N181AW, cancelled Jun 14, 2002
Service difficulty reports · 115
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 = 'N181AW' AND deregistration_id = 'N181AW-2002-06-14' 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 = 'N181AW' AND deregistration_id = 'N181AW-2002-06-14' 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 AWXA200200064Battery Pack · dischargedPHX - EEL - C - DURING INSPECTION THE RT EXTERIOR OVERWING AND LOWER FUSELAGE EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BATTERY PACK IN THE AFT CARGO COMPARTMENT IAW BMM 33-51-31, OPERATIONALSDR AWXA200100458Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB, LBL 4.8, WL 187.2 TO 188 HAS A .8 INCH CRACK CONFIRMED WITH HFEC. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS AND INSTALLED IAW B737 SRM 53-10-11 AND TEMP REV 53-52.SDR AWXA200100456Frame · crackedMCN - C21 CK - C - MAIN CABIN SUB FLOOR PRESSURE DECK FWD CHORD BS 663.75, LBL 24, WL 202 CRACKED 3.5 INCH. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW AWA ER 15-5312-01238-GF1.SDR AWXA200100455Stringer · crackedMCN - C21 CK - "C" - WHILE INVESTIGATING POSSIBLE CORROSION AROUND FASTENERS AT BS 727 + 17, STR 27L TO 27R, FOUND A 3" CRACK IN STR 27R. NOTE; NO CORROSION WAS FOUND. MAINTENANCE REMOVED CRACKED SECTION OF STR 27R AND INSTALLED REPAIR IAW B737 SRM 53-10-6.SDR AWXA0002208Web · crackedD: Frame web cracked 3 ea places at fastener holes, BS 639, RBL 65, WL 206C: Removed cracked web, drilled and installed new web IAW B737 200 SRM 51-40-2 at BS 639, RBL 65, wl 206SDR AWXA200100468Skin · chafedMCN - C21 CK - C - LT WING, I/B FLIPPER FLAP LOWER O/B SKIN CHAFED BEYOND LIMITS. MAINTENANCE REMOVED THE LOWER SKIN PANEL, FABRICATED AND INSTALLED NEW LOWER SKIN PANEL IAW AWA ER 15-5752-01249-DL4.SDR AWXA200100464Stiffener · crackedMCN - C21 - C - BS 178 PRESS BULKHEAD WEB, AFT SIDE, VERT TEE CRACKED 1 INCH ON I/B SIDE, WL 184 TO 185, LBL 5.7, FOUND VISUALLY AND CONFIRMED BY HFEC. MAINTENANCE CUT OUT DAMAGED AREA OF VERT TEE AND FORMED REPAIR ANGLES, STRAPS AND FILLERS AND INSTALLED REPSDR AWXA200100457Bulkhead · crackedC21 CK - C - AFT SIDE OF BS 178 PRESS BULKHEAD CENTER WEB HAS A .5 INCH CRACK AT LBL .7, WL 203 TO 203.5, CONFIRMED WITH HFEC. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS AND INSTALLED REPAIR IAW B737 SRM 53-10-11, PG 83 & 84 AND TSDR AWXA200100469Floorbeam · corrodedMCN - C21 CK - C - BS 967 FLOORBEAM UPPER FLANGE CORRODED IN 4 PLACES BETWEEN LBL 22 AND RBL 49, BEYOND SRM LIMITS. MAINTENANCE REMOVED THE FLOORBEAM UPPER CAP AND FABRICATED AND INSTALLED NEW UPPER CAP IAW B737 SRM 53-10-9, FIG 2, PG 7 - 11.SDR AWXA200100467Floorbeam · corrodedMCN - C21 CK - C - FLOORBEAM BS 986.5, LBL 44 TO RBL 49 HAS CORROSION IN SEVERAL PLACES ON UPPER FLANGE. MAINTENANCE REMOVED THE FLOORBEAM UPPER CAP FROM LBL 44 TO RBL 49 AND FABRICATED NEW UPPER CAP SECTION AND INSTALLED IAW B737 SRM 53-10-9 FIG 2 PG 7 - 11.SDR AWXA200100471Frame · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD 1.7 INCH CRACK CENTER OF RADIUS, RT CHORD, WL 207, RBL 24. MAINTENANCE REMOVED AND REPLACED THE RT SIDE CHORD IAW AWA ER 15-5311-01242-TB2.SDR AWXA200100470Web · crackedMCN - C21 CK - C - RT COCKPIT FLOOR WEB CRACKED 1 INCH AT CUTOUT, BS 180, WL 207, RBL 24. MAINTENANCE REMOVED THE FLOOR WEB, FABRICATED AND INSTALLED NEW FLOOR WEB IAW AWA ER 15-5311-01234-TR1.SDR AWXA200100466Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A 1 INCH CRACK, WL 227.7 TO 228.7, RBL 6.4, BELOW REINFORCEMENT, FOUND WHILE PERFORMING ULTRASONIC INSPECTION. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REPAIR SDR AWXA200100465Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB .7 INCH CRACK, WL 218, RBL 11.7 TO RBL 12.7, BELOW REINFORCEMENT DETECTED BY ULTRASONIC INSPECTION. MAINTENANCE CUT OUT DAMAGED AREA OF WEB AND FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW B737 SRMSDR AWXA200100460Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A 1 INCH CRACK AT LBL 6.6, WL 221.5 TO WL 222.5 BELOW REINFORCEMENT AS DETERMINED WITH ULTRASONIC INSPECTION. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS AND INSTALLED REPAIRSDR AWXA200100459Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A .8 INCH CRACK AT LBL 9.2 TO LBL 10, WL 218, UNDER REINFORCEMENT AS DETERMINED WITH ULTRASONIC INSPECTION. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS AND INSTALLED REPAIR IASDR AWXA200100454Skin · crackedC-21 CK - C - L-1 DOOR CUTOUT FUSELAGE SKIN LOWER EDGE BS 338.5 CRACKED .0625 INCH AT SILL PLATE ATTACH HOLE. MAINTENANCE REAMED CRACKED FASTENER HOLE, DRILLED AND INSTALLED REPAIR DOUBLER AT L-1 DOOR CUTOUT LOWER EDGE, BS 338.5 PER AWA ER 15-5300-01234-DD1.SDR AWXA200100463Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A .75 INCH CRACK, WL 234, RBL 10, FWD SIDE AT A FASTENER HOLE, AS DETERMINED WITH HFEC. MAINTENANCE CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW B737 SRM 53-10-11, PG 1SDR AWXA200100461Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A .5 INCH CRACK, WL 234, LBL 10 AT A FASTENER HOLE AS DETERMINED WITH HFEC. MAINTENANCE CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REPAIR PARTS IAW AWA ER 15-5312-01249-DSDR AWXA200100462Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB, AFT SIDE HAS A 1 INCH CRACK, LBL .7, WL 185 FOUND VISUALLY AND CONFIRMED WITH HFEC. MAINTENANCE CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REPAIR PARTS IAW B737 SRM 53-10-11SDR AWXA200100453Shear Tie · corrodedMCN - C-21 CK - "C" - FUSELAGE SKIN BULGE AND CUPPED FASTENERS IN SKIN AT BS 977, BETWEEN STR 23R TO 24R. MAINTENANCE REMOVER FASTENERS IN SKIN, NO CORROSION FOUND ON FUSELAGE SKIN, HOWEVER FOUND SHEAR TIE CORRODED BS 965, RBL 20. REMOVED AND REPLACED SHEAR TISDR AWXA0001337Packing · brokenINFLIGHT NR 2 ENGINE OIL PRESSURE DROPPED BELOW THE RED RADIAL; THE CREW ACCOMPLISHED ENGINE SHUTDOWN PER THE ORH, RETURNED TO OAK. THE ENGINE WAS SHUTDOWN FOR 25 MIN WITH WINDMILLING OIL PRESSURE OF 20 PS. IN OAK THE OIL PRESSURE TRANSMITTER AND OIL PRESSURSDR AWXA0001338Packing · brokenIN PHX OIL PUMP WAS REPLACED. UPON REMOVAL THE CENTER O-RING WAS FOUND TO BE BROKEN. THE OTHER 2 WERE OK. PUMP WAS REPLACED THOUGH IT APPEARED TO BE NORMAL.SDR AWXA0000744Skin · dentedC-CHECK, LEFT INBD MID FLAP L/E HAS DENT THAT IS OUT OF LIMITS. REMOVED DAMAGE IAW 737 SRM 57-50-4 FIG 3, FABED REPAIR PARTS IAW SRM 57-50-4, AND INSTALLED REPAIR IAW SRM 57-50-4 AND 51-30-2.SDR AWXA0000743Skin · crackedC-CHECK, .5 INCH CRACK IN FUSELAGE SKIN AT TOP OF CAPTAINS NR 1 WINDOW OUTBOARD UPPER CORNER CUTOUT. REMOVED DAMAGE IAW 737 SRM 53-10-01 FIG 210, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW 737 SRM 53-10-1 FIG 210 AND ER 15-5330-00272-JS1.SDR AWXA0000742Web · crackedC-CHECK, CABIN SUB FLOOR STA 664 LBL 35 PRESSURE DECK HAS CRACK. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS (FILLER AND DOUBLER), AND INSTALLED REPAIR IAW ER 15-5710-00273-SSI, 737 SRM 51-30-2, AND 51-30-0.SDR AWXA0000741Skin · damagedC-CHECK, AFT CARGO DOOR HAS TEMP REPAIR, REFER TO AWA ER 15-5361-00210-JS2A, ALLOY STEEL FASTENERS TO BE REPLACED WITH A286 CRES FASTENERS. REMOVED DOOR WEB AND BRACKET IAW 737 SRM 51-30-2, REMOVED AND REPLACED FASTENERS IAW AWA ER 15-5361-00210-JS2A, REINSTSDR AWXA0000740Floor Support · crackedC-CHECK, THREE CRACKS IN LEFT SIDE VERTICAL WEB OF FLOOR SUPPORT AT STA 717, 724, AND 725, BL 0. REMOVED DAMAGE SECTION OF WEB IAW ER 15-B700-00274-JS4, FAB''D AND INSTALLED REPAIR PARTS IAW ER 15-5700-0027.SDR AWXA0000739Web · crackedC-CHECK, WEB AT STA 351.2 STR 20L CRACKED IN TWO PLACES AT E & E BAY. REMOVED DAMAGED WEB IAW 737 SRM 51-30-2, FAB''''D REPLACEMENT WEB IAW DWG 65-458-92, INSTALLED REPLACEMENT WEB IAW 737 SRM 51-30-2.SDR AWXA0000738Skin · crackedC-CHECK, FUSELAGE SKIN BETWEEN BS 727 AND 767, STR 14R TO 20R HAS SEVERAL EXISTING REPAIRS WITH NEW CRACKS IN 3 PLACES. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND SKIN SECTION, INSTALLED SKIN AND SPLICE REPAIR IAW AWA ER 15-5331-00256-DL2.SDR AWXA0000737Web · crackedC-CHECK, AIRSTAIR DOOR INSIDE WEB CRACKED AT AFT UPPER CORNER. REMOVED WEB, CUT OUT DAMAGE, FABRICATED REPAIR WEB, DOUBLER, AND SPLICE, INSTALLED REPAIR PARTS IAW 737 SRM 51-30-2, 51-40-3 FIG 3, AND 51-40-2.SDR AWXA0000736Frame · crackedC-CHECK, FWD CABIN FS 303, STR 17R FRAME IS CRACKED AT LOWER INBD FLANGE. REMOVED DAMAGED AREA, FABED REPAIR PARTS, AND INSTALLED REPAIR PARTS IAW 737 SRM 51-30-2.SDR AWXA0000735Stiffener · crackedC-CHECK, CABIN SUB FLOOR PRESSURE DECK STIFFENER IS CRACKED AT FS 727, RBL 9. REMOVED AND REPLACED STIFFENER (NEW) AT FS 727, RBL 9.SDR AWXA0000734Stiffener · crackedC-CHECK, CABIN SUB FLOOR PRESSURE DECK STIFFENER IS CRACKED AT FS 727, RBL 18. REMOVED AND REPLACED STIFFENER (NEW) IAW 737 SRM 51-30-2.SDR AWXA0000733Frame · crackedC-CHECK, SIDE CHORD CRACKED AT FS 178, WL 195 AND WL 207. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED SIDE CHORD, SPLICE ANGLE AND STRAPS IAW SB 737-53A-1028 AND ER 15-5310-00274-JS5.SDR AWXA0000731Bulkhead · crackedC-CHECK, FWD PRESSURE BULKHEAD CENTER WEB HAS 7 INCH CRACK BEHIND I/B FLANGE OF ANGLE STIFFENER AT FS 178, LBL 5 - 7, WL 226. REMOVED DAMAGE IAW 737 SRM 53-10-11 FIG 1, FAB''D REPAIR PARTS IAW 737 SRM 53-10-11 FIG 1, AND INSTALLED PARTS IAW 737 SRM 53-10-11.SDR AWXA0000730Bulkhead · crackedC-CHECK, BULKHEAD CENTER WEB CRACKED AT FS 178, LBL 5.5, WL 200. CUT OUT DAMAGED AREA IAW 737 SRM 53-10-11, FAB''D REPAIR PARTS IAW SRM 53-10-11 FIG 1, INSTALLED REPAIR PARTS IAW SRM 51-30-2.SDR AWXA0000729Skin · damagedC-CHECK, FUSLAGE HAS CREASE THAT IS OUT OF LIMITS AT FS 1110, STR 14R. CUT OUT DAMAGED AREA IAW 737 SRM 51-30-2, FABED REPAIR DOUBLER AND PARTS IAW 737 SRM 51-30-3, INSTALLED REPAIR PARTS IAW 737 SRM 51-30-2.SDR AWXA0000728Intercostal · crackedC-CHECK, INTERCOSTAL CRACKED AT FS 180, LBL 26, WL 195. REMOVED DAMAGED INTERCOSTAL IAW 737 SRM 53-10-11, FABED REPAIR PARTS PARTS IAW 737 SRM 53-10-16, INSTALLED REPAIR PARTS IAW 737 SRM 51-30-0.SDR AWXA0000727Skin · damagedC-CHECK, SEALANT BLOWN OUT OF EXISTING REPAIR AT FS 907 APPROX STR 22R. REMOVED OLD REPAIR IAW 737 SRM 51-40-02, FAB''D REPAIR PARTS IAW 53-30-3 FIG 28, INSTALLED REPAIR PARTS IAW 51-40-8 AND 53-30-3 FIG 28.SDR AWXA0000726Skin · dentedC-CHECK, FUSLAGE SKIN DENTED BEYOND LIMITS ABOVE DOOR L-1 (A=.7, Y=.05, AY=14). CUT OUT DAMAGED AREA IAW 737 SRM 53-30-5 FIG 3. REWORKED AREA AND INSTALLED DOUBLER IAW 737 SRM 51-30-1, 51-30-2, AND 53-30-3 FIG 1.SDR AWXA0000725Shear Tie · crackedC-CHECK, SHEAR TIE CRACKED AT FS 400 STR 14R. REMOVED DAMAGED SECTION IAW 737 SRM 51-10-1, FABED SHEAR TIE IAW 737 SRM 53-10-4, INSTALLED REPAIR PARTS IAW 737 SRM 53-10-4.SDR AWXA0000724Skin · gougedC-CHECK, FUSELAGE SKIN GOUGED OUT OF LIMITS AT AC GROUND SERVICE DOOR LT SIDE. CUT OUT DAMAGE IAW AWA ER 15-5243-00256-DL1, TREATED IAW 737 SRM 51-10-02.SDR AWXA0000723Stringer · crackedC-CHECK, CRACKED STRINGER AT 500B, STR 16L, FORWARD OF WING ANTI ICE. REMOVED DAMAGED AREA, FABED REPAIR PARTS, AND INSTALLED REPAIR PARTS IAW AWA ER 15-5314-00255-DL1.SDR AWXA0000722Seat Track · gougedC-CHECK, SEAT TRACK GOUGED AT FS 340, RBL 25. REMOVED, FAB''D REPLACEMENT TRACK AND INSTALLED SEAT TRACK IAW 737 SRM 53-10-5 FIG 2.SDR AWXA0000506Skin · crackedCARGO LOADER STRUCK AIRCRAFT AT AFT CARGO DOOR SURROUND STRUCTURE. TEMP REPAIRED IAW ER 15-5361-00210-JS2A, INSPECTION REQUIRED AT EVERY C-CHECK, NOT TO EXCEED 4,500 FLT CYCLES.SDR AWXA0000274Battery Pack · inoperativeNON ROUTINE, EMERGENCY LIGHTS INOP ON LAST SIX LT SEAT ROWS. REMOVED AND REPLACED BATTERY PACK AT ROW 17 ABC, OP CK GOOD. RECOMMENDATION: REMAIN OPEN, MONITOR -- AIRCRAFT HAS SEVERAL DISCREPANCIES IN THIS AREA FOR WIRE REPAIRS AND BATTERY REPLACEMENTS.SDR AWXA0000273Sign · inoperativeNON ROUTINE, R-2 EXIT SIGN WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXIT SIGN ASSEMBLY, OPS CK GOOD.SDR AWXA9900488Wire · brokenSEAT EMERGENCY EXIT LIGHT INOP AT ROW 17 LT. REPAIRED BROKEN WIRE UNDER SEAT, OPS CK NORMAL.SDR AWXA9900294Angle · crackedC-CHECK, FLOORBEAM ATTACH ANGLE TO FUSELAGE AT STA 598 WL 208 LT CUSP LINE CRACK STR 17L. REMOVED, FABRICATED, AND INSTALLED REPAIR PARTS PER AWA ER 2-53-15-86 + SB 737-53-1061.
Back to N181AW, cancelled Jun 14, 2002