Type Certification Procedures Manual 10. Sample Type Certification Templates

Transcription

Type Certification Procedures Manual
10. Sample Type Certification Templates
10.1 Type Certificate Templates
Approved by Executive Manager, SD&FT, Version 1.2: November 2009
10.
Sample Type Certification Templates
10.1
Type Certificate Templates
10.1.1 Type Certificate
Type Certificate
Number: VAzzz
Pursuant to regulation 21.013A of the Civil Aviation Safety Regulations 1998, this Type
Certificate is issued to Acme Pty Ltd in respect of the MKI and MKII aircraft.
This certificate is valid until it is suspended or cancelled by the Civil Aviation Safety
Authority. The basis of certification is as described in type certificate data sheet number
VAzzz.
Date of Application:
28 April 1993
Date of Issuance:
Model Mk I I approved
10 October 2000
XX February 2009
J Citizen
Delegate of the Authority
10-1
10.1.2 Type Certificate Data Sheet
No
VA zzz
Revision 13
Aircraft ACME Pty Ltd
MKI
MKII
Date
22 September 2009
TYPE CERTIFICATE DATA SHEET
This data sheet, which is part of Type Certificate No. VAzzz, lists the conditions and
operational limitations under which the subject aircraft meets the airworthiness requirements
of the Civil Aviation Safety Authority.
Certificate Holder
ACME Pty Ltd
ACN 119 523 830
PO Box 24, Westside
NSW, Australia 3340
I
Approved in Normal Category 10th October 2000
Model MKI.
Engine
Textron Lycoming IO-540-K1A5
Engine Limits
Take Off
2500 rpm and full throttle (275 hp), or
2700 rpm and full throttle (300 hp) – max 2 minutes
Maximum Continuous
Propeller
10-2
2500 rpm and full throttle (275 hp)
Hartzell HC-C2YR-1BF/F8475R metal, constant speed
Diameter
not over
2134 mm
not under
1981 mm
10.1.3 Type Certificate Data Sheet (Continuation Sheet)
II
Model MKII
Approved in Normal Category 9 February 2009
Engine
Textron Lycoming TIO-540-AH1A
Engine Limits
Normal Take Off
Alternate Take Off
2500 rpm and 38 in Hg MAP (300 HP)
2500 rpm and 40 in Hg MAP below 5000’
Pressure Altitude (See Note 7).
Maximum Continuous
2500 rpm at 38 inHg (300 hp)
Propeller
Hartzell HC-C3YR-1RF/F8068 metal, constant speed
Diameter
not over
2083 mm
not under
1981 mm
Data Pertinent to All Models
Fuel
100LL or 100/130 aviation gasoline
Airspeed Limits
Never exceed Vne
185 KIAS
(knots IAS)
Max structural cruise Vno
Manoeuvring Va
Max flaps extended Vfe
143 KIAS
121 KIAS
97 KIAS
Centre of Gravity Limits
Forward Limit
+1219 mm aft of datum at 1089 kg or less
+1422 mm aft of datum at 1814 kg
Variation is linear between 1089 kg and 1814 kg.
Aft Limit
+1626 mm aft of datum at all weights
Datum
Fuselage firewall frame jacking points at fuselage station 0
(Stated arms are +ve aft; and -ve forward)
Levelling Means
Longitudinal Marks (blind rivets) on the port fuselage wall
Lateral Level across cockpit seat rails
Maximum Weights
Take-off
Landing
1814 kg
1814 kg
No. of Seats
Eight
Row 1 (Pilot row)
Row 2
Row 3
Row 4
arm
+ 965 mm
+1772 mm
+2523 mm
+3247 mm
10-3
Type Certificate Data Sheet (Continuation Sheet)
Maximum Baggage
Aft Luggage
Baggage Shelf
Bin
113kg
22kg
at +3763 mm
at +4623 mm
Fuel Capacity
Main wing tanks
two (one tank in each wing)
Total each tank
170 litres at +1715 mm
Useable each tank 166 litres at +1715 mm
Unusable each tank
4 litres
at
+1829 mm
Sump tank
9 litres
at +705 mm
Sump tank capacity is designated unusable fuel.
Oil Capacity
Total
Unusable
11.4 litres at -540 mm
2.6 litres at -540 mm
Crosswind Component
Maximum demonstrated for take-off and landing
Control Surface
Deflections
Horizontal Stabiliser leading edge
15 knots
Up
2.0° ± 0.5°
Down
5.0° ± 0.5°
- measured between the mid-section line of the stabiliser
and the horizontal reference
Elevator trailing edge
Up
15.0° ± 0.5°
Down
19.0° ± 0.5°
- measured between the mid-section line of the elevator and
the mid-section line of the horizontal stabiliser, with the
stabiliser in the full leading edge down position
Aileron trailing edge
Up
17.0° ± 0.5°
Down
16.0° ± 0.5°
- measured between the under-surface of the aileron and the
rear under-surface of the wing main plane
Rudder trailing edge
L&R
Wing flaps
Retracted
Take-off
Landing
All measurements refer to hinge line rotation.
Serial numbers eligible
MK-00-004 and subsequent
Type Design Data
For serial numbers MK-00-004 to GA8-03-025
(i)
(ii)
10-4
21.0° ± 0.5°
0° ± 1°
14.0° ± 1°
38.0° ± 1°
Engineering ReleaseMK-970001, Issue 5 or later
approved revision , and
Master Drawing MK-010001, Issue 2 or later approved
revision, GA8 General Assembly, and
(iii)
Pilot's Operating Handbook and Approved Flight
Manual, document MK01, dated 10 September 2001 or
later approved revision; and
Service Manual document MK1, Chapter 4
Airworthiness Limitations, dated 26 November 2001
or later approved revision.
Additional Type Design Data for Model MKII:
(i)
(ii)
(iii)
Engineering Release GA8-970004, Issue 1 or later
approved revision - GA8-TC 320 Master Data Package.
Pilot's Operating Handbook and Approved Flight
Manual, document C01-01-08, dated 23 January 2009 or
later approved revision and
Service Manual document C01-00-05, Chapter 4
Airworthiness Limitations, dated 19 December 2008 or
later approved revision.
Certification Basis
1.
2.
Production Basis
Production Certificate No. ccc, dated 15 August 2003.
Equipment
1. The CASA approved aircraft flight manual details required
equipment for kinds of operations.
2. Other equipment may be required, to meet applicable
operational regulations.
Placards
The placards detailed in the applicable CASA approved aircraft
Pilot's Operating Handbook and Approved Flight Manual are
required to be fitted.
Notes
1.
Part 21 of the Civil Aviation Safety Regulations 1998, and
Federal Aviation Regulations, Part 23 at Amendment 54.
Weight and Balance.
A current weight and balance report including a list of equipment
included in the certificated empty weight, an approved load data sheet
and an approved loading system, must be provided for each aircraft at
the time of issue of a Certificate of Airworthiness.
Revision History
Revision 7 was issued 14 March 2003 to correct mass arms, and to include
the later design standard for serial number 026 and subsequent.
Revision 8 was issued 15 September 2003 to include IFR approval and
reference to the production certificate.
Revision 9 was issued 25 October 2004 to include the Cargo Pod approval.
10-5
Revision 10 was issued to add an alternative noise certification that allows
take-off at 2700 rpm and full throttle.
Revision 11 was issued due to a change of Type Certificate holder, from
Gippsland Aeronautics Pty Ltd, to GA8 Airvan Pty Ltd.
Revision 12 was issued to incorporate new model GA8-TC 320, and minor
editorial and formatting changes.
Revision 13 was issued to correct a minor typographical error on page 4,
Additional Type Design Data for Model GA8-TC 320: Paragraph (iii) (date of
issue of Service Manual C01-00-05 was changed from 19 December 2009 to
19 December 2008)
- END -
10-6
10.2 Type Acceptance Certificate Templates
10.2
Type Acceptance Certificate Templates
10.2.1 Type Acceptance Certificate
TYPE ACCEPTANCE CERTIFICATE
Number: A000
Pursuant to Regulation 21.029A of the Civil Aviation Safety Regulations 1998 this
certifies acceptance of the ACME Pty Ltd model ASR 2 aeroplane.
Aircraft of the type and models covered by this certificate are eligible for Australian
standard certificates of airworthiness in the acrobatic category.
This certificate is valid until suspended or cancelled by the Civil Aviation Safety
Authority. The basis of certification is as prescribed in Type Certificate Data Sheet
No yyy Issued by the Aviation Administration of the North, and Type Acceptance
Certificate Data Sheet A000 Issued by this authority.
J Citizen
September 2009
10-7
10.2 Type Acceptance Certificate Templates
10.2.2 Type Acceptance Certificate Data Sheet
No: A000
Revision No: Original Issue
Aircraft: ACME Pty Ltd
ASR 2
Date:
September 2009
TYPE ACCEPTANCE CERTIFICATE DATA SHEET
This data sheet is part of Type Acceptance Certificate A000, which is issued under Civil
Aviation Safety Regulation 21.029A. It lists any conditions and/or limitations under which the
type acceptance certificate was issued to meet the requirements of CASA.
Certification Basis:
The basis of certification is as prescribed in Type Certificate Data Sheet (TCDS)
yyy issued by the Aviation Administration of the North.
Certificate of Airworthiness Category:
An aircraft of the type and model covered by this certificate is eligible for an Australian
standard certificate of airworthiness in the acrobatic category.
Eligible Serial Numbers:
This data sheet is applicable to Serial Number ASR 2 only.
Note: Additional serial numbers will be considered upon application.
Conditions and/or Limitations:
1
This Aircraft must be operated in accordance with the limitations defined by Placards
and Markings, the approved Flight Manual, and TCDS yyy, which specifically prohibits
Intentional spinning manoeuvres.
Note: Type Acceptance Certificate A000 will become invalid if Type Certificate A yyy is
cancelled.
END
10-8
10.3 Supplemental Type Certificate Templates
10.3
Supplemental Type Certificate Templates
10.3.1 Supplemental Type Certificate
Supplemental Type Certificate
Number:
SVA zzz
This certificate is issued to:
ACME Pty LTD
PO Box 24, Westside
NSW 3340, Australia.
and certifies that the change in the type design for the following product meets the
airworthiness requirements specified in Supplemental Type Certificate Data Sheet
(STCDS) No. zzz, Revision 2 issued by the Civil Aviation Safety Authority of
Australia.
Original Product:
Type Acceptance Certificate Number:
Referenced TC Number (if applicable):
Make:
A123
A9SW
MK
Model:
I, II
Description of Type Design Change: Installation of the Honeywell TPE 331-1, -2,
-3 or -6 turbo-propeller engine and Hartzell HC-B3TN-5M/T10282N+4 propeller as
per ACME Pty Limited document Master Record Index abc at latest issue.
Limitations and Conditions: This Supplemental Type Certificate is subject to the
limitations and conditions specified in STCDS No. SVAzzz, Revision 1, dated 15
April 2009, or later CASA approved revision.
If the holder agrees to permit another person to use this certificate to alter the
product, the holder shall give the other person written evidence of that permission.
This certificate and the supporting data that is the basis for approval shall remain in
effect until suspended, cancelled or a termination date is otherwise established by the
Civil Aviation Safety Authority.
Date of application:
Date of issuance:
Revision 1 issued:
Date re-issued:
3 November 1997.
17 February 1998.
4 November 2003
15 April 2009
This certificate is issued pursuant to Part 21.113A of the Civil Aviation
Regulations 1998.
J Citizen
10-9
10.3.2 Supplemental Type Certificate Data Sheet
STC No.:
Revision:
Aircraft:
SVA zzz
2
Mk
I
II
Date:
15 April 2009
SUPPLEMENTAL TYPE CERTIFICATE DATA SHEET
1.
Applicability
This data sheet is applicable to MK I and II aircraft with the following
modifications:
Installation of an Allied Signal Aerospace TPE331-1, -2, -3 or -6 Turbopropeller
engine;
Installation of a Hartzell HC-B3TN-5M/T10282+4 propeller.
1.2
This data sheet is part of Australian Supplemental Type Certificate No. SVA zzz
and shall be read in conjunction with Type Certificate xxx, Revision 10, dated
April 22, 1996
1.3
This approval should not be incorporated where other previously approved
modifications are incorporated, unless it is determined by the installer that the
interrelationship between this change and any of those previously approved
modifications will produce no adverse effect upon the airworthiness of the aircraft.
2.
Certificate Holder
The holder of Supplemental Type Certificate No. 220-2 is:
ACME Pty Ltd
PO Box 24,
Westside,
NSW, 3340
AUSTRALIA
3.
SPECIFICATIONS AND LIMITATIONS
3.1
Engine
Allied Signal Aerospace TPE331-1-101B, E, F, J, L, Z
Allied Signal Aerospace TPE331-1-151A, B, G, K
10-10
10.3.3 Supplemental Type Certificate Data Sheet (Continuation Sheet)
Rated Power: 665 SHP/1746 ft.lb torque at 2000 propeller RPM, takeoff and
continuous.
Engine Limits
EGT: 578°C (Take-off)
EGT: 556°C (Max. Cont.)
Torque: 1746 ft.lb
Propeller RPM:
Take-off and Continuous: 100%
Cruise: 96% to 100%
Ground Idle: 65% to 85%
Prohibited Range: 18% to 28% except for start and
shutdown transients.
Oil Pressure:
Normal Operating range: 70 to 120 psi
Ground Idle range: 50 to 130 psi
Maximum Allowable: 130 psi
Caution range: 50 to 70 psi and 120 to 130 psi
Oil Temperature:
Normal Operating range: 55°C to 110°C
Maximum Allowable: 127°C
Caution range: -40°C to 55°C and 110°C to 127°C
Fuel Pressure:
Maximum: 85 psi
Minimum: 15 psi
Caution range: 15 to 25 psi
Engine
Allied Signal Aerospace TPE331-2-201A
continuous.
Engine Limits
EGT: 578°C (Take-off)
EGT: 578°C (Max. Cont.)
Torque: 1786 ft.lb
Propeller RPM:
Cruise: 96% to 100%
Prohibited Range: 18% to 28% except for start and shutdown
transients.
10-11
Supplemental Type Certificate Data Sheet (Continuation Sheet)
Oil Pressure:
Oil Temperature:
Fuel Pressure:
Maximum: 85 psi
Minimum: 15 psi
Engine
Allied Signal Aerospace TPE331-2-201C
continuous.
Engine Limits
ITT: 923°C (Take-off)
ITT: 923°C (Max. Cont.)
Torque: 1786 ft.lb
10-12
Propeller RPM:
Cruise: 96% to 100%
Oil Pressure:
Oil Temperature:
Fuel Pressure:
Maximum: 85 psi
Minimum: 15 psi
Engine
Allied Signal Aerospace TPE331-3 series
TPE331-6 series
continuous.
Engine Limits
ITT: 923°C (Take-off)
ITT: 923°C (Max. Cont.)
Torque: 1786 ft.lb
Propeller RPM:
Cruise: 96% to 100%
3.2
Oil Pressure:
Oil Temperature:
Fuel Pressure:
Maximum: 90 psi
Minimum: 8 psi
Propeller
Hartzell HC-B3TN-5M/T10282+4 (see Note 3)
Number of blades: 3
Governor: Garrett (Woodward)
10-13
Propeller Limits
Maximum diameter: 106 inches
Minimum diameter: 98 inches
Blade angles at Station 30:
Flight Idle:
Feather:
Reverse:
3.3
8.0° ± 1.0°
89°
-3°
Fuel System
Main Tanks Total Capacity: 476 litres (126 U.S. Gal) - Total
454 litres (120 U.S. Gal) - Usable
Header Tank: 21 litres - Total
NIL usable
3.4
Oil System
Specification: EMS 53110 Type II (MIL-L-23699B)
Capacity:
3.5
Minimum 4.0 U.S. quarts
Airframe Limits
Speeds:
VNE = 149 KIAS
VA = 119 KIAS
VNO = 119 KIAS
VFE = 103 KIAS
Air Start Envelope: Above 110 KIAS, below 10,000 feet
3.6
10-14
Weight and Balance
Maximum Take-off Weight:
2268 kg (5000 lb)
Maximum Landing Weight:
2268 kg (5000 lb)
Centre of Gravity limits:
Datum leading edge of the wing
AT-301:
Forward Limit: 356 mm (14.0”) at all weights
Aft Limit:
457 mm (18.0”) at 2268 kg (5000 lb)
584 mm (23.0”) at 1950 kg (4300 lb)
Straight line variation between points
AT-301 aircraft fitted with the factory all-metal elevators and rudder may extend
the aft limits to the following providing a P/N 70466-2 strap and downspring is
installed in accordance with drawing 70465.
457 mm (18.0”) at 2268 kg (5000 lb)
622 mm (24.5”) at 1950 kg (4300 lb)
AT-302:
Forward Limit: 381 mm (15.0”) at all weights
Aft Limit:
457 mm (18.0”) at 2268 kg (5000 lb)
610 mm (24.0”) at 1950 kg (4300 lb)
AT-302 aircraft fitted with the factory all-metal elevators and rudder may extend
the aft limits to the following providing a P/N 70466-1 strap and downspring is
installed in accordance with drawing 70465.
457 mm (18.0”) at 2268 kg (5000 lb)
660 mm (26.0”) at 1950 kg (4300 lb)
3.7
Placards
On the instrument panel in clear view of the pilot:
“MANEUVERING SPEED, VA = 119 KIAS”
“USE OF BETA RANGE IN FLIGHT PROHIBITED”
“THIS AIRCRAFT IS TO BE OPERATED IN AGRICULTURAL CATEGORY IN
ACCORDANCE WITH THE PLACARDS AND MARKINGS DISPLAYED IN THE
COCKPIT AND WITH THE LIMITATIONS IN THE FLIGHT MANUAL”
10-15
Located on inside of each door window next to the top and forward at the door
handle:
“IF DOORS WILL NOT OPEN AFTER OVERTURN,
KICK OUT WINDOWS WITH KNEES OR FEET”
4.
SERIAL NUMBERS ELIGIBLE FOR MODIFICATION
All serial numbers as specified on the Type Certificate Data Sheet A9SW,
Revision 10, dated 22 April 1996 or later.
5.
CERTIFICATION BASIS
Any aircraft which has been modified in accordance with this STC is eligible for a
certificate of airworthiness in the restricted category. The design of the modification
has been shown to conform to the following requirements:
Civil Aeronautics Manual 8 by the USA Federal Aviation Agency, November 15, 1951
6.
DOCUMENTS
The following documents are required to specify the modification:
ACME Pty Ltd Master Records Index abc at Issue 2 dated 12 February 1998 or later.
The following document is required for incorporation of the modification:
ACME Pty Ltd Engineering Instruction Sheet abc at Issue 1 dated 28 November 1997
or later.
The following document is required for operation of the modified aircraft:
CASA approved Flight Manual bbb-FM at Revision 0 dated 10 November 1997 or later
CASA approved revision.
7.
NOTES
1. A current weight and balance report and equipment list, with suitable
approved loading system must be raised for each aircraft modified in
accordance with this STC. The weight and balance data and loading system
shall be incorporated into the aircraft flight manual before issue.
2. An approved Flight Manual shall be issued to each aircraft modified in
accordance with this STC.
10-16
7.
NOTES
1. A current weight and balance report and equipment list, with suitable approved
loading system must be raised for each aircraft modified in accordance with this
STC. The weight and balance data and loading system shall be incorporated into the
aircraft flight manual before issue.
5. An approved Flight Manual shall be issued to each aircraft modified in accordance
with this STC.
6. Hartzell HC-B3TN-5M/T10282N+4 propeller may be used interchangeably with
propeller models HC-B3TN-5C/T10282+4 or HC-B3TN-5E/T10282+4 only if the
propellers have common counterweight & blade angle configuration.
7. Revision 1 of this STCDS identifies a new STC holder and makes minor editorial
and format changes to the STCDS.
- END -
10-17
10.4 Other Type Certification Templates
10.4
Other Type Certification Templates
10.4.1 Sample TAC Notification Email
From:
Sent: Tuesday, 4 March 2008 11:42
To:
Subject: Application For Type Acceptance Acme Pty Ltd Mk3[SEC=UNCLASSIFIED]
Folks, we have received an application for Type Acceptance for the following aircraft
Acme Mk 3 in the Transport Category.
I have also provided a link to the relevant FAA information and PDF copy of the TCDS
http://www.airweb.faa.gov/regulatory_and_guidance_Library/rgMakeModel.nsf/0/ce41b0787460af13862
57228006bf8b2/$FILE/T00011AT.pdf
Team Leader Certification Support
Airworthiness Engineering Branch
Civil Aviation Safety Authority
Email:
Phone:
10-18
10.4 Other Type Certification Templates

Type Certification Procedures Manual 10. Sample Type Certification Templates

Transcription

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