Boeing 737-2B7

Service difficulty reports · 1,360

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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 = '7372B7'
  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.

SDR USAA000750Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .025 INCH, BS 663, STRINGER 10R. INSTALLED TIE CLIP PER EO 5393G227. (M)May 31, 2000 · N283AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000749Tie Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .5 INCHES, STATION 639 LT, STRINGER 4L. REPLACED CLIP PER SRM 51-10-1. (M)May 31, 2000 · N283AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000748Tie Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .5 INCH, STATION 616 LT, STRINGER 2L. INSTALLED TIE CLIP PER EO 5393G227. (M)May 31, 2000 · N283AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000747Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 616 RT, STRINGER 2R. REPLACED TIE CLIP PER SRM 51-10-1. (M)May 31, 2000 · N283AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000746Tie Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .5 INCH, STATION 597 LT, STRINGER 9L. INSTALLED TIE CLIP PER SRM 51-10-1. (M)May 31, 2000 · N283AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000745Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCHES, BS 344, STRINGER 2R. INSTALLED TIE CLIP PER EO 393G227. (M)May 31, 2000 · N283AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000744Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, BS 344, STRINGER 1. INSTALLED TIE CLIP PER EO 5393G227. (M)May 31, 2000 · N283AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000742Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED .250 INCH, BS 520, LBL 45. INSTALLED DOUBLER AND ANGLES PER EA 67167. (M)May 31, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000741Seat Track · crackedCLT - FOUND SEAT TRACK ANGLE CRACKED .5 INCH, BS 520 AND RBL 24.75. INSTALLED REPAIR ANGLE PER EA 67167. (M)May 31, 2000 · N278AU · Boeing 7372B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA000740Doubler · crackedCLT - FOUND DOUBLER WITH TWO 1 INCH CRACKS, ANTENNA DOUBLER, AFT OF STATION 500 FRAME. REPAIRED PER 53-00-01. (M)May 31, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA000734Frame · corrodedCLT - FOUND CORROSION 1 INCH BY 32 INCH, TOP OF STATION 520 LBL 12 TO RBL 20. INSTALLED FILLER AND DOUBLER PER SRM 51-40-3. (M)May 23, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA000730Skin · crackedCLT - FOUND SKIN CRACKED .125 INCH, AFT SERV DOOR LOWER CORNER. INSTALLED DOUBLER PER SRM 53-30-3. (M)May 23, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA000729Stringer · corrodedCLT - FOUND STRINGER CORRODED 2 INCHES BY 6 INCHES, STRINGER 26L AT FS 907. INSTALLED REPAIR SPLICE PER SRM 53-10-3. (M)May 23, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA000728Stringer · corrodedCLT - FOUND STRINGER CORRODED 2 INCH BY 2 INCH AREA, STRINGER 21L AT STATION 907. INSTALLED NEW STRINGER SPLICE PER SRM 51-10-02. (M)May 23, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA000727Stringer · corrodedCLT - FOUND STRINGER CORRODED 1 INCH BY 1 INCH TWO PLACES, STRINGER 21L BETWEEN FS 807 AND 827. REPLACED SECTION SECTION PER SRM 53-10-03. CORROSION LEVEL 2. (M)May 23, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA000717Floorbeam · corrodedCLT - Q-4, FLOORBEAM HAD 3 INCH CORROSION LEVEL 1. REPLACED T-CAP PER TR 53-10-04 B. (X)May 16, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000716Fitting · crackedCLT - Q-4, FITTING HAD .50 INCH CRACK. REPAIRED PER TR 57-40-10. (X)May 16, 2000 · N278AU · Boeing 7372B7 · Main Landing Gear Attach SectionSDR USAA000707Floorbeam · crackedCLT - Q-4, FLOORBEAM HAD 1.5 INCH CRACK, BS 520 AND RBL 24.75. REPLACED REPAIR ANGLE PER EA 67167 AND SB 737-53-1120. (X)May 15, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000706Floorbeam · crackedCLT - Q-4, FLOORBEAM HAD 1.5 INCH CRACK, BS 520 AND RBL 45.5. INSTALLED NEW DOUBLER AND CHANNEL PER SB 737-53-1120 AND EA67167. (X)May 15, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000705Seat Track · crackedCLT - Q-4, SEAT TRACK HAD .50 INCH CRACK, BS 520 AND LBL 24.75, SEAT TRACK SUPPORT ANGLE. REPLACED REPAIR ANGLE PER SRM 51-30-2. (X)May 15, 2000 · N278AU · Boeing 7372B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA000714Stringer · corrodedCLT - Q-4, STRINGER HAD CORROSION, 1 INCH BY 24 INCHES, STR 20L FROM BS 727A TO 727B. REPLACED STRINGER PER SRM 53-10-3, FIG 1 AND EA 67215. (X)May 15, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA000709Skin · crackedCLT - Q-4, SKIN HAD 1 INCH CRACK, STA 344, STR 17 RT FORWARD SERVICE DOOR, LOWER AFT CORNER. INSTALLED TRIPLER PER SRM 53-30-3 AND EA 67235. (X)May 15, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA000708Floorbeam · crackedCLT - Q-4, FLOORRBEAM HAD 1.50 INCH CRACK, BS 520 AND LBL 24.75. NEW PART INSTALLED PER EA 67167. (X)May 15, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000702Floorbeam · corrodedCLT - T-CAP FLOORBEAM HAD LEVEL 1 CORROSION, .50 INCH, BETWEEN LBL 37 AND RBL 34, STA 947.5 T-CAP. (X)May 11, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000674Stringer · crackedCLT - 18-A SHELF CRACKED, .50 INCH. REPLACED SHELF PER SRM 51-10-01. (X)May 8, 2000 · N278AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAASB00136Combustion Liner · failedJAX - FLT 2612 - FLIGHT WAS EN ROUTE FROM BWI TO TPA WITH THE NR 1 GENERATOR ON MEL, WHEN THE APU SHUT DOWN. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND DIVERTED TO THE NEAREST SUITABLE AIRPORT AT JAX. FLIGHT LANDED WITHOUT FURTHER INCIDENT. May 7, 2000 · N266AU · Boeing 7372B7 · APU Core EngineSDR USAASB00134Hose · failedIAD - FLT 2755 - DURING CLIMB-OUT FROM IAD, THE NOSE LANDING GEAR WOULD NOT RETRACT. CREW NOTICED A DROP IN HYDRAULIC PRESSURE. THE NOSE LANDING GEAR NEVER UNLOCKED AS A STEADY NOSE GEAR GREEN LIGHT REMAINED ILLUMINATED. FLIGHT RETURNED TO FIELD AT IAD AND May 6, 2000 · N268AU · Boeing 7372B7 · Hydraulic System, MainSDR USAASB00131Start Valve · failedTPA - FLT 2999 - CLIMBING THROUGH 7,000 FEET OUT OF TPA, THE NR 1 ENGINE START VALVE LIGHT ILLUMINATED. CAPTAIN WENT THROUGH PROCEDURES, DECLARED AN EMEREGNCY AND SHUT DOWN THE NR 1 ENGINE PER PROCEDURES. FLIGHT RETURNED TO FIELD AT TPA AND LANDED WITHOUT FUMay 3, 2000 · N268AU · Boeing 7372B7 · Engine Start Valves/ControlsSDR USAA000691Skin · crackedPIT - SKIN HAD 3 CRACKS, 1 INCH, .50 INCH, 1 INCH, RT AFT FUSELAGE STA 1064 STR 21R. CUT SKIN SECTION .50 INCH BY 2 INCHES AND INSTALLED DOUBLER AND FILLER PER SRM 53-30-3. (X)May 3, 2000 · N288AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA000689Stringer · crackedPIT - STRINGER CRACKED .75 INCH, IN HAT OF STRINGER, RT AFT FUSELAGE, STA 1064L 16R. REMOVED DAMAGED STRINGER, SPLICED IN NEW SECTION WITH SPLICES FORWARD AND AFT OF BULKHEAD PER SRM 53-10-3. (X)May 3, 2000 · N288AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA000597Fitting · crackedCLT - FOUND FITTING CRACKED .5 INCH, RIGHT MIG BEAM OUTBOARD SUPPORT FITTING ABOVE BEAM CUTOUT. NDT PERFORMED BOLTS REINSTALLED PER TR 57-40-10. (M)Apr 24, 2000 · N279AU · Boeing 7372B7 · Wing Miscellaneous StructureSDR USAA000596Frame · crackedCLT - FOUND TWO CRACKS .25 INCH, FS 1064, BETWEEN STRINGER 7R AND 8R. REPAIRED WITH FILLER AND DOUBLER PER EA 67009. (M)Apr 24, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAASB00122Sensor · failedTPA - FLT 2647 - DURING TAKEOFF FROM TPA, THE CAPTS CONTROL WHEEL BEGAN TO VIBRATE. THE F/O WAS FLYING THE AIRCRAFT AT THE TIME AND HIS SIDE WAS OK WITH NO PROBLEM CONTROLLING THE AIRCRAFT. CREW PLACED THE GEAR AND FLAPS DOWN AND CHECKED THE C/B. CAPTS CONTApr 23, 2000 · N279AU · Boeing 7372B7 · Stall Warning SystemSDR USAASB00121Actuator · failedATL - FLT 2967 - ON DESCENT INTO ATL, WHILE EXTENDING FLAPS, CAPTAIN VISUALLY CONFIRMED THE NR 1 SLAT WAS NOT FULLY EXTENDED. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND DECLARED AND EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT AT ATL. MAINTENANCE REApr 23, 2000 · N268AU · Boeing 7372B7 · Leading Edge Slat ActuatorSDR USAASB00123Compressor · damagedBWI - FLT 2697 - AFTER A NORMAL TAKEOFF, ON CLIMB-OUT FROM BWI, THE NR 1 ENGINE SURGED THREE TO FOUR TIMES. CREW ACCOMPLISHED ENGINE STALL CHECKLIST AND OPERATED THE NR 1 ENGINE WITH REDUCED THRUST. THE NR 1 ENGINE RESPONDED TO THROTTLE REDUCTION. CREW DECLApr 23, 2000 · N275AU · Boeing 7372B7 · Engine (Turbine/Turboprop)SDR USAASB00118Wire · chafedBWI - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHTS ILLUMINATED VERY DIM WITH THE COCKPIT SWITCH IN THE ARMED AND OFF POSITION. MAINTENANCE REPAIRED A CHAFED WIRE. OPERATIONAL CHECK GOOD. (X)Apr 20, 2000 · N285AU · Boeing 7372B7 · Light System WiringSDR USAA000573Shear Tie · corrodedCLT - FOUND FRAME SHEAR TIE CORRODED 6 INCHES BY 2 INCHES, FRAME 727A BETWEEN STRINGER 26L TO 27L. CORROSION LEVEL 1. REPLACED SHEAR TIE PER SRM 53-10-02. (M)Apr 17, 2000 · N279AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000572Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH BY .125 INCH, BS 340, STRINGER 17L. REPAIRED FILLER, DOUBLER AND TRIPLER PER EO 5391G694. (M)Apr 17, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA000556Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1 INCH, UPPER RADIUS FLOORBEAM STATION 520 AT RBL 24.75. REPAIRED PER SB 737531120 AND EA 66956A. (M)Apr 14, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000558Skin · crackedCLT - FOUND FUSELAGE CRACKED, .120 INCH, STATION 947 AFT ENTRY DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER, FILLER AND TRIPLER PER SRM 53-30-03 FIG 34. (M)Apr 14, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA000563Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED, .5 INCH BY .5 INCH, STATION 986.5, LBL 15 TO RBL 56. CORROSION LEVEL 2 NR C53-107-02. REPAIRED PER TR 53-60-0. (M)Apr 14, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000551Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1.7 INCH, STATION 520, LBL 45.5 FLOORBEAM RADIUS. REPAIRED FILLER, DOUBLER PER EA 66956A. (M)Apr 13, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000552Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED .4 INCH, STATION 520, RBL 45.5 FLOORBEAM RADIUS. REPAIRED FILLER, DOUBLER PER EA 66956A. (M)Apr 13, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000553Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED .4 INCH AND .7 INCH, STATION 520, LBL 24.75. REPAIRED FILLER, DOUBLER PER EA 66956A. (M)Apr 13, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000545Structure · crackedCLT - FOUND 1 INCH CRACK IN SHELF, STATION 727, STRINGER 18R AFT INBOARD RIVET. INSTALLED DOUBLER PER SRM 51-10-1. (M)Apr 12, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, StructureSDR P2EA00111Spoiler · out of adjMCI - FLT 564 - DURING DESCENT, SPEED BRAKE DEPLOYMENT CAUSED AIRCRAFT TO ROLL TO THE LEFT DURING INITIAL DEPLOYMENT ONLY AT HIGHER SPEEDS. OK BELOW 250 KTS. ADJUSTED ALL FLIGHT SPOILERS PER MM 27-61-51 AND 27-61-0. PERFORMED EVALUATION FLIGHT. CREW REPORTApr 11, 2000 · N127NJ · Boeing 7372B7 · Drag Control SystemSDR USAASB00105Power Supply · failedMCO - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT FAILED TO TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (PN 61-0478-9) AND POWER SUPPLY. OPERATIONAL CHECK GOOD. (X)Apr 6, 2000 · N273AU · Boeing 7372B7 · Emergency LightingSDR USAASB00102Battery Pack · dischargedSYR - MAINTENANCE FOUND THE EXTERIOR OVERWING EMERGENCY LIGHT, RIGHT SIDE, INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)Apr 5, 2000 · N273AU · Boeing 7372B7 · Emergency LightingSDR USAA000529Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH, STATION 827, STRINGER 13L AT RIVET EXT. REPAIRED FILLER AND DOUBLER PER SRM 53-10-4 FIG 2. (M)Apr 5, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA000527Frame · crackedCLT - FOUND 1 INCH CRACK IN FRAME, STATION 400, LEFT BETWEEN STRINGER 13 AND 14 FRAME. REPLACED DOUBLER AND SHEAR TIE PER EA 66975 AND SRM 53-10-04. (M)Apr 5, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, Frame
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