N603FE

Service difficulty reports · 488

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 = 'N603FE' 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 FDEA2019052851158Pump · leakingIN FLIGHT GOT LEVEL 1 "HYDRA. 2 OFF" ALERT. COMPLIED WITH QRH PROCEDURE AND ALSO REVIEWED THE REFERENCED "HYD. 2 FAIL" QRH PROCEDURE. THE "HYDR. 2 FAIL" ALERT APPEARED DURING CONFIG ON APPROACH. SINCE WE ALREADY REVIEWD THE PROCEDURE, AND WE HAD NO DEGRAMay 25, 2019 · N603FE · Doug MD11F · Hydraulic Pump (Electric/Engine), MainSDR FDEA201903110568Transducer · failedON CLIMB OF APPROXIMATELY FL220 LEVEL 1 TIRE PRESSORE LOW, WARNING ILLUMINATED. CONSULTED QRH AT APPROXIMATELY 290 RECEIVED LEVEL 2 TIRE FAIL ALERT. CONSULTED QRH AND CONTINUED TO TPE. NORMAL APPROACH AND LANDING WITH ASSITANCE FROM RUNWAY AND LOCAL EMERGENCY Mar 11, 2019 · N603FE · Doug MD11F · TireSDR FDEA2018092542661Skin · crackedDURING HIGHFREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON RIGHT HAND WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUT OUT FOUND HOLE #7, #33, #34 AND #36 WITH CRACK INDICATION. (AT BETWEEN STA XORS 690 AND STA XORS 700 ). RIGHT HAND WING LOWSep 24, 2018 · N603FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201809202614Skin · corrodedEMPENNAGE - AFT ACCESSORY COMPARTMENT, RIGHT HAND SURFACE AREA FOUND SKIN CORROSION AROUND ANCHOR NUT AT STA Y = 2159 TO Y = 2149. LONGERON 33 RIGHT TO LONGERON 35 RIGHT. AFT ACCESSORY COMPARTMENT, RIGHT HAND SURFACE AREA SKIN CORROSION AROUND ANCHOR NUT AT STSep 20, 2018 · N603FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201809192586Floor Support · corrodedMAIN DECK CARGO FLOOR SUPPORT FOUND WITH CORROSION AT STA 1902 X = 57. FLOOR SUPPORT CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. ORIGINAL THICKNESS: 0.188 INCH MATERIAL REMOVED: 0.100 INCH, REMAINING THICKNESS: 0.088 INCH. FSep 19, 2018 · N603FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2018092092585Former · crackedLEFT HAND WING LEADING EDGE CAVITY FORMER AT STA XOS 1025 FOUND CRACKED. FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG AND 51-33-01-OG. FORMER PART NUMBER ARB2920-13 FABRICATED AS PER DRAWING ARB2920 REVISION BB. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-1Sep 19, 2018 · N603FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA2018092092584Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 655. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 19, 2018 · N603FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018092092583Doubler · crackedRIGHT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 543. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.Sep 19, 2018 · N603FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018092092582Doubler · crackedRIGHT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 626. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 19, 2018 · N603FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201809182564Frame · chafedCABIN MAIN DECK CARGO COMPARTMENT FRAME CHAFED AT RIGHT HAND STA 535 LONGERON 19 RIGHT. FRAME REPAIR AS PER SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 18, 2018 · N603FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201809182563Frame · chafedCABIN MAIN DECK CARGO COMPARTMENT FRAME CHAFED AT RIGHT HAND STA 535, LONGERON 24 RIGHT. FRAME REPAIR AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 18, 2018 · N603FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201809182570Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 763. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 18, 2018 · N603FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201809182569Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 618. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 18, 2018 · N603FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201809182568Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 612. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 18, 2018 · N603FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201809182567Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 626. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 18, 2018 · N603FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201809092426Battery · dischargedR1 EVACUATION SLIDE REMOTE PRESSURE PRESS-TO TEST INDICATION SYSTEM IS INOP ON PREFLIGHT CHECK. R1 EVAC SLIDE REMOTE PRESS INDICATOR INOP. TRIED TO REPLACE IND KIT (26C17528-2) BUT NO HELP. FOUND R1 EVACUATION SLIDE REMOTE PRESSURE PRESS-TO TEST INDICATION Sep 9, 2018 · N603FE · Doug MD11F · Escape SlideSDR FDEA201808071943Warning Message · illuminatedEMERGENCY LIGHT BATTERY 1 LOW ALERT DURING TEST.Aug 7, 2018 · N603FE · Doug MD11F · Emergency LightingSDR FDEA201807221805Light · inoperativeSLIDE BOTTLE TEST LIGHT INOP ON L1 DOOR. R&R BULBS ON SLIDE BOTTLE TEST LIGHT ON L1 DOOR & OPS CHECKED GOOD REF AMM 25-61-04-4.Jul 22, 2018 · N603FE · Doug MD11F · Escape SlideSDR FDEA2018091401208Hydraulic Line · failedHYD 1 FAIL, QTY 0.0. REMOVED AND REPLACED NR 1 ENGINE LEFT PUMP (UPPER) PRESSURE HOSE ASSY REF AMM 20-40-01-2.May 10, 2018 · N603FE · Doug MD11F · Hydraulic System, MainSDR FDEA201801160099Hinge · wornFOUND TWO LOBES ON HINGE BEYOND SRM LIMITS EA T1-5310-T0337841 PT1 WAS ISSUED AND COMPLIED WITH.Jan 16, 2018 · N603FE · Doug MD11F · Fuselage, Door HingeSDR FDEA201701110123Anti-Ice System · malfunctionedLEVEL 1 ALERT "A-ICE SENSOR FAIL" AT FL350. STAYED ON FOR REMAINDER OF FLIGHT. IDENTIFIED PARTS, (W/KIT) PNEUMATIC PRESSURE. UPGRADED PNEU SYSTEM. CFDS SENSOR READOUT, PSC 1 SHOWED PE1 XXXX AND PSC 2 SHOWED PE1B XXXX. READINGS RETURN TO NORMAL AFTER PSC 1 Jan 11, 2017 · N603FE · Doug MD11F · Air Intake Anti/De-Ice SystemSDR FDEA201611284261Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329456A P1, STEP 1F.Nov 28, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611264246Hinge Fitting · corrodedLEFT WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. A WASREPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-72644C PART 2 STEP 1.F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 26, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234230Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE SURFACE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234229Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1C.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234228Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1C.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234227Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) UPPER MOUNT INBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1A.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234226Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1B.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234221Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1C.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234220Hinge Bracket · corrodedLEFT WING OTBD, FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09, A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1C.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234219Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1A AND DTEP 1.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234218Hinge Bracket · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1A AND 1.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234217Hinge Bracket · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1B.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234225Hinge Bracket · corrodedRIGHT WING OUTBD FLAP, INBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO329708 PART 1STEP 1A AND STEP 1.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234224Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-7-TO329708 PART 1 STEP 1A AND STEP 1.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234223Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR OTBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO329708 PART 1 STEP 1A AND STEP 1.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234222Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO329708 PART 1STEP 1B AND STEP 1.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234216Hinge Bracket · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE FOUND WITH CORROSION. FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1C.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234215Hinge Fitting · corrodedRIGHT WING, FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE FOUND CORRODED.Nov 23, 2016 · N603FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR FDEA201611234214Hinge Bracket · corrodedRIGHT WING - OUTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE FOUND WITH CORROSION. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-70329763 PART 1 STEP 1B.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234213Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD FWD HINGE (WING SIDE) BARREL NUTS HOLE BORE CORROSION. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1D.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234212Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD FWD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE FOUND WITH CORROSION. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0329763. PART 1 STEP 1B.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234211Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE FOUND WITH SURFACE CORROSION. REPAIR SHIM FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234210Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE SURFACE CORROSION. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234209Hinge Bracket · corrodedRIGHT WING, OUTBD FLAP OTBD FWD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750- T0329763 PART 1 STEP 1A AND STEP 1.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611234208Hinge Bracket · corrodedRIGHT HAND WING - OUTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750- T0329763 PART 1 STEP 1A AND STEP 1.Nov 23, 2016 · N603FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201611184087Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-72651C PART 5 STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6Nov 18, 2016 · N603FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201611184086Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE FOUND WITH CORROSION. FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-72651C PART 5 STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR INov 18, 2016 · N603FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201611184085Vane · corrodedLEFT WING OUTBOARD FLAP VANE FITTING, BUSHING HOLE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIG 201. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-100680A PART 2 STEP 1E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 18, 2016 · N603FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201611184084Vane · corrodedLEFT WING OUTBOARD FLAP VANE FITTING BUSHING HOLE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIG 201. A NEW BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-100680A PART 2 STEP 1E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 18, 2016 · N603FE · Doug MD11F · Trailing Edge Flaps
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