SECTION A: EA 400 (SALES DESIGNATION: EXTRA 400)
TCDS No. EASA.A.011 Page 2 of 17 EA 400 Issue 06, 14 December 2015
CONTENT
SECTION A: EA 400 (SALES DESIGNATION: EXTRA 400) A.I. General A.II. Certification Basis A.III. Technical Characteristics and Operational Limitations A.IV. Operating and Service Instructions A.V. Notes A.VI. Operational Suitability Data (OSD) SECTION B: EA 400-500 (SALES DESIGNATION: EXTRA 500) B.I. General B.II. Certification Basis B.III. Technical Characteristics and Operational Limitations B.IV. Operating and Service Instructions B.V. Notes B.VI. Operational Suitability Data (OSD) ADMINISTRATIVE SECTION I. Acronyms II. Type Certificate Holder Record III. Change Record IV. Notes for all EA400 variants
SECTION A: EA 400 (SALES DESIGNATION: EXTRA 400)
TCDS No. EASA.A.011 Page 3 of 17 EA 400 Issue 06, 14 December 2015 SECTION A: EA 400 (SALES DESIGNATION: EXTRA 400) A.I. General 1. Data Sheet No.: EASA.A.011 2. a) Type: EA 400 (Sales Designation: EXTRA 400) -- b) Model: -- c) Variant: 3. Airworthiness Category: Normal 4. Type Certificate Holder: SST FLUGTECHNIK GmbH Am Flughafen 12A D-87766, Memmingerberg Germany 5. Manufacturer: SST FLUGTECHNIK GMBH AM FLUGHAFEN 12A D-87766, MEMMINGERBERG GERMANY th 6. Certification Application 16 of April 1993 Date: 7. National Certifying Authority LBA nd 8. National Authority Type 22 of July 1997 Certificate Date: A.II. EASA Certification Basis 1. Reference Date for th determining the applicable 16 of April 1993 requirements: th 2. Airworthiness Requirements: FAR 23, Amendment 45 (9 of July 1993) For operation in known icing conditions additionally compliance has been shown with: FAR 23.49 Amdt. 23-50 FAR 23.1093 Amdt. 23-51 FAR 23.1323 Amdt. 23-51 JAR 23.1323 Amdt. 23-1 3. Special Conditions: Fire Protection of Engine mount Fuselage th Connection (LBA I 335-1086.SF2/94, dated 6 of April 1994) Roll Control in Supercooled Large Droplets (LBA- th 212.SF 1/02, dated 27 of September 2002) 4. Exemptions: None TCDS No. EASA.A.011 Page 4 of 17 EA 400 Issue 06, 14 December 2015 5. Deviations: None 6. Equivalent Safety Findings: See Equivalent Level of Safety Item List Doc. No.
EA-05406.01 7. Requirements elected to None comply: 8. Environmental Standards: Lärmschutzforderung für Luftfahrzeuge (LSL), st dated 1 of January 1991 9. Operational Suitability MMEL: CS-GEN-MMEL, Initial Issue Certification Basis: Flight Crew Data: SST Flugtechnik GmbH elects to comply with CS-FCD, Initial Issue 10. (Reserved) TCDS No. EASA.A.011 Page 5 of 17 EA 400 Issue 06, 14 December 2015 A.III. Technical Characteristics and Operational Limitations 1. Type Design Definition: Type Specification EA-05100.01 Equipment List EA-05100.06 Equipment List Electric/Avionic EA-05100.07 Document List EA-05100.03 2. Description: single engine landplane, reciprocating engine, six- seats, fibre-composite construction, high wing with T- tail configuration, retractable tricycle landing gear with nose wheel, pressurized cabin 3. Equipment: refer to POH Doc. No. EA-05701, Equipment-List 4. Dimensions: Span: 11.68m (38.3ft) Length 9.57m (31.4ft) Height 3.09m (10.14ft) Wing area 14.3m (154sq.ft) 5. Engine: 5.1.1 Model: TSIOL-550-C 5.1.2 Type Certificate: LBA Data Sheet No. 4612 5.1.3 Limitations: Take-off power 261 kW / 350 BHP Max. take-off rotational speed 2600 RPM Manifold pressure 1.30 bar / 39.5’’Hg Continuous power 242 kW / 325 BHP Max. continuous rotational speed 2500 RPM Manifold pressure 1.24 bar / 37.5’’Hg 6. Load factors: Wing Flaps retracted +4 to -1.6 g Wing flaps extended (15° or 30 °) +2 to 0 g 7. Propeller: 7.1 Model: MT-Propeller MTV-14-D/195-30a 7.2 Type Certificate: LBA Data Sheet No. 32.130/78 7.3 Number of blades: 4 7.4 Diameter: 1950 mm +/-0mm 7.5 Sense of Rotation: Right-hand tractor (viewed in direction of flight) 8. Fluids: 8.1 Fuel: 100/100LL minimum grade aviation gasoline 8.2 Oil: Engine: SAE 20W-50; SAE 30 and SAE 50 8.3 Coolant: External reservoir: 60/40 mixture of ethylene glycol / distilled water (ethylene glycol: ETX 6024 or TCM P/N 653125 or equivalent) TCDS No. EASA.A.011 Page 6 of 17 EA 400 Issue 06, 14 December 2015 9. Fluid capacities: 9.1 Fuel: Standard fuel tank: Total: 468 litre Usable: 404 litre 9.2 Oil: Engine: Total: 12.2 litre / 13 US Quarts Maximum: 11.4 litre / 12 US Quarts Minimum: 7.6 litre / 8 US Quarts 9.3 Coolant system 12 Litre / 3.2 US Gallons capacity: 10. Air Speeds: Design Manoeuvring Speed V : A MTOW (1999kg) 156 KIAS @1450kg 133 KIAS Flap Extended Speed V : FE Flaps 15° 120 KIAS Flaps 30° 109 KIAS Maximum Landing Gear Operation Speed V : LO 140 KIAS Maximum Landing Gear Extended Speed V : LE 140 KIAS Maximum Structural Cruising Speed V : NO 188 KIAS Never Exceed Speed V : 219 KIAS NE 11. Maximum Operating 7620m (25,000ft) Altitude: 12. Allweather Operations IFR, FIKI Capability: 13. Maximum Weights: Take-off 1999 kg Zero Wing fuel 1959 kg Landing 1999 kg 14. Centre of Gravity Forward limit 12% MAC up to 1600kg Range: 21% MAC at 1999kg (varies linearly between mass limits) Rear limit 38% MAC (MAC is 1322mm; 0%MAC is at 3200mm aft reference datum) 15. Datum: 3.115m in front of the front edge of main wheel bay 16. Control surface Aileron: 27° upward, 19° downward deflections: Pitch: 33° upward, 18° downward Yaw: 25° left, 25° right TCDS No. EASA.A.011 Page 7 of 17 EA 400 Issue 06, 14 December 2015 Pitch trim tab: 20° upward, 30° downward 17. Levelling Means: Spirit level on the upper edge of lower cabin door 18. Minimum Flight Crew: 1 19. Maximum Passenger 5 Seating Capacity: 20. Baggage/Cargo 90 kg Compartments: 21. Wheels and Tyres: Nose Wheel Tyre Size 5.0-5 6ply Main Wheel Tyre Size 15x6.0-6 6 ply 22. (Reserved): TCDS No. EASA.A.011 Page 8 of 17 EA 400 Issue 06, 14 December 2015 A.IV. Operating and Service Instructions 1. Flight Manual: Pilot’s Operating Handbook & Airplane Flight Manual Doc. No. EA-05701 2. Technical Manual: Maintenance Manual Doc. No. EA-05702 3. Repair Manual: Maintenance Manual Ch. 51 Doc. No. EA-05702 4. Manual for Operation: Pilot’s Operating Handbook & Airplane Flight Manual Doc. No. EA-05701 5. Spare Parts Catalogue: none 6. Table of Dimensions, Limits and Clearances: Maintenance Manual Doc. No. EA-05702 7. Instruments and aggregates: List of Applicable Publications Doc. No. EA-05710 TCDS No. EASA.A.011 Page 9 of 17 EA 400 Issue 06, 14 December 2015 A.V. Notes: 1 This certification applies to serial numbers 3 and on st 2 Approved Noise Levels in accordance to LSL (1 gen. 1991): 79.7 dB(A) 3 Colour specification for composite structure: see Maintenance Manual Chapter 4 Airplane serial numbers 003 through 027 eligible for flight into icing when modified with Extra Service Bulletin SB-400-01-92 or later LBA approved revision. Airplane serial 028 and above have shown compliance to applicable icing requirements and are approved for operation in known icing conditions.
A.VI. Operational Suitability Data (OSD): 1 Minimum Equipment List (MEL) SST report EQ-A500A-0210-10, latest approved revision 2 Flight Crew Data (FCD) SST report DI-A500A-0210-01, latest approved revision
SECTION B: EA 400-500 (SALES DESIGNATION: EXTRA 500)
TCDS No. EASA.A.011 Page 10 of 17 EA 400-500 Issue 06, 14 December 2015 SECTION B: EA 400-500 (SALES DESIGNATION: EXTRA 500) B.I. General 1. Data Sheet No.: EASA.A.011 2. a) Type: EA 400 EA 400-500 (Sales Designation: EXTRA 500) b) Model: -- c) Variant: 3. Airworthiness Category: Normal 4. Type Certificate Holder: SST FLUGTECHNIK GmbH Am Flughafen 12A D-87766, Memmingerberg Germany 5. Manufacturer: SST FLUGTECHNIK GmbH Am Flughafen 12A D-87766, Memmingerberg Germany th 6. Certification Application 05 of July 2001 Date: 7. (Reserved) 8. (Reserved) B.II. EASA Certification Basis 1. Reference Date for th determining the applicable 05 of July 2001 requirements: th 2. Airworthiness Requirements: FAR 23, Amendment 45, issued 09 of July 1993; st JAR 23, Amendment 1, issued 1 of February 2001 affected by the change to EA 400-500 according CRI A-01; In addition for the major flight deck upgrade involving electronic avionic equipment eligible for single pilot IFR day/night compliance has been shown with for the following paragraphs: JAR 23.1311 Electronic display instrument systems JAR 23.1431 Electronic equipment 8. Special Conditions: CRI C-01 Fire Protection of Engine mount- Fuselage -Connection 4. Exemptions: None 5. Deviations: None 6. Equivalent Safety Findings: CRI D-01 Emergency Exits 23.807(b)(2) TCDS No. EASA.A.011 Page 11 of 17 EA 400-500 Issue 06, 14 December 2015 CRI G-01 Airspeed Limitations 23.1505(c) 7. Requirements elected to None comply: 8. Environmental Standards: CRI A-03 ICAO, Annex 16, Volume 1, Chapter 10 9. Operational Suitability MMEL: CS-GEN-MMEL, Initial Issue Certification Basis: Flight Crew Data: SST Flugtechnik GmbH elects to comply with CS-FCD, Initial Issue 10. (Reserved) TCDS No. EASA.A.011 Page 12 of 17 EA 400-500 Issue 06, 14 December 2015 B.III. Technical Characteristics and Operational Limitations 1. Type Design Definition: Type Specification EA-0B100.01 Equipment List EA-0B100.06 Document List EA-0B100.03 2. Description: single engine turboprop, six-seats, fibre-composite construction, high wing with T-tail configuration, retractable tricycle landing gear with nose wheel, pressurized cabin 3. Equipment: refer to POH EA 400-500 Doc. No. EA-0B701 4. Dimensions: Span: 11.60m (38.1ft) Length 10.13m (33.23ft) Height 3.37m (11.06ft) Wing area 14.3m (154sq.ft) 5. Engine: 5.1.1 Model: Rolls-Royce 250-B17F/2 5.1.2 Type Certificate: FAA E10CE 5.1.3 Limitations: Max. take-off propeller rotational speed 2030 RPM Max. continuous propeller rotational speed 2030 RPM Min. continuous propeller rotational speed 1900 RPM 6. Load factors: Wing Flaps retracted +3.8 to -1.5 g Wing flaps extended (15° or 30 °) +2 to 0 g 7. Propeller: 7.1 Model: MT-Propeller MTV-5-1-D-C-F-R(A)/CFR210-56 7.2 Type Certificate: LBA TCDS 32.130/103/PR 7.3 Number of blades: 5 7.4 Diameter: 2100 +/- 5mm 7.5 Sense of Rotation: Right-hand tractor (viewed in direction of flight) 8. Fluids: 8.1 Fuel: JET A or JET A-1 (ASTM D1655-03 or later) 8.2 Oil: Engine & gearbox: MIL-PRF-7808L or later; or MIL- PRF-23699F or later 8.3 Coolant: -- 9. Fluid capacities: 9.1 Fuel: Standard fuel tank: Total: 680 litre (see B.V. Note 4) Usable: 652 litre 9.2 Oil: Engine external oil tank: Maximum: 5.18 litre TCDS No. EASA.A.011 Page 13 of 17 EA 400-500 Issue 06, 14 December 2015 Minimum: 4.08 litre 9.3 Coolant system -- capacity: 10. Air Speeds: Design Manoeuvring Speed V : A MTOW (2130kg) 156 KIAS @1545kg 131 KIAS Flap Extended Speed V : FE Flaps 15° 120 KIAS Flaps 30° 109 KIAS Maximum Landing Gear Operation Speed V : LO 140 KIAS Maximum Landing Gear Extended Speed V : LE 140 KIAS Maximum Structural Cruising Speed V : NO 188 KIAS Never Exceed Speed V : 207 KIAS NE 11. Maximum Operating 7620m (25,000ft) Altitude: 12. Allweather Operations IFR Capability: 13. Maximum Weights: (see B.V. Note 4) Take-off 2130 kg Zero Wing fuel 1945 kg Landing 2000 kg 14. Centre of Gravity Forward limit 18% MAC up to 1600kg Range: 25% MAC at 2130kg (see B.V. Note 4) (varies linearly between mass limits) Rear limit 34.5% MAC (MAC is 1322mm; 0%MAC is at 3200mm aft reference datum) 15. Datum: 3.115m in front of the front edge of main wheel bay 16. Control surface Aileron: 27° upward, 19° downward deflections: Pitch: 33° upward, 18° downward Yaw: 25° left, 25° right Pitch trim tab: 20° upward, 30° downward 17. Levelling Means: Spirit level on the upper edge of lower cabin door 18. Minimum Flight Crew: 1 TCDS No. EASA.A.011 Page 14 of 17 EA 400-500 Issue 06, 14 December 2015 19. Maximum Passenger 5 Seating Capacity: 20. Baggage/Cargo 90 kg Compartments: 21. Wheels and Tyres: Nose Wheel Tyre Size 5.0-5 6ply Main Wheel Tyre Size 15x6.0-6 10 ply 22. (Reserved): TCDS No. EASA.A.011 Page 15 of 17 EA 400-500 Issue 06, 14 December 2015 B.IV. Operating and Service Instructions 9. Flight Manual: Aircraft Flight Manual Doc. No. AFM-A500A- 0210-01 1. Technical Manual: Maintenance Manual Doc. No. EA-0B702 2. Repair Manual: Maintenance Manual Ch. 51 Doc. No. EA-05702 3. Manual for Operation: Aircraft Flight Manual Doc. No. AFM-A500A- 0210-01 (see B.V. Note 4) 4. Spare Parts Catalogue: none 5. Table of Dimensions, Limits and Clearances: Maintenance Manual Doc. No. EA-0B702 6. Instruments and aggregates: none TCDS No. EASA.A.011 Page 16 of 17 EA 400-500 Issue 06, 14 December 2015 B.V. Notes: 1 This certification applies to serial numbers 1002 and on.
2 Approved Noise Levels in accordance to ICAO Annex 16, Chapter 10: 76.7dB(A) 3 Colour specification for composite structure: see Maintenance Manual Chapter 4 For operational reasons a reduced MTOW is available for airplanes registered in the EU. No physical changes to the airplanes other than additional limitation placards are necessary for this MTOW reduction. A Supplement to the POH/AFM is available.
With Extra Kit 33778 installed limitations are as follows: Fuel: Standard fuel tank: Total: 468 litre Usable: 440 litre (Aux. fuel tanks must be empty) Maximum Weights: Take-off 1999 kg Landing 1999 kg Centre of Gravity Range: Forward limit 18% MAC up to 1600kg 23.3% MAC at 1999kg (varies linearly between mass limits) B.VI. Operational Suitability Data (OSD): 1 Minimum Equipment List (MEL) SST report EQ-A500A-0210-11, latest approved revision 2 Flight Crew Data (FCD) SST report DI-A500A-0210-01, latest approved revision TCDS No. EASA.A.011 Page 17 of 17 EA 400 Issue 06, 14 December 2015 ADMINISTRATIVE SECTION I. Acronyms II. Type Certificate Holder Record th Extra Flugzeugbau GmbH: until 15 of September 2003 th Extra Flugzeugproduktions- und Vertriebs GmbH: from 15 of September 2003 th SST FLUGTECHNIK GmbH: from 17 of November 2014 III. Change Record Issue Date Changes TC Issue No. & Date th Issue 01 16 July 2004 Change to EASA TCDS; addition of Model EA 400-500 Original, 16 of July 2004 Issue 02 26. November Editorial changes (Info: EASA TCDS replaces LBA TC N° 1085) Issue 03 16. June IFR day/night certification EA 400-500 Issue 04 24. Februrary EA 400-500: Added option of reduced MTOW 1999kg Issue 05 17. November Type Certificate Transfer to SST FLUGTECHNIK GmbH iaw. Part Revision 1, 17 2014 21, Subpart B, Point 21.A.47 of November Issue 06 Issue 06, 14 Added sections A.VI and B.VI to refer to Operational Suitability Data 14 Dec. 2015 December (OSD) including Notes IV. Notes for all EA400 variants 1. OSD In the absence of an operational evaluation at the entry into service of the EA400 / EA400-500, a type-rating requirement was established by the JAA. With the outcome of the OSD-FCD aircraft evaluation from 07-10 Dec 2015 all the EA400 / EA400-500 are thereafter subject to a Class Rating (prior this date it was a Type Rating) , as follows: Model EA400 as class rating with the license endorsement "SEP (land)” and Model EA400-500 as class rating with the license endorsement "Extra500 SET".