# N616AW: 1989 British Aerospace BAE 146 SERIES 300A, registration cancelled 2014-10-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 29, 2014
- Status when cancelled: Registration expired, pending cancellation
- 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: E3145
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, normal
- Airworthiness date: January 15, 1990
- Certificate issued: January 29, 2009
- Last registry action: January 29, 2009
- Mode S code: A8051D
- Owner when cancelled: [Hr Aviation LLC](https://openairdocs.org/faa-owner/HR%20AVIATION%20LLC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7965° N, 75.6128° W: Placed by OpenAirDocs at the center of ZIP code 19807, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N616AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=616AW
- Page: https://openairdocs.org/deregistered/N616AW-2014-10-29

From the FAA registry file of October 29, 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 (106, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR A6WA200460066](https://openairdocs.org/sdr/A6WA200460066), Dec 30, 2004: ACM. ODOR. NR 2 PACK WAS INADVERTENTLY SWITCHED ON FOR APPROX 10 MINUTES ENROUTE. PILOTS NOTICED ODOR IN COCKPIT, PACK SWITCHED OFF AND A PUFF OF WHITE SMOKE CAME OUT OF V
- [SDR A6WA200460052](https://openairdocs.org/sdr/A6WA200460052), Nov 11, 2004: OXYGEN MASK. MISINSTALLED. DURING INSPECTION, ALL PASSENGER O2 DROP DOWN MASKS WERE FOUND STOWED INCORRECTLY. MAINTENANCE RESTOWED ALL PASSENGER O2 DROP DOWN MASKS, CORRECTLY IAW AMM 35-2
- [SDR A6WA200460032](https://openairdocs.org/sdr/A6WA200460032), Aug 27, 2004: WIRE. SHORTED. SHORTLY AFTER TAKEOFF, LOST ALL RADIO COMMUNICATION. RETURNED TO RDU, LANDED UNDER LANDING WEIGHT. MAINTENANCE REPAIRED SHORTED KEY WIRE TO YOKE MIC JACK SYSTEM
- [SDR A6WA200360005](https://openairdocs.org/sdr/A6WA200360005), Apr 10, 2003: CABLE. UNSERVICEABLE. NR 2 THRUST LEVER WILL NOT MOVE BELOW CRUISE AT 31K (31,000 FEET), OK AFTER 14K (14,000 FEET). REMOVED AND REPLACED UPPER PYLON TELEFLEX CABLE. ON INSPECTION OF
- [SDR A6WA200260078](https://openairdocs.org/sdr/A6WA200260078), Dec 23, 2002: BLEED BAND. OUT OF TOLERANCE. UPON APPLICATION OF TAKEOFF POWER, NR 2 ENGINE DID NOT RESPOND WHILE TGT WENT TO 950 DEGREES FOR AN ESTIMATED 5 SECONDS BEFORE SECURING. MAINTENANCE FOUND NR 2 
- [SDR A6WA200260005](https://openairdocs.org/sdr/A6WA200260005), May 22, 2002: CAGE. CRACKED. REAR CARGO DOOR UPPER AFT INNER SEAL RETAINER CAGE IS CRACKED APPROX 2 INCHES IN LENGTH. REPLACED UPPER AFT INNER CAGE IAW SRM 51-42-00. REPAIRS CARRIED OUT PER
- [SDR A6WA200260010](https://openairdocs.org/sdr/A6WA200260010), May 22, 2002: FRAME. CHAFED. NR 3 ENGINE FORWARD INBOARD COWL DOOR HAS CHAFE MARKS ON FORWARD MOST FRAME. REPAIRED IAW BAE RIL HC711H9089. (M)
- [SDR A6WA200260007](https://openairdocs.org/sdr/A6WA200260007), May 22, 2002: DOOR. CRACKED. NR 4 ENGINE INBOARD AFT COWL DOOR HAS A CRACK NEXT TO DRAIN TUBE. REPAIRED CRACK IAW BAE PROCEDURE REF NR NWH/RJ/0726-02 AND RIL HC7IIH9012. (M)
- [SDR A6WA200260008](https://openairdocs.org/sdr/A6WA200260008), May 22, 2002: RETAINER. DAMAGED. ELECTRICAL EQUIPMENT BAY DOOR RETAINING ANGLE ON FORWARD FRAME DAMAGED. ANGLE REPAIRED IAW BAE PROCEDURE REF NR CH/RJ/0734-02. (M)
- [SDR A6WA200260006](https://openairdocs.org/sdr/A6WA200260006), May 22, 2002: STRUCTURE. CHAFED. FOUND LEFT AFT PAX DOOR AIRSTAIR HOOK CUTOUT HAS CHAFING FROM HOOK. REPAIRS CARRIED OUT IAW BAE PROCEDURE REF NR CH/RJ/0735/02. (M)
- [SDR A6WA200260004](https://openairdocs.org/sdr/A6WA200260004), May 22, 2002: SKIN. DENTED. DENT IN A VERTICAL DIRECTION AT STRINGER 26L BETWEEN FRAME 12 AND 13. FABRICATED A REPAIR PATCH. PERFORMED A DETAILED VISUAL INSPECTION TO ENSURE SOUND CRACK FR
- [SDR A6WA200260011](https://openairdocs.org/sdr/A6WA200260011), May 22, 2002: PANEL. DENTED. DENTS FOUND IN LEFT AND RIGHT WINGS TRAILING EDGE PANELS BETWEEN RIB 14A AND 15B. INSPECTION CARRIED OUT IAW MFG MM.
- [SDR A6WA200260013](https://openairdocs.org/sdr/A6WA200260013), May 22, 2002: TRIM TAB. DENTED. DENTS FOUND IN LEFT AILERON TRIM TAB. INSPECTION CARRIED OUT IAW MM.
- [SDR A6WA200260012](https://openairdocs.org/sdr/A6WA200260012), May 22, 2002: BRACKET. CRACKED. LEFT INBOARD SPOILER OUTBOARD END BRACKET CRACKED AT FORWARD TOP EDGE. CARRIED OUT IAW MFG NWH/RJ/0723-02.
- [SDR A6WA200260009](https://openairdocs.org/sdr/A6WA200260009), May 22, 2002: ATTACH ANGLE. CRACKED. FLOOR BEAM TO CROSSMEMBER ATTACH ANGLE CRACKED AT STA 183.15 FORWARD SIDE AND LBL 47 OUTBOARD SIDE. CROSSMEMBER ATTACH ANGLE REPLACED IAW SRM.
- [SDR A6WA200000082](https://openairdocs.org/sdr/A6WA200000082), Jan 4, 2001: A/C PACK. ODOR. SMOKY SMELL IN CABIN AFTER TAKEOFF, CREW SHUT OFF APU AIR AND SWITCHED TO ENGINE AIR, OPERATED ON NR 2 PACK AND SMOKY SMELL DISSIPATED. MAINTENANCE PERFORMED DU
- [SDR 98ZZZM936](https://openairdocs.org/sdr/98ZZZM936), Mar 19, 1998: DOOR WARNING. ACTIVATED. AFTER GEAR RETRACTION, LEFT MAIN GEAR INTRANSIT LIGHT 'RED' REMAINED ON AND RED LT IN GR HANDLE. COULD NOT DUPLICATE MEGGED AND UPLOCK HARNESSES. GEAR UPLOCK, 5
- [SDR 98ZZZX1234](https://openairdocs.org/sdr/98ZZZX1234), Dec 5, 1997: PAN. BROKEN. CAPTAIN'S SEAT ASSY SEAT PAN BROKEN AT FWD RT CORNER. PAN ALSO HAS SEVERAL OTHER CRACKS. MADE NEW SEAT PAN IAW PS1 DRAWING AW-25-10-9707-06 INSTALLED PER DRAWIN
- [SDR 98ZZZX1205](https://openairdocs.org/sdr/98ZZZX1205), Nov 28, 1997: HINGE. CRACKED. DURING ADJUSTMENT/CHECK OF RT NR 2 CARRIAGE FLAP CANOE, FOUND HINGE ASSY CRACKED AT TOP FORWARD TRANSVERSE BEAD. DRESSED OUT CRACKED AREA (JM/RJ085-97). C/W FLU
- [SDR 98ZZZX1208](https://openairdocs.org/sdr/98ZZZX1208), Nov 25, 1997: BRACKET. CRACKED. PSU RAIL RT OTBD, STAND-OFF BRACKET AT FRAMES 39-40 CRACKED AND RIVETS LOOSE. REPLACED BRACKET.
- [SDR 98ZZZX1209](https://openairdocs.org/sdr/98ZZZX1209), Nov 24, 1997: BULKHEAD FRAME. CHAFED. THERE IS AN L-SHAPED CHAFE MARK ON FRAME 32 PRESSURE BULKHEAD, NEAR CENTERLINE BEHIND RT MLG DOOR UPLOCK ASSY. NEEDS INVESTIGATION. BLENDED ABOVE AREA IAW BAE F
- [SDR 98ZZZX1201](https://openairdocs.org/sdr/98ZZZX1201), Nov 22, 1997: BRACKET. CRACKED. FORWARD PASSENGER DOOR - DOOR HANDLE SUPPORT BRACKET CRACKED. CHECKED WITH ET CRACK DEFECT NOTED. ITEM MARKED WITH TAG. MFG ABOVE BRACKET PER BAE DRAWING AND PS
- [SDR 98ZZZX1229](https://openairdocs.org/sdr/98ZZZX1229), Nov 21, 1997: RIB. CRACKED. ATW - LT WING TIP REMOVEABLE RIB PANEL HAS A FEW CRACKS IN IT. PATCHED SAID CRACKS IAW BAE STD PRACTICES AND AIR WISC MM PSI REF: AW-57-20-9412-06.
- [SDR 98ZZZX1199](https://openairdocs.org/sdr/98ZZZX1199), Nov 21, 1997: INTERCOSTAL. CRACKED. REAR FUSELAGE AREA - CENTER FLOOR SUPPORT INTERCOSTAL CRACKED UNDER GUSSET PLATE BETWEEN FRAMES 41 AND 43. MARKED WITH GREEN DOT. REPAIRED INTERCOSTAL IAW BAE F
- [SDR 98ZZZX1194](https://openairdocs.org/sdr/98ZZZX1194), Nov 21, 1997: FRAME. CRACKED. ATW - RIGHT SIDE OF ECS BAY AT FRAME NR 47 HAS A CRACK IN THE SHEAR ANGLE AT STR 9 THAT IS APPROX .25 INCH LONG IN THE BEND RADIUS. NOTE: VERIFIED WITH EDDY CUR
- [SDR 98ZZZX1207](https://openairdocs.org/sdr/98ZZZX1207), Nov 20, 1997: ANGLE. CRACKED. REAR CARGO BAY FLOOR SUPPORT ANGLE CRACKED AT SCREW HOLE FRAME 34. SPLICED 8 INCH SECTION TO SUPPORT ANGLE PER SRM 51-71-11, DAMAGED AREA REMOVED.
- [SDR 98ZZZX1221](https://openairdocs.org/sdr/98ZZZX1221), Nov 19, 1997: STIFFENER. CRACKED. ATW - RIGHT WING TOP T/E SKIN STIFFENER CRACKED AT FWD END JUST INBD OF RIB NR 8. REPAIRED STIFFENER, REF FAX JM/RJ0317/97, AND JM/RJ0818-97.
- [SDR 98ZZZX1219](https://openairdocs.org/sdr/98ZZZX1219), Nov 19, 1997: INTERCOSTAL. BROKEN. ATW - FORWARD CARGO INTERCOSTAL BROKEN BETWEEN FRAMES 23 AND 23 LT SIDE. REPAIRED INTERCOSTAL IAW BAE 146 SRM AND REINSTALLED IAW BAE 146 SCM. REF: 51-71-11. RE
- [SDR 98ZZZM372](https://openairdocs.org/sdr/98ZZZM372), Nov 19, 1997: STIFFENER. CRACKED. RT WING TOP TE SKIN STIFFENER CRACKED AT FWD END BETWEEN RIBS 8/9, JUST OUTBOARD OF RIB 8. REPAIRED CRACKED STIFFENER IAW FAX NR'S JM/RJO317/97 AND NR JM/RJO818
- [SDR 98ZZZM369](https://openairdocs.org/sdr/98ZZZM369), Nov 19, 1997: STIFFENER. CRACKED. LT WING, TRAILING EDGE AND SHROUD UPPER SKIN STIFFENER IS CRACKED AT FORWARD END IN AREA BETWEEN WING RIBS 7 AND 8. REPAIRED STIFFENER REF FAX JM/RJ0818-97. (M)
- [SDR 98ZZZM365](https://openairdocs.org/sdr/98ZZZM365), Nov 19, 1997: STIFFENER. CRACKED. RT WING TOP TE SKIN STIFFENER CRACKED AT FWD END AT RIB NR 9, JUST INBOARD OF RIB 9. REPAIRED CRACKED STIFFENER IAW FAX NR'S JM/RJ0317/97 AND NR JM/RJO317/97 AN
- [SDR 98ZZZX1195](https://openairdocs.org/sdr/98ZZZX1195), Nov 18, 1997: FRAME. CRACKED. ATW - RIGHT SIDE OF STRUCTURE AFT OF FR 50 HAS A FRAME THAT IS CRACKED LOCATED ABOVE UPPER HINGE BLADE FOR AIRBRAKE BACKSIDE OF FR 50. CRACK IS UNDER OUTER CORN
- [SDR 98ZZZM366](https://openairdocs.org/sdr/98ZZZM366), Nov 18, 1997: FRAME. CRACKED. LEFT SIDE OF STRUCTURE AFT OF FRAME 50 HAS A FRAME ABOVE THE UPPER HINGE BLADE FOR SPEED BRAKE THAT HAS A CRACK ACROSS THE 3RD RIVET HOLE DOWN ON OUTER FLANGE T
- [SDR 98ZZZM364](https://openairdocs.org/sdr/98ZZZM364), Nov 18, 1997: WEB. CRACKED. RT SIDE OF STRUCTURE AFT OF FRAME NR 50 HAS A WEB THAT RUNS VERTICALLY FROM THE REAR FLANGE OF FRAME NR 50 DOWN TO THE LOWER BLADE OF THE SPEED BRAKE HINGE THAT
- [SDR 98ZZZX1202](https://openairdocs.org/sdr/98ZZZX1202), Nov 17, 1997: INSERTS. CORRODED. FORWARD LAV MODULE, METAL INSERTS IN FLOOR CORRODED. REPLACED AS NEEDED. INSTALLED PERMACEL AFTER REPLACMENT OF INSERTS. REPLACED INSERTS AS NEEDED AND INSTALLE
- [SDR 98ZZZX1236](https://openairdocs.org/sdr/98ZZZX1236), Nov 14, 1997: BRACKET. CRACKED. NR 2 ENGINE SHOULDER COWL TERMINAL BOARD FWD BRACKET CRACKED. REPLACED NR 2 ENG SHOULDER COWL TERMINAL BOARD FWD BRACKET.
- [SDR 98ZZZX1233](https://openairdocs.org/sdr/98ZZZX1233), Nov 13, 1997: BRACKET. BROKEN. FWD CLOSET WALL BEHIND FO'S SEAT, LOWER CORNER ATTACH BRACKET BROKEN. FABRICATED AND REPLACED FWD CLOSET WALL BRACKET BEHIND FO'S SEAT (LOWER ATTACH BRACKET).
- [SDR 98ZZZX1227](https://openairdocs.org/sdr/98ZZZX1227), Nov 13, 1997: SILL. CORRODED. AFT VESTIBULE SILL PLATE FOR SERVICE DOOR SIDE HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED AFT VESTIBULE SERVICE DOOR SILL PLATE.
- [SDR 98ZZZX1224](https://openairdocs.org/sdr/98ZZZX1224), Nov 13, 1997: ANGLE. CRACKED. ATW - RT WING T/E LOWER SKIN STIFFENER AFT TAG ANGLE CRACKED BETWEEN RIBS 3 AND 4. REPLACED ANGLE.
- [SDR 98ZZZX1223](https://openairdocs.org/sdr/98ZZZX1223), Nov 13, 1997: ANGLE. CRACKED. RT WING T/E LOWER SKIN STIFFENER AFT TAG ANGLE CRACKED AT RIB NR 4. REPLACED ANGLE.
- [SDR 98ZZZX1222](https://openairdocs.org/sdr/98ZZZX1222), Nov 13, 1997: ANGLE. CRACKED. ATW - RT WING T/E LOWER SKIN STIFFENERS AFT TAG ANGLE CRACKED BETWEEN RIBS 5 AND 6. REPLACED ANGLE.
- [SDR 98ZZZX1206](https://openairdocs.org/sdr/98ZZZX1206), Nov 13, 1997: SEAL CAGE. CRACKED. REAR CARGO DOOR LOWER AFT SEAL CAGE CRACKED. REPLACED LOWER AFT SEAL CAGE.
- [SDR 98ZZZX1226](https://openairdocs.org/sdr/98ZZZX1226), Nov 12, 1997: BOLTS. LOOSE. ATW - AIR WISC EO E92/083/657 RECC ATTACH BOLTS AND NUTS ON RT SIDE, A, B, C, D ARE LOOSE ON THE REAR SPAR ROOT ATTACHMENT FITTING AT WING RIB 2. REPLACED FASTE
- [SDR 98ZZZX1225](https://openairdocs.org/sdr/98ZZZX1225), Nov 11, 1997: MOUNTING. CRACKED. ATW - RT LIFT SPOILER VALVE MOUNTING PLATE CRACKED. REMOVED AND REPLACED RT SPOILER VALVE MOUNTING PLATE. NO DISCONNECTING OF VALVE REQUIRED.
- [SDR 98ZZZX1237](https://openairdocs.org/sdr/98ZZZX1237), Nov 7, 1997: COWL. CHAFED. NR 2 ENGINE LT FWD COWL DOOR AFT FRAME CHAFED AT LATCH AREA AND AT MID-AREA DUE TO CONTACT WITH HYDRAULIC LINE. REPLACED CAP STRIP ON NR 2 ENG LT FWD COWL DOOR 
- [SDR 98ZZZX1216](https://openairdocs.org/sdr/98ZZZX1216), Nov 7, 1997: FLOOR. BUCKLED. REF FAX LM/115-97, LM/116-97, JM/RJ0096-97, AND DJR/RJ0098-97. MLG PRESS FLOOR BETWEEN FRAMES 29 AND 32 OTBD SEAT RAILS 19 INCHES, 20 INCHES OTBD CENTERLINE HV 
- [SDR 98ZZZX1231](https://openairdocs.org/sdr/98ZZZX1231), Nov 6, 1997: BRACKET. CRACKED. ATW - LT WING BRACKET FOR HYD LINES THAT PASS THROUGH THE AFT END OF THE SPOILER HINGE RIB AT WING RIB NR 5 IS CRACKED. REPLACED BRACKET.
- [SDR 98ZZZX1220](https://openairdocs.org/sdr/98ZZZX1220), Nov 6, 1997: ANGLE. CRACKED. FREIGHT ANGLE AT FRAME 19D CRACKED CENTER SECTION. REPLACED FREIGHT ANGLE AT FRAME 19D IAW BAE 146 SRM.
- [SDR 98ZZZX1213](https://openairdocs.org/sdr/98ZZZX1213), Nov 6, 1997: JOBOLTS. DAMAGED. REPLACED JOBOLTS ON RT WING CENTER TANK RIB 2 INBOARD PER RIL HC571H9033. PERFORMED RIL HC571H9033 TO RIB 2 INBD CENTER TANK. REPLACED JOBOLTS WITH MRL FASTENER
- [SDR 98ZZZX1203](https://openairdocs.org/sdr/98ZZZX1203), Nov 6, 1997: SUPPORT. CRACKED. FRONT CARGO BAY CENTER CARGO FLOOR SUPPORT AT 19C CORRODED AND CRACKED. AREA MARKED. REPLACED FREIGHT ANGLE AT FR 19C IAW BAE 146 SRM.

All 106: https://openairdocs.org/deregistered/N616AW-2014-10-29/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 19910325011989I](https://openairdocs.org/incident/19910325011989I), Mar 25, 1991: Bac 146300A (N616AW), Huntsville, AL, Minor damage. Four main tires blew on rollout. Appears brake selector not in correct position. Back up system failed,brakes locked

## Other aircraft with N616AW

- [Registered now](https://openairdocs.org/aircraft/N616AW): Piper PA-28-181, S/N 28-7790171, built 1976

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