N9625W

Service difficulty reports · 89

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 = 'N9625W' AND registry_match = 'registration'
  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 AALA20150322007Cusp Web · corrodedCABIN CUSP SHEET CORRODED BETWEEN FS 503 & 579. R & R CUSP SHEET IAW AARD 53-20-00-16.Mar 13, 2015 · N9625W · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20150320009Cusp Web · corrodedLEFT CUSP CORRODED FROM FS 932 - 942. R & R CUSP FROM FS 905 - 946 IAW SRM 53-14-03-001 FIG 10, DWG FDK3161, DWG 9910151 & DWG 53595.Mar 13, 2015 · N9625W · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20150322006Cusp Web · corrodedCORROSION IN LT CUSP SHEET AT FS 1174 BETWEEN 1 & 2 SEAT TRACKS INSTALLED CUSP REPAIR DOUBLER IAW AARD 53-20-00-16.Mar 12, 2015 · N9625W · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20140307007Computer · inoperativeRDU INFLIGHT DFW ORF CREW REPORTED AUTOPILOT & AUTO THROTTLES WOULD NOT ENGAGE & ENG ANTI-ICE FAILED. FLIGHT DIVERTED RDU LANDED WITHOUT INCIDENT. REPLACED NR 2 DIGITAL FLIGHT GUIDANCE COMPUTER. SYS GND CHECKED NORMAL, OPERATION CLOSED.Mar 7, 2014 · N9625W · Doug DC983 · Flight Management Computing Hardware SystemSDR AALA20110822DWH01Skin · damagedBAGGAGE CART, BLOWN BY HIGH WINDS, PUNCHED HOLE IN FUSELAGE STATION 560 LONGERONS 22 TO 23 RIGHT. ACCOMPLISHED DOUBLER REPAIR PER SG09530002 DRAWING AND SRM 53-04-00.Aug 22, 2011 · N9625W · Doug DC983 · Fuselage Main, Plate/SkinSDR AALA20110117TUL01Cusp Web · corrodedRIGHT CUSP STATIONS 864 TO 886 CORROSION OUT OF LIMITS. REPAIRED CUSP SHEET AT STATIONS 870 TO 875 PER AARD 53-20-00-16.Jan 17, 2011 · N9625W · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20110114TUL01Cargo Track · corrodedAFT CARGO HAS CORROSION ON RIGHT TIE DOWN TRACK BETWEEN STATIONS 1212 TO 1320. INSTALLED NEW TIE DOWN TRACK PER AARD 51-10-00-5.Jan 14, 2011 · N9625W · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR AALA20110113TUL07Longeron · crackedAFT ACCS LONGERON 2 LEFT CRACKED AFT OF STATION 1418. INSTALLED SPLICE REPAIR ON LONGERON 2 LEFT AT STATION 1418 PER SRM 53-02-00.Jan 13, 2011 · N9625W · Doug DC983 · Fuselage Main, Longeron/StringerSDR AALA20110113TUL06Cusp Web · damagedELONGATED HOLE AT AFT OUTBOARD HOLE IN FORWARD CUSP SHEET STATION 845 RIGHT. INSTALLED DOUBLER PER AARD 53-20-00-16.Jan 13, 2011 · N9625W · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20110113TUL02Cusp Web · damagedRIGHT CUSP STATIONS 984 TO 1003 ALL 3 LIGHTNING HOLES IN BAY HAVE TOOLING MARKS BEYOND LIMITS. REMOVED DAMAGE AT STATIONS 984 TO 1003 RIGHT AND INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.Jan 13, 2011 · N9625W · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20110112TUL06Pan · corrodedFORWARD CARGO HAS CORROSION ON LOWER DOOR JAMB PAN BETWEEN STATIONS 370 TO 427. INSTALLED LOWER DOOR PAN PER SRM 53-05-00 FIGURE 44.Jan 12, 2011 · N9625W · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20110112TUL03Cusp Web · damagedRIGHT CUSP STATIONS 984 TO 1003 ALL 3 LIGHTENING HOLES IN BAY HAVE TOOLING MARKS BEYOND LIMITS. REMOVED DAMAGE AT STATIONS 984 TO 1003 RIGHT. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.Jan 12, 2011 · N9625W · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20110112TUL02Frame · corrodedAFT CARGO HAS CORROSION ON FRAME AT STATION 1271 NEAR LONGERON 30. INSTALLED J ANGLE DOUBLER PER AARD 53-10-00-14 FIGURE 1 SHEET 1.Jan 12, 2011 · N9625W · Doug DC983 · Fuselage Main, FrameSDR AALA20110112TUL01Seat Track · corrodedSEAT TRACK NUMBER 5 HAS CORROSION OUT OF LIMITS AT STATIONS 237 TO 239. INSTALLED PLUG REPAIR PER AARD 53-20-00-10.Jan 12, 2011 · N9625W · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR AALA20110111TUL02Longeron · crackedLONGERON 2 LEFT CRACKED AFT OF STATION 1418. INSTALLED LONGERON SPLICE REPAIR PER SRM 53-14-04.Jan 11, 2011 · N9625W · Doug DC983 · Fuselage Main, Longeron/StringerSDR AALA20110111TUL01Beam · corrodedHEAVY CARGO/AFT- CORROSION ON DOOR CUTOUT LOWER BEAM SEVERAL PLACES FROM STATIONS 1155 TO 1212 RIGHT LONGERON 28 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-3.Jan 11, 2011 · N9625W · Doug DC983 · Fuselage Main, StructureSDR AALA20110110TUL02Cusp Web · corrodedLEFT CUSP STATIONS 598 TO 712 HAS AREAS OF BARE METAL AND CORROSION OUT OF LIMITS. REPLACED LEFT CUSP STATIONS 598 TO 712 PER SRM 51-01-00.Jan 10, 2011 · N9625W · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20110106TUL11Pan · crackedLEFT STATION 1041 UPPER AFT EAR CRACKED ON THE WINDOW PAN. INSTALLED DOUBLER PER AARD 53-10-00-25.Jan 6, 2011 · N9625W · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20110106TUL10Pan · crackedLEFT STATION 1098 UPPER AFT EAR CRACKED ON THE WINDOW PAN. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.Jan 6, 2011 · N9625W · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20110106TUL09Pan · crackedLEFT STATION 1022 UPPER AFT EAR CRACKED ON THE WINDOW PAN. INSTALLED DOUBLER PER AARD 53-10-00-25.Jan 6, 2011 · N9625W · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20110106TUL08Pan · crackedRIGHT STATION 1098 FORWARD LOWER EAR CRACKED ON THE WINDOW PAN. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.Jan 6, 2011 · N9625W · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20100730TUL14Oxygen Bottle · low pressureOMA - INFLIGHT ORD-DEN. CREW REPORTED O2 BOTTLE PRESSURE LOW. LANDED OMA WITHOUT INCIDENT. REPLACED CREW O2 BOTTLE PER MAINTENANCE MANUAL. PERFORMED SELF TEST OF FIRST OFFICER’S REGULATOR, NO DEFECTS NOTED. SYSTEM GROUND CHECK NORMAL OPERATION.Jul 30, 2010 · N9625W · Doug DC983 · Crew Oxygen SystemSDR AALA20091217LGA02Battery Pack · dischargedEMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK.Dec 17, 2009 · N9625W · Doug DC983 · Emergency LightingSDR AALA20090817TUL04Beam · crackedCRACK IN VAULT DOOR RIGHT BEAM AT UPPER HINGE AREA. INSTALLED DOUBLER (4090576) PER SRM 52-05-00 FIG 34 (E-58 6337696).Aug 17, 2009 · N9625W · Doug DC983 · DoorsSDR AALA20070420Battery Pack · inoperativeLGA - SEAT MOUNTED EMERGENCY LIGHT IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR AFT SEAT MOUNTED EMERGENCY LIGHT IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.Mar 3, 2007 · N9625W · Doug DC983 · Emergency LightingSDR AALA20070324Module · inoperativeLGA - FOUND EMERGENCY EGRESS LIGHTS FROM SEAT ROWS 1 TO 19 INOPERATIVE. REPLACED EMERGENCY LIGHT MODULE AT SEAT ROW 19 OVERHEAD BIN FOR SEAT ROWS 1 TO 19. SYSTEM GROUND CHECKED NORMAL OPERATION.Feb 12, 2007 · N9625W · Doug DC983 · Emergency LightingSDR AALA20060368Oxygen Bottle · leakingINFLIGHT - CREW OXYGEN PRESSURE LOW. LANDED MSY WITHOUT INCIDENT. FOUND LEAK AT CAPTAIN SIDE OXYGEN EMERGENCY SUPPLY. REPLACED CREW OXYGEN BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION.Jun 6, 2006 · N9625W · Doug DC983 · Crew Oxygen SystemSDR AALA20060333Line · leakingDFW - RIGHT ENGINE SHUT DOWN DUE TO LOSS OF OIL QUANTITY. ENGINE OIL QUANTITY WAS ZERO BUT PRESSURE INDICATION WAS STILL 36 PSI BUT DROPPING WHEN SHUTDOWN. OIL TEMPERATURE WAS ABOVE 100 DEGREES CELSIUS. ENGINE WINDMILLED FOR APPROXIMATELY 22 MINUTES WITH 12May 26, 2006 · N9625W · Doug DC983 · Engine Oil PressureSDR AALA20050573Connector · inoperativeSTL - EMERGENCY EGRESS LIGHTS AT AFT CABIN INOPERATIVE. REPAIRED QUICK DISCONNECT IN TAIL SIDEWALL LIGHT FOR EMERGENCY EGRESS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.Sep 4, 2005 · N9625W · Doug DC983 · Light System WiringSDR AALA20040215Terminal · looseSTL EMERGENCY EXIT LIGHTS AT BOTH FORWARD OVERWING EXIT DOORS INOPERATIVE. FOUND LOOSE TERMINAL ON POWER SUPPLY. SECURED LOOSE TERMINAL ON POWER SUPPLY FOR FORWARD OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.Feb 10, 2004 · N9625W · Doug DC983 · Light System WiringSDR AALA20031345Battery Pack · dischargedDFW OVERHEAD EMERGENCY EXIT LIGHT BETWEEN ROWS 18-20 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY EXIT LIGHT BETWEEN ROWS 18-20. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--Nov 30, 2003 · N9625W · Doug DC983 · Emergency LightingSDR AALA20031337Battery Pack · dischargedTUL LEFT AND RIGHT OVERWING ESCAPE HATCH EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT OVERWING ESCAPE HATCH EXIT SIGN LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.Nov 27, 2003 · N9625W · Doug DC983 · Emergency LightingSDR ZW0A0301401Battery · dischargedTHE CEILING EMERGENCY LIGHTS AT ROW 25 TO THE AFT CABIN WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK.Jan 29, 2003 · N9625W · Doug DC983 · Emergency LightingSDR ZW0A0210604Battery Pack · dischargedCABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE R5-205 AND R5-209 BATTERY PACKS.Oct 18, 2002 · N9625W · Doug DC983 · Emergency LightingSDR TWAA0104602Battery Pack · dischargedTHE FWD OVERHEAD EMERGENCY LIGHTS AROUND THE LIFE RAFT CONTAINER WOULD NOT EXTINGUISH WITH POWER OFF THE AIRCRAFT. PLACED EMERGENCY LIGHT SWITCH TO ARM FOR A HALF HOUR THEN LIGHTS STAYED OFF. ON FOLLOW UP THE NEXT STATION REPLACED THE BATTERY PACK. CHECK-C Mar 11, 2001 · N9625W · Doug DC983 · Emergency LightingSDR TWAA0005901Tube · fracturedTHE RT ENGINE WAS SHUT DOWN DUE TO OIL LOSS. MADE AN UNSCHEDULED LANDING AT SAT. FOUND OIL IN THE TAIL PIPE. REPLACED THE ENGINE. CHECK-C 9-3-99. *S/D* FOUND THE NUMBER 4 1/2 AND NUMBER 6 BEARING INTERNAL PRESSURE TUBE ASSEMBLY HAD FRACTURED, LEAKING OILApr 15, 2000 · N9625W · Doug DC983 · Turbine Engine Oil SystemSDR TWAA0001812Skin · damagedTHE RT SIDE FORWARD CABIN DOOR WAS DAMAGED AT THE FORWARD LOWER CORNER OF DOOR. REWORKED LOWER EDGE OF DOOR AT FWD CORNERS PER SRM 53-02, PAGE 1. CHANGED HINGE ASSY AND TORQUE TUBE ASSY. OPS AND RIG OK REF MM 52-41-00 FIG 401, 405, 501, 513.Jan 31, 2000 · N9625W · Doug DC983 · Passenger/Crew DoorsSDR TWAA9910103Skin · bentTHE LT FWD PASSENGER ENTRY DOOR, FORWARD LOWER EDGE OF THE OUTER SKIN, WAS BENT IN 4 INCHES WIDE BY 1 INCH HIGH AND 0.25 IN DEEP. REPAIRED PER SRM 52-03, PAGE 1 ITEM 1 PARAGRAPH A.Jul 7, 1999 · N9625W · Doug DC983 · Passenger/Crew DoorsSDR TWAA9909708Skin · bentTHE FWD LOWER EDGE OF THE OUTER SKIN WAS BENT IN FOUR INCHES WIDE BY 1 IN HIGH AND 0.25 IN DEEP. REPAIRED PER SRM 52-03, PAGE 1, ITEM 1 PARAGRAPH A.Jul 7, 1999 · N9625W · Doug DC983 · Fuselage Main, Plate/Skin
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