# N928MJ: Britten Norman BN-2A MK III - Status: Valid registration - Airframe: [Britten Norman BN-2A MK III](https://openairdocs.org/model/britten-norman-bn-2a-mk-iii) (registry code 1520203, 18 seats) - Data sheets: [TCDS A29EU](https://openairdocs.org/tcds/A29EU) (Britten-Norman Aerospace Ltd.) (OpenAirDocs) - Serial number: 1040 - Type: Fixed wing multi engine - Engine type: Reciprocating - Certificate issued: September 16, 2023 - Expires: September 30, 2030 - Mode S code: ACDCFE - Registered owner: [Plane Sales & Leasing LLC](https://openairdocs.org/faa-owner/PLANE%20SALES%20%26%20LEASING%20LLC) - Location: [Kalispell, MT](https://openairdocs.org/faa-place/MT/Kalispell) - Owner type: LLC - Owner's area on the map: 48.2306° N, 114.4033° W: Placed by OpenAirDocs at the center of ZIP code 59901, within about 12 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=928MJ - Page: https://openairdocs.org/aircraft/N928MJ From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 51 in force ### Matched by airframe (Britten Norman BN-2A MK III) - [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 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 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 2002-24-01](https://openairdocs.org/ad/2002-24-01): Rear Engine-mounting Frame · B-N Group BN2A MK. III, BN2A MK. III-2 and BN2A MK. III-3. Effective Jan 21, 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 2002-01-11](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 98-04-17](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 86-07-02 R1](https://openairdocs.org/ad/86-07-02-R1): Main Landing Gear Torque Link Lug & Upper Case Inspection · B-N Group BN2A MK. III, BN2A MK. III-2 and BN2A MK. III-3. 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 84-23-06 R1](https://openairdocs.org/ad/84-23-06-R1): Engine Mounting Brackets · B-N Group BN2A MK. III, BN2A MK. III-2 and BN2A MK. III-3. 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 87-13-02](https://openairdocs.org/ad/87-13-02): Elevator Trim Tab Assemblies · B-N Group BN2A MK. III, BN2A MK. III-2 and BN2A MK. III-3. Effective Jul 27, 1987 - [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 83-14-02](https://openairdocs.org/ad/83-14-02): Wing-To-Fuselage Attachments · B-N Group BN2A MK. III, BN2A MK. III-2 and BN2A MK. III-3. Effective Aug 19, 1983 - [AD 83-12-02](https://openairdocs.org/ad/83-12-02): Rudder Drive Lever Support Assembly · B-N Group BN2A MK. III, BN2A MK. III-2 and BN2A MK. III-3. Effective Jul 27, 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 83-03-05](https://openairdocs.org/ad/83-03-05): Undercarriage Shock Absorber · B-N Group BN2A MK. III, BN2A MK. III-2 and BN2A MK. III-3. Effective Feb 22, 1983 - [AD 82-24-06 R1](https://openairdocs.org/ad/82-24-06-R1): Carburetor Air Box Shutter · B-N Group BN-2, BN-2A, BN-2A-26 and 7 more. Effective Feb 7, 1983 - [AD 80-14-10](https://openairdocs.org/ad/80-14-10): Rudder Balance Arm Brackets · B-N Group BN2A MK. III, BN2A MK. III-2 and BN2A MK. III-3. Effective Jul 14, 1980 - [AD 79-21-03](https://openairdocs.org/ad/79-21-03): Elevator Trim Tab Cable · B-N Group BN2A MK. III, BN2A MK. III-2 and BN2A MK. III-3. Effective Nov 12, 1979 - [AD 79-03-05](https://openairdocs.org/ad/79-03-05): Main Landing Gear Extension Tube Assemblies · B-N Group BN2A MK. III, BN2A MK. III-2 and BN2A MK. III-3. Effective Feb 27, 1979 - [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 76-06-05](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 75-22-17](https://openairdocs.org/ad/75-22-17): Rudder Trim Control · B-N Group BN2A MK. III, BN2A MK. III-2 and BN2A MK. III-3. Effective Nov 5, 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 ### 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 All 54: https://openairdocs.org/aircraft/N928MJ/ads.md ## Information bulletins (advisory) (3 in force) - [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 ACE-98-38](https://openairdocs.org/saib/ACE-98-38): . Issued Jul 6, 1998 - [SAIB ACE-95-02](https://openairdocs.org/saib/ACE-95-02): . Issued May 31, 1995 ## NTSB investigations None matched to N928MJ. ## FAA accident and incident reports None matched to N928MJ. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## STCs that may be installed (OpenAirDocs) (70, first 50) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Britten Norman BN-2A MK III) - [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 SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels 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 SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [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 SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [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 SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH - [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 SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation 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 SA615EA](https://openairdocs.org/stc/SA615EA): Installation of a Whelen Anti-Collision Strobe Light System as replacement for originally installed anti-collision lights. Whelen Aerospace Technologies - [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [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 SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine - [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 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 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 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 SA02930NY](https://openairdocs.org/stc/SA02930NY): Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) Instruments. Insight Instrument Corporation - [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 SA02149AK](https://openairdocs.org/stc/SA02149AK): Installation of GX50/60 GPS Navigator, Capstone configured MX20 Multi-Function Display and UAT transceiver. Garmin International Inc - [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc - [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation - [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc - [STC SA02110CH](https://openairdocs.org/stc/SA02110CH): Installation of a Time Trac Data Recorder. P2 Incorporated - [STC SA00769CH](https://openairdocs.org/stc/SA00769CH): Installation of Champion Limited Authority Spark Advance Regulator (LASARTM) ignition system with Cylinder Head Temperature (CHT) monitoring capability on airframes with FAA approved installations of Textron Lycoming model IO-540, AEIO-540 and HIO-540 engines. Champion Aerospace LLC - [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system. Champion Aerospace LLC All 70: https://openairdocs.org/aircraft/N928MJ/stcs.md ## Related - Other Britten Norman BN-2A MK III aircraft: https://openairdocs.org/model/britten-norman-bn-2a-mk-iii/aircraft.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.