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 SWAA051428Stringer Clip · crackedDURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.May 16, 2005 · N660SW · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA050664Splice · crackedPIT - FOUND STRINGER SPLICE CRACKED 1 INCH, LEFT AFT CABIN AT STATION 907 STRINGER 4. FABRICATED PARTS, INSTALLED SPLICE AND SHEAR TIE PER SRM 51-40-02. (M)May 15, 2005 · N574US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA050662Splice · crackedBFM - FOUND STRINGER SPLICE CRACKED .5 INCH, RT CEILING AT STATION 987 STRINGER 4. FABRICATED PARTS AND INSTALLED FABRICATED SPLICE AND SHEAR TIE IAW SRM 51-40-02. (M)May 15, 2005 · N574US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA050699Skin · crackedBFM - FOUND TRIM TAB WEB SKIN CRACKED .20 INCH, RT ELEV TRIM TAB HINGES NR 1 AND 3. BONDED FLIES REPAIR ON TRIM TAB PER SRM 51-70-17 AND TYP REPAIR 55-20-03. (M)May 14, 2005 · N574US · Boeing 737301 · Elevator, Tab StructureSDR SB05061Wire · brokenMAINTENANCE REPORTED THE EMERGENCY LIGHT ON SEAT 5A INOPERATIVE. MAINTENANCE REPAIRED WIRE ON LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.May 14, 2005 · N586US · Boeing 737301 · Light System WiringSDR USAA050665Skin · crackedBFM - FOUND NR 1 LE FLAP CRACKED .125 INCH, WS 505, NR 1 LE FLAP LOWER SKIN. CUT OUT DAMAGED AREA, INSTALLED NEW DOUBLER AND FILLER PER SRM 57-43-01, 51-40-02, 51-21-00, 51-20-05. (M)May 13, 2005 · N574US · Boeing 737301 · Leading Edge DevicesSDR USAA050663Floorbeam · corrodedBFM - FOUND CAP CORRODED 2 INCH BY 51.5 INCH BY .025 INCH AND .018 INCH, STATION 344 LBL 20 - RBL 20. REMOVED FLOORBEAM CAP, APPROX 51.5; FABRICATED NEW CAP AND INSTALLED PER SRM 53-10-51, 51-20-01, 51-40-02. (M)May 11, 2005 · N574US · Boeing 737301 · Fuselage Main, Floor BeamSDR SB05058Cable · inoperativePIT - THE R2 DOOR SLIDE LANYARD WOULD NOT RELEASE. MAINTENANCE REPLACED THE SLIDE.May 8, 2005 · N575US · Boeing 737301 · Escape SlideSDR USAA050589Stiffener · crackedCLT - FOUND STIFFENER CRACKED .4 INCH IN VERTICAL STIFFENER AT AFT SIDE OF PYLON LOWER SIDE OF WING. FABRICATED REPAIR PART AND INSTALLED SRM 51-10-02. (M)May 3, 2005 · N560AU · Boeing 737301 · Nacelle/Pylon Miscellaneous StructureSDR USAA050004ASkin · cracked1.250 INCH CRACK FOUND AT STA 328 AND S17R ON SKIN. INSTALLED "TEXAS" PATCH PER SRM 53-10-01 FIG. 202May 1, 2005 · N335US · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200500526Battery · dischargedMCN - MAJOR REPAIR - DURING C-19 CHECK, FOUND THE AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD.Apr 24, 2005 · N325AW · Boeing 737301 · Emergency EquipmentSDR AWXA200500517Tab · crackedMCN - FLIGHT CONTROL - DURING C-19 CHECK A 3/8 INCH CRACK WAS FOUND RT ELEVATOR TAB OUTBOARD CONTROL ROD ATTACH POINT AT ELE STA 121.59. MAINTENANCE REMOVED AND REPLACED DAMAGED RT ELEVATOR TAB IAW T/C R6C27007, OPERATIONAL CHECK WAS GOOD.Apr 24, 2005 · N325AW · Boeing 737301 · Elevator, Tab StructureSDR SB05049Fuse · blownPIT - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REPLACED THE FUSES IN THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD.Apr 22, 2005 · N577US · Boeing 737301 · Emergency LightingSDR USAA050469Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED 1.75 INCH, STATION 727D, STRINGER 24L, BELOW ICE LIGHT. INSTALLED DOUBLER AND TRIPLER IAW SRM 53-00-01, FIG 229. (M)Apr 9, 2005 · N574US · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200500480Line · brokenMCN - MAJOR REPAIR - DURING C-19 CHECK, FOUND THE OXYGEN GENERATOR HOSE ASSEMBLY BROKEN AT SEAT ROW 12 RT. MAINTENANCE REMOVED AND REPLACED OXYGEN GENERATOR HOSE ASSEMBLY AT SEAT ROW 12 RT IAW BMM 35-22-31.Apr 6, 2005 · N325AW · Boeing 737301 · Passenger Oxygen SystemSDR SWAA051019Skin · crackedDURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CUTOUT. REPAIRED SKIN PER SRM.Apr 6, 2005 · N659SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA051018Skin · crackedDURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.Apr 6, 2005 · N659SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200500479Line · brokenMCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE OXYGEN GENERATOR HOSE ASSEMBLY BROKEN AT SEAT ROW 6 RT. MAINTENANCE REMOVED AND REPLACED OXYGEN GENERATOR HOSE ASSEMBLY AT SEAT ROW 6 R/H IAW BMM 35-22-31.Apr 5, 2005 · N325AW · Boeing 737301 · Passenger Oxygen SystemSDR AWXA200500457Vertical Beam · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL BEAM WEB AT RBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGED AREA OF VERTICAL BEAM WEB AT BS 178 BULKHEAD, RBL 17.1, WL 230; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIApr 5, 2005 · N325AW · Boeing 737301 · Fuselage Main, BulkheadSDR SWAA051007Skin · crackedDURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.Apr 5, 2005 · N659SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA051006Skin · crackedDURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CUTOUT. REPAIRED SKIN PER SRM.Apr 5, 2005 · N659SW · Boeing 737301 · Passenger/Crew DoorsSDR AWXA200500461Frame · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND IN BS 178 BULKHEAD SIDE CHORD AT RBL 60, WL 207. MAINTENANCE REMOVED CRACKED SIDE CHORD AT BS 178 BULKHEAD, RBL 60, WL 207; FABRICATED A NEW REPLACEMENT CHORD PER DWG 65-16300; INSTALLED REPAIRApr 4, 2005 · N325AW · Boeing 737301 · Fuselage Main, BulkheadSDR AWXA200500460Frame · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND IN BS 178 BULKHEAD SIDE CHORD AT LBL 60, WL 207. MAINTENANCE REMOVED CRACKED SIDE CHORD AT BS 178 BULKHEAD, LBL 60, WL 207; FABRICATED A NEW REPLACEMENT CHORD PER DWG 65-16300; INSTALLED REPAIRApr 4, 2005 · N325AW · Boeing 737301 · Fuselage Main, BulkheadSDR AWXA200500459Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK 4 EACH CRACKS WERE FOUND EXTENDING PAST STOP DRILL HOLE AND PREVIOUS REPAIR IN BS 178 BULKHEAD WEB AT RBL 5.7, WL 195. MAINTENANCE CUT OUT DAMAGED AREA OF WEB AT BS 178 BULKHEAD, RBL 5.7, WL 195; PERFORMED HFEC INSPECTIOApr 4, 2005 · N325AW · Boeing 737301 · Fuselage Main, BulkheadSDR AWXA200500458Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND EXTENDING PAST STOP DRILL HOLE AND PREVIOUS REPAIR IN BS 178 BULKHEAD WEB AT LBL 5.7, WL 195. MAINTENANCE CUT OUT DAMAGED AREA OF WEB AT BS 178 BULKHEAD, LBL 5.7, WL 195; PERFORMED HFEC INSPECTApr 4, 2005 · N325AW · Boeing 737301 · Fuselage Main, BulkheadSDR AWXA200500456Vertical Beam · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK 2 EACH .25 INCH CRACKS WERE FOUND IN BS 178 BULKHEAD VERTICAL BEAM WEB AT LBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGED AREA OF VERTICAL BEAM WEB AT BS 178 BULKHEAD, LBL 17.1, WL 230; PERFORMED HFEC INSPECTION OF CUTOUT Apr 4, 2005 · N325AW · Boeing 737301 · Fuselage Main, BulkheadSDR AWXA200500477Door Frame · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A .3125 INCH CRACK WAS FOUND ON L-1 DOOR FRAME AT 6TH DOOR STOP FROM TOP BS 344, STR 14 LT. MAINTENANCE CUTOUT DAMAGED SECTION OF L-1 DOOR FRAME AT 6TH DOOR STOP FROM TOP BS 344, STR 14 LT; FABRICATED A FILLER AND REPAIRApr 3, 2005 · N325AW · Boeing 737301 · Passenger/Crew DoorsSDR AWXA200500466Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON TRANSVERSE FLOORBEAM UPPER CHORD AT BS 986 BETWEEN RBL 18 AND RBL 43, WL 208. MAINTENANCE BLENDED OUT CORROSION ON TRANSVERSE FLOORBEAM UPPER CHORD AT BS 986 BETWEEN RBL 18 AND RBL 43; FABRICATED AApr 1, 2005 · N325AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA200500516Wire Harness · damagedMCN - EEL - DURING C-19 CHECK, FOUND NUMEROUS DAMAGED SPLICES AND CONNECTOR ON PASSENGER CABIN EMERGENCY ESCAPE PATH LIGHT HARNESS. MAINTENANCE REMOVED AND REPLACED DAMAGED SPLICES AND CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT HARNESS IAW SWPM 20-42-01, OPERATMar 31, 2005 · N325AW · Boeing 737301 · Light System WiringSDR AWXA200500510Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK, A 5/8 INCH CRACK WAS FOUND IN R-2 DOOR CUTOUT AT FASTENER HOLE IN THE FORWARD LOWER CORNER BS 961, STR 17 RT. MAINTENANCE TRIMMED OUT DAMAGE IN SKIN AT R-2 DOOR CUTOUT IN FORWARD LOWER CORNER BS 961, STR 17 RT; FABRICATMar 31, 2005 · N325AW · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200500469Skin · crackedDURING C-19 CHECK A .25 INCH CRACK WAS FOUND ON L-1 DOOR INNER SKIN ABOVE UPPER TORQUE TUBE SLEEVE ON FORWARD RT SIDE BS 312, STR 12 LT. MAINTENANCE CUT OUT DAMAGED L-1 DOOR INNER SKIN AT BS 312, STR 12 LT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IMar 31, 2005 · N325AW · Boeing 737301 · Passenger/Crew DoorsSDR AWXA200500498Skin · crackedDURING C-19 CHECK A .5 INCH CRACK WAS FOUND IN L-1 DOOR INNER WEB SKIN AT 4TH DOOR STOP FROM THE TOP BS 342, STR 14 LT. MAINTENANCE CUT OUT DAMAGE IN L-1 DOOR INNER WEB SKIN AT BS 342, STR 14 LT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300Mar 29, 2005 · N325AW · Boeing 737301 · Passenger/Crew DoorsSDR AWXA200500468Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND ON L-1 DOOR INNER WEB SKIN ON AFT SIDE, AT 6TH DOOR STOP FROM TOP BS 344, STR 14 LT. MAINTENANCE CUT OUT DAMAGED L-1 DOOR INNER WEB SKIN AT 6TH DOOR STOP FROM TOP BS 344, STR 14 LT; FABRICATED Mar 29, 2005 · N325AW · Boeing 737301 · Passenger/Crew DoorsSDR AWXA200500478Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE UPPER AND LOWER SURFACE OF NR 4 SLAT WEDGE DELAMINATED AT SS 59 RT. MAINTENANCE CUTOUT DAMAGE IN NR 4 SLAT WEDGE FROM SS 57 TO SS 61 RT; FABRICATED A CORE FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLAT IAW B73Mar 28, 2005 · N325AW · Boeing 737301 · Leading Edge DevicesSDR AWXA200500476Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON FLOORBEAM UPPER CHORD AT BS 312 BETWEEN LBL 8 AND RBL 8, WL 208. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOORBEAM UPPER CHORD AT BS 312 FROM LBL 20 TO RBL 21; FABRICATED A NEW REPLACEMENT SECTION OFMar 28, 2005 · N325AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA200500474Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON UPPER CHORD AT BS 294 BETWEEN RBL 7 AND RBL 44, WL 208. MAINTENANCE CUTOUT DAMAGED UPPER CHORD AT BS 294 FROM RBL 7 TO RBL 44; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD AND 2 EACH REPAIR Mar 28, 2005 · N325AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA200500467Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND ON L-1 DOOR INNER WEB SKIN ON AFT SIDE, AT 5TH DOOR STOP FROM TOP BS 344, STR 13 LT. MAINTENANCE CUT OUT DAMAGED L-1 DOOR INNER WEB SKIN AT 5TH DOOR STOP FROM TOP BS 344, STR 13 LT; FABRICATED Mar 28, 2005 · N325AW · Boeing 737301 · Passenger/Crew DoorsSDR AWXA200500465Channel · corrodedMCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON L-1 DOOR ENTRYWAY INNER CHORD UPPER CHANNEL BETWEEN BS 316 AND BS 341, LBL 62, WL 209. MAINTENANCE REMOVED CORRODED UPPER CHANNEL ON INNER CHORD FROM BS 316 TO BS 341 AT LBL 62; FABRICATED A NEW REMar 28, 2005 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA050375Skin · crackedCLT - RON - SKIN, 1.75 INCHES, CRACKED, STA 727E, STR 18L. INSTALLED DOUBLER IAW SRM. (K)Mar 16, 2005 · N587US · Boeing 737301 · Fuselage Main, Plate/SkinSDR SB05038Circuit Breaker · trippedCLT - FLT406 - AFTER TAKEOFF FROM SRQ, CREW NOTED A SPLIT FLAP INDICATION ON FLAP POSITION INDICATOR. ON APPROACH TO CLT, FLAPS WOULD NOT EXTEND AS FLAPS WERE LOCKED OUT. CREW DECLARED AN EMERGENCY AND ACCOMPLISHED A ZERO FLAPS LANDING WITHOUT INCIDENT. MAIMar 4, 2005 · N350US · Boeing 737301 · Trailing Edge Flap Control SystemSDR SB05034Switch · faultySYR - MAINTENANCE REPORTED THAT WHEN THE BATTERY IS SELECTED OFF, THE EMERGENCY EXIT LIGHTS ILLUMINATE AND WILL NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH. OPERATIONAL CHECK GOOD.Mar 2, 2005 · N586US · Boeing 737301 · Emergency LightingSDR AWXA200500244Light · inoperativePHX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY LIGHT ASSEMBLY AT LOWER FORWARD CORNER OF THE RT OVERWING EMERGENCY EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD.Feb 22, 2005 · N324AW · Boeing 737301 · Emergency LightingSDR AWXA200500297Channel · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND AFT CARGO DOOR SILL LOWER CHANNEL AT BS 837, STR 25 RT. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL LOWER CHANNEL AT BS 837, STR 25 RT; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-47957; INSTFeb 19, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500307Frame · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON FRAME AT FORWARD SIDE OF BS 847 JUST INBOARD OF STR 25 RT. MAINTENANCE REMOVED DAMAGED SECTION OF FRAME AT BS 847 FROM STR 25 RT TO STR 26 RT; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIRFeb 17, 2005 · N326AW · Boeing 737301 · Fuselage Main, FrameSDR SWAA050456Seal · blownDIVERSION, DECLARED EMERGENCY. A-SYSTEM ENGINE LOW PRESSURE LIGHT ILLUMINATED, FOLLOWED BY A-SYSTEM HYDRAULIC FLUID LOSS. REMOVED AND REPLACED RT WING INBOARD FLIGHT SPOILER ACTUATOR O-RING PER MM.Feb 16, 2005 · N659SW · Boeing 737301 · Drag Control ActuatorSDR AWXA200500298Clip · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN AFT CARGO COMPARTMENT FRAME ATTACH CLIP AT BS 807, STR 25 RT. MAINTENANCE REMOVED CRACKED AFT CARGO COMPARTMENT FRAME ATTACH CLIP AT BS 807, STR 25 RT; FABRICATED A NEW REPLACEMENT CLIP PER Feb 15, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500309Bear Strap · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND INTERNAL SURFACE OF AFT CARGO DOOR CUTOUT LOWER FORWARD BEAR STRAP BS 807, STR 25 RT. MAINTENANCE CUT OUT DAMAGE IN AFT CARGO DOOR CUTOUT LOWER FORWARD BEAR STRAP AT BS 807, STR 25 RT; FABRICATED 2 EAFeb 13, 2005 · N326AW · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200500334Web · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR SILL WEB BETWEEN BS 794 AND BS 799, AT STR 25 RT. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL WEB AT STR 25 RT, FROM BS 794 TO BS 799; FABRICATED A NEW REPLACEMENT WEB PER DWG 6Feb 12, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500332Angle · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR SILL ATTACH ANGLE AT BS 847, BETWEEN STR 24 RT AND STR 25 RT. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL ATTACH ANGLE AT BS 847, FROM STR 24 RT TO STR 25 RT; FABRICATED A NEW RFeb 12, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500315Frame · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR FORWARD TORQUE BOX FRAME AT BS 794.3, STR 25 RT. MAINTENANCE REMOVED CORRODED SECTION AFT CARGO DOOR FORWARD TORQUE BOX FRAME AT BS 794.3, STR 25 RT; FABRICATED A NEW REPLACEMENT SECFeb 12, 2005 · N326AW · Boeing 737301 · Fuselage Main, Frame
Back to Boeing 737-301