N569FE, cancelled Apr 13, 2024

Service difficulty reports · 16

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 = 'N569FE' AND deregistration_id = 'N569FE-2024-04-13'
  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 FDEA201208072897Bulkhead Web · crackedCRACK IN LT SIDEWALL 10 INCHES AFT OF BS 1381 AND 4 INCHES DOWN FROM UPPER BULKHEAD. CRACK EMANATE'S OUT OF LIGHTNING HOLE AND ENDS AT FASTENER. REPAIRED LT WW SIDEWALL IAW SRM 53-00-01, FIG 10.Aug 7, 2012 · N569FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201207032452Battery Pack · inoperativeON PRE FLIGHT RECEIVED AN EMERGENCY BATTERY LOW ALERT. R & R EMERGENCY POWER BATTERY PACK IAW MM 33-51-01-4. OPS CHECKS NORMAL.Jul 3, 2012 · N569FE · Doug MD1010F · Emergency LightingSDR FDEA201103010806Indicator · false activationAFTER MIN 0149 MIN ENROUTE FWD LOWER CARGO FIRE AGENT DISCHARGE SWITCH STARTED TO FLASH. DISCHARGED AGENT PER PHASE ONE/QRH. DIVERTED TO PHX, LANDED UNEVENTFULLY. EVIDENCE OF LEAK, REMOVED AND REPLACED NR 2 FIRE EXTINGUISHER CONTAINER PER MM 26-22-01-4.. EMar 1, 2011 · N569FE · Doug MD1010F · Fire DetectionSDR FDEA201102230705Skin · corrodedLOWER FUSELAGE AT STA 1801, CORROSION EMMITING FROM FASTERNER AND SKIN BETWEEN L46R THRU L48R. REMOVED AREA OF CORROSION, FABRICATED REPAIR PARTS REF SRM 53-20-00, FIG 6. INSTALLED FILLER, DOUBLER, AND TRIPLER REF SRM 53-20-00, FIG 6 ALODINED, PRIMED, AND PFeb 23, 2011 · N569FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201102230704Skin · corrodedLOWER FUSELAGE AT STA 1821, CORROSION EMMITING FROM FASTENERS AND SKIN BETWEEN LONGERON 46R THRU 48R. REMOVED AREA OF CORROSION, FABRICATED REPAIR PARTS REF SRM 53-20-00, FIG 6. INSTALLED FILLER, DOUBLER, AND TRIPLER REF SRM 53-20-00, FIG 6. ALODINED, PRIMEFeb 23, 2011 · N569FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201102230703Skin · corrodedHEAVY CORROSION FOUND AT STA 1701, L44 TO L45, CUT OUT DAMAGE AND REMOVED CORROSION, REF SRM 51-21-01. FABRICATED REPAIR PARTS REF SRM 51-21-01, VOL II AND SRM 53-20-00. INSTALLED REPAIR REF SRM 53-20-00, FIG 6. ALODINED REPAIR AREA REF SRM 51-21-01, VOL IIFeb 23, 2011 · N569FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201102230702Skin · corrodedTEAR STRIP BULGING & CORROSION PRESENT AT STA 1884, LONGERON 45R. CUT OUT DAMAGE AND REMOVED CORROSION REF SRM 51-21-01 & SRM 53-20-00. FABRICATED FILLERS, DOUBLERS, AND TRIPPLERS REF SRM 53-20-00, FIG 5, SH. 6. INSTALLED FILLERS, DOUBLERS, AND TRIPPLERS RFeb 23, 2011 · N569FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201101170213Spar Cap · crackedLT WING AFT LWR SPAR CAP, FOUND 3 CRACKED HOLES ON THE OTBD ROW AND 1 CRACKED HOLE ON THE FWD MOST INBD LT WING AFT LOWER SPAR HAS BEEN REPAIRED AND COMPLIES WITH EA NR 8-5710-142566.Jan 17, 2011 · N569FE · Doug MD1010F · Wing SparSDR FDEA201101170214Spar · crackedLEFT WING REAR SPAR LOWER CHORD ANGLE AT STA.XORS 345 HAS A CRACK INDICATION THROUGH 3 FWD FWD HOLES AND CAN BE SEEN ON THE AFT SIDE EXTENDING OUT OF THE RADIUS APPROX.1" AFT AND UP THE VERTICAL LEG UNDER THE FITTING. (VERIFIED BY N.D.T) REPAIRED AND COMPLIJan 17, 2011 · N569FE · Doug MD1010F · Wing SparSDR FDEA200908313185Tube · damagedFUEL ALERT. LEVEL 2 FUEL QTY/USED CHECK AIRBORNE. FOLLOWED QRH, FUEL SYS MANUAL, ISOLATED TANKS. TANK NR 1 SUSPECT. WERE ON DESCENT TO SLC SO LANDED AND SHUT NR 1 ENG DOWN. LEAK CONFIRMED ON GROUND. FACT: FOUND ROD END HOSE BLOWN ON NR 1 ENG MEC. REPLAAug 31, 2009 · N569FE · Doug MD1010F · Aircraft Fuel Distribution SystemSDR FDEA200901130181Firewall · corrodedNR 3 PYLON, AFT MOUNT FIREWALL ATTACH HOLES HAVE CORROSION. NR 3 ENGINE PYLON AFT MOUNT FIREWALL ATTACH HOLES REPAIRED PER EA 8-5450-126149 SEQ 923 W/O 43105.Jan 13, 2009 · N569FE · Doug MD1010F · Nacelle/Pylon, Bulkhead/FirewallSDR 07FDEA02805Line · rupturedPDIS: AT ROTATION LOSS OF HYD "SYS 1", 0.0. FOUND INLET HOSE ON LOWER HYDRAULIC PUMP RUPTURED. NEEDS NEW HOSE, PUMPS, FILTERS. FOUND HYD LINE NR 1 ENGINE DRIVEN PUMP LINE RUPTURED, REPLACED LINE,BOTH ENG DRIVEN PUMPS, ALL RELATED FILTERS AND LEAK CHECKED PEAug 8, 2007 · N569FE · Doug MD1010F · Hydraulic System, MainSDR 07FDEA01857Transponder · failedIN CRUISE FLIGHT FL 340 TOWER REPORTED US 400' LOW THEN 600' HIGH WITHIN 3 SECONDS ON XPDR NR 1. SWITCHED TO TRANSPONDER NR 2, CENTER REPORTED US AS STABLE AT FL 340. REMOVED AND REPLACED NR 1 TRANSPONDER PER EO REF 8-3454-7-5001 AND MM REF 34-54-00-5.May 18, 2007 · N569FE · Doug MD1010F · Visual Omnirange (VOR) SystemSDR 04FDEA01718Angle · crackedEXISTING REPAIR SPLICE ON LEFT WING STRINGER 4 CRACKED AT XORS 930. CRACKED REPAIR ANGLE REPLACED BY A NEW REPAIR ANGLE MADE FROM 7075-73511 THAT ARE MORE FATIGUE RESISTANT IAW FEDEX EA 8-5710-73240.Mar 2, 2004 · N569FE · Doug DC1010 · Wing Main, Frame StructureSDR 04FDEA01719Cap · crackedRIGHT AND LEFT WING UPPER CAP CRACKED AT XORS 372. THE CRACKS ARE AROUND CUTOUTS FOR STRINGER 12 AND 13. CRACKS HAVE BEEN TRIMMED AND ROUTED. REPAIR ANGLE AND DOUBLERS HAVE BEEN INSTALLED IAW FEDEX EA 8-5710-73236.Feb 4, 2004 · N569FE · Doug DC1010 · Wing Miscellaneous StructureSDR 04FDEA01717Skin · crackedHORIZONTAL STABILIZER - UPPER COSTANT SECTION AND OUTBOARD SKINS CRACKS WITHIN FLYABLE LIMITS. PANELS INVOLVED: ALC7436-1, ALC7437-1, ALC7207-1 AND ALC7208-1. CRACKED PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-73235.Feb 3, 2004 · N569FE · Doug DC1010 · Horizontal Stabilizer, Plate/Skin
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