Boeing 737-277
Service difficulty reports · 1,584
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '737277' 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 aircraft_model_key = '737277' 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 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 AWXA0001253Battery Pack · inoperativeDURING SCHEDULED INSPECTION FOUND EMERGENCY LIGHTS OUT IN THE FIRST CLASS CABIN. REPLACED POWER SUPPLY FOR THE FIRST CLASS CABIN EMERGENCY LIGHTS. OPS CHECK OK.SDR AWXA0001243Bushing · damagedNR 2 ENG LOW OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT. CREW SHUT ENGINE DOWN AND COMPLETED CHECK LIST. THE ENGINE MAINTAINED POSITIVE OIL PRESSURE THROUGHOUT THE FLIGHT; ENGINE WINDMILLED 25 - 30 MINUTES. MAINTENANCE FOUND THE HSG PLUG BUSHING THREADS DAMAGSDR AWXA0001230Bearing · wornON LANDING FLARE IN SFO THE ELEVATOR CONTROL WAS STIFF. PERFORMED OPERATIONAL AND VISUAL INSPECTION OF ELEV CONTROL SYSTEM, NO DEFECTS NOTED. DUE TO PRIOR REPORT OF STIFF ELEV; BOEING WAS CONSULTED; PER THEIR RECOMMENDATION THE ELEV TORQUE TUBE BEARINGS WERESDR AWXA0001158Light · brokenSEATS 17C AND 18C ESCAPE PATH LIGHTS BROKEN. REMOVED AND REPLACED LIGHT ASY AT 17C; REATTACHED ESCAPE PATH LIGHT ASSY AT 18C; BOTH FUNCTIONALLY CHECK GOOD.SDR AWXA0001155Light · brokenEMERGENCY ESCAPE PATH LIGHT BROKEN OFF SEAT ROW 6. INSTALLED NEW LIGHT AND OPS CHECK GOOD.SDR AWXA0001116Wire · chafedD: PHX - AIR TURNBACK - NR 1 START VALVE LIGHT ILLUMINATED IN FLIGHT AT 250 KTS. 18000 FEET; WENT THROUGH QRH AND SHUTDOWN THE ENGINE; START VALVE OPEN LIGHT EXTINGUISHED WHEN THE ENGINE WAS SHUT DOWN. REMOVED AND REPLACED THE START VALVE; DURING START VALVE RSDR AWXA0001045Frame · crackedBS 178 WL 207 BULKHEAD L/H O/B SIDE CHORD CRACKED. CHORD REPLACED IAW SRM 51-10-01 DWG 65-16300SDR AWXA0001044Intercostal · crackedSTA 178 WL 207 LBL 28 LT O/B WEB CRACKED AT RIVET HOLE. WEB REPLACED IAW SRM 51-10-01 DWG 65-45833SDR AWXA0001043Attach Angle · crackedRT O/B ANGLE AT STA 178 WL 195 RBL 25 CRACKED IN RADIUS. ANGLE REPLACED IAW SRM 51-10-01 DWG 65-16300SDR AWXA0001042Attach Angle · crackedLEFT OUTBOARD T CHORD AT STA 178 WL 195 LBL 24.67 WAS CRACKED. ATTACHED ANGLES REPLACED IAW SRM 51-10-01 DWG 65-16300SDR AWXA0001041Bulkhead · crackedFWD PRESSURE BULKHEAD HAS TWO CRACK INDICATIONS ON WEB AT STA 178 WL 218 BEHIND STIFFENERS L&R OF BL 0. WEB CRACKS REPAIRED IAW SRM 53-10-11 FIG 1 DET. III.SDR AWXA0001040Frame · crackedSTA 178 WL 200 RBL 26 SIDE CHORD CRACKED. CHORD REPLACED IAW SRM 51-10-01 DWG 65-16300SDR AWXA0001039Intercostal · crackedINTERCOSTAL AT BS 178 WL 207 RBL 26 CRACKED. REPLACED WEB/INTERCOSTAL IAW SRM 51-10-01 DWG 61-45833SDR AWXA0001038Floorbeam · crackedOUTBOARD T-CHORD AT STA 178 WL 207 IS CRACKED THROUGH AT FWD FASTENER HOLE. REPAIRED IAW SRM 51-40-4 FIG 1 DWG 65-45833SDR AWXA0001037Skin · crackedCRACK INDICATION ON FUSELAGE APPROX BS 747 STR 17R. REPAIR CARRIED OUT IAW ENG. REPAIR NO. 15-5331-00334-J51SDR AWXA0001036Bracket · crackedSTA 178 GLIDE SLOPE ANTENNA SUPPORT BRACKET LOWER LT CORNER CRACKED. STOP DRILLED END OF CRACK AND REPAIRED IAW SRM 51-40-3SDR AWXA0000882Plate · bentEXTREMELY LOUD AIR RUSHING NOISE AT L1 DOOR. PRESSURIZATION NORMAL, AIRCRAFT RETURNED TO PHX. FOUND LOWER HINGE FLAP SEAL PLATE BENT AND NOT SEATING PROPERLY. REPLACED FLAP SEAL ASSEMBLY.SDR AWXA0000850Skin · crackedC-CHECK, FUSELAGE SKIN DAMAGED AT FS 294, STR 14L, 7 INCHES ABOVE LOWER DOOR HINGE CUTOUT. REMOVED EXISTING DOUBLER AND SKIN PANEL, FAB''D REPLACEMENT REPAIR DOUBLER AND REPAIR KIT IAW 737 SRM 51-30-3 FIG 31, SRM 51-30-2, AND SRM 51-30-8 IN REF BOE SB 737- SDR AWXA0000849Web · crackedC-CHECK, STA 1138, STR 5R FRAME WEB CRACKED AT SKIN ATTACH ANGLE. REMOVED SHEAR TIE WEB, FABBED AND INSTALLED REPAIR PARTS IAW 737 SRM 51-30-2.SDR AWXA0000848Skin · crackedC-CHECK, MULTIPLE CRACKS AND REPAIRS ON FUSLAGE SKIN AT STA 727 TO 787, STR 15R TO 20R. REMOVED DAMAGED SECTION OF SKIN, FABBED AND INSTALLED REPLACEMENT SKIN AND REPAIR PARTS IAW AWA ER 15-5331-00283-DL1.SDR AWXA0000847Web · crackedC-CHECK, KEEL BEAM AT FS 706, INTERNAL WEB LIGHTENING HOLE CHAFED FROM LOOSE DUCT INSULATION. TRIMMED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW 737 SRM 51-30-2 AND DWG 65-45866.SDR AWXA0000846Web · crackedC-CHECK, CRACK EMANATING FROM FASTENER HOLE IN WEB AT STA 1145, STR 5R. CUT OUT DAMAGED AREA IN WEB IAW 737 SRM 51-40-2 FIG 1, FABBED REPAIR DOUBLER AND FILLER, INSTALLED IAW 737 SRM 51-40-2.SDR AWXA0000845Angle · crackedC-CHECK, ATTACH ANGLE CRACKED AT APPROX 683 RT WING OUTBOARD OF AILERON TRAILING EDGE. REMOVED AND REPLACED CRACKED ATTACH ANGLE IAW 737 SRM 51-30-2, FABBED REPLACEMENT PART IAW DWG 65-63461 AND 737 SRM 51-20-1.SDR AWXA0000844Stringer · corrodedC-CHECK CORROSION LVL 2, STRINGER CORRODED AT FS 907, STR 20L. REMOVED AND REPLACED STRINGER SPLICE IAW 737 SRM 51-30-2.SDR AWXA0000843Web · crackedC-CHECK, CRACK IN HORIZ WEB FLOOR STRUCTURE JUST AFT OF BS 178 BULKHEAD, WL 208, RBL 30. WEB REPLACED ON NR 5323254 BY COMPLIANCE OF AWA EO 53-12-07 (STA 178 BULKHEAD MOD).
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