N614FE

Service difficulty reports · 388

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 = 'N614FE' 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 FDEA202408131116Computer · failedPDIS 614 22-10 5555 13AUG24 06:12 NRT FACT NO PROF ON TAKEOFF. R/I 13AUG24 07:54 NRT REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 4059001-908 POS: 2 SRL: 99030834 ON MPN: 4059001-908 CPN: 2211Aug 13, 2024 · N614FE · Doug MD11F · Autopilot SystemSDR FDEA202408121113Smoke Detector · failedAT BLOCK IN, GOT INTERMITTENT LVL 3 CABIN SMOKE WITH NO ACTUAL OTHER SMOKE INDICATIONS, NOR ANY SMOKE INDICATIONS FROM SENSORS ON AIR SYNOPTIC PAGE. NO FSS ACTIVATION. USED PAN PAN PAN. INDICATIONS WOULD QUICKLY APPEAR, LAST A FEW SECONDS, THEN GO OUT. Aug 12, 2024 · N614FE · Doug MD11F · Smoke DetectionSDR FDEA202305100842Transmitter · looseAFTER TAKEOFF RECEIVED AN MLG AURAL WARNING WITH MLG RAISED. HELD SPEED TO 240KTS & CONTINUED CLIMB. LEVELED AT 8K FT &CYCLED MLG. WITH MLG DOWN & LOCKED WARNING STOPPED. RAISED MLG & CONTINUED CLIMB TO FL230 & WARNING RETURNED AS MLG WAS RAISED. RETURNEMay 10, 2023 · N614FE · Doug MD11F · Trailing Flap Position Indicating SystemSDR FDEA202211112754Flange · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NUMBER SN10550000 REVISION C ON LEFT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FRNov 11, 2022 · N614FE · Doug MD11F · Vertical StabilizerSDR FDEA202210302698Hinge · wornCABIN-UPPER CARGO DOOR, DOOR HINGE FITTING (FUSELAGE SIDE) PART NUMBER ACA7223-1 FOUND 1ST TO 11TH LOBES FROM FORDWARD FOUND OUT OF LIMIT. LOBE HOLES NUMBER 1 TO NUMBER 11 FROM FORWARD AT CABIN - UPPER CARGO DOOR , DOOR HINGE FITTING REWORKED AND FOUND NUMOct 30, 2022 · N614FE · Doug MD11F · Fuselage, Door HingeSDR FDEA202210302697Hinge · wornCABIN- UPPER CARGO DOOR, DOOR HINGE FITTING FOUND 1ST TO 11TH LOBES FROM FORWARD FOUND OUT OF LIMITS. LOBE REWORKED AND FOUND NUMBER 1 TO NUMBER 5 HOLES EXCEED LIMIT. NUMBER 6 TO NUMBER 11 HOLES WITHIN LIMIT AS PER MD- 11 SRM52-30-16-1A FIGURE 101 SHEEOct 30, 2022 · N614FE · Doug MD11F · Fuselage, Door HingeSDR FDEA202210302696Hinge · wornCABIN-UPPER CARGO DOOR, DOOR HINGE FITTING PART NUMBER ACA7332-1 FOUND 1ST TO 9TH LOBES FROM FORWARD FOUND OUT OF LIMIT. LOBE HOLES NUMBER 1 TO NUMBER 9 FROM FORWARD AT CABIN-UPPER CARGO DOOR. DOOR HINGE FITTING PART NUMBER ACA7332-1 REWORKED AS PER MD-11 Oct 30, 2022 · N614FE · Doug MD11F · Fuselage, Door HingeSDR FDEA202210262672Floor Panel · delaminatedCABIN - UPPER CARGO FLOOR PANEL #231HF FOUND DELAMINATED BETWEEN STATION 595 TO STATION 675 CABIN - UPPER CARGO , DELAMINATED FLOOR PANEL #231HF BETWEEN STATION 595 TO STATION 675 REMOVED AND REPLACED AS PER AMM 53-21-04-4. FLOOR PANEL #231HF FABRICATED Oct 26, 2022 · N614FE · Doug MD11F · Fuselage Floor PanelSDR FDEA202210262671Floor Panel · delaminatedCABIN FLOOR PANEL #262LF FOUND DELAMINATED FROM STATION 1321 TO STATION 1361. CABIN - DELAMINATED FLOOR PANEL #262LF FROM STATION 1321 TO STATION 1361 REMOVED AND REPLACED AS PER AMM 53-21-04-4. FLOOR PANEL #262LF FABRICATED AS PER FEDEDX DRAWING SRZ-25-00Oct 26, 2022 · N614FE · Doug MD11F · Fuselage Floor PanelSDR FDEA202210112549Beam · crackedCABIN - R3 DOOR #7 STOP BEAM FOUND CRACK. CABIN AT R3 DOOR CRACKED #7 BEAM REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. ORIG SUB DATE: 10/11/2022Oct 11, 2022 · N614FE · Doug MD11F · Service DoorsSDR FDEA202210102527Frame · crackedEMPENNAGE: WHILE ACCOMPLISHING INSPECTION, ZONE 360 RIGHT SIDE FRAME FOUND CRACKED. FRAME REMOVED AND REPLACED PER MD-11 SRM 51-31-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. FRAME FABRICATED IAW DRAWING AJC7593 REVISION Z.Oct 10, 2022 · N614FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA202210102526Frame · crackedEMPENNAGE: WHILE ACCOMPLISHING INSPECTION, ZONE 360 LEFT HAND SIDE FRAME FOUND CRACKED. FRAME REMOVED AND REPLACED IAW SRM 51-31-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. FRAME FABRICATED IAW DRAWING AJC7593 REVISION Z.Oct 10, 2022 · N614FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA202210062487Anchor Fitting · corroded: AFT ACCESSORY COMPARTMENT, LONGERON - 33 RIGHT TO LONGERON - 35 RIGHT, ATTACHMENT ANCHOR NUT SURROUNDING AREA FOUND WITH CORROSION. ANCHOR NUT AREA AT AFT ACCESSORY COMPARTMENT, LONGERON - 33 RIGHT TO LONGERON - 35 RIGHT, STATION 2144 TO STATION 2164 REOct 6, 2022 · N614FE · Doug MD11F · Fuselage Main, Attach FittingsSDR FDEA202210062486Fitting · damagedTO CARRY OUT BANJO FORWARD AND AFT FITTING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION AT STATION 2164. REPAIR CARRIED OUT ALONG STATION 2164 RIGHT HAND BANJO FITTING FORWARD AND AFT FLANGE AREA IAW EA 1-5530-T0313159 B P4. REPAIR CLASSIFIED AS MAJOR IOct 6, 2022 · N614FE · Doug MD11F · Vertical Stabilizer, Attach FittingsSDR FDEA202210062485Fitting · crackedWHILE ACCOMPLISHING LEFT HAND BANJO FORWARD FITTING INSPECTION, FOUND LEFT HAND BANJO AFT FITTING SUSPECTED CRACK AT STATION 2164. LEFT HAND BANJO FITTING FORWARD AND AFT FLANGE AREA REPAIR CARRIED OUT PER E.A #: 1-5530-T0313159 B P4. REPAIR CLASSIFIED AOct 6, 2022 · N614FE · Doug MD11F · Vertical Stabilizer, Attach FittingsSDR FDEA202210052464Floor Support · corrodedLOWER CENTER CARGO COMPARTMENT STATION 1841 WEB LOWER FLOOR SUPPORT FOUND WITH CORROSION. LOWER CENTER CARGO COMPARTMENT STATION 1841 WEB , CORROSION AT LOWER FLOOR SUPPORT EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 202 ROct 5, 2022 · N614FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA202210052467Stringer · crackedCENTER UPPER AUX TANK - STRINGER 47 AT XCW 48 FOUND CRACK. REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 5, 2022 · N614FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA202210052466Stringer · crackedCENTER UPPER AUX TANK - STRINGER 47 AT STATION XCW - 17 FOUND CRACK. REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 5, 2022 · N614FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA202210052465Stringer · crackedCENTER UPPER AUX TANK - STRINGER 47 AT XCW 19 FOUND CRACK. CENTER UPPER AUX TANK STRINGER 47 AT XCW 19 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 5, 2022 · N614FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA202210012437Doubler · corrodedLEFT WING Ï¿½ UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER AT XORS 283 FOUND CORROSION. LEFT WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN AUX SPAR AND YW 467 AREA CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SOct 1, 2022 · N614FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA202210012436Skin · crackedLEFT WING Ï¿½ FIXED LEADING EDGE NUMBER 12 SLAT TRACK CUTOUT CORNER AT XOS 776.5 FOUND CRACK. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 1, 2022 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202210012435Doubler · crackedLEFT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT XOS 906 FOUND CRACK.Oct 1, 2022 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202210012434Doubler · crackedLEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 FOUND CRACK.Oct 1, 2022 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202210012433Doubler · crackedLEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 655 FOUND CRACK.Oct 1, 2022 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202210012432Doubler · crackedLEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 544 FOUND CRACK.Oct 1, 2022 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202210012431Doubler · crackedRIGHT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 655 FOUND CRACK.Oct 1, 2022 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202210012430Doubler · crackedRIGHT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 789 FOUND CRACK.Oct 1, 2022 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202210012428Floor Support · corrodedLOWER CENTER CARGO COMPARTMENT STATION 1841 WEB UPPER FLOOR SUPPORT FOUND WITH CORROSION. LOWER CENTER CARGO COMPARTMENT STATION 1841 WEB , CORROSION AT UPPER FLOOR SUPPORT EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 202 Oct 1, 2022 · N614FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA202209292385Spar Cap · corrodedRIGHT WING TRAILING EDGE REAR SPAR LOWER CAP AT XORS 1078 FOUND CORROSION. RIGHT WING TRAILING EDGE REAR SPAR LOWER CAP AT XORS 1078 CORROSION REMOVED AND FOUND EXCEED LIMITS IAW SRM 57-00-10-1A ALLOWABLE DAMAGE 1 FIG 101. CORRODED LOWER REAR SPAR CAP AT XOSep 29, 2022 · N614FE · Doug MD11F · Wing SparSDR FDEA202206211479Floorboard · delaminatedFLOOR PANEL L/H 253DF IS DELAM WITH LARGE HOLE. FABRICATED NEW MAIN DECK FLOOR BOARD PANEL # 253DF PER FEDEX DRWG SRZ-25-005 ADA8396.. (MAJOR REPAIR)Jun 21, 2022 · N614FE · Doug MD11F · Fuselage Floor PanelSDR FDEA202205081153Windshield · crackedPDIS 614 56-10 2933 06MAY22 YYZ OPEN U RIGHT WINDSHIELD CRACKED DUE TO ARCING. TURNED OFF WINDSHIELD HEAT. STOPPED CRACKING. FACT 08MAY22 22:56 YYZ REPLACED R/H WINDSHIELD PANEL ASSY I.A.W WITH MD11 AMM 56-11-01-4-1.May 8, 2022 · N614FE · Doug MD11F · Flight Compartment WindowsSDR FDEA202107291887Tire · underservicedRECEIVED LVL 2 TIRE FAIL FOR #3 TIRE TIRE PRESSURE LEAKED OUT AFTER TAKE OFF. T/S PER FIM 32-40-00-2 FIG 119, TIRE #3 BELOW 50PSI. REMOVED AND REPLACED #3 AND #4 TIRES REF AMM 32-41-01-4. PRESSURE CHECK GOOD.Jul 29, 2021 · N614FE · Doug MD11F · TireSDR FDEA202011172884Finger Doubler · delaminatedRIGHT WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD SKIN LOWER SURFACE FINGER DOUBLER AT XW 385 FOUND DELAMINATION. RIGHT WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD SKIN LOWER SURFACE FINGER DOUBLER AT XW 385 REPAIR CARRIED OUT, AS PER SRM 57-50-01-2RNov 17, 2020 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202011082793Skin · crackedWING, LEFT HAND WING FIXED LEADING EDGE LOWER SKIN AT SLAT TRACK NUMBER 14 CUT OUT OUTBOARD STATION XOS 892 FOUND CRACK WING LEFT HAND WING FIXED LEADING EDGE LOWER SKIN AT SLAT TRACK NUMBER 14 CUT OUT OUTBOARD STATION XOS 892. REPAIR CARRIED OUT, AS PER SRM Nov 8, 2020 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202011082792Doubler · delaminatedLEFT WING, TRAILING EDGE INBOARD ISLAND UPPER FORWARD SKIN LOWER SURFACE FINGER DOUBLER AT XW 383 FOUND DELAMINATION. LEFT WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD SKIN LOWER SURFACE FINGER DOUBLER AT XW 383. REPAIR CARRIED OUT, AS PER SRM 57-50-01-Nov 8, 2020 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202011082795Former · crackedWING LEFT HAND WING FIXED LEADING EDGE COMPARTMENT XOS 584 FORMER ASSEMBLY FOUND CRACK.Nov 8, 2020 · N614FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA202011082794Doubler · crackedWING LEFT HAND WING FIXED LEADING EDGE COMPARTMENT XOS 667 DOUBLER FOUND CRACK.Nov 8, 2020 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202011052775Trunnion · crackedCRACK INDICATION FOUND APPROXIMATELY 0.125 INCHES IN LENGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND SIDE NOSE LANDING GEAR TRUNNION FITTING EXISTING TRIM OUT AT STATION 583. LEFT HAND SIDE NOSE LANDING GEAR TRUNNION FITTING EXISTING TRINov 5, 2020 · N614FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA202011052781Seat Track · wornMAIN DECK CARGO COMPARTMENT CABIN, FOUND SEAT TRACK AT STATION 760, X= -47.5 CROWN WORN. MAIN DECK CARGO COMPARTMENT CABIN AT SEAT TRACK STATION 760, X= -47.5, WORN CROWN EVALUATED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE Nov 5, 2020 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202011042770Seat Track · wornMAIN DECK CARGO COMPARTMENT CABIN, FOUND SEAT TRACK AT STATION 1018, X= -8.5 CROWN WORN. MAIN DECK CARGO COMPARTMENT CABIN AT SEAT TRACK STATION 1018, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.Nov 4, 2020 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202011042769Seat Track · wornMAIN DECK CARGO COMPARTMENT CABIN, FOUND SEAT TRACK AT STATION 1060, X=47.5 CROWN WORN. MAIN DECK CARGO COMPARTMENT CABIN AT SEAT TRACK STATION 1060, X=47.5 WORN. CROWN EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.Nov 4, 2020 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2019121323225Terminal · damagedAPPROX 20 MIN AT CRUISE, FL 360, APU FIRE LIGHT ILLUMINATED WITH TRI-TONE ALERT FIRE BELL. APU WAS NOT OPERATING. PULLED APU FIRE HANDLE & ROTATED. PER QRH, WAITED 30 SECS, TRI-TONE ALERT CAME BACK ON & FIRE HANDLE REMAINED ILLUMINATED. MANIPULATING WIREDec 12, 2019 · N614FE · Doug MD11F · Smoke DetectionSDR FDEA201909242335Flex Line · failedAFTER APPROXIMATELY 30MIN OF FLIGHT WE HEARD A LOUD EXCAPING OF AIR COMING FROM THE COURRIER SECTION. WE NOTICED THAT THE O2 SYSTEM READINGS ON SYSTEM 1 & 3 WERE DECREASING, #2 REMAINED @ 2000 PSI. NO AIR WAS AVAILABLE THROUGH THE OXYGEN MASKS IN THE COURRIESep 24, 2019 · N614FE · Doug MD11F · Crew Oxygen SystemSDR FDEA201904160809Warning Light · illuminatedEMER LT BAT 1 LO DURING PREFLIGHT.Apr 16, 2019 · N614FE · Doug MD11F · Emergency LightingSDR FDEA2018091192424Floor Support · corrodedMDCC AFT FLOOR SUPPORT FOUND CORROSION AT STA 2007 X =-25. CORROSION REMOVED PER SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT PER SRM 53-00-00-2R FIG 202. ORIGINAL THK 0.080", MATERIAL REMOVED 0.060", REMAINING THK 0.020". CORRODED FLOOR SUPPORT REMOVED PER AMM 20Sep 9, 2018 · N614FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2018091172417Fitting · corrodedLT O/B FLAP VANE HORN FITTING 'F' HOLE BORE CORROSION. BORE REWORKED AND FOUND EXCEED LIMIT PER SRM 57-50-02-2R FIG 201 SHEET 1. EXISTING SLOT HOLE: LENGTH 0.852", WIDTH 0.600", FINAL SLOT HOLE: LENGTH 0.960", WIDTH 0.708". REPAIR LIMIT - LENGTH 0.940", WIDTH Sep 7, 2018 · N614FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2018091172416Fitting · corrodedLT O/B FLAP VANE HORN FITTING 'E' HOLE BORE CORROSION. BORE REWORKED AND FOUND EXCEED LIMIT PER SRM 57-50-02-2R FIG 201 SHT 1. EXISTING SLOT HOLE: LENGTH 0.857", WIDTH 0.581", FINAL SLOT HOLE: LENGTH 0.952", WIDTH 0.652". REPAIR LIMIT - LENGTH 0.940", WIDTH 0.Sep 7, 2018 · N614FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2018091172415Bracket · corrodedLT WING I/B FLAP I/B DRIVE LINK IDLER BRACKET BORE CORROSION. DRIVE LINK IDLER BRACKET BORE REWORKED PER CMM 57-52-03. EXISTING HOLE DIA 1.00", FINAL HOLE DIA 1.316". REPLACEMENT BUSHING FOR ARC3087-1 & ARC3086-1 FABRICATED PER EA 1-5750-T0342037 P1 STEP 4, 4ASep 7, 2018 · N614FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2018091172414Hinge · corrodedLT WING O/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA: 1.148' FINAL HOLE DIA: 1.163" MAXIMUM ALLOWABLE HOLE: 1.150" OVERSIZED BUSHING FABRICATESep 7, 2018 · N614FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2018091172413Hinge Bracket · corrodedLT WING O/B FLAP I/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.158", MAXIMUM ALLOWABLE HOLE DIA 1.150". OVERSIZED BUSHING FABRICATSep 7, 2018 · N614FE · Doug MD11F · Trailing Edge Flaps
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