# N612AW: 1988 British Aerospace BAE 146 SERIES 300A, registration cancelled 2008-01-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 31, 2008 - Exported to: South Africa - Status when cancelled: Valid registration - Airframe: [British Aerospace BAE 146 SERIES 300A](https://openairdocs.org/model/british-aerospace-bae-146-series-300a) (registry code 1500267) - Engine: [Lycoming ALF-502 SER. series](https://openairdocs.org/engine/lycoming-alf-502-ser-series) (registry code 41580) - Data sheets: [TCDS A49EU](https://openairdocs.org/tcds/A49EU), [TCDS E6NE](https://openairdocs.org/tcds/E6NE) (OpenAirDocs) - Serial number: E3122 - Year built: 1988 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 22, 1989 - Certificate issued: May 5, 2007 - Last registry action: May 5, 2007 - Mode S code: A7F641 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N612AW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=612AW - Page: https://openairdocs.org/deregistered/N612AW-2008-01-31 From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the British Aerospace BAE 146 SERIES 300A: https://openairdocs.org/model/british-aerospace-bae-146-series-300a.md ## Service difficulty reports (82, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR A6WA200460054](https://openairdocs.org/sdr/A6WA200460054), Nov 10, 2004: OXYGEN MASK. MISSING. ROWS 14 AND 16 DEF HAVE NR O2 MASKS INSTALLED IN PSU BOXES. MAINTENANCE INSTALLED PASSENGER ALL O2 MASKS AS REQUIRED IAW 35-20-45. - [SDR A6WA200460033](https://openairdocs.org/sdr/A6WA200460033), Aug 31, 2004: LINE. RUPTURED. FOUND RIGHT MLG FAILED TO RETRACT AFTER TAKEOFF, REV UNSAFE LIGHT ILLUMINATED, CYCLED MLG DOWN, RETUREND TO RDU FOR FERRY FLIGHT BACK TO ATW. INSPECTED AND FOUN - [SDR A6WA200460023](https://openairdocs.org/sdr/A6WA200460023), Jun 14, 2004: SKIN. DAMAGED. FOUND LEFT INBOARD LEADING EDGE HAS WEAR DAMAGE OT THE INBOARD LEADING EDGE WHERE THE STALL BAR ATTACHES. MAINTENANCE REQUESTED REPAIRS FROM BAE SYSTEMS REF AVM - [SDR A6WA200460024](https://openairdocs.org/sdr/A6WA200460024), Jun 14, 2004: SKIN. GOUGED. FOUND RIGHT HORIZONTAL STABILIZER TOP SKIN SMALL GOUGE IN THE UPPER SKIN OF THE RIGHT HORIZONTAL STABILIZER BETWEEN RIBS 9 AND 10. MAINTENANCE REQUESTED REPAIR - [SDR A6WA200360027](https://openairdocs.org/sdr/A6WA200360027), May 12, 2003: PANEL. CHAFED. CHAFE DAMAGE TO LEFT STABILIZER PANEL 275CL. MAINTENANCE BLENDED AND POLISHED DAMAGE AREA IAW BAE FAX BARA/AVR/3037/03-DC. (M) - [SDR A6WA200260043](https://openairdocs.org/sdr/A6WA200260043), Oct 8, 2002: TAB. DENTED. DENTS TO RT ELEVATOR AND TABS X 34 RECEIVED CONCESSION. - [SDR A6WA200260042](https://openairdocs.org/sdr/A6WA200260042), Oct 8, 2002: TAB. DENTED. DENTS TO LEFT ELEVATOR AND TABS X 8 RECEIVED CONCESSION. - [SDR A6WA200260041](https://openairdocs.org/sdr/A6WA200260041), Oct 8, 2002: STRUCTURE. DENTED. RIGHT FLAP INBOARD AND OUTBOARD TABS DENTED, RECEIVED CONCESSION. - [SDR A6WA200260040](https://openairdocs.org/sdr/A6WA200260040), Oct 4, 2002: SKIN. DENTED. DENTS RIGHT FUSELAGE X 4 RECEIVED CONCESSION. - [SDR A6WA200260039](https://openairdocs.org/sdr/A6WA200260039), Oct 4, 2002: DOOR. DENTED. DENTS RT MAIN LANDING GEAR X 26 RECEIVED CONCESSION. - [SDR A6WA200260038](https://openairdocs.org/sdr/A6WA200260038), Oct 4, 2002: DOOR. DENTED. DENTS LEFT MAIN LANDING GEAR DOOR X 18 RECEIVED CONCESSION. - [SDR A6WA200260037](https://openairdocs.org/sdr/A6WA200260037), Oct 4, 2002: TAB. DENTED. DENT LEFT FLAP INBOARD TAB X RECEIVED CONCESSION. - [SDR A6WA200260036](https://openairdocs.org/sdr/A6WA200260036), Oct 4, 2002: TAB. DENTED. DENTS RIGHT AILERON INBOARD AND OUTBOARD TABS X 32 RECEIVED CONCESSION. - [SDR A6WA200260035](https://openairdocs.org/sdr/A6WA200260035), Oct 4, 2002: TAB. DENTED. DENTS LEFT AILERON TABS X 9 RECEIVED CONCESSION. - [SDR A6WA200100047](https://openairdocs.org/sdr/A6WA200100047), Aug 10, 2001: CONTROL BOX. FAILED. NR 1 ENGINE FAILED IN FLIGHT, NO LEAKS NOTED OR DAMAGE NOTED. MAINTENANCE REMOVED AND REPLACED THE HIGH AND LOW PRESSURE FUEL FILTERS, FUEL CONTROL AND PRIMARY - [SDR A6WA200100039](https://openairdocs.org/sdr/A6WA200100039), Jun 18, 2001: O-RING. FAILED. LOST ALL GREEN HYDRAULIC QUANTITY ON GEAR EXTENSION. MAINTENANCE REMOVED AND REPLACED O-RING ON PTU PLUG. - [SDR A6WA200100016](https://openairdocs.org/sdr/A6WA200100016), Feb 22, 2001: A/C PACK. FAILED. AT 20,000 FEET NR 1 PACK VALVE LIGHT CAME ON, FLIGHT CREW TRIED TO RESET COULD NOT. THE RECIRCULATION VALVE WENT FREST COULD NOT RESET. NR 2 PACK VALVE LIGHT CA - [SDR A6WA200000064](https://openairdocs.org/sdr/A6WA200000064), Nov 7, 2000: STRONG OIL SMELL IN CABIN WHEN APU AIR INTRODUCED INTO SYSTEM OK ON ENGINE AIR. MAINTENANCE PERFORMED CONTAMINATED DUCT CLEANING PROCEDURE. APU VACUUM TEST GOOD - [SDR A6WA0000011](https://openairdocs.org/sdr/A6WA0000011), Jan 31, 2000: ENGINE. FAILED. FLT 5510 - ORD-ATW - NR 1 ENGINE FAILED ON TAKEOFF OUT OF ORD. REMOVED AND REPLACED NR 1 ENGINE. (M) - [SDR 99ZZZM426](https://openairdocs.org/sdr/99ZZZM426), Jun 29, 1998: SKIN. WORN. NR 2 ENGINE LEFT AFT AFT COWL DOOR INNER SKIN WORN THROUGH. PATCHED ABOVE DAMAGE PER PSI USING TA2 AND CHERRYMAXNUETS. - [SDR 99ZZZM432](https://openairdocs.org/sdr/99ZZZM432), Jun 24, 1998: DOOR. LACK OF LUBE. COCKPIT DOOR DIFFICULT TO OPEN FROM CABIN SIDE. LUBED AND RESHIMMED DOOR, OPS CHECK OK. (M) - [SDR 99ZZZM544](https://openairdocs.org/sdr/99ZZZM544), Jun 19, 1998: CONTROL CABLE. CORRODED. LEFT MAIN AILERON CONTROL CABLES ARE CORRODED AT PULLEY BETWEEN FUSELAGE FRAME NR 24 AND 25. REMOVED AND REPLACED LEFT MAIN AILERON CENTER CONTROL CABLES, TENSI - [SDR 99ZZZM427](https://openairdocs.org/sdr/99ZZZM427), Jun 19, 1998: VALVE. FAILED. CABIN OXYGEN MASKS AT RIGHT SIDE ROW 2 DEF VALVE PISTON FAIL TEST. REMOVED AND REPLACED VALVE AT SEAT 2 DEF, OPS CHECK GOOD. (M) - [SDR 98ZZZM937](https://openairdocs.org/sdr/98ZZZM937), Jun 19, 1998: STRING. MISINSTALLED. OXYGEN CABIN DROP DOORS FOR MASKS AT POS RIGHT 7 DEF, RT 8 DEF, RT 12 DEF AND LT 5 ABC STRING HINGES ARE NOT LONG ENOUGH FOR DOOR TO SWING OPEN FULLY. ADJUSTED - [SDR 98ZZZM908](https://openairdocs.org/sdr/98ZZZM908), Jun 19, 1998: LAYNARD. WORN. OXYGEN MASK AT 20 RT REBREATHER FEL HAS HOLES AND PIN STRING FRAYED, 11 LT. REBREATHER FELT HAS HOLES. REPLACED FELTS RT 20, 11 LT. REPLACED LANYARD 20 RT. CHEC - [SDR 99ZZZM547](https://openairdocs.org/sdr/99ZZZM547), Jun 18, 1998: STRIP. CRACKED. NR 4 ENGINE FORWARD OUTBOARD COWL DOORIS CRACKED AT INNER DOOR MIDDLE CAPPING. STRIP NEAR DRAIN LINE CLAMP. REPAIRED CAPPING STRIP PER BAE SRM 51-71-11 AND 12. - [SDR 99ZZZM546](https://openairdocs.org/sdr/99ZZZM546), Jun 18, 1998: DOOR. CRACKED. NR 4 ENGINE INBOARD FAN DOOR, 3RD DOOR RIB, CRACKED AT LOWER CORNER AREA NEAR VENT TUBE. REPAIRED CRACK BY PATCHING IAW BAE AIR/WISC SRM STD PRACTICES AND FOUND - [SDR 99ZZZM545](https://openairdocs.org/sdr/99ZZZM545), Jun 18, 1998: DOOR. CRACKED. NR 4 ENGINE INBOARD FAN DOOR, FORWARD INNER TITANIUM FIRESHIELD CRACKED AT CORNERS. REPAIRED CRACK BY PATCHING IAW BAE/AIR WISC SRM STD PRACTICES AND FOUND SERV - [SDR 99ZZZM537](https://openairdocs.org/sdr/99ZZZM537), Jun 15, 1998: STIFFENER. CRACKED. RIGHT WING TE SHROUD LOWER SKIN STIFFENER CRACKED INBOARD OF RIB 10. REMOVED AND REPLACED LOWER SKIN STIFFENER PER SRM. (M) - [SDR 98ZZZX3992](https://openairdocs.org/sdr/98ZZZX3992), Jun 15, 1998: ANGLE. MISSING. ATW - FORWARD CARGO BAY: CENTER FORWARD CARGO FLOOR SUPPORT ANGLE AT FRAME 19D, SECTION MISSING. REPLACED FORWARD CARGO BAY CENTER FLOOR SUPPORT ANGLE AT FRAME - [SDR 98ZZZX3954](https://openairdocs.org/sdr/98ZZZX3954), Jun 15, 1998: RIB. CRACKED. ATW - NR 1 (BOTTOM) RIB ON RUDDER IS CRACKED WITH A SMALL PIECE BROKEN OUT. REPLACED RIB PER REPAIR INSTRUCTIONS HC554H9005. - [SDR 98ZZZX3956](https://openairdocs.org/sdr/98ZZZX3956), Jun 12, 1998: SKIN. DAMAGED. ATW - RIGHT MLG DOOR FORWARD LOWER CORNER DAMAGE DUE REPAIR IN 2,000 FLIGHTS PER AVRO FAX JM/0642-97. SEE SRM FOR SKIN REPAIR CRITERIA CURRENT TCA 25066 DUE REP - [SDR 99ZZZM543](https://openairdocs.org/sdr/99ZZZM543), Jun 11, 1998: STIFFENER. CRACKED. LT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END, INBOARD OF RIB NR 10. REPLACED LEFT TE WING SHROUD TOP SKIN STIFFENER INBOARD OF NR 10 RIB AT THIS - [SDR 99ZZZM542](https://openairdocs.org/sdr/99ZZZM542), Jun 11, 1998: STIFFENER. CRACKED. LT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END, OUTBOARD OF RIB NR 8. REPLACED LEFT WING TE SHROUD TOP SKIN STIFFENER OUTBOARD OF RIB NR 8. - [SDR 99ZZZM540](https://openairdocs.org/sdr/99ZZZM540), Jun 11, 1998: STIFFENER. CRACKED. LEFT WING TE SHROUD LOWER SKIN STIFFENERS, TWO HAVE TAG ANGLE CRACKED AT AFT END, BETWEEN RIBS 8/9. REPLACED TWO ANGLES ON TE SHROUD LOWER SKIN STIFFENERS BETWE - [SDR 99ZZZM538](https://openairdocs.org/sdr/99ZZZM538), Jun 11, 1998: STIFFENER. CRACKED. LEFT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END INBOARD OF RIB NR 6. REPLACED TOP SKIN STIFFENER BETWEEN RIBS 5 AND 6 JUST INBOARD OF RIB 6 AT THI - [SDR 99ZZZM433](https://openairdocs.org/sdr/99ZZZM433), Jun 11, 1998: ANGLE. CRACKED. RIGHT WING TE TOP SKIN STIFFENER AFT TAG ANGLE CRACKED AT LOWER FLANGE BETWEEN RIBS 5 AND 6 OF SHROUD. REMOVED AND REPLACED AFT TAG ANGLE BETWEEN RIBS 5/6 FOR T - [SDR 99ZZZM541](https://openairdocs.org/sdr/99ZZZM541), Jun 10, 1998: STIFFENER. CRACKED. LT WING TE SHROUD TOP SKIN STIFFENER CRACK AT FORWARD END (BETWEEN RIBS 7/8). REPLACED LEFT WING TE SHROUD TOP SKIN STIFFENER BETWEEN RIB 7/8 AT THIS TIME. - [SDR 99ZZZM435](https://openairdocs.org/sdr/99ZZZM435), Jun 8, 1998: STIFFENER. CRACKED. RIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8 OF SHROUD. REMOVED AND REPLACED STIFFENER PER SRM. (M) - [SDR 99ZZZM434](https://openairdocs.org/sdr/99ZZZM434), Jun 8, 1998: STIFFENER. CRACKED. RIGHT WING TOP SKIN TE STIFFENER CRACKED AT FORWARD END, INBOARD OF RIB 9, SHROUD AREA. REMOVED AND REPLACED STIFFENER PER SRM. (M) - [SDR 98ZZZX3957](https://openairdocs.org/sdr/98ZZZX3957), Jun 8, 1998: SKIN. DENTED. ATW - REF W/C DATED 10-19-96, LT AFT FUSELAGE HAS DENT LOCATED 24 INCHES AFT OF LT PRESSURE BULKHEAD AND 6 INCHES BELOW 'N' NUMBERS. DENT IS 5 INCHES LONG BY MI - [SDR 99ZZZM539](https://openairdocs.org/sdr/99ZZZM539), Jun 5, 1998: BRACKET. CRACKED. LEFT WING TE, HYDRAULIC LINE CLAMP BRACKET CRACKED AT FALSE SPAR RIB NR 5. REPLACED HYDRAULIC LINE CLAMP BLOCK BRACKET AT RIB 5 AT THIS TIME. (M) - [SDR 99ZZZM431](https://openairdocs.org/sdr/99ZZZM431), Jun 5, 1998: CONTROL CABLE. CORRODED. THE CENTER FUSELAGE INTERCONNECT CABLES ARE CORRODED AT RIGHT WING ROOT. REMOVED AND REPLACED BOTH CENTER FUSELAGE INTERCONNECT CABLES AND ADJUSTED IAW MM 27-11 - [SDR 99ZZZM430](https://openairdocs.org/sdr/99ZZZM430), Jun 5, 1998: FITTING. LEAKING. COCKPIT OXYGEN SYSTEM HAS A LEAK. FAILED LEAK CHECK. REMOVED AND REPLACED 'T' FITTING BETWEEN SUPPLY GAUGE AND PRESSURE REDUCING VALVE UNDER RIGHT SIDE PANEL. C - [SDR 99ZZZM429](https://openairdocs.org/sdr/99ZZZM429), Jun 5, 1998: SILL. CORRODED. FORWARD VESTIBULE, PAX AND SERVICE DOOR, SILL PLATE HAV SOME CORROSION AROUND SCREW HOLES AND OTHER SMALL AREAS. MINOR SURFACE CORROSION REMOVED FROM SILL PLATE - [SDR 99ZZZM428](https://openairdocs.org/sdr/99ZZZM428), Jun 5, 1998: INTERCOSTAL. CORRODED. GUSSET PLATE AND FORWARD REST FLOOR SUPPORT INTERCOSTAL, LEFT OF CENTER, AT FRAME 18 IS CORRODED. INSTALLED NEW GUSSET PLATE. - [SDR 98ZZZX3958](https://openairdocs.org/sdr/98ZZZX3958), Jun 5, 1998: CAGE. DENTED. ATW - FORWARD CARGO DOOR AFT LOWER SEAL CAGE IS DENTED AND CRACKED. REPLACED FORWARD CARGO DOOR AFT LOWER SEAL CAGE. - [SDR 98ZZZM868](https://openairdocs.org/sdr/98ZZZM868), Jun 3, 1998: MANIFOLD. LEAKING. NR 1 ENGINE FUEL LEAK AT BOTH MANIFOLDS AT START. REPLACED LEFT AND RIGHT FUEL MANIFOLDS, REF WORK CARD NR 29. - [SDR 98ZZZM867](https://openairdocs.org/sdr/98ZZZM867), Jun 3, 1998: MANIFOLD. LEAKING. NR 1 ENGINE FUEL LEAK AT BOTH MANIFOLDS AT START. REPLACED LEFT AND RIGHT FUEL MANIFOLDS, REF WORK CARD NR 29. - [SDR 98ZZZX3991](https://openairdocs.org/sdr/98ZZZX3991), Jun 2, 1998: INTERCOSTAL. CORRODED. ATW - AFT VESTIBULE FLOOR SUPPORT STRUCTURE, FIRST INTERCOSTAL INBOARD OF AIRSTAIR RAILS, LT SIDE HAS A RIVET WITH CORROSION AROUND IT. DRILLED OUT RIVET, REMOV All 82: https://openairdocs.org/deregistered/N612AW-2008-01-31/reports.md ## FAA accident and incident reports (1) 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 19960513019109I](https://openairdocs.org/incident/19960513019109I), May 13, 1996: Bag BAE146300A (N612AW), Denver, CO. Narrative: aircraft was dispatched from springfield, IL (sgf) with #14800 of fuel. Crew confirmed the fuel on board, per their statements. Over goodland, KS… ## Other aircraft with N612AW - [Registered now](https://openairdocs.org/aircraft/N612AW): Hardison Michael R VANS ACFT RV-7, S/N 74045, built 2019 --- 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.