N576FE

Service difficulty reports · 353

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 = 'N576FE' 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 FDEA201111255028Battery · dischargedEMERGENCY POWER TEST FAILED 3 TIMES. PERFORMED BATTERY TEST, EMERGENCY POWER TEST AFTER LETTING BATTERIES CHARGE. OPS NORMAL AT THIS TIME.Nov 25, 2011 · N576FE · Doug MD11F · Battery/Charger SystemSDR FDEA201111104854Unknown · unknownON CLIMB OUT THRU 16,000 HAD LOUD RUMBLE AND ACFT SHOOK BRIEFLY. HAPPENED 6 OR 7 MORE TIMES. DID NOT NOTICE ANY ABNORMAL INDICATIONS. RETURNED BACK TO FIELD. INSPECTED AIRCRAFT, NO DEFECTS FOUND.Nov 10, 2011 · N576FE · Doug MD11F · Standard Practices/StructuresSDR FDEA201103020816Light · inoperativeEMERGENCY LIGHTS INOP DURING POST FLIGHT CHECK.Mar 2, 2011 · N576FE · Doug MD11F · Emergency LightingSDR FDEA201004101130Skin · crackedRT WING - STA XORS 690 TO XORS 700 LOWER SKIN ACCESS DOOR CUT OUT 09 EACH FASTENER HOLES FOUND CRACKED DURING HFEC OPEN HOLE INSP. RT WING - STA XORS 690 TO XORS 700 LOWER SKIN ACCESS DOOR CUT OUT 09 EACH FASTENER HOLES REPAIRED IAW EA NR 1-5710-132404, TITLEApr 10, 2010 · N576FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201004101129Skin · crackedLT WING - STA XORS 690 TO XORS 700 LOWER SKIN ACCESS DOOR CUT OUT 08 EACH FASTENER HOLES FOUND CRACKED DURING HFEC OPEN HOLE INSPECTION. LT WING - STA XORS 690 TO XORS 700 LOWER SKIN ACCESS DOOR CUT OUT 08 EACH. FASTENER HOLES REPAIRED IAW EA NR 1-5710-13Apr 10, 2010 · N576FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201004101128Skin · dentedLT WING - SLAT NR 2 L/E LOWER SURFACE FOUND DENT. LT WING - SLAT NR 2 L/E LOWER SURFACE REPAIRED IAW SRM 57-40-01, FIGURE 201, REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 110.Apr 10, 2010 · N576FE · Doug MD11F · Leading Edge DevicesSDR FDEA201004081110Frame · dentedMAIN DECK CARGO - RT STA 1741 LONGERON 12 RT, FRAME FOUND DENT. FRAME REPAIRED IAW SRM 53-00-07 FIG 201 REPAIR 2, REVISION 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.Apr 8, 2010 · N576FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201004081109Frame · dentedMAIN DECK CARGO - RT STA 1701 LONGERON 12 RT, FRAME FOUND DENT. FRAME REPAIRED IAW SRM 53-00-07 FIG 201 REPAIR 2, REVISION 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.Apr 8, 2010 · N576FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201004081097Longeron Splice · crackedX-RAY INSP AT STA 6-100 LONGERON 1 LT, LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE R & R IAW SRM 51-33-01, REVISION 43. CLASSIFIED MAJOR REPAIR IAW GMM 6-2-100 REV 110.Apr 8, 2010 · N576FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201004071096Skin · crackedLT WING - L/E NR 7 SLAT TRACK CUT OUT INBD SIDE FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 43. CLASSIFIED MINOR REPAIR IAW GMM 6-2-100, REV 110.Apr 7, 2010 · N576FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201004071095Skin · crackedLT WING - L/E NR 6 SLAT TRACK CUT OUT INBD SIDE FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIGURE 201, REPAIR 7, REVISION 43. CLASSIFIED MINOR REPAIR IAW GMM 6-2-100, REV 110.Apr 7, 2010 · N576FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201004061061Skin · crackedCRACK FOUND AT RT WING NR 3 L/E SLAT TELESCOPIC DUCT CUTOUT. RT WING NR 3 L/E SLAT TELESCOPIC DUCT CUTOUT REPAIRED IAW EA NR 1-5710-132397, CLASSIFIED MAJOR REPAIR IAW GMM 6-2-100, REVISION 110.Apr 6, 2010 · N576FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA04385Mount · wornWITH REFERENCE TO SNRM N01236, DURING BEARING REMOVAL AT NR 1 PYLON AFT MOUNT FITTING BORE FOUND WORN. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Oct 17, 2008 · N576FE · Doug MD11F · Nacelle/Pylon, Attach FittingsSDR 08FDEA04374Bearing · migratedNR 1 PYLON AFT MOUNT FOUND WITH BEARING MIGRATION. REMOVED AND REPLACED WITH NEW HIGHER FITTING ASSEMBLY AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 16, 2008 · N576FE · Doug MD11F · Nacelle/Pylon, Main FrameSDR 08FDEA04307Fitting · crackedRIGHT MAIN LANDING GEAR WW DOOR LOWER UPLATCH FITTING (FWD AND AFT ) FOUND CRACKED. R & R WITH FABRICATED UPLATCH FITTING AS PER SRM 51-33-01. UPLATCH FITTING FABRICATED AS PER DRAWING ANB7089. OPERATIONS CHECK CARRIED OUT ON RT MLG LOWER UPLATCH FITTING ASOct 11, 2008 · N576FE · Doug MD11F · Fuselage Main, Attach FittingsSDR 08FDEA04297Frame · corrodedCORROSION ON FRAME LOWER AT AFT CARGO BILGE L50L- L50R. CORRODED FRAME AT AFT CARGO BILGE BS 1967 L50L- L50R REMOVED AND REPLACED WITH A FABRICATED FRAME AS PER SRM 51-31-01. FRAME FABRICATED AS PER E.A. 1-5310-123128. REPAIR CLASSIFIED AS MINOR AS PER GMMOct 10, 2008 · N576FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA04296Frame · corrodedCORROSION ON FRAME LOWER AT AFT CARGO BILGE STA. 1979 L49L-49R. AFT CARGO LOWER FRAME AT BILGE STA. 1979 L49L - L49R DAMAGED REMOVED, REWORKED EXTRUSION P/N: S4933678X7075-0 AS PER DRAWING AGA8002 AND INSTALLED IN PLACED AS PER SRM 51-31-01 VOL. II. REPAIOct 10, 2008 · N576FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA04279Frame · dentedMAIN DECK CARGO COMPARTMENT, LT SIDEWALL STRUCTURE FRAME BS 1701 FOUND DENTED, LONGERON 12L. MAIN DECK CARGO BAY, LT SIDEWALL STRUCTURE FRAME BS 1701 AT L-12L, DENTED AREA REPAIRED AS PER SRM 53-30-00 FIG. 1 VOL. I. REPETITIVE INSPECTION REQUIRED - INITIALOct 8, 2008 · N576FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA04222Skin · dentedLT WING I/B FLAP LOWER SURFACE SCRATCH AND DENT FOUND AT WS 151.3. REPAIR CARRIED OUT AT LT WING INBOARD FLAP LOWER SEGMENT AT STA XW = 151.3 AS PER SRM 57-10-00. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 6, 2008 · N576FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA04221Skin · dentedLT WING I/B FLAP LOWER SURFACE AT WS 288.14 DENT FOUND. REPAIR CARRIED OUT AT LH WING I/B FLAP LOWER SURFACE AT STA. 288.140 AS PER SRM 57-10-00 FIG. 13 VOL. I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 6, 2008 · N576FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA04220Skin · cracked05 EA FASTENER HOLES FOUND CRACK DURING HFEC INPECTION ON RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS=683.4 AND XORS=713.6. REPAIRED AS PER E.A. 1-5710-122580 - A.D. 2007-07-04. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 6, 2008 · N576FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA04219Skin · cracked06 EA FASTENER HOLES FOUND CRACK DURING HFEC INPECTION ON LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS=683.4 AND XORS=713.6. REPAIRED AS PER E.A. 1-5710-122579- A.D. 2007-07-04. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 6, 2008 · N576FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA04218Support Fitting · crackedDURING OPEN HOLE INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C, AND D. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 7 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. Oct 6, 2008 · N576FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA04217Support Fitting · crackedDURING OPEN HOLE INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES C, AND D.Oct 6, 2008 · N576FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA04216Support Fitting · crackedDURING OPEN HOLE INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLES C, AND D.Oct 6, 2008 · N576FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA04215Support Fitting · crackedDURING OPEN HOLE INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLES B, C, AND D. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 3 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. Oct 6, 2008 · N576FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA04213Support Fitting · crackedDURING OPEN HOLE INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D.Oct 6, 2008 · N576FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA04211Support Fitting · crackedDURING OPEN HOLE INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D.Oct 6, 2008 · N576FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200807263093Hmu · failedAPPROACHING CRUISE ALTITUDE GOT A LEVEL 2 'ENG 2 N2 LOW', FOLLOWED BY A ROLL BACK ON ENG 2. ALL INDICATIONS INDICATED FLAME OUT. ACCOMPLISHED QRH PROCEDURES AND LANDED WITHOUT INCIDENT. DID NOT ATTEMPT A RESTART. PERFORMED ENGINE POST-WINDMILLING INSP IAWJul 26, 2008 · N576FE · Doug MD11F · Engine Fuel DistributionSDR 08FDEA03093Hmu · failedAPPROACHING CRUISE ALTITUDE GOT A LEVEL 2 'ENG 2 N2 LOW' FOLLOWED BY A ROLL BACK ON ENG 2. ALL INDICATIONS INDICATED FLAME OUT. ACCOMPLISHED QRH PROCEDURES AND LANDED WITHOUT INCIDENT. DID NOT ATTEMPT A RESTART. PERFORMED ENGINE POST-WINDMILLING INSPECTIONJul 26, 2008 · N576FE · Doug MD11F · Fuel Controlling SystemSDR FDEA200807132873Battery · dischargedAFTER LEVEL OFF AT FL390, APPROX 20 MIN AFTER TAKEOFF GOT LVL 1 BATT LOW ALERT. DIVERTED TO KLAS BATTERY SHOWED AMBER BOXED. REMOVED AND REPLACED ACFT BATTERIES IAW AMM 24-34-02-4. PERF DC TIE BUSS OPS CHK. REMOVED AND REPLACED BATTERY CHARGER. REMOVED ANJul 13, 2008 · N576FE · Doug MD11F · Battery/Charger SystemSDR 08FDEA02873Battery · unknownAFTER LEVEL OFF AT FL390, APPROX 20 MIN AFTER T/O GOT LVL 1 BATT LOW ALERT. DIVERTED TO KLAS BATT SHOWED AMBER BOXED 8 OR 7. REMOVED AND REPLACED A/C BATTERIES IAW AMM 24-34-02-4. PERF DC TIE BUSS OPS CHECK. REMOVED AND REPLACED BATTERY CHARGER. REMOVED AJul 13, 2008 · N576FE · Doug MD11F · Battery/Charger SystemSDR 07FDEA02113Trunnion · corrodedCENTER LANDING GEAR LEFT TRUNNION FITTING AFT HOLE FOUND CORROSION. CENTER LANDING GEAR LEFT TRUNNION FITTING AFT HOLE REAMED TO DIAMETER = 1.385" AND REPAIRED AS PER FEDEX EA NR 1-5310-111115, TITLE: FUSELAGE, CENTER LANDING GEAR LEFT TRUNNION FITTING CORROSJun 13, 2007 · N576FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR 07FDEA02093Skin · corrodedTOP OF CENTER TANK RIGHT SIDE FOUND CORROSION AT STA 1219. CORROSION IN TOP OF CENTER TANK RIGHT SIDE AT STA 1219 CARRIED OUT REPAIR AS PER FEDEX EA NR 1-5710-111114, TITLE: WINGS, CENTER WING FUEL TANK RIGHT SIDE CORROSION REPAIR. REPAIR CLASSIFIED AS MAJJun 8, 2007 · N576FE · Doug MD11 · Wing, Plate/SkinSDR 07FDEA02053Skin · damagedCENTER CARGO DOOR AFT CUTOUT LOWER SKIN FOUND MATERIAL ABRASION. [06-12-07] DAMAGED AREA AT CENTER CARGO DOOR AFT CUTOUT LOWER SKIN TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 17 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 2, 2007 · N576FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 07FDEA02052Skin · damagedCENTER CARGO DOOR AFT CUTOUT LOWER SKIN FOUND MATERIAL ABRASION. [06-12-07] DAMAGED AREA AT CENTER CARGO DOOR AFT CUTOUT LOWER SKIN TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 17 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 2, 2007 · N576FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 07FDEA02015Spar · corrodedLEFT WING REAR SPAR, BETWEEN OUTBOARD ISLAND MOUNTING BRACKET NR 1 AND NR 2 FROM OUTBOARD, LOWER FACE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5710-111113. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 30, 2007 · N576FE · Doug MD11F · Wing SparSDR 07FDEA02014Support · crackedLEFT WING FIXED LEADING EDGE CAVITY INTERIOR UPPER FACE, XORS 562, SUPPORT STRIP FOUND CRACKED. REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5710-111112. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.May 29, 2007 · N576FE · Doug MD11 · Wing Main, Frame StructureSDR 07FDEA02013Skin · corrodedMAIN DECK L3 DOOR CUTOUT FORWARD LOWER CORNER FOUND CORRODED. MAIN DECK L3 DOOR CUTOUT FORWARD LOWER CORNER CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 18 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 29, 2007 · N576FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 07FDEA02012Skin · corrodedAPU - FUSELAGE SKIN EXTERIOR AT APU EXHAUST DOOR LOWER SIDE HINGE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5330-109892. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 29, 2007 · N576FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 07FDEA02011Skin · dentedFORWARD CARGO AFT LOWER CUTOUT SKIN FOUND DENT. [06-12-07] DENT AT FORWARD CARGO AFT LOWER DOOR CUTOUT SKIN TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 17 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 29, 2007 · N576FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 07FDEA01990Unknown · crackedLEFT WING FIXED LEADING EDGE TELESCOPING DUCT CUTOUT FOUND CRACKED. [06-12-07] REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE TELESCOPING DUCT CUTOUT AREA AS PER SRM 57-10-00 FIGURE 43 VOLUME I AND FEDEX E.A. 1-5730-109887. REPAIR CLASSIFIEDMay 27, 2007 · N576FE · Doug MD11F · Wing Main, Frame StructureSDR 05FDEA04195Rudder · damagedDURING AIRPLANE'S CONVERSION FROM P TO F, ACCIDENTAL DAMAGE LOWER AFT RUDDER. DURING BRAKE SYSTEM BLEED PROCURE WITH HYD PRESSURE AND LOCK PINS IMPROPERLY INSTALLED AN ERRONEOUS MANEUVER OF THE RUDDER PEDALS CAUSED SUDDEN MOVEMENT OF THE RUDDER TOUCHED THE WODec 9, 2005 · N576FE · Doug MD11 · Rudder StructureSDR 05FDEA03749Frame · crackedDURING PASSENGER TO FREIGHT COVERSION FOUND CRACK 1.20" LONG ON FRAME STA1305 BETWEEN LT 11 LT 12. DURING PASSENGER TO FREIGHT CONVERSION: FOUND CRACK 1.2" LONG ON FRAME STA 1305 RT SIDE BETWEEN L11 TO L12. TRIMOUT TIME CRACK WITH 0.5" RADIUS AND 2 REMAININGNov 10, 2005 · N576FE · Doug MD11 · Fuselage Main, FrameSDR 05FDEA03748Frame · crackedDURING PASSENGER TO FREIGHT CONVERSION: FOUND CRACK 1.2" LONG ON FRAME STA 1256 LT SIDE BETWEEN L11 TO L12. TRIMOUT TIME CRACK WITH 0.5" RADIUS AND 2 REMAINING FASTENERS. PERFORMED INSPECTION FOR CRACK, INSTALLED FILLER MT 7075T6 , INSTALLED REPAIR STRAP MATNov 10, 2005 · N576FE · Doug MD11 · Fuselage Main, FrameSDR 05FDEA01362Fitting · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 14 HAS BORE CORROSION EXCEEDING LIMITS. SPLICE FITTING REMOVED AND REPLACED IAW EO-1-5510-7-5000 REV D -PT1. MAJOR REPAIR PER GMM 6-2-100.May 18, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer Miscellaneous StructureSDR 05FDEA01356Skin · damagedLT WING LOWER SKIN, XORS 455, WITH EXISTING BLEND OUT. BLEND OUT AT LT WING LOWER SKIN, XORS 455 EVALUATED AND FOUND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 32 VOL I.May 17, 2005 · N576FE · Doug MD11 · Wing Main, Frame StructureSDR 05FDEA01309Skin · damagedAIR COND BAY AT STA 496-615 WITH EXISTING BLEND OUT. EXISTING BLENDOUT AT NR 2 AIR COND BAY DOOR STA 496-615 EVALUATED FOUND CARRIED OUT AS PER ATTACHED FAA FORM 8110-3. REPAIR CLASSIFIFED AS MAJOR PER GMM 6-2-100. EO-1-5100-7-5001 ACCOMLISHED.May 16, 2005 · N576FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 05FDEA01266Skin · damagedRT WING, INBD FLAP, EXTERIOR UPPER SURFACE MOST UPPER ABOUT 20 INCHES FROM INBD TO OUTBD, FOUND 1 EACH EXISTING REPAIR DOUBLER.May 13, 2005 · N576FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA01262Skin · damagedRIGHT WIN , DROOP LEADING EDGE, TOP SURFACE, FOUND WITH A EXISTING REPAIR DOUBLER AND EXISTING FASTENERS HEAD EMITTING RUST. REPAIRED IAW SRM 57-10-00 FIG. 26 VOL I.May 12, 2005 · N576FE · Doug MD11 · Leading Edge Devices
Back to N576FE