# Service difficulty reports: N311FE, cancelled Aug 1, 2024

A list on [N311FE, cancelled Aug 1, 2024](https://openairdocs.org/deregistered/N311FE-2024-08-01.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 5 · 232 reports

- [SDR FDEA202203170534](https://openairdocs.org/sdr/FDEA202203170534.md): Apu · leaking · Mar 17, 2022 · N311FE · Doug MD1030F · Airborne Auxiliary Power Unit (APU) System
  > PDIS 311 49-00 6843 17MAR22 TPA FACT U EMERGENCY EVACUATION PERFORMED IN CHOCKS DUE TO APU FAIL AND SMOKE IN CARGO TUBE. FIRE DEPT CALLED. NO EVIDENCE OF FIRE. FACT 17MAR22 02:11 TPA U SMOKE WAS CAUSED FROM APU FAILED START ATTEMPT AN
- [SDR FDEA202109302437](https://openairdocs.org/sdr/FDEA202109302437.md): None · none · Sep 30, 2021 · N311FE · Doug MD1030F · Hydraulic System, Main
  > HYD 3 ELEV OFF LEVEL ONE ALERT APPROXIMATELY:30 MINUTES INTO FLIGHT, APPROXIMATELY 15 MINUTES LATER HYD 3 OFF LEVEL ONE ALERT, ON FINAL AFTER SELECTING LANDING GEAR DOWN HYD 3 FAIL LEVEL 2 ALERT. REMOVED AND REPLACED PRESSURE PORT UNION O-RING ON 1/3 RMP
- [SDR FDEA202108051946](https://openairdocs.org/sdr/FDEA202108051946.md): Cap · corroded · Aug 5, 2021 · N311FE · Doug MD1030F · Fuselage Main, Bulkhead
  > LOWER BLADDER CELL AFT BULKHEAD LOWER CAP CUTOUT AREA FOUND CORROSION AT STATION 1368.650 X=-4.95 TO X=-13.95. LOWER BLADDER CELL AFT BULKHEAD LOWER CAP CUTOUT AREA CORROSION REMOVED AS PER SRM 51-21-01 VOLUME 2 AND FOUND EXCEED LIMIT AS PER SRM 53-00-01 F
- [SDR FDEA202108011916](https://openairdocs.org/sdr/FDEA202108011916.md): Angle · corroded · Aug 1, 2021 · N311FE · Doug MD1030F · Fuselage Main, Structure
  > CENTER LOWER CARGO COMPARTMENT - WHILE REMOVAL OF ADDITIONAL ACCESS (REFERENCE NRSM 01768) FOUND DOOR JAMB STATION 1708 AREA FOUND CORROSION LONGERON 42 RIGHT TO LONGERON 43 RIGHT CENTER LOWER CARGO COMPARTMENT DOOR CUTOUT FORWARD INNER LOWER FRAME ANGLE
- [SDR FDEA202108011914](https://openairdocs.org/sdr/FDEA202108011914.md): Door Frame · cracked · Aug 1, 2021 · N311FE · Doug MD1030F · Fuselage Main, Structure
  > CABIN - STATION 1256 L3 DOOR CUTOUT FORWARD UPPER JAMB INNER SKIN FOUND CRACKED. CABIN - AT STATION 1256 L3 D00R CUT OUT FORWARD UPPER JAMB, CRACKED INNER SKIN REPAIRED AS PER E.A.#: 8-5300-T0363092 PART 1, TITLE: FUSELAGE - GENERAL - REPAIR FOR L3 AND R
- [SDR FDEA202108011913](https://openairdocs.org/sdr/FDEA202108011913.md): Door Frame · cracked · Aug 1, 2021 · N311FE · Doug MD1030F · Fuselage Main, Structure
  > CABIN - STATION 1305 L3 DOOR CUTOUT AFT UPPER JAMB INNER SKIN FOUND CRACKED. CABIN - AT STATION 1305 L3 DOOR CUT OUT AFT UPPER JAMB, CRACKED INNER SKIN REPAIRED AS PER E.A.#: 8-5300-T0363092 PART 1, TITLE: FUSELAGE - GENERAL - REPAIR FOR L3 AND R3 CENTER
- [SDR FDEA202108011912](https://openairdocs.org/sdr/FDEA202108011912.md): Door Frame · cracked · Aug 1, 2021 · N311FE · Doug MD1030F · Fuselage Main, Structure
  > CABIN - STATION 1256 R3 DOOR CUTOUT FORWARD UPPER JAMB INNER SKIN FOUND CRACKED. CABIN - AT STATION 1256 R3 DOOR CUT OUT FORWARD UPPER JAMB, CRACKED INNER SKIN REPAIRED AS PER E.A.#: 8-5300-T0363092 PART 1, TITLE: FUSELAGE - GENERAL - REPAIR FOR L3 AND R
- [SDR FDEA202107301899](https://openairdocs.org/sdr/FDEA202107301899.md): Web · corroded · Jul 30, 2021 · N311FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO COMPARTMENT - WHILE REPAIR OF FLOOR WEB ( REFERENCE SPECIAL/NONROUTINE MAINTENANCE FORM: N01471), FOUND FLOOR SUPPORT STATION 1841 X=32 FOUND CORROSION. AFT LOWER CARGO COMPARTMENT DAMAGED FLOOR SUPPORT CHORD AT STATION 1841 X=32 REMOVED
- [SDR FDEA202107281879](https://openairdocs.org/sdr/FDEA202107281879.md): Filler · damaged · Jul 28, 2021 · N311FE · Doug MD1030F · Wing, Plate/Skin
  > RIGHT HAND WING INBOARD LEADING EDGE COMPARTMENT STATION XIS 160.500 FILLER FASTENERS HOLES FOUND DAMAGED AFTER EXISTING REPAIR DOUBLER REMOVED (REF: SNRM N00253) RIGHT HAND WING INBOARD LEADING EDGE COMPARTMENT STATION XIS 160.500 FILLER WITH DAMAGED F
- [SDR FDEA202107261864](https://openairdocs.org/sdr/FDEA202107261864.md): Former · damaged · Jul 26, 2021 · N311FE · Doug MD1030F · Wing, Plate/Skin
  > RIGHT HAND WING INBOARD LEADING EDGE COMPARTMENT STATION XIS 160.500 FORMER FASTENER HOLES FOUND ELONGATED AFTER EXISTING REPAIR DOUBLER REMOVED (REF: SNRM N00253) RIGHT HAND WING INBOARD LEADING EDGE COMPARTMENT STATION XIS 160.500 FORMER WITH ELONGATE
- [SDR FDEA202107211828](https://openairdocs.org/sdr/FDEA202107211828.md): Bracket · corroded · Jul 21, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT LUG HOLE SURFACE FOUND WITH CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT LUG HOLE SURFACE REWORKED AS PER MD-10 CMM 57-44-08 AND FOUND UPPER AND LOWER BA
- [SDR FDEA202107201821](https://openairdocs.org/sdr/FDEA202107201821.md): Beam · cracked · Jul 20, 2021 · N311FE · Doug MD1030F · Fuselage Main, Structure
  > CABIN - L3 DOOR PLUG #7 BEAM FORWARD STOP FITTING FOUND CRACKED. CABIN - AT L3 PLUG DOOR CRACKED #7 BEAM REMOVED AND REPLACED WITH NEW BEAM AS PER SRM 51-31-01 VOLUME 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
- [SDR FDEA202107201820](https://openairdocs.org/sdr/FDEA202107201820.md): Beam · cracked · Jul 20, 2021 · N311FE · Doug MD1030F · Fuselage Main, Structure
  > CABIN - L3 DOOR PLUG #6 BEAM FORWARD STOP FITTING FOUND CRACKED AT STATION 1260. CABIN - AT L3 PLUG DOOR CRACKED #6 STOP BEAM AT STATION 1260 REMOVED AND REPLACED AS PER E.A. #: 8-5210-T0363122 PART 1, TITLE: DOORS - PASSENGER / CREW - L3 DOOR - STOP BEAM
- [SDR FDEA202107131755](https://openairdocs.org/sdr/FDEA202107131755.md): Skin · corroded · Jul 13, 2021 · N311FE · Doug MD1030F · Ailerons
  > RIGHT HAND WING INBOARD AILERON LOWER SURFACE AT STATION XIA 316 FOUND WITH CORROSION RIGHT HAND WING INBOARD AILERON LOWER SURFACE AT STATION XIA 316 REPAIR CARRIED OUT AS PER EA 8-5730-T0362995 PART 1 TITLE: WINGS - FLIGHT SURFACES - NEW LOWER SKIN SPL
- [SDR FDEA202107111722](https://openairdocs.org/sdr/FDEA202107111722.md): Frame · cracked · Jul 11, 2021 · N311FE · Doug MD1030F · Fuselage Main, Frame
  > LEFT HAND AIRCON PACK #2 COMPARTMENT FUSELAGE FRAME AT STATION 495 LONGERON 32 LEFT TO LONGERON 33 LEFT FOUND CRACKED. LEFT HAND AIRCON PACK #2 COMPARTMENT FUSELAGE FRAME CRACKED AT STATION 495 LONGERON 32 LEFT TO LONGERON 33 LEFT REPAIR CARRIED OUT AS PER
- [SDR FDEA202107111721](https://openairdocs.org/sdr/FDEA202107111721.md): Frame · chafed · Jul 11, 2021 · N311FE · Doug MD1030F · Fuselage Main, Frame
  > CABIN - RIGHT HAND STATION 535 LONGERON 19 RIGHT FRAME FOUND CHAFFED. CABIN AT RIGHT HAND FRAME STATION 535 LONGERON 19 RIGHT CHAFFED MARKS REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-01 FIGURE 1B VOLUME 1. REPAIR CARRIED OUT AT RIGHT HAND FRAME STATION 53
- [SDR FDEA202107061691](https://openairdocs.org/sdr/FDEA202107061691.md): Floor Support · corroded · Jul 6, 2021 · N311FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO FLOOR PANEL #183KF SUPPORT FOUND CORROSION AT STATION 1841, X = 47" AFT LOWER CARGO FLOOR PANEL #183KF CORRODED SUPPORT AT STATION 1841 X=47" REMOVED AND REPLACED WITH REWORKED SUPPORT AS PER SRM 51-31-01 VOLUME 2. SUPPORT REWORKED AS P
- [SDR FDEA202107061690](https://openairdocs.org/sdr/FDEA202107061690.md): Web · cracked · Jul 6, 2021 · N311FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO COMPARTMENT FLOOR WEB FOUND CRACKED AT STATION 1841 X = 5". WEB REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME 2. WEB FABRICATED AS PER DOUGLAS DRAWING AGA 7170 REVISION: T. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202107061689](https://openairdocs.org/sdr/FDEA202107061689.md): Cap · corroded · Jul 6, 2021 · N311FE · Doug MD1030F · Fuselage Main, Bulkhead
  > LOWER BLADDER CELL AFT BULKHEAD LOWER CUTOUT AREA FOUND CORROSION AT STATION 1368.650. LOWER BLADDER CELL AFT BULKHEAD LOWER CAP CUTOUT AREA CORROSION REMOVED IAW SRM 51-21-01 VOLUME 2 AND FOUND EXCEED LIMIT IAW SRM 53-00-01 FIGURE 1B VOLUME 1 AT STATION
- [SDR FDEA202107061688](https://openairdocs.org/sdr/FDEA202107061688.md): Tee Fitting · cracked · Jul 6, 2021 · N311FE · Doug MD1030F · Fuselage Main, Bulkhead
  > CENTER WHEEL WELL FORWARD BULKHEAD LEFT HAND T-CHORD FITTING FOUND CRACKED AT STATION 1368.650, X= 31.5. CENTER WHEEL WELL FORWARD BULKHEAD LEFT HAND CRACKED T-CHORD FITTING. REMOVED AND REPLACED WITH FABRICATED T-CHORD FITTING IAW SRM 51-31-01 VOLUME 2
- [SDR FDEA202107051681](https://openairdocs.org/sdr/FDEA202107051681.md): Hinge Bracket · corroded · Jul 5, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD LUG HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PE
- [SDR FDEA202107051680](https://openairdocs.org/sdr/FDEA202107051680.md): Hinge Bracket · corroded · Jul 5, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD LUG HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER
- [SDR FDEA202107051679](https://openairdocs.org/sdr/FDEA202107051679.md): Hinge Bracket · corroded · Jul 5, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERS
- [SDR FDEA202107051686](https://openairdocs.org/sdr/FDEA202107051686.md): Hinge Fitting · corroded · Jul 5, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > LEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT BORE LUG HOLE FOUND WITH CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-52-02. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-52- 02 AND E.A.#8-5
- [SDR FDEA202107051685](https://openairdocs.org/sdr/FDEA202107051685.md): Barrel Nut · corroded · Jul 5, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-44- 09 AND E.A.#8-5750-
- [SDR FDEA202107051683](https://openairdocs.org/sdr/FDEA202107051683.md): Barrel Nut · corroded · Jul 5, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER LUG HOLE BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 10 CMM 57-44-09 AND E.A
- [SDR FDEA202107051682](https://openairdocs.org/sdr/FDEA202107051682.md): Barrel Nut · corroded · Jul 5, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER LUG HOLE BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-44-09 AND E.A
- [SDR FDEA202107041672](https://openairdocs.org/sdr/FDEA202107041672.md): Hinge Bracket · corroded · Jul 4, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE (#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS
- [SDR FDEA202107041671](https://openairdocs.org/sdr/FDEA202107041671.md): Hinge Bracket · corroded · Jul 4, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT INBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT INBOARD LUG HOLE BORE (#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PE
- [SDR FDEA202107041670](https://openairdocs.org/sdr/FDEA202107041670.md): Hinge Bracket · corroded · Jul 4, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD LUG HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER M
- [SDR FDEA202107041669](https://openairdocs.org/sdr/FDEA202107041669.md): Hinge Bracket · corroded · Jul 4, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD LUG HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER
- [SDR FDEA202107041668](https://openairdocs.org/sdr/FDEA202107041668.md): Hinge Bracket · corroded · Jul 4, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD LUG HOLE BORE (#2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER
- [SDR FDEA202107041667](https://openairdocs.org/sdr/FDEA202107041667.md): Hinge Bracket · corroded · Jul 4, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT LOWER LUG HOLE BORE FOUND WITH CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT LOWER LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-08.
- [SDR FDEA202107031664](https://openairdocs.org/sdr/FDEA202107031664.md): Seat Track · corroded · Jul 3, 2021 · N311FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - LEFT HAND STATION 1761 - 1781, X = 27.5 SEAT TRACK FOUND WITH CORROSION. CABIN AT LEFT HAND STATION 1761 TO STATION 1781, X = 27.5 CORROSION AT SEAT TRACK EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME 1.CORRO
- [SDR FDEA202107031663](https://openairdocs.org/sdr/FDEA202107031663.md): Doubler · cracked · Jul 3, 2021 · N311FE · Doug MD1030F · Wing, Plate/Skin
  > LEFT HAND WING - LEADING EDGE COMPARTMENT STATION XOS 667 RIB DOUBLER CRACKED CRACKED RIB DOUBLER REMOVED AS PER SRM 51-31-01 VOLUME 2 AND FABRICATED RIB DOUBLER AS PER DOUGLAS DRAWING ARB3954 REV K. INSTALLED FABRICATED RIB DOUBLER AT LEFT HAND WING COMP
- [SDR FDEA202107021656](https://openairdocs.org/sdr/FDEA202107021656.md): Hinge Bracket · corroded · Jul 2, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-08. OVERSIZE
- [SDR FDEA202107021657](https://openairdocs.org/sdr/FDEA202107021657.md): Hinge Bracket · corroded · Jul 2, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT UPPER LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT UPPER LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-08
- [SDR FDEA202107021655](https://openairdocs.org/sdr/FDEA202107021655.md): Hinge Bracket · corroded · Jul 2, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE SURFACE FOUND WITH CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE SURFACE REWORKED AND FOUND EXCEED LIMI
- [SDR FDEA202107021654](https://openairdocs.org/sdr/FDEA202107021654.md): Hinge Bracket · corroded · Jul 2, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND WITH CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE (#10 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERS
- [SDR FDEA202107021653](https://openairdocs.org/sdr/FDEA202107021653.md): Hinge Bracket · corroded · Jul 2, 2021 · N311FE · Doug MD1030F · Trailing Edge Flaps
  > LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSIZE
- [SDR FDEA202107011643](https://openairdocs.org/sdr/FDEA202107011643.md): Frame · dented · Jul 1, 2021 · N311FE · Doug MD1030F · Fuselage Main, Frame
  > CABIN - LEFT HAND STATION 1601 LONGERON 12 LEFT FRAME FOUND DENT. CABIN AT LEFT HAND FRAME STATION 1601 LONGERON 12 LEFT DENT AREA REPAIRED AS PER SRM 53-30-00 FIGURE 4 VOLUME 1. REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPETITIVE INSP
- [SDR FDEA202107011642](https://openairdocs.org/sdr/FDEA202107011642.md): Frame · dented · Jul 1, 2021 · N311FE · Doug MD1030F · Fuselage Main, Frame
  > CABIN - LEFT HAND STATION 1561 LONGERON 12 LEFT FRAME FOUND DENT. CABIN AT LEFT HAND FRAME STATION 1561 LONGERON 12 LEFT, DENT AREA REPAIRED AS PER SRM 53-30-00 FIGURE 4 VOLUME 1. REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPETITIVE IN
- [SDR FDEA202107011641](https://openairdocs.org/sdr/FDEA202107011641.md): Frame · dented · Jul 1, 2021 · N311FE · Doug MD1030F · Fuselage Main, Frame
  > CABIN - LEFT HAND STATION 1541 LONGERON 12 LEFT FRAME FOUND DENT. CABIN AT LEFT HAND FRAME STATION 1541 LONGERON 12 LEFT DENT AREA REPAIRED AS PER SRM 53-30-00 FIGURE 4 VOLUME 1. REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPETITIVE INSP
- [SDR FDEA202107011634](https://openairdocs.org/sdr/FDEA202107011634.md): Seat Track · corroded · Jul 1, 2021 · N311FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - RIGHT HAND STATION 1821 - 1861 X = - 8.5 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND STATION 1821 TO STATION 1861, X = - 8.5 CORROSION AT SEAT TRACK EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME 1. CORRODE
- [SDR FDEA202107011636](https://openairdocs.org/sdr/FDEA202107011636.md): Seat Track · corroded · Jul 1, 2021 · N311FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - LEFT HAND STATION 1236 - 1256 X = 47.5 SEAT TRACK FOUND CORROSION. CABIN AT LEFT HAND STATION 1236 TO STATION 1256, X = 47.5 CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME 1. CORRODED SEAT TRACK REPAI
- [SDR FDEA202107011640](https://openairdocs.org/sdr/FDEA202107011640.md): Seat Track · corroded · Jul 1, 2021 · N311FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - RIGHT HAND STATION 1401 - 1421 X = - 75.25 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND STATION 1401 TO STATION1421, X = - 75.25 CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME 1. CORRODED SEAT TRAC
- [SDR FDEA202107011639](https://openairdocs.org/sdr/FDEA202107011639.md): Seat Track · corroded · Jul 1, 2021 · N311FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - LEFT HAND STATION 1819 X = 27.5 SEAT TRACK FOUND CORROSION. CABIN AT LEFT HAND STATION 1819, X = 27.5 CORROSION AT SEAT TRACK EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME 1. CORRODED SEAT TRACK REPAIRED BY SE
- [SDR FDEA202107011638](https://openairdocs.org/sdr/FDEA202107011638.md): Seat Track · corroded · Jul 1, 2021 · N311FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - LEFT HAND STATION 1841 X = 8.5 SEAT TRACK FOUND CORROSION. CABIN AT LEFT HAND STATION 1841, X = 8.5 CORROSION AT SEAT TRACK EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME 1. CORRODED SEAT TRACK REPAIRED BY SECT
- [SDR FDEA202107011637](https://openairdocs.org/sdr/FDEA202107011637.md): Seat Track · corroded · Jul 1, 2021 · N311FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - RIGHT HAND STATION 1305 - 1339 X = - 75.25 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND STATION 1305 TO STA 1339, X = - 75.25 CORROSION AT SEAT TRACK EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME1. CORRODED
- [SDR FDEA202107011635](https://openairdocs.org/sdr/FDEA202107011635.md): Seat Track · corroded · Jul 1, 2021 · N311FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - RIGHT HAND STATION 1215 X = - 75.25 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND STATION 1215, X = - 75.25 CORROSION AT SEAT TRACK EVALUATED,FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME 1. CORRODED SEAT TRACK REPAIRE

Next page: https://openairdocs.org/deregistered/N311FE-2024-08-01/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 = 'N311FE' AND deregistration_id = 'N311FE-2024-08-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N311FE-2024-08-01/reports

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