Ground - Course Cessna 172S Skyhawk C 172S

Transcription

Ground - Course Cessna 172S
Skyhawk
C 172S
Ground-Course Cessna 172S
© 2004 FSB / Basel
*
1
AFM
•
Design
10 Sections
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Section 1
Section 2
Section 3
Section 4
Section 5
Section 6
Section 7
GENERAL
LIMITATIONS
EMERGENCY PROCEDURES
NORMAL PROCEDURES
PERFORMANCE
WEIGHT and BALANCE
DESCRIPTION and
OPERATION of the
AIRPLANE and its SYSTEMS
Handling, Servicing and
Maintenance
SUPPLEMENTS
OPERATING TIPS
Section 8
Section 9
Section 10
© 2004 FSB / Basel
2
Dimensions
Structure
Maneuver Limits
© 2004 FSB / Basel
3
Dimensions
• Höhe
2.71 m
8' 11"
11.00 m
36' 1"
• Länge
8.28 m
27' 2"
• Min. Wenderadius
8.23 m
27'
• Spannweite
© 2004 FSB / Basel
4
Structure
•
•
•
•
•
Fuselage
Material
Doors
Baggage Door
Windows
© 2002 FSB / Basel
© 2004 FSB / Basel
Semi-Monocoque
All metal, Aluminium skin
2
1
2
5
Maneuver Limits
Normal Category
Flaps Up +3.8g, -1.52g
FlapsDown +3.0g
Non aerobatic maneuvers only,
Turns with max 60° angle of bank
This includes
Chandelles, Lazy Eights
Steep Turns
Stalls
© 2002 FSB / Basel
© 2004 FSB / Basel
6
Maneuver Limits
Flaps
Approved Takeoff Range
0° - 10°
Approved Landing Range
0° - 30°
© 2002 FSB / Basel
© 2004 FSB / Basel
7
Engine
Oil
Propeller
Fuel and Fuel System
© 2004 FSB / Basel
8
Engine
• Engine Manufacturer
• Model Number
• Type
• Rated Horsepower
• Rated Speed
© 2004 FSB / Basel
Textron Lycoming
IO-360-L2A
4 cylinder opposed
normally aspirated
air cooled
fuel injected
180 HP
2700 RPM
9
Power Plant Limitations
• Horse Power max.
180
• Rotation Speed max.
2700
• Oil Temp (°F) max.
245
• Oil Pressure (PSI) min.
max.
20
115
© 2002 FSB / Basel
© 2004 FSB / Basel
10
Oil
• Oil Capacity (QTS)
8
• Oil Specification
15W50 or 20W50
• Min. for FSB Use (QTS)
6
© 2002 FSB / Basel
© 2004 FSB / Basel
11
Propeller
• Propeller Type
McCauley
• Blades
2 (fixed pitch)
• Diameter
76“ / 186 cm
• Ground clearance
11.25“ / 28 cm
© 2004 FSB / Basel
12
Fuel System
•
•
•
•
•
Capacity Total
Capacity Usable
Capacity Filler Neck Usable
Number of Tanks
Fuel Drains
•
•
•
Fuel Quantity Indicator
less than 5 USG
report failures
Fuel Flow Indicator
Fuel Venting
•
Fuel Selector
© 2002 FSB / Basel
© 2004 FSB / Basel
56 USG
53 USG (2x26.5)
35 USG (2x17.5)
2 (1 in each wing)
13, 5 in each wing, 1 below
engine (fuel strainer), 2 below
fuselage (1 for the selector valve,
1 for the fuel reservoir)
Electrical, Low Fuel Indic (LFI)
LFI message per tank
LFI message, Needle OFF
Electrical
Left tank vented and interconnected with right tank
3 Pos. (Both, Right, Left)
13
Fuel System / Switch
© 2002 FSB / Basel
© 2004 FSB / Basel
14
Fuel System
•
•
•
•
Fuel Pump
Electr. Fuel Pump
Fuel Injection System
Fuel Return System
• Fuel Pressure
• Avgas Minimum Grade
© 2002 FSB / Basel
© 2004 FSB / Basel
Engine driven and Electrical
OFF / ON
Continous Flow
Increased Fuel Flow→lower
fuel temp→lower fuel vapor
Measured near manifold
100LL Blue or 100 Green
15
Fuel System – 13 Drain Valves
5
5
1
1
1
© 2002 FSB / Basel
© 2004 FSB / Basel
16
Fuel System Management
• Avgas Minimum Grade
100LL Blue or 100 Green
• Refueling
Always park airplane in a wings-level, normal
ground attitude and place the fuel selector in the
Left or Right Position.
© 2002 FSB / Basel
© 2004 FSB / Basel
17
Fuel Selector Valve (FSV)
• The FSV should in the BOTH position for takeoff, climb,
landing and maneuvers that involve prolonged slips or skids
of more than 30 seconds.
Operation from LEFT or RIGHT is reserved for the cruise.
• Unequal fuel flow from each tank may occur, when the fuel
selector is on BOTH during cruise and the wings are not
maintained level.
• When the tanks are nearly full and the wings are not level,
some sloshing of fuel between tanks can be expected.
© 2002 FSB / Basel
© 2004 FSB / Basel
18
Leaning Procedure
• No leaning above 75% Power
• Full rich up to 5000ft QNH
• At and above 5000ft in cruise: lean to 75°F
rich of peak, not earlier than 2 minutes after
level off
• During climb full rich up to 7000ft. For climbs
at higher altitudes careful leaning is
acceptable during climb.
© 2002 FSB / Basel
© 2004 FSB / Basel
19
Landing Gear
Brake System
Flight Controls
© 2004 FSB / Basel
20
Landing Gear
• Tricycle
• Non Retractable
• Steerable nose wheel
© 2002 FSB / Basel
© 2004 FSB / Basel
21
Landing Gear
• Tire Pressure
• Struts
© 2002 FSB / Basel
© 2004 FSB / Basel
Nose
Main
Nose
Main
45.0 psi
38.0 psi
45.0 psi
45.0 psi
22
Brakes
• Each main gear wheel is equipped with a
hydraulically actuated disc type brake.
• The brakes are operated by applying pressure to
the top set of rudder pedals.
• To operate the parking brake pull the handle aft
and rotate it 90° down.
© 2002 FSB / Basel
© 2004 FSB / Basel
23
Flight Controls
• System
Cable
• Trim
Elevator Manual
• Flaps
Electrical
10°, 20° or 30°
10 Amps circuit breaker
© 2002 FSB / Basel
© 2004 FSB / Basel
24
Electrical System
© 2004 FSB / Basel
25
Electrical System
• System
28-volt dc
• Battery
24 V
• Alternator Output
60 Amp
belt driven
• Annunciator Panel
Fuel, Oil, Vacuum,
Alternator/Low Volt
© 2002 FSB / Basel
© 2004 FSB / Basel
26
Electrical System
• Master/Avionics Master
• Ammeter
indicates the charging rate to battery
• Circuit Breakers
push to reset
switch/breaker
• External Power Source
Master/Avionics
Master off
© 2002 FSB / Basel
© 2004 FSB / Basel
27
Electrical Schematic
© 2002 FSB / Basel
© 2004 FSB / Basel
28
Circuit Breaker Panel(s)
© 2002 FSB / Basel
© 2004 FSB / Basel
29
Vacuum System
Pitot-Static System
Heating and Ventilation System
© 2004 FSB / Basel
30
Vacuum System
• System
2 Engine Driven Pumps
• Stand-By Pump
NO
• Instruments
AI, DG
• Vacuum Gage
• Low Vac Annunciator L or R VAC, if both L VAC R
© 2002 FSB / Basel
© 2004 FSB / Basel
31
Pitot-Static System
• Instruments served ASI, VSI, ALT
• Pitot Tube (Heated) below left wing
measures total pressure
• External Static Port left side of fuselage
measures static pressure
• Alternate Static Source below throttle
© 2002 FSB / Basel
© 2004 FSB / Basel
32
Alternate Static Source
© 2002 FSB / Basel
© 2004 FSB / Basel
33
Heating and Ventilation System
Heater and Defroster
© 2002 FSB / Basel
© 2004 FSB / Basel
34
Stall Warning
ELT
Intercom
Autopilot
Instrument Panel
© 2004 FSB / Basel
35
Stall Warning
•
Lift Detector
5 - 10
KIAS above Stall Speed
© 2002 FSB / Basel
© 2004 FSB / Basel
36
Emergeny Locator Transmiter
• Position
Behind the aft cabin partition wall
on the right side of the tailcone.
• Operation
Remote switch/annunciator is installed on the copilot‘s panel.
The annunciator illuminates when
the ELT is transmitting.
© 2002 FSB / Basel
© 2004 FSB / Basel
37
© 2002 FSB / Basel
© 2004 FSB / Basel
38
© 2002 FSB / Basel
© 2004 FSB / Basel
39
Intercom
• Intercom
© 2002 FSB / Basel
© 2004 FSB / Basel
Pilot and Co-Pilot
40
Autopilot
• Type
Bendix/King KAP 140
Single Axis (Aileron Control)
• Provisions
wing leveler, heading hold, NAV
track, approach and backcourse
lateral modes
• Interrupt
Autopilot Circuit Breakers or
Avionics Master Off
© 2002 FSB / Basel
© 2004 FSB / Basel
41
Autopilot
© 2002 FSB / Basel
© 2004 FSB / Basel
42
© 2002 FSB / Basel
© 2004 FSB / Basel
43
Mass and Balance
© 2004 FSB / Basel
44
Maximum Mass
(for Normal Category in lbs/kg)
• Max. Ramp Mass
2558 / 1160
• Max. Takeoff Mass
2550 / 1157
• Max. Landing Mass
2550 / 1157
• Max. Mass in Bagg. Comp. Total
Baggage Area 1
Baggage Area 2
200 / 91
120 / 54
50 / 23
© 2002 FSB / Basel
© 2004 FSB / Basel
45
Baggage Areas 1 and 2
© 2004 FSB / Basel
46
Running Basic Empty Mass
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•
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•
Basic Empty Mass
CG
Moment
Zero Fuel Mass
1718 lbs
41.07“
70569
Max Ramp Mass –
Basic Empty Mass =
2558 – 1718 = 840 lbs
• Payload w. Fuel Full
237 kg
© 2002 FSB / Basel
© 2004 FSB / Basel
840 – (53x6) = 522 lbs /
47
© 2002 FSB / Basel
© 2004 FSB / Basel
48
© 2004 FSB / Basel
49
© 2004 FSB / Basel
50
© 2004 FSB / Basel
51
© 2004 FSB / Basel
52
Filler neck + 3 Erwachsene + Gepäck = OK
Input
1.
2.
3.
4.
5.
6.
7.
8.
9.
Basic Empty Weight
Usable Fuel (max 53 USG)
Pilot and Front Passenger
Rear Passengers
Baggage Area 2 (max 120 lbs)
Ramp Mass
Fuel for engine start, taxi, run up
Takeoff Mass
Differenz zu max takeoff mass
© 2004 FSB / Basel
Unit
35.0
155.0
77.5
40.0
0.0
USG
kg
kg
kg
kg
1.3 USG
2550
Mass
lbs
1718
210
342
171
88
0
2529
8
2521
29
Arm
ins
41.1
48.0
37.0
73.0
108.0
123.0
45.6
38.1
45.6
Moment
(Lb-ins/1000)
70.6
10.1
12.6
12.5
9.5
0.0
115.3
0.3
115.0
53
Student + FI + Full Fuel = OK
Input
1.
2.
3.
4.
5.
6.
7.
8.
9.
Basic Empty Weight
Usable Fuel (max 53 USG)
Pilot and Front Passenger
Rear Passengers
Ramp Mass
Fuel for engine start, taxi, run up
Takeoff Mass
Differenz zu max takeoff mass
© 2004 FSB / Basel
Unit
53.0
155.0
0.0
5.0
0.0
USG
kg
kg
kg
kg
1.3 USG
2550
Mass
lbs
1718
318
342
0
11
0
2389
8
2381
169
Arm
ins
41.1
48.0
37.0
73.0
108.0
123.0
41.7
38.1
41.7
Moment
(Lb-ins/1000)
70.6
15.3
12.6
0.0
1.2
0.0
99.7
0.3
99.4
54
Speed Limitations
Stall Speeds
Other Important Speeds
© 2004 FSB / Basel
55
Air Speed Limitations (KIAS)
• VNE
• VNO
• VFE 10° Flaps
10-30° Flaps
• VA 2550 lbs
1900 lbs
• VMAX WINDOW OPEN
• Max. Demo. X-wind
© 2002 FSB / Basel
© 2004 FSB / Basel
163
129
110
85
105
90 (d.h. pro -43lbs/20kg -1kts)
163
15 KTS (not a limitation)
56
Airspeed Indicator Markings
Marking
KIAS
Significance
White Arc
40-85
Green Arc
48-120
Yellow Arc
129-163
Red Line
163
Full Flaps Ops Range. Lower limit is max
weight Vso in landing configuration. Upper
limit is max speed with flaps extended.
Normal Ops Range. Lower limit is max
weight Vs at most forward CG with flaps retracted. Upper limit is max structural cruising speed.
Operation with caution and only in smooth
air.
Max speed for all operations.
© 2002 FSB / Basel
© 2004 FSB / Basel
57
Stall Speeds at 2550 lbs
Power off
Flaps
Setting
0°
KIAS
Angle of Bank
30°
45°
KIAS
KIAS
60°
KIAS
UP
48
52
57
68
10°
43
46
51
61
30°
40
43
48
57
Most Forward Center of Gravity
© 2004 FSB / Basel
58
Other Important Speeds (KIAS)
at max Takeoff Mass
•
•
•
•
•
Vr
Vx
Vy
Vcruise climb
Vfinal app, flaps up
Vfinal app, flaps 30°
• Vshort field, flaps 30°
• Vglide
© 2004 FSB / Basel
55
62
74
80
70
65
61
68
59
ICAO Pattern
Throshold 1.1 - 1.2 x Vso
Initial Final 1.3 x Vso
500 ft AGL
45°
Base 1.5 x Vso
1 NM
Downwind 1.8 x Vso
1000 ft AGL
© 2002 FSB / Basel
© 2004 FSB / Basel
60
Air Speeds for APP (KIAS)
•
•
•
•
•
Initial Approach
Intermediate Approach
Final Approach
Short Final
Threshold
© 2002 FSB / Basel
© 2004 FSB / Basel
85
75
65
60
55
61
Performance
© 2004 FSB / Basel
62
Types of Operation
• VFR Day and Night
YES
• IFR Day and Night
NO
• Icing Conditions
NO
© 2002 FSB / Basel
© 2004 FSB / Basel
63
Altitudes
• Service Ceiling
© 2002 FSB / Basel
© 2004 FSB / Basel
14'000 ft
64
Max demonstrated x-Wind = 15 kts
Heading 220°
Wind
250°/25 KTS
X-Wind 14 KTS
© 2004 FSB / Basel
65
Takeoff: Der Ground Roll beträgt 960ft
2550lbs, SL, standard atm, no wind, hard rwy
© 2004 FSB / Basel
66
Rate of Climb at 2550 lbs
© 2004 FSB / Basel
67
Von SL auf 6000ft dauert es 10 Minuten
© 2004 FSB / Basel
68
2400 RPM ~ 65% ~ 110 KTAS ~ 10 USG ~ 5 HRS
© 2004 FSB / Basel
69
Landing: Der Ground Roll beträgt 575ft
2550lbs, SL, standard atm, no wind, hard rwy, short field ldg
© 2004 FSB / Basel
70
Normal Procedures
© 2004 FSB / Basel
71
Outside Check
© 2004 FSB / Basel
72
Important Figures
• 2400 RPM
• 2200 RPM
• 2000 RPM
105 KIAS
95 KIAS
85 KIAS
• +/- 200 RPM
+/- 10 KIAS
+/- 500 ft
© 2004 FSB / Basel
73
Fuel Vapor Procedures
Fuel Vapor may occur on ground
during warm weather (>80°F/26°C)
When fuel vapor occurs proceed as follows:
• Mixture full rich, set throttle at 1800-2000 RPM for
1-2 minutes or until smooth operation returns.
• Retard throttle to idle to verify normal operation.
• Set 1200 RPM and lean to 75° rich of peak.
• Just prior to Takeoff, apply full throttle for ca 10
seconds to verify smooth engine operation.
© 2004 FSB / Basel
74
Normal Takeoff
•
•
•
•
•
Fuel Selector Both
Flaps 0°
Vr 55 KIAS
Vx 62 KIAS
Vy 74 KIAS
• Crosswind: Ailerons partially deflected into the
wind. When clear of ground, make a coordinated
turn into the wind to correct for drift.
© 2004 FSB / Basel
75
Short Field Takeoff
•
•
•
•
•
•
Fuel Selector Both
Flaps 10°
Apply Brakes - Throttle full open - Release Brakes
Elevator Control slightly tail low
Climb Speed 56 KIAS (until obstacle clearance)
Flaps Retract slowly after passing 60 KIAS
© 2004 FSB / Basel
76
Soft and Rough Field Takeoff
• Fuel Selector Both
• Flaps 10°
• Lift the airplane as soon as practical in a slightly
tail low attitude
• Accelerate asap to a higher climb speed
• Flaps Retract slowly after passing 60 KIAS
© 2004 FSB / Basel
77
Cruise Climb
•
•
•
•
•
Fuel Selector Both
Flaps 0°
Full Throttle
Vcruise climb 80 KIAS
Mixture Full Rich during climb up to 7000ft.
Careful leaning during climb at higher altitudes.
• Avoid climb spees <Vy because of engine cooling
© 2004 FSB / Basel
78
Cruise
• Cruise at 65%
• Fuel Selector L or R or BOTH (keep wings level!)
• At 5000ft or above lean to 75°F rich of peak not
earlier than 2 minutes after level off. Use EGT.
© 2004 FSB / Basel
79
Stalls and Spins
Stalls are conventional.
Spin Recovery:
• Throttle idle and ailerons neutral
• Apply and hold full rudder opposite to direction of
rotation
• Hold these control inputs until rotation stops
• After stop of the rotation: move the the control wheel
briskly forward
• Neutralize the rudders and smoothly stop the dive
Spins with flaps extended are prohibited
© 2004 FSB / Basel
80
Descent
•
•
•
•
•
•
A
B
C
D
E
F
ATIS/ALT, Autopilot
Briefing
Circuit Breakers
DG/Avionics
Electrical System
Fuel Seelctor BOTH / Mixture adjust
• Descent Power
• Seats, Seat Belts and Shoulder Harnesses
© 2004 FSB / Basel
81
Approach Preparation
• Before first checkpoint (e.g. S)
• Altimeter and DG
Landing Light
Fuel Quantity
Fuel Selector Both
Mixture Rich
Carburetor Heat
© 2004 FSB / Basel
82
Approach
Threshold Short Final
55 KIAS
60 KIAS
Final Approach
65 KIAS
500 ft AGL
45°
Base 1.5 x Vso
1 NM
ch
a
ro
1000 ft AGL
Initial Approach
85 KIAS
© 2002 FSB / Basel
© 2004 FSB / Basel
pp
A
e
at IAS
i
ed 5 K
m
7
er
t
In
83
Normal Landing
Initial Approach
• 85 KIAS, Flaps 1
Intermediate Approach
• 75 KIAS, Flaps 2
Final Approach
• 65 KIAS, Flaps 3,
• Short Final 60 KIAS
• Threshold 55 KIAS
© 2004 FSB / Basel
84
Crosswind Landing
• Use minimum flap setting for the field length.
• If flap setting >20° are used in sideslips with full
rudder deflection, some elevator oscillation may
be felt at normal approach speeds. This does not
affect control of the airplane.
• Demonstrated X-wind 15 kts.
© 2004 FSB / Basel
85
Go around (balked landing)
• Full power
• Pitch up
• When positive ROC: reduce flaps to 20°
• If obstacles must be cleared during the goaround-climb reduce flaps to 10° and maintain
safe airspeed (min. 56 KIAS as for short field take
off or Vx 62 KIAS).
• After clearing obstacles retract flaps and accelerate to Vy
© 2004 FSB / Basel
86
Emergency Procedures
© 2004 FSB / Basel
87
ENGINE FIRE DURING START ON GROUND
01 STARTER
IF ENGINE STARTS:
02 POWER
03 ENGINE
CONTINUE CRANKING
1800 RPM FOR A FEW MINUTES
SHUTDOWN AND INSPECT
FOR DAMAGE
IF FIRE CONTINUES:
04 THROTTLE
FULL OPEN
05 MIXTURE
IDLE CUT-OFF
06 CRANKING
CONTINUE
07 FUEL SHUT OFF VALVE OFF PULL OUT
08 AUXILIARY FUEL PUMP
OFF
09 BATTERY AND ALTERNATOROFF
10 AIRPLANE
EVACUATE
11 FIRE
EXTINGUISH
© 2004 FSB / Basel
88
ENGINE FAILURE DURING TAKEOFF ROLL
01 THROTTLE
02 BRAKES
03 FLAPS
IDLE
APPLY
RETRACT
ENGINE FAILURE AFTER TAKEOFF
01 NOSE DOWN
02 SPEED
03 AT LOW ALTITUDE
04 FLAPS
© 2004 FSB / Basel
IMMEDIATELY
70 KIAS FLAPS UP
65 KIAS FLAPS DOWN
NO TURNS
AS REQUIRED
89
ENGINE FAILURE IN FLIGHT
01
02
03
04
05
06
07
FLY BEST GLIDE (68 KIAS)
FUEL SHUT OFF VALVE ON/PUSHED FULL IN
FUEL SELECTOR
AUXILIARY FUEL PUMP
MIXTURE
ENGINE GAUGES
FUEL QUANTITY L/R
IF TIME PERMITS
08 IGNITION L/R/BOTH
CHECKED
CHECKED
BOTH
ON
FULL RICH
CHECK FOR CAUSE
CHECKED
09 THROTTLE/MIXTURE
CHECK (OR START IF
PROP STOPPED)
TRY DIFFERENT SETTINGS
WHEN POWER IS RESTORED
10 FUEL PUMP
OFF
WHEN POWER IS NOT RESTORED
11 FOLLOW PROCEDURES OF POWER OFF LANDING
© 2004 FSB / Basel
90
POWER OFF LANDING
01 SUITABLE LANDING FIELD
02 INFORM ATC OR 121.5
03
04
05
06
07
08
09
WHEN COMMITTED TO LANDING:
SPEED
70 KIAS FLAPS UP
65 KIAS FLAPS DOW
FLAPS
AS REQUIRED (30°
RECOMMENDED)
MIXTURE
IDLE CUT OFF
FUEL SHUT OFF VALVE OFF
PULLED FULL OUT
BATTERY AND ALTERNATOR
OFF
SEAT BELTS AND HARNESSES TIGHT
DOOR
OPEN
© 2004 FSB / Basel
CHOOSE
DONE
91
DITCHING
01 INFORM ATC OR 121.5
02 FLAPS 20°-30°
03 ROD 300FPM AT 55 KIAS
IF NO POWER IST AVAILABLE:
04 SPEED
05 ELT
06 SEAT BELTS AND HARNESSES
07 DOOR
© 2004 FSB / Basel
DONE
SET
ESTABLISH
70 KIAS FLAPS UP
65 KIAS FLAPS DOWN
ACTIVATE
TIGHT
OPEN
92
ENGINE FIRE IN FLIGHT
01
MIXTURE
02
03
04
05
FUEL SHUT OFF VALVE OFF
AUXILIARY FUEL PUMP
CABIN HEAT AND AIR
06
07
PULLED FULL OUT
OFF
OFF
OFF (EXCEPT
OVERHEAD VENTS)
AIRSPEED
100 KIAS
PROCEED WITH POWER OFF LANDING
© 2004 FSB / Basel
IDLE CUT OFF
93
ELECTRICAL FIRE IN FLIGHT
01
02
03
04
05
06
07
08
09
10
SOURCE OF FIRE
VENTS
CABIN HEAT
FIRE EXTINGUISHER
ALL OTHER SWITCHES
(EXCEPT IGNITION)
OFF
IF FIRE IS EXTINGUISHED AND ELECTRICAL POWER IS
NECESSARY:
ON
CIRCUIT BREAKERS
CHECKED, DO NOT RESET
RADIO SWITCHES
OFF
RADIO/ELECTRICAL SWITCHES
ON, ONE BY ONE UNTIL SHORT
CIRCUIT IDENTIFIED
DONE
© 2004 FSB / Basel
IDENTIFIED
OFF
CLOSED
OFF
ACTIVATE
94
CABIN FIRE
01 BATTERY AND ALTERNATOR
02 CABIN HEAT AND AIR
03 FIRE EXTINGUISHER
WHEN FIRE IS EXTINGUISHED:
04 CABIN HEAT AND AIR
05 LAND AS SOON AS POSSIBLE
TO INSPECT FOR DAMAGE
© 2004 FSB / Basel
OFF
CLOSED
ACTIVATE
OPEN
95
WING FIRE
01
02
03
04
LANDING AND TAXI LIGHTS
NAVIGATION AND STROBE LIGHTS
PITOT HEAT
PERFORM A SIDESLIP TO KEEP
FLAMES AWAY FROM TANKS
AND CABIN
USING FLAPS ONLY FOR FINAL
APPROACH AND TOUCHDOWN
© 2004 FSB / Basel
OFF
OFF
OFF
DONE
DONE
96
LOSS OF FUEL PRESSURE
02 FUEL SELECTOR
ON
BOTH
OIL / LOSS OF PRESSURE OR HIGHTEMPERATURE
02 PREPARE FOR POWER OFF LANDING
© 2004 FSB / Basel
97
ELECTRICAL FAILURES
IF AMMETER SHOWS EXCESSIVE RATE OF CHARGE:
01 ALTERNATOR
OFF (COMPASS DEV
MAY BE 25°)
02 NONESSENTIAL ELECTRICAL
EQUIPMENT
OFF
03 FLIGHT
TERMINATE AS SOON
AS PRACTICAL
01
02
03
04
05
06
IF LOW VOLTAGE ANNUNCIATOR ILLUMINATES DURING
FLIGHT:
AVIONICS MASTER
OFF
ALTERNATOR CIRCUIT BREAKER CHECK IN
OFF
ON
LOW VOLTAGE ANNUNCIATOR
CHECK OFF
AVIONICS MASTER
ON
© 2004 FSB / Basel
98
ELECTRICAL FAILURES
IF LOW VOLTAGE ANNUNCIATOR ILLUMINATES AGAIN:
07 ALTERNATOR
08 NONESSENTIAL RADIO AND
ELECTRICAL EQUIPMENT
09 FLIGHT
© 2004 FSB / Basel
OFF
OFF
TERMINATE AS
SOON AS PRACTICAL
99
ENGINE ROUGHNESS
SPARK PLUG FOULING/MAGNETO MALFUNCTION
01 MIXTURE
02 MAGNETOS L/R/THEN BOTH
03 PROCEED TO NEAREST
AIRPORT FOR REPAIR
ADJUST FOR MAX
SMOOTHNESS
TRY
DONE
EINGINE-DRIVEN FUEL PUMP FAILURE
05 FLIGHT
© 2004 FSB / Basel
ON
TERMINATE AS SOON
AS PRACTICAL
100
ENGINE ROUGHNESS
EXCESSIVE FUEL VAPOR INDICATION: TRY THE FOLLOWING
07 MIXTURE
ON
ADJUST FOR MAX
SMOOTHNESS
SELECT ANOTHER ONE
08 FUEL TANK
09 INCREASE AIRSPEED (TO
IMPROVE COOLING)
DONE
10 FUEL SELECTOR
SWITCH TANKS
11 ENGINE GAUGES
CHECK
12 CONTINUE FLIGHT ON BEST
MAGNETO AT REDUCED POWER
AND FULL RICH MIXTURE TO
NEAREST AIRPORT
PREPARE FOR POWER OFF LANDING
© 2004 FSB / Basel
101
SPIN RECOVERY
01 THROTTLE
02 AILERONS
03 RUDDER
04 CONTROL WHEEL
WHEN ROTATION STOPS:
05 RUDDER
06 CONTROL WHEEL
© 2004 FSB / Basel
IDLE
NEUTRAL
FULL OPPOSITE
TO ROTATION
FULL FORWARD
NEUTRAL
SMOOTHLY TO REGAIN
LEVEL FLIGHT
102
COM/NAV: BENDIX/KING
KX 155A VHF NAV/COMM
KT 76C TRANSPONDER
KMA 26 AUDIO SELECTOR PANEL
KLN 94 GPS
KMD 550 MULTI-FUNCTION DISPLAY
© 2004 FSB / Basel
103
KX 155A VHF NAV/COMM
1
2
3
4
5
6/12
7
8
9
10
13
COM FREQ (T=Transmit, R=Receive)
NAV FREQ
NAV STANDBY/OBS/BEARING/RADIAL/TIMER
controlled by the Mode Button (7)
NAV FREQ SELECTOR KNOB (50 KHZ STEPS)
NAV FREQ SELECTOR KNOB (1 MHZ STEPS)
TRANSFER BUTTON
MODE SELECTOR (s. 3)
NAV VOL (PULL IDENT)
COM FREQ SELECTOR (50KHZ, 25 KHZ PULL
OUT)
CHANNEL BUTTON (PRESS FOR >2 SEC)
COM VOL CONTROL (OFF/PULL/TEST)
FOR DETAILS SEE INFORMATION MANUAL S1-5
© 2004 FSB / Basel
104
BENDIX/KING KT 76C TRANSPONDER
1
2
3
4
5
6
7
8
IDENT
ALT DISPLAY
MODE ANNUNCIATOR
REPLY INDICATOR
MODE SELECTOR
VFR CODE BUTTON
CLEAR BUTTON
NUMERIC KEYS 0-7
© 2004 FSB / Basel
105
BENDIX/KING 26 AUDIO SELECTOR PANEL
1
2
3
4
5
6
7
8
9
MARKER BEACON ANNUNCIATOR LIGHTS
PHOTOCELL FOR AUTOMATIC DIMMING OF MARKER BEACON LIGHTS
MARKER BEACON SENSITIVIY LAMP AND TEST SWITCH
AUDIO SELECT BUTTONS
MICROPHONE SELECTOR SWITCH
SPEAKER SELECT (PUSH SPKR)
MONITOR SELECT BUTTON
CREW INTERCOM VOLUME AND VOX SENSITIVITY SWITCH
PASSENGER INTERCOM VOLUME
© 2004 FSB / Basel
106
BENDIX/KING KLN 94 GPS
© 2004 FSB / Basel
107
KMD 550 MULTI-FUNCTION DISPLAY
1
BRIGHTNESS CONTROL
2
DATABASE CARD
3
DISPLAY
4
AVAILABLE FUNCTIONS LEGEND
5
ON/OFF CONTROL
6
FUNCTION SELECT INDICATORS
7
FUNCTION SELECT KEYS
8
CONTROL KNOBS (NOT FUNCTIONAL)
9
POWER LABELS
10
SOFT LABELS
11
JOY STICK
12
POWER KEYS
13
FAULT INDICATOR
© 2004 FSB / Basel
108
Happy landings !!!
© 2002 FSB / Basel
© 2004 FSB / Basel
109

Ground - Course Cessna 172S Skyhawk C 172S

Transcription

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