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 AWXA200400163Plate · corrodedLCQ - EES - DURING C-15 CHECK CORROSION WAS FOUND IN L-2 DOOR GIRT BAR FITTING ADAPTER PLATE BS 328, LBL 74. MAINTENANCE REMOVED AND REPLACED L-2 DOOR GIRT BAR FITTING ADAPTER PLATE IAW T/C C1D25006.SDR AWXA200400140Skin · crackedDURING C-15 CHECK A .25 INCH CRACK WAS FOUND AT R-2 DOOR UPPER HINGE CUTOUT RUNNING DOWNWARD AND AFT FROM LOWER CORNER BS 328, RBL 65, STR 10 RT, WL 260. MAINTENANCE BLENDED OUT CRACK AT R-2 DOOR UPPER HINGE CUTOUT BS 328, RBL 65, STR 10 RT, WL 260; FABRICATESDR AWXA200400129Skin · crackedLCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON EXISTING REPAIR ON EXTERNAL FUSELAGE SKIN BS 908, STR 27 LT TO STR 28 LT. MAINTENANCE REMOVED EXISTING DOUBLERS AT BS 908, STR 27 LT TO STR 28 LT; PERFORMED A HFEC INSPECTION AND FOUNSDR AWXA200400048Skin · crackedPHX - MAJOR REPAIR - A 2.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN LEFT SIDE OF AIRCRAFT AT STR 24 LEFT BETWEEN BS 927 AND BS 947. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE SKIN AT STR 24 LEFT BETWEEN BS 927 AND BS 947; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKSDR AWXA200400021Bearing · seizedAFTER LANDING & TAXING TO HOLD BAY, SHORTLY AFTER NR 2 ENG SHUTDOWN COCKPIT BEGAN TO DEVELOP AN ACRID ELEC BURNING ODOR FOLLOWED BY LIGHT BLUE SMOKEY HAZE. TURNED OFF GASPER FAN & WINDOW HEAT, ODOR SUBSIDED. MAINT TROUBLESHOT, FOUND FLT DECK CABIN AIR COND FANSDR AWXA200400024Wire · damagedON CLIMBOUT, WHEN AUTOPILOT-B ENGAGED A/C BANKED HARD RT PAST 30 DEGREES. REATTEMPTED TO ENGAGE AUTOPILOT-B SAME RESULTS. AS SOON AS AUTOPILOT-B ENGAGED CONTROL WHEEL STEERING INDICATED ROLL RT, AUTOPILOT-A NORMAL. MAINT TROUBLESHOT AUTOPILOT SYS, B-SYS GOESDR AWXA200301646Light · wornPHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT OVER THE L-2 DOOR FLICKERS ON AND OFF DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY ABOVE THE L-2 DOOR, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301604Light · damagedPHX - EEL - DURING A-01 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 10 LT WAS FOUND HANGING FROM SEAT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH SEAT LIGHT ASSEMBLY AT SEAT ROW 10 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301569Reflector · defectivePHX - EEL - DURING 4-DAY CHECK FOUND THE R-2 DOOR EXTERIOR EMERGENCY ESCAPE LIGHT INOPERATIVE, AFTER BULB REPLACEMENT LIGHT WAS INTERMITTENT. MAINTENANCE REMOVED AND REPLACED R-2 DOOR EXTERIOR EMERGENCY ESCAPE LIGHT REFLECTOR ASSEMBLY. OPERATIONAL CHECK WAS SDR AWXA200301568Reflector · defectivePHX - EEL - DURING 4-DAY CHECK THE RT LOWER EXTERNAL GROUND ILLUMINATION EMERGENCY ESCAPE LIGHT WAS FOUND INOPERATIVE, BULB REPLACEMENT HAD NO EFFECT. MAINTENANCE REMOVED AND REPLACED RT LOWER EXTERNAL GROUND ILLUMINATION EMERGENCY ESCAPE LIGHT REFLECTOR ASSESDR AWXA200301529Light · brokenEN ROUTE TO PHX THE L-2 DOOR EMERGENCY EXIT LIGHT HOUSING AND LENS FELL OFF. MAINTENANCE REMOVED AND REPLACED L-2 DOOR EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301522Battery · dischargedDURING FUNCTIONAL CHECK OF EMERGENCY LIGHT SYSTEM THE EMERGENCY EXIT SIGN ABOVE THE R-2 FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK ABOVE THE R-2 DOOR, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301513Cover · damagedDURING CLIMB OUT OF OAK EN ROUTE FOR PHX A VERY LOUD SQUEALING SOUND WAS OBSERVED COMING FROM THE L-1 DOOR LOWER FORWARD HINGE SEAL, PRESSURIZATION WAS NORMAL, TURNED BACK TO OAK DUE TO LOUD NOISE. MAINTENANCE FOUND THE LOWER HINGE COVER DAMAGED. REMOVED ANDSDR AWX2004F00000Spring · wornEN ROUTE FROM PHX TO ABQ FLIGHT CREW REPORTED RT WING NR 5 SLAT HANGING DOWN APPROXIMATELY 5 INCHES, AIRCRAFT RETURNED TO PHX. MAINTENANCE REMOVED AND REPLACED NR 5 LEADING EDGE SLAT ACTUATOR PER AWA TASK CARD R3M27020, OPERATIONAL AND LEAK CHECK WAS GOOD. FUSDR AWXA200301502Battery · dischargedAUS - EEL - DURING 4-DAY CHECK THE EMERGENCY EXIT SIGN ABOVE THE L-2 DOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT SIGN BATTERIES, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301483Firewall · crackedLCQ - MAJOR REPAIR - DURING C-14 CHECK 5 EACH CRACKS WERE FOUND ON NR 1 ENGINE PYLON FORWARD FIREWALL. MAINTENANCE PERFORMED WELD REPAIR ON FORWARD FIREWALL PAN ASSEMBLY IAW AWA ER 15-5412-03322-SS1.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 AWXA200301476Frame · crackedLCQ - MINOR REPAIR - DURING C-14 CHECK .75 INCH CRACK WAS FOUND IN NR 1 ENGINE FORWARD OUTBOARD COWLING FRAME NR 7 AT PREVIOUS CUTOUT. MAINTENANCE CUTOUT CRACK IN NR 1 ENGINE FORWARD OUTBOARD COWLING FRAME NR 7; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PARSDR AWXA200301475Rib · crackedLCQ - MINOR REPAIR - DURING C-14 CHECK 1.1875 INCH CRACK WAS FOUND IN LT WING LEADING EDGE RIB, INBOARD OF NR 1 ENGINE AT L/E STA 222.7. MAINTENANCE REMOVED CRACKED LT WING LEADING EDGE RIB AT L/E STA 222.7; FABRICATED A NEW REPLACEMENT RIB PER DWG 65-49353; SDR AWXA200301474Rib · crackedLCQ - MAJOR REPAIR - DURING C-14 CHECK .5 INCH CRACK WAS FOUND IN LT WING LEADING EDGE RIB, INBOARD OF NR 1 ENGINE AT L/E STA 222.7. MAINTENANCE REMOVED CRACKED LT WING LEADING EDGE RIB AT L/E STA 222.7; FABRICATED A NEW REPLACEMENT RIB PER DWG 65-49353; INSTSDR 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 AWXA200301484Skin · crackedLCQ - MAJOR REPAIR - DURING C-14 CHECK A CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727, STR 16 RT. MAINTENANCE REMOVED DAMAGED SKIN FROM BS 727 TO BS 777, STR 16 RT; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILLERS, 4 EACH DOUBLERS,SDR 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 AWXA200301301Battery · dischargedFLIGHT CREW REPORTED THE AFT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD.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 AWXA200301289Wire · brokenDURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT WAS FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT, REPAIRED BROKEN WIRE, OPERATIONAL CHECK WAS GOOD.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
Back to Boeing 737-277