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 USAA061078Skin · crackedFOUND SKIN CRACKED, BS 727E+14" JUST BELOW S-23R. CUT OUT DAMAGE, FABRICATED IAW SRM 53-00-001 FIG 201, DEFECT SIZE: 2.5".SDR USAA061079Skin · crackedFOUND CRACK LEADING EDGE SKIN, JUST AHEAD AND INBOARD OF OUTBOARD AUX TRACK. INSTALLED DOUBLER IAW SRM 57-43-01, DEFECT SIZE: .25".SDR SB06083Transmitter · faultyPHL - FLT238 - ON APPROACH TO PHL FROM DFW, CREW REPORTED THE FLAPS WOULD NOT MOVE FROM 10 UNITS TO 15 UNITS WHEN SELECTED. CREW EXECUTED A MISSED APPROACH, AND DURING GO-AROUND, FLAPS ADJUSTED THEMSELVES AND INDICATED 15 UNITS. FLIGHT MADE A FLAPS 15 LANDINSDR USAA061068Angle · crackedAT STA 348 S16L CRACK. INSTALLED NEW ANGLE AND CLIP IAW SRM 51-40-02, DEFECT SIZE: .50 INCH.SDR USAA061069Frame · crackedSTA 887 S9R CRACKED. INSTALLED DOUBLER IAW TR 53-10-20D, DEFECT SIZE: .25 INCH.SDR USAA061070Support Fitting · crackedNOSE GEAR UPPER ACTUATOR SUPPORT FITTING CRACKED. INSTALLED WEB FILLER AND DOUBLER IAW SRM 51-70-13, DEFECT SIZE: .50 INCH.SDR USAA061071Stringer Clip · crackedAT 727 AND S7L CRACK. REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED TIE CLIP IAW SRM 51-10-02, DEFECT SIZE: .125 INCH.SDR USAA061072Stringer Clip · crackedSTA 727B S7L CRACKED. REMOVED AND REPLACED TIE CLIP IAW SRM 51-10-02, DEFECT SIZE: .187 INCH.SDR USAA061073Intercostal · crackedINTERCOSTAL COMMON TO THE MAIN ENTRY DOOR, STA 348 S16L CRACKED. REPLACED ALUMINUM PARTS WITH STEEL PARTS, IAW SRM 53-10-04, DEFECT SIZE: .50 INCH.SDR COOSDR060032Rib · crackedRT WING AT WBL 114 RIB UPPER CHORD CRACKED NEAR STR-2. (K)SDR USAA061063Frame · crackedSTA 767 STR 9L CRACKED. INSTALLED DOUBLERS IAW TR 53-10-20D, DEFECT SIZE: .250 INCH.SDR USAA061054Stringer Clip · crackedSTA 578, S5R CRACKED. REPLACED DAMAGED CLIP IAW SRM 51-10-02, DEFECT SIZE: .25 INCH.SDR USAA061055Stringer Clip · crackedSTR 2R AT FRAME 639 CRACKED. REMOVED AND REPLACED TIE CLIP IAW SRM 51-10-02, DEFECT SIZE: .25 INCH.SDR USAA061050Stringer Clip · crackedSTA 578, S7R CRACKED. REPLACED DAMAGED CLIP IAW SRM 51-10-02, DEFECT SIZE: .25 INCH.SDR 2007FA0000132Floorbeam · corrodedCABIN BS 312, FROM LBL 55 TO RBL 55 WL 208, FLOORBEAM HAS LIGHT CORROSION. (K)SDR SWAA062953Sign · brokenLT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.SDR SWAA062857Lamp · inoperativeDURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT L2 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.SDR SWAA062789Hydraulic Line · leakingAIR TURN BACK, HYDRAULIC "B" SYSTEM FLUID LOSS. REMOVED AND REPLACED HYDRAULIC LINE AT "B" SYSTEM ACOUSTIC FILTER AND "B" SYSTEM RETURN FILTERS PER MM.SDR SB06069Actuator · faultyFL270 AND 300 KTS, CREW REPORTED L/E AMBER IN-TRANSIT LIGHT ON FWD PNL ILLUMINATED ALONG WITH GREEN LIGHT ON OVERHEAD PANEL. CREW STATED NR 3 L/E DEVICE WAS EXTENDED AND A/C ROLLED TO RIGHT. CREW REDUCED AIRSPEED TO 220 KNOTS AND L/E DEVICE RETRACTED. A/C RETSDR AWXA200601127Battery Pack · inoperativePHX - EEL - FLT 33 - LG 4104284 - LEFT EMERGENCY OVERWING EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-51-2. OPERATIONAL CHECKS GOOD.SDR SWAA062290Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 508, STR 16L. REPAIRED SKIN PER SRM.SDR SB06064Bottle · low pressurePILOT REPORTED THE AFT LEFT ENTRY DOOR EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE IS LOW. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT ENTRY DOOR EMERGENCY ESCAPE SLIDE ASSEMBLY. AIRCRAFT OK FOR SERVICE.SDR SB06060Windshield · crackedEWR FLT 182 EN ROUTE FROM CLT TO EWR, DURING CRUISE AT FL270, THE FIRST OFFICER'S WINDSHIELD CRACKED. CREW DECLARED AN EMERGENCY AND LANDED AT EWR WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICER'S WINDSHIELD PER JOB CARD J356-11-SDR USAA200606006Skin · delaminated3.5" L BY 1.4" W DELAMINATION AT OUTBD AFT UPPER SKIN AT NR 5 SLAT TRAILING EDGE. REPAIRED PER EA 82529.SDR SWAA061957Beltframe · corrodedDURING SCHEDULED C4 CHECK, FOUND FUSELAGE BELT FRAME CORRODED AT BS 747, STR 26R. REPAIRED FRAME PER SRM.SDR SWAA061956Slide · out of adjustDURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.SDR SB06056Switch · faultyCLT - PILOT REPORTED THE FLOOR TRACK EMERGENCY LIGHTS REMAIN ILLUMINATED. MAINTENANCE FOUND THE S7 EMERGENCY LIGHT SWITCH FAULTY. THE SWITCH WAS PROVIDING A GROUND TO PIN 4 OF EACH BATTERY PACK WHILE IN THE ARMED POSITION. REMOVED AND REPLACED S7 EMERGENCY SDR USAA060735Skin · delaminatedINBOARD END OF RT AFT I/B FLAP DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 57-53-02, DEFECT SIZE: 2 X 3 INCH.SDR USAA060736Skin · gougedINBOARD SIDE OF RT INBOARD FOR FLAP GOUGED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-70-10. DEFECT SIZE: 5 X 1 INCH.SDR SWAA061841Slide · out of adjustFOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.SDR SB06055Transmitter · faultyORF - FLT32 - ON APPROACH TO ORF, CREW REPORTED A FLAP ASYMMETRY LOCKOUT. FLIGHT LANDED WITHOUT INCIDENT AT 2 UNITS FLAP POSITION. MAINTENANCE CHECKED WIRING TO BOTH FLAP TRANSMITTERS AND JACKSCREW BALLNUTS FOR DEFECTS. NO DEFECTS NOTED. REMOVED AND REPLACSDR SWAA061823Bulb · inoperativeDURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BULB PER MM.SDR AWXA200600855Coalescer Bag · odorLAS - BURNING SMELL - F/A`S REPORTED A BURNING SMELL OF RUBBER COMING FROM THE AFT GALLEY AREA AT CRUISE ABOUT 25 MINS PRIOR TO LANDING IN LAS WITH NO IND OF SMOKE. ODOR WENT AWAY BUT THEN RETURNED DURING DESCENT AND THEN WENT AWAY AGAIN LATER IN DESCENT. MXSDR USAA200605003Skin · crackedMULTIPLE NUMBER OF CRACKS, TOT APPROX LENGTH 2 INCHES, AT LOWER TIE SURFACE AT ACTUATOR, NR 3 SLAT SKIN. INSTALLED FILLER AND DOUBLER PER SRM 57-43-01, REPAIR 06.SDR SB06054Door Seal · leakingDURING CRUISE, EN ROUTE FROM PHL TO ORD, CREW REPORTED THE AUTO PRESSURE CONTROL FAILED AT FL340. CABIN ALTITUDE CLIMBED TO 10,000 FEET AND THE WARNING HORN SOUNDED. CREW ACCOMPLISHED AN EMERGENCY DESCENT TO FL240 AND SELECTED STANDBY MODE WITH BOTH PACKS INSDR SB06053Light · corrodedFLL - MAINTENANCE REPORTED THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE CLEANED CORROSION FROM BULBS AT LEFT EXTERIOR OVERWING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.SDR SB06052Indicator · faultyON APPROACH TO PHL FROM ORD, AS CREW SELECTED FLAPS TO 10 UNITS FROM 5 UNITS, REPORTED THE RIGHT FLAP POSITION NEEDLE STOPPED AT 7 UNITS WHILE THE LEFT FLAP POSITION NEEDLE STOPPED AT 9 UNITS. LEADING EDGE FLAPS WENT TO FULL EXTEND NORMALLY. NO ASYMMETRICAL SDR SWAA061516Skin · crackedDURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT BEAR STRAP. REPAIRED SKIN PER SRM.SDR SWAA061515Skin · crackedDURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.SDR SWAA061514Skin · crackedDURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.SDR USAA060651Skin · crackedFOUND SKIN CRACKED, STA 727E, STR 24L SRM REPAIR 53-00-01, DEFECT SIZE: 3".SDR AWXA200600767Unknown · low pressureEN ROUTE, CREW REPORTED THAT AT FL 340 AUTO STANDBY DID NOT HOLD ALTITUDE. CREW DESCENDED TO FL 100. MASKS DID NOT DEPLOY DUE TO GRADUAL LOSS OF PRESSURIZATION. CREW DIVERTED TO ICT AND LANDED WITHOUT FURTHER EVENT. MAINT PERFORMED LINE MAINT PRESSURIZATIOSDR USAA200605001Skin · crackedFOUND 1.5" CRACK AT STA 33 LBL, LT SIDE OF MAIN WHEEL WELL. REPAIRED PER TYPICAL REPAIR 53-60-04.SDR SB06045Outflow Valve · faultyDURING CRUISE, CABIN ALT ALERT WARNING HORN SOUNDED, CABIN PRESS CLIMBED. CREW INITIATED AN EMERG DESCENT. AT LOWER ALT, WAS ABLE TO GAIN CONTROL OF CABIN ALT. NO EMERG DECLARED. FLT DIVERTED, LANDED W/O INCIDENT. MX ACCOMP A/C PRESS T/S CARD J321-30-00. SDR USAA060645Stiffener · crackedFOUND VERTICAL STIFFENER CRACKED, STA 663 LBL 6.15. INSTALLED REPAIR PARTS ON VERTICAL STIFFENER IAW TR 57-10-03B, DEFECT SIZE: .5".SDR USAA200705004Skin · cracked2" LONG CRACK FOUND IN FUSELAGE SKIN AT AFT LOWER LEFT FUSELAGE, S23L BETWEEN 727 D & E. [SUP 05-04-07] REMOVED DAMAGE & INSTALLED SKIN & TEAR STRAP DOUBLERS PER SRM 53-00-01, T/REP. 53-60-03ASDR SB06043Ground Wire · disconnectedBWI - MAINTENANCE REPORTED THE FLIGHT DECK EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED LIGHT WITH NO HELP. REQUIRES FURTHER TROUBLESHOOTING. PLACED ON MEL 33-15, C/N 2907C09. AIRCRAFT RESTRICTED TO DAYLIGHT OPERATION ONLY. MAINTENANCE IN PHL, FOUND THSDR SB06037Sign · brokenTHE RIGHT OVERWING EMERGENCY EXIT, LOWER VERTICAL SIGN, WAS FOUND BROKEN. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY EXIT SIGN ASSEMBLY. OPERATIONAL CHECK GOOD.SDR USAA200604001Skin · crackedFOUND SKIN CRACKED 2.75" AT STA 747 STRINGER 20L. TWO FILLERS AND TWO DOUBLERS INSTALLED PER SRM 53-00-01 FIG 201 DETAIL XIX.SDR SB06039Light · brokenORF - THE SEAT MOUNTED EMERGENCY AISLE LIGHT WAS FOUND BROKEN ON SEAT 5C. MAINTENANCE REMOVED AND REPLACED THE SEAT MOUNTED EMERGENCY AISLE LIGHT ASSEMBLY ON SEAT 5C. OPERATIONAL CHECK GOOD.
Back to Boeing 737-301