# Service difficulty reports: N644FE, cancelled Mar 2, 2024

A list on [N644FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N644FE-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 3 · 117 reports

- [SDR FDEA201411063539](https://openairdocs.org/sdr/FDEA201411063539.md): Fire Bottle · discharged · Nov 6, 2014 · N644FE · Doug MD11F · Extinguishing System
  > MULTIPLE BIRD STRIKES DESCENDING TO 7000 FT. RECEIVED ENGINE FIRE AGENT LOW, AGENT 2 LOW NR 3 ENG, ALERT. NO ADDITIONAL ENG ANOMALIES NOTED. REMOVED NR 3 ENGINE, AND NR 2 FIRE BOTTLE IAW AMM 26-21-01-4. VERIFIED BOTTLE WAS DISCHARGED. CHECKED WIRING FROM F
- [SDR FDEA201311022674](https://openairdocs.org/sdr/FDEA201311022674.md): Pump · leaking · Nov 2, 2013 · N644FE · Doug MD11F · Hydraulic Pump (Electric/Engine), Main
  > LEVEL 2 NR 3 HYD FAIL ON SHORT FINAL, 3.9 GAL LEFT BOTH PUMPS WERE OFF. FOUND NR 3 FWD EDP LEAKING AT PUMP HSG ON ENGINE. R & R NR 3 ENGINE FWD EDP IAW AMM 29-11-20-4-2, SERVICE NR 3 HYD SYS TO PROPER LEVEL IAW AMM 12-13-02-3, DRY MOTORED NR 3 ENGINE IAW J
- [SDR FDEA201305100964](https://openairdocs.org/sdr/FDEA201305100964.md): Skin · cracked · May 10, 2013 · N644FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND STA XORS=713.6, SIX FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. REPAIR CLASSIF
- [SDR FDEA201305100963](https://openairdocs.org/sdr/FDEA201305100963.md): Skin · cracked · May 10, 2013 · N644FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND STA XORS=713.6. THREE FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. REPAIR CL
- [SDR FDEA201305080941](https://openairdocs.org/sdr/FDEA201305080941.md): Frame · dented · May 8, 2013 · N644FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK BS 1701, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305080940](https://openairdocs.org/sdr/FDEA201305080940.md): Frame · dented · May 8, 2013 · N644FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK BS 1661, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305080939](https://openairdocs.org/sdr/FDEA201305080939.md): Frame · dented · May 8, 2013 · N644FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK BS 1741, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305080938](https://openairdocs.org/sdr/FDEA201305080938.md): Frame · dented · May 8, 2013 · N644FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK BS 1701, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305080937](https://openairdocs.org/sdr/FDEA201305080937.md): Frame · dented · May 8, 2013 · N644FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK BS 1661, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REVISION 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305060918](https://openairdocs.org/sdr/FDEA201305060918.md): Vane · delaminated · May 6, 2013 · N644FE · Doug MD11F · Trailing Edge Flaps
  > RT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. R & R RT WING INBD FLAP VANE IAW AMM 27-50-22-4, REV 76.1 CARRIED OUT FLAP VANE ADJUSTMENT TEST IAW AMM 27-50-22-5, REV 76.1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305060917](https://openairdocs.org/sdr/FDEA201305060917.md): Seat Track · corroded · May 6, 2013 · N644FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - RT BS 1019 X= -8.5 SEAT TRACK FOUND CORROSION. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT BS 1009 TO 1049 IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REV 52 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201303200618](https://openairdocs.org/sdr/FDEA201303200618.md): Pitot Line · blocked · Mar 20, 2013 · N644FE · Doug MD11F · Pitot/Static System
  > RTO DUE TO IAS ALERT AT 90 KTS ON CAPTAIN`S SIDE. REPLACED CAPTAINS PITOT TUBE, FOUND BLOCKAGE.
- [SDR FDEA201302210401](https://openairdocs.org/sdr/FDEA201302210401.md): Buss · malfunctioned · Feb 21, 2013 · N644FE · Doug MD11F · AC Power Distribution System
  > ON FINAL, RECEIVED "EMER PWR ON" ALERT. AFTER LANDING, RECYCLED EMERGENCY POWER SWITCH AND CPT DISPLAY UNITS 1,2,3 WENT BLANK/DARK WITH NR 2 DISPLAY RED "X". TRIED TO RECYCLE AGAIN WITH NO CHANGE. DUPICATED SYMPTOMS AT BLOCK-IN. ON ELECTRICAL PAGE, FOUND
- [SDR FDEA201107092624](https://openairdocs.org/sdr/FDEA201107092624.md): Computer · failed · Jul 9, 2011 · N644FE · Doug MD11F · Instrument Panel
  > ON TAKEOFF F/O AND STBY FLT INSTRUMENTS WERE ERRATIC. FOUND BOTH FCC'S AND ALL 3 IRU'S WITH NUMEROUS FAULTS ON NR2 ADC, REPLACED NR2 ADC IAW AMM 34-16-01-4 CK'S GOOD. WHILE INSPECTING PITOT PROBES FOUND DEBRIS IN THE F/O'S PROBE AND SOME IN THE STANBY PROB
- [SDR FDEA201106012060](https://openairdocs.org/sdr/FDEA201106012060.md): Doubler · cracked · Jun 1, 2011 · N644FE · Doug MD11F · Fuselage Miscellaneous Structure
  > WHEEL COMPARTMENT LT FWD SIDE SPOILER MIXER ROD CUT-OUT DOUBLER FOUND CRACK. R & R AS SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201105302026](https://openairdocs.org/sdr/FDEA201105302026.md): Skin · chafed · May 30, 2011 · N644FE · Doug MD11F · Wing, Plate/Skin
  > RT WING L/E LOWER SKIN FOUND WITH CHAFE MARKS WHERE PYLON NR1- TO -WING FAIRING CONTACTS. CHAFED SKIN REMOVED AS PER SRM 51-33-01 AND SRM 51-35-01 REV 46. FABRICATED SKIN AS PER DWG ARB2363 AND INSTALLED AS PER SRM 51-33-01 AND MD-11 SRM51-35-01 REV 46.
- [SDR FDEA201105302025](https://openairdocs.org/sdr/FDEA201105302025.md): Skin · chafed · May 30, 2011 · N644FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING FIXED L/E LOWER SKIN FOUND WITH CHAFE MARKS WHERE PYLON-TO-WING CONTACTS. REFER TO SNRM N01217: LT WING FIXED L/E SKIN CHAFED. R & R SRM 51-33-01, REV 46 AND SRM 51-35-01, REV 46 AND DAC DWG ARB2363. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, RE
- [SDR FDEA201105302031](https://openairdocs.org/sdr/FDEA201105302031.md): Rib · cracked · May 30, 2011 · N644FE · Doug MD11F · Wing, Rib/Bulkhead
  > RIGHT HAND WING LEADING EDGE COMPARTMENT NR 16 SLAT TRACK INBOARD SUPPORT BRACKET FOUND CRACKED RIB REMOVED AS PER SRM 51-33-01 & 51- 35-01 REV 46. FABRICATED RIB AS PER DWG ARB2850 REV G & INSTALLED AS PER SRM 51-33-01 & 51-35-01 REV 46. REPAIR AREA
- [SDR FDEA201105292023](https://openairdocs.org/sdr/FDEA201105292023.md): Longeron · corroded · May 29, 2011 · N644FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTER CARGO COMPARTMENT BILGE AREA STA 1651, LONGERON 47R, FOUND CORROSION ACCOMPLISHED EA ED E.A. 1-5310-149713 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
- [SDR FDEA201105292022](https://openairdocs.org/sdr/FDEA201105292022.md): Longeron · corroded · May 29, 2011 · N644FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTER ACCESSORY COMPARTMENT - STA 6-70 TO STA 6-90, LONGERON NR 49R CORRODED CENTER ACCESSORY COMPARTMENT - CORRODED LONGERON NR 49R CUT-OUT AT STA 6-90 IAW SRM 53-00-05, REV 46, REPAIR 1. HFEC INSP CARRIED OUT IAW NDT SPM, REV 13, PART 6-10-01-001 FOUND
- [SDR FDEA201105282017](https://openairdocs.org/sdr/FDEA201105282017.md): Spar Cap · cracked · May 28, 2011 · N644FE · Doug MD11F · Vertical Stabilizer, Spar/Rib
  > CRACK INDICATION FOUND ON THE LOWER VERTICAL STABILIZER LEFT HAND UPPER FORWARD FLANGES OF THE REAR SPAR CAP. ACCOMPLISHED E.A.1-5530-149805, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
- [SDR FDEA201105241959](https://openairdocs.org/sdr/FDEA201105241959.md): Longeron · corroded · May 24, 2011 · N644FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER AFT CARGO STA 1853 TO STA 1863, LONGERON 48R FOUND CORRODED. CORROSION REMOVED IAW SRM 51-31-01, REV 46. FOUND EXCEEDED LIMITS IAW SRM 53-00-00, REV 46, FIG 205. NEW SPLICE CHANNEL FABRICATED IAW DWG AGA7438 AND INSTALLED IAW SRM 51-31-01, REV 46. RE
- [SDR FDEA201105161844](https://openairdocs.org/sdr/FDEA201105161844.md): Support Bracket · cracked · May 16, 2011 · N644FE · Doug MD11F · Leading Edge Devices
  > RIGHT WING FIXED L/E COMPARTMENT NR 16 SLAT TRACK INBD SUPPORT BRACKET FOUND CRACKED. RT WING L/E COMPT NR 16 SLAT TRACK INBD SUPPORT RIB REMOVED IAW SRM 51-33-01 & 51-35-01, REV 46. FABRICATED RIB IAW DWG ARB2850, REV G AND INSTALLED IAW SRM 51-33-01 & 51-3
- [SDR FDEA201105121821](https://openairdocs.org/sdr/FDEA201105121821.md): Seat Track · corroded · May 12, 2011 · N644FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 1561 TO 1661, X = 7.0 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE UPPER AND LOWER SURFACE FOUND CORRODED. TRIMMED OFF AS PER SRM 53-00-52 REV 46, FIGURE 201. NEW SET TRACK REPAIR SECTION AND SPLICE FABRICATED AS SRM PER 53-00-52 REV 46, FIGURE
- [SDR FDEA201105121822](https://openairdocs.org/sdr/FDEA201105121822.md): Seat Track · corroded · May 12, 2011 · N644FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 1561 TO 1661, X = -7.0 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE UPPER AND LOWER SURFACE FOUND CORRODED. ACCOMPLISHED "EA 1-5310-142539, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201105121820](https://openairdocs.org/sdr/FDEA201105121820.md): Seat Track · corroded · May 12, 2011 · N644FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 1581 TO 1601, X = 76.5 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE UPPER AND LOWER SURFACE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201, NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46
- [SDR FDEA201105121819](https://openairdocs.org/sdr/FDEA201105121819.md): Seat Track · corroded · May 12, 2011 · N644FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 1561 TO 1581, X = 76.5 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201 NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IA
- [SDR FDEA201105121817](https://openairdocs.org/sdr/FDEA201105121817.md): Floor Panel · worn · May 12, 2011 · N644FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 5-32 TO 5-53, X =-74 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND ELONGATED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW
- [SDR FDEA201105121816](https://openairdocs.org/sdr/FDEA201105121816.md): Seat Track · corroded · May 12, 2011 · N644FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 1541 TO 1561, X = 7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. SEAT TRACK TRIMMED- OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIGURE 201, AND INSTALLE
- [SDR FDEA201105121813](https://openairdocs.org/sdr/FDEA201105121813.md): Seat Track · corroded · May 12, 2011 · N644FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 5-113 TO 1541, X =7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. TRIMMED OFF IAW SRM 52-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-0
- [SDR FDEA201105121812](https://openairdocs.org/sdr/FDEA201105121812.md): Seat Track · corroded · May 12, 2011 · N644FE · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 5-113 TO 1541, X = 7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. TRIMMED OFF CORROSION IAW SRM 52-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IA
- [SDR FDEA201105121811](https://openairdocs.org/sdr/FDEA201105121811.md): Seat Track · corroded · May 12, 2011 · N644FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 5-93 TO 5-113, X =7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPAIR SECTION FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46.
- [SDR FDEA201105121809](https://openairdocs.org/sdr/FDEA201105121809.md): Seat Track · corroded · May 12, 2011 · N644FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 5-53 TO 5-73, X = 10 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. DAMAGED SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPAIR SECTION FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV
- [SDR FDEA201105121808](https://openairdocs.org/sdr/FDEA201105121808.md): Seat Track · corroded · May 12, 2011 · N644FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 5-113 TO 1541, X =10 SEAT TRACK FLOOR PANEL ATTACHMENT HOLE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SR
- [SDR FDEA201105041746](https://openairdocs.org/sdr/FDEA201105041746.md): Access Panel · worn · May 4, 2011 · N644FE · Doug MD11F · Wing, Center Box
  > NR 2 PYLON ACCESS PANEL 475GR FOUND ONE (1) EACH WORN MOUNTING HOLE. ACCOMPLISHED EA 1-5480-142549, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201105031708](https://openairdocs.org/sdr/FDEA201105031708.md): Bulkhead · cracked · May 3, 2011 · N644FE · Doug MD11F · Fuselage Main, Bulkhead
  > AFT FUSELAGE COMPARTMENT - STA 2033 BULKHEAD, LT SIDE FORGING FOUND CRACK LINE NEAR TO UPPER CEILING CUT-OUT. ACCOMPLISHED EA 1-5310-149742, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201105031707](https://openairdocs.org/sdr/FDEA201105031707.md): Stop Fitting · cracked · May 3, 2011 · N644FE · Doug MD11F · Trailing Edge Flaps
  > LT WING T/E OTBD FLAP UP-STOP FITTING FOUND CRACKED, R & R IAW SRM 51-33-01, REV 46. FLAP OPS CHECK C/OUT IAW AMM 27-50-30-5, REV 69.2 FOUND SATISFACTORY.
- [SDR FDEA201105031706](https://openairdocs.org/sdr/FDEA201105031706.md): Stop Fitting · cracked · May 3, 2011 · N644FE · Doug MD11F · Trailing Edge Flaps
  > RT WING T/E OTBD FLAP UP-STOP FITTING FOUND CRACKED. R & R IAW SRM 51-33-01, REV 46. FLAP OPS CHECK C/OUT IAW AMM 27-50-30-5, REV 69.2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201105031705](https://openairdocs.org/sdr/FDEA201105031705.md): Spar Cap · cracked · May 3, 2011 · N644FE · Doug MD11F · Vertical Stabilizer, Spar/Rib
  > CRACK INDICATION FOUND ON THE LWR VERTICAL STAB ON THE RT UPPER FWD FLANGE OF THE REAR SPAR CAP FITTING. ACCOMPLISHED EA 1-5530-149805, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201105021689](https://openairdocs.org/sdr/FDEA201105021689.md): Channel · damaged · May 2, 2011 · N644FE · Doug MD11F · Fuselage Miscellaneous Structure
  > LOWER CTR CARGO COMPARTMENT BOTH AFT STA 1711 AND STA 1831, X= 38 AND X= -38 SHUTTLE BEAM LT AND RT CHAIN PROTECTIVE HATS BROKEN LOWER CTR CARGO COMPARTMENT AT STA 1711-STA 1831, X=38 AND X= -38, BOTH AFT SHUTTLE BEAM LT AND RT CHAIN PROTECTIVE HATS REMOVED
- [SDR FDEA201105011686](https://openairdocs.org/sdr/FDEA201105011686.md): Skin · chafed · May 1, 2011 · N644FE · Doug MD11F · Wing, Plate/Skin
  > LT WING FIXED L/E OTBD EXTERIOR SURFACE ABOVE PYLON FOUND CHAFED SKIN. REMOVED AS PER SRM 51-33-01 REV 46 AND SRM 51-35-01 REV 46. FABRICATED AS PER DWG ARB2363 AND INSTALLED AS PER SRM 51-33-01 REV 46 AND SRM 51-35-01 REV 46. REPAIR AREA PAINTED AS PER SRM
- [SDR FDEA201105011685](https://openairdocs.org/sdr/FDEA201105011685.md): Skin · chafed · May 1, 2011 · N644FE · Doug MD11F · Wing, Plate/Skin
  > RT WING FIXED L/E OTBD EXTERIOR SURFACE ABOVE PYLON FOUND CHAFED SKIN. REMOVED IAW SRM 51-33-01 AND SRM 51-35-01, REV 46. NEW SKIN FABRICATED IAW DWG ARB236 AND INSTALLED IAW SRM 51-33-01 AND SRM 51-35-01, REV 46. REWORK AREA REPROTECTED & PAINTED IAW SRM
- [SDR FDEA201104261624](https://openairdocs.org/sdr/FDEA201104261624.md): Seat Track · corroded · Apr 26, 2011 · N644FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 457 AND 495, X = -29 SEAT TRACK UPPER AND LOWER FLANGE FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPAIR SECTION FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR C
- [SDR FDEA201104261623](https://openairdocs.org/sdr/FDEA201104261623.md): Stringer · cracked · Apr 26, 2011 · N644FE · Doug MD11F · Wing, Longeron/Stringer
  > LT WING UPPER AUX TANK AT STA XCW 46.500 STRINGER 9 FOUND CRACKED. ACCOMPLISHED EA 1-5710-149709. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201104261622](https://openairdocs.org/sdr/FDEA201104261622.md): Stringer · cracked · Apr 26, 2011 · N644FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > RT WING UPPER AUX TANK AT STA XCW 17 STRINGER 9 FOUND CRACKED. ACCOMPLISHED EA 1-5710-149709, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201104261621](https://openairdocs.org/sdr/FDEA201104261621.md): Stringer · cracked · Apr 26, 2011 · N644FE · Doug MD11F · Wing, Longeron/Stringer
  > RT WING UPPER AUX TANK AT STA XCW 46.500 STRINGER 9 FOUND CRACKED. ACCOMPLISHED EA 1-5710-149709. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201104261620](https://openairdocs.org/sdr/FDEA201104261620.md): Support Bracket · cracked · Apr 26, 2011 · N644FE · Doug MD11F · Leading Edge Devices
  > LT WING L/E COMPARTMENT NR 16 SLAT TRACK INBD SUPPORT BRACKET FOUND CRACKED. SUPPORT REMOVED IAW SRM 51-33-01 & 51-35-01, REV 46. FABRICATED IAW DWG ARB2850, REV G, AND INSTALLED IAW SRM 51-33-01, REV 46 AND SRM 51-35-01, REV 46. REPAIR AREA REPROTECTED IA
- [SDR FDEA201104211542](https://openairdocs.org/sdr/FDEA201104211542.md): Skin · cracked · Apr 21, 2011 · N644FE · Doug MD11F · Wing, Plate/Skin
  > LT WING L/E DROOP SLAT UPPER SKIN FOUND WITH APPROX 0.375 INCH AND 0.3125 INCH CRACK. STOP DRILLED IAW SRM 57-40-01, REV 46, REPAIR 5 FIG 201. REPAIR DOUBLER FABRICATED AND INSTALLED IAW SRM 57-40-01, REV 46, REPAIR 5, FIG 201 AND SRM 51-35-01, REV 46. REPA
- [SDR FDEA201104211541](https://openairdocs.org/sdr/FDEA201104211541.md): Skin · cracked · Apr 21, 2011 · N644FE · Doug MD11F · Wing, Plate/Skin
  > RT WING L/E DROOP SLAT UPPER SKIN FOUND WITH APPROX 1.75 INCH CRACKED. STOP DRILLED IAW SRM 57-40-01 REV 46, REPAIR 5, FIG 201. REPAIR DOUBLER FABRICATED IAW SRM 57-40-01, REV 46, REPAIR 5, FIG 201 AND INSTALLED IAW SRM 51-33-01, REV 46. REPAIR AREA REPROTE
- [SDR FDEA201104201525](https://openairdocs.org/sdr/FDEA201104201525.md): Seat Track · corroded · Apr 20, 2011 · N644FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 1661 TO STA 1669, X = 73 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. FABRICATED REPAIR SECTION AND SPLICE IAW SRM 53-00-52 REV 46, FIG 201 AND INSTALLED IAW SRM 51-31

Next page: https://openairdocs.org/deregistered/N644FE-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 = 'N644FE' AND deregistration_id = 'N644FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N644FE-2024-03-02/reports

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