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 USAASB99082Battery Pack · dischargedALB - MAINTENANCE FOUND THE LOWER SIDEWALL EMERGENCY EXIT SIGNS FOR THE FORWARD ENTRY DOOR AND SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Mar 28, 1999 · N592US · Boeing 737301 · Emergency LightingSDR USAASB99065Switch · malfunctionedBWI - FLT 218, ON TAKEOFF, CAPT HEAD A LOUD NOISE AND WAS UNABLE TO PRESSURIZE THE AIRCRAFT. AT ABOUT 10,000 FT, CREW ELECTED TO RETURN TO FIELD AT BWI WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MX FOUND THE FORWARD ACCESS DOOR IMPMar 6, 1999 · N336US · Boeing 737301 · Door Warning SystemSDR USAASB99062Light · inoperativeROC - MAINTENANCE FOUND THE FLOOR PROXIMITY IDENTIFIER LIGHT ON SEAT 10C END BAY INOPERATIVE. MAINTENANCE REPLACED DEFECTIVE WIRE SLICES T END BAY ON SEAT 10C. OPERATIONAL CHECK GOOD. (M)Mar 3, 1999 · N356US · Boeing 737301 · Emergency LightingSDR USAA990221Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK EXTERNAL SKIN FORWARD SERVICE DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER EA 64060 AND SB 52-1096. (M)Mar 2, 1999 · N339US · Boeing 737301 · Service DoorsSDR USAA990134Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 827 RS 8 RS 9 FRAME SUPPORT. INSTALLED REPAIR PER EA 63769 AND SRM 53-30-07. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, FrameSDR USAA990133Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 17 INCH CORROSION AREA AROUND SCREW HOLES BS 344 RBL 2 LBL 15 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED T-CAP PER SRM 53-10-51. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990131Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 847 BETWEEN RS 8 AND RS 9 SUPPORT FRAME. INSTALLED DOUBLER PER EA 63769. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, FrameSDR USAA990130Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 887 BETWEEN LS 8 AND LS 9 SUPPORT FRAME. INSTALLED DOUBLER PER EA 63769. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, FrameSDR USAA990129Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 400 BETWEEN LS 8 AND LS 9 SUPPORT FRAME. INSTALLED DOUBLER PER EA 63769. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, FrameSDR USAA990128Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 440 BETWEEN LS 8 AND LS 9 SUPPORT FRAME. INSTALLED DOUBLER PER EA 63769. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, FrameSDR USAA990127Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 807 BETWEEN LS 8 AND LS 9 SUPPORT FRAME. INSTALLED DOUBLER PER EA 63769. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, FrameSDR USAA990126Angle · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CORROSION AREA A NUTPLATE HOLE BS 350 LBL 64 SUPPORT ANGLE. REPAIRED PER SRM 51-00-00 AND BOEING DRAWING 65-29818. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990125Floor Panel · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CORROSION AREA FLOOR PANEL UNDER LEFT LAV TOILET TANK. INSTALLED REPAIR FLOOR PANEL PER SRM 53-10-05. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Floor PanelSDR USAA990124Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FUOND A 1 INCH CRACK AFT END ANTENNA MOUNT FUSELAGE SKIN BOTTOM CENTER STATION 727 BL 0 . FABRICATED FILLER AND DOUBLER REPAIR PER SRM 53-00-01 FIG 202. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA990104Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK FROM FASTENER HOLE STATION 616 FRAME INBOARD BOTTOM CHORD ANGLE. INSTALLED DOUBLER PER EA 63678. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, FrameSDR USAA990103Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 827 BETWEEN LS 8 AND LS 9 SUPPORT FRAME. INSTALLED REPAIR ANGLE PER EA 63769. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, FrameSDR USAA990102Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FUOND A CRACK RADIATING FROM RIVET HEAD BS 787 LB 8 LS 9 SUPPORT FRAME. INSTALLED REPAIR ANGLE PER EA 63769. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, FrameSDR USAA990101Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 847 BETWEEN LS 8 AND LS 9 SUPPORT FRAME. REPAIRED PER EA 63769. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, FrameSDR USAA990100Frame · crackedCLT - DURNIG Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD HOLE AREA STATIO N727 CABIN SIDEWALL BETWEEN LS 8 AND LS 9 SUPPORT FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 63769. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, FrameSDR USAA990099Bulkhead Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK STATION 178 BULKHEAD SKIN LBL 1 WL 205.5. INSTALLED REPAIR DOUBLER PER TR 53-10-07. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990098Angle · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK STATION 18 AND STATION 178 SHEAR ANGLE AT RBL 29 WL 195. INSTALLED NEW ANGLE PER SRM 53-10-08 DRAWING 6-72038. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990097Blkhd Stiffener · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STATION 178 BULKHEAD VERTICAL STIFFENER INBOARD FLANGE LBL 5.5 WL 184. FABRICATED REPAIR ANGLE AND STRAP PER SRM 53-10-08 FIG 205. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990096Blkhd Stiffener · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 178 BULKHEAD VERTICAL STIFFENER OUTBOARD FLANGE LBL 6 WL 184. FABRICATED REPAIR ANGLE AND STRAP PER SRM 53-10-08 FIG 205. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990095Bulkhead Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK STATION 178 BULKHEAD/SKIN LBL 4.75 WL 201. INSTALLED DOUBLER PER TR 53-10-07. (M)Feb 26, 1999 · N558AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAASB99054Fuse · failedEWR - PILOT REPORTED THAT THE EMERGENCY EXIT ROW LIGHTS ON THE LEFT SIDE OF THE CABIN ARE INOPERATIVE. MAINTENANCE FOUND A BLOWN FUSE (5 AMP) IN THE POWER SUPPLY. REMOVED AND REPLACED FUSE. OPERATIONAL CHECK GOOD. (M)Feb 25, 1999 · N350US · Boeing 737301 · Emergency LightingSDR USAASB99049Power Supply · failedSYR - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M)Feb 22, 1999 · N336US · Boeing 737301 · Emergency LightingSDR AWXA9900044Wire · brokenDURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT ROW 5, 6, 7, INOP. REPAIRED BROKEN WIRE, OPS CK GOOD.Feb 19, 1999 · N324AW · Boeing 737301 · Light System WiringSDR USAASB99037Charger · failedLGA - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Feb 14, 1999 · N350US · Boeing 737301 · Emergency LightingSDR USAA990081Skin · crackedTPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND 2.125 INCH CRACK IN THE SKIN 1 INCH AFT OF THE EQUIPMENT COOLING EXHAUST BL 0 AND BS 375. REPAIRED PER TR 53-30-07. (M)Feb 10, 1999 · N591US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB99032Battery Pack · dischargedCMH - MAINTENANCE FOUND THE AFT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT BS 753. OPERATIONAL CHECK GOOD. (M)Feb 8, 1999 · N340US · Boeing 737301 · Emergency LightingSDR USAASB99024Strap · out of positionCLT - FLT 83 - IMMEDIATELY AFTER DEPARTING CLT, A LOUD RAPPING NOISE AT THE AFT LEFT ENTRY DOOR WAS HEARD BY PASSENGERS AND THE FLIGHT ATTENDANTS IN THE REAR OF THE CABIN. CAPTAIN WAS NOTIFIED AND THE NOISE WAS DETERMINED TO BE THE YELLOW RESTRAINING STRAP FOJan 29, 1999 · N587US · Boeing 737301 · Passenger/Crew DoorsSDR USAA990061Bulkhead Chord · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK STATION 727 LBL 29 WL 153.5 BULKHEAD LOWER PRIMARY CHORD. INSTALLED REPAIR DOUBLER ANGLE, FILLER AND VERTICAL STIFFENER PER EA 63469. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990057Shear Tie · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STATION 948 STRINGER 27R SHEAR TIE. REMOVED AND REPLACED PER SRM 51-10-02. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990056Stringer · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BETWEEN RIVETS BS 908 STRINGER 4R. INSTALLED NEW TIE CLIP PER SRM 51-10-00. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA990055Channel · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .20 CRACK AND CORROSION BS 520 VHF NR 2 COMM ANTENNA MOUNT CHANNEL. REMOVED AND REPLACED CHANNEL PER SB 737-53-1159 FIG 1 STEP 1. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990050Tie Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP BS 727A STRINGER 2L. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990049Tie Clip · crackedCLT - DURNIG Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP BS 727C STRINGER 6L, STRINGER 7L, STRINGER 8L. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990048Tie Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN TIE CLIP BS 639 STRINGER 4L. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990047Stringer · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STRINGER SPLICE BS 908 STRINGER 4R. INSTALLED NEW SPLICE PER SRM 51-10-02 AND 51-40-02. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA990046Tie Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 4L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-00. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990045Skin · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AFT EDGE OF EQUIPMENT COOLING DUCT STATION 380 FUSELAGE SKIN. INSTALLED EXTERNAL DOUBLER PER BOEING DRAWING 65C33930. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA990044Stringer · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .10 INCH CRACK BETWEEN RIVETS BS 908 STRINGER 4L. INSTALLED NEW TIE CLIP PER SRM 51-10-00. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA990029Frame · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 6 INCH BY 6 INCH AREA OF CORROSION AT STRINGER 27L BS 500D CARGO FLOOR LEVEL FRAME. CORROSION TASK NR C 53-208-01. FABRICATED REPAIR PER SRM 53-00-07. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Main, FrameSDR USAA990026Angle · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .10 INCH CRACK AT LOWER FAST OF INNER CHORD ANGLE BS 616 WL 201 LT SIDE. REPAIRED PER TR 53-10-23 AND EA 63358 INSTALLED FILLER AND DOUBLER. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990025Angle · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .10 INCH CRACK AT LOWER FASTENER OF INNER CHORD ANGLE BS 616 WL 201 RT SIDE. REPAIRED PER TR 53-10-23 AND EA 63358 INSTALLED FILLER AND DOUBLER. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990024Floorbeam · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .20 INCH CRACK STATION 520 LBL 25 FLOORBEAM. INSTALLED DOUBLER AND REPAIR ANGLES PER EA 63326, SB 737-53-1120. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990023Tie Clip · crackCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 8R BS 727A. REPAIRED PER SRM 51-10-02. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990022Tie Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 4R BS 727B. REPAIRED PER SRM 51-10-02. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990021Tie Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 5R BS 727B. REPAIRED PER SRM 51-10-02. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990020Tie Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 7L, STRINGER 8L BS 727B. REPAIRED PER SRM 51-10-02. (M)Jan 25, 1999 · N334US · Boeing 737301 · Fuselage Miscellaneous Structure
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