# Service difficulty reports: N645AW, cancelled May 10, 2006

A list on [N645AW, cancelled May 10, 2006](https://openairdocs.org/deregistered/N645AW-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 · 51 reports

- [SDR AWXA200501150](https://openairdocs.org/sdr/AWXA200501150.md): Circuit Board · false indication · Sep 29, 2005 · N645AW · Airbus A320231 · Landing Gear Position and Warning
  > LAS - EMERGENCY LANDING - FLT 176 - DURING GEAR EXTENSION RECEIVED NOSE LANDING GEAR LIGHT ON UPPER PANEL, ALL OTHER INDICATIONS WERE NORMAL. CREW PERFORMED FLY BY TO VERIFY GEAR STATUS. AIRCRAFT LANDED IN LAS WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE.
- [SDR AWXA200501012](https://openairdocs.org/sdr/AWXA200501012.md): Seat Track · corroded · Aug 15, 2005 · N645AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > SAL - MAJOR REPAIR - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE RT INBOARD SIDE AT FR 20+10" Y-765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 20+10" Y-765 A
- [SDR AWXA200501011](https://openairdocs.org/sdr/AWXA200501011.md): Fitting · corroded · Aug 15, 2005 · N645AW · Airbus A320231 · Fuselage Main, Attach Fittings
  > SAL - MAJOR REPAIR - CORROSION FOUND ON C3 CHECK LOCATED AROUND FITTING AT THE LOWER SILL OF THE FORWARD CARGO DOOR CUTOUT. NO ALLOWABLE DAMAGE LIMITS FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED AND REPLACED THE FITTING LOCATED ON THE LOWER SILL OF FORW
- [SDR AWXA200501010](https://openairdocs.org/sdr/AWXA200501010.md): Seat Track · corroded · Aug 15, 2005 · N645AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > SAL - MAJOR REPAIR - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE RT INBOARD SIDE AT FR 36" Y-765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 36" Y-765 AND IN
- [SDR AWXA200501005](https://openairdocs.org/sdr/AWXA200501005.md): Seat Track · corroded · Aug 15, 2005 · N645AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE RT OUTBOARD SIDE AT FR 39 +3" Y-1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 39 +3" Y-1292 AND INSTALLE
- [SDR AWXA200501004](https://openairdocs.org/sdr/AWXA200501004.md): Seat Track · corroded · Aug 15, 2005 · N645AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE LT INBOARD SIDE AT FR 39 +10" Y765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 39 +10" Y765 AND INSTALLED N
- [SDR AWXA200501003](https://openairdocs.org/sdr/AWXA200501003.md): Seat Track · corroded · Aug 15, 2005 · N645AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE LT OUTBOARD SIDE AT FS 42 +16" Y1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FS 42 +16" Y1292 AND INSTALLE
- [SDR AWXA200501002](https://openairdocs.org/sdr/AWXA200501002.md): Seat Track · corroded · Aug 15, 2005 · N645AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE LT OUTBOARD SIDE AT FS 36 +16" Y1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 36 +16" Y1292 AND INSTALLE
- [SDR AWXA200501001](https://openairdocs.org/sdr/AWXA200501001.md): Seat Track · corroded · Aug 15, 2005 · N645AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED AT LT INBOARD SIDE AT FR 44+7, Y765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 44+7, Y765 AND INSTALLED NEW SEAT
- [SDR AWXA200501000](https://openairdocs.org/sdr/AWXA200501000.md): Seat Track · corroded · Aug 15, 2005 · N645AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > SAL - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED AT RT INBOARD SIDE AT FR 42+17, -Y765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 42+17, -Y765 AND INSTALLED NEW SE
- [SDR AWXA200500999](https://openairdocs.org/sdr/AWXA200500999.md): Seat Track · corroded · Aug 15, 2005 · N645AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED AT RT OUTBOARD SIDE AT FR 42+17, -Y1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 42+17, -Y1292 AND INSTALLED NE
- [SDR AWXA200401002](https://openairdocs.org/sdr/AWXA200401002.md): Wire · open · Sep 10, 2004 · N645AW · Airbus A320231 · Equipment/Furnishings Wiring
  > FLIGHT CREW REPORTED EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1, 2, AND 5 REMAIN ON AND WILL NOT RESET. MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), PROBLEM STILL EXISTS, OHMED L-1 DOOR SLIDE WIRING AND FOUND OPEN READING.
- [SDR AWXA200400578](https://openairdocs.org/sdr/AWXA200400578.md): Wire · chafed · May 27, 2004 · N645AW · Airbus A320231 · Engine Control System Wiring
  > ON CLIMBOUT, RECEIVED ECAM INDICATION NR 2 ENG NACELLE TEMP VARIES BETWEEN 315 & 380 DEGREES, INDICATION INTERMITTENT, DIVERTED TO PHX FOR REPAIR. MX TROUBLESHOT WIRING FROM PIN A/10B OF ENGINE INTERFACE UNIT (EIU) TO PIN 1 OF NACELLE TEMP SENSOR, NO FAULTS W
- [SDR AWXA200400507](https://openairdocs.org/sdr/AWXA200400507.md): Terminal · defective · May 12, 2004 · N645AW · Airbus A320231 · Light System Wiring
  > PHX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT INOPERATIVE. MAINTENANCE REPLACED DEFECTIVE TERMINALS AT EMERGENCY ESCAPE PATH LIGHT ASSEMBLY SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400134](https://openairdocs.org/sdr/AWXA200400134.md): Wire · broken · Feb 1, 2004 · N645AW · Airbus A320231 · Light System Wiring
  > DURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT, OPERATIONAL TEST WAS GOOD.
- [SDR AWXA200400025](https://openairdocs.org/sdr/AWXA200400025.md): Light · broken · Jan 9, 2004 · N645AW · Airbus A320231 · Emergency Lighting
  > PHX - EEL - FLIGHT CREW REPORTED EMERGENCY ESCAPE PATH FIXTURE AT FORWARD BULKHEAD WAS BROKEN. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT FORWARD BULKHEAD, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400022](https://openairdocs.org/sdr/AWXA200400022.md): Epsu · defective · Jan 4, 2004 · N645AW · Airbus A320231 · Emergency Lighting
  > MCN - EEL - DURING C-02 CHECK FOUND EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1, 2, & 4 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (10WL) ABOVE THE L-1 DOOR, OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM WAS GOOD.
- [SDR AWXA200400006](https://openairdocs.org/sdr/AWXA200400006.md): Rib · cracked · Dec 24, 2003 · N645AW · Airbus A320231 · Nacelle/Pylon, Frame/Spar/Rib
  > MCN - MINOR REPAIR - DURING C-02 CHECK A 1.25 INCH CRACK WAS FOUND ON NR 2 PYLON AFT FIXED FAIRING (RIB 12) AT OUTBOARD ANGLE. MAINTENANCE REMOVED CRACKED RIB AT NR 2 PYLON AFT FIXED FAIRING; FABRICATED A NEW REPLACEMENT RIB; INSTALLED REPAIR PART IAW A320 SR
- [SDR AWXA200400007](https://openairdocs.org/sdr/AWXA200400007.md): Skin · eroded · Dec 22, 2003 · N645AW · Airbus A320231 · Nacelle/Pylon, Plate/Skin
  > MCN - MINOR REPAIR - DURING C-02 CHECK THE NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN WAS FOUND ERODED. MAINTENANCE REMOVED ERODED NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICATED A NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 8-1
- [SDR AWXA200301197](https://openairdocs.org/sdr/AWXA200301197.md): Smoke · detected · Oct 9, 2003 · N645AW · Airbus A320231 · Air Distribution System
  > EN ROUTE FROM PHX TO ATL THE FLIGHT ATTENDANT REPORTED A STRONG BURNING ODOR AND ANOTHER FLIGHT ATTENDANT SAID SHE SAW SMOKE AT SEAT ROWS 9 AND 10 RT SIDE. ODOR DISSIPATED AFTER 1 TO 2 MINUTES. MAINTENANCE INSPECTED THE FORWARD GALLEY OVENS, PASSENGER CALL A
- [SDR AWXA200301122](https://openairdocs.org/sdr/AWXA200301122.md): Coffeemaker · malfunctioned · Oct 2, 2003 · N645AW · Airbus A320231 · Buffet/Galleys
  > EN ROUTE, REPORTED STRONG ELECTRICAL BURNING ODOR IN CABIN & COCKPIT. MX INSPECTED WIRING IN MAIN FWD GALLEY AREA BEHIND C/B PANEL, NR 1 & 2 OVENS, COFFEEMAKERS, NO SIGNS OF CHAFING OR BURNING. FOUND BURNT FOOD IN OVENS, DISCOVERED NR 1 COFFEEMAKER BASE UNIT
- [SDR AWXA200300805](https://openairdocs.org/sdr/AWXA200300805.md): Eec · failed · Jul 16, 2003 · N645AW · Airbus A320231 · Fuel Controlling System
  > DURING TAKEOFF AT PHX EN ROUTE FOR DEN THE CREW PUSHED POWER UP FOR TAKEOFF AND THE NR 2 ENGINE DID NOT RESPOND, POWER REMAINED AT IDLE, REJECTED TAKEOFF. FLIGHT CREW NOTED THAT THE NR 1 ENGINE DID RESPOND NORMALLY. APPROXIMATELY 5 MINUTES LATER; RECEIVED EC
- [SDR AWXA200300736](https://openairdocs.org/sdr/AWXA200300736.md): Actuator · faulty · Jun 25, 2003 · N645AW · Airbus A320231 · Compressor Bleed Control
  > AT CRUISE FL 360, NR 2 ENG COMPRESSOR VANE ECAM MSG, AT FL 290 NR 2 ENG STALLED. SHUTDOWN ENG, EMERGENCY EQUIP TO STANDBY. LANDED, TAXIED TO GATE. REPORT INDICATED NR 2 ENG OVERTEMP 663'C APPX 7 SEC. MX INSPECTED INTERMEDIATE PRESSURE CHECK VALVE, FAULT IS
- [SDR AWXA200300370](https://openairdocs.org/sdr/AWXA200300370.md): Engine · malfunctioned · Apr 14, 2003 · N645AW · Airbus A320231 · Engine (Turbine/Turboprop)
  > DURING TOGA POWER APPLICATION NR 2 ENGINE SPOOLED UP SLOWER THAN NR 1 ENGINE CAUSING AN ISSUE ON WET RUNWAY, REJECTED TAKEOFF APPROX 15 KTS. INITIAL SPOOL DIFFERENCE WAS ATTRIBUTED TO ENGINES NOT BEING EXACTLY MATCHED AT 1.05 EPR. ON 2ND ATTEMPT ENGINES MATC
- [SDR AWXA200201014](https://openairdocs.org/sdr/AWXA200201014.md): Cylinder · leaking · Oct 14, 2002 · N645AW · Airbus A320231 · Passenger/Crew Doors
  > DURING C-01 CHECK THE R-2 DOOR WAS FOUND TO HAVE NO DAMPING ACTION WHEN CLOSING DUE TO INTERNAL LEAKAGE. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR DAMPING AND EMERGENCY CYLINDER IAW AMM TASK 52-13-14-000-001 AND TASK 52-13-14-400-001, FUNCTIONAL CHECK WAS
- [SDR AWXA200200999](https://openairdocs.org/sdr/AWXA200200999.md): Fitting · cracked · Oct 4, 2002 · N645AW · Airbus A320231 · Landing Gear Doors
  > MCN - MAJOR REPAIR - DURING C-01 CHECK A 1 1/2" CRACK WAS FOUND ON THE R/H MAIN LANDING GEAR DOOR FORWARD HINGE FITTING. MAINTENANCE REMOVED DAMAGED R/H MAIN LANDING GEAR DOOR FORWARD HINGE FITTING, FABRICATED A NEW REPLACEMENT FITTING, AND INSTALLED REPAIR PA
- [SDR AWXA200200883](https://openairdocs.org/sdr/AWXA200200883.md): Skin · corroded · Sep 12, 2002 · N645AW · Airbus A320231 · Fuselage Main, Plate/Skin
  > PHX - MAJOR REPAIR - DURING INSPECTION THE FUSELAGE SKIN WAS FOUND CORRODED BENEATH AFT AIRPHONE ANTENNA. MAINTENANCE REMOVED CORRODED SECTION OF SKIN FR 63, FABRICATED A DOUBLER, AND INSTALLED REPAIR IAW SRM 53-00-11 FIG 203. BLANKING PLATE INSTALLED IAW AW
- [SDR AWXA200200785](https://openairdocs.org/sdr/AWXA200200785.md): Flashlight · inoperative · Aug 21, 2002 · N645AW · Airbus A320231 · Emergency Equipment
  > SAN - EMERGENCY EQUIPMENT - DURING INSPECTION THE AFT FLIGHT ATTENDANTS FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT FLIGHT ATTENDANTS FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200100517](https://openairdocs.org/sdr/AWXA200100517.md): Valve · leaking · Oct 6, 2001 · N645AW · Airbus A320231 · Main Landing Gear Strut/Axle/Truck
  > PHX - AIR TURNBACK - FLT 27 - AFTER T/O THE LANDING GEAR WOULD NOT RETRACT. CREW RESET LGCIU 1 & 2 PER MAINTENANCE CONTROL, NO HELP. THE AIRCRAFT APPEARED TO REMAIN IN GROUND MODE. THE AIRCRAFT RETURNED TO PHX, MAKING AN UNEVENTFUL LANDING. MAINTENANCE TROUBLE
- [SDR AWXA0001953](https://openairdocs.org/sdr/AWXA0001953.md): Floor Support · corroded · Jul 9, 2001 · N645AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > AFT CABIN FLOOR PANEL SUPPORT AT Y-1732R/H FR 66 SCREWS HOLES CORRODED. REMOVED CORROSION, MATERIAL REMOVED.100 (BEYOND LIMITS AS PER A320 SRM 51-72-11 PG 1). REPLACED BEAM AS PER A320 SRM 51-42-11 PAR 6.
- [SDR AWXA0001999](https://openairdocs.org/sdr/AWXA0001999.md): Floorbeam · corroded · Jul 7, 2001 · N645AW · Airbus A320231 · Fuselage Main, Floor Beam
  > AFT CABIN FLOOR PANEL SUPPORT AT Y-1732 RT FR 66 SCREW HOLES CORRODED. REMOVED CORROSION, MATERIAL REMOVED.100 INCH (BEYOND LIMITS AS PER SRM 51-72-11 PG 1). REPLACED BEAM AS PER A320 SRM 51-42-11 PAR 6.
- [SDR AWXA0001998](https://openairdocs.org/sdr/AWXA0001998.md): Floor Support · corroded · Jul 7, 2001 · N645AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > AFT CABIN FLOOR PANEL SUPPORT AT Y-765 LT FR 66 TO FR68 SCEW HOLES CORRODED. REMOVED CORROSION, MATERIAL REMOVED.035 INCH (BEYOND LIMITS AS PER A320 SRM 53-41-14). REPLACED BEAM AS PER A320 SRM 51-42-11 PG 1.
- [SDR AWXA0001997](https://openairdocs.org/sdr/AWXA0001997.md): Floor Support · corroded · Jun 29, 2001 · N645AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > FWD GALLEY FLOOR SUPPORT AT Y-81 FR 14R, 15R AND 16R CORRODED. FWD GALLEY FLOOR SUPPORT AT Y-81 FR12R-16R REPLACED AS PER A320 SRM 53-11-15 FIG 203.
- [SDR AWXA0001996](https://openairdocs.org/sdr/AWXA0001996.md): Floor Support · corroded · Jun 29, 2001 · N645AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > AFT CABIN FLOOR SUPPORT AT Y1162 FR 66R AND 69R SCREW CLIP ATTACH HOLE CORRODED. AFT GALLEY FLOOR SUPPORT AT Y1162 FR66R-69R REPLACED AS PER A320 SRM 51-42-11 PAGE 1.
- [SDR AWXA0001995](https://openairdocs.org/sdr/AWXA0001995.md): Seat Track · corroded · Jun 29, 2001 · N645AW · Airbus A320231 · Fuselage Floor Panel
  > D: Fwd galley floor support at Y1292 Fr 14R and 16R corrodedC: Fwd galley support/seat track at Y1292 FR12R-16R replaced as per A320 SRM 53-11-15 fig. 203
- [SDR AWXA0001994](https://openairdocs.org/sdr/AWXA0001994.md): Stringer · misdrilled · Jun 29, 2001 · N645AW · Airbus A320231 · Fuselage Main, Longeron/Stringer
  > D: Fr 66 L/H STR 43 has double drilled holesC: Stringer repaired as per SRM 53-00-13 Fig. 201 from sta.3152 to 3167
- [SDR AWXA0001993](https://openairdocs.org/sdr/AWXA0001993.md): Floor Support · damaged · Jun 29, 2001 · N645AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > AFT CABIN FLOOR SUPPORT AT Y1292 RT FR 68 SCREW HOLES DAMAGED. REPLACED FLOOR SUPPORT PER SRM 53-41-11.
- [SDR AWXA0001374](https://openairdocs.org/sdr/AWXA0001374.md): Actuator · contaminated · Feb 19, 2001 · N645AW · Airbus A320231 · Leading Edge Slat Actuator
  > PHX - EMERGENCY LANDING - 2/12/01 - ON APPROACH, THE CREW GOT AN ECAM WARNING, F/CTL SLATS FAULT AND THE CREW DECLARED AN EMERGENCY; AN UNEVENTFUL LANDING WAS MADE IN PHX. MAINTENANCE TROUBLESHOT AND FOUND 1 LT AND 2 RT LEADING EDGE SLAT ROTARY ACTUATORS WITH
- [SDR AWXA0001282](https://openairdocs.org/sdr/AWXA0001282.md): Resolver · malfunctioned · Feb 8, 2001 · N645AW · Airbus A320231 · Fuel Control/Turbine Engines
  > MAINTENANCE TROUBLESHOT IAW TSR 73-22-00-810-851 AND IAE TELEX; CELL CODE FAULT OF 59 ON FMU/HC/EEC 1 MESSAGE; (WFXCF) FUEL FLOW RESOLVER FAULT; CH B ON CONNECTOR J8 HAD HIGH RESISTANCE OF 104 OHMS BETWEEN PINS I & J (NORM: 15-78 OHMS); WIRING CHECKED GOOD; RA
- [SDR AWXA0001281](https://openairdocs.org/sdr/AWXA0001281.md): Fmu · malfunctioned · Feb 8, 2001 · N645AW · Airbus A320231 · Fuel Control/Turbine Engines
  > PHX - AIR TURNBACK - 2/3/01 - DURING INITIAL CLIMB, LEFT ENG UNCOMMANDED THRUST INCREASE ABOVE CLIMB EPR LIMIT WITH DEFINITE YAW TO THE RIGHT; EVENT WAS MOMENTARY AND LEFT EPR WAS NOTICED DECREASING THRU 1.5 BACK TO CLIMB EPR OF 1.3, OTHER PARAMETERS NORMAL.
- [SDR AWXA0000575](https://openairdocs.org/sdr/AWXA0000575.md): Window · cracked · Aug 21, 2000 · N645AW · Airbus A320231 · Flight Compartment Windows
  > AIR TURNBACK, F/O WINDSHIELD CRACKED IN FLIGHT AT APPROX 23000 FT AT 290 KTS IN THE CLIMBOUT. PRESSURE IN THE CABIN WAS NORMAL. REPLACED F/O WINDSHIELD, REMOVED AND REPLACED WINDOW HEAT CONTROLLER FOR ARCING.
- [SDR AWXA0000186](https://openairdocs.org/sdr/AWXA0000186.md): Power Supply · failed · Mar 30, 2000 · N645AW · Airbus A320231 · Emergency Lighting
  > EMERGENCY LIGHTS AT SEAT ROW 3 & 7 INOP. WHEN COMMANDED FROM COCKPIT OR FWD FLT ATTENDANT PANEL--WORKS WITH BREAKER H5 PULLED. REPLACED PWR SUPPLY UNIT AT 11 WL AND REPAIRED WIRES AT 7 ABC, OPS CHECK GOOD. TT 0060466 CURRENT HISTORY: WIRING AT ROW 7 WAS S
- [SDR AWXA0000153](https://openairdocs.org/sdr/AWXA0000153.md): Strap · corroded · Mar 22, 2000 · N645AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > C-CHECK, CABIN FLOOR PANEL 22FF JOIN STRIP CORRODED. CLEANED, PRIMED, AND PAINTED FLOOR STRIP IAW A320 SRM 51-75-00.
- [SDR AWXA0000152](https://openairdocs.org/sdr/AWXA0000152.md): Seat Track · corroded · Mar 22, 2000 · N645AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > C-CHECK, CABIN SEAT TRACK NR 2 Y765 LT FRAME 20 CORRODED. REPAIRED CORROSION IAW A320 SRM 53-00-15 FIG 101.
- [SDR AWXA9900313](https://openairdocs.org/sdr/AWXA9900313.md): Pwr Supply · inop · Sep 13, 1999 · N645AW · Airbus A320231 · Emergency Lighting
  > EMERGENCY EXITS OVERWING RIGHT AND AISLE AFT CENTER REMAIN ON. REMOVED AND REPLACED RT OVERWING EMERG LIGHT POWER SUPPLY.
- [SDR AWXA9900297](https://openairdocs.org/sdr/AWXA9900297.md): Actuator · leaking · Sep 5, 1999 · N645AW · Airbus A320231 · Autopilot System
  > CREW REPORTED GREEN HYDRAULIC SYSTEM LOW IN FLIGHT. AT CRUISE, LF 370, HYD GREEN LOW LEVEL ECAM MESSAGE. ACCOMPLISHED ECAM ACTIONS AND CONTINUED FLIGHT FOR UNEVENTFUL LANDING IN MIAMI. FOUND YAW DAMPER SYSTEM NR 1 LEAKING AT ACTUATOR. COMPLIED WITH MEL 22-
- [SDR AWXA9900276](https://openairdocs.org/sdr/AWXA9900276.md): Hyd Line · loose · Aug 30, 1999 · N645AW · Airbus A320231 · Hydraulic System, Main
  > EMERGENCY DECLARED, HYD GREEN LOW LEVEL RESULTING IN LOSS OF GREEN HYDRAULIC SYSTEM. INSPECTED SYSTEMS, NO LEAKS NOTED. FOUND GREEN SYS 5 QTS LOW. SERVICED QTY, ALL SYSTEMS OPS NML. SUSPECT LOW LEVEL WARNING TRIGGERED AFTER GEAR RET AND TEMP CHANGE. 30 AU
- [SDR AWXA9700653](https://openairdocs.org/sdr/AWXA9700653.md): Manifold · leaking · Nov 1, 1997 · N645AW · Airbus A320231 · Hydraulic System, Main
  > YELLOW HYDRAULIC SYSTEM LOST QUANTITY IN FLIGHT. DECLARED AN EMERGENCY LANDING. FOUND THE SERVICE MANIFOLD LEAKING. REMOVED AND REPLACED MANIFOLD.
- [SDR AWXA9700454](https://openairdocs.org/sdr/AWXA9700454.md): Fan · inoperative · Aug 2, 1997 · N645AW · Airbus A320231 · Air Distribution Fan
  > ON DEPARTURE, NOTICED SLIGHT BURNING ODOR IN COCKPIT. CHECKED COND PAGE AND FOUND COCKPIT FAN INOP. REMOVED AND REPLACED FWD CABIN RECIRCULATION FAN, OPS CHECK GOOD.
- [SDR AWXA9700284](https://openairdocs.org/sdr/AWXA9700284.md): Battery Pack · discharged · May 7, 1997 · N645AW · Airbus A320231 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT BATTERY PACK 11WL INOP. REMOVED AND REPLACED BATTERY PACK 11WL, OPS CHECK NORMAL AT THIS TIME.

Next page: https://openairdocs.org/deregistered/N645AW-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 = 'N645AW' AND deregistration_id = 'N645AW-2006-05-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N645AW-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.