# Service difficulty reports: N614AW, cancelled Sep 23, 2005

A list on [N614AW, cancelled Sep 23, 2005](https://openairdocs.org/deregistered/N614AW-2005-09-23.md).

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

Page 1 of 2 · 51 reports

- [SDR A6WA200560004](https://openairdocs.org/sdr/A6WA200560004.md): Receptacle · sparks · Jan 12, 2005 · N614AW · Bac 146300A · External Power System
  > EXTERNAL AC POWER RECEPTICAL SPARKS EXCESSIVELY AND SCORCHED WHEN ATTEMPTING TO CONNECT EXTERNAL POWER. AIRCRAFT ELECTRICAL SYSTEM OPS NORMAL. MAINTENANCE INSPECTED AREA, FOUND NO EVIDENCE OF SHORTING OR OPEN WIRES. (K)
- [SDR A6WA200360065](https://openairdocs.org/sdr/A6WA200360065.md): Door Frame · cracked · Oct 28, 2003 · N614AW · Bac 146300A · Fuselage Main, Structure
  > AFT PAX DOOR, AFT SIDE FRAME, HAS TWO CRACKS APPROXIMATELY.75 INCH LONG NEAR DOOR SNUBBER ATTACHMENT AREA. MAINTENANCE COMPLIED WITH PERMANENT REPAIR. INSTALLED REPAIR PLATE HC521H9032-200 IAW BAE FAX BARA/AVR/6571/03-MK. (M)
- [SDR A6WA200260033](https://openairdocs.org/sdr/A6WA200260033.md): Fuel Control · malfunctioned · Jul 17, 2002 · N614AW · Bac 146300A · Fuel Control/Turbine Engines
  > 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.md): J-Box · smoke · Jul 6, 2002 · N614AW · Bac 146300A · Electrical Power System Wiring
  > PILOTS REPORT THE FORWARD CARGO SMOKE WARNING LIGHT ILLUMINATED, FIRE BOTTLE WAS FIRED. MAINTENANCE INSPECTED AND FOUND THE SOFT START RESISTOR BOX SMOLDERING. REMOVED AND REPLACED THE RESISTOR BOX ASSEMBLY.
- [SDR A6WA200100029](https://openairdocs.org/sdr/A6WA200100029.md): Elevator · contaminated · Apr 22, 2001 · N614AW · Bag BAE146300A · Elevator Structure
  > PITCH OSCILLATION OCCURRED ON CLIMBOUT. MAINTENANCE DRAINTED WATER FROM ELEVATORS.
- [SDR A6WA200100012](https://openairdocs.org/sdr/A6WA200100012.md): Coupling · cracked · Feb 4, 2001 · N614AW · Bag BAE146300A · Extinguishing System
  > 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 EXTINGUISHER BOTTLE RT TO FLOW VALVE.
- [SDR A6WA9900086](https://openairdocs.org/sdr/A6WA9900086.md): Cover · missing · Jul 21, 1999 · N614AW · Bag BAE146300A · Emergency Equipment
  > 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 CHECK. BOTH CHECKS FOUND WITHIN REQUIRED PARAMETERS. ALL WORK ACOMPLISHED IAW BAE MM AND AIR CR
- [SDR A6WA9900085](https://openairdocs.org/sdr/A6WA9900085.md): Fastener · failed · Jul 7, 1999 · N614AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > 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 HI-LOC FASTENER JUST INBOARD OF BROKEN FASTENER. CLEANED AND INSPECTED HOLE, HOLE FOUND OK, REPL
- [SDR A6WA9900087](https://openairdocs.org/sdr/A6WA9900087.md): Web · cracked · Jul 2, 1999 · N614AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > 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.md): Bolt · failed · Jul 2, 1999 · N614AW · Bag BAE146300A · Nacelle/Pylon Structure
  > 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.md): Skin · cracked · Jun 30, 1999 · N614AW · Bag BAE146300A · Fuselage Main, Plate/Skin
  > 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. REPAIRED SAID CRACK BY CUTTING OUT DAMAGE AND RIVETING PATCH IAW BAE FAX REF BARA/AVRO/3667/99 DATE
- [SDR 98ZZZX3976](https://openairdocs.org/sdr/98ZZZX3976.md): Slide · damaged · Aug 9, 1998 · N614AW · Bag BAE146300A · Escape Slide
  > 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 BATTERY EFF CHECK DUE 3-5-99. COVER LATCH PULL OFF TEST C/W. S/N OFF 0310. S/N ON 0340.
- [SDR 99ZZZM86](https://openairdocs.org/sdr/99ZZZM86.md): Warning System · activated · May 10, 1998 · N614AW · Bag BAE146300A · Trailing Flap Position Indicating System
  > 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.md): Flow Valve · detached · Nov 11, 1997 · N614AW · Bag BAE146300A · Pneumatic Distribution System
  > 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/0385.
- [SDR 97ZZZM857](https://openairdocs.org/sdr/97ZZZM857.md): Rivets · missing · Jun 11, 1997 · N614AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > 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.md): Stop · worn · Jun 6, 1997 · N614AW · Bag BAE146300A · Spoilers
  > 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.md): Stop · worn · Jun 6, 1997 · N614AW · Bag BAE146300A · Spoilers
  > 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.md): Spring · corroded · Jun 6, 1997 · N614AW · Bag BAE146300A · Aileron Control System
  > 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.md): Bolt · failed · Jun 5, 1997 · N614AW · Bag BAE146300A · Trailing Edge Flaps
  > 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.md): Skin · cracked · Jun 5, 1997 · N614AW · Bag BAE146300A · Spoilers
  > 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.md): Structure · cracked · Jun 3, 1997 · N614AW · Bag BAE146300A · Fuselage Main, Structure
  > 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 RIVET MISSING (REF SRM 53-40-31 PG 3 ITEM 14). REPAIRED UPPER FRAME STRUCTURE AFT OF FRAME 50 AT RI
- [SDR 97ZZZM864](https://openairdocs.org/sdr/97ZZZM864.md): Link · chafed · Jun 2, 1997 · N614AW · Bag BAE146300A · Engine Thrust Reverser
  > 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.md): Bolt · cracked · May 31, 1997 · N614AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > 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 146MM. (M)
- [SDR 97ZZZM838](https://openairdocs.org/sdr/97ZZZM838.md): Bolt · cracked · May 31, 1997 · N614AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > 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.md): Actuator Bolts · failed test · May 28, 1997 · N614AW · Bag BAE146300A · Drag Control Actuator
  > 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.md): Rib · chafed · May 27, 1997 · N614AW · Bag BAE146300A · Vertical Stabilizer, Spar/Rib
  > 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 SIDE IS WORN A LITTLE AWAY AND WAS CAUSED BY ANTI-ICE DUCTING THAT PASSES THROUGH THE HOLE. REPAIR V
- [SDR 97ZZZM843](https://openairdocs.org/sdr/97ZZZM843.md): Shear Pin · rusted · May 23, 1997 · N614AW · Bag BAE146300A · Nacelle/Pylon Structure
  > 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.md): Angle · cracked · May 23, 1997 · N614AW · Bag BAE146300A · Passenger/Crew Doors
  > 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 ANGLES PER SRM AND FAN DJR/RJ0318-97. (M)
- [SDR 97ZZZM845](https://openairdocs.org/sdr/97ZZZM845.md): Gusset · corroded · May 20, 1997 · N614AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > 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 PLATE AND REAPPLIED PROTECTIVE FINISHES. (M)
- [SDR 97ZZZM844](https://openairdocs.org/sdr/97ZZZM844.md): Control Cable · corroded · May 20, 1997 · N614AW · Bag BAE146300A · Aileron Control System
  > CENTER AILERON INTERCONNECT CABLES ARE CORRODED. REMOVED AND REPLACED BOTH CENTER MAIN AILERON INTERCONNECT CABLES, TENSIONED TO PROPER SETTING AND SAFETIED, (GEN NEW W/C FOR FUNCTIONAL TEST).
- [SDR 97ZZZM846](https://openairdocs.org/sdr/97ZZZM846.md): Bolts · damaged · May 16, 1997 · N614AW · Bag BAE146300A · Ailerons
  > 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.md): Bolt · damaged · May 15, 1997 · N614AW · Bag BAE146300A · Rudder Actuator
  > 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.md): Intercostal · cracked · May 13, 1997 · N614AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > 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 AND 19 POSITIONS AND AT FRAME 32 NR 19 POSITION IAW BAE REPAIR DRAWING HC536H9211 AND FAX DJR/RJ0450-
- [SDR 97ZZZM848](https://openairdocs.org/sdr/97ZZZM848.md): Bolts · failed · May 13, 1997 · N614AW · Bag BAE146300A · Elevator Structure
  > 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.md): Bolts · corroded · May 12, 1997 · N614AW · Bag BAE146300A · Elevator Structure
  > 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. REPLACE 3 BOLTS. INSTALLED NEW BOLTS AT LEFT ELEVATOR 'A' FRAME LOWER POSITIONS AT 1, 2 AND 4 HINGES,
- [SDR 97ZZZM852](https://openairdocs.org/sdr/97ZZZM852.md): Threshold · corroded · May 9, 1997 · N614AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > AFT PASSENGER DOOR THRESHOLD HAS HOLE CORRODED THROUGH THRESHOLD. REPLACED AFT PASSENGER DOOR SILL PLATE.
- [SDR 97ZZZM851](https://openairdocs.org/sdr/97ZZZM851.md): Bracket · cracked · May 9, 1997 · N614AW · Bag BAE146300A · Wing Miscellaneous Structure
  > 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 BRACKET ATTACHES TO LOWER LIP. REPAIRED IAW SRM AND FAX'S DS/W/TS/28612/97 AND DS/W/TS/28596/97 ON L
- [SDR 97ZZZM853](https://openairdocs.org/sdr/97ZZZM853.md): Skin · dented · May 7, 1997 · N614AW · Bag BAE146300A · Fuselage Main, Plate/Skin
  > 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 SKIN REPLACEMENT LAP JNT E FRAME 14-19 RT SKIN CUT LINE APPROX 83.75 INCHES BELOW LAP JNT E. REPA
- [SDR 97ZZZM856](https://openairdocs.org/sdr/97ZZZM856.md): Cam Box Spring · corroded · May 6, 1997 · N614AW · Bag BAE146300A · Aileron Control System
  > 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.md): Control Cable · corroded · May 6, 1997 · N614AW · Bag BAE146300A · Elevator Control System
  > 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 CABLE COMPENSATORS TO REAR PRESSURE BULKHEAD. ADJUSTED IAW MM 27-31-00. GEN W/C FOR FUNCTIONAL CHEC
- [SDR 97ZZZM854](https://openairdocs.org/sdr/97ZZZM854.md): Bolt · cracked · May 6, 1997 · N614AW · Bag BAE146300A · Fuselage, Wing Attach Fittings
  > 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 CHECKS OK, ALODINE, INSTALLED REPLACEMENT BOLT IAW SRM AND FAX DJR/RJ0022-96, FRAME 29 LT/RT WITH
- [SDR 97ZZZM401](https://openairdocs.org/sdr/97ZZZM401.md): Fairing · cracked · Dec 6, 1996 · N614AW · Bag BAE146300A · Trailing Edge Flaps
  > 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.md): Harness · failed · Feb 3, 1996 · N614AW · Bag BAE146300A · Landing Gear Position and Warning
  > 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.md): Antenna · failed · Oct 19, 1995 · N614AW · Bag BAE146300A · VHF Communications System
  > 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 VHF COMM ANTENNA PER MM. OPS CHECK GOOD.
- [SDR 95ZZZM310](https://openairdocs.org/sdr/95ZZZM310.md): Hyd Selector Vlv · failed · Jul 17, 1995 · N614AW · Bag BAE146300A · Landing Gear Selector
  > GEAR FAILED TO EXTEND WHEN SELECTED. WENT TO EMERGENCY AND GEAR EXTENDED. LANDED WITHOUT INCIDENT. SENT REPLACEMENT VALVE AND ACTUATOR TO DEN. REPLACED VALVE AND ACTUATOR.
- [SDR 95ZZZX4141](https://openairdocs.org/sdr/95ZZZX4141.md): Stiffener · cracked · May 25, 1995 · N614AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > 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, ORIGINAL ISSUE. REPAIR DRAWINGS AW-53-20-9506-06.
- [SDR 95ZZZM314](https://openairdocs.org/sdr/95ZZZM314.md): Sill · corroded · May 24, 1995 · N614AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > 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 ON ANOTHER W/C) REPROTECTED AREA, PRIMED AND REPAINTED. (M)
- [SDR 95ZZZW490](https://openairdocs.org/sdr/95ZZZW490.md): Firewall · cracked · Mar 27, 1995 · N614AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > 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.md): Smoke Hood · malfunction · Mar 25, 1995 · N614AW · Bag BAE146300A · Emergency Equipment
  > FORWARD FLIGHT ATTENDANT SMOKE HOOD APPEARS TO BE ACTIVATED. REPLACED THE SMOKE HOOD.
- [SDR 95ZZZW512](https://openairdocs.org/sdr/95ZZZW512.md): Uplock Jack · req bleed · Jan 18, 1995 · N614AW · Bag BAE146300A · Landing Gear Retraction/Extension System
  > 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.

Next page: https://openairdocs.org/deregistered/N614AW-2005-09-23/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N614AW' AND deregistration_id = 'N614AW-2005-09-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N614AW-2005-09-23/reports

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