717 Aeroplane JAA Data Sheet

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2 The Following Content of this Data Sheet is Complete In Accordance With the Concurrent and Cooperative Certification Process (CCC) Working Procedure, Draft Issue 8 dated 17-May-1994 and JAA Administrative and Guidance Material I. General 1. Airworthiness Category JAR 25 Large Aeroplanes at Change 14. FAR 25 Transport Category Airplanes at Amendment Level Certification Authority Federal Aviation Administration (FAA) Los Angeles Aircraft Certification Office 3960 Paramount Boulevard Lakewood, California United States of America 3. Validating Authority Joint Aviation Authorities (JAA) Saturnusstraat 8-10 PO Box KA Hoofddorp The Netherlands 4. Type Certificate Holder/Manufacturer McDonnell Douglas Corporation 3855 Lakewood Blvd. Long Beach, California United States of America 5. Production Basis FAA Production Certificate Number Performance Category A Data Pertinent to all 717 Aeroplane Variants Page 12 of 18

3 I. General 1. Variant Aeroplane 2. Date of Application for JAA/FAA Type Certification 08-August Date of Recommendation for JAA/FAA Type 01-September-1999 Certification II. Certification Basis 1. Date of Application for JAA/FAA Type Certification 08-August JAA/FAA Certification Date 01-September-1999 See Note 1 FAA Type Certificate Data Sheet A6WE 3. Certification Basis The aircraft type and model numbers defined herein have been certificated in accordance with the Concurrent and Co-operative Certification Process (CCC) Working Procedure, Draft Issue 8 dated 17-May Compliance has been found with the JAA/FAA Jointly Agreed Type Certification Basis, CIP A-01. Page 13 of 18

4 4. Certification Requirements JAR 25, Change 14 with the Following Reversions (b)(2) CIP C-04 Jacking and Tie Down Provisions (b)(2), CIP C-12 Seats, Restraint System and Occupant (c)(5),(c)(6) Protection During Emergency Landing Dynamic Conditions CIP D-01 Fasteners (f) CIP D-25 Changes to Doors and Latching for McDonnell Douglas (b) CIP D-08 Ability to Operate Exits from Inside and Outside the Aircraft Under Adverse Aircraft Position (a)(1)(i) CIP D-09 Deactivation of the Type I Assist Means from (a)(1)(v) CIP D-10 Outside the Aircraft Operation of Assist Means After Being Subjected to the Inertial Forces in FAR (b) (b) CIP E-03 Pressure Refueling Automatic Shutoff 25A1141(f)(2) CIP E-04 Auxiliary Power Unit (APU) Fuel/Fire Shutoff Indication CIP-F-06 Equipment Systems & Installation Safety Analysis JAA Special Conditions CIP E-06 Windshear Triggered Auto-throttle System CIP F-03 High Intensity Radiated Fields (HIRF) Protection CIP F-04 Protection from the Indirect Effects of Lightning Strike CIP F-13 Dual Hydraulic System Failure JAR AWO at Change 1 plus NPA AWO-3, Issue 4 and NPA AWO-4, Issue 2. Page 14 of 18

5 Equivalent Safety Findings (a) CIP B-01 Accelerate-Stop Distance (a)(3) CIP D-06 Overwing, Type III, Aft, Step down Distance; Equivalent Safety Finding (e)(4) CIP D-11 Passenger Emergency Exit Markings for Door Operating Handle (c)(1) CIP D-14 Improved Access to Type III Emergency Exits (a) CIP D-13 Use of Symbol Only Placards in Lieu of Symbol and Lettering Placards for Fire Extinguisher Locations (a) CIP F-18 Red Anticollision Light Environmental Standards Noise Compliance ICAO Annex 16, Volume 1 Chapter 3 (Third Edition) and FAR Part 36. Emissions/Venting Compliance ICAO Annex 16, Volume 2 (Second Edition) and FAR Part 34. For Additional National Requirements for Type Certification, see CIP A-05 (JAA Member States Additional National Requirements). III. Technical Characteristics and Operational Limitations 1. Type Design Definition Boeing General Assembly Drawing No. 79GA001 and JAA Build Standard Definition Report No. MDC 97K Required Equipment The basic equipment (see 1) as prescribed in the type design definition necessary to meet applicable airworthiness regulations of the certification basis must be installed in the aircraft for certification. 3. Dimensions Span m (93 ft 4.2 in) Length m (124 ft 0.4 in) Height 8.88 m (29 ft 1.5 in) Wing Area m 2 (1,000.7 ft 2 ) 4. Engines Two Rolls-Royce Deutschland GmbH Engines BR A1-30.

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7 Engine Limits Joint Aviation Authorities (JAA) Engine Type Certificate Data Sheet No. Federal Aviation Administration (FAA) Engine Type Certificate Data Sheet No. As specified in the approved JAA/FAA Airplane Flight Manual Report No. MDC 97K9227. JAA Engine Data Sheet No. JAA/E/ FAA Engine Data Sheet No. E00061EN. 5. APU and APU Limits One Auxiliary Power International Corporation (APIC) APS APU Limitations as specified in the approved JAA/FAA Airplane Flight Manual Report No. MDC 97K Fuel Fuel, Fuel Additives and Corrosion Inhibitors As specified in the approved JAA/FAA Airplane Flight Manual Report No. MDC 97K Fuel Capacity As specified in the approved JAA/FAA Airplane Flight Manual Report No. MDC 97K Engine Oil Capacity Total Capacity (Engine Oil) Liters (5.3 U.S. Gallons) Total Volume Usable (Engine Only) Liters (1.64 U.S. Gallons) 9. Airspeed and Altitude Limits As specified in the approved JAA/FAA Airplane Flight Manual Report No. MDC 97K All Weather Capability Cat IIIa Page 16 of 18

8 11. Maximum Weights See Note 2 Taxi and Ramp Take-off (MTOW) Landing (MLW) Zero Fuel (MZFW) Gear jacking weight Fuselage and Wing Jack Weight 55,338 kg (122,000 lbs) 54,885 kg (121,000 lbs) 46,267 kg (102,000 lbs) 45,586 kg (100,500 lbs) 55,338 kg (122,000 lbs) 41,730 kg (92,000 lbs) 12. Center of Gravity Range As specified in the approved JAA/FAA Airplane Flight Manual Report No. MDC 97K Datum 7 inches forward of nose (Sta. 0). 14. Mean Aerodynamic Cord in. (L.E. of MAC at Sta ). 15. Leveling Means One of two systems in each airplane: Spirit levels and leveling pads at Sta or; Plumb bob and grid plate at Sta Minimum Flight Crew Pilot and Copilot. 17. Maximum Number of Passengers/Occupants 134/138 (134 plus four (4) flight attendants). See Note Exits 2 Type I 4 Type III 1 Tail Exit 19. Baggage and Cargo Compartments Front Cargo Compartment 18.3 m³ (646 ft³) max allowable load 4389 kgs/9675 lbs Aft Cargo Compartment 8.2 m³ (289 ft³) max allowable load 1966 kgs/4335 lbs 20. Wheels and Tyres Main Wheels Specification PS5620 Main Tyres Four H41x Nose Wheels Specification Nose Tyres Two 26x6.6 Page 17 of 18

9 IV. Operating and Service Instructions 1. Aircraft Flight Manual Approved Boeing JAA/FAA Airplane Flight Manual Report No. MDC 97K Boeing Aeroplane Weight Report No. MDC 97K9261, and Balance Manual Chapter 1, "Master Weight and Balance Manual". 3. Boeing Aeroplane Instructions for Continued Airworthiness Maintenance Manual Structural Repair Manual Airworthiness Limitations Instructions Certification Maintenance Requirements Maintenance Manual TP-717SRM Report No. MDC 96K9063 Report No. MDC 98K9284 See Note 4 V. Notes Note 1: McDonnell Douglas Corporation originally made application for Type Certification of the MD on August 8, Subsequently, McDonnell Douglas Corporation merged with The Boeing Company, and updated its application for Type Certification on March 27, 1998 with the new model designation of The JAA/FAA initially accepted the change in model designation on May 4, The JAA/FAA formally accepted the change in model designation on August 21, 1998, and also agreed on the formal application date and schedule for Type Certification. All compliance substantiation and related correspondence from the JAA/FAA using the MD-95 or MD model designator is applicable to the 717 or , as applicable. Note 2: Certified weights for an individual aircraft must be determined by reference to the JAA/FAA approved Airplane Flight Manual applicable to that aircraft and the associated Boeing Weight and Balance Manual. Note 3: Approved customer interior configurations are specified within the 717 JAA Build Standard Document MDC 97K9281, as defined by the applicable NMC's. Note 4: All documents for the 717 aeroplane Instructions for Continued Airworthiness are available from the manufacturer.

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