# Service difficulty reports: N601FE

A list on [N601FE](https://openairdocs.org/aircraft/N601FE.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 11 · 546 reports

- [SDR FDEA202203300758](https://openairdocs.org/sdr/FDEA202203300758.md): Valve · failed · Mar 30, 2022 · N601FE · Doug MD11F · Landing Gear Retraction/Extension System
  > PDIS 601 32-30 3967 30MAR22 OAK OPEN U AFTER ROTATION ON TAKEOFF AND CALLING FOR GEAR UP, GEAR HANDLE EXTREMELY DIFFICULT TO MOVE STARTING ABOUT A THIRD THROUGH THE RANGE OF TRAVEL. GOT THE GEAR HANDLE TO MOVE TO THE UP POSITION WITH 20-30
- [SDR FDEA202202250370](https://openairdocs.org/sdr/FDEA202202250370.md): None · leaking · Feb 25, 2022 · N601FE · Doug MD11F · Hydraulic Power System
  > PDIS 601 29-02 3869 24FEB22 HNL FACT U HYD 3 ELEV OFF LEVEL 1 APPROX 10 MINUTES AFTER TAKEOFF. HYD 3 LEVEL AT 4.0 AND DECREASING. THEN MOMENTARY HYD 3 OFF LEVEL 1 FOLLOWED BY HYD 3 FAIL LEVEL 2 WITH HYD 3 AT 0.0. COMPLIED WITH QRH, RETURNED T
- [SDR FDEA202112063000](https://openairdocs.org/sdr/FDEA202112063000.md): None · none · Dec 6, 2021 · N601FE · Doug MD11F · Cargo/Baggage Doors
  > UPPER CARGO DOOR,FOUND DOOR SIDE HINGE PART NUMBER ACA7223-523 WITH 18 LOBES WORN. WORN 18 LOBES AT UPPER CARGO DOOR, DOOR SIDE HINGE PART NUMBER ACA7223-523 REWORKED AND FOUND #1 TO #7 LOBE HOLES EXCEED LIMIT AS PER MD-11 SRM 52-30-16-1A FIGURE 101 SHEE
- [SDR FDEA202112022957](https://openairdocs.org/sdr/FDEA202112022957.md): None · none · Dec 2, 2021 · N601FE · Doug MD11F · Fuselage Main, Plate/Skin
  > AGING AIRCRAFT - EXISTING REPAIR AT FWD CARGO DOOR CUTOUT - AFT JAMB SKIN EXTERIOR STATION 1009, LONGERON 39 RIGHT HAND TO 41 RIGHT HAND. EXISTING REPAIR AT FWD CARGO DOOR CUTOUT - AFT JAMB SKIN EXTERIOR STATION 1009, LONGERON 39 RIGHT HAND TO 41 RIGHT HAN
- [SDR FDEA202112022969](https://openairdocs.org/sdr/FDEA202112022969.md): Skin · cracked · Dec 2, 2021 · N601FE · Doug MD11F · Fuselage Main, Structure
  > MAIN DECK R3 DOOR CUTOUT FORWARD JAMB UPPER SKIN CRACKED AT STATION 1256.750 MAIN DECK AT R3 DOOR CUTOUT FORWARD JAMB CRACKED UPPER SKIN AT STATION 1256.750 REPAIRED AS PER E.A.#: 1-5310-T0365682 P1, TITLE: FUSELAGE - MAINFRAME - CRACK REPAIR FOR R3 CENTE
- [SDR FDEA202111262933](https://openairdocs.org/sdr/FDEA202111262933.md): None · none · Nov 26, 2021 · N601FE · Doug MD11F · Wing, Control Surfaces
  > AGING AIRCRAFT - EXISTING REPAIR AT RIGHT HAND WING INBOARD FLAP LOWER SURFACE INBOARD LOWER SEGMENT SKIN STATION XIFH 139. EXISTING REPAIR AT RIGHT HAND WING INBOARD FLAP LOWER SURFACE INBOARD LOWER SEGMENT SKIN STATION XIFH 139 EVALUATED AND FOUND NOT RE
- [SDR FDEA202111262934](https://openairdocs.org/sdr/FDEA202111262934.md): None · none · Nov 26, 2021 · N601FE · Doug MD11F · Passenger/Crew Doors
  > AGING AIRCRAFT - EXISTING REPAIR AT #1 LEFT PASSENGER DOOR SKIN UPPER AFT CORNER STATION 457. EXISTING REPAIR AT #1 LEFT PASSENGER DOOR SKIN UPPER AFT CORNER STATION 457 EVALUATED AND FOUND REPAIRED NOT IAW SRM 52-10-01-2R REPAIR 3 FIGURE 201. REPAIR CAR
- [SDR FDEA202111242927](https://openairdocs.org/sdr/FDEA202111242927.md): None · none · Nov 24, 2021 · N601FE · Doug MD11F · Fuselage Main, Plate/Skin
  > LOWER CENTER CARGO COMPARTMENT DOORWAY DOOR CUT OUT STATION 1707, X= -52 FLANGE FOUND WITH CORROSION. LOWER CENTER CARGO COMPARTMENT DOORWAY DOOR CUT OUT CORROSION AT STATION 1707, X= -52 WORK COMPLIED AS PER EA # 1-5310-T0365753 P1 TITLE: FUSELAGE MAINFRA
- [SDR FDEA202111212912](https://openairdocs.org/sdr/FDEA202111212912.md): Support · cracked · Nov 21, 2021 · N601FE · Doug MD11F · Wing, Control Surfaces
  > RIGHT WING - OUTER FLAP INBOARD HINGE TENSION STRAP AT STATION XORS 580 FOUND CRACK. CRACKED TENSION STRAP REMOVED AND REPLACED AT STATION XORS 580 AS PER SRM 51-33- 01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. FUEL LEAK CHECK CARRIED OUT AT RIGHT W
- [SDR FDEA202111212914](https://openairdocs.org/sdr/FDEA202111212914.md): Intercostal · corroded · Nov 21, 2021 · N601FE · Doug MD11F · Fuselage Miscellaneous Structure
  > AFT OF FORWARD AVIONICS COMPARTMENT 01 EACH INTERCOSTAL AT STATION 426.438 X=2.375 FOUND CORRODED. AFT OF FORWARD AVIONICS COMPARTMENT AT STATION 426.438 X=2.375 INTERCOSTAL CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 REPAI
- [SDR FDEA202111212913](https://openairdocs.org/sdr/FDEA202111212913.md): Intercostal · corroded · Nov 21, 2021 · N601FE · Doug MD11F · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND ON THE INTERCOSTAL AFT OF THE FORWARD AVIONICS COMPARTMENT (FAC) STATION 426.438, X= -2.375. AFT OF FORWARD AVIONICS COMPARTMENT AT STATION 426.438 X=-2.375 INTERCOSTAL CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FI
- [SDR FDEA202111172873](https://openairdocs.org/sdr/FDEA202111172873.md): Beam · cracked · Nov 17, 2021 · N601FE · Doug MD11F · Fuselage Main, Structure
  > LOWER CENTER CARGO COMPARTMENT STATION 1741, X=0 FLOOR BEAM FOUND WITH CRACK. LOWER CENTER CARGO COMPARTMENT STATION 1741, X=0 CRACKED FLOOR BEAM REPAIRED AS PER EA#1-5321-T0365615 PART 1. TITLE: FUSELAGE - CARGO COMP FLOORS - LOWER CENTER CARGO FLOOR BEAM
- [SDR FDEA202111172870](https://openairdocs.org/sdr/FDEA202111172870.md): Beam · none · Nov 17, 2021 · N601FE · Doug MD11F · Fuselage Main, Structure
  > AGING AIRCRAFT - EXISTING REPAIR AT LOWER CENTER CARGO COMPARTMENT STATION 1701, X = 24 FLOOR BEAM. EXISTING REPAIR AT LOWER CENTER CARGO COMPARTMENT STATION 1701, X = 24 FLOOR BEAM EVALUATED AND FOUND NOT REPAIRED IAW SRM 53-00-00-2R FIGURE 203. EXISTI
- [SDR FDEA202111172875](https://openairdocs.org/sdr/FDEA202111172875.md): Floor Support · corroded · Nov 17, 2021 · N601FE · Doug MD11F · Fuselage Miscellaneous Structure
  > LOWER AFT CARGO COMPARTMENT STATION 1841, X= 18 WEB FLOOR SUPPORT FOUND WITH CORROSION. LOWER AFT CARGO COMPARTMENT STATION 1841 X= 18 WEB FLOOR SUPPORT CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 REPAIR GENERAL. CORRODED
- [SDR FDEA202111172874](https://openairdocs.org/sdr/FDEA202111172874.md): Doubler · cracked · Nov 17, 2021 · N601FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 669 FOUND CRACK. LEFT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 669 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202111172872](https://openairdocs.org/sdr/FDEA202111172872.md): Doubler · cracked · Nov 17, 2021 · N601FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 655 FOUND CRACK. LEFT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 655 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202111172871](https://openairdocs.org/sdr/FDEA202111172871.md): Doubler · cracked · Nov 17, 2021 · N601FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 613 FOUND CRACK. LEFT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 613 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202111162865](https://openairdocs.org/sdr/FDEA202111162865.md): None · none · Nov 16, 2021 · N601FE · Doug MD11F · Wing, Plate/Skin
  > AGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 647. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 647 EVALUATED AND FOUND DOUBLER CRACKED AND NOT REPAIRED PER SRM 57-40-02-
- [SDR FDEA202111162864](https://openairdocs.org/sdr/FDEA202111162864.md): None · none · Nov 16, 2021 · N601FE · Doug MD11F · Wing, Plate/Skin
  > AGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 637. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 637 EVALUATED AND FOUND DOUBLER CRACKED AND NOT REPAIRED PER SRM 57-40-02
- [SDR FDEA202111162863](https://openairdocs.org/sdr/FDEA202111162863.md): None · none · Nov 16, 2021 · N601FE · Doug MD11F · Wing, Plate/Skin
  > AGING AIRCRAFT- EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 631. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 631 EVALUATED AND FOUND DOUBLER CRACKED AND NOT REPAIRED PER SRM 57-40-02-2
- [SDR FDEA202111122832](https://openairdocs.org/sdr/FDEA202111122832.md): None · none · Nov 12, 2021 · N601FE · Doug MD11F · Passenger/Crew Doors
  > MAIN DECK #L3 PLUG DOOR AFT UPPER #1 BEAM FOUND CRACKED.
- [SDR FDEA202111122834](https://openairdocs.org/sdr/FDEA202111122834.md): Track · cracked · Nov 12, 2021 · N601FE · Doug MD11F · Fuselage Floor Panel
  > MAIN DECK SEAT TRACK AT STATION 755 X = - 8.5 FOUND CROWN CRACKED. MAIN DECK AT STATION 755, X = - 8.5 CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES FROM STATION 745 TO STATION 785 X = - 8.5 AS PER SRM 53-00-52-2R REP
- [SDR FDEA202111122833](https://openairdocs.org/sdr/FDEA202111122833.md): Track · cracked · Nov 12, 2021 · N601FE · Doug MD11F · Fuselage Floor Panel
  > MAIN DECK SEAT TRACK AT STATION 629, X = - 47.5 CROWN CRACKED. MAIN DECK AT STATION 629, X = - 47.5 CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES FROM STATION 625 TO STATION 685, X = - 47.5 AS PER SRM 53-00-52-2R RE
- [SDR FDEA202111112816](https://openairdocs.org/sdr/FDEA202111112816.md): None · none · Nov 11, 2021 · N601FE · Doug MD11F · Fuselage Main, Structure
  > AGING AIRCRAFT- EXISTING REPAIR AT LOWER AFT CARGO COMPARTMENT WEB STATION 1841, X=-10 AND X=-45. EXISTING REPAIR AT LOWER AFT CARGO COMPARTMENT WEB STATION 1841, X=-10 AND X=-45 EVALUATED AND FOUND NOT REPAIRED IAW SRM 53-00-00-2R FIGURE 211 REPAIR GENERA
- [SDR FDEA202107241888](https://openairdocs.org/sdr/FDEA202107241888.md): Fitting · corroded · Jul 24, 2021 · N601FE · Doug MD11F · Trailing Edge Flaps
  > LH OB FLAP INBD HINGE FAIRING MOUNTING BOLT HOLES TO FLAP, 4 OF 6 SHOW SIGNS OF CORROSION. LH OB HINGE WAS REPAIRED PER MD11 CMM 57-50-04 AND EA 1-5750-T363229 LH OUTBOARD TRAILING EDGE HINGE SUPPORT FITTING-REPAIR OF CORROSION AT FLAP ATTACHMENT SURFACE A
- [SDR FDEA202105091163](https://openairdocs.org/sdr/FDEA202105091163.md): Gland Nut · leaking · May 9, 2021 · N601FE · Doug MD11F · Hydraulic System, Main
  > HYD 3 OFF AT FL 340. FLUID AT 2.5 THEN DROP TO 2.1. HYD 3 FAIL CAME ON AFTER GEAR EXTENSION. FLUID DROP TO.9. FOLLOWED QRH FOR HYD 3 FAIL. RH MLG SWIVEL GLAND, AND MAIN LANDING GEAR RETRACT CYLINDER. OPS CK AND LEAK CK OK REF MD11 MM 32-33-21-4, MD1
- [SDR FDEA202009272334](https://openairdocs.org/sdr/FDEA202009272334.md): Manifold · leaking · Sep 27, 2020 · N601FE · Doug MD11F · Hydraulic System, Main
  > LEVEL 1 HYD 1 OFF 36 MINUTES INTO FLIGHT. HYD QUANTITY SHOWING 2.9 GALLONS IN FLIGHT. ON TAXI IN QTY GOT TO 1.2 GALLONS, BUT CAME BACK UP TO 2.7 ON CLEANUP. INSTALLED NR 1 ENG HYD MANIFOLD ASSY, PER AMM 29-12-30. OPS & LEAK CHECK GOOD. OK FOR SERVICE.
- [SDR FDEA202006021107](https://openairdocs.org/sdr/FDEA202006021107.md): Sprocket · damaged · Jun 2, 2020 · N601FE · Doug MD11 · Horizontal Stabilizer Structure
  > FOUND RH THS DRIVE CHAIN OUTBOARD IDLER SPROCKET DAMAGED AND MISSING BEARING. FOUND DURING HORZ STAB LUBE R&R SPROCKET ASSEMBLY.
- [SDR FDEA2020060321107](https://openairdocs.org/sdr/FDEA2020060321107.md): Sprocket · damaged · Jun 2, 2020 · N601FE · Doug MD11F · Stabilizer Actuator
  > FOUND RT THS DRIVE CHAIN OUTBOARD IDLER SPROCKET DAMAGED AND MISSING BEARING, FOUND DURING HORZ STAB LUBE.
- [SDR FDEA201910302782](https://openairdocs.org/sdr/FDEA201910302782.md): Stiffener · cracked · Oct 30, 2019 · N601FE · Doug MD11F · Fuselage Miscellaneous Structure
  > LANDING GEAR RIGHT HAND MAIN LANDING GEAR WHEEL WELL UNDERWING BARREL TORQUE BOX APPROXIMATELY STA 1441 FORWARD ANGLE STIFFENER FOUND CRACKED APPROXIMATELY 1" RIGHT HAND MAIN LANDING GEAR WHEEL WELL UNDERWING BARREL TORQUE BOX APPROXIMATELY STA 1441 FORW
- [SDR FDEA201910242737](https://openairdocs.org/sdr/FDEA201910242737.md): Hinge Bracket · corroded · Oct 24, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LEFT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE CORROSION. CORROSION AT LEFT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS P
- [SDR FDEA201910242736](https://openairdocs.org/sdr/FDEA201910242736.md): Hinge Bracket · corroded · Oct 24, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LEFT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE CORROSION. CORROSION AT LEFT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER
- [SDR FDEA201910242740](https://openairdocs.org/sdr/FDEA201910242740.md): Hinge · corroded · Oct 24, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS
- [SDR FDEA201910242738](https://openairdocs.org/sdr/FDEA201910242738.md): Hinge · corroded · Oct 24, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS P
- [SDR FDEA2019102102708](https://openairdocs.org/sdr/FDEA2019102102708.md): Doubler · cracked · Oct 20, 2019 · N601FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING LEADING EDGE AT XOS 996 LOWER ACCESS PANEL CUTOUT DOUBLER CRACKED RIGHT HAND WING LEADING EDGE AT XOS 996 LOWER ACCESS PANEL CUTOUT DOUBLER CRACKED CARRIED OUT REPAIR AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 9 AND EA # 1- 5730-T0350370 PAR
- [SDR FDEA2019102102707](https://openairdocs.org/sdr/FDEA2019102102707.md): Skin · cracked · Oct 20, 2019 · N601FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING LEADING EDGE AT XOS 996 LOWER SKIN CRACKED RIGHT HAND WING LEADING EDGE AT XOS 996 LOWER SKIN CRACKED CARRIED OUT REPAIR AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 9 AND EA # 1-5730-T0350370 PART 1 "TITLE: WINGS - PLATES AND SKINS - RH WING F
- [SDR FDEA2019102102706](https://openairdocs.org/sdr/FDEA2019102102706.md): Doubler · corroded · Oct 20, 2019 · N601FE · Doug MD11F · Wing, Plate/Skin
  > LEFT HAND WING - LEADING EDGE CUTOUT STRIP AT STA XOS = 909 FOUND CORROSION LEFT HAND WING - LEADING EDGE CUTOUT STRIP AT STA XOS = 909 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-40-02-2R FIGURE 201 REPAIR 12 AND REPAIR CARRIED OUT AS PER
- [SDR FDEA2019102102705](https://openairdocs.org/sdr/FDEA2019102102705.md): Doubler · corroded · Oct 20, 2019 · N601FE · Doug MD11F · Wing, Plate/Skin
  > LEFT HAND WING - LEADING EDGE CUTOUT STRIP AT STA XOS = 926 FOUND CORROSION LEFT HAND WING - LEADING EDGE CUTOUT STRIP AT STA XOS = 926 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-40-02-2R FIGURE 201 REPAIR 12 AND REPAIR CARRIED OUT AS PER
- [SDR FDEA2019101762670](https://openairdocs.org/sdr/FDEA2019101762670.md): Support · corroded · Oct 16, 2019 · N601FE · Doug MD11F · Wing, Attach Fittings
  > RIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING C MOUNT HOLE FOUND WITH CORROSION RIGHT HAND OUTBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50- 32-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-32-5. REFER SNRM N005
- [SDR FDEA201910162669](https://openairdocs.org/sdr/FDEA201910162669.md): Fitting · corroded · Oct 16, 2019 · N601FE · Doug MD11F · Wing, Attach Fittings
  > RIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING E MOUNT HOLE FOUND WITH CORROSION RIGHT HAND OUTBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50- 32-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-32-5. REFER SNRM N005
- [SDR FDEA2019101762668](https://openairdocs.org/sdr/FDEA2019101762668.md): Fitting · corroded · Oct 16, 2019 · N601FE · Doug MD11F · Wing, Attach Fittings
  > RIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING B MOUNT HOLE FOUND WITH CORROSION RIGHT HAND OUTBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50- 32-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-32-5. REFER SNRM N005
- [SDR FDEA201910162667](https://openairdocs.org/sdr/FDEA201910162667.md): Fitting · corroded · Oct 16, 2019 · N601FE · Doug MD11F · Wing, Attach Fittings
  > LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'F' MOUNT HOLE FOUND WITH CORROSION CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'F' MOUNT HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-20-02-2R REPAIR 5 FIGURE 201. O
- [SDR FDEA2019101762666](https://openairdocs.org/sdr/FDEA2019101762666.md): Vane · corroded · Oct 16, 2019 · N601FE · Doug MD11F · Trailing Edge Flaps
  > LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'E' MOUNT HOLE FOUND WITH CORROSION CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'E' MOUNT HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-20-02-2R REPAIR 5 FIGURE 201. O
- [SDR FDEA2019101762665](https://openairdocs.org/sdr/FDEA2019101762665.md): Vane · corroded · Oct 16, 2019 · N601FE · Doug MD11F · Trailing Edge Flaps
  > LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'B' MOUNT HOLE FOUND WITH CORROSION CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'B' MOUNT HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-20-02-2R REPAIR 5 FIGURE 201. O
- [SDR FDEA201910152643](https://openairdocs.org/sdr/FDEA201910152643.md): Hinge · corroded · Oct 15, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE HAD CORROSION. CORROSION REWORKED AND FOUND TO EXCEED LIMITS. BASE THE DIFFERENCE BETWEEN DRAWING LIMITS AND CMM MAXIMUM REWORK LIMIT FOR BARREL NUT HOLE. REPAIR SHIM FABRIC
- [SDR FDEA201910142637](https://openairdocs.org/sdr/FDEA201910142637.md): Floorbeam · corroded · Oct 14, 2019 · N601FE · Doug MD11F · Fuselage Main, Floor Beam
  > LOWER AFT CARGO COMPARTMENT FORWARD BULKHEAD 'L' ANGLE FLOORBEAM FOUND CORRODED AT BS 1841. CORROSION REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-00-2R, FIGURE 205. FLOORBEAM REMOVED AND REPLACED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MINOR
- [SDR FDEA201910142638](https://openairdocs.org/sdr/FDEA201910142638.md): Skin · corroded · Oct 14, 2019 · N601FE · Doug MD11F · Fuselage Main, Plate/Skin
  > EMPENNAGE RIGHT UPPER FUSELAGE SKIN BS 2122 TO 2164, LONGERONS 33-35R, FOUND WITH SURFACE CORROSION. SURFACE CORROSION REMOVED IAW SRM 51-21-01-0G, AND FOUND OUT OF LIMITS IAW SRM 53-70-01-2R, FIGURE 201, REPAIR 3. REPAIRED IAW EA 1-5330-T0350371, PART 1.
- [SDR FDEA201910142636](https://openairdocs.org/sdr/FDEA201910142636.md): Seat Track · corroded · Oct 14, 2019 · N601FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORRODED, BS 1581 - 1621, LBL 8.5. CORROSION REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIG 101. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1571 TO 1631 IAW SRM 53-00-52-2,
- [SDR FDEA2019101432625](https://openairdocs.org/sdr/FDEA2019101432625.md): Hinge Bracket · corroded · Oct 13, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > CORROSION AT WING, INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE NR 3 HOLE. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 07. OVERSIZED REPAIR BUSHING FABRICATED AND INSTALLED CMM 57-44-07 AND EA 1-5750-T0321647 F PART 3 STEP 1A
- [SDR FDEA2019101432626](https://openairdocs.org/sdr/FDEA2019101432626.md): Hinge Fitting · corroded · Oct 13, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RIGHT WING, INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS CMM 57-44- 07. AN OVERSIZED REPAIR BUSHING WAS FABRICATED AND INSTALLED CMM 57-44-07 AND EA 1-5750-T0321648 D PART 3,

Next page: https://openairdocs.org/aircraft/N601FE/reports.md?page=2

## 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 = 'N601FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N601FE/reports

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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.