Boeing 737-375
Service difficulty reports · 174
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 = '737375' 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 = '737375' 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 AWXA200200947Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A 5/16" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727C, STRINGER 4 L/H. MAINTENANCE REMOVED THE DAMAGED STINGER TIE CLIP AT BS 727C, STRINGER 4 L/H, FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW B737-SDR AWXA200200968Keelbeam · crackedDURING C-03 CHECK EXFOLIATION CORROSION WAS FOUND ON THE RT KEEL BEAM AT BS 633. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS WITHIN LIMITS BUT ALSO DISCOVERED A 2 INCH CRACK. TRIMMED OUT CRACK AND PERFORMED HFEC INSPECTION TO VERIFY CRACKS NO LONGERSDR AWXA200200964Floorbeam · crackedDURING C-03 CHECK A 1 INCH CRACK WAS FOUND ON FLOORBEAM AT BS 294, LBL 28. MAINTENANCE TRIMMED OUT CRACK AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A FILLER, 4 EACH REPAIR ANGLES, AND 2 EACH SHIMS, AND INSTALLED REPAIR PARTS IAW AWA ESDR AWXA200200638Wire · brokenPHX - EEL - DURING INSPECTION WIRES WERE FOUND BROKEN ON THE EMERGENCY ESCAPE PATH LIGHT SEAT ROW 15 L/H. MAINTENANCE REPAIRED BROKEN WIRES ON THE EMERGENCY ESCAPE PATH LIGHT SEAT ROW 15 L/H PER CHAP 20 SWPM, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200529Battery · dischargedPHX - EMERGENCY EQUIPMENT - DURING INSPECTION THE FORWARD EMERGENCY FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLASHLIGHT BATTERY. OPERATIONAL CHECK NORMAL.SDR AWXA200200402Light · inoperativeLAS- EEL R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT IAW BMM 33-50-00. FUNCTIONAL CHECK WAS GOOD.SDR AWXA200200364Adc · failedONT - ABORTED TAKEOFF - FLT 0775 - ON TAKEOFF ROLL AT 95 KTS, FUEL LOAD 98,000 LBS AIRSPEED, ALTIMETER, VSI, AND GPWS FAILED. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT AND REPLACED THE NR 1 AIR DATA COMPUTER (ADC) IAW BMM 34-12-11. ADC OSDR AWXA0001718Rod End · damagedPHX - AIR TURNBACK, AT ROTATION THE LEADING EDGE INTRANSIT LIGHT ILLUMINATED AND THEN EXTINGUISHED AS THE CLIMB WAS INITIATED AND ALL SLATS WERE IN EXTENDED POSITION. WHEN FLAPS WERE RETRACTED A LOUD SOUND WAS HEARD AND THE NR 1 SLAT WAS AT FULL EXTEND WITH OSDR 20010306CW003Slide · crackedSLIDE IS CRACKED ON BOTH SIDES OF SHAFT, ABOUT 0.090IN FROM THE END AND THE SHAFT IS BENT. PROBABLE CAUSE IS EXCESSIVE STRESS AND FATIGUE DURING OPERATIONAL LOAD. INCREASE INSPECTION REQUIREMENTS FOR SERVO VALVE SLIDE AND REQUIRE THAT SLIDE BE EDDY CURRENT ISDR AWXA0001171Charger · failedEMERGENCY LIGHTS INOP ROW 13-18. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER ASSY; LIGHTS OPS CHECKED GOOD.SDR AWXA0000622Pump · failedAIR TURNBACK, LOST NR 2 ENGINE DRIVEN B-PUMP AND B-SYS HYD. REMOVED AND REPLACED ENGINE DRIVEN PUMP (SECOND TIME).SDR AWXA0000510Valve · failedPRESSURIZATION FAILED AT 2000 FT AGL (7500 FT) ON APPROACH. UNCONTROLLABLE CABIN CLIMB AT 2000 FT/MIN TO AIRCRAFT ALTITUDE AND THEN DESCENDED WITH AIRCRAFT. OUTFLOW VALVE INDICATED CLOSED. REMOVED AND REPLACED EQUIPMENT COOLING EXHAUST VALVE, SYS OPS CHK''SDR AWXA0000459Floorbeam · damagedNON-ROUTINE LINE, FLOORBEAM AT FS 986.5 LOWER FLANGE HAS PREVIOUS BLEND OUT OF LIMITS. CUT OUT DAMAGED AREA, FABRICATED ANGLES AND FILLER, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS IAW B737 SRM 53-30-51 FIG 202, SRM 51-20-01, AND SRM 51-40-02.SDR AWXA0000454Skin · gougedLT OUTBD MID FLAP GOUGED ON LEADING EDGE. FABRICATED REPAIR DOUBLER, TREATED AND PRIMED AND INSTALLED IAW 737 SRM 51-40-02, SRM 51-20-2, AND SRM 52-55-01.SDR AWXA0000453Panel · dentedDENTS ON PANEL 7220 IB MID FLAP TE. REMOVED DAMAGE SKIN, FABRICATED REPAIR PARTS AND BONDED TO ASSEMBLY IAW ER 03-5700-00183-JS2.SDR AWXA0000452Keelbeam · corrodedLT KEELBEAM LOWER SECTON AT STA 578 LBL 6 CORRODED. COMPLIED WITH E.R. 03-5360-00182SDR AWXA0000451Skin · damagedAFT CARGO DOOR EXTERNAL SKIN DAMAGED. REMOVED DAMAGED AREA IAW 737 SRM 51-40-02, FABRICATED REPLACEMENT SKIN IAW 737 SRM 52-30-01, TREATED AND PRIMED SKIN IAW 737 SRM 51-20-01, INSTALLED IAW SRM 51-40-02.SDR AWXA0000450Floor Support · crackedFLOOR SUPPORT CRACKED IN RADIUS AT STA 540 RBL 1. REMOVED AND REPLACED FLOOR SUPPORT IAW 737 SRM 51-40-02.SDR AWXA0000449Floorbeam · crackedFWD SIDE OF T CAP OF FLOORBEAM CRACKED AT STA 520 LBL 24. REMOVED DAMAGED T CAP, FABRICATED REPLACEMENT PARTS IAW 737 SRM 53-00-51 FIG 201, INSTALLED REPLACEMENT T CAP IAW 737 SRM 53-00-5, TREATED, PRIMED, AND TOPCOATED IAW SRM 51-20-01.SDR AWXA0000448Floor Support · corrodedFLOOR SUPPORT CORRODED AT FS 951 TO 967 LBL 17. REMOVED FLOOR SUPPORT, FABRICATED, TREATED AND INSTALLED REPAIR PARTS IAW 737 SRM 51-10-02, 51-30-01, 51-20-01 AND 51-40-02.SDR CALA0000731Wire · brokenTHE NR 1 ENGINE A FIRE LOOP FAULT LIGHT ILLUMINATED WHILE EN ROUTE FROM SNA TO EWR (B LOOP WAS ON PLACARD). QRH PROCEDURES WERE FOLLOWED AND THE AIRCRAFT WAS DIVERTED TO PHX WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND WIRE NR 25R1 TERMINAL BROKENSDR AWXA0000246Seal · leakingAFTER DEPARTURE, R-1 WINDOW SEAL CAME LOOSE, SEAL WAS VISIBLE AND AIR COULD BE HEARD ESCAPING. RESEALED WINDOW, PRESSURIZED CABIN TO 4.0. NO LEAKS NOTED. RECOMMENDATION: REMAIN OPEN AND MONITOR. WINDOW WAS REPLACED 10 APR 00 ON LP7637470.SDR AWXA0000015Seal · blownDIVERSION FOR RAPID DEPRESSURIZATION REF LP 7594099, LOST CABIN PRESS RAPIDLY AT FL 33000 PERFORMED EMERG DESCENT TO 11000 FT. CABIN RATE OF CLIMB DURING DEPRESSURIZATION WAS 24000 FT DURING DESCENT. WHILE PERFORMING POSTFLIGHT WALK AROUND, FOUND THE AFT CARSDR AWXA9900301Wire · shortedAIR TURNBACK, ON TAKEOFF NR 2 BLEED TRIPPED ON TAKEOFF ROLL. RESET, LIGHT WENT OUT. HOWEVER, RT BLEED GAUGE WOULD NOT MOVE OFF ZERO UNLESS ISO VALVE OPEN. PRESSURIZATION WENT TO 9500 SEE LOG 7395034, 35, AND 36. FOUND WIRE OPEN BETWEEN C/P D1208 AND AIR BL
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