# Service difficulty reports: N635AW, cancelled May 19, 2003

A list on [N635AW, cancelled May 19, 2003](https://openairdocs.org/deregistered/N635AW-2003-05-19.md).

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

- [SDR AWXA200200849](https://openairdocs.org/sdr/AWXA200200849.md): Landing Gear · collapsed · Aug 28, 2002 · N635AW · Airbus A320231 · Nose/Tail Landing Gear
  > PHX - LANDING GEAR - FLT 0794 - AFTER LANDING AT PHX EN ROUTE FROM IAH AT LATER STAGE OF LANDING ROLL; THE NOSE LANDING GEAR COLLAPSED CAUSING SEVERE DAMAGE TO AIRFRAME, ENGINES, AND NOSE LANDING GEAR.
- [SDR AWXA200200718](https://openairdocs.org/sdr/AWXA200200718.md): Engine · malfunctioned · Aug 11, 2002 · N635AW · Airbus A320231 · Engine Temperature Indicating System
  > ON TAKEOFF FROM FLL EN ROUTE FOR PHX NR 1 ENGINE HAD LOW EPR, EPR AT 1.32 CHARTED EPR WAS 1.40, ABORTED TAKEOFF. CONTRACT MAINTENANCE AT FLL PERFORMED TEST OF BOTH ENGINES, TESTS WERE NORMAL. PLACED NR 1 ENGINE ON MEL 73-20-04, COND. 1, EPR MODE INOP. MAINTENA
- [SDR AWXA200200307](https://openairdocs.org/sdr/AWXA200200307.md): Sensor · failed · Apr 6, 2002 · N635AW · Airbus A320231 · Hydraulic Quantity Sensor
  > EN ROUTE FROM PHX A WARNING FOR GREEN HYD SYS LOW LEVEL APPEARED ON ECAM. FLT CREW REQUESTED EMERGENCY EQUIP STANDBY AT LANDING, ACFT LANDED WITHOUT EVENT. MX REPLACED THE GREEN HYD SYS LOW LEVEL SENSOR. REPLACED WAS THE GREEN HYD SYS DRAIN VALVE, AND THE Q
- [SDR AWXA200100522](https://openairdocs.org/sdr/AWXA200100522.md): Pump · overheated · Oct 9, 2001 · N635AW · Airbus A320231 · Hydraulic Pump (Electric/Engine), Main
  > PHX - AIR TURNBACK - FLT 794 - C - ON CLIMBOUT THE CREW GOT ECAM MESSAGE FOR BLUE HYD SYS ELECTRIC PUMP OVERHEAT. THE CREW FOLLOWED ECAM PROCEDURES AND RETURNED TO PHX. THE ECAM MESSAGE WAS DISPLAYED ENTIRE FLIGHT. MAINTENANCE TROUBLESHOT AND REPLACED THE B
- [SDR AWXA200100514](https://openairdocs.org/sdr/AWXA200100514.md): Seat Track · corroded · Sep 25, 2001 · N635AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > YWG - C1 CK -NR 4 SEAT TRACK CORRODED AT FR 20R, Y-1292. BEYOND LIMITS AFTER CORROSION REMOVAL. MAINTENANCE REMOVED DAMAGED SECTION OF TRACK, FABRICATED REPAIR SECTION AND SPLICES AND INSTALLED REPAIR PARTS IAW SRM 53-00-15, FIG 201.
- [SDR AWXA200100513](https://openairdocs.org/sdr/AWXA200100513.md): Seat Track · corroded · Sep 25, 2001 · N635AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > YWG - C1 CK -NR 3 SEAT TRACK AT FR 20R, Y-765, CORRODED. BEYOND SRM LIMITS AFTER CORROSION REMOVAL. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED REPAIR SECTION AND SPLICES AND INSTALLED REPAIR IAW SRM 53-00-15, FIG 201.
- [SDR AWXA0000445](https://openairdocs.org/sdr/AWXA0000445.md): Seat Track · corroded · Jul 7, 2000 · N635AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN SEAT TRACK CORRODED AT FRAME 20 Y 1292. REPLACED SEAT TRACK IAW D531128152, REMOVED CORROSION IAW A319 SRM 51-74-00, REPAIRED IAW A319 SRM 53-00-14.
- [SDR AWXA0000331](https://openairdocs.org/sdr/AWXA0000331.md): Solenoid Valve · leaking · May 24, 2000 · N635AW · Airbus A320231 · Hydraulic System, Main
  > EMERGENCY LANDING, GREEN HYDRAULIC SYSTEM LOW PRESSURE. FOUND LEAK AT PTU SOLENOID VALVE. REPLACED BOBBINS AND SEALS ON SOLENOID VALVE, LK AND OPS CHK GOOD. RECOMMENDATION: MONITOR.
- [SDR AWXA0000209](https://openairdocs.org/sdr/AWXA0000209.md): Sensor · failed · Apr 1, 2000 · N635AW · Airbus A320231 · Fuel Control/Turbine Engines
  > NR 1 ENG SENSOR FAULT AVOID RAPID THROTTLE CHANGE. REMOVED AND REPLACED NR 1 ENG EEC TT 00409972 M+E 26-7320-9-0016 CURRENT HISTORY NOT AVAILABLE COMPUTER DOWN. REMAIN OPEN PENDING REVIEW OF TEARDOWN REPORT.
- [SDR AWXA0000105](https://openairdocs.org/sdr/AWXA0000105.md): Actuator · failed · Feb 29, 2000 · N635AW · Airbus A320231 · Compressor Bleed Control
  > LP 7624668, ENGINE 2 COMPRESSOR STALL OCCURRED TWICE DURING TRANSITION FROM FLEX TO CLIMB. REPLACED E2 VSV ACTUATOR IAW AWA TASK CARD R5M75303. OPS CHECK OK.
- [SDR AWXA9900465](https://openairdocs.org/sdr/AWXA9900465.md): Wire · broken · Dec 9, 1999 · N635AW · Airbus A320231 · Light System Wiring
  > EMERGENCY EXIT LT OUT, AT AFT MOST LT SEAT ROW. REPAIRED BROKEN WIRE AT AFT SEAT.
- [SDR AWXA9900361](https://openairdocs.org/sdr/AWXA9900361.md): Seat Track · corroded · Oct 4, 1999 · N635AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > C-CHECK, FLOORBEAM TRACK Y 1292 RT CORRODED FR 16 TO FR 20. REPLACED SECTION OF TRACK NR D 53112782200 AS PER SRM 51-72-00 PG 1 AND SRM 53-11-15 PG 213, TREATED, PRIMED AND PAINTED AS PER 51-21-00.
- [SDR AWXA9900360](https://openairdocs.org/sdr/AWXA9900360.md): Floorbeam · corroded · Oct 4, 1999 · N635AW · Airbus A320231 · Fuselage Main, Floor Beam
  > C-CHECK, STA 8433 FLOORBEAM CORRODED, 12 INCHES LEFT OF CENTER FR 21. REPLACED SECTION OF H-ANGLE FLOORBEAM NR D53112818200 AS PER SRM 51-72-00 PG 1. TREATED, PRIMED AND PAINTED AS PER SRM 51-21-00.
- [SDR AWXA9900359](https://openairdocs.org/sdr/AWXA9900359.md): Floorbeam · corroded · Oct 4, 1999 · N635AW · Airbus A320231 · Fuselage Main, Floor Beam
  > C-CHECK, FLOORBEAM BETWEEN STA 7087 & 8077, SIX INCHES RIGHT OF CENTER LINE HAS EVIDENCE OF CORROSION ON TOP SURFACE (FR 16 TO FR 20). REMOVED EXISTING FILLER PLATE, FABRICATED NEW FILLER OF.080 2024T3--MATERIAL, TREATED, PRIMED, PAINTED AND INSTALLED FILLER
- [SDR AWXA9900358](https://openairdocs.org/sdr/AWXA9900358.md): Seat Track · corroded · Oct 4, 1999 · N635AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > C-CHECK, FLOOR TRACK AT 765 RT CORRODED FR 20. REPLACED SECTION OF TRACK AS PER SRM 51-77-00 PG 1 AND SRM 53-11-15 PG 213, TREATED, PRIMED AND PAINTED AS PER SRM 51-21-00.
- [SDR AWXA9900295](https://openairdocs.org/sdr/AWXA9900295.md): Battery Pack · discharged · Sep 2, 1999 · N635AW · Airbus A320231 · Emergency Lighting
  > OVERWING EMER EXIT LIGHTS FLICKERING IN FLIGHT--BATT PACK FAILED TEST. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD.
- [SDR AWXA9900263](https://openairdocs.org/sdr/AWXA9900263.md): Apu · failed · Aug 16, 1999 · N635AW · Airbus A320231 · APU Core Engine
  > OIL SMELL IN CABIN VENTS. REPLACED AUX POWER UNIT.
- [SDR AWXA9900177](https://openairdocs.org/sdr/AWXA9900177.md): Bolt · failed · May 6, 1999 · N635AW · Airbus A320231 · Landing Gear Door Actuator
  > AIR TURNBACK DUE TO LT NLG DOOR NOT RETRACTING. CREW SELECTED GEAR DOWN, THEN FELT VIBRATION IN NLG AREA. CREW RETURNED TO PHL (SINK RATE GOOD -- NO OVERWEIGHT LANDING). MAINTENANCE FOUND THE ATTACH BOLT FOR NLG DOOR ACTUATING CYLINDER BROKEN AND FOUND A BU
- [SDR AWXA9800195](https://openairdocs.org/sdr/AWXA9800195.md): Power Supply · inoperative · Aug 20, 1998 · N635AW · Airbus A320231 · Emergency Lighting
  > DURING ROUTINE WEEKLY MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS FAILED ON RIGHT SIDE OF AIRCRAFT. FOUND BATTERY FAILED AND CHARGER INOP. REMOVED AND REPLACED BATTERY AND CHARGER, BATTERY ASSEMBLY - 321430.
- [SDR AWXA9800014](https://openairdocs.org/sdr/AWXA9800014.md): Battery · discharged · Jan 11, 1998 · N635AW · Airbus A320231 · Emergency Lighting
  > EMERGENCY LIGHTS OVER R2 AND L2 AFT CENTER AISILE INOP. REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD.
- [SDR AWXA9800002](https://openairdocs.org/sdr/AWXA9800002.md): O-Ring · leaking · Jan 4, 1998 · N635AW · Airbus A320231 · Hydraulic System, Main
  > ECAM MESSAGE IN CRUISE, GREEN SYSTEM LOW QUANTITY FOUND GREEN SYSTEM PTU MANIFOLD LEAKING FLUID AT PRIORITY VALVE MATING SURFACE. REMOVED PRIORITY VALVE FROM MANIFOLD AND REPLACED O-RINGS AND SQUARE SECTION SEALS ON BOBBINS AND REINSTALLED PER M/M 29-11-33.
- [SDR AWXA9700411](https://openairdocs.org/sdr/AWXA9700411.md): Skin · corroded · Jul 20, 1997 · N635AW · Airbus A320231 · Fuselage Main, Plate/Skin
  > DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION AT TOILET TANK EXHAUST PORT ON RT SIDE OR AIRCRAFT SKIN. REPAIRED PER EO 53-35-06 AND EVA 002036.
- [SDR AWXA9700307](https://openairdocs.org/sdr/AWXA9700307.md): Battery · discharged · May 23, 1997 · N635AW · Airbus A320231 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT FWD ENTRY AND SERVICE DOORS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY, OPS CHECK GOOD.
- [SDR AWXA960492](https://openairdocs.org/sdr/AWXA960492.md): Connector · disconnected · Jul 30, 1996 · N635AW · Airbus A320231 · Emergency Lighting
  > LAS - FLT 2990 - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROX LIGHTING INOPERATIVE AT 9R. RECONNECTED CANNON PLUG AT SIDE WALL. (X)
- [SDR AWXA960339](https://openairdocs.org/sdr/AWXA960339.md): Slat Lock · failed · Jul 12, 1996 · N635AW · Airbus A320231 · Leading Edge Slat Control System
  > RNO - LAS - EMERGENCY DECLARED, SLAT LOCK FAULT SHORTLY AFTER TAKEOFF FROM PHX. COMPLIED WITH CIRCUIT BREAKER RESET CFDS, SFCC, 1 AND 2 TEST, WING TIP BRAKE RESET WITH NO FAULTS FOUND AND NORMAL OPS CHECK OF FLAP/SLATS SYSTEM. (M)
- [SDR AWXA960289](https://openairdocs.org/sdr/AWXA960289.md): Eec · failed · Jun 24, 1996 · N635AW · Airbus A320231 · Fuel Control/Turbine Engines
  > PHX/ORD - FLT 0004 - ABORTED TAKEOFF. NR 1 ENGINE DID NOT MAKE TAKEOFF POWER. REPLACED NR 1 ENGINE EEC PER R9373301. OPERATIONS CHECK GOOD. PART TOTAL CYCLES, 5,817. (X)
- [SDR AWXA960059](https://openairdocs.org/sdr/AWXA960059.md): Connector · loose · Feb 9, 1996 · N635AW · Airbus A320231 · Power Indicating System
  > PAE-SEA - FLT NR 3851 - AIR TURN BACK, AFTER TAKEOFF, FMGC INDICATION ENGINE 1 EPR FAULT. AIRCRAFT RETURNED TO PAE LANDING UNEVENTFUL. FOUND NR 1 ENGINE COWL CONNECTOR 8DOVC LOOSE, SEATED CONNECTOR FULLY. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR AWXA960045](https://openairdocs.org/sdr/AWXA960045.md): Seat Track · corroded · Feb 3, 1996 · N635AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > PAE - FLT 3851 - DURING SCHEDULED C-4 MAINTENANCE CHECK, FOUND CORROSION AT SEAT TRACK BS 8077, IFR 20Y - 1292 - 2489. SPLICED REPAIR PER SRM 53-11-15. AIRCRAFT TT, 15,138 HOURS. AIRCRAFT TC, 7,863. (X)
- [SDR AWXA960044](https://openairdocs.org/sdr/AWXA960044.md): Seat Track · corroded · Feb 3, 1996 · N635AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > PAE - FLT 3851 - DURING SCHEDULED C-4 MAINTENANCE CHECK, FOUND CORROSION ON TOP SURFACE OF RAIL STA 6877 TO STA 7177 Y+500-2240. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-14, FIGURE 204. AIRCRAFT TT, 15,138 HOURS. AIRCRAFT TC, 7,863. (X)
- [SDR AWXA950043](https://openairdocs.org/sdr/AWXA950043.md): Seat Track · corroded · Feb 3, 1996 · N635AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > PAE - FLT 3851 - DURING SCHEDULED C-4 MAINTENANCE CHECK, FOUND SPOT CORROSION AT SEAT TRACK BS 8077, IFR 20 Y-765. FABRICATED AND REPAIRED PER SRM 53-11-15. AIRCRAFT TT, 15,138 HOURS. AIRCRAFT TC, 7,863. (X)
- [SDR AWXA9500731](https://openairdocs.org/sdr/AWXA9500731.md): Ttl Temp Sensor · failed · Nov 1, 1995 · N635AW · Airbus A320231 · Outside Air Temperature Indicator/Sensor
  > LAS - FLT NR 495 - PHX-DEN - DURING CRUISE, NAV ADRI CLASS 1 MESSAGE ILLUMINATED FOLLOWED BY NUMEROUS ADDITIONAL CLASS 1 AND 2 MESSAGES. AIRCRAFT DIVERTED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TAT 1 PROBE FAILED. REMOVED AND REPLACED PROBE.
- [SDR AWXA9500466](https://openairdocs.org/sdr/AWXA9500466.md): Prox Sensor · failed · Jul 26, 1995 · N635AW · Airbus A320231 · Landing Gear Position and Warning
  > PHX-SEA - FLT 840 - DURING TAKEOFF, THE NOSE GEAR DOORS DID NOT COME UP. GEAR WAS CYCLED AND APPEARED UP AND LOCKED. AFTER GEAR AND DOORS WERE UP AND LOCKED, LANDING GEAR DISAGREE AND LANDING CONTROL ECAM MESSAGE APPEARED. FWD PANEL HAD RED CENTER, UNSAFE T

## 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 = 'N635AW' AND deregistration_id = 'N635AW-2003-05-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N635AW-2003-05-19/reports

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