Boeing 737-3B7
Service difficulty reports · 4,722
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 = '7373B7' 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 = '7373B7' 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 USAA070694Angle · corrodedSTA 344 - 312 FWD ENTRY WAY, LT SIDE HAS CORROSION. REPLACED DAMAGED Z-ANGLE WITH NEW PER SRM 51-10-02, 51-40-03; CORR TASK C53-107-02, DEFECT SIZE: .750 INCH.SDR USAA070693Frame · corrodedSTA 727E, LBBL 8 ON FRAME WHERE IT ATTACHES TO SKIN EXFOLIATED. FABRICATED REPAIR PART & INSTALLED PER SRM 53-60-07; CORR TASK C53-208-01, DEFECT SIZE: 1 INCH.SDR USAA070702Stringer Clip · corrodedSTA 767, S26L, STRINGER TIE CLIP HAS CORROSION. REPLACED STRINGER TIE CLIP PER SRM 51-20-01, 51-10-02; CORR TASK C53-202-01, DEFECT SIZE: .5 INCH.SDR SB07074Relay · faultyCLT - FLT 1979 AFTER TAKEOFF FROM CLT, EN ROUTE TO EWR, CREW COULD NOT RAISE THE LANDING GEAR HANDLE. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND WAS ABLE TO RAISE GEAR HANDLE USING THE OVERRIDE TRIGGER. FLIGHT RETURNED TO FIELD AT CLT AND LASDR USAA070677Skin · crackedPYLON ABOVE NR 2 ENGINE O/B SIDE OF LOAD FITTING PIN HAS CRACK. REMOVED REPAIR, CLEANED AREA, INSTALLED REPAIR WET WITH SEALANT PER TR 57-41-02, DEFECT SIZE: .5 INCH.SDR USAA070690Panel · crackedTOP OF RT ENGINE PYLON AT PANEL 5828R OPENING HAS CRACK. INSTALLED DOUBLER PER TYP REP 54-30-07, DEFECT SIZE: .75 INCH.SDR USAA070689Skin · crackedSKIN AT BS 727E + 13 INCHES JUST BELOW S-23L HAS CRACK. FAB'D & INSTALLED DOUBLER PER SRM 53-00-01, REP 31, DEFECT SIZE: 0.2 INCH.SDR USAA070688Skin · damagedWS 72, RIGHT WING, LOWER SURF, Z-ANGLE 3 FWD ATTACH FASTENERS ELONGATED. REMOVED FASTENERS, OVERSIZE & COLD WORK HOLES, & INSTALLED FIRST-OVER FASTENERS PER SRM 51-40-02, 51-40, DEFECT SIZE: .125 INCHES.SDR USAA070687Skin · damagedTHREE WORKING FASTENER RIGHT WING TO CENTER SECTION Z-ANGLE AT WS 72, AFT 3 FASTENERS ELONGATED. OVERSIZED FIRST OVER, COLD WORKED HOLES & INSTALLED NEW FASTENERS PER SRM 51-40-02, 51-40-03, 51-40-, DEFECT SIZE: .125 INCHSDR USAA070686Wedge · debondedNR 3 SLAT UPPER OUTBOARD WEDGE DISBONDED. INSTALLED REPAIR PARTS PER SRM 51-70-17, 51-70-10, DEFECT SIZE: 1.5 X 2 INCHES.SDR USAA070685Skin · damagedNR 4 SLAT T/E WEDGE HAS ERODED SKIN & DISBOND ON LOWER SURFACE I/B SIDE OF SLAT. REMOVED DISBONDED AREA, INSTALLED REPAIR PARTS PER TR 57-42-03, SRM 51-70-10, DEFECT SIZE: 2 X 3 INCHES.SDR USAA070683Skin · gougedNR 2 SLAT O/B END UPPER SURFACE, SLAT WEDGE SKIN, GROOVE/GOUGE. INSTALLED NEW CORE FILLER & NEW UPPER SURFACE BONDED DOUBLER PER SRM 57-43-01, 51-70-10, DEFECT SIZE: 1.25 X .250 INCH.SDR USAA070682Skin · damagedUPPER SURFACE, LOCATED 19.5 INCHES FWD OF ELEV TAB T/E & 37 INCHES OUTBOARD OF INBOARD T/E TIP HAS DAMAGE. REPAIR INSTALLED CONFORMS TO SRM 55-20-01 REPAIR 1, DEFECT SIZE: 5 INCH DIA.SDR USAA070681Skin · damagedRIGHT ELEV UPPER SKIN, UPPER SURFACE LOCATED 12 INCHES FWD OF T/E & 16 INCHES INBOARD T/E TIP HAS DAMAGE. REPAIR INSTALLED CONFORMS TO SRM 55-20-01 REPAIR 1, DEFECT SIZE: 8 INCH DIA.SDR USAA070680Seat Track · crackedSTA 727B RBL 24.75 HAS CRACK. INSTALLED FABRICATED REPAIR PARTS PER EA 98824, DEFECT SIZE: 3 INCH.SDR USAA070691Panel · crackedTOP OF PYLON 2 PANEL 5727L OPENING HAS CRACK. INSTALLED DOUBLER PER TR 54-30-07, DEFECT SIZE: .5.SDR USAA070678Skin · crackedLEFT WING FIXED LEADING EDGE LOWER SKIN PANEL AT SLAT STA 3.25 HAS CRACK. REMOVED DAMAGE, FAB'D & INSTALLED REPAIR PARTS PER BOEING TR 57-41-02, DEFECT SIZE: .75 INCH.SDR USAA070676Stiffener · crackedSTA 294 BETWEEN STR S10R & S11R, ANGLE STIFFENER HAS CRACK. REMOVED & REPLACED ANGLE STIFFENER WITH NEW PART PER SRM 51-10-02, DEFECT SIZE: .5 INCH.SDR USAA070675Door Frame · crackedBS 492.4 STR 24R FWD CARGO DOOR FRAME HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART; INSTALLED NEW FRAME PER SRM 5-40-00, 53-00-53, DEFECT SIZE: .75 INCH.SDR USAA070674Web · crackedSTA 294.5, S7L HAS CRACK. FABRICATED NEW WEB AND INSTALLED PER BOEING DWG 65-17684, DEFECT SIZE: .350 INCH.SDR USAA070673Intercostal · crackedBS 500 BENEATH RIGHT TRANSITION ANGLE, INTERCOSTAL BAFFLE HAS CRACK. FABRICATED NEW INTERCOSTAL BAFFLE DEFECT SIZE: .375 INCH.SDR USAA070672Frame · crackedSTA 867 AT I/B FASTENER FOR A/C SUPPORT BRACKET, BETWEEN STR 8 & 9R HAS CRACK. INSTALLED TYPICAL FRAME REPAIR DOUBLER PARTS PER TR 53-10-20E, DEFECT SIZE: .125 INCH.SDR USAA070671Stringer Splice · crackedSTA 360 S14L, STRINGER SPLICE HAS CRACK. DRILLED UP NEW PART & INSTALLED PER SRM 51-40-02, DEFECT SIZE: .500 INCH.SDR USAA070670Structure · crackedTHE 500A AND 500B AT STR 26L AT LIGHTENING HOLE HAS CRACK. MANUFACTURED NEW PART PER SRM 53-30-04, 51-10-02, DEFECT SIZE: .375 INCH.SDR USAA070669Door Frame · crackedFWD PAX DOOR FRAME CRACKED AT NR 6 STOP PIN CUTOUT. INSTALLED DOUBLER REPAIR PER EA 98819, DEFECT SIZE: .125 INCH.SDR USAA070668Door Frame · crackedFWD PAX DOOR FRAME CRACKED AT NR 5 STOP PIN CUTOUT. INSTALLED DOUBLER REPAIR PER EA 98819, DEFECT SIZE: .125 INCH.SDR USAA070667Door Frame · crackedFWD PAX DOOR FRAME CRACKED AT NR 7 STOP PIN CUTOUT. INSTALLED DOUBLER REPAIR PER EA 98819, DEFECT SIZE: .125 INCH.SDR USAA070679Skin · crackedNR 6 SLAT, LOWER T/E AT OUTBOARD END, CRACKED AT RIVET HOLES. INSTALLED FILLER/DOUBLER REPAIR PER SRM 57-43-01, DEFECT SIZE: .125 INCH.SDR USAA200708005Strap · corrodedA 1 X 1 INCH CORRODED AREA AT STA 795 I/B OF STR 25R. REPLACED STRAP PER SRM 51-10-02.SDR USAA070664Skin · crackedSTA 727D + 17" TO +19", .5 INCH ABOVE STR 22L CENTER LINE HAS CRACK. DOUBLER REPAIR FROM .050 2024-TS INSTALLED PER SRM 53-00-01, REP 31, DEFECT SIZE: 2 INCHES.SDR USAA070665Door Frame · crackedFWD PASSENGER DOOR FRAME CRACKED AT 37 STOP PIN CUTOUT, L1 DOOR, FWD ENTRY DOOR. INSTALLED DOUBLER REPAIR PER EA 98819, DEFECT SIZE: .125 INCH.SDR USAA070652Intercostal · crackedBS 294.5 & S76 HAS CRACK. REPLACED INTERCOSTAL IAW 51-10-02, DEFECT SIZE: .0625 INCH.SDR USAA070653Intercostal · crackedBS 294.5, S-12L, WEB INTERCOSTAL HAS CRACK. REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: .25 INCH.SDR USAA070654Intercostal · crackedBS 294.5, S-15L, WEB INTERCOSTAL HAS CRACK. REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.SDR USAA070655Skin · crackedBS 407 RBL 1.5, RADIUS ALTIMETER CUTOUT HAS CRACK. INSTALLED REPAIR DOUBLER, FILLER & ADIO ALT PER T/R 53-30-71, DEFECT SIZE: .25.SDR USAA070656Stringer · crackedBS 360 STR 15L HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PER SRM 51-10-02, DEFECT SIZE: .5 INCH.SDR USAA070657Intercostal · crackedSTA 294.5, S-11L, INTERCOSTAL WEB, CRACK IN RADIUS. REMOVED WEB, FABRICATED NEW & INSTALLED PER DWG 50-07946, SRM 51-10-02, DEFECT SIZE: 0.25 INCH.SDR USAA070660Stringer · crackedSTR 15L AT STA 360 HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SM 51-40-00, DEFECT SIZE: 0.7 INCH.SDR USAA070661Fitting · crackedCLIP AT STA 947.5 STR 24L, FWD OF WATER SERVICE PANEL HAS CRACK. FAB'D NEW ANGLE PER BOEING DWG 65-51626 & INSTALLED PER SRM 51-10-02, DEFECT SIZE: .25 INCH.SDR USAA070662Stringer · crackedSTA 500 & 500A STR 26L AT LIGHTENING HOLE HAS CRACK. MANUFACTURED NEW PART PER SRM 51-10-02, 53-30-04, DEFECT SIZE: .5 INCH.SDR USAA070663Bulkhead · crackedSTA 727 RBL 40 FWD BULKHEAD, AFT CARGO CRACKED. FABRICATED WEB STIFFENER BRACKET & INSTALLED PER SRM 52-40-02, DEFECT SIZE: 1 INCH.SDR SB07071Solenoid · faultyCLT - AFTER TAKEOFF FROM CLT, DURING GEAR RETRACTION FROM UP TO OFF, CREW RECEIVED TWO MAIN LANDING GEAR RED LIGHTS AND A LEFT MAIN LANDING GEAR GREEN LIGHT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACESDR SB07062Light · inoperativeDCA - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. MAINTENANCE REPAIRED THE LIGHT ASSEMBLY AT SEAT 22C. OPERATIONAL CHECK GOOD.SDR SB07060Power Supply · inoperativeBOS - MAINTENANCE REPORTED THE R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY ALONG WITH THE BATTERY PACK. OPERATIONAL CHECK GOOD.SDR SB07059Circuit Card · unknownPHL FLT1407 - AFTER TAKEOFF FROM PHL, CREW RECEIVED BOTH MAIN LANDING GEAR RED UNSAFE LIGHTS AFTER RAISING GEAR AND RETURNING GEAR LEVER TO OFF POSITION. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES, CONSULTED MAINTENANCE AND RETURNED TO FIELD AT PHLSDR AWXA200700952Windshield · crackedIAH - PHX - DIV - LOG 7829027 - CREW REPORTED, AT CRUISE THE AIRCRAFT WAS STRUCK FROM AN UNKNOWN OBJECT CRACKING THE FO'S SIDE WINDOW. THE CREW DEPRESSURIZED, DESCENDED TO FL 100, DECLARED AN EMERGENCY AND DIVERTED TO ELP. THE LANDING WAS UNEVENTFUL. MX REPSDR USAA070580Beam · crackedSTA 259.5 AT NOSE W/W CEILING WL 192.5, BL 0, RADIUS OF NOSE GEAR ACT BEAM. REPLACED GUSSET PER SRM 51-10-02, DEFECT SIZE: .75 INCH.SDR SB07057Windshield · crackedJAX - FLT 983 - ON DESCENT INTO JAX, THE CAPTAIN'S NR 1 WINDSHIELD ARCED AND THEN CRACKED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S NR 1 WINDSHIELD PER JOB CARD J356-11-01. ALSO, REMOVED AND REPLACED WINDOW HEATSDR USAA200707003Skin · crackedA .375 INCH LONG CRACK AT RT REAR SERVICE DOOR UPPER HINGE CUTOUT. INSTALLED DOUBLER REPAIR PER SRM 53-60-01 FIG 201.SDR SB07053Battery Pack · dischargedPIT - MAINTENANCE REPORTED THE AFT GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT BATTERY PACK. OPERATIONAL CHECK GOOD.
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