N606FE

Service difficulty reports · 403

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 = 'N606FE' AND registry_match = 'registration'
  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 FDEA201204241549Seat Track · corrodedMAIN DECK CARGO SEAT TRACK AT BS 1545, X= 8.5 LT FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REV 49. SEAT TRACK REWORKED IAW DWG AFA7795, REVISION F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Apr 24, 2012 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201204241548Bulkhead · crackedCENTER LANDING GEAR WHEEL WELL FWD BULKHEAD FOUND CRACK ON RT TEE FITTING UPPER AREA. R & R IAW SRM 51-31-01, REV 49. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100, REV 114.Apr 24, 2012 · N606FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201201230315Indicator · inoperativeL1 DOOR SLIDE TEST LAMP RETAINER FOUND INOPERATIVE, DURING SERVICE CHECK. SWAPED WITH R1, SLIDE LIGHT WORKS NORMALLY. R & R L1 REMOTE PRESSURE INDICATOR ASSY IAW AMM 25-61-04-4. OPS CHECKED GOOD.Jan 23, 2012 · N606FE · Doug MD11F · Escape SlideSDR FDEA201201100075Skin · crackedLEFT INBD FLAP UPPER SKIN CRACKED. REPAIRED IAW EA 1-5750-157587, PART 1.Jan 10, 2012 · N606FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201112125245Bezel · missingEMERGENCY LIGHT ON RT SIDE OF ACFT IN ENTRY AREA ABOVE LAV IS MISSING BEZEL ASSY. INSTALLED EMERGENCY LIGHT BEZEL IAW SMP. PERFORMED EMERGENCY LIGHT TEST IAW 33-50-00-5. OP'S CHECKED GOOD.Dec 12, 2011 · N606FE · Doug MD11F · Emergency LightingSDR FDEA201109063711Switch · faultedEVACUATION SLIDE REMOTE PTT SWITCH REMAINS ILLUMINATED. FOUND PRESSURE SWITCH ON SLIDE BOTTLE AT FAULT. REMOVED AND REPLACED THE DOOR SLIDE ASSEMBLYSep 6, 2011 · N606FE · Doug MD11F · Escape SlideSDR FDEA201108283531Indicator · false indication1R DOOR SLIDE LIGHT ILLUMINATED DURING CRUISE. ON FOR REMAINDER FLIGHT. CHECKED BOTTLE PRESSURE FOUND GREEN BAND AND CONTINUITY CHECK OF THE PRESURE SWITCH FOUND OK. THEN R & R 1R PRESSURE REMOTE INDICATOR ASSY IAW MM 25-61-04-4. INDICATION TEST FOUND OK Aug 28, 2011 · N606FE · Doug MD11F · Escape SlideSDR FDEA201108093148Indicator · inoperativeR1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATOR INOPERATIVE. R & R 2 BATTERIES IAW MM:25-61-04-4-0. OPS CHECK OK. ACFT OK TO CONTINUE.Aug 9, 2011 · N606FE · Doug MD11F · Escape SlideSDR FDEA201009203566Idg · crackedON TAXI OUT MEM LEVEL NR 2 "GEN DRIVE 2 FAULT " WARNING DISCONNECT IDG NR 2 CDG U IN WORK. REMOVED AND REPLACED ENGINE NR 2 IDG.Sep 20, 2010 · N606FE · Doug MD11F · AC Generator-AlternatorSDR FDEA201005291726Skin · deformedSKIN DEFORMATION AT FR STA 5-70, BETWEEN LONG 49R - 50R. SKIN DEFORMED AT FR STA 5-70 BETWEEN LONG 49R -50R TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-00-01 FIG 201 REV 43. HFEC INSP CARRIED OUT IAW DAC NDT SPM REV 13, 06-10-01.001 ON TRIMMED OUT AREMay 29, 2010 · N606FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201005291725Skin · bulgedSKIN BULGE ALONG FR STA 5-70 BETWEEN LONG 51R - 52R APPROX 4" LENGTH. BULGE SKIN AT FR STA 5-70 BETWEEN LONG 51R - 52R APROX 4" LENGTH TRIMMED OUT AND CARRIED REPAIR IAW SRM 53-00-01, FIG 201, REV 43. HFEC INSP CARRIED OUT IAW NDT SPM REV 13, 06-10-01.001May 29, 2010 · N606FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201005291719Seat Track · corrodedMAIN DECK CARGO SEAT TRACK CROWN STA 755 X=-47 FOUND W/ SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 725 TO STA 765 X=-47 IAW SRM 53-00-52, FIG 201. REPAIR REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.May 29, 2010 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201005291717Seat Track · corrodedMAIN DECK CARGO SEAT TRACK INBD FLANGE STA 1501-1521 X=-8 FOUND W/ SURFACE CORROSION. MAIN DECK CARGO CORRODED SEAT TRACK AT STA 1501 TO STA 1521 X=-8, REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1491 TO STA 1531 X=-8 IAW SRM 53-00-52, FIG 201. REPAMay 29, 2010 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201005291715Seat Track · corrodedMAIN DECK CARGO SEAT TRACK INBD FLANGE AT STA 1481 X= 107 FOUND W/ SURFACE CORROSION. MAIN DECK CARGO CORRODED SEAT TRACK INBD FLANGE AT STA 1481 X= 107, REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1471 TO STA 1531/5-0 X= 107 IAW SRM 53-00-52, FIG May 29, 2010 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201005291714Seat Track · corrodedMAIN DECK CARGO SEAT TRACK INBD FLANGE FROM STA 1501 TO 5-0 X= 107 FOUND W/ SURFACE CORROSION. MAIN DECK CARGO CORRODED SEAT TRACK INBD FLANGE FROM STA 1501 TO 5-0 X= 107. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1471 TO 1531 / 5-0 X= 107 IAW SMay 29, 2010 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201005291711Skin Panel · crackedHFEC OPEN HOLE INSP. CARRIED OUT AND FOUND 02EA HOLES W/ CRACK INDICATION RT WING LWR SKIN PANEL OUTER WING ACCESS CUTOUT BTW XORS=683.4 AND XORS=713.6 AS MARKED. QTY 02 EA CRACK FASTENER HOLES ON RT WING LWR SKIN PNL FUEL TANK ACCESS DOOR CUTOUT 636AB BTW STMay 29, 2010 · N606FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201005281705Skin Panel · crackedHPEC OPEN HOLE INSP. CARRIED OUT AND FOUND 01 HOLE WITH CRACK INDICATION ON LT WING LWR SKIN PANELS, OUTER WING ACCESS DOOR BTW XORS=683.4 AND XORS=713.6 AS MARKED. QTY 01 EA CRACK FASTENER HOLE ON LT WING LOWER PNL FUEL TANK ACCESS DOOR CUTOUT 536AB BTW STA May 28, 2010 · N606FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201005271682Support Fitting · crackedLT WING - NR 1 L/E SLAT INBD EDGE FWD LOWER FASTENER SUPPORT FITTING FOUND CRACKED AFTER REMOVAL. LW NR1 L/E SLAT INBD EDGE FWD FASTENER SUPPORT FITTING R & R IAW SRM 51-33-01, REV 43. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.May 27, 2010 · N606FE · Doug MD11F · Leading Edge DevicesSDR FDEA201005271681Rib · crackedLT WING - NR 1 L/E SLAT INBD EDGE RIB FOUND CRACKED. LT WING NR1 L/E SLAT INBD EDGE RIB FABRICATED IAW DWG ARB 7128 REV L. RIB R & R IAW SRM 51-53-01, REV 43, LT NR1 SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-20-5, REV 66. FOUND SATISFACTORY. REPAIMay 27, 2010 · N606FE · Doug MD11F · Leading Edge DevicesSDR FDEA201005271680Wedge · delaminatedRT WING - OTBD FLAP T/E WEDGE INBD EDGE FOUND DELAMINATION. COMPLIED WITH EA 1-5750-140479.May 27, 2010 · N606FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201005261657Skin · crackedRT WING - NR 6 L/E SLAT INBD TRACK CUT-OUT OTBD CORNER FOUND CRACKED. RT WING L/E SLAT NR6 INBD TRACK CUTOUT OTBD CRACK CORNER TRIMMED OFF AND REPAIR CARRIED OUT IAW ARM 57-40-02, FIG 201, REPAIR 7, REV 43. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.May 26, 2010 · N606FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201005261655Skin · crackedLT WING - L/E LOWER ACCESS PANEL 519CB CUT-OUT FWN INBD CORNER FOUND CRACK. LT WING L/E LOWER ACCESS PNL 519CB CUTOUT FWD INBD CRACK CORNER TRIMMED OFF AND REPAIR CARRIED OUT IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 43. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-May 26, 2010 · N606FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201005261656Skin · dentedRT WING - NR 4 SLAT L/E SURFACE FOUND DENT. RT WING NR 4 SLAT L/E SURFACE DENT EVALUATED AND FOUND WITHIN LIMIT IAW SRM 57-40-02, FIG 201. REPAIR G REV. 43. DEPTH OF DENT 0.032" DIA. OF DENT 1" AFFIXED A CLEAR DOT ADJACENT TO THE DENT AREA IAW GMM 6-3-101, REVMay 26, 2010 · N606FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201005251628Vane · delaminatedRT WING - INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. RT WING INBD FLAP VANE R & R IAW AMM 27-50-22-4, REV 66. FLAP VANE ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5, REV 66 FOUND SATISFACTORY.May 25, 2010 · N606FE · Doug MD11 · Trailing Edge FlapsSDR FDEA201001030004Valve · failedREV 3 PRESS FAULT ON T/O REJECTED T/O AT 60KT. PERFORMED HI-POWER RUN IAW JRH, REV 3 PRESS FAULT APPEARED BEFORE 80 PERCENT. SUSPECT NR 3 PRESS REG SHUTOFF VALVE AT FAULT. SWAPPED NR1 AND NR3 PRESS REG SHUTOFF VALVE FOR T/S PURPOSE AND PERFORMED HI-POWER RUJan 3, 2010 · N606FE · Doug MD11F · Engine Thrust ReverserSDR FDEA200904141288Tire · failedJUST PRIOR TO ROTATION NR 1 TIRE FAILURE. REMOVED AND REPLACED NR 1 AND 2 MAIN WHEEL ASSY AS PER MM 32-41-01-4. VISUAL INSP NR 1 BRAKE ASSY CONDITION GOOD AS PER 32-43-00. ANTI-SKID SYSTEM RTS AS PER MM 32-45-00-5, SPIN CHECK ON EACH BRAKE SYSTEM ALL RELEAApr 14, 2009 · N606FE · Doug MD11F · TireSDR 08FDEA04101Spar Cap · crackedHFEC INSPECTION CARRIED OUT AND FOUND ONE CRACK ON LEFT SIDE RADIUS OF LOWER FORWARD SPAR CAP AT LOWER VERTICAL STABILIZER. REPAIR CARRIED OUT AS PER SRM 55-20-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 29, 2008 · N606FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR 08FDEA04042Longeron · crackedCRACK INDICATION FOUND ON STA 6-100 AFT SIDE LONGERON 1R OUTBOARD FLANGE APPROXIMATELY 2 INCHES LONG IMAGE ON X-RAY FILM. REPAIRED AS PER SRM 53-10-00. LONGERON REWORKED AS PER DRAWING AEA7476. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 25, 2008 · N606FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 08FDEA03974Spar Cap · crackedHFEC INSPECTION CARRIED OUT AND FOUND ONE CRACK INDICATION ON RIGHT SIDE RADIUS OF LOWER SPAR CAP AT LOWER VERTICAL STABILIZER. REPAIRED AS PER SRM 55-20-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 22, 2008 · N606FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR 08FDEA03973Spar Cap · crackedHFEC INSPECTION CARRIED OUT AND FOUND ONE CRACK INDICATION ON ONE FASTENER TO EDGE OF LEFT LOWER FORWARD SPAR CAP FORWARD FLANGE AT LOWER VERTICAL STABILIZER. REPAIR CARRIED OUT AS PER SRM 55-20-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 22, 2008 · N606FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR 08FDEA03972Seat Track · corrodedMAIN DECK FLOOR RBL 8.5 SEAT TRACK FLANGE AT APPROXIMATELY STA 5-75 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 22, 2008 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03971Seat Track · corrodedMAIN DECK FLOOR RBL 8.5 SEAT TRACK FLANGE FOUND CORRODED AT APPROXIMATELY STA 5-87. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 22, 2008 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03970Seat Track · corrodedMAIN DECK FLOOR RBL 8.5 SEAT TRACK FLANGE FOUND CORRODED BETWEEN STA 5-11 AND STA 5-53. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 22, 2008 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03969Longeron · crackedDURING HFEC INSPECTION CARRIED OUT AT RIGHT SIDE NOSE LANDING GEAR TRUNNION FITTING TRIM-OUT FOUND LONGERON CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01. LONGERON FABRICATED AS PER EA 1-5310-123112, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 22, 2008 · N606FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 08FDEA03968Longeron · crackedDURING HFEC INSPECTION CARRIED OUT AT LEFT SIDE NOSE LANDING GEAR TRUNNION FITTING TRIM-OUT, FOUND LONGERON CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01. FABRICATED LONGERON AS PER EA 1-5310-123111, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 22, 2008 · N606FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 08FDEA03967Seat Track · corrodedMAIN DECK SEAT TRACK BETWEEN STA 1119 TO 6-10 LBL 8.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 22, 2008 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03966Vane · delaminatedRIGHT WING, INBOARD FLAP VANE LOWER OUTBOARD HALF FOUND DELAMINATION, APPROXIMATELY 7 INCH BY 37 INCH. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 FOUND 'SATISFACTORY'. REPAIR CLASSIFIED AS MINOR PER GMSep 22, 2008 · N606FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA03949Skin · crackedDURING HFEC INSPECTION, FOUND 14 FASTENER HOLES WITH CRACK INDICATIONS AT RIGHT WING LOWER SKIN PANELS OUTER WING ACCESS DOOR CUTOUT BETWEEN XORS 683.400 AND 713.600. REPAIRED AS PER EA 1-5710-122560, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 19, 2008 · N606FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA03948Skin · crackedDURING HFEC INSPECTION, FOUND 11 FASTENER HOLES WITH CRACK INDICATIONS AT LEFT WING LOWER SKIN PANELS OUTER WING ACCESS DOOR CUTOUT BETWEEN XORS 683.400 AND XORS 713.600. REPAIRED AS PER EA 1-5710-122559, THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 19, 2008 · N606FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA03947Seat Track · corrodedMAIN DECK SEAT TRACK BETWEEN STA 5-73 TO 5-93 RBL 8.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENTAS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 19, 2008 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03946Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES A, C AND D. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 19, 2008 · N606FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03945Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FOUND WITH CRACK INDICATIONS AT HOLES A AND D. CARRIED OUT REPAIR AS PER SRM 53-50-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 19, 2008 · N606FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03944Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLES A, B AND D. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMMSep 19, 2008 · N606FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03943Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLES A, B AND C. MAIN DECK CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00Sep 19, 2008 · N606FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03932Seat Track · corrodedMAIN DECK, SEAT TRACK BETWEEN STA 1521 - 5-73 LBL, 65 FOUND CORRODED. MAIN DECK CORRODED SEAT TRACK BETWEEN STA 5-0 TO 5-73 LBL 65 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100Sep 17, 2008 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03931Support Fitting · crackedDURING OPEN HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. MAIN DECK CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING REMOVED AND REPLACED AS PER SSep 17, 2008 · N606FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03930Support Fitting · crackedDURING OPEN HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. MAIN DECK CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING REMOVED AND REPLACED AS PER SRMSep 17, 2008 · N606FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03929Support Fitting · crackedDURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. MAIN DECK DOOR LOWER JAMB NR 4 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-33-0Sep 17, 2008 · N606FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03909Trunnion · crackedNOSE LANDING GEAR RIGHT TRUNNION FITTING FOUND CRACKED. NOSE LANDING GEAR RT TRUNNION FITTING REPAIRED AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1,500 LANDINSep 16, 2008 · N606FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR 08FDEA03908Trunnion · crackedNOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. NOSE LANDING GEAR LT TRUNNION FITTING REPAIRED AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1,500 LANDING INTESep 16, 2008 · N606FE · Doug MD11F · Fuselage, Landing Gear Attach Fittings
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