N180AW, cancelled Nov 15, 2004
Service difficulty reports · 101
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AWXA200300908Battery · dischargedPHX - 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 AWXA200300369Light · brokenPHX - 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 AWXA200300288Frame · crackedDURING 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 ISDR AWXA200300295Stiffener · crackedLCQ - 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 NEWSDR AWXA200300285Skin · damagedDURING 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 AWXA200300287Bulkhead · crackedDURING 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 AWXA200300139Light · shortedSMOKE 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 AWXA200300055Wire · brokenTUS - 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 GSDR AWXA200300286Panel · crackedLCQ - 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; FABRICATEDSDR AWXA200200592Battery · dischargedFORWARD EMERGENCY FLASHLIGHT INOPERATIVE, PLACED IN CHARGER BACKWARDS. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200357Battery · dischargedPHX - 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 AWXA200200235Wire · brokenPHX - 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 AWXA200200116Tee Chord · crackedMCN - 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, REMOVSDR AWXA200200118Skin · gougedMCN - 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 SISDR AWXA200200117Skin · gougedMCN - 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 AWXA200200114Web · crackedMCN - 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 15-5702-0203SDR AWXA200200103Web · crackedMCN - 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 AWXA200200115Skin · gougedMCN - 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 FROSDR AWXA200200102Skin · crackedMCN - 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 AWXA200200080Skin · crackedMCN - 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 INSTALLEDSDR AWXA0001319Fitting · corrodedRT HORIZ STAB REAR SPAR UPPER ATTACH FITTING CORRODED. BLENDED CORROSION IAW ER 15-5510-01027-ES2.SDR AWXA0001313Fitting · corrodedRT 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 AWXA0001312Fitting · corrodedLT 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 AWXA0001323Bulkhead · chafedNR 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 AWXA0001322Fitting · corrodedVERT 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 AWXA0001321Fitting · gougedLT HORIZ STAB REAR SPAR UPPER ATTACH LUG AFT SIDE FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES2.SDR AWXA0001320Fitting · gougedLT 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 AWXA0001318Fitting · gougedLT HORIZ STAB FWD SPAR UPPER ATTACH LUG FWD FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES2.SDR AWXA0001317Fitting · gougedLT HORIZ STAB FWD LWR LUG HAS A GOUGE ON THE FWD SIDE OF SPOT FACE. BLENDED GOUGE IAW ER 15-5510-01027-ES2.SDR AWXA0001316Fitting · gougedRT HORIZ STAB AFT SPAR MID ATTACH AFT FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES1.SDR AWXA0001314Fitting · gougedRT HORIZ STAB AFT SPAR UPPER ATTACH LUG AFT FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES1.SDR AWXA0001311Beam · crackedHFEC 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 AWXA0001310Floorbeam · crackedCABIN 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 AWXA0001309Skin · gougedGOUGED 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 AWXA0001308Bulkhead · crackedULTRASONIC 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 BRSDR AWXA0001307Bulkhead · crackedHFEC 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 ASDR AWXA0001306Floorbeam · corrodedCORROSION 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 RESDR AWXA0001305Rib · chafedAREA 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 AWXA0001304Floorbeam · corrodedFLOORBEAM 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 AWXA0001303Bulkhead · crackedULTRASONIC 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 DOUBLERSDR AWXA0001302Angle · crackedLEFT 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 AWXA0001301Bulkhead · crackedULTRASONIC 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 STIFFENESDR AWXA0001300Floorbeam · corrodedCORROSION 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 AWXA0001299Stringer · corrodedSTR 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 AWXA0001298Floorbeam · crackedUPPER 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; INSTASDR AWXA0000774Light · burned outON 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 AWXA0000446Controller · malfunctionedCOULD 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 AWXA0000373Controller · malfunctionedAIR 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 CONTSDR AWXA0000348Tube · chafedNR 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 AWXA9900498Power Supply · inoperativeLEFT 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.
Back to N180AW, cancelled Nov 15, 2004