N182AW, cancelled Mar 9, 2005
Service difficulty reports · 167
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 = 'N182AW' AND deregistration_id = 'N182AW-2005-03-09' 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 = 'N182AW' AND deregistration_id = 'N182AW-2005-03-09' 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 AWXA200401179Light · inoperativeFLIGHT CREW REPORTED R-2 DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED R-2 DOOR EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200401089Brake · seizedABORTED TAKEOFF, FLT 0109, ON TAKEOFF, EN ROUTE WHEN APPROACHING V1 THE AIRCRAFT NOSE STARTED TO ROTATE ON ITS OWN, LOWERED NOSE AND REJECTED TAKEOFF AT 138 KTS. MAINTENANCE PERFORMED HORIZONTAL STABILIZER TRIM TEST, ALL TRIM INDICATIONS AGREE WITH (B) DIMENSSDR AWXA200401011Packing · tornEN ROUTE, NR 1 ENG SHUTDOWN AT 27,000 FT, ATTEMPTED RESTART WITHOUT SUCCESS, DECLARED EMERGENCY & LANDED WITHOUT FURTHER EVENT. MX FOUND SEALS ON PRESS DUMP VALVE INPUT FUEL LINE TORN & LEAKING. REPLACED SEALS, ENGINE RUN OPERATIONAL CHECK WAS GOOD. MX R/R LSDR AWXA200401022Skin · crackedDURING 4-DAY CHECK, A 1 1/2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727A, STR 16 RT. MAINTENANCE REMOVED EXISTING REPAIR, CUTOUT DAMAGED AREA OF SKIN AT BS 727A, STR 16 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIRSDR AWXA200400886Motor · bindingON CLIMB-OUT OF PHX EN ROUTE FOR SJC AT APPROXIMATELY 3000 FT, FLIGHT CONTROLS SHOOK VIOLENTLY FROM SIDE TO SIDE AS IF IN SEVERE TURBULENCE. NOTICED FEEL DIFFERENTIAL LIGHT ILLUMINATED, TURNED BACK TO PHX, ADJUSTED AILERON TRIM AND ONCE AILERON INPUT WAS ACHISDR AWXA200400816Power Supply · dischargedPHX - EEL - DURING INSPECTION THE EMERGENCY LIGHTS SEAT ROW 15 LEFT AND AFT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNDER SEAT ROW 17 LEFT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400815Light · failedPHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400802Warning Light · false indicationFALSE FIRE WARNING ON CLIMB OUT, AFTER SELECTING FLAPS UP RECEIVED FWD CARGO FIRE LIGHT AND FIRE BELL, DISCHARGED NR 1 CARGO FIRE BOTTLE AND LIGHT EXTINGUISHED, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINT MET AC AND PERFORMED A MAINT BITE TEST SDR AWXA200400636Socket · shortedPHX - EMERGENCY LANDING - FLT 0628 - ON DESCENT INTO PHX EN ROUTE FROM OAK AT FL 120 EXPERIENCED AN ELECTRICAL BURNING ODOR FOLLOWED BY SMOKE IN COCKPIT, DONNED O2 MASKS AND DECLARED AN EMERGENCY. AT FL 030 FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN COMING FROSDR AWXA200400344Hydraulic Line · rupturedSAT - AIR TURNBACK - FLT 0679 - ON CLIMBOUT OF SAT EN ROUTE FOR PHX LOST A-HYDRAULIC SYSTEM, FOLLOWED QRH AND TURNED BACK TO SAT. MAINTENANCE REMOVED AND REPLACED RUPTURED HYDRAULIC PRESSURE LINE BETWEEN A-SYSTEM MODULE AND LT MAIN LANDING GEAR ACTUATOR. REMSDR AWXA200400354Skin · crackedPHX - MAJOR REPAIR - A .25 INCH CRACK WAS FOUND IN FUSELAGE SKIN LT SIDE AT LAP SEAM BETWEEN WINDOWS 11 & 12, BS 540, STR 14 LEFT. MAINTENANCE CUT OUT DAMAGED SECTION OF SKIN JUST BELOW WINDOW BELT BS 540, STR 14 LEFT; FABRICATED 4 EACH FILLERS, A DOUBLER & TSDR AWXA200400179Wire · brokenDURING INSPECTION A BROKEN WIRE WAS FOUND ON THE EMERGENCY ESCAPE PATH LIGHT SEAT ROW 17 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301385Bracket · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A .375 INCH CRACK WAS FOUND IN A BRACKET AT BS 334, LBL 56, WL 206. MAINTENANCE REMOVED THE CRACKED BRACKET AT BS 334, LBL 56, WL 206; FABRICATED A NEW REPLACEMENT BRACKET; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02SDR AWXA200301389Tie Clip · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A 1 .5 INCH CRACK WAS FOUND IN TIE CLIP BS 344-350, STR 16 LT. MAINTENANCE REMOVED THE CRACKED TIE CLIP BS 344-350, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 65-17685; INSTALLED REPAIR PART IAW B737-200 SRM 51SDR AWXA200301369Floorbeam · corrodedDURING C-21 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF UPPER T-CAP REPAIR AT BS 986.5, RBL 0.5 TO RBL 45. MAINTENANCE REMOVED UPPER T-CAP REPAIR AT BS 986.5, LBL 11 TO RBL 51; FABRICATED A NEW REPLACEMENT T-CAP; INSTALLED REPAIR PART IAW B737-200SDR AWXA200301422Web · crackedDURING C-21 CHECK 2 EACH CRACKS WERE FOUND ON SHEAR WEB AT BS 344, AFT OF L-1 DOOR. MAINTENANCE REMOVED DAMAGED SHEAR WEB BS 344; FABRICATED A NEW REPLACEMENT SHEAR WEB; INSTALLED REPAIR PART IAW B737-200 SRM 51-20-02, FIG 7.SDR AWXA200301398Clip · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A 1.5 INCH CRACK WAS FOUND IN RADIUS OF INTERCOSTAL CLIP ANGLE BS 344, STR 16 LT. MAINTENANCE REMOVED DAMAGED INTERCOSTAL CLIP ANGLE BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT FUSELAGE CLIP ANGLE; INSTALLED REPAIR PSDR AWXA200301397Frame · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A 1.125 INCH CRACK WAS FOUND IN RADIUS OF FUSELAGE FRAME CHORD, AFT OF L-1 DOOR BS 344, STR 15 LT. MAINTENANCE REMOVED DAMAGED FUSELAGE FRAME CHORD AFT OF L-1 DOOR BS 344, STR 15 LT; FABRICATED A NEW REPLACEMENT FUSELAGESDR AWXA200301392Angle · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A 1 INCH CRACK WAS FOUND IN CLIP ANGLE ON BOTTOM OF INTERCOSTAL AT STRINGER 16 LT, BS 344. MAINTENANCE REMOVED THE CRACKED CLIP ANGLE BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP ANGLE PER DWG 69-16509; INSTALLEDSDR AWXA200301391Angle · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A 1.125 INCH CRACK WAS FOUND IN CLIP ANGLE ON TOP OF INTERCOSTAL AT STRINGER 16 LT, BS 344. MAINTENANCE REMOVED THE CRACKED CLIP ANGLE BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP ANGLE PER DWG 69-26555; INSTALLESDR AWXA200301390Attach Angle · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A 2.875 INCH CRACK WAS FOUND IN STRINGER 15 LT TO FRAME 344 ATTACH ANGLE. MAINTENANCE REMOVED THE CRACKED ATTACH ANGLE BS 344, STR 15 LT; FABRICATED A NEW REPLACEMENT ATTACH ANGLE DWG 69-16970; INSTALLED REPAIR PART IAW SDR AWXA200301386Clip · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A .375 INCH CRACK WAS FOUND IN FRAME ATTACH CLIP ON L-1 DOOR AFT FRAME AT NR 6 DOOR STOP BS 344, STR 16 LT. MAINTENANCE REMOVED THE CRACKED FRAME ATTACH CLIP AT BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWSDR AWXA200301365Floor Support · corrodedDURING C-21 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 1003, LBL 38. MAINTENANCE REMOVED FLOOR SUPPORT FROM BS 986.5 TO BS 1006, LBL 38; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 FIG 11 SDR AWXA200301338Stringer Clip · crackedDURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 380, STR 25 LT. MAINTENANCE REMOVED AND REPLACED STRINGER TIE CLIP AT BS 380, STR 25 LT IAW B737-300 SRM 51-30-02, PG 2-3, & 8-10.SDR AWXA200301399Fairing · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A 2 INCH CRACK WAS FOUND ON NR 1 THRUST REVERSER LOWER DEFLECTOR DOOR LT FAIRING AT 2ND FASTENER HOLE FROM FORWARD END. MAINTENANCE CUT OUT DAMAGE SECTION OF NR 1 THRUST REVERSER LOWER DEFLECTOR DOOR LT FAIRING; PERFORMESDR AWXA200301387Clip · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A .375 INCH CRACK WAS FOUND IN FRAME ATTACH CLIP ON L-1 DOOR AFT FRAME AT NR 6 DOOR STOP BS 344, STR 16 LT. MAINTENANCE REMOVED THE CRACKED FRAME ATTACH CLIP AT BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWSDR AWXA200301370Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-21 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF UPPER T-CAP REPAIR AT BS 967, RBL 10 TO RBL 48. MAINTENANCE REMOVED UPPER T-CAP REPAIR AT BS 967, RBL 10 TO RBL 48; FABRICATED A NEW REPLACEMENT T-CAP; INSTALLED REPAIR PSDR AWXA200301367Splice · corrodedDURING C-21 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR ATTACH STRAP BS 771, STR 26 LT TO STR 26 RT. MAINTENANCE REMOVED DAMAGED FLOOR ATTACH STRAP BS 771, STR 26 LT TO STR 26 RT; FABRICATED A NEW REPLACEMENT STRAP; INSTALLED REPAIR PART IAW B737-200 SDR AWXA200301364Floorbeam · corrodedDURING C-21 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER AFT LEG AT BS 947 FROM RBL 5 TO LBL 53. MAINTENANCE CUT OUT DAMAGED FLOORBEAM UPPER AFT LEG AT BS 947 FROM RBL 5 TO LBL 53; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTASDR AWXA200301342Tail Cone · delaminatedMCN - MINOR REPAIR - DURING C-21 CHECK THE TAIL CONE WAS FOUND DELAMINATED AT LOWER CENTER 7 INCHES, 11 INCHES, & 24 INCHES FROM FORWARD END, 7.5 INCHES LT LOWER SIDE 12.5-15 INCHES FROM FORWARD END, 4-7 INCHES RT SIDE OF CENTER LOWER 16.5 INCHES FROM FORWARD SDR AWXA200301419Web · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON SHEAR WEB AT FORWARD INBOARD SIDE END OF CREASE BEAM BS 995.5, LBL 43.5. MAINTENANCE REMOVED CRACKED SHEAR WEB AT FORWARD INBOARD SIDE END OF CREASE BEAM BS 995.5, LBL 43.5; FABRICATED A NEW RSDR AWXA200301418Clip · crackedMCN - MINOR REPAIR - DURING C-21 CHECK A .25 INCH CRACK WAS FOUND ON L-ANGLE CLIP AT UPPER AFT END OF NR 2 ENGINE COWLING. MAINTENANCE REMOVED CRACKED L-ANGLE CLIP; FABRICATED A NEW REPLACEMENT CLIPPER DWG 65-552263-27; INSTALLED REPAIR PART IAW B737-22 SRM 5SDR AWXA200301388Angle · corrodedMCN - MAJOR REPAIR - DURING C-21 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR ZEE ANGLE AT BS 520, RBL 20. MAINTENANCE CUT OUT DAMAGED SECTION OF ZEE ANGLE AT BS 520, RBL 20; FABRICATED A ZEE ANGLE AND 4 EACH REPAIR ANGLES; INSTALLSDR AWXA200301366Web · crackedDURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON FORWARD END OF LT SHEAR WEB AT BS 995.5, LBL 43.5, AND EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF LT OUTBOARD SHEAR WEB, BS 1002, LBL 40. MAINTENANCE REMOVED DAMAGED SHEAR WEB FROM BS 995.5 TO BS 1014, LBSDR AWXA200301363Angle · crackedDURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON ANGLE (CLIP) FORWARD SIDE OF BS 500B FRAME, ABOVE STR 26 LT. MAINTENANCE REMOVED CRACKED ANGLE FORWARD SIDE OF BS 500B FRAME, ABOVE STR 26 LT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-51411; INSTALLED REPAIR SDR AWXA200301343Intercostal · crackedMCN - MINOR REPAIR - DURING C-21 CHECK A .5 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 480, LBL 24. MAINTENANCE REMOVED INTERCOSTAL FROM BS 460 TO BS 480, LBL 24; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 69-41473; INSTALLED REPAIR PART IAW B737-200 SRMSDR AWXA200301395Skin · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A 1 .375 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT FASTENER HOLE LOWER AFT CORNER OF L-1 DOOR, BS 344. MAINTENANCE CUTOUT DAMAGE ON FUSELAGE SKIN AT LOWER AFT CORNER OF L-1 DOOR; PERFORMED HFEC INSPECTION TO VERIFY NO CRASDR AWXA200301368Frame · crackedDURING C-21 CHECK A .3125 INCH CRACK WAS FOUND ON AFT SIDE OF R-1 DOOR INBOARD OF THE 3RD AFT STOP FITTING FROM THE BOTTOM BS 327, STR 14 RT. MAINTENANCE CUT OUT DAMAGE ON AFT SIDE OF R-1 DOOR 3RD AFT STOP FITTING FROM THE BOTTOM BS 327, STR 14 RT; FABRICATEDSDR AWXA200301341Slat · delaminatedMCN - MAJOR REPAIR - DURING C-21 CHECK THE NR 1 LEADING EDGE SLAT WAS FOUND DELAMINATED AT THE INBOARD UPPER SURFACE WS 510 TO WS 512 LT. MAINTENANCE CUT OUT DELAMINATED AREA ON NR 1 L/E SLAT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-2SDR AWXA200301396Skin · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A .5 INCH CRACK WAS FOUND ON PREVIOUS REPAIR AT FASTENER HOLE OF LOWER FUSELAGE SKIN BS 454, RBL 3. MAINTENANCE TRIMMED OUT DAMAGE ON PREVIOUS REPAIR AT FASTENER HOLE OF LOWER FUSELAGE SKIN BS 454, RBL 3; PERFORMED HFEC SDR AWXA200301394Skin · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A .75 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT FASTENER HOLE ON FORWARD UPPER CORNER OF R-1 DOOR, BS 292.50. MAINTENANCE PERFORMED HFEC ON CRACK AND IDENTIFIED CRACK END; STOP DRILLED CRACK IN FUSELAGE SKIN AT R-1 DOOR FSDR AWXA200301030Circuit Breaker · inoperativeON APPROACH INTO PHX EN ROUTE FROM BUR AFTER LANDING GEAR EXTENSION THERE WAS NO LANDING GEAR DOWN AND LOCKED OR UNSAFE GEAR INDICATIONS, ABORTED APPROACH. FOUND CIRCUIT BREAKER (SECT5) EXTENDED, AFTER DISCUSSION WITH MAINTENANCE CONTROL, CIRCUIT BREAKER WAS RSDR AWXA200300995Light · brokenFLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300944Light · brokenDURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300941Controller · malfunctionedON INITIAL TAKEOFF ROLL EN ROUTE, THE CABIN CLIMB INDICATOR NEEDLE WENT TO RAPID RATE OF DESCENT OF ABOUT 4000 FPM, REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER IAW BMM 21-31-21, PERFORMED OPERATIONAL CSDR AWXA200300812Bleed Valve · malfunctionedDEN - ABORTED TAKEOFF - FLT 0640 - DURING TAKEOFF ROLL AT DEN EN ROUTE FOR PHX, A LOUD "BANG" CAME FROM THE NR 1 ENGINE, REJECTED TAKEOFF, SUSPECT COMPRESSOR STALL. MAINTENANCE PERFORMED A BORESCOPE INSPECTION IAW T/C I5M72008, NO DAMAGE NOTED. REMOVED AND REPSDR AWXA200300550Transmitter · malfunctionedPHX - ABORTED TAKEOFF - FLT 0445 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR TUS, SETTING REDUCED FOR POWER 1.96, NR 2 ENGINE EPR DID NOT COME UP TO POWER, EPR STAGNATED AT 1.45 EPR WHILE THRUST LEVER ADVANCED. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TRSDR AWXA200300300Engine · out of trimON TAKEOFF AT PHX EN ROUTE FOR ONT WHEN SELECTING TAKEOFF POWER, TAKEOFF POWER WAS SET TO 2.11 EPR AND THE NR 2 ENGINE ONLY CAME UP TO 1.59 EPR. FURTHER ADVANCEMENT OF THROTTLE DID NOT VARY 1.99 EPR , REJECTED TAKEOFF. MAINTENANCE PERFORMED ENGINE TRIM RUNS PESDR AWXA200300273Battery · dischargedFLIGHT CREW REPORTED THAT THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300270Vane · damagedWHEN PREPARING FOR TAKEOFF AT DFW EN ROUTE FOR PHX WHEN THROTTLES ADVANCED RECEIVED COMPRESSOR VANE FAULT. MAINTENANCE REMOVED AND REPLACED THE PRESSURE RATIO BLEED CONTROL IAW T/C R5M75002, AND LUBRICATED THE 13TH STAGE BLEED VALVE IAW BMM 75-31-0, PG. 602.
Back to N182AW, cancelled Mar 9, 2005