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 AWXA200200940Skin · crackedMCN - MAJOR REPAIR - DURING C-13 CHECK EXFOLIATION CORROSION WAS FOUND ON THE FORWARD LAV PAN RING AT BS 275. MAINTENANCE REMOVED EXTERNAL DOUBLER AND LAV PAN RING; FABRICATED A NEW EXTERNAL DOUBLER; INSTALLED REPAIR PART AND LAV PAN RING IAW B737-200 SRM 51-SDR AWXA200200881Skin · crackedMCN - MAJOR REPAIR - DURING C-13 CHECK A 1" CRACK WAS FOUND ON OUTER SKIN NEAR THE R/H MAIN LANDING GEAR WHEEL WELL KEEL BEAM AREA, BETWEEN 2 REPAIR DOUBLERS, BS 707. MAINTENANCE REMOVED DAMAGED SECTION OF OUTER SKIN, FABRICATED A SECTION OF KEEL BEAM OUTER SKSDR AWXA200200867Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-13 CHECK THE OUTBOARD UPPER LEG OF STRINGER CLIP WAS FOUND CRACKED ON THE AFT SIDE OF FRAME 663, STR 11 LT, ABOVE CABIN WINDOW. MAINTENANCE REMOVED DAMAGED STRINGER CLIP AT BS 663, STR 11 LT, FABRICATED A NEW STRINGER CLIP AND INSDR AWXA200200897Frame · crackedMCN - MAJOR REPAIR - DURING C-13 CHECK A 2 1/2" CRACK WAS FOUND ON THE FORWARD CARGO COMPARTMENT FRAME BODY ABOVE STRINGER 21 L/H, BS 480. MAINTENANCE CUTOUT DAMAGED SECTION OF FRAME, REMOVED 3 EACH INTERCOASTALS FOR ACCESS, REMOVED 2 EACH STRINGER TIE CLIPS CSDR AWXA200200896Skin · crackedMCN - MAJOR REPAIR - DURING C-13 CHECK A .25 INCH CRACK WAS FOUND ON THE R2 DOOR EXTERNAL SKIN AT THE LOWER HINGE CUTOUT UPPER AFT CORNER, BS 962. MAINTENANCE TRIMMED OUT DAMAGE AT LOWER HINGE CUTOUT UPPER AFT CORNER AND PERFORMED A HFEC INSPECTION TO VERIFY SDR AWXA200200857Skin · crackedMCN - MAJOR REPAIR - DURING C-13 CHECK A .5 INCH CRACK WAS FOUND ON L1 DOOR INNER SKIN AT UPPER CORNER ACCESS HOLE FOR FOR UPPER END OF VERTICAL TORQUE TUBE. MAINTENANCE REMOVED DAMAGED AREA OF SKIN, FOUND MATERIAL LOSS TO BE WITHIN LIMITS PER B737-200 SRM 5SDR AWXA200200841Switch · defectiveAFTER TAKEOFF NR 5 SLAT REMAINED IN EXTENDED POSITION, DECLARED EMERGENCY, TURNED BACK. MX INSPECTED AND LUBRICATED NR 5 L/E SLAT ROD ENDS & TRACKS IAW BMM 12-22-71. CYCLED FLAPS SEVERAL TIMES, OPERATIONAL CHECK WAS NORMAL. MX WROTE A CRITICAL FOLLOW-UP TO LSDR AWXA200200843Light · damagedPHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200837Keelbeam · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK A .5 INCH CRACK WAS FOUND ON LT KEEL BEAM BETWEEN BS 727 & BS 727A UNDER A PREVIOUS REPAIR. MAINTENANCE TRIMMED OUT DAMAGED AREA OF KEEL BEAM AT BS 727 & BS 727A AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST.SDR AWXA200200824Web · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 2" CRACK WAS FOUND ON TORQUE BOX WEB AT BS 1138 L/H. MAINTENANCE CUTOUT DAMAGE AT TORQUE BOX WEB, FABRICATED A REPAIR DOUBLER, AND INSTALLED REPAIR IAW B737-200 SRM 51-40-2, PG. 1-3, FIG. 1, SRM 51-10-2, PG.7 & 32, FIG.SDR AWXA200200813Skin · gougedYVR - MAJOR REPAIR - DURING C-20 CHECK THE RT OUTBOARD TRAILING EDGE FOREFLAP FAILED CONDUCTIVITY TEST AFTER REPAIR OF 5 INCH LONG GOUGE FROM A CHAFING PANEL BOLTHEAD. MAINTENANCE REMOVED DAMAGED RT OUTBOARD TRAILING EDGE FOREFLAP SKIN, FABRICATED NEW REPLACESDR AWXA200200781Skin · crackedSJC - MAJOR REPAIR - DURING ROUTINE INSPECTION RAMPER FOUND A 4.25 INCH CRACK 8 FT AFT OF THE AFT CARGO DOOR, APPROXIMATELY 20 INCHES UP FROM RT SIDE OF CENTER BELLY, BS 940, STR 18 RT. MAINTENANCE CUT OUT DAMAGED AREA OF SKIN AND PERFORMED A HFEC INSPECTION SDR AWXA200200775Wire · brokenPHX - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHT SEAT ROW 10 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT SEAT ROW 10 L/H, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200782Circuit Board · burned outPHX - AIR TURN BACK - FLT 0620 - ON TAKEOFF FROM PHX EN ROUTE TO OAK FIRST OFFICERS AIRSPEED INDICATOR FROZE AT 60 KTS, REMAINED AT 60 KTS AFTER TAKEOFF, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE TROUBLESHOT AND REPLACED THE NR 2 AIR DATSDR AWXA200200806Intercostal · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON INTERCOSTAL IN THE AFT CARGO COMPARTMENT AT BS 800, RBL 43, WL 164. MAINTENANCE REMOVED DAMAGED INTERCOSTAL AT BS 800, RBL 43, WL 164. FABRICATED A NEW REPLACEMENT INTERCOSTAL, AND INSTALLEDSDR AWXA200200743Light · inoperativePHX - EEL - DURING INSPECTION THE LT OVERWING EMERGENCY EXIT DOOR LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY EXIT DOOR LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200836Light · brokenYVR - EEL - DURING C-20 CHECK THE AFT SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND BROKEN. REPLACED AFT SERVICE DOOR EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200831Floorbeam · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND IN THE UPPER FLANGE OF LONGITUDINAL FLOORBEAM AT RBL 45 APPROXIMATELY 2 INCHES FROM BS 727B, WL 208.1. MAINTENANCE CUT OUT CRACK IN UPPER FLANGE OF LONGITUDINAL FLOORBEAM RBL 45 AND PERFORMED HSDR AWXA200200795Frame · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 3/4" CRACK WAS FOUND ON THE R-1 DOOR FRAME AT INBOARD LOWER END, BS 300, RBL 55. MAINTENANCE REMOVED DAMAGED SECTION OF R-1 DOOR LOWER FORWARD STUB BEAM FRAME AND FOUND SILL CLIP ALSO CRACKED. REMOVED SILL CLIP, FABRICASDR AWXA200200820Web · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK HFEC INSPECTION INDICATED A 7/8" CRACK ON VERTICAL PRESSURE BEAM AT BS 663, RBL 32, WL 199. MAINTENANCE TRIMMED OUT DAMAGE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED 2 EACH REPAIR DOUBLERS, AND SDR AWXA200200770Stringer · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON THE UPPER AFT END OF STRINGER 26 R/H, BS 380 (E&E COMPARTMENT). MAINTENANCE REMOVED 1 EACH STRINGER SPLICE BS 360, 2 EACH STRINGER CLIPS BS 360 & BS 380, AND CUTOUT DAMAGED SECTION OF STRINGER BS 3SDR AWXA200200805Web · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON R-2 DOOR INTERCOSTAL WEB AT BS 954, WL 252. MAINTENANCE REMOVED 3 STRAPS AND CRACKED INTERCOSTAL WEB AT BS 954, WL 252. FABRICATED A NEW INTERCOSTAL WEB, AND INSTALLED NEW WEB AND 3 STRAPS ISDR AWXA200200698Light · brokenPHX - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT WAS FOUND BROKEN OFF. MAINTENANCE REMOVED AND REPLACED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200810Bracket · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND ON THE L-1 DOOR LINER LOWER PAN FORWARD SUPPORT BRACKET AT BS 312. MAINTENANCE REMOVED DAMAGED LOWER PAN FORWARD SUPPORT BRACKET AT BS 312, FABRICATED A NEW BRACKET PER DWG 65-49649, AND INSTALLED REPAIRSDR AWXA200200803Angle · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1/2" CRACK WAS FOUND ON TOP OF CABIN FLOOR BEAM SUPPORT ANGLE BS 344, LBL 12, WL 206. MAINTENANCE REMOVED DAMAGED FLOOR BEAM SUPPORT ANGLE BS 344, LBL 12. FABRICATED A NEW FLOOR BEAM SUPPORT ANGLE, AND INSTALLED REPAIRSDR AWXA200200823Shear Tie · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON THE AFT CARGO PIT FLOOR FRAME ON TOP OF THE FORWARD LEG OUTBOARD SIDE, INBOARD OF STR 27 L/H, WL 149, BS 807. MAINTENANCE REMOVED STIFFNER, STRINGER CLIP, AND CUTOUT DAMAGED SKIN ATTACHMENT (SHEAR TSDR AWXA200200822Stringer · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON CENTER INBOARD SIDE OF STRINGER 22 L/H, AFT OF DOME PLATE NUT AND ABOVE EMERGENCY LIGHT ASSEMBLY AT BS 776. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. CUTOUT DASDR AWXA200200821Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1/16" CRACK WAS FOUND ON EXTERNAL FUSELAGE SKIN EXTENDING FROM FASTENER HOLE AT BS 303, STR 17 R/H, WL 210. MAINTENANCE CUTOUT DAMAGED SKIN AND BONDED DOUBLER AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FSDR AWXA200200819Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION WAS FOUND ON THE UPPER SURFACE OF TEE CHORD AT BS 986, LBL 21 TO RBL 40, WL 208. MAINTENANCE BLENDED DAMAGED SECTION OF TEE CHORD, MATERIAL LOSS OUT OF LIMITS. REMOVED FLOOR SUPPORTS BS 966 TO BS 986.5, AND SDR AWXA200200765Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF TEE CHORD BS 967, RBL 27 - 41, WL 208. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED TEE CHORD BS 967 FROM BL 0 TO RBL 43. FABRISDR AWXA200200802Floorbeam · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 2.7 INCH CRACK WAS FOUND ON THE LOWER SIDE OF FLOORBEAM UPPER CHORD AT BS 663, RBL 24, WL 202; VERIFIED BY HFEC INSPECTION. MAINTENANCE REMOVED CRACKED SECTION OF UPPER CHORD BS 663, RBL 24, WL 202. FABRICATED 2 REPAISDR AWXA200200767Stringer · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON BOTH SIDES OF STRINGER 26 R/H BETWEEN BS 887 AND BS 927. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED STRINGER 26 R/H FROM BS 885 TO BS 917, REMOVED TSDR AWXA200200692Shuttle Valve · faultySLC - EMERGENCY LANDING - FLT 0454 - ON SHORT FINAL APPROACH AT SLC EN ROUTE FROM PHX LOST A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE. AIRCRAFT SHUT DOWN AND TOWED TO GATE. MAINTENANCE FOUND THE NR 1 THRUST REVERSER SHUTTLE VALVE HAD A BLOWN PLUG, REMOVED AND SDR AWXA200200834Frame · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1/2" CRACK WAS FOUND IN THE AFT CARGO DOORWAY FORWARD DOOR CUTOUT FRAME BS 827, RBL 43, WL 164. MAINTENANCE REMOVED THE THRESHOLD WEB, CLIP FROM STRINGER 27 R/H, INTERCOASTAL ASSEMBLY, 3 EACH STIFFNERS, AND THE CRACKEDSDR AWXA200200796Web · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND IN CLOSE OUT WEB AT BS 1005, RBL 43, CORROSION WAS ALSO FOUND ON LOWER SIDE OF SAME WEB AT RBL 44. MAINTENANCE REMOVED THE DAMAGED CLOSE OUT WEB BS 986.5 TO 1016, RBL 44. FABRICATED A NEW CLOSESDR AWXA200200768Intercostal · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON INTERCOSTAL AT BS 500A, STRINGER 25 RT. MAINTENANCE REMOVED INTERCOSTAL FROM BS 500A, STRINGER 25 RT, FABRICATED A NEW INTERCOSTAL PER DWG 69-41473, AND INSTALLED REPAIR IAW B737-200 SRM 51-3SDR AWXA200200848Web · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN THE FORWARD END OF LOWER WEB ON FORWARD CARGO DOOR BS 446, STR 23 RT. MAINTENANCE REMOVED CRACKED SECTION OF WEB, FABRICATED 2 FILLERS, AND INSTALLED REPAIR PARTS IAW EO 52-31-04, FIG 2, PG SDR AWXA200200835Gusset · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1" CRACK WAS FOUND ON GUSSET AT AFT END OF NOSE GEAR ACTUATOR SUPPORT FITTING BS 240, BL 0, WL 190. MAINTENANCE REMOVED NOSE GEAR ACTUATOR SUPPORT FITTING AND THE CRACKED GUSSET BS 240, BL 0, WL 190. FABRICATED A NEW GSDR AWXA200200804Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK .25 INCH CRACKS WERE FOUND ON RT WING LEADING EDGE AT THE NR 6 SLAT CENTER STOP FITTING CUTOUT, WS 557. MAINTENANCE BLENDED OUT CRACKS ON RT WING LEADING EDGE NR 6 SLAT CENTER STOP CUTOUT IAW AWA ER 15-5741-02232-SS1.SDR AWXA200200801Web · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 3/8" CRACK WAS FOUND ON THE NOSE LANDING GEAR ACTUATOR SUPPORT BEAM WEB EXTENDING FROM UPPER CENTER RIVET HOLE, HFEC INSPECTION CONFIRMED CRACK. MAINTENANCE REMOVED NOSE LANDING GEAR ACTUATOR SUPPORT BEAM AND WEB, FABRISDR AWXA200200791Door Frame · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND L-1 DOOR FRAME CUTOUT FORWARD LOWER STOP FITTING ATTACH PLATE WEB DOUBLER, BS 294.5, STR 16 LT. MAINTENANCE REMOVED THE L-1 DOOR FORWARD LOWER STOP FITTING ATTACH PLATE; REMOVED CLOSE OUT ANGLE SDR AWXA200200790Longeron · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK THE #1 ENGINE FIXED FAIRING LOWER END "Z" ANGLE WAS FOUND CRACKED BETWEEN 1ST AND 2ND ATTACH FITTINGS FROM THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE LOWER END "Z" ANGLE ON THE #1 ENGINE FIXED FAIRING IAW B737-SDR AWXA200200789Angle · brokenMCN - MAJOR REPAIR - DURING C-18 CHECK A "T" ANGLE CLIP WAS FOUND BROKEN ON INBOARD SIDE OF THE #1 ENGINE FIXED FAIRING BETWEEN 2ND AND 3RD ATTACH FITTINGS FROM THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE "T" ANGLE CLIP ON INBOARD SIDE OF THE #1 ENGISDR AWXA200200788Angle · brokenMCN - MAJOR REPAIR - DURING C-18 CHECK A "T" ANGLE CLIP WAS FOUND BROKEN ON INBOARD SIDE OF THE #2 ENGINE FIXED FAIRING BETWEEN 2ND AND 3RD ATTACH FITTINGS FROM THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE "T" ANGLE CLIP ON INBOARD SIDE OF THE #2 ENGISDR AWXA200200769Plate · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FORWARD CORNER SCUFF PLATE. MAINTENANCE PREPARED, TREATED, AND WELDED THE CRACK ON FORWARD CORNER SCUFF PLATE IAW AWA ER 15-5333-01016-JS2.SDR AWXA200200764Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4" CRACK WAS FOUND ON L-1 DOOR INTERNAL SKIN AT THE AFT UPPER CORNER DOOR STOP ADJUSTMENT CUTOUT, BS 346. MAINTENANCE CUTOUT CRACK AT L-1 DOOR AFT UPPER CORNER DOOR STOP ADJUSTMENT CUTOUT, BS 346. FABRICATED REPAIR DOSDR AWXA200200750Angle · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1" CRACK WAS FOUND ON FLOOR BEAM SUPPORT ANGLE BS 400, BL 0. MAINTENANCE REMOVED DAMAGED FLOOR BEAM SUPPORT ANGLE AT BS 400, BL 0. FABRICATED A NEW FLOOR BEAM SUPPORT ANGLE, AND INSTALLED REPAIR IAW B737-200 SRM 51-30-2SDR AWXA200200686Light · inoperativeLAS - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 6 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 6 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200201046Skin · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK THE R/H WING INBOARD FORE FLAP WAS FOUND TO HAVE DELAMINATION ON UPPER SKIN 6" INBOARD OF THE #3 FORE FLAP TRACK. MAINTENANCE CUTOUT DELAMINATED AREA OF SKIN ON R/H WING INBOARD FORE FLAP; BONDED AND POTTED REPAIR CORE; FSDR AWXA200200766Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4" CRACK WAS FOUND ON R-1 DOOR EXTERNAL SKIN AT UPPER AFT CORNER OF HINGE CUTOUT, CONFIRMED BY HFEC INSPECTION. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN AT R-1 DOOR UPPER AFT CORNER OF HINGE CUTOUT AND PERFORMED HFEC I
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