# N614AW: 1988 British Aerospace BAE 146 SERIES 300A, registration cancelled 2005-09-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 23, 2005
- Exported to: United Kingdom
- 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: E3132
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, normal
- Airworthiness date: July 18, 1989
- Certificate issued: September 8, 2005
- Last registry action: September 8, 2005
- Mode S code: A7FDAF
- Owner when cancelled: [Rpk Capital Management Group LLC](https://openairdocs.org/faa-owner/RPK%20CAPITAL%20MANAGEMENT%20GROUP%20LLC)
- Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago)
- Owner type: Corporation
- Owner's area on the map: 41.9022° N, 87.6833° W: Placed by OpenAirDocs at the center of ZIP code 60622, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N614AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=614AW
- Page: https://openairdocs.org/deregistered/N614AW-2005-09-23

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 (51, newest 50)

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

- [SDR A6WA200560004](https://openairdocs.org/sdr/A6WA200560004), Jan 12, 2005: RECEPTACLE. SPARKS. EXTERNAL AC POWER RECEPTICAL SPARKS EXCESSIVELY AND SCORCHED WHEN ATTEMPTING TO CONNECT EXTERNAL POWER. AIRCRAFT ELECTRICAL SYSTEM OPS NORMAL. MAINTENANCE INSPE
- [SDR A6WA200360065](https://openairdocs.org/sdr/A6WA200360065), Oct 28, 2003: DOOR FRAME. CRACKED. AFT PAX DOOR, AFT SIDE FRAME, HAS TWO CRACKS APPROXIMATELY .75 INCH LONG NEAR DOOR SNUBBER ATTACHMENT AREA. MAINTENANCE COMPLIED WITH PERMANENT REPAIR. INSTALLE
- [SDR A6WA200260033](https://openairdocs.org/sdr/A6WA200260033), Jul 17, 2002: FUEL CONTROL. MALFUNCTIONED. NR 2 ENGINE WENT SUB-IDLE ON APPROACH, HUNG AT 39-40 PERCENT NR 2 AND WOULD NOT ACCELERATE. CREW SHUT DOWN ENGINE. MAINTENANCE REMOVED AND REPLACED FUEL CONTROL
- [SDR A6WA200260032](https://openairdocs.org/sdr/A6WA200260032), Jul 6, 2002: J-BOX. SMOKE. PILOTS REPORT THE FORWARD CARGO SMOKE WARNING LIGHT ILLUMINATED, FIRE BOTTLE WAS FIRED. MAINTENANCE INSPECTED AND FOUND THE SOFT START RESISTOR BOX SMOLDERING. 
- [SDR A6WA200100029](https://openairdocs.org/sdr/A6WA200100029), Apr 22, 2001: ELEVATOR. CONTAMINATED. PITCH OSCILLATION OCCURRED ON CLIMBOUT. MAINTENANCE DRAINTED WATER FROM ELEVATORS.
- [SDR A6WA200100012](https://openairdocs.org/sdr/A6WA200100012), Feb 4, 2001: COUPLING. CRACKED. PIPE ASSEMBLY COUPLING, BOTTLE RT, TO COUPLING FLOW VALVE WAS CRACKED ON NR 3 ENGINE. MAINTENANCE REMOVED AND REPLACED NR 3 ENGINE PIPE ASSEMBLY FROM FIRE EXTIN
- [SDR A6WA9900086](https://openairdocs.org/sdr/A6WA9900086), Jul 21, 1999: COVER. MISSING. UPON REMOVAL OF LEFT FORWARD EVACUATION SLIDE, FOUND D-SHACKLE ASSY MISSING. INSTALLED LT FORWARD EVAC SLIDE. C/W COVER LATCH PULL CHECK AND BATTERY EFFICIENCY 
- [SDR A6WA9900085](https://openairdocs.org/sdr/A6WA9900085), Jul 7, 1999: FASTENER. FAILED. RIGHT MLG BAY, ON EACH FASTENER BROKEN IN MAIN BEAM TO SIDESTAY AT FRAME 29, FASTENER JUST INBOARD APPEARS TO BE LOOSE. REPLACED ONE EACH BROKEN HI-LOC. REMOVED
- [SDR A6WA9900087](https://openairdocs.org/sdr/A6WA9900087), Jul 2, 1999: WEB. CRACKED. NOSE LANDING GEAR SIDEWALL DIAPHRAGM CRACKED AT UPPER PIN BOSS. REPLACED LT NOSE GEAR DIAPHRAGM IAW BARA/AVRO/3677/99. (X)
- [SDR A6WA9900084](https://openairdocs.org/sdr/A6WA9900084), Jul 2, 1999: BOLT. FAILED. NR 2 ENGINE PYLON TO WING, OUTBOARD LOWER BOLT HAD IS SHEARED OFF. REPLACED LOWER OUTBOARD WING TO PYLON BOLT IAW MM 54-52-00. (X)
- [SDR A6WA9900088](https://openairdocs.org/sdr/A6WA9900088), Jun 30, 1999: SKIN. CRACKED. THERE IS A 2.75 INCH CRACK IN LT FUSELAGE BETWEEN FRAMES 35 AND 36 AT STR 19, 6 INCHES FORWARD OF FRAME 38. CRACK RUNS STRAIGHT ALONG EDGE OF INNER LAP JOINT. R
- [SDR 98ZZZX3976](https://openairdocs.org/sdr/98ZZZX3976), Aug 9, 1998: SLIDE. DAMAGED. MKE - FLT 621 - LEFT FORWARD PASSENGER DOOR EMERGENCY SLIDE HAS DROPPED DOWN IN ITS OWN CONTAINER. REMOVED AND REPLACED LEFT FORWARD PASSENGER SLIDE IAW MM BATT
- [SDR 99ZZZM86](https://openairdocs.org/sdr/99ZZZM86), May 10, 1998: WARNING SYSTEM. ACTIVATED. CLIMBING OUT OF 20,000 FT, FLAP FAULT ILLUMINATED WITH FLAP GAUGE SHOWING 24 DEGREES AFTER LANDING. FLAPS RETRACTED NORMALLY, GAUGE INDICATED 0 DEGREES.
- [SDR 98ZZZX1184](https://openairdocs.org/sdr/98ZZZX1184), Nov 11, 1997: FLOW VALVE. DETACHED. ATW - NR 2 DIRECTIONAL FLOW VALVE FLAPPER FOUND DETACHED DURING SCHEDULED MAINTENANCE. REPLACED VALVE. VALVE IS PART OF NOSE COWL P/N HC716H001-028B, S/N SB/BAE
- [SDR 97ZZZM857](https://openairdocs.org/sdr/97ZZZM857), Jun 11, 1997: RIVETS. MISSING. INSTALL 2 RIVETS AT RIGHT FUSELAGE FRAME 19 AND STRINGER 21 (REF W/C 2132). INSTALLED 2 RIVETS.
- [SDR 97ZZZM860](https://openairdocs.org/sdr/97ZZZM860), Jun 6, 1997: STOP. WORN. LEFT MIDDLE LIFT SPOILER INBOARD HINGE BOLT ANTI-ROTATION STEP WORN FROM WORKING BOLT HEAD. REMOVED AND REPLACED ANTI ROTATION STOP. (M)
- [SDR 97ZZZM859](https://openairdocs.org/sdr/97ZZZM859), Jun 6, 1997: STOP. WORN. LT INBOARD LIFT SPOILER OUTBOARD HINGE BOLT ANTI-ROTATION STOP WORN FROM WORKING BOLT HEAD. REMOVED AND REPLACED ANTI-ROTATION STOP. (M)
- [SDR 97ZZZM858](https://openairdocs.org/sdr/97ZZZM858), Jun 6, 1997: SPRING. CORRODED. RIGHT WING AILERON/SPOILER CAM BOX SPRING CORRODED. REMOVED AND REPLACED RIGHT WING AILERON/SPOILER CAM BOX SPRING.
- [SDR 97ZZZM862](https://openairdocs.org/sdr/97ZZZM862), Jun 5, 1997: BOLT. FAILED. LEFT NR 4 FLAP UPPER CARRIAGE TO MAIN FLAP FAIL/SAFE BOLT FAILS NDT. INSTALLED SERVICEABLE FAIL/SAFE BOLT AT LEFT NR 4 UPPER CARRIAGE TO FLAP POSITION.
- [SDR 97ZZZM861](https://openairdocs.org/sdr/97ZZZM861), Jun 5, 1997: SKIN. CRACKED. LEFT INBOARD LIFT SPOILER HAS SMALL CRACK IN TOP SKIN AT CENTER HINGE AREA. REPAIRED LEFT INBOARD LIFT SPOILER CENTER, HINGE AREA IAW BAE FAX DJR/RJ0498-97.
- [SDR 97ZZZM863](https://openairdocs.org/sdr/97ZZZM863), Jun 3, 1997: STRUCTURE. CRACKED. UPPER FRAME IN STRUCTURE AFT OF FRAME NR 50 HAS ITS LOWER RIGHT CORNER CRACKED AND THE CLEAT THAT ATTACHES IT TO THE UPPER RIGHT HINGE MEMBER IS LOOSE WITH ONE 
- [SDR 97ZZZM864](https://openairdocs.org/sdr/97ZZZM864), Jun 2, 1997: LINK. CHAFED. NR 1 ENGINE REAR LINK UPPER HALF CHAFED BEYOND MAX ALLOWABLE DEPTH. REPLACED NR 1 ENGINE REAR LINK UPPER HALF, REF ENG CHANGE CHECKLIST FOR DETAILS.
- [SDR 97ZZZM839](https://openairdocs.org/sdr/97ZZZM839), May 31, 1997: BOLT. CRACKED. FUSELAGE MAIN FRAME LEFT OUTBOARD LOWER FRAME 4 BOLT CRACK INDICATION UNDER HEAD. REPLACED LEFT OUTBOARD LOWER FRAME 4 ATTACH BOLT TO FLT DECK FL00R IAW BAE 146
- [SDR 97ZZZM838](https://openairdocs.org/sdr/97ZZZM838), May 31, 1997: BOLT. CRACKED. FUSELAGE MAIN FRAME, RIGHT INBOARD LOWER FRAME 4 DAMAGED BOLT NO CRACK INDICATIONS. REPLACED RT INBOARD LOWER FRAME 4 BOLT FOR FLT DECK FLOOR IAW BAE 146 MM. (M
- [SDR 97ZZZM840](https://openairdocs.org/sdr/97ZZZM840), May 28, 1997: ACTUATOR BOLTS. FAILED TEST. LEFT OUTBOARD LIFT SPOILER ACTUATORS AFT ATTACH BOLT FAILS NDT. INSTALLED SERVICEABLE BOLT AT LEFT OUTBOARD SPOILER AFT ACTUATOR ATTACH POINT IAW BAE MM. (M)
- [SDR 97ZZZM841](https://openairdocs.org/sdr/97ZZZM841), May 27, 1997: RIB. CHAFED. VERT STABILIZER LEADING EDGE NOSE RIB NR 1 HAS CHAFING DAMAGE ON BOTH SIDES OF LIGHTNING HOLE AT ITS LIP. RT SIDE IS CRACKED DOWN TO THE LIPS RADIUS AND LEFT SI
- [SDR 97ZZZM843](https://openairdocs.org/sdr/97ZZZM843), May 23, 1997: SHEAR PIN. RUSTED. NR 1 PYLON INBOARD SHEAR LINK PIN IS RUSTY, BOLT HAS BEEN REMOVED. REPLACED NR 1 PYLON INBOARD SHEAR LINK PIN IAW BAE DRAWING HC574H0030. (M)
- [SDR 97ZZZM842](https://openairdocs.org/sdr/97ZZZM842), May 23, 1997: ANGLE. CRACKED. FORWARD PASS DOOR ANGLE CRACKED UNDER MOUNTING BOX TO DOOR OPERATING MECHANISM. REF SRM 52-11-11 FIG 1 (SHEET 1 INCH, DETAIL 'E') ITEM NR 27. REPLACED BOTH ANGL
- [SDR 97ZZZM845](https://openairdocs.org/sdr/97ZZZM845), May 20, 1997: GUSSET. CORRODED. GUSSET PLATE AT FRAME 15, 2ND INTERCOSTAL INBOARD FROM LEFT SIDE AT FORWARD END IS CORRODED IN THE FORWARD VESTIBULE FLOOR SUPPORT STRUCTURE. REPLACED GUSSET PL
- [SDR 97ZZZM844](https://openairdocs.org/sdr/97ZZZM844), May 20, 1997: CONTROL CABLE. CORRODED. CENTER AILERON INTERCONNECT CABLES ARE CORRODED. REMOVED AND REPLACED BOTH CENTER MAIN AILERON INTERCONNECT CABLES, TENSIONED TO PROPER SETTING AND SAFETIED, (G
- [SDR 97ZZZM846](https://openairdocs.org/sdr/97ZZZM846), May 16, 1997: BOLTS. DAMAGED. LEFT AILERON RIB 20 'A FRAME' BOLTS SHOW EVIDENCE OF DISPLACED 'FAIL/SAFE' PIN. INSTALLED SERVICEABLE FAIL/SAFE BOLTS LEFT RIB 20 AILERON 'A FRAMES'.
- [SDR 97ZZZM847](https://openairdocs.org/sdr/97ZZZM847), May 15, 1997: BOLT. DAMAGED. TOP RUDDER ACTUATOR AFT BOLT WAS SCRAPPED BY INSPECTED DEPT DUE TO THREAD DAMAGE. INSTALLED A NEW BOLT IN TOP RUDDER ACTUATOR AFT POSITION.
- [SDR 97ZZZM849](https://openairdocs.org/sdr/97ZZZM849), May 13, 1997: INTERCOSTAL. CRACKED. FRAME 29 UNDER CABIN FLOOR INTERCOSTAL CRACKED 19 AND 3, 9 FRAME 32 UNDER CABIN FLOOR INTERCOSTAL CRACKED NR 19. REPAIRED INTERCOSTALS AT FRAME 29 AT NR 3, 9 AN
- [SDR 97ZZZM848](https://openairdocs.org/sdr/97ZZZM848), May 13, 1997: BOLTS. FAILED. RIGHT ELEVATOR NR 4 'A' FRAME BOTH BOLTS FAILED NDT. INSTALLED NEW BOLTS IN RIGHT NR 4 ELEVATOR 'A' FRAME. SECURED AND SAFETIED.
- [SDR 97ZZZM850](https://openairdocs.org/sdr/97ZZZM850), May 12, 1997: BOLTS. CORRODED. LEFT ELEVATOR A FRAME HINGE ATTACH BOLTS (BOTTOM) AT HORIZ STAB REAR SPAR AT HINGE POSITIONS 1, 2 AND 4 HAVE PITTING CORROSION AND LESS OF CADNIUM PLATING. REPL
- [SDR 97ZZZM852](https://openairdocs.org/sdr/97ZZZM852), May 9, 1997: THRESHOLD. CORRODED. AFT PASSENGER DOOR THRESHOLD HAS HOLE CORRODED THROUGH THRESHOLD. REPLACED AFT PASSENGER DOOR SILL PLATE.
- [SDR 97ZZZM851](https://openairdocs.org/sdr/97ZZZM851), May 9, 1997: BRACKET. CRACKED. LEFT WING UPPER TRAILING EDGES SHROUD STIFFENER IN AREA BETWEEN WING RIB 3 AND 4 HAS THE BRACKET AT ITS AFT END CRACKED AND A CRACK AT A RIVET HOLE WHERE SAME B
- [SDR 97ZZZM853](https://openairdocs.org/sdr/97ZZZM853), May 7, 1997: SKIN. DENTED. FUSELAGE SKIN DENTED BETWEEN FRAME 14/15 JUST BELOW REPAIR PATCH RT. ALSO, OIL CANNING OF SKIN HAS BEEN FOUND JUST AFT OF PATCH. COMPLIED WITH RT FUSELAGE PART 
- [SDR 97ZZZM856](https://openairdocs.org/sdr/97ZZZM856), May 6, 1997: CAM BOX SPRING. CORRODED. RIGHT WING AILERON/SPOILER CAM BOX SPRING CORRODED. REMOVED AND REPLACED RIGHT WING AILERON/SPOILER CAM BOX SPRING.
- [SDR 97ZZZM855](https://openairdocs.org/sdr/97ZZZM855), May 6, 1997: CONTROL CABLE. CORRODED. LEFT AND RIGHT ELEVATOR CONTROL CABLES HAVE SIGNS OF CORROSION AT TOP VERTICAL STAB PULLEYS. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR CONTROL CABLES FROM CA
- [SDR 97ZZZM854](https://openairdocs.org/sdr/97ZZZM854), May 6, 1997: BOLT. CRACKED. FRAME 27 LEFT AND RIGHT WING TO FUSELAGE LUG ATTACHMENT BOLT, LOWER, APPEARS TO BE BROKEN. REMOVED BOLTS, NDT SHOWED CRACKS IN BOLTS. CLEAN, INSPECTED HOLE, DIM
- [SDR 97ZZZM401](https://openairdocs.org/sdr/97ZZZM401), Dec 6, 1996: FAIRING. CRACKED. LEFT INBOARD FLAP TRACK AFT FAIRING HAS DAMAGE ON THE INBOARD SIDE. REMOVED AND REPLACED LEFT INBOARD FLAP TRACK AFT FAIRING. (M)
- [SDR 96ZZZM758](https://openairdocs.org/sdr/96ZZZM758), Feb 3, 1996: HARNESS. FAILED. LANDING GEAR HANDLE REQ OVERRIDE ON GEAR RETRACTION AFTER TAKEOFF FROM ORD. REMOVED AND REPLACED RIGHT MLG WEIGHT OFF HARNESS ASSY.
- [SDR 95ZZZX6227](https://openairdocs.org/sdr/95ZZZX6227), Oct 19, 1995: ANTENNA. FAILED. DEN - FLT 354 - NR 1 COMM RADIO BECOMES TOTALLY UNUSEABLE AS DISTANCE INCREASES TO STATION. COMPLETELY DEAD ON 1ST CENTER FREQUENCY. REMOVED AND REPLACED NR 1 V
- [SDR 95ZZZM310](https://openairdocs.org/sdr/95ZZZM310), Jul 17, 1995: HYD SELECTOR VLV. FAILED. GEAR FAILED TO EXTEND WHEN SELECTED. WENT TO EMERGENCY AND GEAR EXTENDED. LANDED WITHOUT INCIDENT. SENT REPLACEMENT VALVE AND ACTUATOR TO DEN. REPLACED VALVE AN
- [SDR 95ZZZX4141](https://openairdocs.org/sdr/95ZZZX4141), May 25, 1995: STIFFENER. CRACKED. LEFT AND RIGHT FRAME 29 STIFFENERS CRACKED AT STA 25.94 E.O. E95/005/653. ORIGINAL ISSUE NEEDS TO BE C/W. REPAIRED CRACKED STIFFENERS IAW E.O. E95/005/653, ORIG
- [SDR 95ZZZM314](https://openairdocs.org/sdr/95ZZZM314), May 24, 1995: SILL. CORRODED. FORWARD PASSENGER DOOR LOWER SILL TO FLOOR FLANGE SILL CORRODED, FRAME 15-18. DRILLED OUT CORROSION, CONFIRMED AREA FREE FROM CRACKS AND CORROSION VIA NDT (DOC 
- [SDR 95ZZZW490](https://openairdocs.org/sdr/95ZZZW490), Mar 27, 1995: FIREWALL. CRACKED. CRACKING HAS BEEN NOTED AT FWD FACE OF THE APU BAY FWD. FIREWALL IN THE AREA OF THE EXHAUST PIPE. DEACTIVATED APU AND PLACED ON MEL. (W)
- [SDR 95ZZZW486](https://openairdocs.org/sdr/95ZZZW486), Mar 25, 1995: SMOKE HOOD. MALFUNCTION. FORWARD FLIGHT ATTENDANT SMOKE HOOD APPEARS TO BE ACTIVATED. REPLACED THE SMOKE HOOD.
- [SDR 95ZZZW512](https://openairdocs.org/sdr/95ZZZW512), Jan 18, 1995: UPLOCK JACK. REQ BLEED. AFTER TAKEOFF FROM ATW RT MAIN GEAR WOULD NOT COME UP. RECYCLE ONE TIME GEAR CAME UP. JACKED A/C AND BLEED RT UPLOCK JACK. OPS CK OK. GEAR SWING OK.

All 51: https://openairdocs.org/deregistered/N614AW-2005-09-23/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 19920310008439I](https://openairdocs.org/incident/19920310008439I), Mar 10, 1992: Bag BAE146300A (N614AW), Cedar Rapids, IA. Unable to lower gear on approach. After orbiting airport gear extended and locked spontaneously. Landed safely.

---
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.