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 AWXA200200763Attach Angle · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1 1/2" CRACK WAS FOUND ON WEB UPPER CHORD (ATTACH ANGLE) AT FASTENER HOLES BS 500B TO BS 520, BL 0, WL 208.1. MAINTENANCE REMOVED WEB UPPER CHORD BS 500B TO BS 520, FABRICATED A REPAIR ANGLE AND INSTALLED REPAIR IAW DWGSDR AWXA200200797Skin · damagedYVR - MAJOR REPAIR - DURING C-20 CHECK FUSELAGE SKIN WAS FOUND TO REQUIRE REPLACEMENT DUE TO NUMEROUS REPAIR PATCHES, BS 727 - 908, STR 14 - 20 LT. MAINTENANCE CUT OUT SKIN BS 727 - 908, STR 14 - 20 LT. AFTER THE SKIN WAS REMOVED FOUND 2 CRACKED TIE CLIPS ATSDR AWXA200200748Door Frame · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK A .125 INCH CRACK WAS FOUND ON THE FORWARD ENTRY DOOR CUTOUT FRAME AT BS 312, STR 6 LT. MAINTENANCE BLENDED OUT CRACK ON FORWARD ENTRY DOOR CUTOUT FRAME AT BS 312, STR 6 LT. HFEC INSPECTION VERIFIED CRACK NO LONGER EXISSDR AWXA200200735Angle · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND ON ANGLE AT THE FORWARD GALLEY DOOR LOWER SILL, BS 294.5. MAINTENANCE REMOVED CRACKED ANGLE AT BS 294.5, FABRICATED A NEW ANGLE PER DWG 69-37402-4, AND INSTALLED REPAIR IAW B737-200 SRM 51-10-01, PGSDR AWXA200200798Shear Tie · corrodedYVR - MAJOR REPAIR - DURING C-20 CHECK CORROSION WAS FOUND ON BELT FRAME SUPPORT ANGLE (SHEAR TIE) IN FORWARD CARGO COMPARTMENT, BS 520, BL 0. MAINTENANCE REMOVED BELT FRAME SUPPORT ANGLE BS 520, BL 0. FABRICATED A NEW BELT FRAME SUPPORT ANGLE, AND INSTALLED RSDR AWXA200200677Battery Pack · dischargedPHX - DURING INSPECTION THE LT EXTERIOR EMERGENCY EXIT LIGHT ON BELLY OF AIRCRAFT, AFT OF THE WING WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT EXTERIOR EMERGENCY EXIT LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200676Battery Pack · dischargedPHX - DURING INSPECTION THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200671Terminal · brokenPHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 6 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE TERMINAL CONNECTOR AT SEAT ROW 6 L/H, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200814Rib · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK CRACKS WERE FOUND ON THE LT AILERON LEADING EDGE RIBS AT THE OUTBOARD END, AND INBOARD OF THE NR 2 HINGE FITTING. MAINTENANCE REMOVED OUTBOARD RIB OF LT AILERON, FABRICATED A NEW RIB, AND INSTALLED REPAIR PER DWG 65-4645SDR AWXA200200809Pressure Panel · chafedYVR - MAJOR REPAIR - DURING C-20 CHECK CHAFING WAS FOUND ON THE RT WHEEL WELL CEILING WEB CAUSED BY CONTACT WITH THE SPOILER RATION MIXER. MAINTENANCE BLENDED OUT DAMAGE PER B737-200 SRM 51-10-6 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRSDR AWXA200200736Web · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND ON THE LOWER WEB OF THE AFT CARGO DOOR FORWARD FUSELAGE FRAME, BS 787. MAINTENANCE REMOVED DAMAGED WEB AT AFT CARGO DOOR FORWARD FUSELAGE FRAME, FABRICATED A NEW WEB, AND INSTALLED REPAIR IAW B737-2SDR AWXA200200734Intercostal · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK A .5 INCH CRACK WAS FOUND ON INTERCOSTAL INNER CHORD BS 360, STR 14 LT. MAINTENANCE REMOVED CRACKED INNER CHORD ANGLE AT BS 360, STR 14 LT. FABRICATED A NEW INNER CHORD ANGLE, AND INSTALLED REPAIR IAW DWG 65-17685-52, ASDR AWXA200200733Intercostal · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK A .75 INCH CRACK WAS FOUND ON INTERCOSTAL BS 294, STR 15 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 294, STR 15 LT. FABRICATED A NEW INTERCOSTAL AND INSTALLED REPAIR IAW DWG 65-17684 AND B737-200 SRM 51-10-01 PG SDR AWXA200200732Intercostal · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK A .375 INCH CRACK WAS FOUND ON INTERCOSTAL BS 294, STR 8 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 294, STR 8 LT. FABRICATED A NEW INTERCOSTAL AND INSTALLED REPAIR IAW DWG 65-17684, AND B737-200 SRM 51-10-01 PG SDR AWXA200200731Doubler · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND ON BELT FRAME DOUBLER BS 303, BETWEEN STRINGERS 16 AND 17 L/H. MAINTENANCE REMOVED CRACKED DOUBLER, FABRICATED A NEW DOUBLER, AND INSTALLED REPAIR IAW DWG 65-17684, AND B737-200 SRM 51-10-1, PG. 8.SDR AWXA200200839Flap · delaminatedYVR - MAJOR REPAIR - DURING C-20 CHECK DELAMINATION OF THE L OUTBOARD FOREFLAP WAS FOUND AT THE INBOARD TRAILING EDGE. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOARD FOREFLAP IAW T/C M3M57004.SDR AWXA200200838Wedge · delaminatedYVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND IN THE R/H INBOARD MID FLAP TRAILING EDGE WEDGE OUTBOARD END POTTING COMPOUND, SKIN WAS ALSO FOUND DEBONDING FROM THE WEDGE AT THE INBOARD TRACK CUTOUT. MAINTENANCE REMOVED DAMAGED WEDGE, FITTED AND INSTSDR AWXA200200816Skin · delaminatedYVR - MAJOR REPAIR - DURING C-20 CHECK DELAMINATION WAS FOUND ON THE LOWER OUTBOARD END OF THE RT AILERON. MAINTENANCE REMOVED AND REPLACED THE RT AILERON PER T/C R3M27015.SDR AWXA200200815Skin · debondedYVR - MAJOR REPAIR - DURING C-20 CHECK THE RT OUTBOARD AFT FLAP WAS FOUND TO EVIDENCE OF DEBONDING ON THE LOWER SURFACE INBOARD END. MAINTENANCE REMOVED AND REPLACED THE RT OUTBOARD AFT FLAP ASSEMBLY IAW T/C R3R27001.SDR AWXA200200811Wedge · delaminatedYVR - MAJOR REPAIR - DURING C-20 CHECK THE LT INBOARD MIDFLAP TRAILING EDGE WEDGE END WAS FOUND TO HAVE CRACKS AND DELAMINATION IN POTTING COMPOUND AT THE 1ST, 2ND, AND 3RD INBOARD TRACK CUTOUTS AND OUTBOARD BLOCK. MAINTENANCE REMOVED DAMAGED LT INBOARD MIDFLSDR AWXA200200807Stop Fitting · gougedYVR - MAJOR REPAIR - DURING C-20 CHECK THE FORWARD CARGO DOOR BOTTOM AFT DOOR STOP SHOWS EVIDENCE OF WEAR FROM CONTACTING DOOR STOP FITTING BOLTS. MAINTENANCE REMOVED DAMAGED FORWARD CARGO DOOR BOTTOM AFT DOOR STOP; FABRICATED A NEW BOTTOM AFT DOOR STOP, AND 2SDR AWXA200200749Frame · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND AT FASTENER HOLE ON THE FORWARD GALLEY DOOR CUTOUT, FORWARD LOWER FRAME SECTION, INBOARD LOWER ATTACHMENT, BS 291.5. MAINTENANCE CUTOUT DAMAGED AREA OF FRAME AT FORWARD GALLEY DOOR CUTOUT, FORWARD LSDR AWXA200200747Frame · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND ON THE FORWARD GALLEY DOOR CUTOUT FORWARD UPPER FRAME, BS 291.5. MAINTENANCE CUTOUT DAMAGED AREA OF FRAME AT FORWARD GALLEY DOOR CUTOUT, BS 291.5. FABRICATED 3 EACH REPAIR ANGLES, 2 EACH CHANNELS, ASDR AWXA200200667Blade · failedPHX - EMERGENCY LANDING - EN ROUTE FROM AUS TO PHX FLIGHT CREW NOTICED A NR 1 ENGINE VIBRATION WITH A SPIKE IN EGT, ALL ENGINE GAUGES LOOKED NORMAL, LANDED AT PHX. DAMAGE NOTED TO TURBINE SECTION, MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE PER T/C'S R5M7SDR AWXA200200840Skin · delaminatedYVR - MAJOR REPAIR - DURING C-20 CHECK DELAMINATION ON THE UPPER SURFACE OF THE NR 7 FLIGHT SPOILER WAS FOUND AT THE 3 INCH FOLD OF THE TRAILING EDGE AT INBOARD SIDE. MAINTENANCE REMOVED AND REPLACED THE NR 7 FLIGHT SPOILER PANEL IAW BMM 27-61-11 PG 401.SDR AWXA200200818Shutoff Valve · failedYVR - ENGINE FLAMEOUT - DURING C-20 CHECK ENGINE PERFORMANCE DETERIORATION TEST THE NR 2 ENGINE EXPERIENCED IMPENDING FLAME-OUT WITHIN 40 SECONDS OF SHUTTING OFF THE NR 2 FUEL TANK BOOST PUMPS, ENGINE RECOVERED NORMALLY WITH BOOST PUMPS WERE RESELECTED TO THE SDR AWXA200200812Attach Angle · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND ON THE L-1 DOOR LINER LOWER AFT SUPPORT BRACKET ATTACH ANGLE AT BS 344. MAINTENANCE REMOVED DAMAGED LOWER AFT SUPPORT BRACKET ATTACH ANGLE AT BS 344, FABRICATED A NEW ATTACH ANGLE PER DWG 65-49649, AND ISDR AWXA200200799Skin · damagedYVR - MAJOR REPAIR - DURING C-20 THE RT WING LOWER SURFACE NR 5 SLAT TROMBONE CUTOUT HAS SMALL PIECE OF SKIN MISSING AT OUTBOARD END. MAINTENANCE REMOVED DAMAGED AREA OF SKIN RT WING LOWER SURFACE NR 5 SLAT TROMBONE CUTOUT, FABRICATED A NEW SECTION OF SKIN, ASDR AWXA200200772Skin · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND ON FORWARD UPPER CORNER OF SKIN CUTOUT AT THE L-2 DOOR BS 951. MAINTENANCE REMOVED DAMAGED AREA OF SKIN AND BONDED DOUBLER, FABRICATED A DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW B737-200 SSDR AWXA200200629Computer · faultyON TAKEOFF WHEN ENGAGING THE A-AUTOPILOT AIRCRAFT WENT TO CWS PITCH MODE AND NOSE PITCHED UP 5 TO 10 ABOVE NORMAL TAKEOFF ATTITUDE. SWITCHED TO B-CHANNEL AND SYS OPERATED NORMALLY. MX PLACED SYS ON MEL 22-01-11, COND 1 A-AUTOPILOT INOPERATIVE. TROUBLESHOT SSDR AWXA200200619Flashlight · dischargedFLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT AFT LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LT EMERGENCY FLASHLIGHT.SDR AWXA200200618Battery · dischargedDURING INSPECTION THE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE ABOVE L2 DOOR. MAINTENANCE REMOVED AND REPLACED THE BATTERIES AT THE EMERGENCY EXIT LIGHT ABOVE THE L2 DOOR, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200617Battery · dischargedDURING INSPECTION THE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE AT THE COCKPIT ENTRANCE. MAINTENANCE REMOVED AND REPLACED BATTERIES FOR FORWARD EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200616Wire · brokenPHX - EEL - DURING INSPECTION THE EMERGENCY EXIT PATHWAY LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 7 L/H. MAINTENANCE SPLICED A BROKEN WIRE AT SEAT ROW 7 L/H IAW CHAP 20 SWPM, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200592Battery · dischargedFORWARD EMERGENCY FLASHLIGHT INOPERATIVE, PLACED IN CHARGER BACKWARDS. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200578Power Supply · dischargedDURING INSPECTION THE LOWER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE ON LEFT EMERGENCY EXIT DOOR. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY, OPERATIONAL CHECK WAS GOOD IAW BMM 33-51-11.SDR AWXA200200577Power Supply · dischargedDURING INSPECTION THE EMERGENCY EXIT LIGHTS AT BOTH LWR L2 & R2 DOORS WERE FOUND INOPERATIVE, RELAMP NO HELP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY, OPERATIONAL CHECK WAS GOOD IAW BMM 33-51-11.SDR AWXA200200574Light · brokenDURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT WAS FOUND INOPERATIVE AND BROKEN OFF SEAT. MAINTENANCE REPLACED BOTTLE CAP SEAT LIGHT ASSEMBLY AT SEAT ROW 4 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200520Actuator · bindingBOI - AIR TURN BACK - FLT 0166 - ON DEPARTURE OUT OF BOI EN ROUTE TO PHX THE NR 4 SLAT REMAINED IN EXTENDED POSITION; FLAPS WERE CYCLED AND NR 4 SLAT STILL REMAINED EXTENDED; TURNED BACK TO BOI AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE INSPECTED THE NR 4 SDR AWXA200200534Floorbeam · corrodedYVR - MAJOR REPAIR - DURING C-15 CHK, CORROSION WAS FOUND ON FLOOR BEAM 987 IN THE CENTER OF THE CABIN AT BL 0 HAD CORROSION ON TOP SURFACE. FLOORBEAM REPAIRED IAW SRM 53-10-9 PAGE 7 FIG 2.SDR AWXA200200546Bulkhead · crackedYVR - MAJOR REPAIR - DURING C-15 INSPECTION A WEB CRACK WAS FOUND AT FOUR RIVETS AT STA 1016 S-6L NEAR THE FWD SIDE OF THE PRESSURE BULKHEAD. DAMAGED AREA WAS CUT OUT AND HVEC WAS PERFROMED AND INSPECTED PER NDT MANUAL PART 6 , 51-00-00 FIG. 23. NO CRACKS FOUSDR AWXA200200506Wire · brokenPHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 L/H WAS FOUND INOPERATIVE. MAINTENANCE FOUND THE WIRING UNDER SEAT COMING OUT OF THE SPLICE. RE-SPLICED BROKEN E-PATH WIRE UNDER SEAT ROW 4 L/H, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200565Skin · wornYVR - MAJOR REPAIR - DURING C-15 CHECK THE L/H WING OUTBD MIDFLAP FLAPTRACK FAIRING CONTACT AREA WAS FOUND WORN ON LOWER SKIN AT THE #2 FLAP TRACK POSITION. MAINTENANCE BLENDED DAMAGED, FABRICATED AN EXTERNAL DOUBLER, AND INSTALLED REPAIR IAW AWA 15-5754-0217SDR AWXA200200564Web · chafedYVR - MAJOR REPAIR - DURING C-15 CHECK THE TOP OF THE SPOILER RATIO CHANGER WAS FOUND CHAFING INTO THE WHEEL WELL CEILING BS 700. MAINTENANCE BLENDED CHAFED AREA AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR TRIPLER AND FILLER ANSDR AWXA200200547Floorbeam · crackedYVR - MAJOR REPAIR - DURING C-15 INSPECTION A CRACK WAS FOUND ON A FLOORBEAM WEB AT BS 639 BETWEEN RIVETS AT STA RBL 64. MAINTENANCE REPAIRED CABIN FLOOR BEAM BS 639 WEB RBL 64 IAW AWA ER 15-5310-02168-JS1.SDR AWXA200200555Web · crackedYVR - MAJOR REPAIR - DURING C-15 CHECK A 1/2" CRACK WAS FOUND ON R/H SRTINGER 18A SHEAR BEAM (WEB) AT BS 727 BULKHEAD ATTACHMENT. MAINTENANCE REMOVED CRACKED WEB, FABRICATED A NEW WEB, AND INSTALLED REPAIR IAW B737-200 SRM 51-10-1, PG. 8, DWG 65-46877 SHT 9, SDR AWXA200200535Crease Beam · crackedYVR - MAJOR REPAIR - DURING C-15 CHECK A CRACK WAS FOUND ON THE HORIZONTAL FLANGE OF THE RT INNER CHORD FO CREASE BEAM AT BS 639, RBL 64. MAINTENANCE REMOVED AND REPLACED THE RT CREASE BEAM INNER CHORD AT BS 639, RBL 64 PRE DRAWING 65-47973, AND B737-200 SRM SDR AWXA200200536Skin · corrodedYVR - MAJOR REPAIR - DURING C-15 CHECK TWO RIVET HEADS WERE FOUND POPPED FROM THE FUSELAGE AT STA. 495, STR. 495. MAINTENANCE FABRICATED DOUBLER AND INSTALLED REPAIR PER SRM 51-10-02 PAGE 7. INTALLED PROTECTIVE FINISH PER MM 51-21-0 PAGE 1.SDR AWXA200200480Skin · crackedPHX - MAJOR REPAIR - DURING INSPECTION A CRACK WAS FOUND ON FUSELAGE SKIN AT BS 747, STR 16 L/HCRACK FOUND ON FUSELAGE L/H SIDE APPROX. STA. 747 STR.16LSDR AWXA200200429Battery Pack · dischargedPHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED WITH THE SWITCH IN THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS AT THE L1 AND R1 DOORS, AND THE BATTERY PACK AT THE FWD DROP CEILING, OPERATIONAL CHECK WAS G
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