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 SWAA010008Lens · brokenDURING SCHEDULED C1 CHECK, FOUND LT & RT OVERWING EMERGENCY EXIT LIGHT LENSES BROKEN. REMOVED AND REPLACED LENS ASSYS PER MM.Jan 1, 2001 · N659SW · Boeing 737301 · Emergency LightingSDR SWA010008Lens · brokenDURING SCHEDULED C1 CHECK, FOUND LT & RT OVERWING EMERGENCY EXIT LIGHT LENSES BROKEN. REMOVED AND REPLACED LENS ASSY''S PER MM.Jan 1, 2001 · N659SW · Boeing 737301 · Emergency LightingSDR AWXA0001162Charger · inoperativeEMERGENCY ESCAPE PATH LIGHTS INOP ROWS 11-15. REPLACED BATTERY CHARGER; LIGHTS OPERATIONALLY CHECKED GOODDec 29, 2000 · N326AW · Boeing 737301 · Emergency LightingSDR USAA002204Bulkhead · crackedCLT - FOUND WEB CRACKED 1 INCH, STATION 178, WL 198, LBL 4. INSTALLED DOUBLER PER EA 68679. (M)Dec 27, 2000 · N355US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA002197Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 727B STRINGER 14R. INSTALLED ANGLE PER SRM 53-00-07. (M)Dec 26, 2000 · N355US · Boeing 737301 · Fuselage Main, FrameSDR USAA002198Frame · crackedCLT - FOUND CHORD CRACKED 1.5 INCH, BS 178, WL 207, RBL 29. REMOVED SECTION AND INSTALLED NEW SECTION PER EA 68680 AND EO 5300V157. (M)Dec 26, 2000 · N355US · Boeing 737301 · Fuselage Main, FrameSDR USAA002199Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 1 INCH BY 1 INCH, BS 178, WL 195, LBL 24. INSTALLED NEW INTERCOSTAL PER SRM 51-10-02. (M)Dec 26, 2000 · N355US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA002200Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .750 INCH BY 1 INCH, BS 178, WL 195, RBL 24. INSTALLED NEW INTERCOSTAL PER SRM 51-10-02 AND EO5300V157. (M)Dec 26, 2000 · N355US · Boeing 737301 · Fuselage Main, BulkheadSDR USAASB00358Uplock Sensor · faultyCLT - FLT 458 - DURING CLIMB-OUT FROM YYZ, THE RIGHT MAIN LANDING GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CREW EXTENDED AND RETRACTED GEAR TWICE. THE RED LIGHT EXTINGUISHED UPON GEAR EXTENSION BUT RE-ILLUMINATED WHEN GEAR HANDLE WAS UP AD Dec 25, 2000 · N589US · Boeing 737301 · Landing Gear Position and WarningSDR USAA002194Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1 INCH BY 1 INCH, STATION 344, LBL 9. CORROSION LEVEL 1. REMOVED T-CAP AND FABRICATED NEW T-CAP AND SPLICE PER SRM 53-10-51 AND 53-40-51. (M)Dec 22, 2000 · N355US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA002184Doubler · crackedCLT - FOUND ANTENNA DOUBLER CRACKED .5 INCH, STATION 727D-727E, BL 0. INSTALLED NEW DOUBLER PER SRM 51-10-02. (M)Dec 21, 2000 · N355US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB00352Jackscrew · wornCLT - FLT 1974 - ON DESCENT INTO CLT, FROM MBJ, CAPTAIN NOTIFIED TOWER THAT THE FLAPS WOULD NOT EXTEND BEYOND FIVE DEGREES. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MX TDec 20, 2000 · N585US · Boeing 737301 · Trailing Edge Flap Control SystemSDR USAA002175Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 1 INCH, STATION 328 FLOORBEAM AT RBL 14, 21, 35. CORROSION LEVEL 1 C53-107-01. INSTALLED NEW T-CAP AND FABRICATED SPLICE ANGLES PER SRM 53-10-51. (M)Dec 20, 2000 · N355US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA002176Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED 1 INCH, STATION 344, STRINGER 10R. FABRICATED NEW CLIP PER SRM 53-10-15 AND SRM 51-10-2. (M)Dec 20, 2000 · N355US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA002177Shear Tie · crackedCLT - FOUND TIE ANGLE CRACKED .333 INCH, FRAME 360 BETWEEN STRINGER 14R AND STRINGER 15R. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-07 FIG 207. (M)Dec 20, 2000 · N355US · Boeing 737301 · Fuselage Main, StructureSDR USAA002178Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .25 INCH, INTERCOSTAL AT FS 294.5, STRINGER 7L. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M)Dec 20, 2000 · N355US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA002163Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH, STATION 312 BL 0. CORROSION LEVEL 2 C53-107-02. REPLACED T-CAP PER SRM 53-00-51. (M)Dec 18, 2000 · N355US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA002160Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED .5 INCH, FORWARD OF FS 303.9 ABOVE STRINGER 10L. INSTALLED NEW ATTACH ANGLE PER SRM 51-10-02. (M)Dec 18, 2000 · N355US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA002161Attach Angle · crackedCLT - FOUND FRAME ATTACH ANGLE CRACKED .25 INCH, FRAME ATTACH ANGLE AT FS 348.2 STRINGER 11L. FABRICATED NEW ATTACH ANGLE PER SRM 51-10-2. (M)Dec 18, 2000 · N355US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA002162Shear Tie · crackedCLT - FOUND FRAME SHEAR TIE CRACKED .5 INCH, STATION 967, BETWEEN STRINGER 6L AND 7L. REMOVED AND INSTALLED DOUBLER PER EA 68751. (M)Dec 18, 2000 · N355US · Boeing 737301 · Fuselage Main, StructureSDR USAA002158Floorbeam · corrodedCLT - FOUND SPLICE ANGLE T-CAP CORRODED, STATION 344, RBL 9, LBL 37. REPLACED T-CAP PER SRM 53-10-51. (M)Dec 15, 2000 · N355US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA002156Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, FRAME STATION 887 STRINGER 9R. REPAIRED DOUBLER PER TR 53-10-14. (M)Dec 15, 2000 · N355US · Boeing 737301 · Fuselage Main, FrameSDR USAA002157Angle · crackedCLT - FOUND CORNER ANGLE CRACKED .75 INCH, DOOR CUTOUT LOWER AFT CORNER ANGLE. INSTALLED NEW CORNER ANGLE. (M)Dec 15, 2000 · N355US · Boeing 737301 · Fuselage Main, StructureSDR USAA002148Stringer Clip · crackedCLT - FOUND STRINGER CLIP CRACKED 1 INCH, STATION 807, STRINGER 4L. REPLACED CLIP PER SRM 51-10-02. (M)Dec 14, 2000 · N355US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA002149Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, FS 847, STRINGER 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)Dec 14, 2000 · N355US · Boeing 737301 · Fuselage Main, FrameSDR USAA002150Frame · crackedCLT - FOUND FUSELAGE FRAME CRACKED .5 INCH, STATION 827 ABOVE STRINGER 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Dec 14, 2000 · N355US · Boeing 737301 · Fuselage Main, FrameSDR USAA002151Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, FRAME 400 ABOVE STRINGER 9R. REPAIRED DOUBLER PER TR 53-10-14. (M)Dec 14, 2000 · N355US · Boeing 737301 · Fuselage Main, FrameSDR USAA002152Stringer Clip · crackedCLT - FOUND STRINGER CLIP CRACKED .5 INCH, STATION 639, STRINGER 2L CLIP. REPLACED PART PER SRM 51-10-2 AND 51-40-2. (M)Dec 14, 2000 · N355US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAASB00348Gcu · looseMSY - FLT 796 - PRIOR TO DEPARTURE, THE RT GENERATOR WAS PLACED ON MEL BECAUSE IT WOULD NOT COME ON LINE. SHORTLY AFTER TAKEOFF FROM MSY, THE APU FAILED TO POWER THE RIGHT SIDE, THEN THE TRANSFER BUS FAILED. FLIGHT RETURNED TO FIELD AT MSY AND LANDED WITHOUTDec 14, 2000 · N353US · Boeing 737301 · AC RegulatorSDR USAA002092Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .50 INCH, STATION 616 STRINGER 2R. INSTALLED TIE CLIP PER SRM 51-10-02 AND SRM 51-40-03. (M)Dec 11, 2000 · N355US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA002093Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, STATION 727E, STRINGER 7R. REPAIRED PER SRM 51-10-02. (M)Dec 11, 2000 · N355US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA002077Web · crackedCLT - FOUND WEB PLATE CRACKED 2 INCHES, STATION 639 STRINGER 17R. REPAIRED PER SRM 51-10-2. (M)Dec 7, 2000 · N355US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA002078Crease Beam · crackedCLT - FOUND CREASE BEAM CRACKED 1 INCH, BS 639 BETWEEN STATION 619-639 STRINGER 17L REPAIRED PER SRM 51-10-2. (M)Dec 7, 2000 · N355US · Boeing 737301 · Fuselage Main, StructureSDR SWAA002513Stiffener · crackedDURING SCHEDULED RON CHECK, FOUND BS 663 BULKHEAD MLG W/W STIFFNER CRACKED AT RBL 3. R&R STIFFNER PER SRM.Nov 30, 2000 · N659SW · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB0034Indicator · faultyPIT - FLT 1912 - ON DESCENT INTO PIT FROM PVD, CAPTAIN REPORTED A FLAP ASYMMETRY PROBLEM AS FLAPS WERE MOVED BETWEEN 1 AND 5 POSITION. LEFT FLAP POSITION INDICATED 1 AND RIGHT FLAP POSITION INDICATED 3. AFTER FOLLOWING QUICK REFERENCE HANDBOOK PROCEDURES, FLNov 28, 2000 · N590US · Boeing 737301 · Trailing Flap Position Indicating SystemSDR AWXA0000993Light · inoperativeEMERGENCY LIGHT AT ROW 18 AND ROW 3 INOP. SPLICED BROKEN WIRES AT THE SEATS, OPS CHECKS GOODNov 27, 2000 · N326AW · Boeing 737301 · Emergency LightingSDR AWXA0000991Fuel Control · failedOAK - ABORTED TAKEOFF - NR 2 ENGINE WOULD NOT DEVELOP TAKEOFF POWER. AFTER TROUBLESHOOTING, THE NR 2 ENGINE DRIVEN FUEL PUMP AND MEC (MAIN ENGINE FUEL CONTROL) WERE CHANGED; ALL OPS AND POWER RUNS GOOD.Nov 27, 2000 · N326AW · Boeing 737301 · Fuel Controlling SystemSDR USAASB00324Control Handle · lack of lubePHL - FLT 1091 - ON APPROACH INTO PHL, FROM BOS, CREW RECEIVED THREE GREEN AND THREE RED GEAR LIGHTS WHEN GEAR HANDLE WAS SELECTED DOWN. CREW ACCOMPLISHED GO-AROUND AND FOUND THAT GEAR HANDLE DID NOT SEAT INTO DOWN DETENT. CREW RECYCLED GEAR AND PUSHED HANDLNov 22, 2000 · N336US · Boeing 737301 · Landing Gear SelectorSDR USAASB00318Computer · failedTPA - FLT 1091 - EN ROUTE FROM PHL TO GCM, BOTH FLIGHT MANAGEMENT COMPUTER SYSTEM CONTROL DISPLAY UNITS FAILED. FLIGHT DIVERTED TO TPA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLIGHT MANAGEMENT COMPUTER. SYSTEM OPERATIONAL CNov 19, 2000 · N342US · Boeing 737301 · Flight Management Computing Hardware SystemSDR SWAA002412Light · inoperativeFWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.Nov 19, 2000 · N659SW · Boeing 737301 · Emergency LightingSDR USAA001958Skin · crackedCLT - FOUND CUT OUT FOR A/C HOOK CRACKED .25 INCH, AIR CONDITION GROUND CONNECTION STATION 527 STRINGER 28L. MANF STRAP .0637075T-6 AND FILLED .125 2024T-3 PER EA 66651. (M)Nov 17, 2000 · N334US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB00316Transformer · malfunctionedFLT 1514 - DEPARTING DCA EN ROUTE TO SYR, PILOT REPORTED ELECT SMELL IN COCKPIT AND CABIN WITH A/C ON THE GROUND AFTER ENG START AND THROUGHOUT T/O. AFTER 2,000 FT, MAIN ELECTRIC TRIM YOKE SWITCHES WERE INOP. CREW FOUND TRANSFORMER RECTIFIER NR 2 C/B POPPED.Nov 16, 2000 · N590US · Boeing 737301 · DC Rectifier/ConverterSDR USAASB00314Flap · malfunctionedBWI - FLT 2046 - ON APPROACH TO DCA, FROM MCI, THE TRAILING EDGE FLAPS STOPPED AT 8-10 DEGREES WITH NEEDLES SPLIT ON INDICATOR. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND DIVERTED TO BWI. FLIGHT LANDED AT 5 DEGREES TRAILING EDGE FLAPS AND WITHOUT Nov 14, 2000 · N585US · Boeing 737301 · Trailing Edge Flap Control SystemSDR USAASB00313Valve · leakingCLT - FLT 9228 - ON CLIMB-OUT FROM CLT, BETWEEN 13,000 - 14,000 FEET, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW FOLLOWED PROCEDURES FOR THIS AND THEN HAD TO SHUTDOWN THE NR 2 ENGINE. CREW DECLARED AN EMERGENCY AND THE FLIGHT RETURNED TO FIELD AT CLT WNov 13, 2000 · N336US · Boeing 737301 · Pneumatic Distribution SystemSDR USAASB00309Door · not closedATL - FLT 1273 - AFTER TAKEOFF FROM ATL, THE AIRCRAFT WOULD NOT PRESSURIZE. CRWE NOTICED THE AFT RIGHT SERVICE DOOR WAS LEAKING AIR. FLIGHT RETURNED TO FIELD AT ATL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE AFT RNov 6, 2000 · N346US · Boeing 737301 · Service DoorsSDR SWAA002171Skin · corrodedDURING SCHEDULED SPECIAL VISIT, FOUND SKIN BULGED AT BS 741, KEEL BEAM, LT. REPAIRED SKIN PER RA 1-353-2387.Oct 27, 2000 · N660SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA001814Splice · crackedCLT - FOUND SPLICE CRACKED .25 INCH, STATION 907 STRINGER 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-10-02. (M)Oct 25, 2000 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001813Splice · crackedCLT - FOUND SPLICE CRACKED .25 INCH, STATION 907, STRINGER 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-10-02. (M)Oct 25, 2000 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001812Frame · crackedCLT - FOUND BELT FRAME CRACKED .5 INCH, BS 827, STRINGER 9L. REMOVED DAMAGED AND INSTALLED DOUBLER PER EA 68156. (M)Oct 25, 2000 · N356US · Boeing 737301 · Fuselage Main, FrameSDR USAA001811Keelbeam · crackedCLT - FOUND KEEL BEAM LOWER SKIN CRACKED 3 INCHES, BS 730, LBL 3 KEEL BEAM LOWER SKIN PANEL. INSTALLED NEW SKIN PANEL AND DOUBLER PER EA 68213. (M)Oct 25, 2000 · N356US · Boeing 737301 · Fuselage Main, Keel
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