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 USAA051033Web · crackedSTA 699 INSIDE KEEL BEAM STRUT LOWER RT CORNER OF LIGHTENING HOLE IN BULKHEAD. REMOVED DAMAGE, INSTALLED DOUBLER IAW EA 69760 DEFECT SIZE: LOWER RT CORNER OF LIGHTENING HOLE CRACKED .500 INCH.SDR USAA051040Bushing · corrodedVERTICAL FIN AFT ATTACH LUGS RT SIDE FWD FACES. REMOVED CORROSION MACHINED & INSTALLED BUSHINGS IAW BOEING DWG 69-72039, 65-52274 DEFECT SIZE: 1 X 2 INCHES TYPICAL.SDR USAA051039Angle · crackedLEFT PACK BAY, AFT RIGHT CORNER CRACKED. FABRICATED ATTACH ANGLE SRM 51-10-02 BOEING DWG 66-24798, DEFECT SIZE: 1 INCH.SDR USAA051037Attach Fitting · corrodedRIGHT AFT O/B VERTICAL FIN ATTACH LUG ON FUSELAGE. MACHINED AFT CHAMFER AND BOR TO CLEAN UP CORROSION & INSTALL NEW BUSHING IAW EA 96788, DEFECT SIZE .080 INCH DEEP.SDR USAA051036Seat Track · crackedBS 662-670, RBL 24 CRACKED. STOP DRILLED CRACKS, INSTALLED REPAIR DOUBLER/CHANNELS IAW EA 96799, DEFECT SIZE: .250 X 2 INCH.SDR USAA051035Seat Track · crackedSEAT TRACK VERTICAL LEG HAS 0250 INCH CRACK AT CUTOUTS FOR FASTENERS. STOP DRILL CRACKS, INSTALL REPAIR ANGLES IAW EA 96799, DEFECT SIZE: 0250 INCH, CRACKED AT CUTOUTS FOR FASTENERS.SDR USAA051034Keelbeam · wornKEEL BEAM LEFT OUTBOARD FLANGE STA 664 TO 727 DAMAGED. REMOVED DAMAGE, FAB & INSTALLED FILLER PLUGS, REPAIR STRAP AND APPROP SHIMS INCLUDED IAW EA 96777, DEFECT SIZE: 60 INCHES OF SURFACE WEAR AT FAIRING ATTACH HOLES AND STRAP.SDR USAA051043Bushing · corrodedVERTICAL FIN LT MOUNT LUGS, AFT FACE CORRODED. REMOVED CORROSION, FABRICATED & INSTALLED BUSHINGS IAW BOEING DWGS 69-72039 & 65-52274 DEFECT SIZE: 1 X 2 INCH AREA.SDR USAA051032Pan · crackedCLT - C4 - PAN AND SERVICE DOOR, .25 INCH CRACK, BS 1000, STRINGER S26R. INSTALLED DOUBLER IAW EA. (K)SDR USAA200508002Pressure Panel · crackedA .75 INCH CRACK FOUND IN LT MLG WHEEL WELL PRESSURE FLOOR WEB STA 665/LBL 30. INSTALLED DOUBLER PER TYPICAL REPAIR 53-60-04A & EA 81311.SDR SB05092Odor · detectedCREW REPORTED A SLIGHT ELECTRICAL/BURNING ODOR IN THE AFT GALLEY. CREW TURNED GALLEY POWER OFF AND ODOR DISSIPATED. MAINTENANCE TURNED GALLEY POWER ON AND INVESTIGATED PROBLEM. COULD NOT VERIFY OR FIND ANY SOURCE OF THE ODOR. AIRCRAFT OK FOR SERVICE.SDR SB05090Circuit Card · faultyAFTER TAKEOFF, ENROUTE, CAPTAIN REPORTED THE RT MLG RED UNSAFE LIGHT ILLUMINATED. CREW RECYCLED THE GEAR AND LIGHT EXTINGUISHED. CAPTAIN ELECTED TO RETURN TO FIELD WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NORMAL GEAR INDICATION OF 3 GREEN LIGHTS WERESDR SWAA052259Tire · separatedAIR TURNBACK, NR 2 MAIN TIRE TREAD SEPARATED AND LOST A SYSTEM HYDRAULICS DURING MAIN GEAR RETRACTION. FOUND LT INBD GROUND SPOILER, LT AILERON BUS CABLE , 4 HYDRAULIC LINES AND LT INBD T/E AFT FLAP DAMAGED. REMOVED AND REPLACED MAIN TIRE ASSY, LT INBD T/E ASDR AWXA200500900Warning System · false activationSJC - ABORTED TAKEOFF - FLT 165 - ABORTED TAKEOFF FOR UNSPECIFIED WARNING. CLEARED RUNWAY THEN RE-ATTEMPTED T/O. TAKEOFF WAS UNEVENTFUL.SDR AWXA200500978Tab · debondedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON UPPER SURFACE OF THE L/H AILERON TAB AT OUTBOARD END. MAINTENANCE REMOVED DISBONDED SKIN ON UPPER SURFACE OF THE L/H AILERON TAB AT THE OUTBOARD END IAW BOEING 737-300 SRM 51-70-07-0. BONDED FISDR USAA050900Angle · corrodedCLT - Q6 - TRANSITION ANGLE, 12 INCH X 1 INCH, CORROSION, AFT CARGO STA 737-767. REMOVED DAMAGE, FABRICATED NEW PART AND INSTALLED IAW SRM. (K)SDR AWXA200500831Light · inoperativeDEN - EEL - DURING 4 DAY CHECK DISCOVERED THE EMERGENCY EXIT LIGHT AT ROW 19C IS INOPERATIVE. MAINTENANCE PLACED ON MEL. REQUIRES NEW LIGHT ASSEMBLY.SDR USAA050886Web · dentedBFM - Q6 - WEB SKIN, 18 INCH X 2.0 INCH X .040 INCH DENT. BS 1016, BTW STR 24R-27R. FAB DOUBLER, FILLER, NEW SKIN SECTION, INSTALLED IAW EA AND SRM. (K)SDR USAA050885Vertical Support · crackedBFM - Q6 - VERTICAL STIFFENER, 1.0 INCH RACK, CRACKED, WHEEL WELL FWD BULKHEAD 663 LBL 6.15. REPLACED STIFFENER IAW EA AND SRM. (K)SDR SWAA052046Bulb · inoperativeDURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.SDR SB05082Battery Pack · dischargedMAINTENANCE REPORTED FORWARD SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT AND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.SDR SB05081Door Seal · out of positionDURING CRUISE, AT APPROX FL320, CABIN PRESSURE WENT TO 10,000 FT WITH CABIN ALT WARNING HORN SOUNDING. CREW ACCOMP EMERGENCY DESCENT TO 10,000 FT AND RETURNED TO FIELD. FLT LANDED W/O FURTHER INCIDENT. NO OXYGEN MASKS WERE DEPLOYED. FLT WAS MX FERRIED FOR SDR SB05080Socket · dirtyMAINTENANCE REPORTED EMERGENCY LIGHT IN SEAT ROW 21 INOPERATIVE. MAINTENANCE CLEANED CONNECTION ON EMERGENCY LIGHT SOCKET AND REPLACED BULB. OPERATIONAL CHECK GOOD.SDR SWAA052010Wire · damagedDURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY LOWER EMERGENCY EXIT LIGHT INOP. REPAIRED WIRES TO LIGHT PER WDM.SDR USAA200506003Skin · crackedA 1.5 INCH CRACK IN SKIN AND HOLE IN STRINGER 22R AT STA 727E, STR 22R. INSTALLED DOUBLER ON SKIN AND STRINGER PER SRM 53-00-01 FIG 229, DET 19 AND 53-00-03 FIG 201.SDR USAA050799Floorbeam · corrodedFOUND FLOORBEAM CORRODED 48 INCHES LONG BY 2 INCHES WIDE BY .035 INCH DEEP, 2.5 INCHES LONG BY 2 INCHES WIDE BY .033, FLOORBEAM, BS 328, RBL 12 INCHES-50 INCHES AND LBL 50 INCHES. FABRICATED PARTS, INSTALLED NEW T-CHORD AND REPAIR ANGLE PER SRM 53-00-51, FIG SDR USAA050798Intercostal · crackedBFM - FOUND WEB/INTERCOSTAL CRACKED .125 INCH, STATION 294.5 STRINGER 7L. INSTALLED ANGLE REPAIR OVER CRACKED AREA PER SRM 53-10-15, 51-70-13. (M)SDR SB05074Outflow Valve · faultyAT FL330, CREW REPORTED CABIN BEGAN A 6,000 FPM CLIMB. AUTO FAIL LIGHT ILLUMINATED ALONG WITH STANDBY ON LIGHT. CREW SWITCHED TO MANUAL AC/DC PRESSURIZATION MODE AND CONFIRMED OUTFLOW VALVE FULLY CLOSED. CREW APPLIED THRUST ON ENGINES AND DESCENDED TO LOWERSDR SB05073Outflow Valve · failedEN ROUTE FROM CLT TO BUF, 100 MILES SOUTH OF PIT, AIRCRAFT LOST AUTO AND STANDBY PRESSURIZATION MODES. HOWEVER, CREW WAS ABLE TO REGAIN CONTROL IN MANUAL PRESSURIZATION MODE AT FL230. DUE TO OPERATIONAL CONCERNS, FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURSDR USAA050768Skin · crackedCLT - FOUND SKIN CRACKED 4 INCHES, STATION 727D, S23R. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 229 DETAIL XI. (M)SDR USAA050767Skin · puncturedCLT - FOUND SKIN PUNCTURED 1 INCH BY 2.5 INCH, BS 312-322 AT S23R. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. (M)SDR SB05070Outflow Valve · inoperativeEN ROUTE WITH THE AUTO PRESSURIZATION ON MEL, LOST CONTROL OF STANDBY PRESSURIZATION MODE. CABIN ALTITUDE BEGAN TO CLIMB, PILOT REQUESTED AN EMERGENCY DESCENT. REGAINED PRESSURIZATION CONTROL AT APPROX FL280. LANDED WITHOUT INCIDENT. MX CLEARED MEL WITH RESDR SB05069Indicator · failedEN ROUTE FROM PHL TO CUN, CREW REPORTED THE STANDBY ATTITUDE INDICATOR FAILED. DECISION WAS MADE TO DIVERT TO CLT FOR REPAIRS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE STANDBY ATTITUDE INDICATOSDR SB05068Circuit Card · unknownON CLIMBOUT FROM CLT, CREW RAISED THE LANDING GEAR AND RECEIVED A RIGHT MAIN LANDING GEAR UNSAFE INDICATION OF BOTH RED AND GREEN LIGHTS. FLIGHT RETURNED TO FIELD AT CLT WITHOUT INCIDENT AND TAXIED TO THE GATE NORMALLY. NO EMERGENCY WAS DECLARED. CREW NOTEDSDR SWAA051724Wire · chafedDIVERSION/DECLARED EMERGENCY. CABIN ALTITUDE HORN SOUNDED, PERFORMRED EMERGENCY PROCEDURE AND INITIATED EMERGENCY DESCENT. REPAIRED WIRING HARNESS ON BLEED VALVE PER WDM.SDR USAA050750Skin · crackedCLT - FOUND FORWARD SERVICE DOOR SKIN CRACKED .620 INCH, UPPER HINGE CUTOUT. REPAIR DOUBLER INSTALLED IAW TR 52-10-13. (M)SDR USAA050738Channel · crackedCLT - C4- CHANNEL, 1 INCH CRACK, NR 3 SLAT JUST BELOW ROD END ACTUATOR ATTACHMENT POINT (L) CHANNEL. FABRICATED AND INSTALLED NEW CHANNEL. (K)SDR AWXA200500668Sign · inoperativePHX - EEL - DURING 4 DAY CHECK, FOUND EMERGENCY EXIT SIGN AT FOWARD LOWER CORNER OF L1 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CK GOOD .SDR SWAA051639Floor Panel · crackedDURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FLOOR WEB CRACKS AT BS 188 TO BS 196, LEFT & RIGHT SIDE, WL 208. REMOVED AND REPLACED WEB SECTIONS PER SRM.SDR SWAA051638Frame · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, LEFT SIDE, WL 208. REPAIRED STUB FRAME PER SRM.SDR SWAA051617Splice · corrodedDURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, BETWEEN STR 27L & STR 28R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.SDR SWAA051620Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 887, STR 9L. REMOVED AND REPLACED CLIP PER SRM.SDR SWAA051619Stringer · crackedDURING SCHEDULED D-CHECK, FOUND BS 1016 AFT PRESS BULKHEAD RADIAL STRINGER CRACKED AT 8 O'CLOCK POSITION. REPAIRED RADIAL STRINGER PER SRM.SDR SWAA051618Shear Tie · corrodedDURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 360, STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.SDR SWAA051622Floorbeam · crackedDURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 727A + 17.5, RBL 44 & RBL 46, WL 208. REPAIRED FLOORBEAM PER BFG ER.SDR SWAA051621Frame · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, RIGHT SIDE, WL 208. REPAIRED STUB FRAME PER SRM.SDR SWAA051610Wedge · delaminatedDURING SCHEDULED D-CHECK, FOUND NR 5 L/E SLAT UPPER INBOARD T/E WEDGE DELAMINATED. REPAIRED NR 5 SLAT PER SRM.SDR SWAA051609Wedge · delaminatedDURING SCHEDULED D-CHECK, FOUND NR 4 L/E SLAT UPPER INBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER MM.SDR SWAA051608Skin · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 7, STR 24L. REPAIRED SKIN PER SRM.SDR SWAA051607Stringer · corrodedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 363, STR 25R. REMOVED AND REPLACED STRINGER SECTION PER SRM.
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