Type Certificate. Number: VAzzz

Transcription

1 10.1 Type Certificate Templates 10.1 Type Certificate Templates Type Certificate Type Certificate Number: VAzzz Pursuant to regulation A 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: 10 October 2000 Model Mk I I approved XX February 2009 J Citizen Delegate of the Authority 10-1

2 10.1 Type Certificate Templates 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 PO Box 24, Westside NSW, Australia 3340 I Model MKI. Approved in Normal Category 10th October 2000 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 2500 rpm and full throttle (275 hp) Propeller Hartzell HC-C2YR-1BF/F8475R metal, constant speed Diameter not over 2134 mm not under 1981 mm 10-2

3 10.1 Type Certificate Templates 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 2500 rpm and 38 in Hg MAP (300 HP) Alternate Take Off 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 143 KIAS Manoeuvring Va 121 KIAS Max flaps extended Vfe 97 KIAS Centre of Gravity Limits Forward Limit mm aft of datum at 1089 kg or less mm aft of datum at 1814 kg Variation is linear between 1089 kg and 1814 kg. Aft Limit 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 1814 kg Landing 1814 kg No. of Seats Eight Row 1 (Pilot row) arm mm Row mm Row mm Row mm 10-3

4 10.1 Type Certificate Templates Type Certificate Data Sheet (Continuation Sheet) Maximum Baggage Baggage Shelf 113kg at mm Aft Luggage Bin 22kg at mm Fuel Capacity Main wing tanks two (one tank in each wing) Total each tank 170 litres at mm Useable each tank 166 litres at mm Unusable each tank 4 litres at mm Sump tank 9 litres at +705 mm Sump tank capacity is designated unusable fuel. Oil Capacity Total 11.4 litres at -540 mm Unusable 2.6 litres at -540 mm Crosswind Component Maximum demonstrated for take-off and landing 15 knots Control Surface Horizontal Stabiliser leading edge Up 2.0 ± 0.5 Deflections Down 5.0 ± measured between the mid-section line of the stabiliser and the horizontal reference Elevator trailing edge Up 15.0 ± 0.5 Down 19.0 ± 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 ± measured between the under-surface of the aileron and the rear under-surface of the wing main plane Rudder trailing edge L & R 21.0 ± 0.5 Wing flaps Retracted 0 ± 1 Take-off 14.0 ± 1 Landing 38.0 ± 1 All measurements refer to hinge line rotation. Serial numbers eligible Type Design Data MK and subsequent For serial numbers MK to GA (i) (ii) Engineering ReleaseMK , Issue 5 or later approved revision, and Master Drawing MK , Issue 2 or later approved revision, GA8 General Assembly, and 10-4

5 10.1 Type Certificate Templates Type Certificate Data Sheet (Continuation Sheet) (iii) Additional Type Design Data for Model MKII: 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. (i) Engineering Release GA , Issue 1 or later approved revision - GA8-TC 320 Master Data Package. (ii) Pilot's Operating Handbook and Approved Flight Manual, document C , dated 23 January 2009 or later approved revision and (iii) Service Manual document C , Chapter 4 Airworthiness Limitations, dated 19 December 2008 or later approved revision. Certification Basis 1. Part 21 of the Civil Aviation Safety Regulations 1998, and 2. Federal Aviation Regulations, Part 23 at Amendment 54. Production Basis Production Certificate No. ccc, dated 15 August Equipment Placards 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. The placards detailed in the applicable CASA approved aircraft Pilot's Operating Handbook and Approved Flight Manual are required to be fitted. Notes 1. 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

6 10.1 Type Certificate Templates Type Certificate Data Sheet (Continuation Sheet) 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 C was changed from 19 December 2009 to 19 December 2008) - END

7 10.2 Type Acceptance Certificate Templates 10.2 Type Acceptance Certificate Templates Type Acceptance Certificate TYPE ACCEPTANCE CERTIFICATE Number: A000 Pursuant to Regulation A 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 Delegate of the Authority September

8 10.2 Type Acceptance Certificate Templates 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 A. 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

9 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: A123 Referenced TC Number (if applicable): A9SW Make: 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: 3 November Date of issuance: 17 February Revision 1 issued: 4 November 2003 Date re-issued: 15 April 2009 This certificate is issued pursuant to Part A of the Civil Aviation Regulations J Citizen Delegate of the Authority 10-9

10 Supplemental Type Certificate Data Sheet 1. Applicability STC No.: SVA zzz Revision: 2 Aircraft: Mk I II Date: 15 April 2009 SUPPLEMENTAL TYPE CERTIFICATE DATA SHEET 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/T 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, 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 is: ACME Pty Ltd PO Box 24, Westside, NSW, 3340 AUSTRALIA 3. SPECIFICATIONS AND LIMITATIONS 3.1 Engine Allied Signal Aerospace TPE B, E, F, J, L, Z Allied Signal Aerospace TPE A, B, G, K 10-10

11 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: Normal Operating range: 25 to 85 psi Maximum: 85 psi Minimum: 15 psi Caution range: 15 to 25 psi Engine Allied Signal Aerospace TPE A Rated Power: 680 SHP/1786 ft.lb torque at 2000 propeller RPM, takeoff and continuous. Engine Limits EGT: 578 C (Take-off) EGT: 578 C (Max. Cont.) Torque: 1786 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

12 Supplemental Type Certificate Data Sheet (Continuation Sheet) 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: Normal Operating range: 25 to 85 psi Maximum: 85 psi Minimum: 15 psi Caution range: 15 to 25 psi Engine Allied Signal Aerospace TPE C Rated Power: 680 SHP/1786 ft.lb torque at 2000 propeller RPM, takeoff and continuous. Engine Limits ITT: 923 C (Take-off) ITT: 923 C (Max. Cont.) Torque: 1786 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: 120 psi Caution range: 40 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 10-12

13 Supplemental Type Certificate Data Sheet (Continuation Sheet) Fuel Pressure: Normal Operating range: 25 to 85 psi Maximum: 85 psi Minimum: 15 psi Caution range: 15 to 25 psi Engine Allied Signal Aerospace TPE331-3 series TPE331-6 series Rated Power: 680 SHP/1786 ft.lb torque at 2000 propeller RPM, takeoff and continuous. Engine Limits ITT: 923 C (Take-off) ITT: 923 C (Max. Cont.) Torque: 1786 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: 40 to 120 psi Maximum Allowable: 120 psi Caution range: 40 to 70 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: Normal Operating range: 20 to 80 psi Maximum: 90 psi Minimum: 8 psi Caution range: 8 to 20 psi and 80 to 90 psi 3.2 Propeller Hartzell HC-B3TN-5M/T (see Note 3) Number of blades: 3 Governor: Garrett (Woodward) 10-13

14 Supplemental Type Certificate Data Sheet (Continuation Sheet) Propeller Limits Maximum diameter: 106 inches Minimum diameter: 98 inches Blade angles at Station 30: Flight Idle: 8.0 ± 1.0 Feather: 89 Reverse: 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 Type II (MIL-L-23699B) Capacity: Minimum 4.0 U.S. quarts 3.5 Airframe Limits Speeds: V = 149 KIAS NE V A = 119 KIAS V = 119 KIAS NO V = 103 KIAS FE Air Start Envelope: Above 110 KIAS, below 10,000 feet 3.6 Weight and Balance Maximum Take-off Weight: Maximum Landing Weight: 2268 kg (5000 lb) 2268 kg (5000 lb) 10-14

15 Supplemental Type Certificate Data Sheet (Continuation Sheet) 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 strap and downspring is installed in accordance with drawing mm (18.0 ) at 2268 kg (5000 lb) 622 mm (24.5 ) at 1950 kg (4300 lb) Straight line variation between points 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) Straight line variation between points AT-302 aircraft fitted with the factory all-metal elevators and rudder may extend the aft limits to the following providing a P/N strap and downspring is installed in accordance with drawing mm (18.0 ) at 2268 kg (5000 lb) 660 mm (26.0 ) at 1950 kg (4300 lb) Straight line variation between points 3.7 Placards On the instrument panel in clear view of the pilot: MANEUVERING SPEED, V A = 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

16 Supplemental Type Certificate Data Sheet (Continuation Sheet) 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, 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

17 Supplemental Type Certificate Data Sheet (Continuation Sheet) 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/T or HC-B3TN-5E/T 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

18 10.4 Other Type Certification Templates 10.4 Other Type Certification Templates Sample TAC Notification From: Sent: Tuesday, 4 March :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 bf8b2/$FILE/T00011AT.pdf Team Leader Certification Support Airworthiness Engineering Branch Civil Aviation Safety Authority Phone: 10-18

19 10.4 Other Type Certification Templates