# Service difficulty reports: N569FE, cancelled Apr 13, 2024 A list on [N569FE, cancelled Apr 13, 2024](https://openairdocs.org/deregistered/N569FE-2024-04-13.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA201208072897](https://openairdocs.org/sdr/FDEA201208072897.md): Bulkhead Web · cracked · Aug 7, 2012 · N569FE · Doug MD1010F · Fuselage Main, Bulkhead > CRACK 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. - [SDR FDEA201207032452](https://openairdocs.org/sdr/FDEA201207032452.md): Battery Pack · inoperative · Jul 3, 2012 · N569FE · Doug MD1010F · Emergency Lighting > ON PRE FLIGHT RECEIVED AN EMERGENCY BATTERY LOW ALERT. R & R EMERGENCY POWER BATTERY PACK IAW MM 33-51-01-4. OPS CHECKS NORMAL. - [SDR FDEA201103010806](https://openairdocs.org/sdr/FDEA201103010806.md): Indicator · false activation · Mar 1, 2011 · N569FE · Doug MD1010F · Fire Detection > AFTER 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.. E - [SDR FDEA201102230705](https://openairdocs.org/sdr/FDEA201102230705.md): Skin · corroded · Feb 23, 2011 · N569FE · Doug MD1010F · Fuselage Main, Plate/Skin > LOWER 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 P - [SDR FDEA201102230704](https://openairdocs.org/sdr/FDEA201102230704.md): Skin · corroded · Feb 23, 2011 · N569FE · Doug MD1010F · Fuselage Main, Plate/Skin > LOWER 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, PRIME - [SDR FDEA201102230703](https://openairdocs.org/sdr/FDEA201102230703.md): Skin · corroded · Feb 23, 2011 · N569FE · Doug MD1010F · Fuselage Main, Plate/Skin > HEAVY 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 II - [SDR FDEA201102230702](https://openairdocs.org/sdr/FDEA201102230702.md): Skin · corroded · Feb 23, 2011 · N569FE · Doug MD1010F · Fuselage Main, Plate/Skin > TEAR 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 R - [SDR FDEA201101170213](https://openairdocs.org/sdr/FDEA201101170213.md): Spar Cap · cracked · Jan 17, 2011 · N569FE · Doug MD1010F · Wing Spar > LT 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. - [SDR FDEA201101170214](https://openairdocs.org/sdr/FDEA201101170214.md): Spar · cracked · Jan 17, 2011 · N569FE · Doug MD1010F · Wing Spar > LEFT 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 COMPLI - [SDR FDEA200908313185](https://openairdocs.org/sdr/FDEA200908313185.md): Tube · damaged · Aug 31, 2009 · N569FE · Doug MD1010F · Aircraft Fuel Distribution System > FUEL 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. REPLA - [SDR FDEA200901130181](https://openairdocs.org/sdr/FDEA200901130181.md): Firewall · corroded · Jan 13, 2009 · N569FE · Doug MD1010F · Nacelle/Pylon, Bulkhead/Firewall > NR 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. - [SDR 07FDEA02805](https://openairdocs.org/sdr/07FDEA02805.md): Line · ruptured · Aug 8, 2007 · N569FE · Doug MD1010F · Hydraulic System, Main > PDIS: 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 PE - [SDR 07FDEA01857](https://openairdocs.org/sdr/07FDEA01857.md): Transponder · failed · May 18, 2007 · N569FE · Doug MD1010F · Visual Omnirange (VOR) System > IN 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. - [SDR 04FDEA01718](https://openairdocs.org/sdr/04FDEA01718.md): Angle · cracked · Mar 2, 2004 · N569FE · Doug DC1010 · Wing Main, Frame Structure > EXISTING 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. - [SDR 04FDEA01719](https://openairdocs.org/sdr/04FDEA01719.md): Cap · cracked · Feb 4, 2004 · N569FE · Doug DC1010 · Wing Miscellaneous Structure > RIGHT 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. - [SDR 04FDEA01717](https://openairdocs.org/sdr/04FDEA01717.md): Skin · cracked · Feb 3, 2004 · N569FE · Doug DC1010 · Horizontal Stabilizer, Plate/Skin > HORIZONTAL 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. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N569FE-2024-04-13/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.