# Service difficulty reports: N645FE, cancelled Mar 2, 2024

A list on [N645FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N645FE-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 2 · 74 reports

- [SDR FDEA201501310398](https://openairdocs.org/sdr/FDEA201501310398.md): Lens · broken · Jan 31, 2015 · N645FE · Doug MD11F · Emergency Equipment
  > EVACUATION SLIDE REMOTE PRESS TO TEST INDICATING SYS INOPERATION COVER BROKEN. REPLACED PTT LENS AND LAMP REATAINER. OPS CHECK GOOD
- [SDR FDEA201307041478](https://openairdocs.org/sdr/FDEA201307041478.md): Transmitter · inoperative · Jul 4, 2013 · N645FE · Doug MD11F · Engine Fuel Indicating System
  > SHORTLY AFTER BEGINNING TAKEOFF ROLL, NR 1 FUEL FLOW SHOWED AMBER X. REJECTED TAKEOFF AT ABOUT 60 TO 70 KTS. FUEL FLOW INDICATING NORMAL AGAIN WHILE TURNING OFF RUNWAY. TROUBLESHOOTING FOUND FUEL LEAK FROM THE FUEL FLOW TRANSMITTER. R & R NE 1 ENGINE FUEL
- [SDR FDEA201307021466](https://openairdocs.org/sdr/FDEA201307021466.md): Skin · separated · Jul 2, 2013 · N645FE · Doug MD11F · Ailerons
  > RIGHT WING INBD AILERON T/E FOUND SKIN SEPARATED. REPAIRED RIGHT WING INBOARD AILERON TRAILING EDGE AS PER SRM 57- 50-02 REPAIR 3 FIGURE 201 REVISION 52 AND EA 1-5750-T0301032 PART 1. REPAIR CLASSIFIED CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.
- [SDR FDEA201307011428](https://openairdocs.org/sdr/FDEA201307011428.md): Skin · delaminated · Jul 1, 2013 · N645FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING OTBD FLAP LOWER SURFACE T/E FOUND DELAMINATED XOFH 681.500 TO XOFH 689.500. REPAIRED IAW EA 1-5750-T0300982. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201307011427](https://openairdocs.org/sdr/FDEA201307011427.md): Skin · delaminated · Jul 1, 2013 · N645FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING OTBD FLAP LOWER SURFACE T/E FOUND DELAMINATED XOFH 553.00 TO XOFH 568.00. REPAIRED IAW EA 1-5750-T0300982. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 116.
- [SDR FDEA201307011426](https://openairdocs.org/sdr/FDEA201307011426.md): Skin · delaminated · Jul 1, 2013 · N645FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING OTBD FLAP LOWER SURFACE FOUND DELAMINATED XOFH 673.542 TO XOFH 667.542. REPAIRED IAW EA 1-5750-T0300985 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201307011425](https://openairdocs.org/sdr/FDEA201307011425.md): Skin · delaminated · Jul 1, 2013 · N645FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING OTBD FLAP T/E, LOWER SURFACE FOUND DELAMINATED XOFH 527.690 TO XOFH 552.690. REPAIRED IAW EA 1-5750-T0300985, PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REVISION 116.
- [SDR FDEA201307011424](https://openairdocs.org/sdr/FDEA201307011424.md): Skin · delaminated · Jul 1, 2013 · N645FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING OTBD FLAP T/E, UPPER SURFACE FOUND DELAMINATED AT XOFH 524.690 TO XOFH 554.690. REPAIRED IAW EA 1-5750-T0300985, PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201306241379](https://openairdocs.org/sdr/FDEA201306241379.md): Skin · cracked · Jun 24, 2013 · N645FE · Doug MD11F · Wing, Plate/Skin
  > TEN FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION, RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS= 683.4 AND 713.6. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. REPAIR CLASSIFIED
- [SDR FDEA201306241378](https://openairdocs.org/sdr/FDEA201306241378.md): Skin · cracked · Jun 24, 2013 · N645FE · Doug MD11F · Wing, Plate/Skin
  > EIGHT FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS. DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ONE LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 683.4 AND 713.6. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. REPAIR
- [SDR FDEA201306211363](https://openairdocs.org/sdr/FDEA201306211363.md): Fitting · corroded · Jun 21, 2013 · N645FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING INBD FLAP DRIVE ARM SUPPORT BORE FOUND CORRODED. BORE REWORKED IAW SRM 51-21-01 REVISION 52 REPAIRED IAW EA 1-5750-T0300933A PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306211362](https://openairdocs.org/sdr/FDEA201306211362.md): Hinge · corroded · Jun 21, 2013 · N645FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT INBD FLAP, OTBD HINGE (FLAP MOUNTED) PIVOT ATTACHMENT OTBD LUG BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. REPAIRED IAW EA 1-5750-T0300874 B PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306211361](https://openairdocs.org/sdr/FDEA201306211361.md): Hinge · corroded · Jun 21, 2013 · N645FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT INBD FLAP, OTBD HINGE (FLAP MOUNTED) PIVOT ATTACHMENT INBD LUG BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. REPAIRED IAW EA 1-5750-T0300874 B PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306211360](https://openairdocs.org/sdr/FDEA201306211360.md): Hinge Bracket · corroded · Jun 21, 2013 · N645FE · Doug MD11F · Trailing Edge Flaps
  > LEFT INBD FLAP, OTBD HINGE (FLAP MOUNTED) PIVOT ATTACHMENT INBOARD LUG BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. REPAIRED IAW EA 1-5750-T0300889. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306211359](https://openairdocs.org/sdr/FDEA201306211359.md): Hinge Bracket · corroded · Jun 21, 2013 · N645FE · Doug MD11F · Trailing Edge Flaps
  > LT INBD FLAP, OTBD HINGE (FLAP MOUNTED) PIVOT ATTACHMENT OTBD LUG, BORE FOUND CORRODED. BORE REWORKED FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. REPAIRED IAW EA 1-5750-T0300889. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306191343](https://openairdocs.org/sdr/FDEA201306191343.md): Frame · dented · Jun 19, 2013 · N645FE · Doug MD11F · Fuselage Main, Frame
  > FRAME BS 1761, LONGERON 12L FOUND DENTED. REPAIRED IAW SRM 53- 00-07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR AS IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306181332](https://openairdocs.org/sdr/FDEA201306181332.md): Frame · dented · Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, Frame
  > FRAME, BS 1701, LONGERON 12R FOUND DENTED. REPAIR CARRIED OUT IAW SRM 53-00 07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306181328](https://openairdocs.org/sdr/FDEA201306181328.md): Frame · dented · Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, Frame
  > FRAME BS 1721, LONGERON 12R, FOUND DENTED. REPAIR CARRIED OUT IAW SRM 53-00 07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306181326](https://openairdocs.org/sdr/FDEA201306181326.md): Frame · dented · Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, Frame
  > RIGHT FRAME BS 1641, LONGERON 12R FOUND DENTED. REPAIR CARRIED OUT IAW SRM 53-00 07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306181322](https://openairdocs.org/sdr/FDEA201306181322.md): Frame · chafed · Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, Frame
  > CABIN - LEFT SUPPORT YOKE, BS 535, LONGERON 19L, FRAME FOUND CHAFED. REPAIRED IAW SRM 53-20-07 FIGURE 202 REPAIR 1 REVISION 52. CLASSIFIED A MAJOR REPAIR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306181331](https://openairdocs.org/sdr/FDEA201306181331.md): Frame · dented · Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, Frame
  > FRAME BS 1681, LONGERON 12L FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306181329](https://openairdocs.org/sdr/FDEA201306181329.md): Frame · dented · Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, Frame
  > FRAME BS 1701, LONGERON 12L FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306181324](https://openairdocs.org/sdr/FDEA201306181324.md): Frame · chafed · Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, Frame
  > LEFT SUPPORT YOKE BS 535, LONGERON 21L FRAME FOUND CHAFED. REPAIRED IAW SRM 53-20-07 FIGURE 201 REPAIR 1 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306181319](https://openairdocs.org/sdr/FDEA201306181319.md): Skin · chafed · Jun 18, 2013 · N645FE · Doug MD11F · Ailerons
  > LEFT INBD AILERON LOWER SKIN CHAFED AT TWO LOCATIONS. DAMAGED SKIN REMOVED AND FABRICATED NEW SKIN AS PER EA 1-5750-T0300853 AND REPLACED. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 116.
- [SDR FDEA201302210403](https://openairdocs.org/sdr/FDEA201302210403.md): Unknown · unknown · Feb 21, 2013 · N645FE · Doug MD11F · Trailing Edge Flap Control System
  > REJECT TAKE OFF AT 85 KTS FOR FLAP WARNING ON EAD. PERFORMED R-T-S OF NR 1 AND NR 2 FCC'S IAW MM 27-54-00-5. RAN FLAPS FULL TRAVEL DOWN AND UP ALL INDICATIONS NORMAL. BOTH FCC'S PASSED R-T-S.
- [SDR FDEA201301200151](https://openairdocs.org/sdr/FDEA201301200151.md): Landing Gear · malfunctioned · Jan 20, 2013 · N645FE · Doug MD11F · Landing Gear Retraction/Extension System
  > ON APPROACH, THE EAD DISPLAYED A WHITE BOX WITH "LANDING GEAR." THE "GEAR UNSAGE INDICATION WITH GEAR HANDLE DOWN," QRH CHECKLIST WAS ACCOMPLISHED. ON SECOND APPROACH ALL INDICATION NORMAL. PVG U CONSULTED WITH CREW, KNEW THAT SECOND L/G INDICATION ON LT
- [SDR FDEA201107192789](https://openairdocs.org/sdr/FDEA201107192789.md): Skin · corroded · Jul 19, 2011 · N645FE · Doug MD11F · Fuselage Main, Plate/Skin
  > MAIN DECK INTERIOR, FOUND UNDERFLOOR STRUCTURE AT STA. 1230, LBL 103" WTH CORROSION. EXCEEDED LIMIT PER SRM57-10-01 FIG 101 REV 46. HFEC INSPECTION FOUND NO CRACKS. MAIN DECK INTERIOR STA.1230 LBL 103 UNDERFLOOR DOUBLER / SHIM FABRICATED & INSTALLED P
- [SDR FDEA201107192788](https://openairdocs.org/sdr/FDEA201107192788.md): Skin · corroded · Jul 19, 2011 · N645FE · Doug MD11F · Fuselage Main, Plate/Skin
  > MAIN DECK INTERIOR, FOUND UNDERFLOOR STRUCTURE AT STA.1203", LBL 103" WITH CORROSION. CORROSION REMOVED PER SRM51-21-01 REV 46. EXCEEDED LIMIT PER SRM57-10-01 FIG 101 REV 46. HFEC INSPECTION FOUND NO CRACKS. FABRICATED & INSTALLED REPAIR PER EA 1-5730-15
- [SDR FDEA201107192787](https://openairdocs.org/sdr/FDEA201107192787.md): Skin · corroded · Jul 19, 2011 · N645FE · Doug MD11F · Fuselage Miscellaneous Structure
  > MAIN DECK INTERIOR, FOUND UNDERFLOOR STRUCTURE AT STA 1235,RBL 51" WITH CORROSION. CORROSION REMOVED PER SRM51-21-01 REV 46. FOUND EXCEEDED LIMIT PER SRM 57-10-01 FIG 101 REV 46. CARRIED OUT ON REWORKED AREA FOUND NO CRACK & NO CORROSION. HFEC INSPECTION C
- [SDR FDEA201107192786](https://openairdocs.org/sdr/FDEA201107192786.md): Skin · cracked · Jul 19, 2011 · N645FE · Doug MD11F · Wing, Plate/Skin
  > RT WING FIXED L/E TELESCOPIC DUCT DOOR CUTOUT CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-01, FIG 202. REPAIR 10, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201107192785](https://openairdocs.org/sdr/FDEA201107192785.md): Skin · cracked · Jul 19, 2011 · N645FE · Doug MD11F · Wing, Plate/Skin
  > LT WING FIXED L/E TELESCOPIC DUCT DOOR CUTOUT CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-01 FIG 202, REV 46. REPAIR 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201107042559](https://openairdocs.org/sdr/FDEA201107042559.md): Skin · damaged · Jul 4, 2011 · N645FE · Doug MD11F · Fuselage Main, Plate/Skin
  > CABIN - DOOR 4 LT AFT CUTOUT INBD SKIN BETWEEN LONGERON 20 LT TO 21 LT SKIN PUNCTURED. DAMAGED AREA TRIMMED OUT PER SRM53-00-00 FIG 204 REV 46. HFEC INSPECTION CARRIED OUT ON TRIMMED AREA, FOUND NO CRACK. REPAIR DOUBLER FABRICATED AND INSTALLED PER SRM53-0
- [SDR FDEA201107012522](https://openairdocs.org/sdr/FDEA201107012522.md): Seat Track · corroded · Jul 1, 2011 · N645FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - LT STRUCTURE UNDER DADO SUPPORT FROM FRAME 5-113 TO 1541 FOUND CORRODED. CARRIED OUT SEAT TRACK SECTIONAL REPAIR PER SRM53-00-52 FIG 101 REV 46. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100 REV 112.
- [SDR FDEA201107012521](https://openairdocs.org/sdr/FDEA201107012521.md): Shroud · cracked · Jul 1, 2011 · N645FE · Doug MD11F · Aircraft Fuel Distribution System
  > AFT CARGO COMPARTMENT - TAIL TANK TRANSFER FUEL LINE SHROUD FOUND CRACKED AT STATION Y=2005 DURING CHECK. REPAIRED LINE, LEAK CHECK CARRIED OUT AS PER AMM 28-25-00-5 REV 70.0, NO LEAK FOUND. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.
- [SDR FDEA201106202342](https://openairdocs.org/sdr/FDEA201106202342.md): Bulkhead · misrepaired · Jun 20, 2011 · N645FE · Doug MD11F · Fuselage Main, Plate/Skin
  > REPAIR FOUND AT RT MLG WW HORIZONTAL PANEL CTR AREA SPLICE PLATE. FOUND MISREPAIRED. CARRIED OUT REPAIR AS PER EA1-5310-147672 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.
- [SDR FDEA201106132216](https://openairdocs.org/sdr/FDEA201106132216.md): Intercostal · corroded · Jun 13, 2011 · N645FE · Doug MD11F · Fuselage Miscellaneous Structure
  > LONGERON NR 20R BETWEEN STA 1341 TO STA 1361 CORRODED INTERCOSTAL REMOVED. NEW INTERCOSTAL FABRICATED IAW DWG AEA0163 REV 'C'. FPI CARRIED OUT ON NEW FABRICATED INTERCOSTAL FOUND NO CRACK. NEW FABRICATED INTERCOSTAL HOLES TRANSFERRED, PROTECTED, PAINTED, PA
- [SDR FDEA201106122209](https://openairdocs.org/sdr/FDEA201106122209.md): Structure · corroded · Jun 12, 2011 · N645FE · Doug MD11F · Fuselage Main, Structure
  > UPON REMOVAL OF LT WINDSHIELD, CUTOUT AREA FOUND CORRODED. CARRIED OUT REPAIR IAW EA 1-5310-147652, REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100, REV 112.
- [SDR FDEA201106102197](https://openairdocs.org/sdr/FDEA201106102197.md): Spar · cracked · Jun 10, 2011 · N645FE · Doug MD11F · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER REAR SPAR NR 4 BANJO FITTING SUSPECT CRACK AT STA 2164 AND ZID 54.5 AREA. (REFER TO SRM 55-30-02, FIG 201). REPAIRED AS PER SRM 55-30-02 FIG 201 REPAIR 3 REV 46. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112. TO CARRY OU
- [SDR FDEA201106072141](https://openairdocs.org/sdr/FDEA201106072141.md): Longeron · corroded · Jun 7, 2011 · N645FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPARTMENT, DURING REPAIR OF CORROSION LONG.48R STA 1059-1079 FOUND OUT CORROSION AT STA 1099 OF LONG 48R. CORRODED AREA REMOVED IAW SRM 51-21-01, REV 46. ORIGINAL THICKNESS: 0.080" & REMAINING THICKNESS: 0.00" FOUND EXCEEDED LIMIT IAW SRM 53-0
- [SDR FDEA201106072139](https://openairdocs.org/sdr/FDEA201106072139.md): Seat Track · corroded · Jun 7, 2011 · N645FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > LT SEAT TRACK UNDER DADO SUPPORT FROM FRAME 5-53 TO 5-73 FOUND CORRODED. CARRIED OUT SEAT TRACK SECTION REPAIR. REPAIR CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201106022094](https://openairdocs.org/sdr/FDEA201106022094.md): Hinge Fitting · corroded · Jun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE FOUND CORRODED. REPAIRED IAW EA1-5740-147656. EXISTING HOLE: 2.252" FINAL HOLE: 2.3185" MAX HOLE: 2.3135". NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5740-147656. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-
- [SDR FDEA201106022093](https://openairdocs.org/sdr/FDEA201106022093.md): Hinge Fitting · corroded · Jun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RT WING OTBD FLAP INBD HINGE (WING SIDE) SIDE LINK HOLE FOUND SURFACE CORRODED. REWORKED IAW CMM 20-11-02, REV 70. UPPER FACE EXISTING THICKNESS 0.481", MATERIAL REMOVED 0.003", REMAINING THICKNESS 0.478", LOWER FACE EXISTING THICKNESS 0.486" MATERIAL REMOVE
- [SDR FDEA201106022092](https://openairdocs.org/sdr/FDEA201106022092.md): Hinge Fitting · corroded · Jun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RT WING OTBD FLAP, OTBD HINGE (WING SIDE) SIDE LINK HOLE, FOUND SURFACE CORRODED. REWORKED IAW EA 1-5740-147651. EXISTING THICKNESS 0.3845", MATERIAL REMOVED 0.003", REMAINING THICKNESS 0.3815". REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201106022091](https://openairdocs.org/sdr/FDEA201106022091.md): Hinge Fitting · corroded · Jun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LEFT WING OTBD FLAP, INBD HINGE (WING SIDE) SIDE LINK HOLE SPOT FACE, FOUND CORRODED. REPAIRED IAW EA 1-5740-147655. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201106022090](https://openairdocs.org/sdr/FDEA201106022090.md): Hinge Fitting · corroded · Jun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LEFT WING OTBD FLAP, OTBD HINGE (WING SIDE) SIDE LINK HOLE SPOT FACE, FOUND CORRODED. REWORKED IAW CMM 20-11-02 REV 70. REMOVED: 0.003", FOUND THE REMAINING THICKNESS OF 0.460" AND 0.464" IS WITHIN DWG ARC 503 SHEET 2 BG LIMITS AND CMM 57-44-09 REV 70 FIG.
- [SDR FDEA201106022089](https://openairdocs.org/sdr/FDEA201106022089.md): Hinge Fitting · corroded · Jun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LEFT WING OTBD FLAP, OTBD HINGE (WING SIDE) LOWER INBD MOUNT HOLE SPOT FACE FOUND CORRODED. REPAIRED IAW EA 1-5740-147654. EXISTING THICKNESS: 0.439", MATERIAL REMOVED: 0.003"(FWD), MATERIAL REMOVED: 0.050"(AFT). REMAINING THICKNESS: 0.386",MINIMUM THICKN
- [SDR FDEA201106022088](https://openairdocs.org/sdr/FDEA201106022088.md): Hinge Fitting · corroded · Jun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LEFT WING OTBD FLAP, OTBD HINGE (WING SIDE) UPPER OTBD MOUNT HOLE FOUND CORRODED. REWORKED IAW EA 1-5740-147654, PART 1(B). EXISTING HOLE: 0.881", FINAL HOLE: 0.947", MAX.HOLE: 0.944". NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5740-147654, PART 1(B).
- [SDR FDEA201106022087](https://openairdocs.org/sdr/FDEA201106022087.md): Hinge Fitting · corroded · Jun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LEFT WING OTBD FLAP, OTBD HINGE (WING SIDE) PIVOT HOLE FOUND CORRODED. REWORKED IAW EA 1-5740-147654 PART 1 A. EXISTING HOLE 2.251", FINAL HOLE 2.352", NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5740-147654, PART 1 A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-1
- [SDR FDEA201106022086](https://openairdocs.org/sdr/FDEA201106022086.md): Floor Support · corroded · Jun 2, 2011 · N645FE · Doug MD11F · Fuselage Miscellaneous Structure
  > RT FLOOR STRUCTURE BELOW DADO PANEL SUPPORT FROM STATION 1501 TO STATION 1521 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 101, REV 46.
- [SDR FDEA201106022085](https://openairdocs.org/sdr/FDEA201106022085.md): Support · corroded · Jun 2, 2011 · N645FE · Doug MD11F · Fuselage Miscellaneous Structure
  > LEFT STRUCTURE UNDER DADO SUPPORT FROM STATION 1481 TO STATION 1501, FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, REV 46. ORIGINAL THICKNESS: 0.080", MATERIAL REMOVED 0.026" & REMAINING THICKNESS: 0.054" FOUND EXCEEDED LIMIT IAW SRM 53-00-52 FIG 101,

Next page: https://openairdocs.org/deregistered/N645FE-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 = 'N645FE' AND deregistration_id = 'N645FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N645FE-2024-03-02/reports

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