# Britten Norman BN-2B-20

- Type: Aircraft model (FAA registry)
- Registry code: 1520302
- Manufacturer (registry): BRITTEN NORMAN LTD.
- Model: BN-2B-20
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Reciprocating
- Seats: 10
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A17EU](https://openairdocs.org/tcds/A17EU) (OpenAirDocs)
- Holder: Britten-Norman Aerospace Ltd.
- Registered aircraft: 2
- Page: https://openairdocs.org/model/britten-norman-bn-2b-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 2002-22-02](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 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 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

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 97-03-03](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 (2)

- [N70AS](https://openairdocs.org/aircraft/N70AS): [International Air Services Inc Trustee](https://openairdocs.org/faa-owner/INTERNATIONAL%20AIR%20SERVICES%20INC%20TRUSTEE), [Carson City, NV](https://openairdocs.org/faa-place/NV/Carson%20City), built 2019, S/N 2314
- [N989YG](https://openairdocs.org/aircraft/N989YG): [Bn Aerospace Sales Inc Trustee](https://openairdocs.org/faa-owner/BN%20AEROSPACE%20SALES%20INC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 2279

## NTSB investigations (1)

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 LAX95LA041](https://openairdocs.org/ntsb/LAX95LA041), Dec 2, 1994: Britten-Norman Islander BN2B-20 (N16VM), Pacific Ocean (Pacific Ocean), destroyed. Probable cause: An undetermined failure of the left engine. The inability of the airplane to maintain level flight and exceeding the one-engine capability was a factor in the accident.

## FAA accident and incident reports (3)

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 20170222005699I](https://openairdocs.org/incident/20170222005699I), Feb 22, 2017: Britten-Norman BN-2B (N848MA), Kenai, AK, Minor damage. Pilot of aircraft received taxi clearance from ramp to runway 2L via golf and foxtrot taxiway. No mention of snowplow was made to aircraft from ATC(contract…
- [Incident 20080823857139I](https://openairdocs.org/incident/20080823857139I), Aug 23, 2008: Bnorm BN2 (N848MA), Boise, ID, Minor damage. (-23) While departing mackey bar with varible surface winds, the pilot stated shortly after his liftoff, the aircraft settled back onto the runway which…
- [Accident 19941202040259A](https://openairdocs.org/incident/19941202040259A), Dec 2, 1994: Bnorm BN2B20 (N16VM), Majaro, PS, Destroyed. Smoke from left engine. Loosing oil and quit. Unable continue. Ditched. Recent engine overhaul. Over gross weight.

## Service difficulty reports (59, newest 50)

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

- [SDR HYIA20260508001](https://openairdocs.org/sdr/HYIA20260508001), May 3, 2026: EXHAUST PIPE. BROKEN. DURING PREFLIGHT THE PILOT NOTED THAT AN EXHAUST PIPE ON THE RIGHT ENGINE WAS CRACKED, WHICH CAUSED DAMAGE TO THE ENGINE COWLING. MAINTENANCE REPLACED THE RIGHT
- [SDR HYIA20211105001](https://openairdocs.org/sdr/HYIA20211105001), Nov 3, 2021: NONE. NONE. THE PILOT REPORTED DURING CRUISE THE RIGHT ENGINE RPM AND OIL PRESSURE NOTICEABLE GOING DOWN, WITH THE ENGINE GOING INTO A FEATHER. THE PILOT ELECTED TO SHUT DO
- [SDR HYIA20200110001](https://openairdocs.org/sdr/HYIA20200110001), Jan 8, 2020: SEAL. UNSECURE. PILOT REPORTED CRACKLING SOUND AND FAINT SMELL OF BURNING ON LANDING - THOUGHT TO BE COMING FROM THE RIGHT SIDE OF THE AIRCRAFT. MAINTENANCE INSPECTED ALL ELECT
- [SDR HYIA20191206001](https://openairdocs.org/sdr/HYIA20191206001), Dec 5, 2019: BALL JOINT. WORN. AFTER TAKE OFF WHILE REDUCING POWER TO CRUISE SPEED PILOT REPORTED LEFT ENGINE STOPPED REDUCING AT 2800-2900 RPM THE PILOT ELECTED TO RETURN TO THE FIELD. AFTER
- [SDR HYIA20190717003](https://openairdocs.org/sdr/HYIA20190717003), Jul 13, 2019: ENGINE. SHUTDOWN. PILOT REPORTED ENGINE SHUT DOWN AND FEATHERED ON ITS OWN ON TAKE-OFF. MAINTENANCE INSPECTED THE LT AND RT ENGINE FUEL SYSTEM, INTAKE SYSTEM, IGNITION SYSTEM AND
- [SDR 2019F00168](https://openairdocs.org/sdr/2019F00168), Mar 20, 2019: IMPULSE COUPLING. BROKEN. HARD START CONDITION ISOLATED TO BROKEN MAGNETO IMPULSE COUPLING. FLYWEIGHT BIAS SPRING FOUND TO HAVE BROKEN LOOSE FROM PAWL RIVET.
- [SDR HYIA20160711001](https://openairdocs.org/sdr/HYIA20160711001), Jul 5, 2016: CYLINDER. FAILED. DURING INSPECTION OF RIGHT ENGINE AFTER FAILED ENGINE CHANGE FUNCTIONAL CHECK FLIGHT; MAINTENANCE NOTED LARGE AMOUNTS OF METAL IN OIL SAMPLES. FURTHER INVESTIGA
- [SDR HYIA20160414001](https://openairdocs.org/sdr/HYIA20160414001), Apr 7, 2016: CRANKSHAFT. DAMAGED. PILOT REPORTED PARTIAL LOSS OF POWER IN FLIGHT ON RT ENG, ENGINE RUNNING ROUGH. AFTER BOTH ENGS FULL POWER FOR ABOUT 30 SECONDS, POWER CAME BACK. ENGS WERE BROU
- [SDR HYIA20151223004](https://openairdocs.org/sdr/HYIA20151223004), Dec 17, 2015: CALIPER. FAULTY. PILOT REPORTED NO PRESS LT BRAKE. PERFORMED DETAILED INSPECTION ON LT BRAKE SYS & FOUND BOTH BRAKE CALIPERS MAKING A SQUEAKING SOUND & VERY SPONGY. R & R BOTH L
- [SDR HYIA2015FA0000642](https://openairdocs.org/sdr/HYIA2015FA0000642), Nov 24, 2015: AXLE. CRACKED. DURING OPERATOR RUTTING MAINTENANCE MECHANIC NOTICED UNUSUAL MARKS ON AXLE. THEN SENT TO NDT AND CRACK FOUND ON INNER AXLE.
- [SDR HYIA20151203001](https://openairdocs.org/sdr/HYIA20151203001), Nov 23, 2015: AXLE. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE LT MLG AXLE. THE PART WAS REMOVED & SENT FOR NDT INSPECTION, WHERE THE CRACK WAS CONFIRMED.
- [SDR HYIA20150820002](https://openairdocs.org/sdr/HYIA20150820002), Aug 14, 2015: CALIPER. LEAKING. PILOT REPORTED LT BRAKE FAILED. MX VISUALLY INSPECTED & FOUND THE OTBD BRAKE CALIPER LEAKING. R & R LT MLG OTBD CALIPER ASSEMBLY IAW MM CHAPTER 2.9. OPERATIONAL
- [SDR HYIA20150403001](https://openairdocs.org/sdr/HYIA20150403001), Apr 1, 2015: CALIPER. FAILED. PILOT REPORTED RT BRAKE FAILURE. R & R THE CALIPER & LINING ON THE RT BRAKE & SERVICED SYS. OPERATIONALLY CHECKED IT WITH NO FURTHER DEFECT NOTED.
- [SDR HYIA20150311001](https://openairdocs.org/sdr/HYIA20150311001), Mar 6, 2015: BLOWER. BURNED OUT. PILOT REPORTED STRONG ODOR IN COCKPIT, POSSIBLY ELEC, INFLIGHT. PERFORMED VISUAL INSP ON ALL ACFT SYS & FOUND THE VENTILATION BLOWER BURNT OUT. THE ITEM WAS PLA
- [SDR HYIA20141224002](https://openairdocs.org/sdr/HYIA20141224002), Dec 23, 2014: BRAKE PADS. WORN. LEFT BRAKE INOPERATIVE, PEDAL TO THE FLOOR, BRAKE PAD VERY WORN. R & R LT OTBD BRAKE LININGS IAW MM CH 2 9. R & R LT OTBD BRAKE CALIPER IAW MM CH 2 9, SERVICED 
- [SDR HYIA20141219002](https://openairdocs.org/sdr/HYIA20141219002), Dec 18, 2014: CALIPER. DEFECTIVE. NO LT BRAKE ON LANDING. R & R THE LT OTBD BRAKE CALIPER ASSEMBLY IAW MM CHAPTER 2 9. OPERATIONS CHECKED SATISFACTORY WITH NO FURTHER DEFECTS NOTED.
- [SDR HYIA20141219001](https://openairdocs.org/sdr/HYIA20141219001), Dec 18, 2014: BRAKE ASSY. DEFECTIVE. RIGHT MAIN OTBD TIRE LOCKS UP DURING NORMAL BRAKING. R & R THE RT MAIN OTBD BRAKE IAW MM SEC 2 9. OPERATIONS CHECKED SATISFACTORY WITH NO FURTHER DETAILS NOTED.
- [SDR HYIA20140415107](https://openairdocs.org/sdr/HYIA20140415107), Apr 12, 2014: PUMP. WEAK. DURING CLIMB THE PILOT REPORTED THE RT FUEL PRESS WOULD NOT REMAIN IN THE GREEN ARC. THE ENG DRIVEN FUEL PUMP WAS REPLACED & OPERATIONAL & LEAK CHECK WERE ACCOM
- [SDR AUS20040480](https://openairdocs.org/sdr/AUS20040480), Jun 2, 2004: CONTROL ROD. CORRODED. (AUS) ELEVATOR CONTROL ROD CORRODED ON INTERNAL THREADS. FOUND DURING INSPECTION IAW SB 303 AND AD/BN2/082.
- [SDR AUS20040292](https://openairdocs.org/sdr/AUS20040292), Feb 17, 2004: CONTROLLER. FAULTY. (AUS) AUTOPILOT BURNED OUT. ROLL SERVO ALSO BURNED OUT.
- [SDR AUS20031251](https://openairdocs.org/sdr/AUS20031251), Nov 28, 2003: CONNECTOR. CORRODED. (AUS) COMPASS FLUX DETECTOR CONNECTOR CORRODED. SEE MDR 03/1246 FOR ASSOCIATED DEFECT.
- [SDR AUS20031246](https://openairdocs.org/sdr/AUS20031246), Nov 28, 2003: SERVO. FAILED. (AUS) AUTOPILOT ROLL SERVO FAULTY.
- [SDR AUS20031183](https://openairdocs.org/sdr/AUS20031183), Nov 19, 2003: ALTERNATOR. FAILED. (AUS) RT ALTERNATOR FAILED.
- [SDR AUS20031148](https://openairdocs.org/sdr/AUS20031148), Nov 11, 2003: PITOT TUBE. CONTAMINATED. (AUS) PITOT/STATIC SYSTEM CONTAMINATED WITH WATER.
- [SDR AUS20030836](https://openairdocs.org/sdr/AUS20030836), Aug 12, 2003: PUMP. MISMARKED. (AUS) LT FUEL TRANSFER PUMP UNAPPROVED PART. PUMP HAD A LABEL ATTACHED STATING THE MANUFACTURER DOES NOT RECOMMEND USAGE IN AIRCRAFT APPLICATIONS. PUMP WAS SUPP
- [SDR AUS20030635](https://openairdocs.org/sdr/AUS20030635), Jun 18, 2003: BALL JOINT. BROKEN. (AUS) RT ENGINE MIXTURE CONTROL BALL JOINT FAILED.
- [SDR AUS20021455](https://openairdocs.org/sdr/AUS20021455), Dec 23, 2002: FUSE. CORRODED. (AUS) BUSBAR UNDERVOLTAGE FUSE F86 CORRODED AND BROKEN.
- [SDR AUS20021153](https://openairdocs.org/sdr/AUS20021153), Oct 11, 2002: SLEEVE. SPLIT. (AUS) LH AILERON CONTROL ROD SLEEVE SPLIT THROUGH TAPER PIN HOLE.
- [SDR AUS20021014](https://openairdocs.org/sdr/AUS20021014), Sep 10, 2002: SCREW. MISSING. (AUS) LH ENGINE COWL SCREW MISSING. SCREW IS LOCATED ON THE FORWARD INBOARD SIDE OF THE LH COWL.
- [SDR AUS20020955](https://openairdocs.org/sdr/AUS20020955), Aug 28, 2002: DISTRIBUTOR. UNSERVICEABLE. (AUS) MAGNETO DISTRIBUTOR BLOCK BEARING LOOSE. MAGNETO CONTAMINATED WITH METAL DUE TO CONTACT BETWEEN DISTRIBUTOR GEAR ANDELECTRODES. SUSPECT FAILURE DUE TO APP
- [SDR AUS20020754](https://openairdocs.org/sdr/AUS20020754), Jul 17, 2002: MAGNETO. FAULTY. (AUS) NO2 ENGINE NO2 MAGNETO FAULTY. MAGNETO MODELS 10-349370-4 AND 10-349310-8.
- [SDR AUS20020676](https://openairdocs.org/sdr/AUS20020676), Jun 16, 2002: DRIVE SHAFT. WRONG PART. (AUS) ENGINE FUEL PUMP DRIVE SHAFT INCORRECT ITEM. INVESTIGATION FOUNDTHAT THE DRIVE SHAFT WAS APPROXIMATELY 6.35MM (0.25IN) SHORTERTHAN NORMAL. THE INCORRECT D
- [SDR AUS20020404](https://openairdocs.org/sdr/AUS20020404), Apr 30, 2002: PUMP. WRONG PART. (AUS) AFTER ENGINE CHANGE AND DURING GROUND RUNS THE ENGINE FAILED WHEN THE BOOST PUMP WAS TURNED OFF. SUBSEQUENT INVESTIGATION FOUND THAT THE INCORRECT FUEL PU
- [SDR AUS20020266](https://openairdocs.org/sdr/AUS20020266), Mar 15, 2002: PIPE. LOOSE. (AUS) RH ENGINE CRANKCASE TO OIL COOLER PIPE LOOSE AND LEAKING. ENGINEHAD BEEN RECENTLY REPLACED. PERSONNEL/MAINTENANCE ERROR.
- [SDR AUS20020191](https://openairdocs.org/sdr/AUS20020191), Mar 11, 2002: TAPPET. CRACKED. (AUS) RH ENGINE NO6 CYLINDER INLET TAPPET AND NO4 CYLINDER EXHAUSTTAPPET BODIES CRACKED.
- [SDR AUS20011463](https://openairdocs.org/sdr/AUS20011463), Dec 28, 2001: CONTROLLER. FAULTY. (AUS) AUTOPILOT CONTROL PROGRAMMER FAULTY.
- [SDR AUS20010888](https://openairdocs.org/sdr/AUS20010888), Aug 5, 2001: ROD END. WORN. (AUS) ELEVATOR TRIM TAB DRIVE ROD END WORN. INSPECTION FOUND THE LEFT THREADED LOCKNUT STRIPPED.
- [SDR AU010274](https://openairdocs.org/sdr/AU010274), Mar 21, 2001: LEVER. LOOSE. (AUS) RUDDER CONTROL RT IDLER LEVER LOOSE AND CATCHING ON FUSELAGE FRAME OPENING.
- [SDR AU010160](https://openairdocs.org/sdr/AU010160), Feb 23, 2001: HOSE. FAILED. (AUS) NR 1 ENGINE INTAKE HOSE LOCATED BETWEEN THE AIR FILTER AND THE FCU COLLAPSED DUE TO LOOSE INNER SUPPORT WIRE.
- [SDR AU001097](https://openairdocs.org/sdr/AU001097), Nov 22, 2000: PIN. SHEARED. (AUS) THROTTLE FRICTION ADJUSTMENT SHAFT SPLIT PIN SHEARED DURING FRICTION ADJUSTMENT. FOUND DURING INVESTIGATION OF EXCESSIVETHROTTLE FRICTION AND AD/BN-2/69. 
- [SDR AU990349](https://openairdocs.org/sdr/AU990349), Apr 13, 1999: BOLT. BROKEN. (AUS) LEFT MAIN LANDING GEAR INBOARD WHEEL ASSEMBLY BOLTS (2OFF3) BROKEN IN AN AREA APPROXIMATELY 1-2 THREADS ABOVE THE SHANK. WHEN THE WHEEL WAS DISASSEMBLED, 
- [SDR AU970545](https://openairdocs.org/sdr/AU970545), May 21, 1997: CAMSHAFT. DETERIORATED. (AUS) CAMSHAFT LOBE CASE HARDENING BREAKING DOWN - CRANKSHAFT GEAR ALSO HAD BREAKING DOWN OF THE CASE HARDENING
- [SDR AU970542](https://openairdocs.org/sdr/AU970542), May 19, 1997: CAMSHAFT. DAMAGED. (AUS) CAMSHAFT LOBE CASE HARDENING DAMAGED
- [SDR AU970090](https://openairdocs.org/sdr/AU970090), Feb 9, 1997: REGULATOR. BURNT. (AUS) RH ALTERNATOR VOLTAGE REGULATOR BURNT OUT DUE TO FAILURE OF THE DRIVER TRANSISTOR IN THE ALTERNATOR FIELD WINDING
- [SDR EY2R9601164](https://openairdocs.org/sdr/EY2R9601164), Oct 1, 1996: BEARING. CORRODED. CORROSION FOUND ON SPLIT BEARING.
- [SDR EY2R9601163](https://openairdocs.org/sdr/EY2R9601163), Oct 1, 1996: HUB. CORRODED. CORROSION FOUND ON HUB.
- [SDR AU961051](https://openairdocs.org/sdr/AU961051), Jul 30, 1996: GASCOLATOR. LEAKING. (AUS) RH ENGINE GASCOLATOR BOWL DISLODGED AND THE CLAMP SPRING ARM DISCONNECTED - FUEL LEAKING
- [SDR AU960861](https://openairdocs.org/sdr/AU960861), Jun 21, 1996: MOTOR. FAILED. (AUS) AIRCONDITIONING SYSTEM DISCHARGE PIPE BURST - FAILURE WAS DUE TO FAILURE OF THE CONDENSER COOLING FAN MOTOR RESULTING IN AN INCREASE OF DISCHARGE PRESSURE
- [SDR AU960904](https://openairdocs.org/sdr/AU960904), Jun 14, 1996: TRANSMITTER. FAULTY. (AUS) RH TIP TANK FUEL CONTENTS TRANSMITTER FLOAT MISSING - THE FLOAT RETAINING CLIP WAS STILL IN POSITION SUGGESTING THAT THE FLOAT HAD DISINTEGRATED
- [SDR AU960431](https://openairdocs.org/sdr/AU960431), Mar 28, 1996: HOSE. FAULTY. (AUS) RH ENGINE INDUCTION HOSE INTERNAL WIRE SEPARATING FROM HOSE - FOUND DURING INSPECTION IAW AD/BN2/57

All 59: https://openairdocs.org/model/britten-norman-bn-2b-20/reports.md

## STCs that may be installed (OpenAirDocs) (102, 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 SA02426AK](https://openairdocs.org/stc/SA02426AK): Approval of the FreeFlight FDL-978-TX ADS-B system installed. FreeFlight Systems
- [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

All 102: https://openairdocs.org/model/britten-norman-bn-2b-20/stcs.md

## PMA parts (OpenAirDocs) (303, 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.

- [RAP164-01506](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124067462220260722154716.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-01506 · Jun 3, 2026
- [RAP164-02201](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170501026820250829181749.0001): Brake Disc. Rapco Inc · PMA PQ2101CE · Replaces 164-02201 Cleveland · Aug 27, 2025
- [20006A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196551474020250303152539.0001): Air-Oil Cooler. Boyd Niagara LLC · PMA PQ0872NE · Replaces 8534108 · Oct 30, 2024
- [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
- [8000215](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164504601620221130202548.0001): Engine Oil Cooler. Aero-Classics Heat Transfer Products Inc · PMA PQ2543NM · Replaces Niagara 20006AHarrison M/N: AP13AU06-01 · Oct 21, 2022
- [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
- [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
- [9100-001-C](https://drs.faa.gov/browse/excelExternalWindow/DD343890DCD8BFDB86258569004013FB.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-D](https://drs.faa.gov/browse/excelExternalWindow/C7B6725B325949E98625856900401478.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9200-000-B](https://drs.faa.gov/browse/excelExternalWindow/BD58B0712CA0C6AA86258569004016AD.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-G](https://drs.faa.gov/browse/excelExternalWindow/ADE62C91D97E8B788625856900401557.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-E](https://drs.faa.gov/browse/excelExternalWindow/A37F050253EE808A86258569004014BA.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9200-000-A](https://drs.faa.gov/browse/excelExternalWindow/8E10EF4D973C1D6D8625856900401662.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-A](https://drs.faa.gov/browse/excelExternalWindow/62DC748A2B9B1D9386258569004012FD.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-F](https://drs.faa.gov/browse/excelExternalWindow/3746AAB4CC0D6883862585690040151B.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-B](https://drs.faa.gov/browse/excelExternalWindow/32446D71EB78157686258569004013B2.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [01-0771833-20](https://drs.faa.gov/browse/excelExternalWindow/FFF505DF238D9E3E86258557004EB967.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019
- [01-0771833-25](https://drs.faa.gov/browse/excelExternalWindow/D17366A21258BFC186258557004EB9A2.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019

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

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Pilatus Britten-Norman BN2B-20](https://openairdocs.org/model/pilatus-britten-norman-bn2b-20): 6 registered aircraft, registry code 7080220

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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.