N515AU, cancelled Feb 14, 2008

Service difficulty reports · 26

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 = 'N515AU' AND deregistration_id = 'N515AU-2008-02-14'
  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 SB07083Battery Pack · dischargedBFM - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGNS AT THE LEFT-HAND AND RIGHT-HAND FORWARD DOORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK PER MM 33-51-51. OPERATIONAL CHECK GOOD.Sep 26, 2007 · N515AU · Boeing 7373B7 · Emergency LightingSDR USAA200705U04Skin · crackedAPPROX 15.5 INCH CRACK IN FUSELAGE RUNS LONGITUDINAL, LOCATED BETWEEN STA 482 & 500, BETWEEN STR 28L & 28R. INSTALLED DOUBLER REPAIR & INSTALLED NEW ANTENNA SUPPORT KIT PER EA 84528.May 8, 2007 · N515AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR SB06103Windshield · crackedORD FLT 1623 DURING CRUISE AT FL340, EN ROUTE FROM CLT TO MSP, THE CAPTAIN'S L1 WINDSHIELD OUTER PANE CRACKED. PRESSURIZATION HELD OK. WINDOW HEAT WAS TURNED OFF AND NO FURTHER CRACKING WAS NOTED. FLIGHT DIVERTED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. Oct 21, 2006 · N515AU · Boeing 7373B7 · Flight Compartment WindowsSDR USAA200608002Skin · crackedA 2.5 INCH CRACK FOUND ON FUSELAGE SKIN STA 727E AT STR 25R. INSTALLED TRIPLER PER SRM 53-00-01 PROCEDURES II & V.Aug 24, 2006 · N515AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA200607001Skin · crackedA 2 INCH LONG CRACK AT STA 727 S-24R. CUT OUT DAMAGE, ACCOMPLISHED HF/EC AND INSTALLED DOUBLER WITH SHIMS FOR FILLET FAIRING PER SRM 53-00-01 FIG 201, DETAIL XI AND EA 82696.Jun 9, 2006 · N515AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR SB06038Sign · inoperativePIT - THE LEFT EMERGENCY EXIT LOW LEVEL SIGN WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.Apr 20, 2006 · N515AU · Boeing 7373B7 · Emergency LightingSDR SB05106Battery Pack · dischargedCLT - MAINTENANCE REPORTED THE FORWARD RIGHT EMERGENCY LIGHT AT THE SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.Sep 1, 2005 · N515AU · Boeing 7373B7 · Emergency LightingSDR SB05064Light · inoperativeMAINTENANCE FOUND THE INTERIOR EMERGENCY EXIT LIGHT ASSEMBLY, FORWARD OF THE FORWARD SERVICE DOOR, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.May 26, 2005 · N515AU · Boeing 7373B7 · Emergency LightingSDR USAA040976Support Angle · crackedPIT - C5 - SUPPORT ANGLE, 1 INCH LONG CRACK AT STA 540 S - 22L. SPLICE ANGLE IAW TYP REP 53-50-03.Nov 16, 2004 · N515AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040709Skin Panel · crackedUNSCHEDULED MAINTENANCE, KEEL BEAM SKIN PANEL, 3 INCH CRACK, BS 690 KEEL BEAM PANEL. INSTALLED DOUBLER (TEMP REPAIR) IAW SRM 53-60-12, FIG 202.Sep 14, 2004 · N515AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB04090Sensor · malfunctionedPIT - FLT 1058 - AFTER TAKEOFF FROM PIT, EN ROUTE TO PVD, CREW REPORTED THE NR 4 LEADING EDGE FLAP WOULD NOT RETRACT AND THE LEADING EDGE FLAP TRANSIT AMBER LIGHT WAS ILLUMINATED. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGEJul 12, 2004 · N515AU · Boeing 7373B7 · Leading Edge Slat Position Indicating SystemSDR USAA040006Keelbeam · chafedPIT - FOUND KEELBEAM CHAFFING 16 INCH AREA, STATION 727 FORWARD TO 711 RT OUTBOARD FLANGE OF LT KEELBEAM BY FAIRING AND ATTACH FAST. INSTALLED DOUBLERS, STRAP AND NUT PLATES PER TYPICAL REPAIR 53-60-05 AND EA 77518. (M)Jan 12, 2004 · N515AU · Boeing 7373B7 · Fuselage Main, KeelSDR USAA040005Keelbeam · chafedPIT - FOUND KEEL BEAM CHAFING 16 INCH AREA, STATION 727 FORWARD TO 711 LEFT OUTBOARD FLANGE OF LT KEEL BEAM BY FASTENERS AND PANELS. INSTALLED DOUBLERS, STRAPS AND NUTPLATES PER TYPICAL REPAIR EA 77719, T/R 53-60-05. (M)Jan 1, 2004 · N515AU · Boeing 7373B7 · Fuselage Main, KeelSDR USAA030321Door Frame · crackedPIT - FOUND DOOR FRAME SKIN CRACKED .5 INCH LONG, FORWARD SERVICE DOOR FRAME CRACK AT DOOR STOP NR 4. DOUBLER INSTALLED AT DOOR STOP NR 4 PER TR 52-10-11. (M)Dec 30, 2003 · N515AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA030320Door Frame · crackedPIT - FOUND DOOR FRAME CRACKED 1 INCH, LOWER AFT FORWARD SERVICE DOOR CORNERS. INSTALLED DOUBLER PER EA 77600. (M)Dec 29, 2003 · N515AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAASB03125Socket · shortedCLT - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 12 INOPERATIVE. MAINTENANCE FOUND THE LIGHT SOCKET SHORTED. REMOVED AND REPLACED LIGHT SOCKET AT SEAT ROW 12 AND REPLACED BATTERY PACK, P/N 2013-1A, AS PRECAUTIONARY. OPERATIONAL CHECK GOOD. (M)Aug 1, 2003 · N515AU · Boeing 7373B7 · Emergency LightingSDR USAASB03116Programming Arm · out of adjustAFTER TAKEOFF FROM PHL, CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE IN AUTO, STANDBY OR MANUAL PRESSURIZATION MODES. OUTFLOW VALVE WAS SHOWING CLOSED. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTJul 19, 2003 · N515AU · Boeing 7373B7 · Service DoorsSDR USAASB02171Uplock Sensor · faultyON CLIMB OUT, ENROUTE, CREW RECEIVED A RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT AFTER GEAR RETRACTION. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND CYCLED THE GEAR. THEY RECEIVED THREE GEAR GREEN LIGHTS WHEN EXTENDING GEAR BUT RECEIVED RIGHT MAIN LASep 14, 2002 · N515AU · Boeing 7373B7 · Landing Gear Position and WarningSDR USAASB01237Control Panel · failedCLT - FLT 572 - APPROACH TO CLT,'B' A/P ON, A/C MADE UNCOMMANDED 30 DEGREE ROLL TO THE RT. AFTER A 20 DEGREE HEADING CHANGE (30 DEGREE AOB SELECTED ON TURN KNOB), A/P CORRECTED TO HEADING SELECTED. NO DEFLECTION WAS NOTED ON RUDDER PEDALS. AFTER CORRECTION Aug 19, 2001 · N515AU · Boeing 7373B7 · Autopilot SystemSDR USAA010455Skin · damagedTPA - FOUND FUSELAGE SKIN DAMAGED 4 INCHES, BS 747, BETWEEN S18L AND S19L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 202. (M)Apr 25, 2001 · N515AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA010454Skin · crackedFOUND FUSELAGE SKIN CRACKED .25 INCH, BS 360, LOWER BELLY, BL 0. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-07. (M)Apr 25, 2001 · N515AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB99248Relay · failedPHL - FLT 346 - AFTER TAKEOFF THE CREW REPORTED THAT EVERYTIME THE STAB TRIM SWITCH WAS ACTUATED FROM EITHER YOKE, THE FIRST OFFICERS HSI HEADING FLAGS APPEARED. RELEASING THE SWITCH CAUSES THE FLAGS TO DISAPPEAR. DECISION WAS MADE TO RETURN TO FIELD AT PHL.Oct 12, 1999 · N515AU · Boeing 7373B7 · Integrated Flight SystemSDR USAASB99121Indicator · failedLGA - FLT 420, ON APPROACH, TRAILING EDGE FLAPS WOULD NOT EXTEND MORE THAN FLAPS 10. ACCOMPLISHED GO AROUND AND FLAPS EXTENDED TO FLAPS 15 WITH FLAP HANDLE AT 15. FLAPS RETRACTED NORMALLY. DURING SECOND APPROACH, FLAPS EXTENDED NORMALLY. FLIGHT LANDED WITHMay 6, 1999 · N515AU · Boeing 7373B7 · Trailing Flap Position Indicating SystemSDR USAASB97024Connector · dirtyALB - FL 561 - ON CLIMB-OUT FROM ALB, CREW RECEIVED A FAULT LIGHT FOR THE NR 2 ENG ON THE FIRE WARNING PNL. CREW FOLLOWED ISOLATION PROCEDURES AND DETERMINED THAT THE FIRE DETECT 'B' LOOP WAS INOP. 'A' LOOP TESTED GOOD. MOMENTS LATER, CREW RECEIVED A FAULT Jan 22, 1997 · N515AU · Boeing 7373B7 · Fire DetectionSDR USAA960473Floor Beam · corrosionCLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION AT NUT PLATE HOLES, ACROSS FLOORBEAM LOCATED AT STATION 986.5. INSTALLED NEW CHORD AND REPAIR ANGLES AS PER T/R 53-10-05. (M)Jun 14, 1996 · N515AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA960472Floor Beam · corrosionCLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION, AT NUT PLATE HOLES ACROSS FLOORBEAM, LOCATED AT STATION 967. INSTALLED NEW CHORD AND REPAIR ANGLES PER T/R 53-15-91A. (M)Jun 14, 1996 · N515AU · Boeing 7373B7 · Fuselage Main, Floor Beam
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