# Service difficulty reports: N180AW, cancelled Nov 15, 2004

A list on [N180AW, cancelled Nov 15, 2004](https://openairdocs.org/deregistered/N180AW-2004-11-15.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 3 · 101 reports

- [SDR AWXA200300908](https://openairdocs.org/sdr/AWXA200300908.md): Battery · discharged · Aug 11, 2003 · N180AW · Boeing 737277 · Emergency Equipment
  > PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD LOWER CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN THE FORWARD LOWER CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200300369](https://openairdocs.org/sdr/AWXA200300369.md): Light · broken · Apr 14, 2003 · N180AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT ON SEAT ROW 9 LT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ON SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200300288](https://openairdocs.org/sdr/AWXA200300288.md): Frame · cracked · Mar 3, 2003 · N180AW · Boeing 737277 · Fuselage Main, Frame
  > DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD SIDE FRAME WL 207, RBL 24, JUST ABOVE FLIGHT COMPARTMENT FLOOR. MAINTENANCE REMOVED CRACKED BS 178 BULKHEAD SIDE FRAME AT WL 207, RBL 24; FABRICATED A NEW REPLACEMENT FRAME; INSTALLED REPAIR PARTS I
- [SDR AWXA200300295](https://openairdocs.org/sdr/AWXA200300295.md): Stiffener · cracked · Mar 1, 2003 · N180AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > LCQ - MAJOR REPAIR - DURING C-18 CHECK A 1" CRACK WAS FOUND ON VERTICAL STIFFENER AT FORWARD BULKHEAD, AFT CARGO COMPARTMENT BILGE, BS 727, RBL 6. MAINTENANCE REMOVED CRACKED STIFFENER AT FORWARD BULKHEAD, AFT CARGO COMPARTMENT, BS 727, RBL 6; FABRICATED A NEW
- [SDR AWXA200300285](https://openairdocs.org/sdr/AWXA200300285.md): Skin · damaged · Mar 1, 2003 · N180AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > DURING C-18 CHECK 4 SMALL CREASES WERE FOUND IN FUSELAGE SKIN AT BS 450, STR 26-27 RT. MAINTENANCE CUTOUT CREASED SKIN AT BS 450, STR 26-27 RT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PART IAW B737-200 SRM 53-30-3, FIG. 6, PG. 11.
- [SDR AWXA200300287](https://openairdocs.org/sdr/AWXA200300287.md): Bulkhead · cracked · Feb 26, 2003 · N180AW · Boeing 737277 · Fuselage Main, Bulkhead
  > DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB AT WL 190, BL 0, UNDER VOR/LOC ANTENNA MOUNT. MAINTENANCE CUTOUT CRACKED BS 178 BULKHEAD WEB AT WL 190, BL 0; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER,
- [SDR AWXA200300139](https://openairdocs.org/sdr/AWXA200300139.md): Light · shorted · Feb 13, 2003 · N180AW · Boeing 737277 · Flight Compartment Lighting
  > SMOKE IN COCKPIT - FLT 0227 - DURING TAXI TO GATE IN PHX THE GLARE SHIELD FLUORESCENT LIGHTS BEGAN TO SMOKE, SHUT LIGHTS OFF SMOKE DISSIPATED. MAINTENANCE PERFORMED VISUAL INSPECTION OF ALL COCKPIT AND INSTRUMENT LIGHTING AND FOUND WIRE INSULATION BURNED, AND
- [SDR AWXA200300055](https://openairdocs.org/sdr/AWXA200300055.md): Wire · broken · Jan 20, 2003 · N180AW · Boeing 737277 · Emergency Lighting
  > TUS - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H WAS FOUND INOPERATIVE. MAINTENANCE DISCOVERED A WIRE PULLED FROM SPLICE UNDER SEAT, REPAIRED BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H; OPERATIONAL CHECK WAS G
- [SDR AWXA200300286](https://openairdocs.org/sdr/AWXA200300286.md): Panel · cracked · Jan 17, 2003 · N180AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > LCQ - MAJOR REPAIR - DURING C-18 CHECK A 2" CRACK WAS FOUND ON KEEL BEAM PANEL BETWEEN THE L/H AND R/H WHEEL WELLS BS 600 TO 724. MAINTENANCE REMOVED EXISTING DOUBLER; PERFORMED NDT INSPECTION OF CRACK; REPLACED BLIND FASTENERS WITH SOLID FASTENERS; FABRICATED
- [SDR AWXA200200592](https://openairdocs.org/sdr/AWXA200200592.md): Battery · discharged · Jul 10, 2002 · N180AW · Boeing 737277 · Emergency Equipment
  > FORWARD EMERGENCY FLASHLIGHT INOPERATIVE, PLACED IN CHARGER BACKWARDS. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200200357](https://openairdocs.org/sdr/AWXA200200357.md): Battery · discharged · Apr 23, 2002 · N180AW · Boeing 737277 · Emergency Equipment
  > PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED LOWER FLASHLIGHT IN AFT CABIN IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES IN THE AFT CABIN LOWER FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200200235](https://openairdocs.org/sdr/AWXA200200235.md): Wire · broken · Mar 19, 2002 · N180AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - "C" - DURING INSPECTION OF EMERGENCY ESCAPE PATH LIGHTING A BROKEN WIRE WAS FOUND AT SEAT ROW 19 L/H. MAINTENANCE REPAIRED BROKEN WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H IAW SWP 20-30-12, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200200116](https://openairdocs.org/sdr/AWXA200200116.md): Tee Chord · cracked · Jan 30, 2002 · N180AW · Boeing 737277 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A 1.3" CRACK WAS FOUND ON INBOARD OF SEAT TRACK ON UPPER TEE CHORD OF LONGITUDINAL BEAM BS 727B, RBL 44, WL 208. MAINTENANCE TRIMMED OUT CRACKED AREA OF CHORD AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS, REMOV
- [SDR AWXA200200118](https://openairdocs.org/sdr/AWXA200200118.md): Skin · gouged · Jan 23, 2002 · N180AW · Boeing 737277 · Nacelle/Pylon, Plate/Skin
  > MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A GOUGE.009 TO.027 DEEP X 7" LONG WAS FOUND ON THE #1 ENGINE AFT PYLON INBOARD SIDE SKIN JUST FORWARD OF THE FLIPPER DOOR. MAINTENANCE REMOVED THE CLOSEOUT DOUBLER BELOW MIDFLAP OUTBOARD ATTACH POINT ON INBOARD SI
- [SDR AWXA200200117](https://openairdocs.org/sdr/AWXA200200117.md): Skin · gouged · Jan 23, 2002 · N180AW · Boeing 737277 · Nacelle/Pylon, Plate/Skin
  > MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A GOUGE.015 DEEP X 3" LONG WAS FOUND ON THE #1 ENGINE AFT PYLON INBOARD SIDE SKIN JUST AFT OF THE FLIPPER DOOR. MAINTENANCE REMOVED THE AFT INBOARD SKIN, FABRICATED NEW SKIN REPAIR DOUBLER AND INSTALLED IAW AWA ER
- [SDR AWXA200200114](https://openairdocs.org/sdr/AWXA200200114.md): Web · cracked · Jan 23, 2002 · N180AW · Boeing 737277 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A 1/4" CRACK WAS FOUND ON FLOOR BEAM WEB BS 714, RBL 25. MAINTENANCE TRIMMED OUT DAMAGED SECTION OF FLOOR BEAM AT BS 714, RBL 25, FABRICATED A REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIRS IAW AWA ER 15-5702-0203
- [SDR AWXA200200103](https://openairdocs.org/sdr/AWXA200200103.md): Web · cracked · Jan 23, 2002 · N180AW · Boeing 737277 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A CRACK WAS FOUND ON FLOOR BEAM WEB AT BS 714, RBL 25. MAINTENANCE REMOVED DAMAGED AREA OF WEB AT BS 714, RBL 25, FABRICATED REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW AWA ER 15-5702-02033-GF1.
- [SDR AWXA200200115](https://openairdocs.org/sdr/AWXA200200115.md): Skin · gouged · Jan 22, 2002 · N180AW · Boeing 737277 · Passenger/Crew Doors
  > MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A GOUGE WAS FOUND ON INNER SKIN AT FRAME TORQUE TUBE BOX OF THE L1 DOOR BS 305, STR 11-12, IN ADDITION TWO EXISTING REPAIRS WILL NEED TO BE INCORPORATED IN CORRECTIVE ACTION. MAINTENANCE REMOVED EXISTING REPAIRS FRO
- [SDR AWXA200200102](https://openairdocs.org/sdr/AWXA200200102.md): Skin · cracked · Jan 21, 2002 · N180AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A CRACK WAS FOUND ON THE UPPER HINGE CUTOUT OF THE L1 DOOR AT UPPER CORNER BS 300. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED. FABRICATED AND INSTALLED REPAIR DOUBLER
- [SDR AWXA200200080](https://openairdocs.org/sdr/AWXA200200080.md): Skin · cracked · Jan 21, 2002 · N180AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A CRACK WAS FOUND ON L1 DOOR UPPER HINGE CUTOUT AT UPPER CORNER BS 319.5. MAINTENANCE STOP DRILLED THE CRACK AND PERFORMED HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED; FABRICATED A REPAIR DOUBLER AND INSTALLED
- [SDR AWXA0001319](https://openairdocs.org/sdr/AWXA0001319.md): Fitting · corroded · Feb 9, 2001 · N180AW · Boeing 737277 · Horizontal Stabilizer, Attach Fittings
  > RT HORIZ STAB REAR SPAR UPPER ATTACH FITTING CORRODED. BLENDED CORROSION IAW ER 15-5510-01027-ES2.
- [SDR AWXA0001313](https://openairdocs.org/sdr/AWXA0001313.md): Fitting · corroded · Feb 9, 2001 · N180AW · Boeing 737277 · Vertical Stabilizer, Attach Fittings
  > RT AFT VERT STAB I/B (FAILSAFE) LUG CORRODED/GOUGED ON ID AND CORRODED/GOUGED ON FWD FACE. LOCALLY BLENDED GOUGE AREAS IAW ER 15-5510-01023-JS3.
- [SDR AWXA0001312](https://openairdocs.org/sdr/AWXA0001312.md): Fitting · corroded · Feb 9, 2001 · N180AW · Boeing 737277 · Vertical Stabilizer, Attach Fittings
  > LT AFT VERT STAB I/B (FAILSAFE) LUG GOUGED IN ID AND CORRODED ON FWD FACE. LOCALLY BLENDED GOUGED AREAS OF LUG FWD SPOT FACE AREA IAW ER 15-5510-0123-JS3.
- [SDR AWXA0001323](https://openairdocs.org/sdr/AWXA0001323.md): Bulkhead · chafed · Feb 9, 2001 · N180AW · Boeing 737277 · Nacelle/Pylon, Bulkhead/Firewall
  > NR 2 PYLON O/B STRUCTURE CHAFED AT FWD END ABOVE ENGINE. REMOVED BLKHEAD; LOCATED, DRILLED AND INSTALLED NEW BLKHEAD (P/N 65-79415-92) IAW SRM 51-30-02.
- [SDR AWXA0001322](https://openairdocs.org/sdr/AWXA0001322.md): Fitting · corroded · Feb 9, 2001 · N180AW · Boeing 737277 · Horizontal Stabilizer, Attach Fittings
  > VERT STAB REAR LUGS, RT AFT O/B LUG HAS CORROSION ON ID OF BORE. REAMED LUG IAW BAC DWG 65C22124-10 AND EO 55-50-01; HFEC INDICATES NO DEFECTS NOTED.
- [SDR AWXA0001321](https://openairdocs.org/sdr/AWXA0001321.md): Fitting · gouged · Feb 9, 2001 · N180AW · Boeing 737277 · Horizontal Stabilizer, Attach Fittings
  > LT HORIZ STAB REAR SPAR UPPER ATTACH LUG AFT SIDE FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES2.
- [SDR AWXA0001320](https://openairdocs.org/sdr/AWXA0001320.md): Fitting · gouged · Feb 9, 2001 · N180AW · Boeing 737277 · Horizontal Stabilizer, Attach Fittings
  > LT HORIZ STAB CENTER SECTION LUGS, LT REAR, AFT SIDE OF MID LUG HAS GOUGES AND NICKS ON AFT SIDE OF LUG. BLENDED NICKS AND GOUGES IAW ER 15-5510-01027-SS4.
- [SDR AWXA0001318](https://openairdocs.org/sdr/AWXA0001318.md): Fitting · gouged · Feb 9, 2001 · N180AW · Boeing 737277 · Horizontal Stabilizer, Attach Fittings
  > LT HORIZ STAB FWD SPAR UPPER ATTACH LUG FWD FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES2.
- [SDR AWXA0001317](https://openairdocs.org/sdr/AWXA0001317.md): Fitting · gouged · Feb 9, 2001 · N180AW · Boeing 737277 · Horizontal Stabilizer, Attach Fittings
  > LT HORIZ STAB FWD LWR LUG HAS A GOUGE ON THE FWD SIDE OF SPOT FACE. BLENDED GOUGE IAW ER 15-5510-01027-ES2.
- [SDR AWXA0001316](https://openairdocs.org/sdr/AWXA0001316.md): Fitting · gouged · Feb 9, 2001 · N180AW · Boeing 737277 · Horizontal Stabilizer, Attach Fittings
  > RT HORIZ STAB AFT SPAR MID ATTACH AFT FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES1.
- [SDR AWXA0001314](https://openairdocs.org/sdr/AWXA0001314.md): Fitting · gouged · Feb 9, 2001 · N180AW · Boeing 737277 · Horizontal Stabilizer, Attach Fittings
  > RT HORIZ STAB AFT SPAR UPPER ATTACH LUG AFT FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES1.
- [SDR AWXA0001311](https://openairdocs.org/sdr/AWXA0001311.md): Beam · cracked · Feb 9, 2001 · N180AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > HFEC INDICATES A 2 INCH CRACK AT I/B SIDE OF VERTICAL CHORD ON AFT SIDE OF FS 178 BLKHEAD BETWEEN WL 183 AND 185 LBL 5.7. REPAIRED I/B SIDE OF VERTICAL CHORD ON AFT SIDE OF FS 178 BLKHEAD BETWEEN WL 183 AND 185 LBL 5.7 IAW SRM 53-10-11 FIG 8 PG 46-65.
- [SDR AWXA0001310](https://openairdocs.org/sdr/AWXA0001310.md): Floorbeam · cracked · Feb 9, 2001 · N180AW · Boeing 737277 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM UPPER CHORD FWD FACE HAS A CRACK IN RADIUS EXTENDING BEYOND STOP DRILL FS 526 RBL 24.75. REPAIRED FLOORBEAM UPPER CHORD IAW BOEING MESSAGE CPZ-MCN-01-0010N AND ER 15-5310-01023-JS1.
- [SDR AWXA0001309](https://openairdocs.org/sdr/AWXA0001309.md): Skin · gouged · Feb 9, 2001 · N180AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > GOUGED AREA ON RT AFT UPPER FUSELAGE SKIN BETWEEN STA 807 AND 827 APPROX 50 INCHES ABOVE WINDOW. REMOVED DAMAGED SKIN; FABED, TREATED FILLER AND DOUBLER; DRILLED AND INSTALLED IAW SRM 53-30-03.
- [SDR AWXA0001308](https://openairdocs.org/sdr/AWXA0001308.md): Bulkhead · cracked · Feb 9, 2001 · N180AW · Boeing 737277 · Fuselage Main, Bulkhead
  > ULTRASONIC INSPECTION REVEALED CRACK INDICATION AT FS 178 BULKHEAD WEB BENEATH STRAP AT RBL 7 TO RBL 15 WL 218. REMOVED STIFFENERS, BRACKETS AND ANGLES; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER, FILLERS AND SHIMS IAW SRM 53-10-11; INSTALLED STIFFENERS BR
- [SDR AWXA0001307](https://openairdocs.org/sdr/AWXA0001307.md): Bulkhead · cracked · Feb 9, 2001 · N180AW · Boeing 737277 · Fuselage Main, Bulkhead
  > HFEC INDICATES A.200 INCH LONG CRACK EMINATING FROM FASTENER HOLE AT BLKHD FS 178 RBL 12.75 WL 234. REMOVED STIFFENERS, BRACKETS AND ANGLES; FABED, DRILLED, TREATED AND INSTALLED DOUBLER, FILLERS AND SHIMS IAW SRM 53-10-11; REINSTALLED STIFFENERS, BRACKETS A
- [SDR AWXA0001306](https://openairdocs.org/sdr/AWXA0001306.md): Floorbeam · corroded · Feb 9, 2001 · N180AW · Boeing 737277 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR SUPPORT FWD OF LT LAV WASTE EXIT AND FLOORBEAM AT FS 1006 FOUND TO BE OUT OF LIMITS IAW B737-200 SRM 53-10-6. REMOVED CORROSION ON SUPPORT AND FLOORBEAM IAW SRM 52-10-2; CUT OUT DAMAGED AREA ON BEAM; FABED, DRILLED, TREATED AND INSTALLED RE
- [SDR AWXA0001305](https://openairdocs.org/sdr/AWXA0001305.md): Rib · chafed · Feb 8, 2001 · N180AW · Boeing 737277 · Vertical Stabilizer, Spar/Rib
  > AREA OF DEEP CHAFING ON VERT STAB FWD LWR END CAP RIB. REMOVED FWD LWR END CAP AND REPLACED WITH A NEW PART IAW SRM 53-10-11 AND 51-30-2.
- [SDR AWXA0001304](https://openairdocs.org/sdr/AWXA0001304.md): Floorbeam · corroded · Feb 8, 2001 · N180AW · Boeing 737277 · Fuselage Main, Floor Beam
  > FLOORBEAM TOP CAP AT BS 294.5 RBL 41 FOUND TO BE OUT OF LIMITS AFTER CORROSION CLEAN UP IAW SRM 53-10-01. REPAIRED FLOORBEAM UPPER CHORD IAW SRM 53-10-02 FIG 7 AND 53-40-04.
- [SDR AWXA0001303](https://openairdocs.org/sdr/AWXA0001303.md): Bulkhead · cracked · Feb 8, 2001 · N180AW · Boeing 737277 · Fuselage Main, Bulkhead
  > ULTRASONIC INSPECTION REVEALED CRACK INDICATION AT FS 178 BLKHEAD BENEATH STRAP FROM LBL 5 TO LBL 8 WL 217 IN WEB. REMOVED STIFFENERS, BRACKETS AND ANGLES AT FS 178 WL 207 TO WL 241 FROM RBL 18 TO LBL 18; LOCATED, DRILLED, TREATED AND INSTALLED REPAIR DOUBLER
- [SDR AWXA0001302](https://openairdocs.org/sdr/AWXA0001302.md): Angle · cracked · Feb 8, 2001 · N180AW · Boeing 737277 · Trailing Edge Flaps
  > LEFT WING O/B HINGED FLAP TRACK ATTACH ANGLE CRACKED. REMOVED ANGLE; FABED, TREATED AND PRIMED IAW SRM 51-20-1 AND 51-10-2; INSTALLED ANGLE IAW SRM 51-30-2.
- [SDR AWXA0001301](https://openairdocs.org/sdr/AWXA0001301.md): Bulkhead · cracked · Feb 8, 2001 · N180AW · Boeing 737277 · Fuselage Main, Bulkhead
  > ULTRASONIC INSPECTION REVEALED CRACK INDICATION AT FS 178 BLKHEAD WEB BENEATH STRAP AT LBL 6 WL 230 TO 233. REMOVED STIFFENERS, BRACKETS AND ANGLES; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER, FILLERS AND SHIMS IAW B737-200 SRM 53-10-11; INSTALLED STIFFENE
- [SDR AWXA0001300](https://openairdocs.org/sdr/AWXA0001300.md): Floorbeam · corroded · Feb 8, 2001 · N180AW · Boeing 737277 · Fuselage Main, Floor Beam
  > CORROSION ON UPPER SURFACE OF FLOORBEAM AT FS 312 RBL 8 TO RBL 10; OUT OF LIMITS IAW B737-200 SRM 53-16-1 PG 7. REPAIRED FLOORBEAM IAW B737-200 SRM 53-10-9.
- [SDR AWXA0001299](https://openairdocs.org/sdr/AWXA0001299.md): Stringer · corroded · Feb 8, 2001 · N180AW · Boeing 737277 · Fuselage Main, Longeron/Stringer
  > STR 27L IS CORRODED OUT OF LIMITS IAW B737-200 SRM 53-20-2, FROM FS 1016 TO FS 986. REMOVED CORRODED SECTION; FABED AND TREATED REPAIR PARTS; INSTALLED NEW SECTION OF STRINGER AND REPAIR PARTS IAW B737-200 SRM 53-10-2 AND 51-20-2.
- [SDR AWXA0001298](https://openairdocs.org/sdr/AWXA0001298.md): Floorbeam · cracked · Feb 8, 2001 · N180AW · Boeing 737277 · Fuselage Main, Floor Beam
  > UPPER CHORD, FWD FACE OF FLOORBEAM AT BS 520 HAS A CRACK EXTENDING THROUGH PREVIOUS STOP DRILL. REMOVED PREVIOUS REPAIR; CUT OUT PREVIOUS REPAIR; FABED DOUBLERS, T-CAP AND STRAPS; DRILLED, DEBURRED, TREATED AND INSTALLED IAW B737-200 SRM 53-10-09 FIG 2; INSTA
- [SDR AWXA0000774](https://openairdocs.org/sdr/AWXA0000774.md): Light · burned out · Oct 13, 2000 · N180AW · Boeing 737277 · Instrument Panel
  > ON TAKEOFF MULTIPLE LIGHTS ILLUMINATED. TROUBLESHOT WITH MAINT CONTROL TO CONTINUE TO LAS. PUSHED WINDSHEAR INOP LIGHT EXTINGUISHED ON GROUND IN LAS. SMELLED ELECTRICAL BURNED WIRES. REMOVED AND REPLACED CAPTAIN WINDSHEAR INOP LIGHT ASSY PER MM 34-36, SYS
- [SDR AWXA0000446](https://openairdocs.org/sdr/AWXA0000446.md): Controller · malfunctioned · Jul 7, 2000 · N180AW · Boeing 737277 · Cabin Pressure Controller
  > COULD NOT CONTROL PRESSURIZATION CLIMBING FROM FL 300 TO 310, O2 MASK DID NOT DEPLOY, NO EMERGENCY CALLED. NO CORRECTIVE ACTION IN SCEPTRE AT THIS TIME.
- [SDR AWXA0000373](https://openairdocs.org/sdr/AWXA0000373.md): Controller · malfunctioned · Jun 6, 2000 · N180AW · Boeing 737277 · Cabin Pressure Controller
  > AIR TURNBACK, 1ST EVENT-- AFTER T/O, BLEEDS OFF, COULD NOT GET NR 2 ENG BLEED TO COME ON. ALSO, CABIN CLIMBING WITH THE A/C. REPLACED NR 2 BLEED AIR SHUT-OFF VALVE. 2ND EVENT REF LP 7730322 UNABLE TO PRESSURIZE CABIN. REMOVED AND REPLACED CABIN PRESS CONT
- [SDR AWXA0000348](https://openairdocs.org/sdr/AWXA0000348.md): Tube · chafed · May 30, 2000 · N180AW · Boeing 737277 · Engine Oil Cooler
  > NR 2 ENGINE LOST OIL QUANTITY AND PRESSURE, ENGINE SHUT DOWN. TROUBLESHOT SYS, FOUND CHAFED OIL COOLER INLET LINE. REPLACED LINE, LEAK AND OPS CHECK GOOD. RECOMMENDATION: CLOSE, NO RELATED HISTORY.
- [SDR AWXA9900498](https://openairdocs.org/sdr/AWXA9900498.md): Power Supply · inoperative · Dec 27, 1999 · N180AW · Boeing 737277 · Emergency Lighting
  > LEFT AND RIGHT FWD EMERGENCY EXIT DOOR LIGHTS AND CEILING LIGHT STARTED FLASHING AFTER 1 MINUTE. REPLACED FWD BATTERY PACK AND POWER SUPPLY, OPS CK GOOD.

Next page: https://openairdocs.org/deregistered/N180AW-2004-11-15/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 = 'N180AW' AND deregistration_id = 'N180AW-2004-11-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N180AW-2004-11-15/reports

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