Boeing 737-3B7

Service difficulty reports · 4,722

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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 = '7373B7'
  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 USAA051339Skin · damagedLEFT RUDDER SKIN 96 INCHES FROM THE BASE AND 11 INCHES FROM THE TRAILING EDGE DAMAGED. REMOVED DAMAGED, LAID UP AND INSTALLED REPAIR IAW SRM 55-40-01. DEFECT SIZE: 1.5 INCH.Nov 7, 2005 · N525AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA051340Skin · delaminatedLEFT RUDDER SKIN 99 INCHES FROM THE BASE AND 19 INCHES IN FROM THE TRAILING EDGE DELAMINATED. REMOVED DAMAGE, LAID UP AND INSTALLED REPAIR IAW SRM 55-40-01. DEFECT SIZE: 6 INCHES.Nov 7, 2005 · N525AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA051341Skin · gougedWEDGE SKIN 13.5 INCH FROM THE OUTBOARD END GOUGED. REMOVED SKIN AND DAMAGED CORE, INSTALLED CORE, FILLER AND DOUBLER IAW SRM 57-50-15 REV A. DEFECT SIZE: 4.3 X .5 INCH.Nov 7, 2005 · N525AU · Boeing 7373B7 · Trailing Edge FlapsSDR USAA051342Floorbeam · corrodedBS 312, WL 208, LBL 16 TO RBL 16 LEVEL 1 CORROSION. SPLICED IN REPLACEMENT EXTRUSION IAW SRM 53-10-51 FIG 201. DEFECT SIZE: .50 X .50 INCH.Nov 7, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR SB05144Ballast · overheatedJAX FLT1067 DURING CRUISE, EN ROUTE FROM CLT TO MIA AT FL340, FLIGHT ATTENDANTS NOTICED SMOKE COMING FROM THE AFT LEFT LAVATORY. FLIGHT ATTENDANT EMPTIED PORTABLE HALON FIRE EXTINGUISHER INTO THE AREA. NO SMOKE ALARM SOUNDED. CREW DECLARED AN EMERGENCY Nov 6, 2005 · N384US · Boeing 7373B7 · Passenger Compartment LightingSDR USAA051333Tie Clip · crackedFUSELAGE STATION 277 STRINGER 10R. REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-10-02. DEFECT SIZE: .075 INCH.Nov 4, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051334Frame · crackedBETWEEN STRINGERS S-8R AND S-9R STA 480. CUT OUT DAMAGE, INSTALL FRAME DOUBLERS IAW TR 53-10-20. DEFECT SIZE: .5 INCH.Nov 4, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA051326Skin · crackedIN LOWER SKIN OF NR 5 SLAT AT RIVET, ADJACENT TO SLAT ACTUATOR ATTACH. A 30.25 X 3.75 INCH REPAIR DOUBLER ON LOWER SKIN AT CTR OF SLAT ADJ TO ACTUATOR ATTACH IAW SRM 57-43-01. DEFECT SIZE: .250 INCH LONG CRACK AT RIVET.Nov 3, 2005 · N525AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA051327Skin · crackedFLOOR SKIN, STA 665, LBL 30. REMOVED DAMAGE, INSTALL FILLER DOUBLER & STIFFENER IAW TYPE REPAIR 53-60-04. DEFECT SIZE: .500 INCH CRACK.Nov 3, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA051331Skin · crackedLOWER SKIN T/E CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-43-01 FIG 201, DEFECT SIZE: 6 INCH CRACK.Nov 3, 2005 · N525AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA051332Trim Tab · delaminatedOUTBOARD T/E CORNER DELAMINATED. ROUTED TO COMPOSITE FOR REPAIR IAW SRM 51-70-06 REPAIR NR 6 DEFECT SIZE: 3 INCHES DELAM.Nov 3, 2005 · N525AU · Boeing 7373B7 · Aileron TabsSDR USAA200511003Skin · crackedA 2.5 INCH CRACK FOUND IN FUSELAGE SKIN. INSTALLED EXT SKIN DOUBLER PER SRM 53-00-01 FIG 2.Nov 2, 2005 · N396US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA051319Bracket · crackedLOWER FWD CORNER OF MAIN ENTRY DOOR. FABRICATED AND INSTALLED NEW BRACKET IAW SRM 51-10-02. DEFECT SIZE: .50 INCH.Nov 2, 2005 · N525AU · Boeing 7373B7 · Passenger/Crew DoorsSDR USAA051320Angle · damagedFOUND VERT STAB TRANSITION ANGLE LEFT SIDE AFT OF REAR ATTACH POINT. FABRICATED AND INSTALLED NEW ANGLE IAW TR 53-20-05A, DEFECT SIZE: 12".Nov 2, 2005 · N525AU · Boeing 7373B7 · Vertical StabilizerSDR USAA051321Stringer · crackedS-5AR B.S. 1138 ACTION: INTERIM REPAIR WAS PREVIOUSLY INSTALLED IAW EA 73450B IAW EA 73450B. LENGTH UNKNOWN.Nov 2, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA051289Angle · corrodedFOUND Z-ANGLE CORRODED, STA 955 TO 990 . REMOVED CORRODED PART AND INSTALLED NEW PART AND REPAIR PARTS IAW SRM 53-60-15, DEFECT SIZE: CORROSION ON "Z" ANGLE 1 INCH BY 1 INCH.Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051291Floorbeam · corrodedFOUND FLOORBEAM CORRODED STA 986.5 AT LT DOOR SILL AREA. REPLACED ENTIRE T-CAP IAW TR 53-10-05B, DEFECT SIZE: .500" AREA OF CORROSION AROUND SEVERAL SCREW HOLES.Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA051292Angle · corrodedFOUND CORROSION STA 955 TO 990, LBL 53. REMOVED DAMAGED PARTS AND INSTALLED NEW PARTS IAW SRM 51-10-02, DEFECT SIZE: NUMEROUS AREAS OF CORROSION THROUGHOUT THE PART/TYPICAL 1/2" DIA OF CORROSION.Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051293Angle · corrodedFOUND Z-ANGLE CORRODED, FLOOR STRUCTURE AT L2 DOOR, STA 986 AND LBL 53. REMOVED CORRODED PART AND INSTALLED NEW PART IAW SRM 51-10-02, DEFECT SIZE: 1" BY 3" AREA OF CORROSION.Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051294Skin · debondedFOUND DISBOND O/B END OF T/E WEDGE. REMOVED DAMAGE, FAB AND INSTALLED REPAIR PARTS IAW TR 51-30-03, DEFECT SIZE: 2" BY 5" DISBOND.Nov 1, 2005 · N525AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA051295Skin · debondedFOUND SLAT DISBOND, T/E WEDGE O/B END. REMOVED DAMAGE, FAB AND INSTALLED REPAIR PARTS IAW TR 57-42-04, DEFECT SIZE: 3" X 5" DISBOND.Nov 1, 2005 · N525AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA051296Crease Beam · corrodedAROUND RIVET HEADS AT CREASE BEAM BS 500B+8 S17L. REMOVED CORROSION AND TREATED AREA IAW SRM 51-20-01, DEFECT SIZE: APPROXIMATE 1/16" DIA SPOTS OF CORROSION.Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA051297Support · crackedFOUND CRACK VERTICAL STANCHION SUPPORT AT FWD E1 RT SHELF. FABRICATED AND INSTALLED DOUBLER IAW SRM 51-70-11, DEFECT SIZE: 1" CRACK.Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051287Floorbeam · corrodedFOUND FLOORBEAM SHIM FAULTY AT STA 986. CLEANED AREA, REMOVED CORRODED SHIMS AND RETREATED AREA IAW SRM 53-60-51, DEFECT SIZE: APPROX .250" DAMAGE.Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA051286Stringer · crackedFOUND STRINGER SPLICE CORRODED, STA 907, S4L. REMOVED AND REPLACE WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: .250" CRACKS AT TWO RIVET HOLES.Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA051285Floorbeam · corrodedFOUND FLOORBEAM CORRODED STA 986.5. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 53-60-51, DEFECT SIZE: 1/4" AREA'S OF CORROSION.Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA051288Stringer · corrodedFOUND STRINGER CORRODED, S26R, STA 1016. REPLACED STRINGER SECTION AND BULKHEAD FITTING IAW SRM 51-10-02, DEFECT SIZE: .75" BY 3" STRINGER HAS A CORRODED AREA.Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA051266Frame · crackedFOUND FRAME CRACKED, STA 480 S-9L ON FRAME AT PSU RAIL. CUT OUT DAMAGE. INSTALL REPAIR DOUBLERS IAW TR 53-10-20, DEFECT SIZE: .25".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA200511002Skin · cracked2.5 INCH CRACK FOUND AT STA 727E AT STRINGER 23L. REPAIR: INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG. 201.Oct 31, 2005 · N396US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA200511001Skin · cracked1.5 INCH CRACK FOUND STA 867 AT STRINGER S23R. REPAIR: INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG. 201.Oct 31, 2005 · N396US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA051261Intercostal · corrodedFOUND INTERCOSTAL AT BS 312-328 LBL 12. REPLACED STIFFENER IAW BOEING DWG 65-45834, DEFECT SIZE: 2" BY 2".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051262Fitting · corrodedFOUND FITTING CORRODED GIRT BAR ATTACH FITTING AT BS344 RBL 58. REMOVED AND REPLACED ANGLE IAW BOEING DWG 65C16121, DEFECT SIZE: 1".Oct 31, 2005 · N525AU · Boeing 7373B7 · Escape SlideSDR USAA051263Seat Track · corrodedFOUND SEAT TRACK CORRODED, LBL 45 BS 500A + 12. BLENDED AREA, WITHIN LIMITS IAW SRM 53-00-52, DEFECT SIZE: 1" BY 2".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA051264Seat Track · corrodedFOUND SEAT TRACK CORRODED, LBL 45 BS 494. BLENDED WITHIN LIMITS IAW SRM 53-00-52, DEFECT SIZE: 1" BY 2".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA051265Web · crackedFOUND WEB CRACKED AT STR 16 STA 294.5. FABRICATED WEB AND INSTALLED IAW SRM 53-10-15 AND 51-10-02, DEFECT SIZE: .50".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051267Lug · gougedFOUND LUG GOUGE OB FWD FACE OF LT MLG BEAM. BLEND OUT DAMAGE IAW TYP REP 57-40-05 BOEING DWG 65-82763, DEFECT SIZE: .750 BY .008.Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage, Landing Gear Attach FittingsSDR USAA051268Stringer · corrodedFOUND STRINGER CORRODED, S26R, STA 1016. REPLACED STRINGER SECTION AND BLKHD FITTING IAW SRM 51-10-02, DEFECT SIZE: .75" BY 3".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA051269Shim · corrodedFOUND FLOORBEAM SHIM CORRODED AT STA 986. CLEANED AREA, REMOVED CORRODED SHIMS AND RETREATED AREA IAW SRM 53-60-51, DEFECT SIZE: .250".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA051275Clip · crackedFOUND CLIP CRACKED, STA 685 S4L. REPLACED CLIP IAW SRM 51-10-02, 51-40-03, DEFECT SIZE: 2.00".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051276Frame · crackedFOUND FRAME CRACKED BETWEEN STRINGERS S-8R AND S-9R STA 480. CUT OUT DAMAGE, INSTALL FRAME DOUBLERS P/N 1133533 AND 1133534 PER TR 53-10-20, DEFECT SIZE: .5".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA051277Web · crackedFOUND WEB CRACKED, STA 294.5, S12L. REMOVED DAMAGED PART, REPLACED W/FABRICATED REPLACEMENT WEB/INTERCOSTAL, DEFECT SIZE: .500".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051278Splice · crackedFOUND SPLICE CHANNEL CRACKED, STA 360 S14L. REPLACED SPLICE PART IAW SRM 51-10-02, DEFECT SIZE: .500".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051281Stringer Clip · crackedFOUND TIE CLIP CRACKED, STA68, S10R. REPLACED WITH NEW CLIP IAW SRM 51-10-02, 51-40-03, DEFECT SIZE: .250".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051282Mount · corrodedFOUND LAV MOUNTS CORRODED, RT AFT LAV/FWD MOUNTS. REMOVED CORRODED PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-60-51, DEFECT SIZE: 2".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051283Mount · corrodedFOUND LAV MOUNTS CORRODED, STA. 986.5 AND 1016. REMOVED CORRODED PARTS AND INSTALLED REPAIR PIECES IAW SRM 51-10-02, DEFECT SIZE: 1" BY 3".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051284Support · corrodedFOUND LT MLG SUPPORT FITTING BOTTOM SURFACE CORRODED. BLENDED AREAS AS REQUIRED IAW TR 57-53-53A, DEFECT SIZE: .25".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage, Landing Gear Attach FittingsSDR USAA051271Splice · crackedFOUND STRINGER SPLICE CRACKED, STA 907 S4L. REMOVED AND REPLACED W/NEW PART IAW 51-10-02, DEFECT SIZE: .250".Oct 31, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR SB05141Charger · inoperativeCLT - MAINTENANCE REPORTED THE AFT CABIN SEAT/AISLE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY CHARGER AND BATTERY. OPERATIONAL CHECK GOOD.Oct 30, 2005 · N395US · Boeing 7373B7 · Emergency LightingSDR USAA051258Strap · crackedFOUND STABILIZER AT BS 344 AND RBL 47. INSTALLED DOUBLER IAW SRM 53-10-51, DEFECT SIZE: .50".Oct 28, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051260Stiffener · corrodedFOUND STIFFENER CORRODED, BS 328-344 LBL 12. REMOVED CORROSION AND TREATED IAW SRM 51-10-02, DEFECT SIZE: .25".Oct 28, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
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