TYPE-CERTIFICATE DATA SHEET NO. EASA.IM.A.502 for Cessna 510 (Mustang)

11. Maximum Operating Altitude 12,497 m (41,000 ft.) 12. Operational Capacity: VFR Day and Night IFR Day and Night RVSM (See Note 6) Flight into Known Icing (See Limitations Section of EASA Approved Airplane Flight Manual) 13 Maximum Certified Weights in kg (lbs) Aircraft Serial Number Max. Zero Fuel Weight Max. Ramp Weight Max. Take-Off Weight Max. Landing Weight 525-0001 and on 1728 kg (6750 lbs) 3960 kg (8730 lbs) 3921 kg (8645 lbs) 3629 kg (8000 lbs) 14. Center of Gravity Range (Gear Extended)* Forward Limits: Linear variation from 287.04 in. aft of datum (21.32% MAC) at 8730 lb. to 285.59 in. aft of datum (19.00 % MAC) at 6927 lb.; 285.59 in. aft of datum (19.00 % MAC) at 6927 lb. or less. Aft Limits: 292.46 in. aft of datum (30% MAC) at 8730 lb. or less Landing Gear retracting moment (-1302.87) in-lb. * Straight line variation between given points 15. Datum 143.7 in. forward of the jig point (nose jack pad location) 16. (Reserved) 17. Levelling means Longitudinal – In board crew seat rails at FS 196.00. Lateral - In board crew seat rails at FS 196.00. 18. Minimum Flight Crew (See Note 5 for cockpit equipment/arrangement restrictions): One pilot (in the left pilot seat) plus additional equipment as specified in the Kinds of Operations Equipment List (KOEL) contained in the Limitations Section of the FAA Approved Airplane Flight Manual OR One pilot and one copilot 19. Maximum Passenger Seating Capacity: 6 Passengers (two crew plus four passenger seats) 20. (Reserved) TCDS No.: EASA.IM.A.502 Cessna 510 (Mustang) Issue: 03 Date: 21 June 2018 TE.CERT.00048-001 © European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 7 of 10 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union 21. Baggage / Cargo Compartment Nose Compartment 145 kg (320 lbs) Tailcone 136 kg (300 lbs) 22. Wheels and Tires Main Landing Gear (MLG) 22 x 6.75-10 (Dunlop DR25526T) Main Landing Gear (MLG) 22 x 6.75-10 (Michelin 021-523-0) Nose Landing Gear (NLG) 16 x 4.4 (Dunlop DR17026T) Nose Landing Gear (NLG) 16 x 4.4 (Michelin 079-606-0) A.IV. Operation and Service Instructions Airplane Flight Manual (AFM) Airplanes must be operated according to the EASA Approved Airplane Flight Manual, part number 510FM-00 (or later approved revision). Airplane Maintenance Manual Model 510 Maintenance Manual, 510MM00 or later approved revision. See Chapter 4, “Airworthiness Limitations” for inspections, mandatory retirement life information and other requirements for continued airworthiness. “Airworthiness Limitations” may not be changed without the approval of EASA. A.V. Operational Suitability Data OSD FC OSD FC Original Issue or later approved Revision MMEL MMEL 510MMELEU, Initial Issue or later Approved Revision V. Notes NOTE 1: Current weight and balance information, including list of equipment included in certificated empty weight, and loading instructions are provided for each airplane in the EASA Approved Airplane Flight Manual (AFM) at the time of original certification. The certificated empty weight and corresponding center of gravity location must include: Unusable fuel 53.40 lbs at +290.56 in Full oil 20.2 lbs at +363.11 in Hydraulic Fluid 10.23 lbs at +192.45 in NOTE 2: Airplanes must be operated according to the EASA Approved Airplane Flight Manual (AFM), part number 510FM-00. Required placards and markings are listed in Chapter Eleven (11) of Maintenance Manual, part number 510MM00. TCDS No.: EASA.IM.A.502 Cessna 510 (Mustang) Issue: 03 Date: 21 June 2018 TE.CERT.00048-001 © European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 8 of 10 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union NOTE 3: See Maintenance Manual, Chapter Four (4), “Airworthiness Limitations” for inspections, mandatory retirement life information, and other requirements for continued airworthiness. NOTE 4: All replacement seats (crew and passenger), although they may comply with TSO C127, must also be demonstrated to comply with installation requirements into the aircraft listed in 14 CFR §§23.2, 23.561, 23.562, and 23.785. The foam cushion buildup of all seats (crew and passenger) may not be altered. Any deviations in the foam construction or stiffness must be demonstrated by test to comply with the 14 CFR 23.562 paragraph. NOTE 5: Approval for operation with a minimum crew of one pilot is based upon the cockpit equipment installation and arrangement evaluated during FAA certification testing. No significant changes may be made to the installed cockpit equipment or arrangement (EFIS, autopilot, avionics, etc.), except as permitted by the approved MMEL, without prior approval from the responsible Aircraft Certification Office. NOTE 6: S/N 510-001 and On: All airplanes are equipped with Garmin G1000 dual RVSM capable Air Data Computers and pilot’s and o-pilot’s Primary Flight Displays as standard equipment. Each operator must obtain RVSM operating approval in accordance with applicable operating rules. NOTE 7: The model 510 is approved for One Engine Inoperative 10 minutes thrust capability with the Pratt & Whitney Canada PW615F-A turbofan engine, per FAA Policy Memo “Project Specific Policy on Approval for 10-Minute Rated Takeoff Thrust during Takeoff with One- Engine Inoperative (OEI) under 14 CFR Part 23 and 14 CFR Part 33 for Cessna model 510 Airplane with PW615F-A Engines”, dated August 15, 2006, from Standards Office, Small Airplane Directorate and Standards Office, Engine and Propeller Directorate. NOTE 8: The System Safety Assessment process has identified mandatory maintenance actions, which must be performed at specific intervals to compensate for latent failures. A list of those actions is contained in report RL-510-176, and cannot be changed without participation from the certificating ACO. This document has influenced certain maintenance actions documented in Airworthiness Limitations section (Chapter 4) of the maintenance manual. Those particular items cannot be changed without participation from the certificating ACO. TCDS No.: EASA.IM.A.502 Cessna 510 (Mustang) Issue: 03 Date: 21 June 2018 TE.CERT.00048-001 © European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 9 of 10 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union ADMINISTRATIVE SECTION I. Acronyms A.C. – Advisory Circular A.D. – Airworthiness Directives AFM – Airplane Flight Manual C.G. – Centre of Gravity CFR – Code of Federal Regulations CRI – Certification Review Items CS – Certification Specifications EASA – European Aviation Safety Agency EFIS – Electronic Flight Information System EU – European Union F.S. – Frame Status FAA – Federal Aviation Administration FADEC – Full Authority Digital Engine Control FC – Flight Crew FT – Feet GAL – Gallons ICAO – International Civil Aviation Organization IFR – Instrument Flight Rules KCAS – Knots Calibrated Air Speed KG – Kilo Grams KIAS – Knots Indicated Air Speed LBS – Pounds L.E. – Leading Edge MAC – Mean Aerodynamic Chord MIL – Military Standard MMEL – Master Minimum Equipment List N.A.A. – National Aviation Authority OSD – Operational Suitability Data RVSM – Reduced Vertical Separation Minimum S.B. – Service Bulletin T.O. – Take Off TC – Type Certificate TCDS – Type Certificate Data Sheet TCDSN – Type Certificate Data Sheet – Noise. TSO – Technical Standards Order VFR – Visual Flight Rules TCDS No.: EASA.IM.A.502 Cessna 510 (Mustang) Issue: 03 Date: 21 June 2018 TE.CERT.00048-001 © European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 10 of 10 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union II. Type Certificate Holder Record Since 29 July 2015: Textron Aviation Inc. One Cessna Boulevard P.O. Box 7704 Wichita, Kansas 67277 USA From 15 Oct 1992 to 28 Jul 2015: Cessna Aircraft Company P.O. Box 7704 Wichita, Kansas 67277 USA III. Change Record Issue Date Changes Issue 1 21 May 2007 Initial Release Issue 2 17 Dec 2015 TC holder transfer from Cessna Aircraft Company to Textron Aviation Inc. Corrections throughout all documents, Addition of OSD, Issue 3 21 June 2018 Alignment of Type name