N615FE

Service difficulty reports · 469

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 = 'N615FE' 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 FDEA201008112923Longeron · crackedCRACK INDICATION APPROX 0.5" IN LENGTH FOUND DURING X-RAY INSP AT STA 6-100, LONGERON -4R FWD SECTION EDGE. CRACKED LONGERON-4R AT FORWARD SECTION EDGE STATION 6-100, REPAIRED AS PER SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 44 AND E.A. 1-5310-140453. THIS RAug 11, 2010 · N615FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201008112922Longeron · crackedCRACK INDICATION APPROX 4" IN LENGTH DURING X-RAY INSP AT STA 6-100, LONGERON -3R FWD SEC EDGE. CRACKED LONGERON-3R AT FORWARD SECTION EDGE STATION 6-100, REPAIRED AS PER SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 44 AND EA 1-5310-140453. REPAIR IS CLASSAug 11, 2010 · N615FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201008112921Skin · crackedCRACK INDICATION APPROX 1" IN LENGTH FOUND DURING X-RAY AT STA 6-100, LONGERON -2R FWD SECTION EDGE. REPAIRED AS PER SRM 53- 00-05 FIGURE 202 REPAIR 1 REVISION 44 AND E.A. 1-5310-140453. REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 110.Aug 11, 2010 · N615FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201008112920Skin · crackedCRACK INDICATION APPROX 1" LENGTH FOUND DURING X-RAY INSP AT STA 6-100, LONGERON -2L FWD SECTOR. REPAIRED AS PER SRM 53-00- 05 FIGURE 202 REPAIR 1 REVISION 44 AND E.A. 1-5310-140453. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 110.Aug 11, 2010 · N615FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201008102913Access Panel · crackedLT WING L/E LOWER ACCESS PANEL 519CB CUTOUT FWD INBD CORNER SUSPECTED CRACK. TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-40-02 FIG. 201 REPAIR 7 REVISION 44. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 110Aug 10, 2010 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201008092890Longeron · crackedCENTER ACCESSORIES COMPT. LT SIDE LONGERON 37L SUSPECT CRACK AT 2 PLACES. FASTENER TO FASTENER APROX 4" IN AFT OF FUSLAGE STA Y=1129/6-100. CRACK LONGERON 37L IN CTR ACCESORY COMPARTMENT IN AFT OF FUSELAGE STA Y=1129/6-100 REMOVED AND REPLACED WITH A FABRICAAug 9, 2010 · N615FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201008092894Floorbeam · crackedMAIN DECK CARGO AT STA 1887 X=-57, BELOW FLOOR SUPPORT BEAM END FOUND CRACKED AS MARKED. R & R IAW SRM 51-31-01, REV 44. NEW FLOOR SUPPORT FABRICATED BY MACHINING IAW DWG AGA7551, REV G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.Aug 9, 2010 · N615FE · Doug MD11F · Fuselage Main, Floor BeamSDR FDEA201008092893Seat Track · corrodedMAIN DECK CARGO SEAT TRACK, STA 1561 X=-8, CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1531 TO STA 1571 X=-8 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REV 43. REPAIR CLASSIFIED AS MAJOR AS GMM 6-2-100 REV 110.Aug 9, 2010 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201008092892Frame · damagedMAIN DECK CARGO RT STA 5-53 L-12 FRAME FOUND DAMAGED. REPAIRED IAW SRM 53-00-07, FIG 201 REPAIR 4, REV 44. REPETITIVE INSP REQUIRED INITIAL AT 12,000 CYCLES AND REPETITIVE AT 8,000 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07, FIG 201, REPAIR 4 REV 44. REPAIR CAug 9, 2010 · N615FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201008092891Frame · dentedMAIN DECK CARGO RT STA 5-33 L-12 FRAME FOUND DENTED. REPAIR CARRIED OUT IAW SRM 53-00-07, REPAIR 2 FIG 201, REV 44. INITIAL INSP TO BE CARRIED OUT ON 14,500 FLT CYCLE AND REPETITIVE INSP ON 9,500 FLT CYCLE IAW SRM 53-00-07, REPAIR 2, TABLE 201, REV 44. REPAIAug 9, 2010 · N615FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201008052817Frame · dentedMAIN DECK CARGO RT STA 1601, L-12 FRAME FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-00-07 REPAIR 2 FIG 201 REV 43. INITIAL INSPECTION TO BE CARRIED OUT ON 14,500 FLT CYCLE AND REPETITIVE INSPECTION ON 9,500 FLT CYCLE AS PER SRM 53-00-07 REPAIR 2 TABLE 201 Aug 5, 2010 · N615FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201008052816Frame · dentedMAIN DECK CARGO RT STA 1761 L-12 FRAME FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-00-07 REPAIR 2 FIG 201 REV 44. INITIAL INSPECTION TO BE CARRIED OUT ON 14,500 FLT CYCLE AND REPETITIVE INSPECTION ON 9,500 FLT CYCLE AS PER SRM 53-00-07 REPAIR 2 TABLE 201 RAug 5, 2010 · N615FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201008052815Frame · dentedMAIN DECK CARGO LT STA 1761 L-12 FRAME FOUND DENT. MAIN DECK CARGO STA 1761 L-12 FRAME FOUND DENT. REPAIR CARRIED OUT AS PER SRM 53-00-07 REPAIR 2 FIG 201 REV 43. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 110. INITIAL INSPECTION TO BE CARRIED OUT ON 14Aug 5, 2010 · N615FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201004191252Power Unit · failedON TAKEOFF ROLL AT 75 KTS GEN 1 & GEN 3 FLASHED OFF. REJECTED TAKEOFF. GENS BOTH RESET AUTOMATICALLY. TRIED SECOND T/O. AT 52 KTS GEN 1,2,3 ALL OFF. REJECTED TAKEOFF. ALL 3 GENS CAME BACK ONLINE THEIR OWN. WX 040/4 KTS,15 DEG C. LIGHT RAIN. ACFT WAS LOADApr 19, 2010 · N615FE · Doug MD11F · Alternator-Generator DriveSDR FDEA200907312854Hydraulic System · lowRECEIVED "HYD 3 OFF" ALERT AT CRUISE, WITHIN 35 MINS HYD SYS 3 QTY WENT FROM 4.0 TO 2.6 GALLONS. DURING LANDING, GEAR EXTENSION RECEIVED " HYD 3 FAIL" ALERT. REMOVED AND REPLACED, HORIZ STAB PRIMARY CONTROL VALVE "PRESSURE FITTING UNION ASSY" OPS CHECK NORMJul 31, 2009 · N615FE · Doug MD11F · Hydraulic System, MainSDR FDEA200904231389Fire Warning · false activationON TAXI INTO CAN TX RAMP, HAD CARGO FIRE LWR FWD LEVEL 3 ALERT. COMPLIED QRH CALLED FIRE DEPT, ASKED FOR FX MECHANIC TO INSPECT EXTERIOR AIRCRAFT, NO FIRE ACTUALLY OBSERVED. REMOVED AND REPLACED LOWER CARGO NR 1 FIRE BOTTLE AS PER AMM 26-22-01-4, AND ALSO RApr 23, 2009 · N615FE · Doug MD11F · Fire DetectionSDR FDEA200901010001Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATION. RT WING INBOARD FLAP VANE REMOVED AND REPLACED AS PER AMM 27-50-22-4. FLAP VANE ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-5 FOUND SATISFACTORY.Jan 1, 2009 · N615FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200812285312Fuel Tank · corrodedMAIN DECK CARGO, CENTER AUXILIARY TANK UPPER SURFACE FOUND CORROSION AT STA 1229 X = 6. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. FOUND TO EXCEED LIMIT AS PER SRM 57-20-00 FIGURE 13 VOLUME I. REPAIR CARRIED OUT AS PER EA 1-5710-122666. REPAIR CLASSIFDec 28, 2008 · N615FE · Doug MD11F · Fuel StorageSDR FDEA200812275311Frame · dentedMAIN DECK CARGO RT FRAME STATION 1741 AT LONGERON 11 FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. DAMAGE TOLERANCE INSPECTION REQUIRED AT INITIAL FLIGHT CYCLE 14,500 AS PER SRM 53-30-0Dec 27, 2008 · N615FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200812275310Frame · dentedMAIN DECK CARGO - LT FRAME STATION 1741 AT LONGERON 11 FOUND DENT. REPAIR CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. DAMAGE TOLERANCE INSPECTION REQUIRED AT INITIAL FLIGHT CYCLE 14,500 AS PER SRM 53-30-00Dec 27, 2008 · N615FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200812265293Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES A, B, C AND D. AT MAIN CARGO DOOR LOWER JAMB, CRACKED NR 2 SUPPORT FITTING REMOVED AND REPLDec 26, 2008 · N615FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA200812265309Skin · corrodedEMPENNAGE, RIGHT AFT FUSELAGE SKIN COMMON TO AFT BODY FAIRING NR 347DF LOWER MATING SURFACE FOUND WITH SURFACE CORROSION. SURFACE CORROSION ON EMPENNAGE RT AFT FUSELAGE SKIN COMMON TO AFT BODY FAIRING 347DF LOWER MATING SURFACE REMOVED AS PER SRM 51-21-01 VDec 26, 2008 · N615FE · Doug MD11F · Horizontal Stabilizer, Plate/SkinSDR FDEA200812265308Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE LOWER ATTACH INBOARD HOLE FORWARD AND AFT SURFACE FOUND WITH CORROSION. REWORKED AS PER EA 1-5750-127701. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Dec 26, 2008 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200812265307Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE LOWER ATTACH INBOARD HOLE FOUND WITH CORROSION. REWORKED AS PER EA 1-5750-127701. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Dec 26, 2008 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200812265306Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR ATTACH OUTBOARD HOLE FOUND WITH CORROSION. REPAIRED AS PER EA 1-5750-122667. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Dec 26, 2008 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200812265305Hinge · corrodedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR ATTACH INBOARD HOLE FOUND WITH CORROSION. REPAIRED AS PER EA 1-5750-122667. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Dec 26, 2008 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200812265298Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 7 SUPPORT FITTING AT HOLES NR B, NR C AND NR D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMDec 26, 2008 · N615FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200812265297Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 6 SUPPORT FITTING AT HOLES A, B AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJODec 26, 2008 · N615FE · Doug MD11 · Fuselage Main, StructureSDR FDEA200812265296Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLE D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJORDec 26, 2008 · N615FE · Doug MD11 · Fuselage Main, StructureSDR FDEA200812265295Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB, NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED ADec 26, 2008 · N615FE · Doug MD11 · Fuselage Main, StructureSDR FDEA200812265294Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 3 SUPPORT FITTING AT HOLE NR A. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMDec 26, 2008 · N615FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA200812265292Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 1 SUPPORT FITTING AT HOLES NR A, NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIEDec 26, 2008 · N615FE · Doug MD11 · Fuselage Miscellaneous StructureSDR FDEA200812235267Skin · damagedCENTER CARGO DOOR LOWER FORWARD CORNER FOUND DOOR SKIN DAMAGED. CENTER CARGO DOOR LOWER FORWARD CORNER, DOOR SKIN DAMAGED AREA REPAIR CARRIED OUT AS PER EA 1-5230-127702. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Dec 23, 2008 · N615FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA200812235262Skin · damagedCENTER CARGO DOOR LOWER FORWARD CORNER FOUND DOOR SKIN DAMAGED. REPAIR CARRIED OUT AS PER E.A. NO. 1-5230-127702 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Dec 23, 2008 · N615FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA200812235261Structure · crackedCENTER LANDING GEAR WHEEL WELL, FOUND RIGHT FORWARD MOST CORNER CUTOUT DOUBLER CRACKED. CENTER MLG WW, RIGHT FORWARD MOST CORNER CUTOUT CRACKED. DOUBLER REMOVED AS PER SRM 51-33-01 VOLUME II. FASTENER HOLES PICKED UP ON NEW DOUBLER AND INSTALLED AS PER SRMDec 23, 2008 · N615FE · Doug MD11F · Fuselage Main, StructureSDR FDEA200812225259Skin · crackedRIGHT WING FIXED LEADING EDGE ACCESS PANEL NR 619CB CUTOUT FOUND CRACKED. RIGHT WING FIXED LEADING EDGE ACCESS PANEL 619CB CUTOUT CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Dec 22, 2008 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200812225258Skin · crackedRIGHT WING FIXED LEADING EDGE SLAT TRACK 12 SKIN FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Dec 22, 2008 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200812225257Rib · crackedRT WING FIXED LEADING EDGE SLAT TRACK 16 INBD RIB FOUND CRACKED. RIB REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-35-01 VOLUME II AND SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Dec 22, 2008 · N615FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA200812225256Stiffener · crackedEMPENNAGE: AFT FUSELAGE COMPARTMENT PRESSURE BULKHEAD STA 2007 QUANTITY 01 STIFFENER X = -15.25 FOUND CRACKED APPROX 0.35 INCH AT UPPER CORNER AREA. AFT FUSELAGE COMPARTMENT PRESSURE BULKHEAD STATION 2007 X = -11.25 STIFFENER CARRIED OUT REPAIR AS PER EA 1-Dec 22, 2008 · N615FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 07FDEA02448Floorbeam · dentedCENTER CARGO COMPT: DOORWAY CEILING AREA MAIN DECK CARGO FLOORBEAM LOWER FLANGE AT STA 1761, X = -100 FOUND DENTED. [07-25-07] REPAIRED AS PER EA 1-5310-112358.Jul 13, 2007 · N615FE · Doug MD11F · Fuselage Main, Floor BeamSDR 07FDEA02438Stringer · crackedLT WING FUEL TANK AT STRINGER 15 FOUND CRACKED. [07-24-07] SLOTTED OUT AND REPAIRED AS PER SRM 57-20-00, FIG 11, VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jul 12, 2007 · N615FE · Doug MD11F · Wing, Longeron/StringerSDR 07FDEA02398Floorbeam · crackedCTR CARGO COMPT, FLOORBEAM STA 1781 FWD FLANGE AT X = -50 CRACKED. [07-24-07] REPAIRED AS PER FEDEX EA 1-5310-112354. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jul 9, 2007 · N615FE · Doug MD11F · Fuselage Main, Floor BeamSDR 07FDEA02389Trunnion · crackedNOSE LANDING GEAR LT TRUNNION FOUND CRACKED. [07-24-07] REPAIR CARRIED OUT AS PER SRM 53-40-00 VOL.I. FIG. 23. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Jul 7, 2007 · N615FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR 06FDEA04309Engine · making metalENG 1 OIL FILTER ALERT CAME ON DURING CRUISE, ACCOMPLISHED QRH CHECKLIST, SHUTDOWN ENG 1. DUMPED 20K AND LANDING IN TPE. ENG 1 OIL FILTER ALERT CAME ON DURING CRUISE. ACCOMPLISHED CHECKLIST SHUTDOWN ENG 1. DUMPED 20K OF FUEL AND LANDING IN TPE. DUE TO THEDec 23, 2006 · N615FE · Doug MD11F · Engine (Turbine/Turboprop)SDR 06FDEA1927Pressure Switch · malfunctionedRECEIVED "ENG 1 OIL FILTER". PROCEEDED VIA QRH PROCEDURES, SHUT DOWN ENGINE AND DESCENDED TO 300 (FROM 360). ALL ENGINE PARAMETERS NORMAL OTHER THAN THE ALERT. DECLARED EMERGENCY AND LANDED AT PANC. INSPECTED MASTER CHIP DETECTOR AND SCAVANGE FILTER ELEMEMay 15, 2006 · N615FE · Doug MD11F · Engine Oil PressureSDR 06FDEA1386Wire Harness · faultyENG 2 A/I OFF ALERT AT FL 050 WITH A/I ON IN MODERATE ICING. DEPARTED ILE RETURNED CDG. R&R HARNESS ON ENG 2 PER AMM 71-50-04-4 AND INSTALLED ANTI ICE VALVE NEW ONE PER AMM 30-22-01-4 AND INSTALLED ALL PLUGS. REMOVED BEFORE PER ESMP AND RECONNECTED SENSE LIApr 9, 2006 · N615FE · Doug MD11 · Ice/Rain Protection System WiringSDR 06FDEA1275Shutoff Valve · malfunctionedON CLIMB-OUT AT APPROX 8,000 FT RECEIVED ENGINE 2 A/ICE DUCT ALERT. COMPLIED W/CHECKLIST LIGHT WENT OUT AT IDLE. RTB FOR UNEVENTFUL LANDING. PERFORMED FIM 30-22-05, NO LEAK DETECTED ON ENG NR 2 ANTI-ICE DUCT. ENG NR 2 COWL ANTI-ICE SHUTOFF VLV, FOUND DEFEMar 31, 2006 · N615FE · Doug MD11 · Airfoil Anti/De-ice SystemSDR 06FDEA0856Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE RIB DOUBLER FOUND CRACKED AT XORS=683. RIGHT HAND WING FIXED LEADING EDGE RIB DOUBLER AT XORS=683 REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER AS PER SRM 51-33-01 VOLUME II. NEW DOUBLER FABRICATED AS PER DRAWING ARB3954Feb 27, 2006 · N615FE · Doug MD11 · Wing Main, Frame StructureSDR 06FDEA0855Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE RIB DOUBLER FOUND CRACKED AT XORS=562. RIGHT HAND WING FIXED LEADING EDGE RIB DOUBLER AT XORS=562 REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER AS PER SRM 51-33-01 VOLUME II. NEW DOUBLER FABRICATED AS PER DRAWING ARB3954Feb 27, 2006 · N615FE · Doug MD11 · Wing Main, Frame StructureSDR 06FDEA0854Doubler · crackedLEFT HAND WING FIXED LEADING EDGE INTERNAL RIB DOUBLER FOUND CRACKED AT XORS=562. LEFT HAND WING FIXED LEADING EDGE INTERNAL RIB DOUBLER AT XORS=562 REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER AS PER SRM 51-33-01 VOLUME II. NEW DOUBLER FABRICATED AS PERFeb 27, 2006 · N615FE · Doug MD11 · Wing Main, Frame Structure
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