# Service difficulty reports: N577FE, cancelled Mar 2, 2024

A list on [N577FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N577FE-2024-03-02.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 6 · 256 reports

- [SDR FDEA201310022380](https://openairdocs.org/sdr/FDEA201310022380.md): Window · loose · Oct 2, 2013 · N577FE · Doug MD11F · Emergency Equipment
  > LEFT SIDE COCKPIT ESCAPE ROPE VIEWING DOOR GLASS IS LOOSE. CORRECTLY INSTALLED VIEWING GLASS.
- [SDR FDEA201204241541](https://openairdocs.org/sdr/FDEA201204241541.md): Skin · misrepaired · Apr 24, 2012 · N577FE · Doug MD11F · Leading Edge Devices
  > RT WING NR 5 SLAT AFT SURFACE OTBD LOWER CORNER STA XORS 682 MISREPAIRED. REPAIRED IAW EA 1-5750-160032. CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 114.
- [SDR FDEA201204241539](https://openairdocs.org/sdr/FDEA201204241539.md): Skin · misrepaired · Apr 24, 2012 · N577FE · Doug MD11F · Leading Edge Devices
  > RT WING NR 8 SLAT UPPER SURFACE STATION XORS 995 MISREPAIRED. REPAIRED IAW EA 1-5750-160031 PART 1. CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 114.
- [SDR FDEA201204191487](https://openairdocs.org/sdr/FDEA201204191487.md): Skin · misrepaired · Apr 19, 2012 · N577FE · Doug MD11F · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON EXTERIOR APPROX STA Y = 2334 FOUND MISREPAIRED. REPAIRED IAW EO E1-5100-7-5001B PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
- [SDR FDEA201204171449](https://openairdocs.org/sdr/FDEA201204171449.md): Skin · misrepaired · Apr 17, 2012 · N577FE · Doug MD11F · Leading Edge Devices
  > LT WING SKIN AT NR 3 SLAT LOWER SURFACE XORS 372. REPAIRED IAW EA1-5750-159830. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
- [SDR FDEA201204161431](https://openairdocs.org/sdr/FDEA201204161431.md): Skin · misrepaired · Apr 16, 2012 · N577FE · Doug MD11F · Fuselage Main, Plate/Skin
  > SKIN AT BS 2147 - 2160, L33L MISREPAIRED. REPAIRED IAW SRM 53-70-01 FIGURE 201 REPAIR 3 REVISION 49 & EO E1-5100-7-5001B PT1. MAJOR REPAIR.
- [SDR FDEA201204141399](https://openairdocs.org/sdr/FDEA201204141399.md): Attach Fitting · cracked · Apr 14, 2012 · N577FE · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AROUND STOP DRILL HOLE OF LT NOSE LANDING GEAR TRUNNION FITTING FOUND ONE NEW ADDITIONAL CRACK PROPAGATED FROM THE STOP DRILL HOLE TOWARDS THE LOWER EDGE, APPROX 0.25". REPAIR CARRIED OUT AT LT NLG TRUNNION FITTIN
- [SDR FDEA201204121373](https://openairdocs.org/sdr/FDEA201204121373.md): Longeron · cracked · Apr 12, 2012 · N577FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > FOUND LONGERON 49 LT FASTENER HOLE (COMMON TO NLG TRUNNION FITTING) CRACKED, APPROX 0.025". LONGERON REMOVED IAW SRM 51-31-01, REV 49. NEW LONGERON FABRICATED IAW DWG ACA 3796 REV A. NEW FABRICATED LONGERON INSTALLED IAW SRM 51-31-01, REV 49. REPAIR CLASS
- [SDR FDEA201204101337](https://openairdocs.org/sdr/FDEA201204101337.md): Frame · misrepaired · Apr 10, 2012 · N577FE · Doug MD11F · Fuselage Main, Frame
  > FRAME STA 535 AT LONGERON 19 LT MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
- [SDR FDEA201204101335](https://openairdocs.org/sdr/FDEA201204101335.md): Skin · misrepaired · Apr 10, 2012 · N577FE · Doug MD11F · Trailing Edge Flaps
  > RT WING INBD FLAP UPPER SURFACE MISREPAIRED. REPAIRED IAW SRM 57-00-01, FIG 201, REPAIR 1, REV 49.
- [SDR FDEA201204101334](https://openairdocs.org/sdr/FDEA201204101334.md): Frame · misrepaired · Apr 10, 2012 · N577FE · Doug MD11F · Fuselage Main, Plate/Skin
  > CABIN AT FRAME BS 535, LONGERON 23L FOUND MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 201 REPAIR 1, REV 49. CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
- [SDR FDEA201204101344](https://openairdocs.org/sdr/FDEA201204101344.md): Skin · corroded · Apr 10, 2012 · N577FE · Doug MD11F · Fuselage Miscellaneous Structure
  > MAIN DECK UPPER CARGO COMPARTMENT UNDER FLOOR AT CENTER WING TANK BETWEEN BS 1219 TO 1239, "X" = -90 TO "X" = -107.5 FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.180", REMAINING THICKNE
- [SDR FDEA201204101343](https://openairdocs.org/sdr/FDEA201204101343.md): Skin · corroded · Apr 10, 2012 · N577FE · Doug MD11F · Fuselage Miscellaneous Structure
  > MAIN DECK UPPER CARGO COMPARTMENT UNDER FLOOR AT CENTER WING TANK BETWEEN BS 1219 TO 1239, "X" = -75.25 TO "X" = -90 FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.168", REMAINING THICKN
- [SDR FDEA201204101342](https://openairdocs.org/sdr/FDEA201204101342.md): Skin · corroded · Apr 10, 2012 · N577FE · Doug MD11F · Fuselage Miscellaneous Structure
  > MAIN DECK UPPER CARGO COMPARTMENT UNDER FLOOR AT CENTER WING TANK BETWEEN STATION 1219 TO STATION 1239, "X" = -75.25. FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.171", REMAINING T
- [SDR FDEA201204101341](https://openairdocs.org/sdr/FDEA201204101341.md): Skin · corroded · Apr 10, 2012 · N577FE · Doug MD11F · Fuselage Miscellaneous Structure
  > MAIN DECK UPPER CARGO COMPARTMENT, UNDER FLOOR AT CENTER WING TANK BETWEEN STATION 1219 TO STATION 1239, "X" = -27.5 FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.175", REMAINING TH
- [SDR FDEA201204101340](https://openairdocs.org/sdr/FDEA201204101340.md): Skin · corroded · Apr 10, 2012 · N577FE · Doug MD11F · Fuselage Miscellaneous Structure
  > MAIN DECK UPPER CARGO COMPARTMENT, UNDER FLOOR AT CTR WING TANK BETWEEN BS 1219 TO 1239, "X" = -8.5 TO "X = -27.5. FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.182", REMAINING THICKN
- [SDR FDEA201204101339](https://openairdocs.org/sdr/FDEA201204101339.md): Longeron · corroded · Apr 10, 2012 · N577FE · Doug MD11F · Fuselage Main, Structure
  > CENTER CARGO COMPARTMENT, BILGE AREA BS 1646 LONGERON 50 LT FOUND WITH SURFACE CORROSION. REPAIR CARRIED OUT AT CENTER CARGO COMPARTMENT BILGE AREA STA 1646, LONGERON 50L IAW EA 1-5310-159838. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
- [SDR FDEA201204101338](https://openairdocs.org/sdr/FDEA201204101338.md): Longeron · corroded · Apr 10, 2012 · N577FE · Doug MD11F · Fuselage Main, Structure
  > CENTER CARGO COMPARTMENT BS 1676 LONGERON 51 LT FOUND WITH SURFACE CORROSION. REPAIRED IAW SRM 53-00-05, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
- [SDR FDEA201204101333](https://openairdocs.org/sdr/FDEA201204101333.md): Skin · cracked · Apr 10, 2012 · N577FE · Doug MD11F · Vertical Stabilizer, Plate/Skin
  > LOWER VERTICAL STABILIZER FOUND RT SIDE REAR CENTER SPAR TO REAR SPAR LOWER PANEL CRACKED. REPAIR CARRIED OUT IAW SRM 55-30-02, FIG 201, REPAIR 2, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114. NR 2 ENGINE FIRE DETECTION CONTROL UNIT CARRIED
- [SDR FDEA201204101332](https://openairdocs.org/sdr/FDEA201204101332.md): Skin · corroded · Apr 10, 2012 · N577FE · Doug MD11F · Fuselage Main, Plate/Skin
  > AFT ACCESSORY COMPARTMENT, FOUND CORROSION ON RT SKIN BS 2163 BODY FAIRING CUTOUT LOCATION. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL THICKNESS: 0.95", MATERIAL REMOVED: 0.80", REMAINING 0.015" AND FOUND EXCEED LIMIT IAW SRM 53-70-01, FIG 201, RE
- [SDR FDEA201204091326](https://openairdocs.org/sdr/FDEA201204091326.md): Longeron · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTER ACCESSORY COMPARTMENT STA 6-95, LONGERON 43 RT FOUND WITH CORROSION. REPAIRED IAW EA 1-5310-157171, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
- [SDR FDEA201204091324](https://openairdocs.org/sdr/FDEA201204091324.md): Bushing · worn · Apr 9, 2012 · N577FE · Doug MD11F · Trailing Edge Flaps
  > RT WING (FLAP SIDE) OTBD FLAP, OTBD HINGE, OTBD PIVOT HOLE BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.152" AND FOUND EXCEED LIMIT IAW CMM 57-52-04, REV 72. MAXIMUM ALLOWABLE DIAMETER 1.150". REPAIR ACCOMPLISHED
- [SDR FDEA201204091323](https://openairdocs.org/sdr/FDEA201204091323.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RT WING (WING SIDE) OTBD FLAP, OTBD HINGE, OTBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72. EXISTING BORE DIAMETER 1.222". FINAL BORE DIAMETER 1.246", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR CARRIED OUT EA 1-
- [SDR FDEA201204091322](https://openairdocs.org/sdr/FDEA201204091322.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RT WING (WING SIDE) OTBD FLAP, OTBD HINGE, INBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING BORE DIAMETER = 1.2215", FINAL BORE DIAMETER 1.246", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED E
- [SDR FDEA201204091321](https://openairdocs.org/sdr/FDEA201204091321.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RT WING (WING SIDE) OTBD FLAP, OTBD HINGE, LOWER MOUNT, OTBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. OTBD BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING BORE DIAMETER = 0.597", FINAL BORE DIAMETER 0.612", M
- [SDR FDEA201204091320](https://openairdocs.org/sdr/FDEA201204091320.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT, INBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. INBOARD HOLE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING BORE DIAMETER = 0.581", FINAL BORE DIAMETER 0.612",
- [SDR FDEA201204091319](https://openairdocs.org/sdr/FDEA201204091319.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LT WING (WING SIDE) OTBD FLAP, INBD HINGE, OTBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 72. ORIGINAL BORE DIAMETER = 1.2295", FINAL BORE DIAMETER 1.236", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED E
- [SDR FDEA201204091318](https://openairdocs.org/sdr/FDEA201204091318.md): Bushing · worn · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LT WING (WING SIDE) OTBD FLAP, INBD HINGE, INBD ACTUATOR HOLE BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, DIAMETER = 1.231" AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 72. MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMP
- [SDR FDEA201204091317](https://openairdocs.org/sdr/FDEA201204091317.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LT WING (WING SIDE) OTBD FLAP, INBD HINGE LOWER MOUNT OTBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 72. EXISTING HOLE DIAMETER:0.707", FINAL HOLE DIAMETER 0.713", MAXIMUM AL
- [SDR FDEA201204091316](https://openairdocs.org/sdr/FDEA201204091316.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LT WING (WING SIDE) OTBD FLAP, INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 72. UPPER EXISTING THICKNESS: 0.400", MATERIAL REMOVED: 0.004", REMAINING THICKNESS: 0.396". LOWER EXISTING THICKNESS: 0.387", MATERIAL REMOV
- [SDR FDEA201204091314](https://openairdocs.org/sdr/FDEA201204091314.md): Bushing · worn · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LT WING (WING SIDE) OTBD FLAP, OTBD HINGE, INBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE DIAMETER 1.251" AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. MAXIMUM ALLOWABLE DIAMETER: 1.220". REPAIR ACCOMPLISHED EA 1-5750-
- [SDR FDEA201204091312](https://openairdocs.org/sdr/FDEA201204091312.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LT WING (WING SIDE) OTBD FLAP, OTBD HINGE SIDE LOAD FITTING SURFACE FOUND CORROSION. REWORKED IAW CMM 20-11-02, REVISION 72. UPPER EXISTING THICKNESS: 0.425", MATERIAL REMOVED: 0.009", REMAINING THICKNESS: 0.416". LOWER EXISTING THICKNESS: 0.413", MATERIAL
- [SDR FDEA201204091311](https://openairdocs.org/sdr/FDEA201204091311.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LT WING (WING SIDE) OTBD FLAP, OTBD HINGE, SIDE LOAD FITTING LOWER HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE REWORKED AND FOUND EXCEEDED LIMIT CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.389", FINAL HOLE DIAMETER 0.408", MAXIMUM
- [SDR FDEA201204091310](https://openairdocs.org/sdr/FDEA201204091310.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LT WING (WING SIDE) OTBD FLAP, OTBD HINGE SIDE LOAD FITTING UPPER HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. UPPER HOLE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.389", FINAL HOLE DIAMETER 0.408",
- [SDR FDEA201204091309](https://openairdocs.org/sdr/FDEA201204091309.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT, OTBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. OTBD BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.581", FINAL HOLE DIAMETER 0.596", MAXIM
- [SDR FDEA201204091308](https://openairdocs.org/sdr/FDEA201204091308.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. INBD BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.580", FINAL HOLE DIAMETER 0.5975", MAXI
- [SDR FDEA201204091307](https://openairdocs.org/sdr/FDEA201204091307.md): Bushing · worn · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RT WING (WING SIDE) OTBD FLAP, INBD HINGE, OTBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, DIAMETER 1.252" FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. MAXIMUM ALLOWABLE DIAMETER: 1.220". REPAIR ACCOMPLISHED IAW
- [SDR FDEA201204091306](https://openairdocs.org/sdr/FDEA201204091306.md): Hinge Fitting · damaged · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RT WING (WING SIDE) OTBD FLAP, INBD HINGE, INBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.253" AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. MAXIMUM ALLOWABLE DIAMETER 1.220", REPAIR ACCOMPLISHED IAW E
- [SDR FDEA201204091305](https://openairdocs.org/sdr/FDEA201204091305.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RT WING (WING SIDE) OTBD FLAP, INBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. LOWER MOUNT INBD BORE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING BORE DIAMETER 0.705", FINAL BORE DIAMETER 0.7
- [SDR FDEA201204091304](https://openairdocs.org/sdr/FDEA201204091304.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RT WING (WING SIDE) OTBD FLAP, INBD HINGE LOWER MOUNT OTBD HOLE, FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. LOWER MOUNT OTBD BORE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING BORE DIAMETER 0.708", FINAL BORE DIAMETER 0.7
- [SDR FDEA201204091303](https://openairdocs.org/sdr/FDEA201204091303.md): Hinge Fitting · corroded · Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RT WING (WING SIDE) OTBD FLAP, INBD HINGE SIDE LOAD FITTING SURFACE, FOUND CORRODED. REWORKED IAW CMM 20-11-02 REV 72. UPPER EXISTING THICKNESS: 0.412", MATERIAL REMOVED: 0.005", REMAINING THICKNESS: 0.407". LOWER EXISTING THICKNESS: 0.403", MATERIAL REMO
- [SDR FDEA201204091301](https://openairdocs.org/sdr/FDEA201204091301.md): Hinge Fitting · damaged · Apr 9, 2012 · N577FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING (FLAP SIDE), INBD FLAP OTBD HINGE, OTBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, OTBD LUG DIAMETER 1.254", OTBD STRAP DIAMETER 1.190" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE D
- [SDR FDEA201204091300](https://openairdocs.org/sdr/FDEA201204091300.md): Hinge Fitting · damaged · Apr 9, 2012 · N577FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, INBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURE, INBD LUG, DIAMETER 1.283", INBD STRAP DIAMETER 1.217" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DI
- [SDR FDEA201204091299](https://openairdocs.org/sdr/FDEA201204091299.md): Hinge Fitting · damaged · Apr 9, 2012 · N577FE · Doug MD11F · Trailing Edge Flaps
  > RT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, OTBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, OTBD LUG DIAMETER 1.250", OTBD STRAP DIAMETER 1.21" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DIAM
- [SDR FDEA201204091298](https://openairdocs.org/sdr/FDEA201204091298.md): Hinge Fitting · damaged · Apr 9, 2012 · N577FE · Doug MD11F · Trailing Edge Flaps
  > RT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, INBD PIVOT HOLE FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURE, INBD LUG DIAMETER 1.252 IN, INBD STRAP DIAMETER 1.218" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DIA
- [SDR FDEA201204071285](https://openairdocs.org/sdr/FDEA201204071285.md): Skin · cracked · Apr 7, 2012 · N577FE · Doug MD11F · Wing, Plate/Skin
  > HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON LT WING FUEL TANK LOWER ACCESS DOOR PANEL NR 536AB CUTOUT AND FOUND CRACK INDICATION ON 04 EACH FASTENER HOLES. REPAIR CARRIED OUT IAW EA 1-5710-157169 PART 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 11
- [SDR FDEA201204071284](https://openairdocs.org/sdr/FDEA201204071284.md): Skin · cracked · Apr 7, 2012 · N577FE · Doug MD11F · Wing, Plate/Skin
  > HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON RT WING FUEL TANK LOWER ACCESS DOOR PANEL NR 636AB CUTOUT AND FOUND CRACK INDICATION ON 06 EACH FASTENER HOLES. REPAIR CARRIED OUT IAW EA 1-5710-157168 PART 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 11
- [SDR FDEA201204061275](https://openairdocs.org/sdr/FDEA201204061275.md): Skin · cracked · Apr 6, 2012 · N577FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING LOWER FIXED L/E AT REFUELING PANEL CUTOUT INBD FORWARD CORNER AREA FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02. REPAIR 7 FIG 201 REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 114.
- [SDR FDEA201204051266](https://openairdocs.org/sdr/FDEA201204051266.md): Skin · misrepaired · Apr 5, 2012 · N577FE · Doug MD11F · Wing, Plate/Skin
  > LT WING DROOP L/E UPPER SURFACE FOUND MISREPAIRED IAW SRM 57-40-01, REPAIR 5, FIGURE 201. REPAIRED IAW EA 1-5730-159836, CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
- [SDR FDEA201204051270](https://openairdocs.org/sdr/FDEA201204051270.md): Skin · cracked · Apr 5, 2012 · N577FE · Doug MD11F · Wing, Plate/Skin
  > RT WING FIXED L/E LOWER SURFACE AT NR 14 SLAT TRACK LOWER CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT RT WING FIXED L/E LOWER SURFACE AT NR 14 SLAT TRACK LOWER CUTOUT IAW SRM 57-40-02. REPAIR 7, FIG 201, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, RE

Next page: https://openairdocs.org/deregistered/N577FE-2024-03-02/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 = 'N577FE' AND deregistration_id = 'N577FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N577FE-2024-03-02/reports

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