N429US, cancelled Sep 8, 2017

Service difficulty reports · 37

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 = 'N429US' AND deregistration_id = 'N429US-2017-09-08'
  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 USAASB03099Charger · failedMAINTENANCE REPORTED THE FORWARD FLOOR PROXIMITY EMERGENCY EXIT LIGHT AT SEAT ROW 11, LEFT SIDE, ALONG WITH THE FLOOR PATH EMERGENCY LIGHTS FROM SEAT ROWS 7 THROUGH 11 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, P/N 2013-1A, AND CHARGER ASJul 3, 2003 · N429US · Boeing 7374B7 · Emergency LightingSDR USAASB02208Warning Light · illuminatedPBI - FLT 1246 - ON CLIMB-OUT FROM MIA, EN ROUTE TO PIT, THE NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. ALL OTHER ENGINE INDICATIONS WERE NORMAL. CREW OPERATED THE NR 2 ENGINE AT REDUCED THRUST BUT THE LIGHT STILL FLICKERED OFF AND ON. FLIGHT DIVERTEDNov 21, 2002 · N429US · Boeing 7374B7 · Engine Oil Indicating SystemSDR USAASB01249Downlock SensorSDF - FLT 1144 - IN PREPARATION FOR LANDING AT SDF, THE CREW RECEIVED A RIGHT MAIN LANDING GEAR UNSAFE LIGHT DURING GEAR EXTENSION. CAPTAIN ACCOMPLISHED A FLYBY AT SDF TOWER FOR VISUAL THAT GEAR WAS DOWN. TOWER CONFIRMED GEAR WAS DOWN. CAPTAIN ALSO REPORTEDSep 8, 2001 · N429US · Boeing 7374B7 · Landing Gear SystemSDR USAA010763Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCH, BS 727D, STRINGER 23R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-60-03. (M)Jun 28, 2001 · N429US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA010472Bulkhead · crackedCLT - FOUND PRESSURE WEB WITH 5 CRACKS, TWO .250 INCH, TWO .150 INCH AND ONE .100 INCH, BS 178, WL 195, 198, 201.5, 206.6; LBL 5 TO RBL 7. DAMAGE CUTOUT, REPAIR DOUBLER INSTALLED PER EO 5300V153 AND EA 69566. (M)Apr 27, 2001 · N429US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA000712Skin · crackedCLT - FOUND SKIN CRACKED .250 INCH, EXT SKIN AFT ENTRANCE DOOR LOWER HINGE UPPER CUTOUT. INSTALLED DOUBLER PER SRM 52-00-01. (M)May 15, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA000701Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 440, STRINGER 8L. INSTALLED DOUBLER PER TR 53-10-14. (M)May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA000699Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 787, STRINGER 8L. INSTALLED DOUBLER PER TR 53-10-14. (M)May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA000698Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 440, STRINGER 8R. INSTALLED DOUBLER PER TR 53-10-14. (M)May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA000697Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 296, STRINGER 17R FORWARD SERVICE DOOR CUTOUT. INSTALLED DOUBLER AND FILLER ANGLE PER SRM 51-70-11. (M)May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA000696Frame · crackedCLT - FOUND FRAME CRACKED 2 INCHES, BS 601 RT, WL 202. INSTALLED STIFFENER AND FILLER PER EA 67119. (M)May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA000703Floor Support · corrodedCLT - FOUND FLOOR SUPPORT BEAM CORRODED 1 INCH BY 2 INCH, 9 INCHES INBOARD OF AFT ENTRY DOOR STATION 986.5. INSTALLED NEW T-CAP PER TR 53-60-01. CORROSION LEVEL 2. (M)May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA000700Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 747, STRINGER 8L. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA000695Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 70 INCHES, FS 328 BETWEEN RBL 56 AND RBL 14. INSTALLED NEW T-CAP PER SRM 53-10-51. CORROSION LEVEL 2. (M)May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA000668Skin · crackedCLT - FOUND SKIN CRACKED .25 INCH, OUTBOARD EDGE OF PANEL 5727L CUTOUT. INSTALLED DOUBLER PER TR 54-30-07. (M)May 4, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA000655Floor Support · corrodedCLT - FOUND FLOOR SUPPORT CORRODED, RIGHT AFT DOOR Z-ANGLE. LEVEL 1 CORROSION. INSTALLED DOUBLER PER SRM 51-70-11. (M)May 1, 2000 · N429US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA000656Floorbeam · corrodedCLT - FOUND BEAM CRACKED 2 INCHES BY 55 INCHES, NUMEROUS CORROSION LEVEL 2, FLOORBEAM AT FS 344 BETWEEN RBL 11 AND LBL 44. INSTALLED NEW T-CAP AND SPLICE PER SRM 53-10-51. (M)May 1, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA000657Angle · corrodedCLT - FOUND Z-ANGLE CORRODED .250 INCH BY .250 INCH, FORWARD SERVICE DOOR JAM. INSTALLED NEW Z-ANGLE PER SRM 53-10-13. (M)May 1, 2000 · N429US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA000658Frame · crackedCLT - FOUND FRAME CRACKED 2 INCHES, BS 601 LT AT WL 202. INSTALLED DOUBLER PER EA 67119 AND TR 53-62-01. (M)May 1, 2000 · N429US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA000659Bulkhead · crackedCLT - FOUND WEB CRACKED 1 INCH, 178 BULKHEAD, LBL 5.7 AND WL 202 AND 199. INSTALLED DOUBLER PER TR 53-10-07 REV A. (M)May 1, 2000 · N429US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA000612Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 727D, STRINGER 8 RT. INSTALLED DOUBLER PER TR 53-10-14. (M)Apr 28, 2000 · N429US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA000613Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 727D, STRINGER 8 LEFT. INSTALLED DOUBLER PER TR 53-10-14. (M)Apr 28, 2000 · N429US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA000614Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 380 STRINGER 8 RIGHT. INSTALLED DOUBLER PER TR 53-10-14. (M)Apr 28, 2000 · N429US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA000615Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 380 STRINGER 8 LEFT. INSTALLED DOUBLER PER TR 53-10-14. (M)Apr 28, 2000 · N429US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA000616Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 400 STRINGER 8 LEFT. INSTALLED DOUBLER PER TR 53-10-14. (M)Apr 28, 2000 · N429US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA000617Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 867, STRINGER 8 LEFT. INSTALLED DOUBLER PER TR 53-10-14. (M)Apr 28, 2000 · N429US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA000618Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 907 STRINGER 8 RIGHT. INSTALLED DOUBLER PER TR 53-10-14. (M)Apr 28, 2000 · N429US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA000423Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED 1 INCH, LEFT SIDE FUSELAGE AFT OF LT WING BODY FAIRING. REPAIRED DOUBLER AND FILLER PER TR 53-60-03. (M)Mar 21, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAASB00031Circuit Breaker · trippedBOS - FLT 2030 - CREW RECEIVED A GEAR INDICATION WARNING FOR THE NOSE GEAR WHILE PREPARING TO LAND AT BOS. CAPTAIN ACCOMPLISHED A FLYBY THE TOWER TO VERIFY THE GEAR WAS DOWN. AFTER CONFIRMATION, CREW ALSO VERIFIED THE NOSE GEAR WAS DOWN THROUGH THE VIEWFINDEFeb 2, 2000 · N429US · Boeing 7374B7 · Landing Gear Position and WarningSDR USAA991425Skin · crackedTPA - DURING AC-5 CHECK VISUAL INSPECTION, FOUND THE DOOR SKIN BENT AND CRACKED JUST ABOVE LOWER HINGE CUTOUT. REPAIRED PER EA 66130. (M)Dec 18, 1999 · N429US · Boeing 7374B7 · Passenger/Crew DoorsSDR USAASB98302Light · inoperativeTPA - MAINTENANCE FOUND THE FORWARD ENTRY EGRESS EMERGENCY LIGHT AND THE RIGHT AFT FUSELAGE EGRESS EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE REFLECTOR ASSEMBLIES AT BOTH LOCATIONS. OPERATIONAL CHECK GOOD. (M)Nov 15, 1998 · N429US · Boeing 7374B7 · Emergency LightingSDR USAA980549Skin · crackedTPA - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK ELEVATOR STATION 81.54 AT STAB STATION 67.54 HORIZ STAB SKIN. CUTOUT CRACK AND INSTALLED DOUBLER PER TR 55-10-07. (M)Oct 19, 1998 · N429US · Boeing 7374B7 · Horizontal Stabilizer, Plate/SkinSDR USAA980525Skin · crackedTPA - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK ELEV STATION 51-54 AT STAB STATION 67.54 HORIZONTAL STABILIZER SKIN. CUTOUT CRACK AND INSTALLED DOUBLER PER TR 55-10-07. (M)Oct 19, 1998 · N429US · Boeing 7374B7 · Horizontal Stabilizer, Plate/SkinSDR USAASB97011Battery Pack · dischargedCLE - MX FOUND THE FORWARD SERVICE DOOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)Jan 8, 1997 · N429US · Boeing 7374B7 · Emergency LightingSDR usaasb96139Coalescer Bag · failedDEN-PIT - FLT 132 - CREW REPORTED A SMOKE TYPE SMELL IN THE COCKPIT AND FORWARD CABIN. SMELL IS STRONGEST IN THE COCKPIT. HAPPENS AT DIFFERENT FLIGHT CONDITIONS. SUSPECT LEFT PACK. MAINTENANCE REPLACED THE LEFT PACK SECONDARY (REAR) WATER EXTRACTOR. RAN PJul 25, 1996 · N429US · Boeing 7374B7 · Humidity Control SystemSDR USAASB96116Fan · failedMCO - FLT 1981 - ON DESCENT TO MCO, CREW NOTICED A VERY STRONG ODOR. SMELLED LIKE HYDRAULIC FLUID ON A HOT DUCT. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT AIR CONDITIONING RECIRCULATING FAN. OPSJun 25, 1996 · N429US · Boeing 7374B7 · Air Distribution FanSDR USAA950759Circuit Breaker · failedLGA - FLT 2235 - THE 'NOSE GEAR UNSAFE' LIGHT ILLUMINATED WHEN THE POWER WAS BROUGHT TO IDLE. VISUALLY VERIFIED GEAR POSITION AND PERFORMED TOWER FLYBY. FLIGHT CREW FOUND AIR/GRD RELAY AND LANDING GEAR LIGHTS CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. Jul 20, 1995 · N429US · Boeing 7374B7 · Landing Gear Position and Warning
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