# Britten-Norman BN-2A-20

- Type: Aircraft model (FAA registry)
- Registry code: 1520220
- Manufacturer (registry): BRITTEN-NORMAN
- Model: BN-2A-20
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Reciprocating
- Seats: 10
- Weight class: Up to 12,499 lb
- Cruise speed: 92 mph
- Certification: Type certificated
- Data sheet: [TCDS A17EU](https://openairdocs.org/tcds/A17EU) (OpenAirDocs)
- Holder: Britten-Norman Aerospace Ltd.
- Registered aircraft: 3
- Page: https://openairdocs.org/model/britten-norman-bn-2a-20

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2025-01-01](https://openairdocs.org/ad/2025-01-01): Landing Gear System · Britten-Norman Aerospace BN-2, BN-2A, BN-2A-2 and 18 more. Effective Mar 11, 2025
- [AD 2024-08-03](https://openairdocs.org/ad/2024-08-03): Flight Control System Wiring · Britten-Norman BN-2, BN-2A, BN-2A-2 and 18 more. Effective Jun 3, 2024
- [AD 2021-18-01](https://openairdocs.org/ad/2021-18-01): Rudder Control System · B-N Group BN-2, BN-2A, BN-2A-2 and 14 more. Effective Oct 14, 2021
- [AD 2016-26-09](https://openairdocs.org/ad/2016-26-09): Navigation · B-N Group BN-2, BN-2A, BN-2A-2 and 17 more. Effective Feb 9, 2017
- [AD 2016-04-05](https://openairdocs.org/ad/2016-04-05): Engine Controls · B-N Group BN-2, BN-2A, BN-2A-2 and 15 more. Effective Mar 24, 2016
- [AD 2013-13-02](https://openairdocs.org/ad/2013-13-02): Fuel · B-N Group BN-2, BN-2A, BN-2A-2 and 17 more. Effective Aug 1, 2013
- [AD 2011-05-09](https://openairdocs.org/ad/2011-05-09): Flight Controls · B-N Group BN-2, BN-2A, BN-2A-2 and 14 more. Effective Apr 26, 2011
- [AD 2006-23-03](https://openairdocs.org/ad/2006-23-03): Horizontal stabilizer attachment bolts · B-N Group BN-2, BN-2A, BN-2A-2 and 14 more. Effective Dec 14, 2006
- [AD 2006-16-19](https://openairdocs.org/ad/2006-16-19): Elevator final drive control rods. · B-N Group BN-2, BN-2A, BN-2A-2 and 14 more. Effective Sep 18, 2006
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2002-25-05](https://openairdocs.org/ad/2002-25-05): Universal joint · B-N Group BN-2, BN-2A, BN-2A-2 and 17 more. Effective Feb 3, 2003
- [AD 2002-25-03](https://openairdocs.org/ad/2002-25-03): Left-hand rudder bar · B-N Group BN-2A, BN-2A-2, BN-2A-20 and 10 more. Effective Jan 31, 2003
- [AD 2002-22-02](https://openairdocs.org/ad/2002-22-02): Engine Mount Bracket · B-N Group BN-2, BN-2A, BN-2A-2 and 17 more. Effective Dec 20, 2002
- [AD 2002-03-04](https://openairdocs.org/ad/2002-03-04): Emergency Exit Window Sealant · B-N Group BN-2, BN-2A, BN-2A-2 and 17 more. Effective Mar 29, 2002
- [AD 2002-02-11](https://openairdocs.org/ad/2002-02-11): Oleo Attachment Brackets · B-N Group BN-2, BN-2A, BN-2A-2 and 17 more. Effective Mar 25, 2002
- [AD 2002-02-10](https://openairdocs.org/ad/2002-02-10): Inboard Brackets of Elevator Outboard Hinge · B-N Group BN-2, BN-2A, BN-2A-2 and 14 more. Effective Mar 25, 2002
- [AD 2002-01-11](https://openairdocs.org/ad/2002-01-11): Throttle Friction-Shaft · B-N Group BN-2, BN-2A, BN-2A-2 and 17 more. Effective Feb 28, 2002
- [AD 98-18-07](https://openairdocs.org/ad/98-18-07): Generator System · B-N Group BN-2, BN-2A, BN-2A-2 and 15 more. Effective Oct 12, 1998
- [AD 98-16-14](https://openairdocs.org/ad/98-16-14): Main Landing Gear Fitting Attachment Bolts, Nuts, and Washers · B-N Group BN-2, BN-2A, BN-2A-2 and 14 more. Effective Sep 21, 1998
- [AD 98-04-17](https://openairdocs.org/ad/98-04-17): Diodes On Terminal Switches · B-N Group BN-2, BN-2A, BN-2A-2 and 15 more. Effective Mar 23, 1998
- [AD 98-04-21](https://openairdocs.org/ad/98-04-21): Airplane Flight Manual (AFM) - Limitations - Icing · B-N Group BN-2A, BN-2A-2, BN-2A-20 and 16 more. Effective Mar 13, 1998
- [AD 97-22-01](https://openairdocs.org/ad/97-22-01): Main Landing Gear Torque Link Assembly Area · B-N Group BN-2, BN-2A, BN-2A-2 and 13 more. Effective Nov 28, 1997
- [AD 97-22-02](https://openairdocs.org/ad/97-22-02): Engine Mounting Brackets, Bolts, and Bushes · B-N Group BN-2, BN-2A, BN-2A-2 and 17 more. Effective Nov 24, 1997
- [AD 96-18-21](https://openairdocs.org/ad/96-18-21): Aileron Mass Balance Clamp Unit · B-N Group BN-2, BN-2A, BN-2A-2 and 11 more. Effective Oct 25, 1996
- [AD 95-04-09](https://openairdocs.org/ad/95-04-09): Nose Wheel Steering System · B-N Group BN-2A, BN-2A-2, BN-2A-20 and 16 more. Effective Apr 14, 1995
- [AD 83-10-06 R1](https://openairdocs.org/ad/83-10-06-R1): Elevator Trim Tabs · B-N Group BN-2, BN-2A, BN-2A-2 and 15 more. Effective Feb 12, 1987
- [AD 86-23-02](https://openairdocs.org/ad/86-23-02): Modification NB/M/990 · B-N Group BN-2, BN-2A, BN-2A-2 and 11 more. Effective Dec 8, 1986
- [AD 83-23-01](https://openairdocs.org/ad/83-23-01): Wing Tank Fuel System Modification · B-N Group BN-2, BN-2A, BN-2A-2 and 15 more. Effective Dec 8, 1983
- [AD 83-07-12 R1](https://openairdocs.org/ad/83-07-12-R1): Fuel Transmitter Float Inspection · B-N Group BN-2, BN-2A, BN-2A-2 and 15 more. Effective Apr 11, 1983
- [AD 83-05-02](https://openairdocs.org/ad/83-05-02): Teleflex Swivel Assembly Inspection · B-N Group BN-2A, BN-2A-2, BN-2A-20 and 10 more. Effective Mar 7, 1983
- [AD 78-11-08](https://openairdocs.org/ad/78-11-08): Elevator and Flap Control Rods · B-N Group BN-2A, BN-2A-2, BN-2A-20 and 10 more. Effective Jun 6, 1978
- [AD 77-07-10](https://openairdocs.org/ad/77-07-10): Aileron Mass Balance Support Arm · B-N Group BN-2A, BN-2A-2, BN-2A-20 and 10 more. Effective Apr 18, 1977
- [AD 76-21-07](https://openairdocs.org/ad/76-21-07): Engine Mounting · B-N Group BN-2A, BN-2A-2, BN-2A-20 and 10 more. Effective Nov 5, 1976
- [AD 76-13-12](https://openairdocs.org/ad/76-13-12): Flap Retraction · B-N Group BN-2, BN-2A, BN-2A-2 and 6 more. Effective Jul 15, 1976
- [AD 76-06-05](https://openairdocs.org/ad/76-06-05): Pilot's Seat · B-N Group BN-2A, BN-2A-2, BN-2A-20 and 10 more. Effective Apr 19, 1976
- [AD 76-02-04](https://openairdocs.org/ad/76-02-04): Engine Mounting Frame · B-N Group BN-2A, BN-2A-2, BN-2A-20 and 10 more. Effective Jan 30, 1976
- [AD 75-26-01](https://openairdocs.org/ad/75-26-01): Rudder Control · B-N Group BN-2A, BN-2A-2, BN-2A-20 and 10 more. Effective Dec 23, 1975
- [AD 71-05-05](https://openairdocs.org/ad/71-05-05): Elevator Trim Tab System · B-N Group BN-2, BN-2A, BN-2A-2 and 11 more. Effective Jan 26, 1971
- [AD 70-12-11](https://openairdocs.org/ad/70-12-11): Flap Actuating System · B-N Group BN-2, BN-2A, BN-2A-2 and 11 more. Effective Jun 11, 1970
- [AD 70-07-05](https://openairdocs.org/ad/70-07-05): Carburetor Air Box · B-N Group BN-2, BN-2A, BN-2A-2 and 11 more. Effective Mar 31, 1970
- [AD 70-07-04](https://openairdocs.org/ad/70-07-04): Tail Plane Front Spar · B-N Group BN-2, BN-2A, BN-2A-2 and 11 more. Effective Mar 31, 1970
- [AD 70-06-05](https://openairdocs.org/ad/70-06-05): Elevator Trim System Drive · B-N Group BN-2, BN-2A, BN-2A-2 and 11 more. Effective Mar 17, 1970
- [AD 70-06-04](https://openairdocs.org/ad/70-06-04): Fuselage Attach Spindles · B-N Group BN-2, BN-2A, BN-2A-2 and 11 more. Effective Mar 17, 1970
- [AD 70-03-06](https://openairdocs.org/ad/70-03-06): Rudder Bar Assembly · B-N Group BN-2, BN-2A, BN-2A-2 and 11 more. Effective Feb 5, 1970
- [AD 70-02-06](https://openairdocs.org/ad/70-02-06): Elevator Trim Tab Attach · B-N Group BN-2, BN-2A, BN-2A-2 and 11 more. Effective Jan 11, 1970
- [AD 69-13-08](https://openairdocs.org/ad/69-13-08): Fuel Line Leak · B-N Group BN-2, BN-2A, BN-2A-2 and 11 more. Effective Jul 2, 1969
- [AD 69-13-01](https://openairdocs.org/ad/69-13-01): Nose Wheel Steering · B-N Group BN-2, BN-2A, BN-2A-2 and 11 more. Effective Jun 23, 1969

Historical (superseded or no longer in force):

- [AD 2016-06-01](https://openairdocs.org/ad/2016-06-01) (historical): Navigation · B-N Group BN-2, BN-2A, BN-2A-2 and 15 more. Effective Apr 19, 2016
- [AD 2014-03-18](https://openairdocs.org/ad/2014-03-18) (historical): Engine Controls · B-N Group BN-2, BN-2A, BN-2A-2 and 15 more. Effective Apr 1, 2014
- [AD 2007-06-06](https://openairdocs.org/ad/2007-06-06) (historical): Inner shell of the pitot/ static pressure heads · B-N Group BN-2, BN-2A, BN-2A-2 and 17 more. Effective Apr 20, 2007
- [AD 97-14-01](https://openairdocs.org/ad/97-14-01) (historical): Left-Hand Rudder Bar Assembly · B-N Group BN2A MK. 111, BN2A MK. 111-2, BN2A MK. 111-3 and 10 more. Effective Aug 18, 1997
- [AD 97-03-03](https://openairdocs.org/ad/97-03-03) (historical): Diodes On Terminal Switches · B-N Group BN-2, BN-2A, BN-2A-2 and 12 more. Effective Mar 23, 1997

## Information bulletins (advisory) (2)

- [SAIB CE-15-12](https://openairdocs.org/saib/CE-15-12): Flight Controls; Control System Interference with Access Panel Fasteners. Issued Apr 15, 2015
- [SAIB CE-07-15](https://openairdocs.org/saib/CE-07-15): FHL landing gear and components. Issued Feb 6, 2007

## Registered aircraft (3)

- [N442S](https://openairdocs.org/aircraft/N442S): [Griffing Flying Service Inc](https://openairdocs.org/faa-owner/GRIFFING%20FLYING%20SERVICE%20INC), [Port Clinton, OH](https://openairdocs.org/faa-place/OH/Port%20Clinton), built 1976, S/N 770
- [N4438](https://openairdocs.org/aircraft/N4438): [Spirit Air Inc](https://openairdocs.org/faa-owner/SPIRIT%20AIR%20INC), [Salmon, ID](https://openairdocs.org/faa-place/ID/Salmon), built 1976, S/N 766
- [N6561B](https://openairdocs.org/aircraft/N6561B): [Spirit Air Inc](https://openairdocs.org/faa-owner/SPIRIT%20AIR%20INC), [Salmon, ID](https://openairdocs.org/faa-place/ID/Salmon), built 1976, S/N 520

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA07CA221](https://openairdocs.org/ntsb/SEA07CA221), Jul 15, 2007: Britten-Norman BN-2A-20 (N6561B), Stanley, ID, substantial damage. Probable cause: The pilot's failure to verify that the airplane was refueled, which resulted in a loss of engine power from both engines due to fuel exhaustion and a forced landing. A contributing factor was the…
- [NTSB SEA07LA114](https://openairdocs.org/ntsb/SEA07LA114), Apr 28, 2007: Britten-Norman BN-2A-20 (N634MA), Hamilton, MT, substantial damage. Probable cause: The loss of power in one engine, for undetermined reasons, soon after establishing the takeoff departure climb. Factors include rough/uneven terrain.

## FAA accident and incident reports (4)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20220831008459I](https://openairdocs.org/incident/20220831008459I), Aug 31, 2022: Britten-Norman BN-2A-20 (N4438), Hat Creek, ID, No damage. Pilot had refueled the aircraft (N4438) the evening prior to this incident (8/30/2022) in salmon, ID (smn) and then flew it that evening on a FAR 135 flight to…
- [Accident 20070715015579A](https://openairdocs.org/incident/20070715015579A), Jul 15, 2007: Bnorm BN2A20 (N6561B), Stanley, ID, Substantial damage. (-23) After dropping off 8 passengers, the islander took off from Stanley airport, upon reaching 300 ft AGL, the port enigne lost power so pilot decided to…
- [Accident 20070428006199A](https://openairdocs.org/incident/20070428006199A), Apr 28, 2007: Bnorm BN2A20 (N634MA), Hamilton, MT, Destroyed. (-23) On April 28, 2007, at 10:59 a.m. mountain daylight time, a britten-norman BN-2A lost power to the right engine shortly after take-off at the Ravalli…
- [Incident 20001230039409I](https://openairdocs.org/incident/20001230039409I), Dec 30, 2000: Bnorm BN2A20 (N442S), Sandusky, OH, Minor damage. (-23) The pilot stated: that on Saturday December 30, 2000 on a detroit trip to sky, due to weather conditions of snow and blowing snow, he was unable to see…

## Service difficulty reports (16)

As reported by operators and repair stations, by the model named in the report.

- [SDR M2L2007F00001](https://openairdocs.org/sdr/M2L2007F00001), Apr 28, 2007: DRIVE GEAR. BROKEN. BENDIX DRIVE GEAR OF RT ENGINE BROKE LOCKING RING GEAR OF CRANKSHAFT LOCKING ENGINE TO A STOP CONDITION. (K)
- [SDR M2L2007F00000](https://openairdocs.org/sdr/M2L2007F00000), Apr 28, 2007: DRIVE GEAR. BROKEN. RT ENGINE STARTER DRIVE GEAR SHAFT WAS DAMAGED TO THE EXTENT, THAT THE BENDIX COULD NOT RETRACT FROM THE ENGAGED POSITION. THUS CAUSING THE GEAR TO REMAIN ENGAG
- [SDR AUS20030748](https://openairdocs.org/sdr/AUS20030748), Jul 14, 2003: INTAKE VALVE. FAILED. (AUS) NR 6 CYLINDER INTAKE VALVE BROKEN OFF AT UPPER PART OF VALVE STEM. BROKEN INTAKE VALVE CAUSED EXTENSIVE DAMAGE TO CYLINDER.
- [SDR AUS20020173](https://openairdocs.org/sdr/AUS20020173), Feb 18, 2002: THROTTLE. BROKEN. (AUS) LT ENGINE THROTTLE SLIDING END ASSEMBLY BROKEN.
- [SDR AUS20011394](https://openairdocs.org/sdr/AUS20011394), Dec 17, 2001: CAM. WORN. (AUS) MAGNETO IMPULSE CAM WORN BEYOND LIMITS.
- [SDR AUS20011357](https://openairdocs.org/sdr/AUS20011357), Dec 14, 2001: CAM. FAILED. (AUS) MAGNETO CAM PIVOT PIN HAD EXCESSIVE PLAY. PIN HAD APPROXIMATELY 0.508MM (0.020IN) OF PLAY. MAXIMUM PLAY 0.3556MM (0.014IN).
- [SDR AUS20010823](https://openairdocs.org/sdr/AUS20010823), Aug 3, 2001: INJECTOR. BLOCKED. (AUS) NO1 ENGINE FUEL INJECTOR NOZZLE PARTIALLY BLOCKED.
- [SDR AU001158](https://openairdocs.org/sdr/AU001158), Dec 8, 2000: BRACKET. CRACKED. (AUS) ENGINE MOUNT BRACKETS CRACKED ON SPAR ATTACHMENT FLANGE. FORWARD SPAR CRACKED.
- [SDR AU000820](https://openairdocs.org/sdr/AU000820), Sep 11, 2000: PIN. DAMAGED. (AUS) THROTTLE FRICTION ADJUSTER SHAFT SPLIT PIN DEFORMED AND PARTIALLY SHEARED. (X)
- [SDR AU000484](https://openairdocs.org/sdr/AU000484), Jun 2, 2000: PIPE. CORRODED. (AUS) RIGHT ENGINE NR 5 CYLINDER ROCKER COVER OIL DRAIN PIPE HOLED DUE TO CORROSION. LOSS OF ENGINE OIL.
- [SDR AU991039](https://openairdocs.org/sdr/AU991039), Oct 1, 1999: TAPE. UNAPPROVED PART. (AUS) LEADING EDGE TAPES FITTED TO WINGS HAD NO DOCUMENTATION. MANUFACTURER DOES NOT APPROVE OF TAPE FITMENT. TAPE WAS ALSO POORLY FITTED AND WAS NOT ADHERING C
- [SDR AU991030](https://openairdocs.org/sdr/AU991030), Oct 1, 1999: BRACKET. DAMAGED. (AUS) CENTER RUDDER ATTACHMENT BRACKET DAMAGED.
- [SDR AU990520](https://openairdocs.org/sdr/AU990520), Jun 2, 1999: SPAR. CRACKED. (AUS) WING MAIN SPAR CRACKED IN TWO PLACES ON THE LT SIDE AND IN THREE PLACES ON THE RT SIDE IN THE AREA COVERED BY AD/BN2/62 AND SB BN2/SB237. THE AIRCRAFT STI
- [SDR AU981418](https://openairdocs.org/sdr/AU981418), Oct 30, 1998: RETAINER. BROKEN. (AUS) LT ENGINE FUEL FILTER BOWL RETAINER BROKEN.
- [SDR AU980413](https://openairdocs.org/sdr/AU980413), Apr 15, 1998: FLYWEIGHT. FAILED. (AUS) ON THE FIRST SHUTDOWN OF THE DAY, THE PROPELLER WOULD NOT LATCH AND WENT INTO FEATHER. LATER IN THE DAY, THE PROPELLER FAILED TO ACHIEVE MAXIMUM RPM. THE 
- [SDR AU970108](https://openairdocs.org/sdr/AU970108), Feb 8, 1997: CONTROL CABLE. MISROUTED. (AUS) RUDDER PEDAL ADJUSTMENT CABLE INCORRECTLY ROUTED - CABLE ROUTED BELOW THE CONTROL COLUMN ELECTRICAL CORD INSTEAD OF ABOVE IT -THIS CAUSED THE CABLE TO SNA

## STCs that may be installed (OpenAirDocs) (103, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [STC SA02254AK](https://openairdocs.org/stc/SA02254AK): Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen". Genesys Aerosystems Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA04424AT](https://openairdocs.org/stc/SA04424AT): Installation of Continental Motors, Inc. (CMI) Shower-of-Sparks Starting Vibrator Booster Systems. Continental Motors, Inc
- [STC SA01828SE](https://openairdocs.org/stc/SA01828SE): Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System. J. P. Instruments
- [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC
- [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation
- [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA1842WE](https://openairdocs.org/stc/SA1842WE): Installation of Brittain Industries, Inc. Model B-5 Flight Control System. Brittain Industries, Inc
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA01559CH](https://openairdocs.org/stc/SA01559CH): Install Aero Medical Products air ambulance stretcher P/N 125 using Installation Kit P/N 805. Approval is for stretcher structure, structural attachment of an oxygen bottle, and optional medical oxygen system only. Paul/ Lanna Egan LLC
- [STC SA02954CH](https://openairdocs.org/stc/SA02954CH): Installation of a replacement pitot static probe. Seginus, Inc
- [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc
- [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC
- [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA01669CH](https://openairdocs.org/stc/SA01669CH): Installation of Challenger Reusable Air Filter. Challenger Aviation Products Inc
- [STC SA02283SE PAGE 2](https://openairdocs.org/stc/SA02283SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc
- [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [STC SA02717NY PAGE 1](https://openairdocs.org/stc/SA02717NY%20PAGE%201): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC
- [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument. J P Instruments
- [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments
- [STC SA01026SE](https://openairdocs.org/stc/SA01026SE): Improved fuel gascolator assembly. Steve's Aircraft
- [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc

All 103: https://openairdocs.org/model/britten-norman-bn-2a-20/stcs.md

## PMA parts (OpenAirDocs) (326, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [AG3026-836](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113361094020260806140328.0001): Control Shaft Assembly. Aero Accessories LLC · PMA PQ1206CE · Replaces Woodward P/N:3026-836 · Jul 21, 2026
- [RAP164-01506](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124067462220260722154716.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-01506 · Jun 3, 2026
- [AG210331](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187664979720260616140345.0001): Plunger Ass’y, Pilot Valve. Aero Accessories LLC · PMA PQ1206CE · Replaces Woodward P/N:210331 · May 27, 2026
- [8850-7CJ](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126603900620240625133922.0001): MOTOR (28 VDC). McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 8850-7 · Mar 14, 2024
- [12-50011](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195967766820231121213753.0001): Assembly: saf-Tglo® Whiter Background EXIT Sign (USES). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50011 · Nov 20, 2023
- [10-50008-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193301962220231121213611.0001): SSUL-X Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50008-XFCCC · Nov 20, 2023
- [10-50011-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184314853620231121213636.0001): SSUL-X11 Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50011-XFCCC · Nov 20, 2023
- [SG8916](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183099284920231121213701.0001): Filler. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8916 · Nov 20, 2023
- [12-50003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179454486820231121213724.0001): Assembly: saf-Tglo® Exit (USES). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50003 · Nov 20, 2023
- [12-50013](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178620059020231121213759.0001): Assembly: saf-Tglo® Whiter Background Door Operation Signage. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50013 · Nov 20, 2023
- [10-50009-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171981532920231121213619.0001): SSUL-X Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50009-XFCCC · Nov 20, 2023
- [12-50005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163594466420231121213731.0001): Assembly: saf-Tglo® Door Operation Sign. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50005 · Nov 20, 2023
- [12-50007](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161986353120231121213738.0001): Assembly: saf-Tglo® Supplemental Signage/Placard. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50007 · Nov 20, 2023
- [30-50001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140205643320231121213710.0001): Scapa 5169 Filler. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 30-50001 · Nov 20, 2023
- [SG8995](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139973266720231121213644.0001): Flexible Overcarpet for SSUL with Tape. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8995 · Nov 20, 2023
- [SG8996](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133100709220231121213653.0001): Flexible Overcarpet End Cap for SSUL with Tape. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8996 · Nov 20, 2023
- [12-50009](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127997737420231121213746.0001): Assembly: saf-Tglo® Whiter Background EXIT Sign (Text). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50009 · Nov 20, 2023
- [12-50001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122213192420231121213718.0001): Assembly: saf-Tglo® Exit (Text). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50001 · Nov 20, 2023
- [10-50010-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115365142320231121213628.0001): SSUL-X11 Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50010-XFCCC · Nov 20, 2023
- [APS68-01100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171282344920231102131425.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01100 · Sep 25, 2023
- [APS68-01700](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109958449020231102131429.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01700 · Sep 25, 2023
- [ST-989PL-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156063576820230612132631.0001): Installation of S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation · PMA PQ0445SW · Modification part · May 25, 2023
- [ST-989PL](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131700241320230612132630.0001): Installation of S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation · PMA PQ0445SW · Modification part · May 25, 2023
- [ST-989PL-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101323459020230612132632.0001): Installation of S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation · PMA PQ0445SW · Modification part · May 25, 2023
- [01-0790906-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115473606320220706160103.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Jun 21, 2022
- [8850-7CJ](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121796954520220720120316.0001): Motor (28 Vdc). C J Aviation, Inc. · PMA PQ1607CE · Replaces Weldon Pumps8850-7 · Jun 17, 2022
- [EA-21000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166117473920220525194206.0001): Six-Cylinder Ignition Controller. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-22000T](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156661745920220525194450.0001): Controller Wire Harness- Twin (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-22000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118131946020220525194338.0001): Controller Wire Harness (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID726347214620210923143653.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID289916139020210923143754.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID263927867620210921142535.0001): SkyTrax 100B/200 ADS-B Receiver. Avidyne Corporation · PMA PQ4035CE · Replaces ModificationPart · Jul 28, 2021
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID342188225202106221424550.0001): AeroLEDs LLC · PMA PQ5259NM · Mar 11, 2021
- [409-00003-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID871206669720210702175216.0001): Internal Battery Pack, Refresh. Aspen Avionics · PMA PQ03868SW · Modification part · Jan 20, 2021
- [1049-4000-03-001C](https://drs.faa.gov/browse/excelExternalWindow/FB6A4D62429A217F86258633006145AB.0001): Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4201-20](https://drs.faa.gov/browse/excelExternalWindow/ED78E4F8D3C63347862586330061461D.0001): Annunciator Kit GDC31. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4200-20](https://drs.faa.gov/browse/excelExternalWindow/CBC6239248334CCE86258633006145E5.0001): Connector Kit GDC31. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4200-50](https://drs.faa.gov/browse/excelExternalWindow/86CBD103649292948625863300614693.0001): Isolation Coupler Installation Kit. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4000-03-001B](https://drs.faa.gov/browse/excelExternalWindow/80F9B5EC9801FD16862586330061456E.0001): Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4801-01](https://drs.faa.gov/browse/excelExternalWindow/39A0DF401545910A8625863300614652.0001): Isolation Coupler. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [APS68-01700](https://drs.faa.gov/browse/excelExternalWindow/51CDE584B1A22102862586290049EFF5.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01700 · Nov 4, 2020
- [APS68-01100](https://drs.faa.gov/browse/excelExternalWindow/1A9437DB989160E2862586290049EF86.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01100 · Nov 4, 2020
- [APS068-01100](https://drs.faa.gov/browse/excelExternalWindow/48A12ED2A35F49FE862585EC00452205.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01100 · Aug 26, 2020
- [APS068-01700](https://drs.faa.gov/browse/excelExternalWindow/068001A41B0BCCA9862585EC004522B5.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01700 · Aug 26, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID973140915420220125131317.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID675692768120220125131411.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID660995348920220125131435.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID369070383320220125131336.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID294678645620220125131458.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181024387320220125131353.0001): DAC International · PMA PQ0986SW · Jul 31, 2020

All of them: https://openairdocs.org/model/britten-norman-bn-2a-20/pma.md

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