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.

SDR USAASB00179Transformer · overheatedMDT - FLT 1924 - EN ROUTE FROM ROC TO DCA, F/A NOTIFIED CAPTAIN THAT THERE WAS A STRONG BURNING ELECTRICAL ODOR IN THE CABIN. CAPT MADE A RAPID DESCENT, DECLARED AN EMERGENCY AND DIVERTED TO THE FIRST SUITABLE AIRPORT AT MDT. FLHT LANDED W/O FURTHER INCIDENTJun 27, 2000 · N576US · Boeing 737301 · DC Rectifier/ConverterSDR USAA000888Frame · wornCLT - FOUND FRAME WORN 3 INCHES WEAR AREA CAUSED BY APU DUCT CLAMP, STATION 1040. REPAIRED PER EA 67421/SRM 53-00-03. (M)Jun 20, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000880Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCHE''S, BS 664, LBL 30, WL 203 PRESSURE DECK WEB. REPAIRED PER TR 53-60-04. (M)Jun 20, 2000 · N588US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA000878Angle · crackedCLT - FOUND CHORD ANGLE CRACKED 4 INCHES, STATION 1138, STRINGER 5R INSIDE UPPER STRAP CHORD ANGLE. FABRICATED REPAIR AND INSTALLED PER SRM 53-00-01 FIG 221. (M)Jun 20, 2000 · N585US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000868Frame · crackedCLT - FOUND FRAME CRACKED .5 INCHES, STATION 480, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER AND FILLER PER TR 53-10-14A. (M)Jun 19, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000869Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 440, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER AND FILLER PER TR 53-10-14A. (M)Jun 19, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000870Frame · crackedCLT - FOUND FRAME CRACKED .5 INCHES, STATION 500A, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)Jun 19, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000871Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 400, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)Jun 19, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000858Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 400, STRINGER 9L AT OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER SRM 53-10-14A. (M)Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000859Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 440, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000861Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 727D, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000862Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 747, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000863Frame · crackedCLT - FOUND FRAME CRACKED, STATION 747 STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000864Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 787, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000865Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 827, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000866Frame · crackedCLT - FOUND FRAME .5 INCH CRACKED, STATION 827, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000867Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 867, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000860Frame · crackedCLT - FOUND FRAME CRACKED .5 INCHES, STATION 480, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000848Door Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, FORWARD SERVICE DOOR JAMB FRAME UPPER FORWARD DOOR STOP FITTING. REMOVED AND REPLACED PART PER BOEING DWG 65-55878. (M)Jun 14, 2000 · N585US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB00166Outflow Valve · failedCLT - FLT 665 - EN ROUTE FROM CLT-PBI, AT FL350, THE CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE WAS AT 10,000 FEET AND CLIMBING. CAPTAIN DECLARED AN EMERGENCY, DESCENDED THE FLIGHT TO 10,000 FEET AND REGAINED CONTROL OF CABIN WITH MANUAL DC. FLIGHTJun 13, 2000 · N587US · Boeing 737301 · Pressure Regulator/Outflow ValveSDR USAA000815Bulkhead · crackedCLT - FOUND TWO CRACKS IN BULKHEAD .25 INCH AND .75 INCH, WL 201, LBL 5. FABRICATED AND INSTALLED REPAIR PART PER TR 53-10-08 FIG 209. (M)Jun 12, 2000 · N585US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA000814Angle · crackedCLT - FOUND ANGLE CRACKED 1 INCH, LOWER FORWARD WING TO BS 540 ABOVE RT RAM AIR DUCT. INSTALLED DOUBLER PER TR 53-50-03. (M)Jun 12, 2000 · N585US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB00162Feel Unit · failedCLT - FLT 1050 - AFTER T/O FROM CLT, AT APPROX 1,000 FT, THE ELEVATOR FEEL DIFFERENTIAL LIGHT ILLUMINATED AND THE NR 1 AUTOPILOT WOULD NOT ENGAGE, THE NR 1 ATC FAIL LIGHT ILLUMINATED, THE NR 2 EGT IND FAILED AND THE LEFT PACK WAS BLOWING SO HARD IT CREATED A SJun 10, 2000 · N336US · Boeing 737301 · Elevator Control SystemSDR USAASB00159Gcu · failedBOS - FLT 6535 - ON CLIMB-OUT FROM BOS, AT APPROXIMATELY 3,500 FEET, THE NR 1 GENERATOR WENT OFF LINE AND ALL ELECTRICAL AVIONIC SYSTEMS ON THE CAPTAINS SIDE WENT BLANK. THE FIRST OFFICERS SIDE WAS FLICKERING AND EVENTUALLY RETURNED AFTER THE APU WAS STARTED.Jun 7, 2000 · N342US · Boeing 737301 · AC Generation SystemSDR USAA000786Skin · crackedCLT - FOUND SKIN CRACKED .250 INCH, LEFT C/D WINDOW POST. INSTALLED DOUBLER PER EA 67382. (M)Jun 5, 2000 · N563AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA000884Channel · crackedCLT - FOUND U-CHANNEL CRACKED .375 INCH, STRINGER 18A SHAFT LEFT W/W PLUS 727. REPLACED STRINGER 18A SHELF. (M)Jun 4, 2000 · N585US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000885Frame · corrodedCLT - FOUND 1 INCH CORROSION, STATION 807 BETWEEN STRINER 23R-24R. FABRICATED REPLACEMENT STIFFENER PER DWG 69-38178. CORROSION LEVEL 1, TASK NR C53-202-01. (M)Jun 3, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000883Support Bracket · crackedCLT - FOUND DOOR SUPPORT CRACKED 2 INCHES, LOWER CORNER AT FORWARD DOOR SUPPORT. INSTALLED DOUBLER PER SRM 51-70-11. (M)Jun 3, 2000 · N585US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000882Drag Brace · crackedCLT - FOUND DRAG BRACE ANGLE CRACKED .5 INCH, BS 536, STRINGER 21L. INSTALLED FABRICATED SUPPORT ANGLE SECTION PER TR 53-50-03. (M)Jun 3, 2000 · N585US · Boeing 737301 · Fuselage Main, StructureSDR USAA000887Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH IN FRAME AT INBOARD RIVET HOLE, STATION 787, STRINGER 9L AT OVERHEAD BIN SUPPORT. INSTALLED REPAIR DOUBLER PER TR 53-10-14A. (M)Jun 2, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA000886Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH IN FRAME AT INBOARD RIVET HOLE, STATION 867, STRINGER 9L AT OVERHEAD BIN SUPPORT. INSTALLED REPAIR DOUBLER PER T/R 53-10-14A. (M)Jun 2, 2000 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAASB00155Outflow Valve · failedPIT - FLT 1031 - FLIGHT WAS EN ROUTE FROM IAH TO PIT, WITH BOTH PACKS IN HIGHT FOR MAXIMUM COOLING. UPON REACHING FL370, CREW TURNED BOTH PACKS TO AUTO AND THE CABIN CLIMBED ABOVE 10,000 FEET WITH WARNING HORN SOUNDING. AN EMERGENCY DESCENT WAS ACCOMPLISHED.Jun 2, 2000 · N592US · Boeing 737301 · Pressure Regulator/Outflow ValveSDR AWXA0000362Fan · failedSTRONG CHEMICAL ODOR IN CABIN. DURING DESCENT A STRONG CHEMICAL ODOR ORIGINATED IN AFT CABIN AND PROGRESSED FORWARD, FILLING ENTIRE CABIN. REPLACED NORMAL EQUIPMENT COOLING FAN BLOWER. FOUND MOTOR BURNED.Jun 2, 2000 · N325AW · Boeing 737301 · Air Distribution FanSDR USAA000769Stiffener · corrodedCLT - FOUND STIFFENER CORRODED 1 INCH BY 1 INCH, NOSE W/W STIFFENER BS 235.8, RBL 10. INSTALLED REPAIR ANGLE PER SRM 51-70-12. CORROSION LEVEL 1. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000770Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 312, LBBL 1 PLUS 8. FABRICATED ANGLES AND INSTALLED PER SRM 53-10-51. CORROSION LEVEL 2. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000771Angle · crackedCLT - FOUND Q-3 CHECK, FOUND Z-ANGLE CRACKED 2 INCHES, LEFT AFT ENTRY DOOR THRESHOLD. REPAIRED PER SRM 51-10-2. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000772Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES, 328 FLOORBEAM, RBBL 36 TO 38. REPLACED T-CAP PER SRM 53-10-51 FIG 205. CORROSION LEVEL 2. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000759Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH IN TWO PLACES, BS 178, WL 199 AND 202 AT RBL 5. INSTALLED REPAIR ANGLE PER TR 53-10-07. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA000760Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 1 INCH, STATION 291.5 AND STATION 270 BETWEEN STRINGER 11 AND 12R. INSTALLED NEW FABRICATED PART PER SRM 51-30-2. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000761Door Frame · crackedCLT - FOUND DOOR FRAME CRACKED .25 INCH, STATION 294.5 INBOARD SIDE OF R-1 DOOR FRAME. INSTALLED DOUBLER PER SRM 51-70-11. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, StructureSDR USAA000762Frame · crackedCLT - FOUND FORWARD SERVICE DOOR FRAME CRACKED .75 INCH, STATION 294.5, WL 207.5. INSTALLED REPAIR ANGLE PER SRM 53-10-02. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, StructureSDR USAA000763Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, BS 727C, STRINGER 4L. REPLACED TIE CLIP PER SRM 51-10-02. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000764Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, BS 727D, STRINGER 4L. REPLACED TIE CLIP PER SRM 51-10-02. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000765Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 807, RIGHT BIN RAIL ATTACH STRINGER 8 TO 9. INSTALLED DOUBLER PER TR 53-10-14. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000766Track · crackedCLT - FOUND O/H BIN RAIL CRACKED .5 INCH, STATION 827, LEFT O/H BIN RAIL ATTACH STRINGER 8 TO 9. INSTALLED DOUBLER PER TR 53-10-14A. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage, Seat/Cargo Attach FittingsSDR USAA000767Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 847, LT O/H BIN RAIL ATTACH STRINGER 8 TO 9. INSTALLED DOUBLER PER TR 53-10-14A. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000768Frame · crackedCLT - FOUND FRAME CRACKED .5 INCHES, STATION 908, RIGHT O/H BIN ATTACH RAIL STRINGER 8 TO 9. FABRICATED DOUBLER PER TR 53-10-14A. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000743Stiffener · crackedTPA - FOUND VERT STIFFENER CRACKED THROUGH AND WEB CRACKED 3.5 INCHES, STATION 597, 37 INCHES RIGHT OF CENTER LINE, WL 154.5. INSTALLED DOUBLER PER EA 67349. (M)May 31, 2000 · N584US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000757Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH IN TWO PLACES, BS 178, WL 199 AND 202 AT LBL 5. INSTALLED REPAIR ANGLE PER TR 53-10-07. INSTALLED REPAIR ANGLE PER TR 53-10-07. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA000758Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH IN TWO PLACES, BS 178, WL 190, LBL 1 AND RBL 1. INSTALLED REPAIR ANGLE PER TR 53-10-08. (M)May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Plate/Skin
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