N525AU, cancelled Nov 6, 2007

Service difficulty reports · 118

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N525AU' AND deregistration_id = 'N525AU-2007-11-06'
  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 USAA200703007Skin · crackedFOUND 3 INCH CRACK AT STA 767 STR 21L SKIN. REPAIRED PER SRM 53-00-01, REPAIR 31, TR 53-60-03A.Mar 27, 2007 · N525AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA20703006Skin · crackedA 1 INCH CRACK FOUND RT SIDE OF FUSELAGE, STA 767, STR 21R. REPAIRED AS PER BAC SRM 53-00-01 REPAIR 31.Mar 26, 2007 · N525AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB06120Lamp · burned outPIT FLT1904 - ON APPROACH TO PIT FROM CLT, DURING GEAR EXTENSION, CAPTAIN REPORTED HE DID NOT RECEIVE GREEN LIGHTS FOR ALL THREE OF THE GEAR. THE RIGHT MAIN LANDING GEAR INDICATION LIGHT WOULD NOT ILLUMINATE. CREW REQUESTED A FLY-BY THE ATC TOWER FOR VISUALNov 30, 2006 · N525AU · Boeing 7373B7 · Landing Gear Position and WarningSDR USAA061218Skin · crackedAT 2 INCHES FWD OF BS 727E AT S24R CRACK. INSTALLED REPAIR DOUBLER IAW EA 98168, DEFECT SIZE: 2 INCHES.Oct 16, 2006 · N525AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA051409Spar · crackedLBL 135.5, 12 INCHES FWD FROM REAR SPAR CRACKED. MAJOR REPAIR, REMOVED DAMAGE, INSTALLED REPAIR TEE, FILLERS, AND VERT STIFFENER IAW EA 97047. DEFECT SIZE: 1.5 INCH.Nov 22, 2005 · N525AU · Boeing 7373B7 · Wing SparSDR USAA051377Angle · corrodedLEFT TRANSITION ANGLE, STA 727D-807 CORRODED. FABRICATED NEW TRANS ANGLE AND INSTALLED IAW SRM 53-60-53, SRM 51-10-02. DEFECT SIZE: .500 INCH AREA CORROSION AT EACH FASTENER.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051378Floor Support · corrodedBS 500D BETWEEN 26L AND 26R CORRODED. REMOVED DAMAGED PART AND INSTALLED NEW ANGLE IAW SRM 53-30-53 AND SRM 53-00-53. DEFECT SIZE: CORROSION AREAS APPROXIMATELY 1 INCH IN DIAMETER.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051379Angle · corrodedTOP OF TRANSITION ANGLE BETWEEN STA 767 AND 787 CORRODED. REMOVED DAMAGED SECTION, FAB AND REPLACED WITH NEW SECTION IAW SRM 51-10-2 & BOEING DWG 65-47957. DEFECT SIZE: SPOTS OF CORROSION APPROXIMATELY .125 INCH IN DIAMETER.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051380Door Frame · crackedAFT CARGO DOOR FRAME AFT WEBBING CRACKED. FABRICATED AND INSTALLED NEW WEBBING IAW SRM 51-70-13. DEFECT SIZE: 1 INCH CRACK.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA051381Angle · corrodedRBL 13.80, STA 787-847 CORRODED. CUT OUT DAMAGED SECTION AND SPLICE IN NEW SECTION IAW SRM 53-00-53 FIG 201. DEFECT SIZE: 6 INCH CORROSION.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051382Shear Tie · corrodedSTA 727E BETWEEN STRINGER 27L TO 27R CORRODED. INSTALLED REPAIR PARTS PER SRM 53-00-07. DEFECT SIZE: 2 INCH LONG AREA OF CORROSION.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Internal Mounting StructureSDR USAA051383Support · corrodedSTA 294-312, LBL 12 CORRODED. REPLACE INTERCOSTAL MEMBER AND T-FITTING IAW SRM 51-10-02. DEFECT SIZE: INTERCOSTAL HAS A 70 INCH AREA OF CORROSION.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051384Angle · crackedBS 294; S-17R; ATTACHED TO OUTBOARD SIDE OF ZEE ANGLE CRACKED. PART REPLACED WITH IDENTICAL PART IAW SRM 51-10-02. DEFECT SIZE: 1.5 INCH CRACK IN A 4 INCH LONG ANGLE.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051385Angle · corrodedBS 300-353; ZEE ANGLE AT S-17L CORRODED. REPLACED WITH IDENTICAL PART, REMOVED CORRODED ZEE ANGLE WITH NEW IAW SRM 51-10-02 BOEING DWG 65-17688. DEFECT SIZE: APPROX 1 X 43 INCH CORRODED AREA.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051386Angle · corrodedTRANSITION ANGLE 727B THRU 727D CORRODED. FABRICATED AND INSTALLED REPAIR PART IAW SRM 53-60-53, DEFECT SIZE: 1 INCH CORROSION.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA051366Angle · corrodedFOUND CORROSION BS 300-353 ZEE ANGLE AT S-17L. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED CORRODED ZEE ANGLE IAW 65-17688, DEFECT SIZE: 1 BY 43 INCHES.Nov 11, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051365Angle · corrodedFOUND CORROSION ON R-1 DOOR THRESHOLD INNER CHORD ANGLE BS 296. REPAIR, DEFECTIVE PART REPLACED WITH IDENTICAL PARTY IAW SRM 51-10-02, DEFECT SIZE: 2" BY 5".Nov 11, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051364Web · crackedFOUND CRACK FUSELAGE STATION 353 STRINGER 16 LEFT. REPAIR, CUT WEB TO REMOVE DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-04, EA 97004 DEFECT SIZE: 2.1".Nov 11, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051363Intercostal · crackedSTA 344, STA 360, BL0 MAJOR REPAIR, FABRICATED NEW REPAIR PARTS IAW SRM 51-70-11, DEFECT SIZE: .250".Nov 10, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051362Frame · damagedFOUND HOLE IN FRAME STA 380, S15L. ENLARGED HOLE TO .125 AND INSTALLED RIVET IAW EA 97066, DEFECT SIZE: .100".Nov 10, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA051355Attach Angle · crackedFOUND STR 25L AND FRAME AT BS 380 CRACKED. FABRICATED AND INSTALLED NEW ANGLE BOEING DWG 69-38780 AND SRM 53-00-01, DEFECT SIZE: 1".Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051354Floorbeam · corrodedFOUND STA 344, LBL42-RBL31; AROUND CLIP NUT HOLES IN FLOOR BEAM CORRODED. REMOVED CORRODED OUT OF LIMITS SECTION OF "T" CAP FROM LBL31 TO RBL31 IAW SRM 53-10-51, FIG 201, DEFECT SIZE: 1" BY 1".Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA051356Floorbeam · crackedFOUND BS28/LBL27 CRACKED. FABRICATED AND INSTALLED STIFFENER IAW SRM 51-10-02, DEFECT SIZE: 1".Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA051357Stringer Clip · crackedCRACK FOUND STATION 343 AT STRINGER 11R. STRINGER TIE CLIP WAS FABRICATED IAW BOEING DRAWING 69-38939-5, DEFECT SIZE: .025.Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051359Floorbeam · corrodedFOUND STA 344, LBL 42-RBL3, AROUND CLIP NUT HOLES IN FLOORBEAM. REMOVED AND REPLACED T-CAP FROM LBL 1 TO RBL 32 IAW SRM 53-10-51, FIG 201, DEFECT SIZE: 1" BY 1".Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA051360Intercostal · crackedFOUND CRACK BS312 BL0 CABIN FLOOR SUPPORT STRUCTURE. CUTOUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 51-70-11, DEFECT SIZE: .25".Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051361Stiffener · crackedFOUND STA 328 LBL45 FWD ENTRY FLOOR SUPPORT STRUCTURE CRACKED. REPAIR, FABRICATED NEW L-ANGLE AND INSTALLED IAW SRM 51-10-02 BOEING DWR 65-45812 DEFECT SIZE: .250"Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051358Floorbeam · corrodedFOUND CORROSION BS 328 AT RBL 15 AND 12. FABRICATED SPLICE ANGLES AND INSTALLED SPLICE ANGLES AND "T" CAP IAW SRM 53-10-51, DEFECT SIZE: 7" BY.65".Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA051352Angle · crackedFOUND STA 350 AT STRINGER 16L CRACKED. REMOVED, FAB, HEAT TREATED AND INST NEW ANGLE IAW SRM 51-10-02, DWG 69-26555 JOB CARD J020-37-20, DEFECT SIZE: .250" CRACK.Nov 8, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051351Channel · crackedFOUND BS 360; S15L CRACKED. REMOVED CRACKED CHANNEL AND INSTALLED NEW CHANNEL IAW SRM 51-10-02, DEFECT SIZE: APPROX 1" CRACK.Nov 8, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR 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 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 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, Structure
Back to N525AU, cancelled Nov 6, 2007