Boeing 737-301
Service difficulty reports · 4,797
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 = '737301' 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 = '737301' 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 USAA000430Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 1 INCH BY 48 INCHES, FORWARD ENTRY DOOR Z-ANGLE. INSTALLED NEW Z-ANGLE PER SRM 53-10-02. (M)SDR USAA000431Door Frame · crackedCLT - DOOR FRAME CRACKED .5 INCH, FORWARD SERVICE DOOR FRAME, LOWER FORWARD CORNER. INSTALLED DOUBLER AND FILLER PER SRM 51-40-04. (M)SDR USAA000405Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 787, STRINGER 9R. INSTALLED OVERSIZE FASTENER PER SRM 51-40-02. (M)SDR USAA000406Frame · crackedCLT - FOUND FRAME CRACKED .500 INCH, BS 807 STRINGER 9R. INSTALLED DOUBLER PER EA 66834. (M)SDR USAA000407Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 827 STRINGER 9L. INSTALLED DOUBLER PER EA 66834. (M)SDR USAA000408Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 827, STRINGER 9R. INSTALLED DOUBLER PER EA 66834. (M)SDR USAA000409Frame · crackedCLT - FOUND FRAMED CRACKED .50 INCH, BS 847, STRINGER 9L. INSTALLED DOUBLER PER EA 66834. (M)SDR USAA000410Frame · crackedCLT - FOUND FRAME CRACKED, BS 867, STRINGER 9R. INSTALLED OVERSIZED HI-LOCKS PER SRM 51-40-02. (M)SDR USAA000411Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 887, STRINGER 9R. INSTALLED DOUBLER. (M)SDR USAA000412Frame · crackedCLT - FOUND FRAMED CRACKED .500 INCH, BS 907, STRINGER 9R. INSTALLED REPAIR DOUBLER PER EA 66834. (M)SDR USAA000413Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, UPPER HINGE CUTOUT SERVICE DOOR BS 947 STRINGER 11R. INSTALLED DOUBLER PER SRM 53-60-01 FIG 205. (M)SDR USAA000414Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 2 INCHES, STATION 312, 77 INCHES INBOARD OF FORWARD ENTRY DOOR SILL. INSTALLED T-CAP PER SRM 53-10-51. (M)SDR USAASB00076Battery Pack · dischargedCLE - MAINTENANCE FOUND THE MID CABIN EMERGENCY LIGHT ON THE RIGHT SIDE AISLE INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)SDR USAASB00079Battery Pack · dischargedPHL - WHILE PERFORMING OVERNIGHT CHECK, MAINTENANCE FOUND THE EMERGENCY EXIT SIGNS INOPERATIVE AT SEAT ROW 10 ABC CEILING AND SIDEWALL. MAINTENANCE TROUBLESHOT SYSTEM TO THE CEILING BATTERY PACK. REMOVED AND REPLACED BATTERY PACK IN CEILING. OPERATIONAL CHESDR AWXA0000140Stringer · corrodedFWD CARGO COMPARTMENT FS 500 TO 500B STRINGER 27L CORRODED OUT OF LIMITS. CUT OUT DAMAGED AREA, FABRICATED PARTS FROM (BAC 1498-161 QQA 250/13C R757812) IAW 737 51-40-02. U-CHANNELS FROM (.065 7075-0 QQA 250/13 HT TO T6), TREATED, PRIMED, AND INSTALLED IAW 7SDR AWXA0000139Frame · crackedFUSELAGE FRAME CRACKED FROM GUSSET FASTENER TO TOOLING HOLE IN FWD CARGO COMPARTMENT AT STA 500 RBL 2.0. CUT OUT DAMAGED AREA IAW 737 SRM 53-00-07, NDT HFEC INSP CW IAW 737 NTM PT 6 51-00-00. FABRICATED PARTS FROM (7075T6 ..050 R698980) ALODINED AND PRIMED PSDR USAA000340Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED 1 INCH, BS 178, BL 0 BETWEEN HORIZ STIFFENERS. INSTALLED DOUBLER PER SRM 53-10-08 FIG 203. (M)SDR USAA000341Stiffener · crackedCLT - FOUND VERTICAL STIFFENER CRACKED 1 INCH, BS 178, LBL 5, WL 183. INSTALLED DOUBLER PER SRM 53-10-08 FIG 209. (M)SDR USAA000342Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED 1 INCH, BS 178, RBL 5, WL 200. INSTALLED DOUBLER PER SRM 53-10-08 FIG 209. (M)SDR USAA000343Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .5 INCH, BS 178, RBL 5, WL 197. INSTALLED DOUBLER PER SRM 53-10-08 FIG 209. (M)SDR USAA000344Web · crackedCLT - FOUND 3 CRACKS IN WEB FLANGE 1 INCH LONG, BS 500D TO 520D, BL 0 WEB FLANGE. REPLACED WEB FLANGE PER SRM 51-10-02. (M)SDR USAA000345Web · crackedCLT - FOUND WEB CRACKED .25 INCH, 5 CRACKS, BETWEEN STATION 927 AND 947, BL 0 WEB. INSTALLED NEW ANGLE PER SRM 51-30-01 AND 51-10-02. (M)SDR USAA000346Stringer Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .25 INCH, BS 663-675, STRINGER 10L, REMOVED AND REPLACED. (M)SDR USAA000335Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 639, STRINGER 8R TIE CLIP. REPLACED CLIP PER SRM 53-30-03. (M)SDR USAA000336Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 685, STRINGER 4 TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 53-30-03. (M)SDR USAA000361Skin · crackedBOS - FOUND SKIN CRACKED 3 INCHES, STATION 727D, STRINGER 24R. INSTALLED DOUBLER 5.75 INCHES BY 11 INCHES. (M)SDR USAASB00059Acm · failedPHL - FLT 515 - DURING CLIMB-OUT FROM PHL, AT FL100, FLIGHT ATTENDANT REPORTED SMELLING SMOKE IN AFT GALLEY AREA AND A CHALKY HAZE THROUGHOUT THE CABIN. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENASDR USAASB00058Battery Pack · inoperativeCLT - MAINTENANCE FOUND THE AFT RIGHT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK NORMAL. (M0SDR USAASB00055Actuator · failedPHL - FLT 1063 - EN ROUTE FROM RIC TO BOS, THE STABILIZER ELECTRIC TRIM HAD FAILED. FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTEHR INCDIENT. NO EMEGENCY WAS DECLARED. MAINTENANCE PERFORMED FUNCTIONAL CHECK ON STABILIZER TRIM SYSTEM AND FOUND ALL FUNCTIONSDR USAASB00051Controller · failedCLT - FLT 58 - ON CLIMB-OUT FROM CLT, AIRCRAFT FAILED TO PRESSURIZE IN AUTO MODE. WHEN STANDBY MODE WAS SELECTED, CABIN RATE OF DESCENT WENT TO 3,500 FEET PER MINUTE. CABIN RATE KNOB HAD NO EFFECT ON RATE. SWITCHED TO MANUAL MODE AND GAINED CONTROL OF CABINSDR DL733000356Controller · inoperativeAIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR STANDBY, CONTROL POSSIBLE IN MANUAL A/C. REPLACED PRESSURE CONTROLLER PER MM. OPS CHECKED OK. RAN ENGINES TO PRESSURIZE ACFT PER PFHB, CKS OK.SDR USAASB00045Fire Loop · malfunctionedCLT - FLT 7031 - EN ROUTE FROM TPA-BOS, THE NR 1 ENGINE FIRE DETECTION FAULT LIGHT BEGAN TO ILLUMINATE INTERMITTENTLY TO STEADY. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND DIVERTED TO CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY SDR USAASB00039Battery Pack · dischargedCLT - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTING INOPERATIVE AT ROW 12 ABC THROUGH ROW 16 ABC AND AT ROW 21 AND 22 ABC. ALSO, FOUND THE RIGHT AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PASDR AWXA0000065Wire · brokenNON-ROUTINE LINE EMERGENCY LIGHTING. EMERGENCY LIGHTS 17C AND 18C INOP. RESPLICED FAULTY WIRING, OPS CHECK NORMAL.SDR USAASB00033Bulb · failedTPA - FLT 8550 - ON APPROACH TO MCO, DURING LANDING GEAR EXTENSION, NO LIGHTS ILLUMINATED ON LANDING GEAR PANEL TO INDICATE STATUS OF LANDING GEAR. CREW NOTICED ' SECTION 5' CIRCUIT BREAKER WAS POPPED, BUT WOULD NOT RESET. CREW LOWERED LANDING GEAR MANUALLY SDR 2000ZZZM219Bulb · failedTPA - FLT 8550 - ON APPROACH TO MCO, DURING LANDING GEAR EXTENSION, NO LIGHTS ILLUMINATED ON LANDING GEAR PANEL TO INDICATE STATUS OF LANDING GEAR. CREW NOTICED ' SECTION 5' CIRCUIT BREAKER WAS POPPED, BUT WOULD NOT RESET. CREW LOWERED LANDING GEAR MANUALLY SDR USAASB00028Track · contaminatedBNA - FLT 1524 - ON CLIMB-OUT FROM BNA, CAPTAIN NOTICED AN AIR LEAK ON THE LEFT SIDE OF THE COCKPIT SLIDING WINDOW. AIRCRAFT HAD TROUBLE PRESSURIZING ALSO. FLIGHT RETURNED TO FIELD AT BNA AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINSDR USAASB00025Indicator · failedGSO - FLT 1462 - ON APPROACH INTO GSO, A FLAP ASYMMETRY OCCURRED. SPLIT FLAPS OF 1 DEGREE LEFT AND 25 DEGREES RIGHT WAS INDICATED. FLAP HANDLE WAS LOCKED OUT ALSO. THERE WAS NO INDICATION OF LEADING EDGE DEVICES ON OVERHEAD OR FORWARD PANEL. FIRST OFFICERSSDR SWAA000164Line · contaminatedAIR TURNBACK, NR 1 ENG A-SYS HYD LOW PRESS LIGHT ILLUMINATED AND NLG WOULD NOT RETRACT. FOUND AIR TRAPPED ON NR 1 ENG HYD PUMP SUPPLY LINE WHICH WAS PREVIOUSLY REMOVED AND REPLACED BLED SYS. OPS CHECKED GOOD PER MM.SDR AWXA0000023Wire · brokenEMERGENCY ESCAPE LIGHT AT SEAT 4C INOPERATIVE. RESPLICED WIRE RECOMENDATION, CLOSE NO RELATED HISTORY.SDR USAASB00020Transceiver · inoperativeNAS - FLT 1166 - UPON DESCENT INTO NAS, AT APPROXIMATELY 5,000 FT, CREW EXPERIENCED A TERRAIN WARNING FROM THE GPWS. CAPTAINS RADIO ALTIMETER INDICATED 1,000 FT. CAPTAIN PERFORMED EVASIVE MANEUVER, MAXIMUM THRUST NOSE UP CLIMB TO STICK SHAKER, AND LEVELED OFSDR USAASB00019Transformer · failedBWI - FLT 549 - FLIGHT DEPARTED LGA WITH AN MEL ON THE APU FOR NOT STARTING. WHILE EN ROUTE TO CLT, THE NR 1 GENERATOR TRIPPED OFF LINE TWICE AND WAS ABLE TO BE RESET BOTH TIMES. GENERATOR THEN TRIPPED A THIRD TIME AND WOULD NOT RESET. AN EMERGENCY WAS DECLSDR USAASB00016Smoke Detector · malfunctionedPIT - FLT 2147 - AFTER TAKEOFF FROM PIT, FLIGHT ATTENDANT INFORMED CAPTAIN THAT THERE WAS SMOKE IN THE AFT CABIN WITH THE AFT RIGHT LAVATORY SMOKE DETECTOR SOUNDING OFF. CAPTAIN DECLARED AN EMERGENCY. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHESDR USAASB00014Controller · failedPIT - FLT 723 - ON CLIMB-OUT FROM PIT, THE AUTO FAIL PRESSURIZATION LIGHT ILLUMINATED. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES BUT WAS UNABLE TO PRESSURIZE AIRCRAFT. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WSDR USAA000039Frame · corrodedSTATION 747 - AFT BAG BIN FRAME HAS A 1 INCH AREA OF CORROSION, LEVEL 1. FABRICATED REPAIR PER SRM 51-30-01 AND 53-00-07. (M)SDR USAA000033Keelbeam · corrodedRBL 6.5 STATION 528 TO 533 KEEL BEAM HAS A 5 INCH BY 1 INCH AREA OF CORROSION, LEVEL 2. INSTALLED REPAIR ANGLE PER EA 66434, SRM 51-70-12. (M)SDR USAA000032Keelbeam · corrodedFOUND LBL 6.5, STATION 528, 537 TO 539 KEEL BEAM HAS A 2 INCH BY 1 INCH AREA OF CORROSION, LEVEL 2. INSTALLED REPAIR ANGLE PER EA 66434, SRM 51-70-12. (M)SDR USAA991447Bulkhead · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT STATION 178, RBL 4.75, WL 201 BULKHEAD. INSTALLED DOUBLER PER SRM 53-10-8 AND EA 66276. (M)SDR USAA991448Angle · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .500 INCH CRACK AT STATION 294, OUTBOARD SIDE OF Z-ANGLE VERTICAL LEG SUPPORT ANGLE. REMOVED AND REPLACED PER SRM 51-10-02. (M)SDR USAA991449Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK FORWARD SERVIEC DOOR CUTOUT UPPER FORWARD FRAME WEB UPPER DOOR STOP FRAME. REMOVED AND REPLACED PER SRM 51-10-02. (M)
Back to Boeing 737-301