Boeing 737-2B7

Service difficulty reports · 1,360

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 = '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 USAA000519Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 807, STRINGER 10L TIE CLIP. REPLACED TIE CLIP PER EO5393G227. (M)Apr 4, 2000 · N279AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000518Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .375 INCH, STATION 559, STRINGER 4R TIE CLIP. REMOVED AND INSTALLED PER SRM 51-10-02. (M)Apr 4, 2000 · N279AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000525Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH BY .5 INCH, STATION 947.5 LBL 4. REPAIRED FILLER, DOUBLER AND SPLICE ANGLES PER SRM 53-10-09 DET 1. CORROSION LEVEL 2. (M)Apr 4, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000514Skin · crackedCLT - .75 INCH SKIN CRACK, RIGHT FORWARD SERVICE DOOR JUST ABOVE LOWER HINGE CUTOUT. REMOVED CRACK AND INSTALLED DOUBLER PER SRM 52-00-03. (M)Mar 31, 2000 · N279AU · Boeing 7372B7 · Service DoorsSDR USAA000511Skin · crackedTPA - FOUND .25 INCH CRACK IN DOOR SKIN, AFT UPPER CORNER RADIUS OF HAND HOLD OPENING. INSTALLED DOUBLER PER TR 52-30-03 REV A. (M)Mar 30, 2000 · N287AU · Boeing 7372B7 · Cargo/Baggage DoorsSDR USAA000505Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH BY .5 INCH, STATION 967, LBL 6 TO RBL 53. INSTALLED STRAPS PER EA 66921. CORROSION LEVEL 2. (M)Mar 30, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000500Floorbeam · corrodedCLT - FOUND .5 INCH BY .5 INCH CORROSION, BS 1016, LBL 7 TO LBL 16. INSTALLED STRAP REPAIR PER EA 66920. (M)Mar 29, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000499Floorbeam · corrodedCLT - FOUND 2 INCHES OF CORROSION ON FLOORBEAM, BS 312 AT BL 0, LBL 7 AND LBL 10. INSTALLED T-CAP REPAIR PER TR 53-10-13. CORROSION LEVEL 1. (M)Mar 29, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000480Floorbeam · crackedCLT - FOUND TWO CRACKS IN FLOORBEAM, STATION 706, BL 0 LOWER CHORD FLOORBEAM WEB. REPAIRED FILLER AND DOUBLER PER TR 57-10-05. (M)Mar 28, 2000 · N279AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAASB00090Sensor · failedFLL - FLT 2828 - AFTER TAEKOFF FROM FLL, AT 200 FEET, THE STICK SHAKER ACTIVATED. AIRCRAFT SLOWED TO 250 KNOTS AND FLAPS WERE RETRACTED BUT STICK SHAKER CONTINUED. DURING RETURN TO FIELD TO FLL, STICK SHAKER WAS INTERMITTENT. FLIGHT LANDED WITHOUT FURTHER IMar 28, 2000 · N277AU · Boeing 7372B7 · Stall Warning SystemSDR USAA000463Tie Clip · crackedCLT - DURING Q-5 CHECK, FOUND TIE CLIP CRACKED .250 INCH, STATION 747, STRINGER 6L. REPAIRED PER EO 5393G227. (M)Mar 27, 2000 · N279AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000462Tie Clip · crackedCLT - FOUND Q-5 CHECK TIE CLIP .150 INCH CRACK, STATION 663.75, STRINGER 10L. REPAIRED PER EO 5393G227. (M)Mar 27, 2000 · N279AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000461Tie Clip · crackedCLT - FOUND TIE CLIP .150 INCH CRACK, STATION 847, STRINGER 10L. REPAIRED PER EO 5393G227. (M)Mar 27, 2000 · N279AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000460Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .025 INCH, STATION 827, STRINGER 6L TIE CLIP. REPAIRED PER EO 5393G227. (M)Mar 27, 2000 · N279AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAASB00087Engine · contaminatedTPA - FLT 2636 - ON CLIMB-OUT FROM TPA, CAPT REPORTED A HEAVY PLASTIC TYPE SMELL COMING FROM THE AIR CONDITIONING SYSTEM. SUPPLY DUCT TEMPERATURE NEVER WENT ABOVE 25 DEGREES. NO ABNORMAL INDICATIONS WERE NOTED. SMELL WENT AWAY AS POWER WAS REDUCED BUT CAME Mar 25, 2000 · N271AU · Boeing 7372B7 · Engine (Turbine/Turboprop)SDR USAA000452Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED 1.125 INCH, AFT END OF E/E COOLING DUCT OUTLET. INSTALLED DOUBLER PER TR 53-30-04 AND DWG 65C33930. (M)Mar 23, 2000 · N269AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB00078Coupler · failedTPA - FLT 8050 - FLIGHT RETURNED TO FIELD AT TPA DUE TO EXCESSIVE RUDDER TRIM TO MAINTAIN WINGS LEVEL. A CORRECTION OF 3 TO 3.5 DEGREES LET, AT 250 KNOTS, AT FL100 WAS REQUIRED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCEMar 22, 2000 · N278AU · Boeing 7372B7 · Autopilot SystemSDR USAA000385Skin · crackedTPA - FOUND FUSELAGE SKIN 2.24 INCH CRACKED, STATION 767, STRINGER 19R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)Mar 20, 2000 · N269AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA000339Strap · crackedCLT - FOUND 6 INCH, STATION 1138, STRINGER 5L ABOVE LEFT HORIZ STAB INTERIOR. INSTALLED DOUBLER AND REPAIR ANGLE PER EA 66738 AND SRM 53-00-01. (M)Mar 10, 2000 · N277AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000338Frame · crackedCLT - FOUND .2 INCH CRACK, BS 1138, STRINGER 12L. INSTALLED DOUBLER AND TRIPLER PER EA 66783. (M)Mar 10, 2000 · N277AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA000310Web · crackedCLT - FOUND .5 INCH CRACK, BS 706 TO 714. INSTALLED NEW SPLICE AND FILLER. (M)Mar 6, 2000 · N277AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000311Web · crackedCLT - FOUND 2 CRACKS, 1.5 INCH AND .375 INCH, FORWARD CARGO DOOR, INNER SKIN LIGHTENING HOLES FORWARD CARGO DOOR. REPAIRED PER EA 66767. (M)Mar 6, 2000 · N277AU · Boeing 7372B7 · Cargo/Baggage DoorsSDR USAA000297Stringer · corrodedCLT - FOUND CORROSION 8 INCHES BY 3 INCHES, AT STATION 968, STRINGER 25L FROM FORWARD EDGE OF STRINGER. SPLICED IN NEW STRINGER PER SRM 53-10-3. CORROSION LEVEL 2. (M)Mar 3, 2000 · N277AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA000293Stringer · corrodedCLT - FOUND 1 INCH OF CORROSION AT BS 908, STRINGER 20L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-10-1. CORROSION LEVEL 1. (M)Mar 2, 2000 · N277AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA000291Frame · crackedFRAME CRACKED AT BS 767, STRINGER 13L. INSTALLED DOUBLER PER SRM 53-10-4. (M)Feb 29, 2000 · N277AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA000283Stringer · crackedCLT - FOUND 7 INCH CRACK, 3 INCHES AFT PLUS 4 INCHES FORWARD OF STATION 967, STRINGER 27L. NEW SECTION OF STRINGER AND DOUBLER PER SRM 53-10-3. (M)Feb 28, 2000 · N277AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA000284Frame · crackedCLT - FOUND CRACK .375 INCH, BS 747, STRINGER 13L. INSTALLED DOUBLER PER SRM 51-40-3. (M)Feb 28, 2000 · N277AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA000285Frame · crackedCLT - APU CHANGE, FOUND FUSELAGE FRAME HAS 3 INCH CRACK, STATION 1138 JUST BELOW TOP APU TORQUE BOX LEFT SIDE. REPAIRED PER SRM 51-40-3 FIG 1. (M)Feb 28, 2000 · N266AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA000282Floorbeam · corrodedCLT - FOUND CORROSION LEVEL 1, 2 INCHES BY 12 INCHES, STATION 244, LBL 44 TO LBL 56 FLOOR LEVEL. INSTALLED REPAIR PER TR 53-10-13. (M)Feb 28, 2000 · N277AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000258Web · crackedWEB HAS TWO .5 INCH CRACKS AT BS 711 AND 714 RBL 24.75. INSTALLED SPLICE AND FILLER PER SRM 51-40-02-18. (M)Feb 24, 2000 · N277AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000259Skin · crackedSKIN CRACKED AT BS 378 BETWEEN STRINGER 21L AND 22L. INSTALLED REPAIR DOUBLER PER TR 53-30-03. (M)Feb 24, 2000 · N277AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA000264Stringer · crackedTPA - STRINGER HAS A 1 INCH CRACK AT BS 1138. REMOVED CRACK FABRICATED PART PER SRM 51-10-3 PAGE 1-9. (M)Feb 24, 2000 · N266AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA000156Floorbeam · corrodedCLT - FOUND 3 FEET OF CORROSION ON FLOORBEAM, STATION 312, LBL 13 TO RBL 13. INSTALLED FILLER AND DOUBLER PER SRM 53-10-9. (M)Feb 22, 2000 · N277AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000255Web · crackedCLT - FOUND 1 INCH CRACK IN WEB PLATE, BS 947 PLUS 1, STRINGER 11L FWD AFT ENTRY. INSTALLED DOUBLER PER TR 53-30-07. (M)Feb 22, 2000 · N277AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000245Frame · corrodedCLT - FRAME CORRODED AT BS 273. REMOVED CORROSION PER SRM 53-10-1. (M)Feb 22, 2000 · N277AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA000246Angle · corrodedCLT - Z ANGLE HAS 2 INCH BY 8 INCH SECTION OF CORROSION AT BS 967-986.5. REPLACED Z ANGLE PER SRM 51-10-2. (M)Feb 22, 2000 · N277AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000247Angle · corrodedCLT - Z ANGLE HAS A 6 INCH AREA OF CORROSION AT BS 967. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-1. (M)Feb 22, 2000 · N277AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000248Floorbeam · corrodedCLT - FLOORBEAM HAS A 1 INCH BY 2 INCH AREA OF CORROSION AT BS 344 LBL 29. REMOVED CORROSION PER SRM 51-10-06. (M)Feb 22, 2000 · N277AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000249Floorbeam · crackedCLT - FLOORBEAM WEB HAS A 1 INCH AREA OF COROSION AT BS 947 PLUS 1 STRINGER 11R. INSTALLED DOUBLER PER TR 53-30-07A. (M)Feb 22, 2000 · N277AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA000250Stringer Clip · crackedCLT - STRINGER CLIP CRACKED AT BS 747, STRINGER 10L. INSTALLED TIE CLIP PER EO 5393G227. (M)Feb 22, 2000 · N277AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000251Stringer Clip · crackedCLT - STRINGER CLIP CRACKED AT BS 664, STRINGER 10L. REPLACED TIE CLIP PER EO 5393G227. (M)Feb 22, 2000 · N277AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000252Stringer Clip · crackedCLT - STRINGER CLIP CRACKED AT BS 597, STRINGER 8R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Feb 22, 2000 · N277AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000253Stringer Clip · crackedSTRINGER CLIP IS CRACKED AT BS 664, STRINGER 10L. REPLACED TIE CLIP PER EO 5393G227. (M)Feb 22, 2000 · N277AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000254Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 807 STRINGER 7L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Feb 22, 2000 · N277AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAASB00046Landing Gear · brokenIAD - FLT 2724 - ON CLIMB OUT FROM IAD, CAPTAIN HEARD A POP FOLLOWED BY SOME VIBRATION. THE AIRCRAFT SEEMED NORMAL OTHERWISE. AFTER WHAT WAS BELIEVED TO BE A BIRD STRIKE, FLIGHT RETURNED TO FIELD AT IAD AS PRECAUTION. FLIGHT LANDED WITHOUT FURTHER INCIDENT.Feb 20, 2000 · N271AU · Boeing 7372B7 · Landing Gear Door Retract SectionSDR USAA000190Strap · crackedCLT - FOUND .25 INCH CRACK, STATION 1138, 5A LT SIDE STRAP. REPAIRED DOUBLER AND FILLER PER EA 66505. (M)Feb 11, 2000 · N275AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA000189Stringer · corrodedCLT - FOUND .250 INCH BY .250 INCH OF CORROSION, BS 903 TO BS 1016, STRINGER 27L. INSTALLED DOUBLER AND EXTERNAL STRAP PER SRM 53-30-3 FIG 6 AND 17 AND SRM 53-10-3. (M)Feb 11, 2000 · N275AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAASB00034Battery Pack · dischargedATL - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROW 6 AND BEYOND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS AT SEAT ROWS 6, 12 AND 17 ABC. OPERATIONAL CHECK GOOD. (M)Feb 8, 2000 · N284AU · Boeing 7372B7 · Emergency LightingSDR USAA000187Frame · crackedCLT - FOUND 1.5 INCH CRACK, BS 727, RBL 1, LBL 25, RBL 25. INSTALLED REPAIR CHORD PER EA 66520. (M)Feb 8, 2000 · N275AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA000173Frame · crackedCLT - FOUND 1.5 INCH CRACK UPPER COMP CHORD, BS 727, RBL 01. INSTALLED NEW CHORD PER EA 66520 AND SRM 51-70-10. (M)Feb 7, 2000 · N275AU · Boeing 7372B7 · Fuselage Main, Frame
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