# TCDS A56EU: British Aerospace Regional Aircraft - Type: Type certificate data sheet - Status: Current - Holder: British Aerospace Regional Aircraft - Revision: 7 - Revised: March 2, 2007 - Product: Aircraft, Small/Large Airplane - Certification basis: Part 21, Part 23, Part 25, Part 36, Part 135 - Data sheet PDF: https://openairdocs.org/files/sha256/9b/0e/9b0ee28b2b12d14bed213de7b8adde8cd8132aa4b65388fa172d1e7670936a28 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6BA8C6358B963F0486257625004E9A9D.0001 - Page: https://openairdocs.org/tcds/A56EU ## Models (1) As the data sheet lists them. - Jetstream 3201 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 3 4 5 6 Rev. No. 7 2 7 7 7 2 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A56EU Revision 7 Jetstream Aircraft Limited (British Aerospace) Jetstream Model 3201 March 2, 2007 TYPE CERTIFICATE DATA SHEET No. A56EU This data sheet which is part of Type Certificate No. A56EU, prescribes conditions and limitations under which the product for which the type certificate was issued, meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder. British Aerospace Regional Aircraft Prestwick International Airport Ayrshire KA9 2RW S c o t l a n d I. Jetstream Model 3201 (Commuter Category), approved September 30, 1988. Engine. 2 Garrett TPE 331-12UA-701H (Mod. 8001) or TPE 331-12UAR-701H (Mods. 8020, 8112, 8127) or TPE 331-12UAR-702H (Mod. 8135) or TPE 331-12UAR-703H (Mod. 8132) or TPE 331-12UAR-704H (Mod. 8138) or TPE 331-12UAR-705H (Mod. 8161) or TPE 331-12UAR-706H (Mod. 8162) or TPE 331-12UAR-707H (Mod. 8163) or TPE 331-12UAR-708H (Mod. 8164) or TPE 331-12UHR-701H (Mod. 8205A or B) or TPE 331-12UHR-702H (Mod. 8205A or B) or TPE 331-12UHR-703H (Mod. 8205A or B) or TPE 331-12UHR-704H (Mod. 8205A or B) Both engines must ha ve the same model number. Fuel. American British NATO A S T M J e t A ASTM Jet A1 D.Eng.RD 2494 F-35 MIL-T-83133, JP8* D.Eng.RD 2453* F-34* Fuel marked thus * contain fuel system icing inhibitor (FSII) and no further additions shall be made. (Specifications as revised) Oil. American NATO (Engine & Gearbox) MIL-L-23699B 0-156 (Specifications as revised) A56EU Page 2 of 6 Engine Limits. Static Ratings The static ratings for the Garrett e ngines are based on the conditions specified o n T C D S E 4 W E . E x h a u s t G a s T e m p . ( E G T ) Shaft Horse Prop Shaft Single Red Conditions Power (SHP) Speed (RPM) Line (°C) Take-off 1020 1591 650 (Pre-Mod 8191) and or 660 (Post-Mod 8191) Max. cont. Starting - - 770 All new and overhauled engines must meet the above acceptable limits. See CAA-approved Flight Manual HP.4 .16 for additional engine Operating Limitations. Propeller and 2 Dowty Rotol (c) R.333/4-82-F/12 Propeller Limits. Blades : 4 (See Note 6) Diameter : 106 inches (No reduction permitted) Pitch angles at Section J-J setting line: Start Locks - 1° 45' + 0° 30' Flight Idle + 9° + 0° 30' Feathered + 82° 20' ± 0° 20' Reverse - 13° + 0° 30' or 2 McCauley 4HFR34C653/L106FA (Mod. 8133) B l a d e s : 4 Diameter : 106 inches - one inch reduction permitted Pitch angles at 30 inch radius setting line: S t a r t L o c k s + 9 ° ± 2 4 ' Flight idle + 15°45' ± 6' Feathered + 88° ± 30' Reverse - 4° ± 24' Airspeed Limits. V MO (Maximum Operating Speed) up to 16,750 ft 250 knots at 25,000 ft 210 knots V A (Manoeuvering Speed) 180 knots V FE (Flaps Extended Speed) Take-off (Flaps 10°) 170 knots Approach (Flaps 20°) 160 knots Landing (Flaps 35°) 150 knots Lift Dump (Flaps 70°) 120 knots V LE (Landing Gear Extended Speed) 160 knots V LO (Landing Gear Operating Speed) 160 knots V MC (Minimum Control Speed) Take-off (Flaps 10°) 100 knots N o t e : V MC at sea level/15°C standard atmosphere condition. See FAA- approved Flight Manua l HP.4.16 for other conditions. C.G. Limit. (+ 213.5 in.) to (+ 227.5 in.) at 11,000 lb or less; (Landing Gear Extended (+ 219.0 in.) to (+ 227.5 in.) at 16,204 lb take-off weight. Straight line variation between points given. Moment change (landing gear retraction) -4550 lb in. ( m o v e s C . G . f o r w a r d ) Datum. Fuselage station '0' (140 inches forward of marked "cowling type" screw on the bottom surface of fuselage). Page 3 of 6 A56EU Levelling Means. Levelling marks provided on fuselage seat rails. At station 225.5 left and right. At station 252.5 right only. Maximum Weight. Ramp 16,314 lb (7400 kg) Take-off 16,204 lb (7350 kg) Landing 15,609 lb (7080 kg) Zero fuel 14,330 lb (6500 kg) (Pre-Mod 8177) or 14,850 lb (6736 kg) (Post-Mod 8177) Minimum Crew. 2 pilots. Maximum Passengers. 19. Maximum Baggage. 695 lb. (+ 377.0 in.), or as otherw ise placarded at baggage compartment. Fuel Capacity. 493 U.S. Gals. in 2 tanks (+ 225.6 in.); 488 U.S. Gals. usable. (See NOTE 1 for data on system fuel) Oil Capacity. 1.56 U.S. Gals./tank in each engine compartment (+ 179.8 in.); 1.50 U.S. Gals./tank usable; (See NOTE 1 for data on system oil) Maximum Operating Altitude 25,000 ft. Control Surface Elevator 28° Up 15° Down Elevator Trim Tab 5.5° Up 8.5° Down Rudder 25° Right 25° Left Rudder Trim Tab 25° Right 25° Left, relative to 7.75° Right (neutral) Aileron 25° Up 15° Down Aileron Trim Tab 8.5° Up 8.5° Down F l a p s T a k e - o f f 1 0 ° D o w n Approach 20° Down Landing 35° Down Lift Dump 70° Down DATA PERTINENT TO ALL MODELS Serial Numbers Eligible. The United Kingdom Certificate of Airworthiness for Export endorsed as noted under "Import Requirements" must be submitted for each individual aircraft for which application for certification is made. Import Requirements. A United States Airworthiness Certificate may be issued on the basis of a United Kingdom Certificate of Airworthiness for Export signed by a representative of the United Kingdom Civil Aviation Authority containing the following statement; "The airplane covered by this certificate has been examined, tested and found to conform to the 14 CFR Part 23 type design approved under U.S. Type Certificate A56EU and is to be in a condition for safe operation". Certification Basis. - FAR 21.29 and FAR Part 23, effective February 1, 1965 including (See Note 4) Amendments 23-1 through 23.34; - Special Conditions No. 23-ACE-36 issued April 12, 1988 for Automatic Power Reserve (APR) Systems and Alcohol-Water Injection (AWI) Systems; - Federal Aviation Administrati on Exemption No. 4908 issued May 20, 1988 to allow certification with one la rger overwing exit on the side opposite the main entrance door in lieu of the two smaller exits required by Section 23.807(d)(1)(ii); A56EU Page 4 of 6 - Federal Aviation Administrati on Exemption No. 4927 issued August 24, 1988 to allow compliance to be shown with the Ground Load and Landing Gear requirements of FAR Part 25 in effect on June 1, 1987 in lieu of the corresponding requirements of FAR Part 23 in effect on June 1, 1987; - - Special Federal Aviation Regul ation No. 27-5, effective March 18, 1986: The approved Garrett TPE 331 engines comply with the fuel venting emission requirements of SFAR 27 with the installation of Garrett Fuel Manifold Purge System Kit No. 3101458-1; - FAR Part 36, effective December 1, 1969 including Amendments 36-1 through 36-15. Date of application for Type Certificate Jetstream Model 3201: June 1, 1987. The U.S. airworthiness certification basis for aircraft type certificated under FAR Section 21.29 and exported by the country of manufacture is FAR Section 21.183(c). The United Kingdom CAA originally type certificated this aircraft under is type certificate Number BA15. The FAA validated this product under U.S. Type Certificate number A56EU. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of the United Kingdom CAA. Service Information. The Type Certificate for Jetstream Model 3201 (Series 3200) is held by BAE SYSTEMS (Operations) Ltd of Prestwick International Airport, Flight Manual, Overhaul and Maintenance Manuals, Manufacturer's Operating Manual, Structural Repair Manual, Service Bulletins, Technical Information Leaflets, Vendor Manuals, including amendments thereto, and related documents, issued by either: British Aerospace PLC - Civil Aircraft Division - Prestwick, or British Aerospace (Commercial Aircraft) Limited - Airlines Division - Prestwick, or British Aerospace Regional Aircraft Limited - Prestwick, or Jetstream Aircraft Limited or BAE SYSTEMS (Operations) Ltd, which contain a statement that the document is CAA approved, or CAA approved through the Manufacturer's CAA Approval Ref DAI/1743/44 or DAI/1011/55 or DAI/9386/92 or JAA JAR 21 Approval Ref. CAA.JA02034, are accepted by the FAA and are considered FAA approved. These approvals pertain to the type design only. Other available service documents that are required for the British Aerospace Jetstream include: 1) SA.4-3100/ AMM/xxx Maintenance Manual 2) SA.4-3100/MS/2 Maintenance Schedule, including appropriate supplements 3) SA.4-3100/WM/xxx Wiring Diagram Manual 4) SA.4-3100/ITEM/1 Illustrated Tool & Equipment Manual 5) SA.4-3100/IPC/1 Illu strated Parts Catalogue 6) SA.4-3100/CMM/xxx Component Maintenance Manual 7) SA.4-3100/QEC/1 Quick Engine Change Manual 8) SA.4-3100/SRM/1 Structural Repair Manual 9) SA.4-3100/WBM/xxx Weight and Balance manual Each of the documents listed below must state that it is approved by the European Aviation Safety Agency (EAS A) or – for approvals made before September 28, 2003 – by the United Kingdom CAA. • Service bulletins, Page 5 of 6 A56EU • Structural repair manuals, • Vender manuals, • Aircraft flight manuals, and • Overhaul and maintenance manuals. The FAA accepts such documents and considers the FAA-approved unless on of the following conditions exits: • The documents change the limitations, performance, or procedures of the FAA approved manuals: or • The documents make an acoustical or emissions change to this product’s U. S. type certificate as defined in 14 CFR 21.93. The FAA uses the post type validation pr ocedures to approve these documents. The FAA may delegate on case-by-case to EASEA to approve on Behalf of the FAA for the U.S. type certificate. If this is the case it will be noted on the document. Equipment. The basic equipment as prescribed in the applicable airworthiness regulations (See Note 5) (see Certification Basis) must be installed in the airplane. British Aerospace Illustrated Parts Catalogue Docu ment No. SA.4-3100/IPC/1 identifies all required equipment and all optional equipment approved by the CAA of the United Kingdom. In addition, CAA- Approved Flight Manual HP.4.16, as appropriately amended in relation to the actual modification standard of the airplane is required. NOTES: NOTE 1. Current weight and balance report, including list of equipment included in the certified empty weight and loading instructions when necessary, mu st be in each airplane at the time of original certification and at all times thereafter (except in the case of operators having an approved weight control system). The certificated empty weight and correspondi ng center of gravity locations must include: Unusable fuel of 38 lb. at (+ 215.6 in.) Unusable oil of 7 lb. at (+ 200.0 in.) NOTE 2. The following placards must be displayed in full view of the pilot: a) "This airplane must be operated as a commu ter category airplane in compliance with the operating limitations stated in the form of placards, markings and manuals. No aerobatic manoeuvers, including spins, approved". Footnote All placards required in the FAA-approved Flight Manual must be installed in the appropriate locations. b) Each individual airplane will be supplied with a placard that specifies the kinds of operation, such as VFR or IFR, Day and Night to which the operation of the airplane is limited by the equipment installed. NOTE 3. The service life limits for ai rcraft structural parts which are fatigue critical are listed in the Airworthiness Limitations Section 5 of Ma intenance Manual Doc No. SA-4-3100/MM/XXX for the airplane. NOTE 4. Compliance with the Special Conditions for AWI systems has been shown for BAe Modification No. KIT 3465. Embodiment of this Modification requires the incorporation of Supplement No. S1 and Particular Amendments Nos. P/4 and P/14 in CAA-approved Flight Manual HP.4.16 for the airplane. Compliance with the Special Conditions for APR systems has been shown for BAe Modification A56EU Page 6 of 6 No. KIT 3469. Embodiment of this Modification re quires the incorporation of Supplement No S2 in CAA-Approved Flight Manual HP.4.16 for the airplane. Modifications Nos KIT 3465 and KIT 3469 cannot be simultaneously embodied on the same airplane. NOTE 5. The Flight Data Recorder of BAe KIT 2625 installed under cover of BAe Modification No KIT 2616 (or equivalent installation modification), doe s not comply with the requirements of FAR 135.152(a) as insufficient parameters are being r ecorded and is not approved for installation on aircraft which are brought onto the US register after October 11, 1991. NOTE 6. The Dowty Rotol propeller is compatib le only with Garrett TPE 331-12UA(R)-701H, 12UAR- 703H, 12UAR-705H, 12UAR-707H, 12UHR-701H and 12UHR-703H engines. The McCauley propeller is compatible onl y with Garrett TPE 331-12UAR-702H, 12UAR-704H, 12UAR-706H, 12UAR-708H, 12UHR-702H and 12UHR-704H engines. Embodiment of McCauley propellers requires the in corporation of Particular Amendment No P/17 in the basic part of CAA-Approved Flight Manua l HP.4.16 and the incorporation of Particular Amendment No P/22 in Supplemen t No 52 in the CAA-Approved Flight Manual HP.4.16 for the airplane. .....END..... ``` ## ADs (68, first 50, in force first) - [AD 2023-19-05](https://openairdocs.org/ad/2023-19-05): Rudder Tab Control System; Fuselage Main, Plate/Skin · British Aerospace Regional Jetstream Series 3101 and Jetstream 3201. Effective Nov 6, 2023 - [AD 2022-12-09](https://openairdocs.org/ad/2022-12-09): Main Landing Gear Attach Section · BAE Systems Jetstream Series 3101, H.P. 137 Jetstream Mk. 1, Jetstream Series 200 and 1 more. Effective Jul 21, 2022 - [AD 2022-11-16](https://openairdocs.org/ad/2022-11-16): Rudder Control System, Elevator Control System · BAE Systems Jetstream Series 3101 and Jetstream 3201. Effective Jul 13, 2022 - [AD 2022-03-18](https://openairdocs.org/ad/2022-03-18): Gust Lock/Damper System · BAE Systems Jetstream Series 200, Jetstream 3201 and Jetstream Series 3101. Effective Mar 21, 2022 - [AD 2018-02-15](https://openairdocs.org/ad/2018-02-15): Landing Gear · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Mar 5, 2018 - [AD 2015-16-05](https://openairdocs.org/ad/2015-16-05): Landing Gear · British Aerospace Regional Jetstream 3201 and Jetstream Series 3101. Effective Sep 21, 2015 - [AD 2015-16-06](https://openairdocs.org/ad/2015-16-06): Wings · British Aerospace Regional Jetstream 3201. Effective Sep 21, 2015 - [AD 2015-06-01](https://openairdocs.org/ad/2015-06-01): Landing Gear · British Aerospace Regional Jetstream 3201 and Jetstream Series 3101. Effective Apr 24, 2015 - [AD 2014-13-05](https://openairdocs.org/ad/2014-13-05): Time Limits · British Aerospace Regional Jetstream 3201. Effective Aug 5, 2014 - [AD 2011-11-01](https://openairdocs.org/ad/2011-11-01): Landing Gear · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Jun 22, 2011 - [AD 2010-25-02](https://openairdocs.org/ad/2010-25-02): Landing Gear · British Aerospace Regional Jetstream 3201 and Jetstream Series 3101. Effective Jan 11, 2011 - [AD 2010-09-02](https://openairdocs.org/ad/2010-09-02): Flight Controls · British Aerospace Regional Jetstream 3201 and Jetstream Series 3101. Effective Jun 3, 2010 - [AD 2010-08-04](https://openairdocs.org/ad/2010-08-04): Landing Gear · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective May 19, 2010 - [AD 2009-19-03](https://openairdocs.org/ad/2009-19-03): Landing gear · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Oct 5, 2009 - [AD 2008-12-02](https://openairdocs.org/ad/2008-12-02): Nose-wheel · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Jul 16, 2008 - [AD 2008-06-12](https://openairdocs.org/ad/2008-06-12): Steering jack gland housing · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Apr 16, 2008 - [AD 2007-21-17](https://openairdocs.org/ad/2007-21-17): Landing gear radius rods · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Nov 28, 2007 - [AD 2007-15-01](https://openairdocs.org/ad/2007-15-01): Wing spigot post assembly · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Aug 22, 2007 - [AD 2003-04-07](https://openairdocs.org/ad/2003-04-07): Horizontal and Vertical Stabilizer Attachment Fittings and Associated Hardware · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Apr 7, 2003 - [AD 2002-20-08](https://openairdocs.org/ad/2002-20-08): Fuel quantity indication system · British Aerospace Regional Jetstream 3201. Effective Dec 18, 2002 - [AD 2002-01-05](https://openairdocs.org/ad/2002-01-05): Main Landing Gear Radius Rods · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Feb 11, 2002 - [AD 2001-03-11](https://openairdocs.org/ad/2001-03-11): Main Landing Gear Radius Rods · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Apr 6, 2001 - [AD 2001-01-02](https://openairdocs.org/ad/2001-01-02): Steering Jack Assembly · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Mar 5, 2001 - [AD 2001-01-03](https://openairdocs.org/ad/2001-01-03): Nose Landing Gear Steering Actuator · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Feb 24, 2001 - [AD 2000-20-13](https://openairdocs.org/ad/2000-20-13): Rudder Quadrant Support Structure · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Nov 27, 2000 - [AD 2000-16-13](https://openairdocs.org/ad/2000-16-13): Nose Wheel Steering System · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Sep 29, 2000 - [AD 99-15-11](https://openairdocs.org/ad/99-15-11): NLG Steering Selector Valve · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Sep 10, 1999 - [AD 99-07-09](https://openairdocs.org/ad/99-07-09): Hydraulic Components · British Aerospace Regional Jetstream 3201. Effective May 10, 1999 - [AD 99-06-11](https://openairdocs.org/ad/99-06-11): Elevator Bias Spring Assembly · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Apr 26, 1999 - [AD 99-06-12](https://openairdocs.org/ad/99-06-12): Nose Landing Gear Steering · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Apr 26, 1999 - [AD 99-04-21](https://openairdocs.org/ad/99-04-21): MLG Brakes Units · British Aerospace Regional Jetstream 3201 and Jetstream Series 3101. Effective Apr 2, 1999 - [AD 98-26-17](https://openairdocs.org/ad/98-26-17): MLG Bay Auxiliary Spar Booms · British Aerospace Regional Jetstream 3201. Effective Feb 5, 1999 - [AD 98-21-25](https://openairdocs.org/ad/98-21-25): Ground Inhibit Relay · British Aerospace Regional Jetstream 3201 and Jetstream Series 3101. Effective Nov 26, 1998 - [AD 98-12-23](https://openairdocs.org/ad/98-12-23): Windshield Wiper Arm and NLG Toggle and Axle Bracket Lugs · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Jul 28, 1998 - [AD 97-24-07](https://openairdocs.org/ad/97-24-07): Magnetically ltching Relays · British Aerospace Regional Jetstream 3201 and Jetstream Series 3101. Effective Dec 31, 1997 - [AD 97-07-11](https://openairdocs.org/ad/97-07-11): NLG Actuator Support Structure · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective May 23, 1997 - [AD 96-17-12](https://openairdocs.org/ad/96-17-12): Nose Landing Gear Bolts · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Oct 21, 1996 - [AD 96-13-02](https://openairdocs.org/ad/96-13-02): Inspect Spigot Housing Plate · British Aerospace Regional Jetstream 3201. Effective Aug 7, 1996 - [AD 96-11-01](https://openairdocs.org/ad/96-11-01): Automatic Airframe De-Ice System · British Aerospace Regional Jetstream 3201 and Jetstream Series 3101. Effective Jul 2, 1996 - [AD 96-09-17](https://openairdocs.org/ad/96-09-17): AFM - Icing · British Aerospace Regional Jetstream 3201 and Jetstream Series 3101. Effective Jun 11, 1996 - [AD 95-24-12](https://openairdocs.org/ad/95-24-12): MLG Bay Forward Lower Edge Wing Skin · British Aerospace Regional Jetstream 3201. Effective Jan 17, 1996 - [AD 95-24-13](https://openairdocs.org/ad/95-24-13): Inspect Mounting Spigots · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Jan 17, 1996 - [AD 94-24-01](https://openairdocs.org/ad/94-24-01): Flap Torque Shaft Assembly · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Dec 1, 1995 - [AD 95-17-10](https://openairdocs.org/ad/95-17-10): Central Annunciator Panel Test Button Circuit · British Aerospace Regional Jetstream 3201 and Jetstream Series 3101. Effective Oct 3, 1995 - [AD 95-15-13](https://openairdocs.org/ad/95-15-13): Passenger/Crew Door · British Aerospace Regional Jetstream 3201 and Jetstream Series 3101. Effective Sep 7, 1995 - [AD 95-12-06](https://openairdocs.org/ad/95-12-06): Shear Fitting of Right-Hand Escape Hatch · British Aerospace Regional Jetstream 3201 and Jetstream Series 3101. Effective Jul 24, 1995 - [AD 95-11-17](https://openairdocs.org/ad/95-11-17): Electrical System · British Aerospace Regional Jetstream 3201 and Jetstream Series 3101. Effective Jul 19, 1995 - [AD 95-02-05](https://openairdocs.org/ad/95-02-05): Passenger/Crew Door Internal Handle · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Mar 17, 1995 - [AD 95-02-19](https://openairdocs.org/ad/95-02-19): Inspect Left & Right Windscreen · British Aerospace Regional H.P. 137 Jetstream Mk. 1, Jetstream 3201, Jetstream Series 200 and 1 more. Effective Mar 10, 1995 - [AD 93-08-10](https://openairdocs.org/ad/93-08-10): AFM Preflight Main Cabin Door Checks · British Aerospace Regional Jetstream 3201 and Jetstream Series 3101. Effective May 14, 1993 All 68: https://openairdocs.org/tcds/A56EU/ads.md ## Registered aircraft by registry model (OpenAirDocs) - [British Aerospace JETSTREAM 3201](https://openairdocs.org/model/british-aerospace-jetstream-3201): 0 aircraft (registry code 1500219) ## STCs approved under this data sheet (68, first 50) - [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc. - [STC SA5884NM](https://openairdocs.org/stc/SA5884NM): Installation of interior fluorescent cabin lighting system.. Bruce Aerospace Inc. - [STC SA03020AT](https://openairdocs.org/stc/SA03020AT): Installation of a Sandel Model ST3400 Terrain Awareness and Warning System (TAWS). Woven Electronics LLC - [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited - [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH - [STC ST03269AT](https://openairdocs.org/stc/ST03269AT): Installation of a Honeywell CAS 67A Traffic Alert and Collision Avoidance System IT (TCAS IT) and Dual MST 67A Mode S Transponder. Woven Electronics LLC - [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT).. Woven Electronics LLC - [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC - [STC SA00105WI-D](https://openairdocs.org/stc/SA00105WI-D): Installation of provisions for Bendix/King CAS 66A TCAS I System.. Honeywell International Inc - [STC SA02677LA](https://openairdocs.org/stc/SA02677LA): Modification to upgrade the existing Mode S Transponder system by installing the ACSS NXT-700 Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS as the position source for ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC SA02678LA](https://openairdocs.org/stc/SA02678LA): Modification to upgrade the existing Mode S Transponder system by installing the ACSS NXT-600 Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS as the position source for ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies - [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS - [STC SA02177CH](https://openairdocs.org/stc/SA02177CH): Install air ambulance conversion.. Spectrum Aeromed LLC dba Spectrum Aeromed - [STC SA01513SE](https://openairdocs.org/stc/SA01513SE): Installation of the Sandel Terrain Awareness Warning System (TAWS). Cascade Aviation Services Inc - [STC SA01806WI](https://openairdocs.org/stc/SA01806WI): Modification of Rockwell Collins TCAS II System Installation with DC powered TCAS Transmitter Receiver Processor. Rockwell Collins Inc - [STC SA00674WI-D](https://openairdocs.org/stc/SA00674WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II system installation.. Rockwell Collins Inc - [STC SA00907WI-D](https://openairdocs.org/stc/SA00907WI-D): Modification of a Rockwell Collins, Inc. TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc - [STC SA482NE](https://openairdocs.org/stc/SA482NE): Remove existing starter-generator and install Aircraft Parts starter - generator P/N 300SG121Q.. Shurka Aerospace Inc - [STC ST02540AT-D](https://openairdocs.org/stc/ST02540AT-D): Installation of replacement fuel tank sealant system. FFC Manufacturing - [STC SA02621CH](https://openairdocs.org/stc/SA02621CH): Installation of a cargo door. Murray Aircraft Modifications - [STC SA02593CH](https://openairdocs.org/stc/SA02593CH): Installation of a cargo floor. Murray Aircraft Modifications - [STC SA02592CH](https://openairdocs.org/stc/SA02592CH): Installation of a pressure bulkhead. Murray Aircraft Modifications - [STC SA02542CH](https://openairdocs.org/stc/SA02542CH): Install Cargo Net. Murray Aircraft Modifications - [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc - [STC SA01306WI-D](https://openairdocs.org/stc/SA01306WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation.. Rockwell Collins Inc - [STC ST02284NY](https://openairdocs.org/stc/ST02284NY): Installation of Concorde RG-380 Battery.. Infinion Certification Engineering Inc. - [STC SA01141WI-D](https://openairdocs.org/stc/SA01141WI-D): Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94 Mode S Transponder System installation with CTL-92E control head.. Rockwell Collins Inc - [STC SA10188SC](https://openairdocs.org/stc/SA10188SC): Cabin reconfiguration.. Rose Aircraft Interiors, Inc. - [STC SA1416GL](https://openairdocs.org/stc/SA1416GL): Installation of McCauley Model 4HFR34C653/L106FA-0 propellers.. McCauley Propeller Systems - [STC SA01313WI-D](https://openairdocs.org/stc/SA01313WI-D): Modification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installation in accordance with Collins Drawing Index as listed on AML No. SA01313WI-D, Revision -, or later FAA approved revision.. Rockwell Collins Inc - [STC ST03088AT](https://openairdocs.org/stc/ST03088AT): Installation of a Honeywell MK VI Enhanced Ground Proximity Warning Systems (EGPWS). Chippewa Aerospace, Inc. - [STC SA01945NY](https://openairdocs.org/stc/SA01945NY): Cockpit voice recorder replacement with Universal CVR 30B or CVR 120.. MidCanada Mod Center - [STC SA01874CH](https://openairdocs.org/stc/SA01874CH): Replacement of certain Goodrich pneumatic deicer boots.. SMR Technologies - [STC SA4963NM](https://openairdocs.org/stc/SA4963NM): Installation of a NSA sunvisor system.. Rosen Sunvisor Systems LLC - [STC SA7512SW](https://openairdocs.org/stc/SA7512SW): Installation of an external baggage pod.. BAE Systems Regional Aircraft Inc. - [STC SP00922CH](https://openairdocs.org/stc/SP00922CH): Installation of various SMR Technologies electrical propeller de-icer models. (RHFR34C6( ) 53/L106FA-0) (HC-B4T N-5ML/LT10574). SMR Technologies - [STC SA00084DE-D](https://openairdocs.org/stc/SA00084DE-D): Installation of Sundstrand MK-VI GPWS system.. Learjet Inc - [STC SA00085DE-D](https://openairdocs.org/stc/SA00085DE-D): Installation of Bendix/King CAS-66 TCAS I system.. Learjet Inc - [STC SA00086DE-D](https://openairdocs.org/stc/SA00086DE-D): Installation of Radio Altimeter System.. Learjet Inc - [STC SA00091DE-D](https://openairdocs.org/stc/SA00091DE-D): Installation of Collins TCAS-94 TCAS II System.. Learjet Inc - [STC SA01046WI](https://openairdocs.org/stc/SA01046WI): Installation of a two-place side facing divan.. Aviation Fabricators Inc - [STC SA00845WI-D](https://openairdocs.org/stc/SA00845WI-D): Modification of Collins TCAS II or TCAS-94 (TCAS II) system installation with Collins TTR-920 Change 7.0 Receiver Transmitter to a Collins TCAS II or TCAS-94 (TCAS II) system installation with Collins TTR-921 or Collins TTR-4000 Change 7.0 TCAS II receiver transmitter.. Rockwell Collins Inc - [STC SA7595SW](https://openairdocs.org/stc/SA7595SW): Installation of a freon air conditioning system.. AAR Airframe and Accessories Group Inc - [STC SA7597SW](https://openairdocs.org/stc/SA7597SW): Installation of dual auxiliary electric heater systems.. AAR Airframe and Accessories Group Inc - [STC SA7616SW](https://openairdocs.org/stc/SA7616SW): Installation of a cabin air temperature gage.. AAR Airframe and Accessories Group Inc - [STC ST02151AT](https://openairdocs.org/stc/ST02151AT): Installation of a heads-up cabin briefer (HUCAB).. CCAir, Inc. - [STC SA7514SW](https://openairdocs.org/stc/SA7514SW): Installation of tail floodlights.. DeVore Aviation Corporation of America, a New Mexico Corporation - [STC SA8729SW-D](https://openairdocs.org/stc/SA8729SW-D): Installation of Sundstrand ground proximity warning system (GPWS) Mark VI.. Sierra Industries, Inc - [STC SA8002SW](https://openairdocs.org/stc/SA8002SW): Installation of Fairchild A100 cockpit voice recorder.. British Aerospace Reg Aircraft, Inc All 68: https://openairdocs.org/tcds/A56EU/stcs.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.