.
__Inboard__ tanks, because of __Uneven weight distribution and tilting__
8.
How many fuel boost pumps are there? ___4___
9.
The Fuel Boost pumps are located in the _COLLECTOR_ tanks inside each inboard tank.
10.
c. True
d. False
Page 4
APPENDIX
PAGE:
DATE:
REVISION:
1B
5
2 FEB 2011
0
EA.4
CASA 212
AIRCRAFT GENERAL EXAM
1.
2.
Total usable fuel capacity is ____528______ US gallons.
3.
Max Takeoff Weight is ____16,976______ lbs.
4.
Max Landing Weight is ___16,424_______ lbs.
5.
Max Zero Fuel Weight is __15,653_______lbs.
6.
Max Allowable Gross Weight is 14,410__ lbs.
7.
8.
9.
The aircraft Wing Span is ___62__ ft and __4___ inches.
10.
Aircraft power is provided by __3___ onboard batteries and __2___ generators.
11.
The highest point of a CASA 212 is _20__ ft and __8_ inches.
12.
Tire pressure for the CASA 212-100 is _56_psi for the main gear
True or False
True or False
True or False
and _53 _ psi for the nose tire.
Page 5
EA.5
CASA 212
1.
e.
f.
g.
h.
APPENDIX
PAGE:
DATE:
REVISION:
1B
6
2 FEB 2011
0
HYDRAULICS EXAM ANSWERS
_BRAKES__(Normal & Emergency)
_NOSEWHEEL STEERING & SHIMMY DAMPENING
_REAR LOADING DOOR/RAMP
_FLAPS
2.
Hydraulic fluid type used is: MIL H 5606 B
3.
What is the normal hydraulic system pressure? 2000 psi
4.
What is the hydraulic pump duty cycle? _25_ minutes ON and _15_ minutes OFF.
5.
Release all trapped fluid, Parking Brake OFF, Flaps UP, Rear Loading Door – CLOSED,
Accumulator Discharged
6.
c. Yes
d. No
7.
The Pressure retained in the Accumulator
8.
Approximately how many braking applications will the normal brake system accumulator give in
the event of a hydraulic failure?
a. 10
b. 20
c. 30
d. 40
9.
Approximate hydraulic system capacity is _11_ liters and a reservoir capacity of _7_
liters.
10.
so, how?
YES – With Manual Hand pump
Page 6
APPENDIX
PAGE:
DATE:
REVISION:
1B
7
2 FEB 2011
0
EA.6
CASA 212
LANDING GEAR AND BRAKES EXAM
1.
Nose wheel is steerable through _____45____ degrees either side of center.
2.
CASA 212 has __Oleo___ - __Pneumatic____ type shock struts.
3.
__Disconnect the scissors linkage with the 2 pins___
4.
Can pilots determine the brake wear?
c. Yes
d. No
5.
The accumulator brake pressure is sufficient for approximately __30_ applications.
Page 7
EA.7
APPENDIX
PAGE:
DATE:
REVISION:
1B
8
2 FEB 2011
0
OXYGEN EXAM ANSWERS
3.
A full main oxygen bottle will provide both pilots with approximately _6__ hours
of oxygen supply at _20,000_ feet with the masks on normal (diluter-demand).
2.
Minimum oxygen cylinder pressure of __280__ psi prevents condensation
in the bottle and lines.
5.
6.
___The Cabin Is Unpressurized___
___To keep smoke/fumes from getting into the supply of oxygen___
Page 8
EA.8
CASA 212
APPENDIX
PAGE:
DATE:
REVISION:
1B
9
2 FEB 2011
0
ANNUNCIATOR PANEL LIGHTS EXAM ANSWERS
10. The ―GENERATOR‖ Light comes on when the affected generator _Drops Off Line_.
11. Battery No. Temp Light is __AMBER__ (color) and comes on when the battery temp goes above
_54__ degrees.
12. The Fuel Level light comes on when the fuel level in the collector tank goes below _120__
pounds of fuel.
13. The ―CHIP DETECTOR‖ light is __RED__ (Color) and comes on when __metal__ is detected.
14. The ―UNSAFE DOOR‖ light is __RED__ colored.
15. ―ENGINE FIRE‖ light is __RED__colored.
16. The ―BAGGAGE COMPARTMENT SMOKE‖ light is __RED__ colored.
Page 9
APPENDIX
PAGE:
DATE:
REVISION:
1B
10
2 FEB 2011
0
EA.9
CASA 212
FIRE DETECTION & SUPPRESSION EXAM ANSWERS
1.
discharged? If so, how?
Yes – No How: ___ AMBER PTT Light__
2.
Bottle # ___1__, discharged into _# 2 __ engine.
3.
pressure?
____Green Disc Cover on left side of engine nacelle is gone/blown out____
4.
__2_, located: __Behind the F/O & AFT Cabin near emergency door__
5.
c. True
d. False
Page 10
EA.10 CASA 212
APPENDIX
PAGE:
DATE:
REVISION:
1B
11
2 FEB 2011
0
POWERPLANT EXAM ANSWERS
1.
The Garrett TPE331-5 is rated to 776 SHP? a. True
2.
The main rotating group of the TPE-331 engine consists of a __2__ stage centrifugal
compressor section and a __3__ stage axial turbine section.
3.
At what engine station is the highest pressure? P3
4.
The pressure and temperature of the air, as it passes through the two stage compressor section
will _INCREASE.
5.
a. True
6.
Normal operation of the oil vent valve will be indicated by a sudden rise of __OIL__
__PRESSURE__ at 60% RPM.
7.
During normal start of the -5 engine fuel is supplied to the engine automatically at 10% RPM.
b. False
8.
ITT limit during start/acceleration is _1149_ C / for _1_ second.
9.
__Shutoff Valve armed to open__, _
_Fuel flow to primaries-only solenoid valve__
__Closes valve to secondary nozzels__.
11.
Ground start OAT: MIN - _40_ C, MAX + _55__ C.
12.
MAX residual ITT for start is _300_ C.
13.
―Light Off‖ time from 10% RPM: GND Start: _10_seconds
14.
The Fuel Purge Accumulator is fully charged at: _95_% RPM.
Page 11
EA.11 CASA 212
APPENDIX
PAGE:
DATE:
REVISION:
1B
12
2 FEB 2011
0
PROPELLERS EXAM ANSWERS
1. Propeller Governor (PG) Mode: The power lever is forward of Flight Idle.
The RPM range is 96 – 100%
a. True
or
b. False
2. Beta Mode: In response to movement of the power lever aft of Flight Idle.
RPM range 65 – 97%.
a. True
or
b. False
3. At about __25_ % RPM the Start Lock pins extend as their spring forces overcome the
decreasing centrifugal force.
4. The locks are disengaged, ―prop off the locks‖, after engine start by moving the Power Lever to
__REVERSE__.
5. The Power Lever is mechanically connected to the __MANUAL FUEL VALVE
Unit) and the _PROP PITCH CONTROL_.
(Fuel Control
6. The Speed Lever is mechanically connected to the _UNDERSPEED GOVERNOR_ and the
_PROP GOVERNOR__.
7. MAX reverse speed is: _90_ KIAS.
8. Loss of propeller oil pressure during operation would: _FEATHER THE PROPELLOR(S)_.
9. NTS is an _AUTOMATIC_ drag reduction system.
10. What is the unfeathering pump duty cycle?
__1_ min. ON and _3_ min. OFF
Page 12
EA.12 CASA 212
1.
APPENDIX
PAGE:
DATE:
REVISION:
1B
13
2 FEB 2011
0
EMERGENCY EQUIPMENT EXAM ANSWERS
Where are the following emergency equipment items located onboard the aircraft?
Crash Axe _On floor mount by the Captain’s seat__
First Aid Kit
_To the left (rear) of the Captain’s seat____
Fire Extinguisher(s) _Behind the Co-Pilots seat_________
__Right rear section of the airplane – cargo exit_
2.
In case of a fire – what part of the fire do you direct the extinguishing agent at?
____At the BASE of the flames__________
3.
___Iridium Cell Phone___________________
__GPS Unit____________________________
__Map & Compass______________________
Page 13
EA.13 CASA 212
APPENDIX
PAGE:
DATE:
REVISION:
1B
14
2 FEB 2011
0
EMERGENCY EVACUATION EXAM ANSWERS
1.
There are ___4__doors and ___1___ hatch that can be used as emergency exits.
2.
When departing the aircraft remember to stay away from the _propellers____.
3.
Always remember to take _fellow crew members_ & _emergency equipment_ with you
Page 14
EA.14 CASA 212
5.
APPENDIX
PAGE:
DATE:
REVISION:
EMERGENCY PROCEDURES EXAM ANSWERS
The Memory items to ENGINE FIRE ON THE GROUND are:
_Emergency Shutdown Lever____
_FUEL__Switch______________
_GENERATOR Switch________
_OFF_
_OFF_
_OFF_
_Engine Fire Discharge Switches_
6.
1B
15
2 FEB 2011
0
_OFF_
The Memory items to
ENGINE FAILURE DURING TAKEOFF – ABORTED TAKEOFF are:
_Power Levers___________________
_Flight Idle__
_Control Column_________________
_Full Forward
_Power Levers___________________
_Ground Idle_
_Steer With Rudder____________
_Nose Wheel Steering Below 60 KIAS_
7.
_Brakes________________________
_As Required_
_Reverse_______________________
_As Required_
The Memory items to ELECTRICAL FIRE IN FLIGHT are:
_Oxygen Masks__ ______________
_ON/100%____
_Oxygen Main Line Valve________
_OPEN_______
_Smoke Goggles________________
8.
_ON_________
The Memory items for BATTERY OVERTEMP WARNING are:
_Affected Battery________________
_Identify_________
_Battery Switch(s)________________
_OFF____________
Page 15
APPENDIX
PAGE:
DATE:
REVISION:
1B
16
2 FEB 2011
0
EA.15 CASA 212 ICE & RAIN PROTECTION EXAM
1.
The pneumatic de-ice boots consist of __7__ pneumatically inflated boots molded to leading
edge of outer wings, vertical and horizontal stabilizers.
2.
a. True
3.
or
b. False
Pneumatic air is ducted to __5__ ejector valves. Where are they located?
___2 in each wing___
___1 in the tail group___
4.
What heats the lower air intake surface? __HOT BLEED AIR___
5.
What heats the upper air intake surface? __WARM ENGINE GEARBOX OIL__
6.
7.
a. Yes
or
b. No
__10__ seconds ON and __10__ seconds OFF for 1 minute.
8.
Pitot heat operation is limited to __1__ minute with the aircraft stationary.
9.
Where are the propeller de-ice fuses located?
__Upper right hand side of the bulkhead, inside crew access door__
Page 16
EA.16 CASA 212
APPENDIX
PAGE:
DATE:
REVISION:
1B
17
2 FEB 2011
0
AIRCRAFT OPERATIONS LIMITATIONS EXAM ANSWERS
1.
MAX Ramp Weight: __14,410__ lbs.
2.
MAX Taxi Weight: __14,410__ lbs.
3.
MAX Takeoff Weight: __14,300__ lbs.
4.
MAX Landing Weight: __13,750__ lbs.
5.
Max. Zero Fuel Weight: __11,847__ lbs.
6.
MAX Operating Speed (Vmo): __200__ KIAS
7.
MAX Inflight Ramp/Cargo Door Speed: __170__ KIAS
8.
Maneuvering Speed: __146__ KIAS
9.
Flap Extension Speed (Approach): __135__ KIAS
10.
Flap Extension Speed (Landing – Full): __115__ KIAS
11.
MAX Reverse Speed: __90__ KIAS
12.
MAX Demonstrated Crosswind: __20__ KIAS
13.
MAX Tail Wind: __10__KIAS
14.
MAX Operating Altitude: ___25,000__ Ft.
15.
Operating Temperature Range: __+54__ C, to __-40__ C.
16.
Landing Lights Use (on the ground): 5 Minutes ON, 5 Minutes OFF (Cooling)
17.
Maximum Allowable Torque: __100.0%__
18.
19.
PROHIBITED Range of Propeller: __18% - 28% RPM__
20.
Maximum Airport Elevation for Take Off: __8,000’__
__106.0__
Page 17
EA.17 CASA 212
1.
1B
18
2 FEB 2011
0
PERFORMANCE & PLANNING EXAM ANSWERS
At the airports from which we operate, which condition is the most limiting?
a. Takeoff Runway length
2.
APPENDIX
PAGE:
DATE:
REVISION:
or
b. Climb Gradient
Which segment of the takeoff flight path are we most weight limited?
__SECOND SEGMENT__
3.
In our performance planning _Temperature__, __Altitude____,
and ___Aircraft weight__ are all factors in computing V1/Vr – V2 & Vref.
Page 18
EA.18 CASA 212
APPENDIX
PAGE:
DATE:
REVISION:
1B
19
2 FEB 2011
0
WEIGHT & BALANCE EXAM ANSWERS
1.
What is the usual forward & aft C.G. limits?
2.
MAX Taxi Weight? __14,410_ lbs.
3.
MAX Takeoff Weight? __14,300__ lbs.
4.
MAX Zero Fuel Weight? __11,847__ lbs.
5.
MAX Landing Weight? __13,750_ lbs.
__16__ to __30__
6.
Each multi-engine aircraft operated by the Company will be weighed at intervals not to exceed
__36__ calendar months.
7.
As you burn fuel - the Center of Gravity of the airplane shifts _Forward_
Page 19
EA.19 CASA-212
1.
Primary bus
Secondary bus
Essential bus
Start bus
Primary bus
Secondary bus
Essential bus
Start bus
a.
b.
c.
d.
7.
Secondary bus
Essential bus
Start bus
a.
b.
c.
d.
6.
1
2
3
4
a.
b.
c.
d.
5.
54 C
66 C
25 C
65 C
a.
b.
c.
d.
4.
ELECTRICAL SYSTEM EXAM ANSWERS
a.
b.
c.
d.
3.
1B
20
2 FEB 2011
0
What temperature will cause the battery overtemp light to come on?
a.
b.
c.
d.
2.
APPENDIX
PAGE:
DATE:
REVISION:
Essential master switch
Secondary master switch
Bus tie switch
Bus tie circuit breaker
supplied to that first engine start?
a.
b.
c.
d.
24
28
30
48
Page 20
8.
APPENDIX
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DATE:
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1B
21
2 FEB 2011
0
a. Yes
b. No
9.
Can the battery switches be left on when doing an APU start?
a. Yes, they should always be on for an APU start.
b. No, they should never be on for an APU start.
10.
a.
b.
c.
d.
11.
a.
b.
c.
d.
12.
28 VAC
115 VAC
400 VAC
None of the above.
1
2
3
4
a.
b.
c.
d.
Loss of all AC instruments
Turn of all the inverters and then turn them back on one at a time
Warning light on the warning panel
None of the above
13.
If a fault develops on the Essential bus bar will the generators automatically switch to connect
the Secondary bus bar?
14.
a. Yes
b. No
a.
b.
c.
d.
15.
24 volts, 22 amps
28 volts, 200 amps
30 volts, 300 amps
None of the above
a. Yes
b. No
Page 21
APPENDIX
PAGE:
DATE:
REVISION:
1B
22
2 FEB 2011
0
16.
In flight or on the ground, where is the main DC volt indicator taking the voltage from when the
switch is in the center position?
a.
b.
c.
d.
17.
a.
b.
c.
d.
18.
Primary bus
Secondary bus
Essential bus
Start bus
24 volts
28 volts
23 volts
15 volts
a.
b.
c.
d.
28 volts, 22 amps
26 volts, 22 amps
24 volts, 40 amps
None of the above
19.
20.
a. 28 volts, 600 amps with 1200 amps overload capacity
b. 24 volts, 700 amps with 800 amps intermittent capability
c. 48 volts, 500 amps with no intermittent capability
d. 22 volts, 800 amps with 1000 overload capability
21.
b. 24 volts, 7 amps
c. 28 volts, 7 amps
d. 24 volts, 22 amps
The generator control (DC control panel) incorporates what forms of generator protection?
a.
b.
c.
d.
22.
Over voltage, fault, synchronization of frequency
Over voltage from APU
Over temperature and ground fault protection
What percentage of RPM can the Starter-Generator function as a generator and be put
a.
b.
c.
d.
55%
60%
65%
70%
Page 22
on-line?
23.
1B
23
2 FEB 2011
0
a.
b.
c.
d.
24.
APPENDIX
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DATE:
REVISION:
a. To provide an artificial over voltage in order to automatically disconnect the generator
when it reaches 31 volts.
b. To simulate an absence of the ground in the generators.
c. To provide an artificial over voltage in order to connect the generator.
d. To provide an over intensity in the generator.
25.
a.
b.
c.
d.
To supply 24 VDC to critical engine instruments during an engine start.
Page 23
EA.20 CASA 212
APPENDIX
PAGE:
DATE:
REVISION:
1B
24
2 FEB 2011
0
FLIGHT INSTRUMENTS EXAM ANSWERS
1.
On the CASA 212, there are _6_ static ports of which one on each side is integrated in the
__PITOT TUBE__ .
2.
The overspeed sensor receives its pitot static information from the:
a. Captain’s side
or
b. First Officer’s side
pitot static system?
3.
Pitot tube heating is electrical through what bus bar(s)?
___#1 ESS BUS BAR___, __#2 SEC BUS BAR__
4.
In the event that we lose static source, we can select a back-up source in the cockpit?
b. True or b. False
5.
The difference between IAS and CAS is negligible throughout the speed range of the
aircraft?
a. True
6.
or
b. False
What is the purpose of Pitot Heat in the CASA 212?
__For Operations in moisture/Precip as well as actual icing conditions__
7.
If the #1 DG/Compass systems fails – a __COMPASS SELECTOR__ switch will allow the
copilot’s data to supply the pilots HSI.
8.
The CASA 212 is equipped with _2_ identical, but independent remote sensing compass
system(s).
Page 24
EA.21 CASA-212
APPENDIX
PAGE:
DATE:
REVISION:
1B
25
2 FEB 2011
0
LIGHTING SYSTEM EXAM ANSWERS
1.
Position Lights, emergency lights, essential instrument lights, internal lights and one landing light
are powered through the circuit breakers on the __28 VDC ESS__ bus bar.
2.
The Taxi light switch operates the _150_ watts wide angle taxi light in the nose radome.
3.
The Landing light Left & Right operates the _250_ watts dual lights in the nose radome.
4.
Max ground operating time: _5_min. ON and _5_ min. OFF prevents overheating.
5.
__COCKPIT__ and __HALL__
Page 25
POWERPOINT PRESENTATION
APPENDIX
PAGE:
DATE:
REVISION:
2
1
2 FEB 2011
0
APPENDIX 2
POWERPOINT PRESENTATIONS
The following is a list of the PowerPoint presentations that accompany the CASA 212 course.
The printed hard copy of this course has a DVD included with the presentations.
The software copy includes links to the actual presentations.
Day 1—
Environmental
Flight Controls
Fuel
General Information
Introduction to the Organization
Organization Chart
Day 2—
Engines
Fire Detection and Suppression
Annunciator Lights
Day 3—
Normal and Emergency Procedures
Checklists and QRH
Deicing
Emergency Equipment
Limitations
Wt. & Bal and Performance
Day 4—
Blue Sky Tracker
Differences
Electrical and Lighting
Crew Duties and Responsibilities
Page 1
QUICK REFERENCE HANDBOOK
APPENDIX
PAGE:
DATE:
REVISION:
3
1
2 FEB 2011
0
APPENDIX 3
Performance and Checklists
The following pages show copies of the QRH. This handbook has the Normal, Abnormal,
and Emergency checklists, as well as a quick reference to performance.
Page 1
APPENDIX
PAGE:
DATE:
REVISION:
3
2
2 FEB 2011
0
Page 2
APPENDIX
PAGE:
DATE:
REVISION:
3
3
2 FEB 2011
0
Page 3
APPENDIX
PAGE:
DATE:
REVISION:
3
4
2 FEB 2011
0
Page 4
APPENDIX
PAGE:
DATE:
REVISION:
3
5
2 FEB 2011
0
Page 5
APPENDIX
PAGE:
DATE:
REVISION:
3
6
2 FEB 2011
0
Page 6
APPENDIX
PAGE:
DATE:
REVISION:
3
7
2 FEB 2011
0
Page 7
APPENDIX
PAGE:
DATE:
REVISION:
3
8
2 FEB 2011
0
Page 8
APPENDIX
PAGE:
DATE:
REVISION:
3
9
2 FEB 2011
0
Page 9
APPENDIX
PAGE:
DATE:
REVISION:
3
10
2 FEB 2011
0
Page 10
APPENDIX
PAGE:
DATE:
REVISION:
3
11
2 FEB 2011
0
Page 11
APPENDIX
PAGE:
DATE:
REVISION:
3
12
2 FEB 2011
0
Page 12
APPENDIX
PAGE:
DATE:
REVISION:
3
13
2 FEB 2011
0
Page 13
APPENDIX
PAGE:
DATE:
REVISION:
3
14
2 FEB 2011
0
Page 14
APPENDIX
PAGE:
DATE:
REVISION:
3
15
2 FEB 2011
0
Page 15
APPENDIX
PAGE:
DATE:
REVISION:
3
16
2 FEB 2011
0
Page 16
APPENDIX
PAGE:
DATE:
REVISION:
3
17
2 FEB 2011
0
Page 17
APPENDIX
PAGE:
DATE:
REVISION:
3
18
2 FEB 2011
0
Page 18
APPENDIX
PAGE:
DATE:
REVISION:
3
19
2 FEB 2011
0
Page 19
APPENDIX
PAGE:
DATE:
REVISION:
3
20
2 FEB 2011
0
Page 20
APPENDIX
PAGE:
DATE:
REVISION:
3
21
2 FEB 2011
0
Page 21
SUBPART
PAGE:
DATE:
REVISION:
B
1
2 FEB 2011
0
SUBPART ‘B’
CASA 212 FLIGHT TRAINING
Page 1
APPENDIX
PAGE:
DATE:
REVISION:
1
2 FEB 2011
0
APPENDIX
CASA 212 AIRCRAFT OPERATING MANUAL
[NOTE: It is common practice on some aircraft types to divide the AOM into AOM 1 and AOM 2 for line
operations and training. AOM-1 usually contains the standard items for everyday operations such as the
checklists, expanded checklists, and the normal, abnormal, irregular, and emergency procedures.
AOM-2 usually contains systems diagrams and explanations and flight maneuver pictorials and
explanations.
An example can be found in the Ryan manuals for the 757 and 767. There is a CPM ( Cockpit
Procedures Manual), AOM-1, and AOM-2. This splitting of the master AOM is designed to reduce cockpit
clutter and ease finding additional information by having the minimum necessary manual immediately
accessible to the pilot.
We can split the CASA manual like this. It would be much easier to do that now and then we would not
have to re-write FOTM-3. References can be made now to AOM-1 and AOM-2. This manual may be
small enough that splitting is not necessary, however the next aircraft types will benefit from this and it
would be good to standardize. It should not add to our manual creation time as we are only creating two
parts of one approved manual.]
Page 1

flight operations training manual—part three

Transcription

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