# Service difficulty reports: N607FE

A list on [N607FE](https://openairdocs.org/aircraft/N607FE.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 10 · 454 reports

- [SDR FDEA202609261439](https://openairdocs.org/sdr/FDEA202609261439.md): Skin · corroded · Sep 26, 2026 · N607FE · Doug MD11F · Fuselage Main, Plate/Skin
  > FOUND RIVETS WITH POPPED HEADS AND BUBBLING PAINT ON THE BELLY CENTERLINE JUST AFT OF THE FWD CARGO DOOR. MARKED AREA WITH TAPE. PICTURES ATTACHED. REPAIRED SKIN USING MD11 SRM 53-00-01-2R - FIG 201 (FUSELAGE PLATING REPAIR, WITH DOUBLER & TRIPLER) SH 13
- [SDR FDEA202510081922](https://openairdocs.org/sdr/FDEA202510081922.md): Sensor · failed · Oct 8, 2025 · N607FE · Doug MD11F · Landing Gear Position and Warning
  > ON FINAL WITH FLAPS 35 & GEAR DOWN, DID NOT GET A GREEN BOX & HAD AN UNSAFE IND ON LT MLG SECONDARY IND ON CONFIG SYNOPTIC. ALL PRIMARY MLG INDS ON FWD PANEL GREEN. EXECUTED A GO AROUND & RETRACTED MLG & RAN QRH. SECOND APPROACH NORMAL WITH ALL MLG INDS GRE
- [SDR FDEA202508051369](https://openairdocs.org/sdr/FDEA202508051369.md): Spoiler · damaged · Aug 5, 2025 · N607FE · Doug MD11F · Spoilers
  > POST FLIGHT WALK AROUND FOUND SPOILER NR 5 DAMAGED ON RIGHT WING. R & R'D RH O/B #5 SPOILER OPS & FUNCTION CHK GOOD. A/C OK FOR SERVICE IAW AMM 27-60-30-4 ANN: 27-60-30-6.
- [SDR FDEA202507271326](https://openairdocs.org/sdr/FDEA202507271326.md): Battery · no test · Jul 27, 2025 · N607FE · Doug MD11F · Emergency Lighting
  > EMER LT BATT 1 LOW, NOTED DURING POST FLIGHT WALK AROUND. REMOVED AND REPLACED EMERGENCY POWER LIGHTING BATTERY AS PER MD11 M.M. 33-51-01-4, OPS CHECKS NORMAL. O.K. FOR FLIGHT.
- [SDR FDEA202507221291](https://openairdocs.org/sdr/FDEA202507221291.md): Indicator · no test · Jul 22, 2025 · N607FE · Doug MD11F · Emergency Equipment
  > ON POST FLIGHT, THE R1 DOOR RAFT PUSH LIGHT WAS POPPED OUT. LIGHT WOULD NOT TEST. REMOVED AND REPLACED R1 SLIDE REMOTE PRESSURE INDICATOR ASSY IAW AMM 25-61-04-4.
- [SDR FDEA202504270654](https://openairdocs.org/sdr/FDEA202504270654.md): Trunnion · corroded · Apr 27, 2025 · N607FE · Doug MD11F · Wing, Landing Gear Attach Fittings
  > SUSPECT CORROSSION ON RIGHT MLG AFT TRUNNION FITTING AFT LUG FWD FACE. REPAIRED PER EA T 1-5720-T0383069.
- [SDR FDEA202501210110](https://openairdocs.org/sdr/FDEA202501210110.md): Skin · worn · Jan 21, 2025 · N607FE · Doug MD11F · Wing, Plate/Skin
  > PER WORKCARD T1-5710-125557A P2, LEFT HAND LOWER SKIN PLANK CUT-OUT 536AB BETWEEN STATION XORS 683.400 AND XORS 713.650 FOUND HOLE QUANTITIES (21) STATED IN STEP ON 1 NOT TALLY WITH STEP 1.A, 1.B AND 1C AND FASTENER HOLE #1 FOUND WITH NO BUSHING INSTALLE
- [SDR FDEA202501160085](https://openairdocs.org/sdr/FDEA202501160085.md): Rib · cracked · Jan 16, 2025 · N607FE · Doug MD11F · Wing, Rib/Bulkhead
  > LEFT HAND WING: AFTER NUMBER:6 SLAT INNER SKIN REMOVAL, INNER RIB FOUND CRACKED AT STATION XOS 868.476 (REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM: N00935). LEFT HAND WING NUMBER 6 SLAT CRACKED INNER RIB AT STATION XOS 868.476 REPAIRED AS PER EA# 1-5750-
- [SDR FDEA202501160084](https://openairdocs.org/sdr/FDEA202501160084.md): Rib · cracked · Jan 16, 2025 · N607FE · Doug MD11F · Wing, Rib/Bulkhead
  > LEFT HAND WING: AFTER NUMBER:6 SLAT INNER SKIN REMOVAL, INNER RIB FOUND CRACKED AT STATION XOS 814.825 (REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM: N00935). LEFT HAND WING NUMBER 6 SLAT CRACKED INNER RIB AT STATION XOS 814.825 REPAIRED AS PER EA# 1-5750-
- [SDR FDEA202501160083](https://openairdocs.org/sdr/FDEA202501160083.md): Rib · cracked · Jan 16, 2025 · N607FE · Doug MD11F · Wing, Rib/Bulkhead
  > LEFT HAND WING: UPON BORESCOPE INSPECTION ON NUMBER:6 SLAT LOWER SURFACE LOOSE FASTENER INNER RIBS, CRACK FOUND ON INNER RIB (REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM: N00589) AT STATION XOS 863.325. LEFT HAND WING NUMBER 6 SLAT CRACKED INNER RIB AT ST
- [SDR FDEA202501160074](https://openairdocs.org/sdr/FDEA202501160074.md): Rib · cracked · Jan 16, 2025 · N607FE · Doug MD11F · Wing, Rib/Bulkhead
  > LEFT HAND WING: AFTER NUMBER: 7 SLAT INNER SURFACE SKIN REMOVAL, FOUND INNER RIB CRACKED AT STATION XOS 988.762.(REFER TO SPECIAL/NONROUTINE MAINTENANACE FORM: N00936) LEFT HAND WING NUMBER 7 SLAT CRACKED INNER RIB AT STATION XOS 988.762 REPAIRED AS PER
- [SDR FDEA202501160073](https://openairdocs.org/sdr/FDEA202501160073.md): Rib · cracked · Jan 16, 2025 · N607FE · Doug MD11F · Wing, Rib/Bulkhead
  > LEFT HAND WING: UPON BORESCOPE INSPECTION ON NUMBER:7 SLAT LOWER SURFACE LOOSE FASTENER INNER RIBS, CRACK FOUND ON INNER RIB. (REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM: N00594) AT STATION XOS 978.461. LEFT HAND WING NUMBER 7 SLAT CRACKED INNER RIB AT S
- [SDR FDEA202501160086](https://openairdocs.org/sdr/FDEA202501160086.md): Rib · cracked · Jan 16, 2025 · N607FE · Doug MD11F · Wing, Rib/Bulkhead
  > LEFT HAND WING: DURING #8 SLAT SKIN REPAIR, #8 SLAT INNER RIB FOUND CRACKED AT STATION XOS 1124.439 (REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM: N00579). LEFT HAND WING #8 SLAT CRACKED INNER RIB AT STATION XOS 1124.439 REPAIRED AS PER EA# 1- 5730-T0381884
- [SDR FDEA202501100055](https://openairdocs.org/sdr/FDEA202501100055.md): Hinge Bracket · corroded · Jan 10, 2025 · N607FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE FOUND CORROSION. CORROSION AT RIGHT HAND, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MAC
- [SDR FDEA202501100053](https://openairdocs.org/sdr/FDEA202501100053.md): Hinge Bracket · corroded · Jan 10, 2025 · N607FE · Doug MD11F · Trailing Edge Flaps
  > LEFT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED
- [SDR FDEA202501100052](https://openairdocs.org/sdr/FDEA202501100052.md): Skin · cracked · Jan 10, 2025 · N607FE · Doug MD11F · Fuselage Main, Structure
  > 02 EACH FASTENER HOLES (#14 AND #15) FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=683.400 AND STATION XORS=713.600. REPAIR CARRIED OUT AT RIGHT HAND WIN
- [SDR FDEA202501090049](https://openairdocs.org/sdr/FDEA202501090049.md): Doubler · damaged · Jan 9, 2025 · N607FE · Doug MD11F · Fuselage Main, Plate/Skin
  > LOWER FORWARD CARGO DOOR LOWER FORWARD JAMB EXISTING REPAIR DOUBLER EDGE FOUND WITH CHAFED MARKS AT STATION 899 LOWER FORWARD CARGO DOOR LOWER FORWARD JAMB AT STATION 899 CHAFFED EXISTING REPAIR DOUBLER REMOVED AS PER MD11 SRM 51-33-01-0G. REPAIR CARRIED O
- [SDR FDEA202501090048](https://openairdocs.org/sdr/FDEA202501090048.md): Doubler · damaged · Jan 9, 2025 · N607FE · Doug MD11F · Fuselage Main, Plate/Skin
  > LOWER FORWARD CARGO DOOR CUTOUT LOWER AFT JAMB EXISTING REPAIR DOUBLER LOWER CORNER FOUND CHIPPED OFF AT STATION 999 LOWER FORWARD CARGO DOOR CUTOUT LOWER AFT JAMB LOWER CORNER AT STATION 999 CHIPPED OFF EXISTING REPAIR DOUBLER REMOVED AS PER MD11 SRM 51-3
- [SDR FDEA202501090047](https://openairdocs.org/sdr/FDEA202501090047.md): Longeron Splice · cracked · Jan 9, 2025 · N607FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER FORWARD CARGO COMPARTMENT BILGE AREA LONGERON SPLICE FITTING FOUND CRACK APPROXIMATELY 0.5 INCH AT BETWEEN STATION 6-0 TO 6-10 LONGERON 50 LEFT. LOWER FORWARD CARGO COMPARTMENT BILGE AREA AT BETWEEN STATION 6-0 TO 6-10 LONGERON 50 LEFT CRACKED LONGER
- [SDR FDEA202501090046](https://openairdocs.org/sdr/FDEA202501090046.md): Longeron Splice · cracked · Jan 9, 2025 · N607FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER FORWARD CARGO COMPARTMENT BILGE AREA LONGERON SPLICE FITTING FOUND CRACK APPROXIMATELY 0.5 INCH AT BETWEEN STATION 6-0 TO 6-10 LONGERON 50 RIGHT. LOWER FORWARD CARGO COMPARTMENT BILGE AREA AT BETWEEN STATION 6-0 TO 6-10 LONGERON 50 RIGHT CRACKED LONG
- [SDR FDEA202501090045](https://openairdocs.org/sdr/FDEA202501090045.md): Longeron · corroded · Jan 9, 2025 · N607FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER CENTER CARGO BILGE AREA SKIN FOUND WITH SURFACE CORROSION STATION 1681 UNDERNEATH LONGERON 50 RIGHT CORROSION ON LONGERON 50 RIGHT STATION 1681 REMOVED PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED ALLOWABLE LIMITS PER MD11 SRM 53-00-00-2R FIGURE 205 R
- [SDR FDEA202501090044](https://openairdocs.org/sdr/FDEA202501090044.md): Longeron · corroded · Jan 9, 2025 · N607FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > FUSELAGE: CAC COMPARTMENT BILGE APPROXIMATELY STATION 1152 LONGERON 46 RIGHT, SPLICE FOUND CORRODED. FUSELAGE: CAC COMPARTMENT BILGE APPROXIMATELY STATION 1152 LONGERON 46 RIGHT CORRODED SPLICE REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER MD11 SRM
- [SDR FDEA202501090043](https://openairdocs.org/sdr/FDEA202501090043.md): Longeron · cracked · Jan 9, 2025 · N607FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LANDING GEAR: UPON TRIMMED OUT OF RIGHT HAND NOSE TRUNNION CRACKED AREA REPAIR, FOUND LONGERON 49 WITH APPROXIMATELY 1" CRACK AT STATION 583 (REFER SNRM: N00117). LANDING GEAR: CRACKED LONGERON 49 WITH APPROXIMATELY 1" CRACK AT STATION 583 REMOVED AND REPL
- [SDR FDEA202501090042](https://openairdocs.org/sdr/FDEA202501090042.md): Skin · cracked · Jan 9, 2025 · N607FE · Doug MD11F · Leading Edge Devices
  > LEFT HAND WING: #8 SLAT INTERIOR SIDE SKIN UPPER AFT AREA FOUND CRACKED ABOUT 4"AT STATION XOS 1124.439. LEFT HAND WING #8 SLAT CRACKED INTERIOR SKIN AT STATION XOS 1124.439 REPAIRED AS PER EA# 1-5730-T0381884 P1 TITLE: WINGS - FLIGHT SURFACES - SLAT INNER
- [SDR FDEA202501090041](https://openairdocs.org/sdr/FDEA202501090041.md): Cargo Track · corroded · Jan 9, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1401 X = -8.5" FOUND WITH EXFOLIATION CORROSION. CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1401 X = -8.5" EXFOLIATION CORROSION REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT A
- [SDR FDEA202501080036](https://openairdocs.org/sdr/FDEA202501080036.md): Doubler · corroded · Jan 8, 2025 · N607FE · Doug MD11F · Wing, Landing Gear Attach Fittings
  > LEFT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN STRINGER 4 AND STRINGER 6, ALONG STATION XORS 164 FOUND CORRODED. LEFT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT DOUBLER BETWEEN STRINGER 4 AND STRINGER 6 AL
- [SDR FDEA202501080034](https://openairdocs.org/sdr/FDEA202501080034.md): Seat Track · worn · Jan 8, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 885 X = 8.5 FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 885 X=8.5 WORN AT CROWN REMOVED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE
- [SDR FDEA202501080033](https://openairdocs.org/sdr/FDEA202501080033.md): Seat Track · worn · Jan 8, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 824 X = -8.5 FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 824 X = -8.5 WORN AT CROWN REMOVED AND FOUND EXCEEDED LIMIT IN ACCORDANCE WITH SRM 53-00-52-1A FIGURE 1
- [SDR FDEA202501080032](https://openairdocs.org/sdr/FDEA202501080032.md): Seat Track · worn · Jan 8, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 999 X = 75.25" FOUND CROWN WORN. CABIN-MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 999 X=75.25" WORN ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SRM 5
- [SDR FDEA202501080029](https://openairdocs.org/sdr/FDEA202501080029.md): Seat Track · worn · Jan 8, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1014 X = -47.5 FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1014 X = -47.5" CROWN WORN REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 S
- [SDR FDEA202501080028](https://openairdocs.org/sdr/FDEA202501080028.md): Seat Track · worn · Jan 8, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1165 X = 8.5" FOUND CROWN WORN. CABIN-MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1165 X=8.5" WORN MARK ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SR
- [SDR FDEA202501070027](https://openairdocs.org/sdr/FDEA202501070027.md): Skin · cracked · Jan 7, 2025 · N607FE · Doug MD11F · Fuselage Main, Plate/Skin
  > FUSELAGE: #1 AIRCON COMPARTMENT CUTOUT UPPER AFT CORNER SUSPECT CRACK STATION 587.250 LONGERON 31 - LONGERON 33. FUSELAGE: #1 AIRCON COMPARTMENT CUTOUT UPPER AFT CORNER CRACK STATION 587.250 LONGERON 31 - LONGERON 33 CARRIED OUT REPAIR IN ACCORDANCE WITH S
- [SDR FDEA202501070026](https://openairdocs.org/sdr/FDEA202501070026.md): Seat Track · worn · Jan 7, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-5 X = 47.5" CROWN WITH GOUGE MARK. CABIN-MAIN DECK CARGO COMPARTMENT SEAT TRACK ST STATION 5-5 X=47.5" GOUGE MARK ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SR
- [SDR FDEA202501070025](https://openairdocs.org/sdr/FDEA202501070025.md): Seat Track · worn · Jan 7, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1059 X = 47.5" FOUND CROWN WORN CABIN-MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1059 X=47.5" WORN MARK ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 S
- [SDR FDEA202501070024](https://openairdocs.org/sdr/FDEA202501070024.md): Seat Track · worn · Jan 7, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 806 X = 47.5" FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 806 X = 47.5" CROWN WORN REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SRM
- [SDR FDEA202501070023](https://openairdocs.org/sdr/FDEA202501070023.md): Seat Track · worn · Jan 7, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1119 X = -27.5" FOUND CROWN WORN. CABIN-MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1119 X=-27.5" WORN MARK ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS P
- [SDR FDEA202501070022](https://openairdocs.org/sdr/FDEA202501070022.md): Doubler · chafed · Jan 7, 2025 · N607FE · Doug MD11F · Fuselage Main, Structure
  > FORWARD CABIN 9G NET LEFT HAND SUPPORT YOKE STATION 535 LONGERON 18 - LONGERON 21, FOUND FRAME UPPER EXISTING DOUBLER REPAIR CHAFED CABIN - FORWARD CABIN 9G NET LEFT HAND SUPPORT STATION 535 LONGERON 18 - LONGERON 21 CHAFFED EXISTING REPAIRED FRAME CARRIED
- [SDR FDEA202501070021](https://openairdocs.org/sdr/FDEA202501070021.md): Doubler · chafed · Jan 7, 2025 · N607FE · Doug MD11F · Fuselage Main, Structure
  > FORWARD CABIN 9G NET LEFT HAND SUPPORT YOKE STATION 535 LONGERON 24- LONGERON 25, FOUND FRAME LOWER EXISTING DOUBLER REPAIR CHAFFED. CABIN-FORWARD CABIN 9G NET LEFT HAND SUPPORT STATION 535 LONGERON 24-LONGERON 25 CHAFFED EXISTING REPAIRED FRAME CARRIED OUT
- [SDR FDEA202501060020](https://openairdocs.org/sdr/FDEA202501060020.md): Skin · cracked · Jan 6, 2025 · N607FE · Doug MD11F · Wing, Plate/Skin
  > HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND FIXED LEADING EDGE SKIN CORNER 13 - SLAT TRACK #10 CUTOUT AFT INBOARD CORNER FOUND CRACK APPROXIMATELY 0.1" REPAIR CARRIED OUT AT RIGHT HAND FIXED LEADING EDGE SKIN CORNER 13-SLAT TRACK #10 CUTOUT AFT
- [SDR FDEA202501060019](https://openairdocs.org/sdr/FDEA202501060019.md): Cargo Track · worn · Jan 6, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 6-40 X = -27.5" FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 6-40 X=-27.5" WORN AT CROWN REMOVED AND FOUND EXCEEDED LIMIT IN ACCORDANCE WITH SRM 53-00-52-1A FIGU
- [SDR FDEA202501060018](https://openairdocs.org/sdr/FDEA202501060018.md): Cargo Track · worn · Jan 6, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 6-80 X = 47.5" FOUND CROWN WORN CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 6-80 X = 47.5" CROWN WORN REMOVED PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT PER MD11 SRM 53-00-
- [SDR FDEA202501060017](https://openairdocs.org/sdr/FDEA202501060017.md): Cargo Track · worn · Jan 6, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 6-10 X = -8.5" FOUND CROWN WORN CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 6-10 X = -8.5" CROWN WORN REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SRM
- [SDR FDEA202501060016](https://openairdocs.org/sdr/FDEA202501060016.md): Cargo Track · worn · Jan 6, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 6-30 X = -47.5" FOUND CROWN WORN CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 6-30 X = -47.5" CROWN WORN REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 S
- [SDR FDEA202501060015](https://openairdocs.org/sdr/FDEA202501060015.md): Cargo Track · worn · Jan 6, 2025 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 6-10 X = 8.5" FOUND CROWN WORN CABIN-MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10 X=8.5" WORN MARK ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SRM
- [SDR FDEA202501040011](https://openairdocs.org/sdr/FDEA202501040011.md): Former · cracked · Jan 4, 2025 · N607FE · Doug MD11F · Wing Main, Frame Structure
  > LEFT HAND WING: FIXED LEADING EDGE FORMER AT STATION XOS 584 FOUND CRACK ABOUT 5 INCHES. CRACKED FORMER AT LEFT HAND WING FIXED LEADING EDGE STATION XOS 584 REMOVED AND REPLACED WITH FABRICATED FORMER AS PER MD-11 SRM 51-31-01-0G. FORMER FABRICATION CARR
- [SDR FDEA202501030007](https://openairdocs.org/sdr/FDEA202501030007.md): Trunnion · cracked · Jan 3, 2025 · N607FE · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND NOSE LANDING GEAR TRUNNION WEB STATION 583 EXISTING TRIMMED OUT AREA FOUND CRACK APPROXIMATELY 0.35". LEFT HAND NOSE LANDING GEAR TRUNNION WEB STATION 583 EXISTING TRIMMED OUT AREA WITH CRACK OF 0.35" CAR
- [SDR FDEA202501030006](https://openairdocs.org/sdr/FDEA202501030006.md): Trunnion · cracked · Jan 3, 2025 · N607FE · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > LANDING GEAR: NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING SUSPECTED CRACKED AT STATION 583. LANDINIG GEAR: NOSE LANDING GEAR RIGHT HAND TRUNNION AT STATION 583 WITH CRACK LENGTH OF 0.9" CARRIED OUT REPAIR IN ACCORDANCE WITH EA # 1-5310-T0381762 P1 TITLE
- [SDR FDEA202408031081](https://openairdocs.org/sdr/FDEA202408031081.md): Floorbeam · cracked · Aug 3, 2024 · N607FE · Doug MD11F · Fuselage Main, Floor Beam
  > FLOOR BEAM AT STA. 1701 DAMAGED ON R SIDE REPAIRED FLOOR BEAM REF. MD11 SRM 53-50-51-2R. THIS IS A MAJOR REPAIR
- [SDR FDEA202406180817](https://openairdocs.org/sdr/FDEA202406180817.md): Computer · faulted · Jun 18, 2024 · N607FE · Doug MD11F · Autopilot System
  > DURING CRUISE, WE RECEIVED LEV2 FCC2A DATA FAULT, LEV1 SEL LSAS RIB OFF, LEV1 SEL YAW UPR B OFF, FOLLOWED BY AUTOPILOT DISENGAGING. WE RAN QRH PROCEDURES AND WERE NOT ABLE TO GET AN AUTOPILOT BACK. DIVERTED TO RJBB. REMOVED AND REPLACED FCC-2
- [SDR FDEA202406180811](https://openairdocs.org/sdr/FDEA202406180811.md): None · none · Jun 18, 2024 · N607FE · Doug MD11F · Standard Practices/Structures
  > LANDED ABOVE MGLW AT 484K. LANDING WAS WITHIN PARAMETERS. AMM: 05-51-03-6 OVERWEIGHT L/G INSP IN PROGRESS. AMM: 05-51-03-6 PERFORMED A1 & A2 OVERWEIGHT L/G INSP AND NO DEFECT FOUND. A/C OK FOR SERVICE. AMM: 05-51-03-6 PERFORMED A1 & A2 OVERWEIGHT L

Next page: https://openairdocs.org/aircraft/N607FE/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 = 'N607FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N607FE/reports

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