N645FE, cancelled Mar 2, 2024

Service difficulty reports · 74

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201501310398Lens · brokenEVACUATION SLIDE REMOTE PRESS TO TEST INDICATING SYS INOPERATION COVER BROKEN. REPLACED PTT LENS AND LAMP REATAINER. OPS CHECK GOODJan 31, 2015 · N645FE · Doug MD11F · Emergency EquipmentSDR FDEA201307041478Transmitter · inoperativeSHORTLY 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 FUELJul 4, 2013 · N645FE · Doug MD11F · Engine Fuel Indicating SystemSDR FDEA201307021466Skin · separatedRIGHT 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.Jul 2, 2013 · N645FE · Doug MD11F · AileronsSDR FDEA201307011428Skin · delaminatedLEFT 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.Jul 1, 2013 · N645FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307011427Skin · delaminatedLEFT 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.Jul 1, 2013 · N645FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307011426Skin · delaminatedRIGHT 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.Jul 1, 2013 · N645FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307011425Skin · delaminatedRIGHT 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.Jul 1, 2013 · N645FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307011424Skin · delaminatedRIGHT 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.Jul 1, 2013 · N645FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201306241379Skin · crackedTEN 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 Jun 24, 2013 · N645FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201306241378Skin · crackedEIGHT 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. REPAIRJun 24, 2013 · N645FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201306211363Fitting · corrodedLEFT 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.Jun 21, 2013 · N645FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201306211362Hinge · corrodedRIGHT 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.Jun 21, 2013 · N645FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201306211361Hinge · corrodedRIGHT 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.Jun 21, 2013 · N645FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201306211360Hinge Bracket · corrodedLEFT 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.Jun 21, 2013 · N645FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201306211359Hinge Bracket · corrodedLT 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.Jun 21, 2013 · N645FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201306191343Frame · dentedFRAME 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.Jun 19, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181332Frame · dentedFRAME, 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.Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181328Frame · dentedFRAME 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.Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181326Frame · dentedRIGHT 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.Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181322Frame · chafedCABIN - 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.Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181331Frame · dentedFRAME 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.Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181329Frame · dentedFRAME 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.Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181324Frame · chafedLEFT 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.Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181319Skin · chafedLEFT 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.Jun 18, 2013 · N645FE · Doug MD11F · AileronsSDR FDEA201302210403Unknown · unknownREJECT 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.Feb 21, 2013 · N645FE · Doug MD11F · Trailing Edge Flap Control SystemSDR FDEA201301200151Landing Gear · malfunctionedON 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 LTJan 20, 2013 · N645FE · Doug MD11F · Landing Gear Retraction/Extension SystemSDR FDEA201107192789Skin · corrodedMAIN 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 PJul 19, 2011 · N645FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201107192788Skin · corrodedMAIN 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 1-5730-15Jul 19, 2011 · N645FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201107192787Skin · corrodedMAIN 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 CJul 19, 2011 · N645FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201107192786Skin · crackedRT 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.Jul 19, 2011 · N645FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201107192785Skin · crackedLT 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.Jul 19, 2011 · N645FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201107042559Skin · damagedCABIN - 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 SRM53-0Jul 4, 2011 · N645FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201107012522Seat Track · corrodedCABIN - 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.Jul 1, 2011 · N645FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107012521Shroud · crackedAFT 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.Jul 1, 2011 · N645FE · Doug MD11F · Aircraft Fuel Distribution SystemSDR FDEA201106202342Bulkhead · misrepairedREPAIR 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.Jun 20, 2011 · N645FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201106132216Intercostal · corrodedLONGERON 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, PAJun 13, 2011 · N645FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201106122209Structure · corrodedUPON 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.Jun 12, 2011 · N645FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201106102197Spar · crackedVERTICAL 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 OUJun 10, 2011 · N645FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA201106072141Longeron · corrodedFWD 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 53-0Jun 7, 2011 · N645FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201106072139Seat Track · corrodedLT 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.Jun 7, 2011 · N645FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106022094Hinge Fitting · corrodedRT 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-Jun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201106022093Hinge Fitting · corrodedRT 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 REMOVEJun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201106022092Hinge Fitting · corrodedRT 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.Jun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201106022091Hinge Fitting · corrodedLEFT 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.Jun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201106022090Hinge Fitting · corrodedLEFT 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.Jun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201106022089Hinge Fitting · corrodedLEFT 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 THICKNJun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201106022088Hinge Fitting · corrodedLEFT 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). Jun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201106022087Hinge Fitting · corrodedLEFT 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 6-2-1Jun 2, 2011 · N645FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201106022086Floor Support · corrodedRT FLOOR STRUCTURE BELOW DADO PANEL SUPPORT FROM STATION 1501 TO STATION 1521 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 101, REV 46.Jun 2, 2011 · N645FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201106022085Support · corrodedLEFT 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,Jun 2, 2011 · N645FE · Doug MD11F · Fuselage Miscellaneous Structure
Back to N645FE, cancelled Mar 2, 2024