# Service difficulty reports: N646AW, cancelled May 10, 2006

A list on [N646AW, cancelled May 10, 2006](https://openairdocs.org/deregistered/N646AW-2006-05-10.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 · 61 reports

- [SDR AWXA200600414](https://openairdocs.org/sdr/AWXA200600414.md): Battery · inoperative · Mar 3, 2006 · N646AW · Airbus A320231 · Emergency Lighting
  > PHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED THE LEFT FORWARD CABIN EPSU BATTERY PACK HAD -LOW CHARGE-. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD CABIN EPSU BATTERY PACK IAW AMERICA WEST AIRLINES TASK CARD A1C33302. OPERATIONAL CHECKS WERE GOO
- [SDR AWXA200500954](https://openairdocs.org/sdr/AWXA200500954.md): Blades · failed · Aug 12, 2005 · N646AW · Airbus A320231 · Turbine Section
  > DURING CLIMBOUT, 500 AGL, LOUD BANG ACCOMPANIED WITH ACFT YAWING LT 5-10 FT. ENG RECOVERED IMMEDIATELY. ACFT CONTINUED & LANDED WITHOUT FURTHER EVENT. NO EMERGENCY ACTION TAKEN/DECLARED. MX BORESCOPED BOTH ENGINES TO ENSURE INTEGRITY. NO DEFECTS NOTED ON
- [SDR AWXA200500750](https://openairdocs.org/sdr/AWXA200500750.md): Battery Pack · discharged · Jun 24, 2005 · N646AW · Airbus A320231 · Emergency Lighting
  > DURING 8-DAY CHECK, FOUND BOTH LT AND RT OVERWING SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT (11WL) AND RT (12WL) BATTERY PACKS IAW AIRBUS MM 33-51-38-04. OPERATIONAL TESTS WERE GOOD.
- [SDR AWXA200500594](https://openairdocs.org/sdr/AWXA200500594.md): Epsu · faulty · May 22, 2005 · N646AW · Airbus A320231 · Emergency Lighting
  > PHX - EEL - DURING 8-DAY CHECK, A LT EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE LT EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK. OPERATIONAL CHECK WAS GOOD. BATTERY PACK INFORMATION: MANUFACTURER: DIEHL GM
- [SDR AWXA200500559](https://openairdocs.org/sdr/AWXA200500559.md): Flashlight · inoperative · May 14, 2005 · N646AW · Airbus A320231 · Emergency Equipment
  > LAS - EMERGENCY EQUIPMENT DURING 8-DAY CHECK, THE AFT FLIGHT ATTENDANT FOLD OUT JUMP SEAT EMERGENCY FLASHLIGHT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200401353](https://openairdocs.org/sdr/AWXA200401353.md): Slide · delaminated · Nov 30, 2004 · N646AW · Airbus A320231 · Escape Slide
  > PHX - EES - DURING 4-DAY CHECK THE LOWER AFT CORNER OF THE RT OVERWING SLIDE WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING SLIDE ASSEMBLY IAW T/C R1A25301.
- [SDR AWXA200400561](https://openairdocs.org/sdr/AWXA200400561.md): Deu · faulty · May 21, 2004 · N646AW · Airbus A320231 · Emergency Lighting
  > PHX - EEL DURING 4-DAY CHECK: FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM FAILED AT CIDS PANEL. MAINTENANCE REMOVED AND REPLACED DECODER ENCODER UNIT (DEU) B (300RH5) IAW AMM 23-73-47, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400333](https://openairdocs.org/sdr/AWXA200400333.md): Flashlight · inoperative · Apr 1, 2004 · N646AW · Airbus A320231 · Emergency Equipment
  > PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT OUTBOARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT OUTBOARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400302](https://openairdocs.org/sdr/AWXA200400302.md): Bearing · failed · Mar 23, 2004 · N646AW · Airbus A320231 · Air Distribution Fan
  > PHX - EMERGENCY LANDING - FLT 0272 - ON SHORT AND FINAL INTO PHX EN ROUTE FROM SNA ENCOUNTERED SMOKE AND A STRONG ELECTRICAL BURNING ODOR IN CABIN, DONNED MASKS AND DECLARED EMERGENCY. MAINTENANCE FOUND THE AVIONICS COOLING FAN (EXTRACT FAN) BEARINGS SEIZED C
- [SDR AWXA200301080](https://openairdocs.org/sdr/AWXA200301080.md): Diaphragm · leaking · Sep 12, 2003 · N646AW · Airbus A320231 · Passenger/Crew Doors
  > DURING INSPECTION FOUND THE L-2 DOOR EMERGENCY OPERATION CYLINDER PRESSURE GAUGE READING ZERO. MAINTENANCE REMOVED AND REPLACED THE DIAPHRAGM IN PERCUSSION MECHANISM OF L-2 DOOR EMERGENCY OPERATION CYLINDER, SERVICED TO PROPER PRESSURE, LEAK AND OPERATIONAL CH
- [SDR AWXA200301008](https://openairdocs.org/sdr/AWXA200301008.md): Connector · damaged · Sep 1, 2003 · N646AW · Airbus A320231 · Engine Bleed Air System
  > EN ROUTE, AFTER TAKEOFF BLEEDS OFF RECEIVED ECAM MESSAGE NR 2 ENG BLEED ABNORMAL PRESS. TURNED OFF APU BLEED SWITCH NR 2 ENG BLEED ONLY AT 24 PSI, DIVERTED FOR REPAIR. MAINT REMOVED AND REPLACED BLEED PRESS REG VALVE CTRL SOLENOID (10HA2), DUE TO CLASS 3 FAULT
- [SDR AWXA200300939](https://openairdocs.org/sdr/AWXA200300939.md): Lanyard · torn · Aug 17, 2003 · N646AW · Airbus A320231 · Escape Slide
  > ON DECENT, EN ROUTE FROM PHX THE FLIGHT ATTENDANT REPORTED A LOUD SQUEAL COMING FROM THE L-2 DOOR. MAINTENANCE FOUND THE L-2 DOOR SLIDE LOWER LANYARD TORN AND IN THE DOOR SEAL, AIRCRAFT WAS MAINTENANCE FERRIED BACK TO PHX WHERE THE L-2 DOOR SLIDE WAS REMOVED A
- [SDR AWXA200300598](https://openairdocs.org/sdr/AWXA200300598.md): Terminal · broken · May 21, 2003 · N646AW · Airbus A320231 · Light System Wiring
  > DURING C-01 CHECK THE EMERGENCY EXIT LIGHT BETWEEN THE L/H OVER-WING HATCHES WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED A BROKEN EMERGENCY EXIT LIGHT TERMINAL LUG BETWEEN L/H OVER-WING EXITS IAW A320 ESPM 20-48-14, PG. 1-3, OPERATIONAL CHECK WAS GO
- [SDR AWXA200300601](https://openairdocs.org/sdr/AWXA200300601.md): Floor Panel · delaminated · May 19, 2003 · N646AW · Airbus A320231 · Fuselage Floor Panel
  > DURING C-01 CHECK CENTER WING FLOOR PANEL 241EF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 241EF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70057; INSTALLED REPAIR PART IAW AWA T/C R1C25306.
- [SDR AWXA200300600](https://openairdocs.org/sdr/AWXA200300600.md): Floor Panel · delaminated · May 19, 2003 · N646AW · Airbus A320231 · Fuselage Floor Panel
  > MCN - MAJOR REPAIR - DURING C-01 CHECK CABIN FLOOR PANEL 241FF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 241FF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70057; INSTALLED REPAIR PART IAW AWA T/C R1C25306.
- [SDR AWXA200300599](https://openairdocs.org/sdr/AWXA200300599.md): Floor Panel · delaminated · May 19, 2003 · N646AW · Airbus A320231 · Fuselage Floor Panel
  > MCN - MAJOR REPAIR - DURING C-01 CHECK CENTER WING FLOOR PANEL 242FF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 242FF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70055; INSTALLED REPAIR PART IAW AWA T/C R1C25306.
- [SDR AWXA200300571](https://openairdocs.org/sdr/AWXA200300571.md): Floor Panel · delaminated · May 19, 2003 · N646AW · Airbus A320231 · Fuselage Floor Panel
  > MCN - MAJOR REPAIR - DURING C-01 CHECK CABIN FLOOR PANEL 242GF WAS FOUND DELAMINATED. MAINTENANCE REMOVED CABIN FLOOR PANEL 242GF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D536-70055; INSTALLED NEW PANEL IAW AWA T/C R1C25306, AND A320 SRM 53-02-00, PG
- [SDR AWXA200300597](https://openairdocs.org/sdr/AWXA200300597.md): Terminal · broken · May 15, 2003 · N646AW · Airbus A320231 · Light System Wiring
  > DURING C-01 CHECK THE L-1 DOOR CLASS DIVIDER EMERGENCY EXIT LIGHT CONNECTOR WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR CLASS DIVIDER EMERGENCY EXIT LIGHT CONNECTOR IAW A320 ESPM 20-48-24, PG. 18, OPERATIONAL CHECK WAS GOOD IAW AMM SUBTASK
- [SDR AWXA200300570](https://openairdocs.org/sdr/AWXA200300570.md): Fitting · broken · May 15, 2003 · N646AW · Airbus A320231 · Escape Slide
  > MCN - EES - DURING C-01 CHECK THE LT OVERWING HATCH SLIDE BOTTLE CABLE FITTING WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING HATCH SLIDE BOTTLE IAW AMM SUBTASK 25-62-46-020-050-A, AND 25-62-46-420-050-A, OPERATIONAL CHECK WAS GOOD IAW AMM
- [SDR AWXA200300096](https://openairdocs.org/sdr/AWXA200300096.md): Pipe · leaking · Jan 30, 2003 · N646AW · Airbus A320231 · Hydraulic System, Main
  > LAS - EMERGENCY LANDING - EN ROUTE FROM DFW TO LAS ON DECENT THE GREEN HYDRAULIC SYSTEM FAILED. MAINTENANCE FOUND CHAFED HYDRAULIC RETURN LINE IN LT ENGINE PYLON, REPLACED HYDRAULIC LINE LT PYLON. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP DUE TO POSSIBLE CAVI
- [SDR AWXA200200842](https://openairdocs.org/sdr/AWXA200200842.md): Cable · broken · Aug 26, 2002 · N646AW · Airbus A320231 · Emergency Lighting
  > PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AND REPLACED CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 L/H, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200200675](https://openairdocs.org/sdr/AWXA200200675.md): Scavenge Pump · leaking · Jul 29, 2002 · N646AW · Airbus A320231 · Turbine Engine Oil System
  > PHX - FLT 0536 - WHILE AIRCRAFT WAS TAXIING TO GATE, THE AIRCRAFT TAXIING BEHIND REPORTED SEEING A TAILPIPE FIRE AT NR 1 ENGINE TAILPIPE. MAINTENANCE PERFORMED A HOT SECTION BORESCOPE PER T/C 15M72304, NO DEFECTS WERE NOTED. AS A PRECAUTION THE NR 1 ENGINE
- [SDR AWXA200200596](https://openairdocs.org/sdr/AWXA200200596.md): Engine · fire · Jul 9, 2002 · N646AW · Airbus A320231 · Engine (Turbine/Turboprop)
  > FLT 0279 - AFTER LANDING AT IAH INBOUND FROM PHX, AFTER ENGINE SHUTDOWN AT GATE, GROUND CREW OBSERVED FIRE IN THE TAILPIPE OF THE NR 1 ENGINE. FLIGHT CREW MOTORED ENGINE APPROXIMATELY 1 MINUTE BEFORE FLAME EXTINGUISHED, ESTIMATE TAILPIPE FIRE LASTED TOTAL OF 2
- [SDR AWXA200200178](https://openairdocs.org/sdr/AWXA200200178.md): Power Supply · discharged · Feb 24, 2002 · N646AW · Airbus A320231 · Emergency Lighting
  > YWG - EEL -C- DURING C-08 CHECK EMERGENCY ESCAPE PATH LIGHTING AT ROWS 13, 17, 19, 24 WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 13WL IAW AMM 33-51-38-401, OPERATIONAL CHECK PERFORMED IAW T/C F1C33301.
- [SDR AWXA200200129](https://openairdocs.org/sdr/AWXA200200129.md): Floor Support · corroded · Feb 12, 2002 · N646AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > YWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM Y1292 RT BETWEEN FR 66 AND FR 67. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 51-74-00, PG 1. REMOVED FLOOR SUPPORT BEAM Y1292 RT, FABRIC
- [SDR AWXA200200133](https://openairdocs.org/sdr/AWXA200200133.md): Seat Track · corroded · Feb 10, 2002 · N646AW · Airbus A320231 · Fuselage Main, Floor Beam
  > YWG - MAJOR REPAIR - "C" - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT SEAT TRACK Y254 L/H FR 20. MAINTENANCE REMOVED CORROSION FROM FLOOR SUPPORT SEAT TRACK AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 53-11-14. REMOVED FLOOR SUPPORT
- [SDR AWXA200200132](https://openairdocs.org/sdr/AWXA200200132.md): Seat Track · corroded · Feb 10, 2002 · N646AW · Airbus A320231 · Fuselage Main, Floor Beam
  > YWG - MAJOR REPAIR - "C" - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SEAT TRACK Y765 R/H FR 16. MAINTENANCE REMOVED FLOOR SEAT TRACK Y765 R/H, FABRICATED NEW FLOOR SEAT TRACK AND INSTALLED REPAIR IAW DWG 53112782.
- [SDR AWXA200200131](https://openairdocs.org/sdr/AWXA200200131.md): Floor Support · corroded · Feb 10, 2002 · N646AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > YWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT BEAM Y1292 RT BETWEEN FR 15 AND FR 19. MAINTENANCE REMOVED FLOOR SUPPORT BEAM Y1292 RT, FABRICATED NEW FLOOR SUPPORT BEAM AND INSTALLED REPAIR IAW DWG 53112782.
- [SDR AWXA200200130](https://openairdocs.org/sdr/AWXA200200130.md): Floor Support · corroded · Feb 10, 2002 · N646AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > YWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT BEAM Y254 LT BETWEEN FR 15 AND FR 21. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 53-11-14. REMOVED FLOOR SUPPORT BEAM Y254 LT, FABR
- [SDR AWXA200200181](https://openairdocs.org/sdr/AWXA200200181.md): Frame · damaged · Feb 8, 2002 · N646AW · Airbus A320231 · Fuselage Main, Frame
  > YWG - MAJOR REPAIR - C - DURING C-08 CHECK TOOLING HOLES AT FR 38-40 LT TO RT WERE FOUND TO BE OVERSIZED. COLD EXPANDED THE HOLES PER SRM 51-48-00, MAINTENANCE DRILLED HOLES TO APPLICABLE DIAMETER, COUNTERSUNK HOLES TO A MAXIMUM OF 0.4MM, INSTALLED FASTENERS
- [SDR AWXA2002TESTI](https://openairdocs.org/sdr/AWXA2002TESTI.md): Frame · cracked · Feb 2, 2002 · N646AW · Airbus A319132 · Fuselage Main, Structure
  > TEST
- [SDR AWXA2002TESTJ](https://openairdocs.org/sdr/AWXA2002TESTJ.md): Frame · cracked · Feb 2, 2002 · N646AW · Airbus A319132 · Fuselage Main, Structure
  > TEST
- [SDR AWXA2002TESTF](https://openairdocs.org/sdr/AWXA2002TESTF.md): Frame · cracked · Feb 2, 2002 · N646AW · Airbus A319132 · Fuselage Main, Structure
  > TEST
- [SDR AWXA2002TESTC](https://openairdocs.org/sdr/AWXA2002TESTC.md): Frame · cracked · Feb 2, 2002 · N646AW · Airbus A319132 · Fuselage Main, Structure
  > TEST
- [SDR AWXA200200145](https://openairdocs.org/sdr/AWXA200200145.md): Floor Support · corroded · Jan 25, 2002 · N646AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > YWG - MAJOR REPAIR - C - DURING C-08 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT Y1292 AT FR 66 RT. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT, FABRICATED NEW FLOOR SUPPORT AND INSTALLED REPAIR IAW DWG D53472090, AND SRM 51-42-11.
- [SDR AWXA200200167](https://openairdocs.org/sdr/AWXA200200167.md): Floor Support · corroded · Jan 25, 2002 · N646AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > YWG - MAJOR REPAIR - "C" - DURING C-08 CHECK CORROSION WAS FOUND AROUND SCREW HOLES ON FLOOR SUPPORT AT Y1162R, BETWEEN FR 68 & 69. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT Y1162R, BETWEEN FR 68 & 69; FABRICATED A NEW FLOOR SUPPORT AND INSTALLED REPAIRS I
- [SDR AWXA200200166](https://openairdocs.org/sdr/AWXA200200166.md): Floor Support · corroded · Jan 22, 2002 · N646AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > YWG - MAJOR REPAIR - "C" - DURING C-08 CHECK CORROSION WAS FOUND ON FORWARD AND AFT FLOOR SUPPORT IN FORWARD CABIN AT Y254, FR 15-19. MAINTENANCE CLEANED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER SRM 53-11-14; REMOVED CORRODED FLOOR SUPPORT; FABRICAT
- [SDR AWXA200200007](https://openairdocs.org/sdr/AWXA200200007.md): Battery · discharged · Jan 5, 2002 · N646AW · Airbus A320231 · Emergency Lighting
  > PHX - EEL - C - DURING INSPECTION ALL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. NOTE: AIRCRAFT HAS BEEN PARKED SINCE 30 NOVEMBER, 2001. MAINTENANCE REPLACED ALL FOUR EMERGENCY LIGHT BATTERY PACKS 10WL-13WL, ZONES 221, 241, 242, AND 263 IAW AMM 33-51-38,
- [SDR AWXA0001883](https://openairdocs.org/sdr/AWXA0001883.md): Warning System · false activation · Jun 19, 2001 · N646AW · Airbus A320231 · Door Warning System
  > PHX- AIR TURNBACK - FLT 752- AFTER TAKEOFF, ECAM MESSAGE AFT CARGO DOOR APPEARED AND THE AIRCRAFT WAS RETURNED TO PHX. IN PHX MAINTENANCE INSPECTED THE AFT CARGO DOOR TO ENSURE IT WAS FULLY CLOSED AND LOCKED, WHICH IT WAS. THE AFT CARGO DOOR INDICATION WAS P
- [SDR AWXA0001373](https://openairdocs.org/sdr/AWXA0001373.md): Fmc · failed · Feb 19, 2001 · N646AW · Airbus A320231 · Flight Management Computing Hardware System
  > PHX - DIVERTED FLIGHT - 2/14/01 - AFTER TAKEOFF FROM LAS TO BOS THE MCDU FROZE IN THE FLIGHT PLAN MODE; RNAV UNAVAILABLE; THE FLIGHT WAS DIVERTED TO PHX. IN PHX MAINTENANCE REPLACED THE LEFT AND RIGHT FMGC; AFTER REPLACEMENT, CURRENT NAV DATA WAS UPLOADED AND
- [SDR AWXA0001257](https://openairdocs.org/sdr/AWXA0001257.md): Actuator · leaking · Jan 26, 2001 · N646AW · Airbus A320231 · Drag Control Actuator
  > PHX- EMERGENCY LANDING, FLIGHT CREW HAD ECAM MESSAGE FOR YELLOW HYDRAULIC SYSTEM LOW LEVEL. AN UNEVENTFUL LANDING WAS MADE. IN PHX MAINTENANCE FOUND THE RT NR 2 SPOILER SERVO CONTROL LEAKING. THE SERVO CONTROL WAS REPLACED AND THE YELLOW HYDRAULIC SYSTEM SE
- [SDR AWXA0001019](https://openairdocs.org/sdr/AWXA0001019.md): Servo · malfunctioned · Dec 6, 2000 · N646AW · Airbus A320231 · Aileron Control System
  > PHX - AIR TURNBACK - ON CLIMB OUT AND CRUISE AIRCRAFT HAD LEFT WING DOWN 5 TO 7 DEGREES AND RUDDER TRIM 2.8 DEGREES RT. MOST NOTICABLE AT 250 KTS. AND ABOVE; AT 210 KTS. CONDITION LESS NOTICABLE AND AT 170 KTS. FLAP 2 RUDDER TRIM WAS NORMAL AND AIRCRAFT WAS ST
- [SDR AWXA0000091](https://openairdocs.org/sdr/AWXA0000091.md): Fire Detector · malfuntioned · Feb 20, 2000 · N646AW · Airbus A320231 · Fire Detection
  > NR 2 ENGINE FIRE LIGHT AND MASTER FIRE LIGHT INDICATED FIRE, NO ECAM, NO MASTER WARNING. ENGINE 2 SHUTDOWN IN-FLIGHT AND BOTH FIRE BOTTLES FIRED. REMOVED AND REPLACED NR 2 FIRE DETECT UNIT, OPS CK GOOD. TT 0003704 M+E = 26-2612-9-0001. REPLACED NR 1 AND 2
- [SDR AWXA9900353](https://openairdocs.org/sdr/AWXA9900353.md): Wire · broken · Oct 11, 1999 · N646AW · Airbus A320231 · Light System Wiring
  > SEAT 9 RT EMERGENCY EXIT LIGHT INOP. REPAIRED WIRING, OPS CK NML.
- [SDR AWXA9900345](https://openairdocs.org/sdr/AWXA9900345.md): Oil Cooler · leaking · Oct 6, 1999 · N646AW · Airbus A320231 · APU Oil System
  > DURING DESCENT WITH POWER AT IDLE, NOXIOUS ODORS EMANATED FROM THE LT PACK, CAPABLE OF EYE AND THROAT IRRITATION. ISOLATED TO LEAKING OIL COOLER. REMOVED AND REPLACED OIL COOLER AND OZONE FILTERS.
- [SDR AWXA9900343](https://openairdocs.org/sdr/AWXA9900343.md): Actuator · failed · Oct 6, 1999 · N646AW · Airbus A320231 · Compressor Bleed Control
  > EMERGENCY DECLARED (NOT BY PILOT) ENG NR 1 COMPRESSOR VANE FAULT ON DESCENT, NO OTHER ABNORMAL ENG INDICATIONS OR FAILURES. FIRST TIME FAULT FADEC CONFIRMS 2.5 BLEED ACTUATOR FAIL CURRENT HISTORY.
- [SDR AWXA9900298](https://openairdocs.org/sdr/AWXA9900298.md): B Nut · loose · Sep 6, 1999 · N646AW · Airbus A320231 · Hydraulic Accumulator, Auxiliary
  > AMBER ECAM MESSAGE, CLASS NR 1. YELLOW HYDRAULIC RESERVOIR LOW QUANTITY. FOUND 'B' NUT LOOSE ON YELLOW HYDRAULIC ACCUMULATOR. TIGHTENED NUT. SERVICED SYSTEM WITH APPROXIMATELY 4 GALLONS.
- [SDR AWXA9900243](https://openairdocs.org/sdr/AWXA9900243.md): Pack · malfunctioned · Jul 14, 1999 · N646AW · Airbus A320231 · Cabin Cooling System
  > NOTICEABLE OFFENSIVE ODOR FROM AIR CONDITIONING SYSTEM DURING CLIMB AND DESCENT. LT PACK PRODUCING SMELL. PLACED ON MEL 21-52-01.
- [SDR AWXA9900227](https://openairdocs.org/sdr/AWXA9900227.md): Coalescer · dirty · Jun 22, 1999 · N646AW · Airbus A320231 · Humidity Control System
  > ACRID SMELL AFTER TAKEOFF AND INCREASINGLY WORSE THROUGHOUT THE FLIGHT. SMELL INCREASED FROM SMELL ON GROUND. ACCOMPLISHED TSM 21-00-00-801-810 TO CHECK FOR OIL IN THE APU BLEED AIR SYSTEM, BOTH EXTERNALLY AND INTERNALLY. ALL DUCTING REINSTALLED AND BAY SEC
- [SDR AWXA9900225](https://openairdocs.org/sdr/AWXA9900225.md): Air Dist · odor · Jun 21, 1999 · N646AW · Airbus A320231 · Air Distribution System
  > STRONG OILY SMELL AFTER TAKEOFF, BELIEVE TO BE PACK SMELL. STILL COULD SMELL AT CRUISE. INSPECTED APU INLET FOR SIGNS OF OIL, NONE FOUND. RAN ENGINES ALTERNATING BLEEDS, SMELL STRONGEST WITH APU BLEED. INSTALLED MEL 49-10-01, CONTROL NR 106292. *S/D* APU

Next page: https://openairdocs.org/deregistered/N646AW-2006-05-10/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 = 'N646AW' AND deregistration_id = 'N646AW-2006-05-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N646AW-2006-05-10/reports

---
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.