Boeing 737-301

Service difficulty reports · 4,797

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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 = '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.

SDR USAA010807SkinPIT - FOUND SKIN OIL CANNING 12 INCH BY 12 INCH, 178 BULKHEAD BETWEEN WL 195-207 BL 17L AND BL 17R. ACCOMPLISHED EXTERNAL DOUBLER, REMOVED DAMAGE PER SRM 53-10-08 FIG 211. (M)Jun 12, 2001 · N335US · Boeing 737301 · Fuselage Structure (General)SDR USAA010661Frame · crackedCLT - FOUND SIDE CHORDS HAVE TWO CRACKS, 1 INCH ON RIGHT SIDE, 3 INCHES ON LEFT SIDE, BS 178 WL 207. REMOVED DAMAGE, SPLICED IN NEW SIDE CHORD ANGLE PER EO 5300V157. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Main, FrameSDR USAA010662Web · crackedCLT - FOUND WEB CRACKED .25 INCH AND .125 INCH, BS 178, WL 198 AT LBL 6, WL 234 AT LBL 13.3. DAMAGED REMOVED, INSTALLED DOUBLER AND FILLERS PER EO 5300V153. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Structure (General)SDR USAA010650Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH, BS 967, RBL 5. REMOVED AND REPLACED ENTIRE T-CAP PER TR 53-10-05A. REMOVED AND REPLACED ENTIRE TEE CAP PER TR 53-10-05A. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA010647Doubler · dentedCLT - FOUND DOUBLER DENTED .5 INCH BY .5 INCH, BS 360-380, BL 0 BELLY, E/E COOLING DUCT CUTOUT. REMOVED AND REPLACED PREVIOUSLY INSTALLED PER SRM 51-10-02 AND BOEING DRAWING NR 65C33930. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA010649Web · corrodedCLT - FOUND CREASE BEAM WEB CORRODED, .5 INCH BY 10 INCHES, BS 747 TO 767, STRINGER 17L. FABRICATED AND INSTALLED NEW WEB PER BOEING DRAWING NR 65-46818, SRM 51-40-02, 51-10-02. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Structure (General)SDR USAA010651Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 100 INCH BY 2 INCH AREA, BS 986, AFT ENTRY DOOR TO AFT GALLEY SERVICE DOOR. REMOVED AND REPLACED ENTIRE T-CAP PER TR 53-10-05A. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA010652Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 3 SQUARE INCH AREA, BS 312, RBL 8. REMOVED AND REPLACED T-CAP SECTION PER SRM 53-10-51 AND 51-20-01. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA010653Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 12 SQUARE INCH AREA, BS 328, BL 0 TO RBL 60. REMOVED AND REPLACED ENTIRE TEE CAP PER SRM 53-10-51. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA010654Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 1 SQUARE INCH AREA, BS 344, LBL 24 TO RBL 11. REMOVED AND REPLACED T-CAP SECTION PER SRM 51-10-2 AND 53-10-51. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA010655Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 60 INCHES BY 2 INCHES, BS 947 TO 1006, RBL 50. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-02. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA010656Angle · corrodedCLT - FOUND Z-ANGLE CORRODED, BS 947 TO 1006, LBL 50. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-2. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA010657Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED APPROX 14 SQUARE INCHES, BS 1016 LBL 45 TO RBL 45. REMOVED AND REPLACED T-CAP PER SRM 53-00-51. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA010658Keelbeam · corrodedCLT - FOUND KEEL BEAM CORRODED .25 INCH BY .050 INCH, BS 710, LBL 6.5. DAMAGED REMOVED, INSTALLED REPAIR STRAP PER EA 69728 AND SRM 53-60-12. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Main, KeelSDR USAA010659Keelbeam · corrodedCLT - FOUND KEEL BEAM APPROX 6 SQUARE INCH AREA, CORROSION AT SCREW HOLES, BS 663-720, RBL 6.5. DAMAGED REMOVED, INSTALLED REPAIR STRAP PER EA 69728 AND SRM 53-60-12. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Main, KeelSDR USAA010660Web · crackedCLT - FOUND HORIZONTAL WEB WITH TWO 1 INCH CRACKS ON BOTH LEFT AND RIGHT, BS 180, WL 207, RBL 24 AND LBL 24, FLOOR STRUCTURE. REMOVED AND REPLACED WEBS, LEFT AND RIGHT, PER EO 5300V157. (M)Jun 12, 2001 · N584US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB01170Tire · separatedPIT - FLT 1185 - CAPT REPORTED ON T/O FROM PIT, THE NR 3 MLG TIRE TREAD HAD SEPARATED AND CAUSED A RT MLG UNSAFE LIGHT TO ILLUMINATE. CREW RECYCLED GEAR AND RECEIVED THREE GREEN LIGHTS. UPON PREPARATION FOR LANDING, CREW RECEIVED THE SAME RT MLG LANDING GEARJun 10, 2001 · N340US · Boeing 737301 · TireSDR USAA010856Beltframe · crackedPIT - FOUND BELTFRAME CRACKED .25 INCH, STATION 480 S8. DOUBLER INSTALLED PER SRM T/R 53-10-14. (M)Jun 9, 2001 · N576US · Boeing 737301 · Fuselage Structure (General)SDR USAA010857Beltframe · crackedPIT - FOUND BELTFRAME CRACKED 1 INCH, STATION 787 BELTFRAME ABOVE S9R. INSTALLED REPAIR DOUBLER PER T/R 53-1014. (M)Jun 9, 2001 · N576US · Boeing 737301 · Fuselage Structure (General)SDR USAA010863Stringer · crackedPIT - FOUND STRINGER CRACKED 1 INCH, STATION 440 STRINGER 8 RIGHT. INSTALLED DOUBLER PER SRM T/R 53-10-14. (M)Jun 8, 2001 · N576US · Boeing 737301 · Fuselage Structure (General)SDR USAA010640Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 500A, STRINGER 8R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Main, StructureSDR USAA010641Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH BS 440, STRINGER 8R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Structure (General)SDR USAA010633Frame · crackedCLT - FOUND FRAME CRACKED, BS 867, BETWEEN STRINGER 8 AND 9L. DAMAGE REMOVED, INSTALLED DOUBLER PER TR 53-10-14. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Structure (General)SDR USAA010634Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 480, STRINGER 8L. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Structure (General)SDR USAA010635Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 500A, STRINGER 8L. INSTALLED DOUBLER PER TR 53-10-14. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Structure (General)SDR USAA010636Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 400 STRINGER 8R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Structure (General)SDR USAA010637Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 440, STRINGER 8L. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Structure (General)SDR USAA010638Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 400, STRINGER 8L. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Main, StructureSDR USAA010639Frame · crackedCLT - FOUND FRAME CRACKED.5 INCH, BS 500C, STRINGER 8R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Main, StructureSDR USAA010626Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 578, STRINGER 10R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-2. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Main, StructureSDR USAA010627Tie Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .25 INCH, BS 597, STRINGER 10R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-2. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Structure (General)SDR USAA010628Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 727, STRINGER 16R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER, FILLERS, ANGLES PER EA 69664. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Structure (General)SDR USAA010629Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 787, STRINGER 8 AND 9 RIGHT. DAMAGED REMOVED, INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Structure (General)SDR USAA010630Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 747, BETWEEN STRINGER 8/9L. DAMAGED REMOVED, INSTALLED REPAIR PER TYPICAL REPAIR 53-10-14. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Structure (General)SDR USAA010631Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 727D, BETWEEN STRINGER 8L AND 9L. DAMAGED REMOVED, INSTALLED REPAIR DOUBLER AND FILLER PER TR 53-10-14. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Structure (General)SDR USAA010632Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 747, BETWEEN STRINGER 8/9R. DAMAGED REMOVED, INSTALLED DOUBLER AND FILLER PER TR 53-10-14. (M)Jun 8, 2001 · N584US · Boeing 737301 · Fuselage Structure (General)SDR AWXA0001841Turbine · failedDTW - aborted takeoff - 6/7/01 - FLT 528 - on takeoff, loud noise heard from left side of aircraft, lost several fan blades, E-1 LPT-1 turbine failed. takeoff aborted. no airframe damage; engine changed and aircraft returned to service.Jun 8, 2001 · N324AW · Boeing 737301 · Turbine SectionSDR USAA010855Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH SPOT, STATION 727C CHANNEL NR 5 FLOOR SUPPORT. BLENDED PER 53-60-51 FIG 101. CORROSION LEVEL 1. (M)Jun 7, 2001 · N576US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA010615Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED APPROXIMATELY .1875 INCH, BS 887, STRINGER 23R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLE WITH FILLER PER SRM 53-00-01, FIG 227. (M)Jun 5, 2001 · N334US · Boeing 737301 · Fuselage Main, Plate/SkinSDR DL733010905Bulkhead · crackedINSPECTION OF THE FS 178 BULKHEAD WEB REVEALED A CRACK IN A TOOLING HOLE AT WL 234 AND LBL 12. A SECOND CRACK WAS FOUND AT A FASTENER HOLE AT WL 233 AND LBL 12. THE HOLES WERE OVERSIZED TO REMOVE THE CRACKS. THE AREA WAS THEN REPAIRED WITH AN EXTERNAL ALUMIJun 1, 2001 · N948WP · Boeing 737301 · Fuselage Main, BulkheadSDR USAA010858Strap · crackedPIT - FOUND STRAP CRACKED TWO PLACES .5 INCH ON BOTH FORWARD SIDES, STATION 312 BOTTOM FLOORBEAM SUPPORT STRAP 10 INCHES LEFT C/L. DEFECTIVE PART REPLACED WITH IDENTICAL PART. REPLACED RIVETS PER SRM 52-40-02. (M)May 31, 2001 · N576US · Boeing 737301 · Fuselage Structure (General)SDR USA2001F00006Panel · departedAFTER TAKEOFF, FLIGHT ENCOUNTERED COMPLETE LOSS OF SYSTEM A HYDRAULICS AND PRESSURE. LOST LG TRIANGULAR PANEL OFF TOP OF RT WING. NOSE GEAR WOULD RETRACT BUT MAIN GEAR WOULD NOT. HYDRAULIC LINE HAD BROKEN. PANEL DEPARTED AIRCRAFT AT END OF RUNWAY. CAPTAINMay 31, 2001 · N585US · Boeing 737301 · Wing, Plate/SkinSDR USAA010853Seat Track · corrodedPIT - FOUND SEAT TRACK CORRODED 3 INCHES BY 6 INCHES, NR 2 GALLEY OUTBOARD SEAT TRACK STATION 328 GOING AFT. (M)May 29, 2001 · N576US · Boeing 737301 · Fuselage, Seat/Cargo Attach FittingsSDR USAASB01141Adc · failedPVD - FLT 310 - ON TAKEOFF FROM DCA, EN ROUTE TO PVD, CREW DETECTED AN ACRID SMELL IN THE COCKPIT. SMELL WENT AWAY EVENTUALLY. CREW REPORTED THAT THEY HAD NO V-NAV, THE FIRST OFFICERS ALTIMETER WAS OFF AND THE AUTOTHROTTLES WERE INOPERATIVE. FLIGHT CONTINUEMay 20, 2001 · N577US · Boeing 737301 · Air Data ComputerSDR USAASB01142Static Line · leakingDCA - FLT 556 - EN ROUTE FROM DCA TO MHT, AT FL200, THE F/O'S ALTIMETER WAS READING 500 FT LOW AT 19,500 FEET. DUE TO PREVIOUS PROBLEMS AND LACK OF MX IN MHT, FLIGHT RETURNED TO FIELD AT DCA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLAREDMay 20, 2001 · N577US · Boeing 737301 · Navigation SystemSDR USAA010704Bellcrank · brokenPIT - FOUND BELLCRANK HAD .75 INCH SECTION BROKEN OUT, RT INBOARD AILERON HINGE ASSY. NOTCHED OUT TOP OF FITTING, REMOVED LOWER FLANGE, INSTALLED TWO MACHINED DOUBLERS PER EA 71077. (M)May 18, 2001 · N586US · Boeing 737301 · Aileron Control SystemSDR USAA010733Web · crackedPIT - FOUND ANGLE WEB CRACKED 1 INCH, UNDER AFT SERVICED DOOR SILL PLATE. MANUFACTURED AND INSTALLED NEW WEB PER BOEING DRAWING 65.45855. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA010734Skin · crackedPIT - FOUND PYLON SKIN CRACKED 1 INCH, UPPER RIGHT CORNER OF PANEL 5724L OPENING. STOP DRILLED CRACK, INSTALLED DOUBLER PER TYPICAL REPAIR 54-50-07. (M)May 17, 2001 · N586US · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR USAA010735Skin · crackedPIT - FOUND SKIN CRACKED .25 INCH, BS 947 AT STRINGER 11R. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-60-01. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010736Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BS 663 AT S2L. CUT OUT DAMAGE, INSTALLED DOUBLER PER SRM 53-00-07 FIG 208, SRM 51-70-13, SRM 53-60-08, SRM 53-60-08. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)
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