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 F3LA00163Skin · crackedDEN - DURING C-2 CHECK, INSPECTION REPORTED CRACKS AROUND FORWARD LAVATORY SERVICE PANEL AT FILL PORT BACKSIDE OF RIVET HOLES, 1, 3, 5, AND 9 O''CLOCK POSITIONS. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED DAMAGE PER SRM 51-60-02, 51-20-02, 51-30-05Jul 30, 2000 · N578US · Boeing 737301 · Fuselage Main, Plate/SkinSDR F3LA00162Skin · corrodedDEN - DURING C-2 CHECK, INSPECTION REPORTED CORROSION BEHIND FORWARD LAVATORY DUMP VALVE. MAINTENANCE REPAIRED PER SRM 51-10-6 AND SRM 51-20-02. (X)Jul 30, 2000 · N578US · Boeing 737301 · Fuselage Main, Plate/SkinSDR F3LA00161Skin · delaminatedDEN - DURING C-2 CHECK, INSPECTION REPORTED LT AILERON TAB DELAMINATED AT TRAILING EDGE. MAINTENANCE REPAIRED PER SRM 51-70-06, REPAIR NR 6 AND 51-60-03 AND REINSTALLED PER MM 27-11-21. (X)Jul 30, 2000 · N578US · Boeing 737301 · Aileron TabsSDR F3LA00160Skin · crackedDEN - DURING C-2 CHECK, INSPECTION REPORTED R-1 DOOR UPPER HINGE ARM CUT-OUT CRACKED (APPROXIMATELY .250 INCH LONG). MAINTENANCE REMOVED DAMAGED AREA AND REPAIRED PER SRM 51-10-02 AND SRM 51-20-01 AND MM 51-21. (X)Jul 29, 2000 · N578US · Boeing 737301 · Passenger/Crew DoorsSDR F3LA00159Skin · delaminatedDEN - DURING C-2 CHECK, INSPECTION REPORTED LEFT AILERON INBOARD BOTTOM CORNER IN HINGE AREA DELAMINATED IN THREE PLACES. MAINTENANCE REPLACED LEFT AILERON PER MM 27-11-11. (X)Jul 26, 2000 · N578US · Boeing 737301 · AileronsSDR F3LA00158Floor Panel · corrodedDEN - DURING C-2 CHECK, INSPECTION REPORTED CORROSION AT BOTTOM OUTBOARD FORWARD CORNER OF NR 2 GALLEY. MAINTENANCE REPLACED FLOOR PANEL PER SRM 51-10-2. (X)Jul 25, 2000 · N578US · Boeing 737301 · Fuselage Floor PanelSDR USAA001038Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 2 INCHES, FS 328 BETWEEN RBL 42 AND LBL 29. CORROSION 12 AREAS LEVEL 1. REMOVED DAMAGED PER SRM 53-10-51 FIG 205. (M)Jul 21, 2000 · N353US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001042Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, BS 344, STRINGER 11R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02 AND DWG 69 389396. (M)Jul 21, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001041Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, STRINGER 10 LT AT STATION 663. REMOVED AND REPLACED CLIP PER TR 51-10-02. (M)Jul 21, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001040Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, STRINGER 10R TIE CLIP AT STATION 663. REPLACED TIE CLIP PER TR 51-10-02. (M)Jul 21, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001037Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .75 INCH, STATION 178, RBL 4.75 WL 201. INSTALLED DOUBLER PER SRM 53-10-08. (M)Jul 21, 2000 · N353US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001036Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .75 INCH, STATION 178, LBL 4.75, WL 201. INSTALLED DOUBLER PER SRM 53-10-08. (M)Jul 21, 2000 · N353US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001035Bulkhead · crackedCLT - FOUND BULKHEAD WEB .75 INCH, STATION 178 BULKHEAD WEB, LBL 4.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)Jul 21, 2000 · N353US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001034Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .75 INCH, STATION 178 BULKHEAD WEB, RBL 4.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)Jul 21, 2000 · N353US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001033Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .25 INCH, STATION 178 BULKHEAD, WEB RBL .5, WL 206. INSTALLED DOUBLER PER SRM 53-10-08. (M)Jul 21, 2000 · N353US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001032Frame · crackedCLT - FOUND FRAME WEB CRACKED .25 INCH, STATION 847 AT STRINGER 9 RT. INSTALLED DOUBLER PER TR 53-10-14. (M)Jul 21, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA001010Support Bracket · crackedCLT - FOUND DOOR SUPPORT CRACKED .25 INCH, STATION 294.5, FRAME AT STRINGER 14L. FABRICATED NEW WEB AND INSTALLED PER SRM 51-70-11. (M)Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001009Door Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 294.5, STRINGER 7L. REPAIRED PER SRM 53-10-15. (M)Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, StructureSDR USAA001008Door Frame · crackedCLT - FOUND FRAME CRACKED 2.5 INCHES, STATION 294.5, FORWARD SERVICE DOOR FRAME WL 208. REMOVED DAMAGED AREA INSTALLED REPAIR DOUBLER PER SRM 50-70-11. (M)Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, StructureSDR USAA001007Web · crackedCLT - FOUND WEB CRACKED .500 INCH, STRINGER 14R, WEB INNER CHORD ANGLE STATION 278. FABRICATED NEW WEB AND INSTALLED PER SRM 51-40-00 AND DWG 6 45807. (M)Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001006Bulkhead · crackedCLT - FOUND WEB CRACKED TWO PLACES .25 INCH AND 1.5 INCH, STATION 178 BULKHEAD, WEB RBL 6.75, WL 201. FABRICATE REPAIR DOUBLER PER SRM 53-10-08 DETAIL 111. (M)Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001005Angle · crackedCLT - FOUND CHORD ANGLE CRACKED .5 INCH, LBL 5.7 VERT CHORD L/B FLANGE STATION 178, WL 184. INSTALLED REPAIR ANGLE AND STRAPS PER SRM 53-10-08. (M)Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001000Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 500A BETWEEN STRINGER 8 AND 9L. REMOVED AND INSTALLED DOUBLER PER TR 53-10-14. (M)Jul 20, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA000999Frame · crackedCLT - FOUND FUSE FRAME CRACKED .250 INCH, BS 480 BETWEEN STRINGER 8 AND 9R. REMOVED AND INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)Jul 20, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA001004Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344, LBL 36. FABRICATED T-CAP PER REPAIR DOCUMENT 53-10-51. (M)Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001003Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344, LBL 28. REMOVED AND REPLACED T-CAP PER SRM 53-10-51. CORROSION LEVEL 1. (M)Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001002Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344, LBL 14. CORROSION LEVEL 1. FABRICATED T-CAP PER SRM 53-10-51. (M)Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001001Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 312, LBL 12. REMOVED DAMAGED T-CAP PER SRM 53-10-51 FIG 205. (M)Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001022Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 328, LBL 28. CORROSION LEVEL 1. FABRICATED NEW T-CAP AND INSTALLED PER REPAIR 51-70-12. (M)Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001021Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 312, BL 0. CORROSION LEVEL 1. FABRICATED NEW T-CAP AND SPLICE ANGLE PER SRM 53-10-51. (M)Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001020Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 312, RBL 36. FABRICATED NEW T-CAP AND SPLICE ANGLE PER SRM 53-10-51. CORROSION LEVEL 1. (M)Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001019Frame · crackedCLT - FOUND FRAME WEB CRACKED .25 INCH, STATION 787 FRAME WEB AT STRINGER 9LT. INSTALLED DOUBLER PER TR 53-10-14. (M)Jul 20, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA001018Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 767 FRAME, WEB AT STRINGER 9 RT. INSTALLED DOUBLER PER TR 53-10-14. (M)Jul 20, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA001017Stringer Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .250 INCH, FORWARD OUTBOARD HOLE TIE CLIP STATION 887, STRINGER 13R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M)Jul 20, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001016Stringer Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .250 INCH, STRINGER 13R TIE CLIP FORWARD OUTBOARD HOLE STATION 867. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM 51-10-2. (M)Jul 20, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA00157Skin · corrodedDEN - FOUND DURING C-2 CHECK, CORROSION AROUND AFT LAVATORY DUMP VALE, INTERIOR SIDE OF AIRCRAFT SKIN, REF EO 38-30-737-001. MAINTENANCE REPLACED INTERIOR STRUCTURE OF AFT LAVATORY DUMP VALE PER SRM 51-10-2. (M)Jul 19, 2000 · N578US · Boeing 737301 · Fuselage Main, Plate/SkinSDR F3LA00155Panel · crackedDEN - DURING C-2 CHECK INSPECTION, FOUND 4 CRACKS IN NR 2 ENGINE PYLON PANEL NR 5824R IN UPPER FORWARD CORNER OF ACCESS HOLE. MAINTENANCE REPAIRED DAMAGED AREA PER EA 54-737-015A. (M)Jul 14, 2000 · N578US · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR USAASB00187Sensor · failedBOS - FLT 6527 - AFTER TAKEOFF, THE LANDING GEAR LEVER WOULD NOT MOVE UP TO THE RETRACT POSITION. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND RETURNED TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENJul 9, 2000 · N349US · Boeing 737301 · Landing Gear Retraction/Extension SystemSDR F3LA00153Tab · damagedDEN - DURING C-2 INSPECTION, REPORTED LEFT AILERON TAB DAMAGED. MAINTENANCE REPAIRED DAMAGE PER SRM 51-70-06. REPAIR NR 6. (M)Jul 8, 2000 · N578US · Boeing 737301 · Aileron TabsSDR F3LA00156Skin · corrodedDEN - DURING C-2 CHECK INSPECTION, FOUND AREA BEHIND FORWARD LAVATORY FILL PORT CORRODED. MAINTENANCE REMOVED CORROSION AND REPAIRED PER SRM 51-10-06. (M)Jul 8, 2000 · N578US · Boeing 737301 · Fuselage Main, Plate/SkinSDR F3LA00154Floor Support · crackedDEN - DURNG C-2 CHECK INSPECTION, FOUND FLOOR ANGLE CRACKED AT CENTER OF FLOOR, BS 360-380, FLOOR CAP SECTION. MAINTENANCE REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED REPLACEMENT SHEAR WEB TOP ANGLE PER SRM 53-30-51. (M)Jul 8, 2000 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB00185Control Panel · failedPHL - FLT 637 - EN ROUTE FROM BOS-PHL, AT FL280, THE CABIN PRESSURE BEGAN TO SLOWLY CREEP UP TO 10,000 FEET. THE ALTITUDE WARNING HORN SOUNDED AND THE CREW BEGAN AN IMMEDIATE DESCENT. NO EMERGENCY WAS DECLARED AND NO OXYGEN MASKS WERE DEPLOYED. FLIGHT CONTIJul 4, 2000 · N585US · Boeing 737301 · Cabin Pressure IndicatorSDR USAA000891Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, BS 344 STRINGER 11R. FABRICATED CLIP PER BOEING DWG 6938939. (M)Jul 3, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000892Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STRINGER 1 BS 380. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)Jul 3, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000893Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 380, STRINGER 2L. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)Jul 3, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000894Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .0625 INCH, BS 616, STRINGER 4L. INSTALLED NEW TIE CLIP PER SRM 51-10-2. (M)Jul 3, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000895Tie Clip · crackedCLT - FOUND TIE CILP CRACKED .0625 INCH, BS 639, STRINGER 4L. INSTALLED CLIP PER SRM 51-10-2. (M)Jul 3, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000896Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, FORWARD SIDE FRAME 907, BELOW STRINGER 1. REPLACED TIE CLIP PER BOEING DWG 69-47869. (M)Jul 3, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000897Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED TWO PLACES .5 INCH, FS 663, STRINGER 10L. INSTALLED CLIP PER SRM 51-10-2. (M)Jul 3, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB00181Structure · crackedPIT - FLT 9234 - EN ROUTE FROM ROC-CMH, CAPTAIN REPORTED AN AIRFRAME VIBRATION WHICH WAS FELT IN THE AFT GALLEY/LAVATORY AREA. VIBRATION WAS OF HIGH FREQUENCY AND MODERATE FROM 5,000 TO 31,000 FEET BETWEEN 220 TO 300 KNOTS. CAPTAIN ACCOMPLISHED TROUBLESHOOTIJun 29, 2000 · N562AU · Boeing 737301 · Elevator, Tab Structure
Back to Boeing 737-301