Boeing 737-4B7

Service difficulty reports · 5,757

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 = '7374B7'
  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 USAA010035Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH, BS 440, BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-04. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010036Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 480 BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010037Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 500A BETWEEN STRINGER 8L AND 9L. REMOVED DAMAGE AND INSTALLED OVERSIZED HI-LOCK PER SRM 51-40-03. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010038Frame · crackedCLT - FOUND FRAME CRACKED .500 INCH, BS 727B BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLE RPER TR 53-10-14. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010024Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY .5 INCHES, BS 967, LBL 14-18. CORROSION LEVEL 1 C53-107-02. INSTALLED LEG REPAIR AND DOUBLER PER SRM 53-60-51 FIG 203. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010025Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 2.25 INCH BY 40 INCH, LEFT AFT ENTRY DOOR Z-ANGLE STATION 953-994, LBL 53. REPLACED Z-ANGLE PER 51-10-1. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA002189Skin · crackedPIT - FOUND LEFT ELEVATOR .625 INCH LONG CRACK, TOP SIDE SKIN AT CORNER OF TAB CUT OUT ELEV STATION 123. REMOVED CRACK, TAPER SANDER BACK THEN REPLACED LAYER PLUS 2 EXTRAS EPR SRM 55-20-01, AND 51-70-17 AND EA. (M)Dec 18, 2000 · N436US · Boeing 7374B7 · Elevator, Plate/SkinSDR USAA002137Skin · crackedTPA - FOUND SKIN CRACKED 1.5 INCH, RIGHT HORIZ STAB LOWER SKIN STATION 125. INSTALLED REPAIR DOUBLER PER SRM 55-10-01 AND TR 55-10-07. (M)Dec 13, 2000 · N445US · Boeing 7374B7 · Horizontal Stabilizer, Plate/SkinSDR USAA002106Crossbeam · wornPIT - FOUND ENGINE MOUNT CROSSBEAM .015 INCH WEAR, BEARING BORE ON TOP OF MOUNT. OPEN UP BORE .005 ON TOP OF MOUNT. OPEN UP BORE .005 INCH TO INSTALL 2 OVERSIZE BEARINGS PER EA 57451. (M)Dec 8, 2000 · N436US · Boeing 7374B7 · Engine Mount SectionSDR USAASB00345Relay · faultyCLT - FLT 1893 - ON APPROACH INTO CLT, AFTER LOWERING L/G, CAPT RECEIVED A NOSE GEAR UNSAFE IND AND HAD NO IND AS TO THE POSITION OF THE MAIN GEAR. CAPT ATTEMPTED TO RECYCLE THE GEAR BUT THE GEAR HANDLE WOULD NOT MOVE PAST THE NEUTRAL POSITION. THE F/O ACCOMDec 7, 2000 · N435US · Boeing 7374B7 · Landing Gear Retraction/Extension SystemSDR USAASB00343Light · defectiveLGA - FLT 798 - ON APPROACH TO LGA, AFTER LANDING GEAR EXTENSION, CREW DID NOT RECEIVE A GREEN LIGHT FOR THE LEFT MAIN LANDING GEAR. CREW RECYCLED THE GEAR AND RECEIVED SAME INDICATION. A GO-AROUND WAS EXECUTED AND THE LANDING GEAR WAS RECYCLED AGAIN. THIS Dec 6, 2000 · N438US · Boeing 7374B7 · Landing Gear Position and WarningSDR USAASB00344Windshield · crackedLGA - FLT 236 - ON DESCENT INTO LGA, PASSING THROUGHT FL270, THE CAPTAINS WINDSHIELD ARCED ALONG THE TOP OF THE WINDOW AND LATER CRACKED. CAPTAIN REQUESTED A LOWER ALTITUDE, BUT AIR TRAFFIC CONTROL ADVISED THAT HE WOULD HAVE TO WAIT. IN THE CAPTAINS OPINION,Dec 6, 2000 · N426US · Boeing 7374B7 · Flight Compartment WindowsSDR USAA002223Skin · crackedPIT - FOUND SKIN CRACKED 2 INCHES, RIGHT STATION 727E STRINGER 24 RT. REMOVED CRACK, INSTALLED EXT DOUBLER WITH BLIND FASTENERS PER SRM 53-00-01 FIG 201. (M)Nov 30, 2000 · N432US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAASB00335Light · failedCLT - PILOT REPORTED THAT THE EMERGENCY EXIT ROW END LIGHT WAS BROKEN/INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT ROW END LIGHT ASSEMBLY. OPS CHECK GOOD. (M)Nov 28, 2000 · N430US · Boeing 7374B7 · Emergency LightingSDR USAA001982Frame · crackedCLT - FOUND CHORD CRACKED 1.5 INCH, STATION 178, WL 207, RT FUSELAGE CHORD. REPAIRED DOUBLER PER EA 68417. (M)Nov 27, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001983Angle · crackedCLT - FOUND SUPPORT ANGLE CRACKED .5 INCH, STATION 301 FORWARD OF FORWARD ENTRY DOOR UPPER HINGE AREA. REPAIRED DOUBLER PER SRM 51-10-02. (M)Nov 27, 2000 · N431US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA001984Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 460, BETWEEN STRINGER 8 AND 9R. REPAIRED DOUBLER PER TR 53-10-14. (M)Nov 27, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001985Doubler · crackedCLT - FOUND ANTENNA DOUBLER 5 INCH CRACK, STATION 727D PLUS 6 INCH BL 0. FABRICATED NEW BRACKET PER SRM 51-10-02. (M)Nov 27, 2000 · N431US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA001986Frame · crackedCLT - FOUND FRAME CRACKED, BS 867, BETWEEN STRINGER 8/9L. REMOVED AND FABRICATED DOUBLER PER TR 53-10-14. (M)Nov 27, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAASB00332Slat · lack of lubeIAD - FLT 1827 - CLIMBING OUT OF PHL THROUGH FL240, EN ROUTE TO CLT, THE NR 4 LEADING EDGE SLAT INTRANSIT LIGHT ILLUMINATED ON FORWARD AND OVERHEAD PANELS ALONG WITH A VIBRATION. CREW DESCENDED AND FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES. AT FL200, CREWNov 26, 2000 · N431US · Boeing 7374B7 · Leading Edge Slat Control SystemSDR USAASB00326Switch · faultyBWI - FLT 317 - EN ROUTE FROM BDL TO CLT, AND APU SHUTDOWN OCCURRED IN FLIGHT AT FL350 AND FL260. THE APU LOW OIL PRESSURE AND HIGH OIL TEMPERATURE LIGHTS ILLUMINATED. WITH THE NR 1 ENGINE GENERATOR ALREADY ON MEL, FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FNov 22, 2000 · N444US · Boeing 7374B7 · APU Indicating SystemSDR USAASB00323Harness · faultyMSP - FLT 1181 - EN ROUTE FROM PIT TO MSP, CREW REPORTED ON APPROACH TO MSP LOST FLIGHT DIRECTOR, NR 1 ENG N1, NR 1 ENG FUEL FLOW, ANTI-SKID, YAW DAMPER, NR 1 ELECTRIC HYD PUMP, CABIN AND COCKPIT EMERGENCY LIGHTS AND THE NR 1 TRU C/B TRIPPED. FLT LANDED W/O FNov 21, 2000 · N444US · Boeing 7374B7 · AC Power Distribution SystemSDR USAASB00320Battery · dischargedEWR - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 12 THROUGH 19ABC, RIGHT AFT OVERWING AND AFT EXTERIOR LIGHTS. MAINTENANCE REPAIRED WIRING AT SEAT ROW 14ABC AND REPLACED BATTERY AND BATTERY CHARGER. ALSO, REPLACED AFT M1197 BATTERY CHARGNov 20, 2000 · N777AU · Boeing 7374B7 · Emergency LightingSDR USAASB00319Charger · failedPHL - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTS FOR SEAT ROWS 12 THROUGH 18 AND 20 THROUGH 23 ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY CHARGER M1136 AND M1197. ALSO, REPLACED THE BATTERY (P/N AD2013-1A) IN BATTERY CHARGER M1197. OPENov 18, 2000 · N777AU · Boeing 7374B7 · Emergency LightingSDR USAA001928Frame · crackedCLT - FOUND CHORD CRACKED 1.5 INCHES, STATION 178, WL 207, LT CHORD SIDE SKIN. REPAIRED DOUBLER PER EA 68426. (M)Nov 13, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001929Bulkhead · crackedCLT - FOUND SKIN CRACKED 1 INCH IN TWO PLACES, BS 178, LBL 5.5, WL 201, 198 BBL 0, WL 190. DOUBLER REPLACED PER EA 68454. (M)Nov 13, 2000 · N431US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA001937Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 907, BETWEEN STRINGER 8 AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Nov 13, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001930Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 380, BETWEEN STRINGER 8 AND 9 R. INSTALLED DOUBLER PER TR 53-10-14. (M)Nov 13, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001931Frame · crackedCLT - FOUND FRAME CRACKED BS 400, BETWEEN STRINGER 8 AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)Nov 13, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001932Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 747, BETWEEN STRINGER 8/9R. REMOVED DAMAGED AND FABRICATED DOUBLER PER TR 53-10-14. (M)Nov 13, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001933Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 827, BETWEEN STRINGER 8/9R. INSTALLED OUTSIDE REPAIR DOUBLER PER TR 53-10-14. (M)Nov 13, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001934Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 827, BETWEEN STRINGER 8 AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Nov 13, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001935Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 867, BETWEEN STRINGER 8/9R. REPAIRED DOUBLER PER TR 53-10-14. (M)Nov 13, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001936Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 907, BETWEEN STRINGER 8/9R. REPAIRED DOUBLER PER TR 53-10-14. (M)Nov 13, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAASB00312Unknown · odorSYR - FLT 1862 - EN ROUTE FROM BTV-PIT, DURING CRUISE, THE AFT FLIGHT ATTENDANT REPORTED A BURNED RUBBER SMELL IN THE AFT CABIN BETWEEN THE REAR LAVATORIES NEAR THE OVERHEAD. CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO SYR. FLIGHT LANDED WITHOUT FURTHER INNov 11, 2000 · N439US · Boeing 7374B7 · Air Distribution SystemSDR USAA001918Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, STATION 986.5, LBL 7 - LBL 31. CORROSION LEVEL 1 C 53-107-02. REMOVED AND REPLACED T-CAP PER TR 53-60-01. (M)Nov 9, 2000 · N431US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA001919Channel · corrodedCLT - FOUND Z-CHANNEL CORRODED 1 INCH BY 2 INCH, LEFT AFT DOOR SILL. CORROSION LEVEL 1 C 53-107-02. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-02. (M)Nov 9, 2000 · N431US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA001909Seat Track · corrodedCLT - FOUND SEAT TRACK CORRODED .5 INCH BY .5 INCH BY .100 INCH DEEP, SEAT TRACK STATION 328-360, RBL 24. FABRICATED SEAT TRACK SECTION PER SRM 53-00-52 PAGE 202. (M)Nov 8, 2000 · N431US · Boeing 7374B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA001882Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 727D BETWEEN STRINGER 8 AND 9R. FABRICATED NEW FRAME DOUBLER PER TR 53-10-14. (M)Nov 7, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001883Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 3 INCHES, BL 0 STATION 312 CABIN FLOORBEAM LBL 18 - RBL 18. INSTALLED SPLICE ANGLES EPR SRM 52-10-51. (M)Nov 7, 2000 · N431US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA001884Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH BY 1 INCH, STATION 947 FROM LBL 12 THROUGH RBL 12 TOP SURFACE. INSTALLED NEW SECTION PER TR 53-60-02 REV A. (M)Nov 7, 2000 · N431US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA001885Floor Support · corrodedCLT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH, BETWEEN FLOORBEAM 947 AND 967 AT RBL 16. INSTALLED NEW PART PER SRM 51-10-2. (M)Nov 7, 2000 · N431US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA001872Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 747 BETWEEN STRINGER 8 AND 9L. DRILLED OUT DAMAGE AND FABRICATED DOUBLER PER TR 53-10-14. (M)Nov 3, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001875Floorbeam · corrodedCLT - FOUND FLOORBEAM 2 INCH BY 3 INCH, STATION 328, BL 0 CABIN FLOORBEAM. CORROSION LEVEL 1. INSTALLED NEW T-CAP PER SRM 53-10-51 FIG 205. (M)Nov 3, 2000 · N431US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA001873Frame · crackedCLT - FOUND FRAME CRACKED .75 INCH, BS 787, BETWEEN STRINGER 8 AND 9L. DRILLED OUT DAMAGE AND FABRICATED DOUBLER PER TR 53-10-14. (M)Nov 3, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001874Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH, BS 727F BETWEEN STRINGER 8 AND 9L. FABRICATED DOUBLER DRILLED OUT DAMAGE PER TR 53-10-14. (M)Nov 3, 2000 · N431US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001805Skin · crackedCLT - FOUND SKIN CRACKED 2.375 INCH, FUSE EXT SKIN STATION 727D, STRINGER 23R. INSTALLED DOUBLER PER TR 53-60-03. (M)Oct 24, 2000 · N434US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAASB00275Trim Motor · failedPHL - FLT 2295 - EN ROUTE FROM PHL-SJU, THE STABILIZER OUT OF TRIM LIGHTS ILLUMINATED ON BOTH AUTOPILOTS. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE AUTOPILOT STABILIZSep 25, 2000 · N785AU · Boeing 7374B7 · Autopilot Trim ServoSDR USAASB00271Regulator · defectiveCLT - FLT 1080 - EN ROUTE FROM TPA-PHL, 150 MILES SOUTH OF CAE AT FL370, AIRCRAFT BEGAN TO LOSE PRESSURIZATION AT A SLOW RATE. CREW COULD NOT CONTROL CABIN. THEY PERFORMED AN EMERGENCY DESCENT, AT SLOW RATE, FROM FL370 TO FL100. OXYGEN MASKS WERE DEPLOYED. Sep 24, 2000 · N437US · Boeing 7374B7 · Pneumatic Distribution SystemSDR USAA001512Frame · corrodedCLT - FOUND FRAME CORRODED 1 INCH, STATION 794 FORWARD SIDE UPPER LEG AND AFT SIDE. FABRICATED REPAIR ANGLE AND DOUBLER PER SRM 53-00-07 FIG 201. (M)Sep 12, 2000 · N427US · Boeing 7374B7 · Fuselage Main, Frame
Back to Boeing 737-4B7