N522AU, cancelled Feb 12, 2008

Service difficulty reports · 65

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 = 'N522AU' AND deregistration_id = 'N522AU-2008-02-12'
  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 USAA061429Door Frame · crackedBS 492 FRAME AT LOWEST DOOR STOP CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND REPAIR ANGLES IAW EA 98327, DEFECT SIZE: .125 INCH.Dec 15, 2006 · N522AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA061430Frame · crackedBS 847 FRAME AT LOWER DOOR STOP MOUNT BOLT HOLE NEAR S-24R CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND REPAIR ANGLES IAW EA 98328, DEFECT SIZE: .125 INCH.Dec 15, 2006 · N522AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA200608001Skin · crackedTWO CRACKS FOUND, 2.5 INCH AND 3 INCH. THE 2.5 INCH CRACK AT 727E S24R, 3 INCH CRACK AT 727E + 5 INCH S25R ON FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-00-01 REPAIR 31.Aug 21, 2006 · N522AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR SB05165Battery Pack · dischargedBDL - SEVERAL CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE LEFT EMERGENCY LIGHT BATTERY PACK. OPERATIONALLY CHECKS OK.Dec 12, 2005 · N522AU · Boeing 7373B7 · Emergency LightingSDR SB05159Sensor · out of adjustBOS - FLT203, AFTER TAKEOFF FROM BOS, CREW COULD NOT RETRACT THE LANDING GEAR. THE GEAR HANDLE WOULD NOT MOVE UP PAST THE OFF POSITION. FLIGHT RETURNED TO THE FIELD AT BOS AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANDec 1, 2005 · N522AU · Boeing 7373B7 · Landing Gear Position and WarningSDR SB05128Actuator · faultyPHL - FLT1243 - ON APPROACH TO PHL, WHEN AUTO PILOT WAS MANUALLY DISCONNECTED AT 1,000 FT AGL, THE AIRCRAFT ROLLED TO THE LEFT. AILERON TRIM SYSTEM WAS FOUND TO BE INTERMITTENT. BOTH THE CAPTAIN AND FIRST OFFICER WERE REQUIRED TO REGAIN LEVEL FLIGHT. CREW NOct 8, 2005 · N522AU · Boeing 7373B7 · Aileron Control SystemSDR USAA200506002Skin · crackedA 2.625 INCH CRACK IN FUSELAGE SKIN AT STR 3L, STA 727D. INSTALLED DOUBLER PER EA 81022.Jun 13, 2005 · N522AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050085Threshold · corrodedPIT - Q3 - WEB PLATE, .2500 INCH AROUND, CORROSION; LEVEL 1; TASK NR C53-202-01; AFT CARGO DOOR THRESHOLD AROUND NUT PLATE HOLES. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG 65-47957 AND SRM 51-40-03. (K)Jan 19, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050083Stringer · crackedPIT - FOUND STRINGER CRACKED .3750 INCH AT S-8 UPPER STRINGER AT WBL 355 AT ATTACH BOLT ON, RT WING. INSTALLED REPAIR ANGLES PER EA 79684. (M)Jan 5, 2005 · N522AU · Boeing 7373B7 · Wing, Longeron/StringerSDR USAA050071Skin · tornPIT - FOUND SKIN WITH .5 INCH TEAR, STATION 1025 LBBL 33. PART REPLACED PR JOB CARD J3-58-53500-C-010. (M)Jan 4, 2005 · N522AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050078Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .5 INCH, AT KEEL BEAM BETWEEN STATION 500 AND 520 IN DISTRIBUTION BAY. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-40-02. (M)Jan 3, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050079Stringer · crackedPIT - FOUND STRINGER CRACKED .5 INCH, RT WING WBL 479 AT S-8. REPAIR ANGLES PER EA 79684. (M)Jan 2, 2005 · N522AU · Boeing 7373B7 · Wing, Longeron/StringerSDR USAA050080Stringer · crackedPIT - FOUND STRINGER CRACKED .5 INCH, RT WING WBL 355 AT S-8. REPAIR ANGLES PER EA 79684. (M)Jan 2, 2005 · N522AU · Boeing 7373B7 · Wing, Longeron/StringerSDR USAA050077Stringer · crackedPIT - FOUND UPPER STRINGER 2 INCH CRACK, WBL 505 RT WING. INSTALLED REPAIR ANGLES WITH MINOR DEVIATION PER EA 79684 AND SRM 57-00-03. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Wing, Longeron/StringerSDR USAA050075Stiffener · crackedPIT - FOUND STIFFENER CRACKED .75 INCH, MAIN LANDING GEAR WHEEL WELL BS 663.75 AT LBL 6.15. REPLACED STIFFENER PER EA 75002 AND BOEING DWG 65-45402. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050076Support Bracket · crackedPIT - FOUND ANTENNA CHANNEL, SUPPORT BRACKETS WITH THREE .5 INCH CRACKS, BETWEEN STATION 500/500A, STRINGER 28L-28R, VHF-2 ANTENNA CHANNEL. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050074Crease Beam · crackedPIT - FOUND CREASE BEAM CRACKED 2.5 INCHES, AFT OF FRAME 616 RT SIDE CREASE BEAM. MODIFIED PART INSTALLED PER TYPICAL REPAIR 53-10-02 REV A. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050170Skin · bentPIT - FOUND SLAT EXT SKIN BENT AREA 3.5 INCH BY 1.5 INCH AREA, NR 1 SLAT UPPER T/E SURFACE INBOARD END. REMOVED DAMAGED AREA, INSTALLED FILLER AND INTERNAL DOUBLER PER SRM 51-70-10. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050082Web · crackedPIT - FOUND WEB CRACKED 1.25 INCH, STATION 927-947.5 INTERCOSTAL CRACKED 1.25 INCH FROM FORWARD CORNER. INSTALLED SAME PART PER DWG 69-36656. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040081AFlange · crackedFOUND FLANGE CRACKED .5 INCH,PANEL 582-8R OPENING IN RT PYLON. STOP DRILLED THE CRACK, INSTALLED DOUBLER PER TYPICAL REPAIR 54-30-07. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Structure (General)SDR USAA050053Skin · crackedPIT - FOUND NR 1 SLAT WITH .125 INCH CRACKS ON 6 RIVET HOLES, CENTER OF SLAT BY ACTUATOR MOUNT LOWER SKIN. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050050Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .25 INCH, INTERCOSTAL AT BL0 BETWEEN STATION 344 AND 360. INSTALLED DOUBLER, STOP DRILLED PER SRM 51-70-11. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050073Beam · crackedPIT - FOUND BEAM CRACKED .75 INCH, STATION 616 BELOW RT SIDE CREASE BEAM. ROUTED OUT CRACK, INSTALLED FILLER AND REPAIR ANGLE PER TYPICAL REP 53-62-01. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050072Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .125 INCH, FORWARD END INTERCOSTAL FASTENER BS 328 LBBL 44. REPLACED INTERCOSTAL PER SRM 53-10-51. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050068Panel · delaminatedPIT - FOUND PANEL DELAMINATED, INBOARD AND OUTBOARD ENDS OF NR 5 SLAT PANEL. INSTALLED DOUBLER PER SRM 51-70-10. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050066Angle · brokenPIT - FOUND ANGLES BROKEN, RAM AIR INLET DUCT UPPER SUPPORT LEFT SIDE. DEFECTIVE PART REPLACED WITH IDNT PART PER TYPICAL REPAIR 21-50-07C. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050056Attach Fitting · crackedPIT - FOUND ATTACH CLIP CRACKED .125 INCH, STRINGER TO FRAME ATTACH CLIP AT BS 706, S-11L. DEFECTIVE PART REPLACED WITH IDENT PART PER BOEING DWG 66-23574. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050055Door Frame · crackedPIT - FOUND FORWARD ENTRY DOOR CRACKED .125 INCH, DOOR FRAME NR 6 DOOR STOP AFT SIDE. CUT OUT DAMAGE, INSTALLED DOUBLER PER TYPICAL REP 52-10-16. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Passenger/Crew DoorsSDR USAA050052Skin · chafedPIT - FOUND FLAP SKIN LEADING EDGE WITH CHAFE MARK .020 BY 4.25 INCH LONG BY .5 INCH WIDE, RT OUTBOARD MID FLAP ADJACENT TO OUTBOARD FLAP TRACK. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Trailing Edge FlapsSDR USAA050051Skin · crackedPIT - FOUND NR 3 SLAT CRACKED .125 INCH, LOWER SURFACE AT MID SPAN RIVET HOLE. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050048Stringer · crackedPIT - FOUND STRINGER CRACKED .125 INCH, FRAME 380 AT S16R. REPAIR FILLER AND FABRICATED SHEAR TIE PR SRM 53-00-07. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA050067Frame · brokenPIT - FOUND FRAME BROKEN OUT EDGES, DOOR FRAME STATION 492 AT STATION 27R, LOWER AFT CORNER OF CARGO DOOR FRAME. FABRICATED DOUBLER PER SRM 51-70-13. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA050057Beam · crackedPIT - FOUND BEAM CRACKED 1 INCH, FORWARD OF FRAME 639 RIGHT SIDE CREASE BEAM. MODIFIED PART C/C 1109171 AND INSTALLED PER TYPICAL REPAIR 53-10-02 REV A. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050054Angle · crackedPIT - FOUND ANGLE CRACKED .25 INCH LONG, EDGE OF SUPPORT ANGLE AT FS 294.5, FORWARD LOWER CORNER AT FLOOR LINE. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-40-02. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050070Skin · chafedPIT - FOUND SKIN CHAFED, .023 INCH DEEP, SKIN STATION 860-880 AT DORSAL FIN. INSTALLED DOUBLER, TRIPLER AND BONDED STAINLESS RUB STRIP PER SRM 53-60-01 FIG 209. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050065Clip · brokenPIT - FOUND BROKEN FRAME CLIP, STATION 597 STRINGER 8R. REMOVED AND REPLACED FRAME CLIP PER SRM 51-40-00. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050049Frame · crackedPIT - FOUND RIVET CRACKED .125 INCH, FRAME 360, RIVET AT S9L. INSTALLATION OF TWO, REPAIR ANGLES PER TYP REP 53-10-20A. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA050069Skin · delaminatedPIT - FOUND SLAT DELAMINATED 4 INCHES BY 6 INCHES, NR 3 SLAT. REMOVED TOP SKIN CORE AND DAMAGE, INSTALLED FILLER, DOUBLER PER SRM 51-70-09. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050089Floor Support · corrodedPIT - Q3 - FLOOR SUPPORT, 1 INCH X 2 INCH AT 3 AREAS; CORROSION; LEVEL 1; TASK NR C53-107-02, STA 947.5-966 RBBL. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-00.Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050088Intercostal · corrodedPIT - Q3 - INTERCOSTAL, 1 INCH DIA (4 EA AREAS) CORROSION ; LEVEL 1; TASK NR C53-107-01, RBBL 10 BS 312 TO 328. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02. (K)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050087Angle · corrodedPIT - Q3 - ANGLE, 1 INCH DIA. SPOT; EXFOLIATED CORROSION; BS 530, RT AT KEELBEAM, S-27R. KEELBEAM SECTION, -2 DOUBLER, -1 STRAP IAW TYP. REP. 53-60-09.Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050086Floorbeam · corrodedFLOORBEAM, 1INCH X 1 INCH AREA (2 EA) CORROSION; LEVEL 1; TASK NR C53-107-01, STA 328 FROM RBBL TO IB SEAT TRACK. REMOVED CORRODED SECTION, FABRICATED NEW AND INSTALLED IAW 53-10-51. (K)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050084Threshold · corrodedPIT - Q3 - WEB PLATE, .2500 INCH AROUND, CORROSION; LEVEL 1; TASK NR C53-20201, AFT CARGO DOOR THRESHOLD; CORROSION AROUND NUT PLATE HOLES. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG NR 65-47957. (K)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USA2004F00093Circuit Breaker · trippedON APPROACH, CREW DID NOT RECEIVE ANY LANDING GEAR INDICATION LIGHTS AFTER GEAR EXTENSION. A MISSED APPROACH WAS EXECUTED. CREW TESTED THE LIGHTS BUT HAD NO ILLUMINATION OF THE GEAR LIGHTS. BULBS CHECKED OK ALONG WITH CIRCUIT BREAKERS. MAINTENANCE FOUND THJun 26, 2004 · N522AU · Boeing 7373B7 · Landing Gear SystemSDR USAA040029Frame · corrodedPIT - FOUND FRAME CORRODED 6 INCHES BY 4 INCHES, BLO '0' AT Y FRAME STATION 1016 AT 6 O'CLOCK. Y FRAME LOWER LEGS AND WEB SKIN DOUBELR EPR EO 5302V112 AND SRM 51-20-01. (M)Feb 28, 2004 · N522AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAASB03218Outflow Valve · failedEN ROUTE FROM PIT TO IND, AT FL200, THE CABIN ALTITUDE WARNING HORN SOUNDED WITH NO AUTO FAIL LIGHT. CREW DESCENDED FLIGHT TO 12,000 FEET AND USED MANUAL AC TO CLOSE OUTFLOW VALVE BUT COULD NOT OPEN IT. CREW HAD TO USE MANUAL DC TO OPEN OUTFLOW VALVE. FLIGHDec 19, 2003 · N522AU · Boeing 7373B7 · Pressure Regulator/Outflow ValveSDR USAASB03117Video Monitor · odorCLT - FLT 1009 - AFTER TAKEOFF FROM CLT, AT APPROXIMATELY 7,000 FEET, THE FLIGHT ATTENDANT REPORTED TO THE FLIGHT CREW A STRONG ELECTRICAL ODOR IN THE MID AND AFT CABIN. NO SMOKE WAS NOTED. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIEDL AT CLT. FLIGHTJul 20, 2003 · N522AU · Boeing 7373B7 · Entertainment SystemSDR USAA020387Angle · crackedPIT - FOUND VERTICAL Z-ANGLE CRACKED IN HALF, CENTER OF ANGLE FORWARD BULKHEAD LEFT OF W/W STATION 663 LBBL 6.15. INSTALLED TEMP SUPPORT ANGLE AND STRAPS EPR EA 75002. (M)Oct 4, 2002 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAASB02142Wire · brokenSYR - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTS AT SEAT ROWS 8, 9 AND 10L LEFT SIDE, INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONAL CHECK OF EVACUATION LIGHTS GOOD. (M)Jul 26, 2002 · N522AU · Boeing 7373B7 · Light System WiringSDR USAA020132Stringer · damagedTPA - FOUND STRINGER HAS DEFECTIVE FASTENER HOLES, FS 616, S3L STRINGER TIE CLIP. REMOVED TEMP REPAIR, SPLICED IN NEW SECTION OF STRINGER PER SRM 53-00-03 FIG 203. (M)Mar 25, 2002 · N522AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
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