N617FE

Service difficulty reports · 467

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 = 'N617FE' 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 FDEA200907132599Fitting · crackedDURING OPEN HOLE INSP ON RT SIDE BANJO FITTING FASTENER HOLE COMMON TO REPAIR DOUBLER, CRACKED FOUND ON AFT FLANGE LOWEST FASTENER HOLE BANJO FITTING LAYER AT 3 AND 6 O'CLOCK POSITION. REPAIR CARRIED OUT IAW EA 1-5530-132118. REPAIR CATEGORY B, ACCOMPLISH INJul 13, 2009 · N617FE · Doug MD11F · Vertical Stabilizer, Attach FittingsSDR FDEA200907132598Fitting · crackedDURING OPEN HOLE INSP CRACKED FOUND ON LT SIDE BANJO FITTING SECOND FASTENER HOLE COMMON TO BANJO FITTING AND CARRY THROUGH STRUCTURE AFT ROW ON BANJO FITTING LAYER. REPAIR CARRIED OUT IAW EA 1-5530-132118. REPAIR CATEGORY B, ACCOMPLISH INITIAL INSP WITHINJul 13, 2009 · N617FE · Doug MD11F · Vertical Stabilizer, Attach FittingsSDR FDEA200907062488Vane · delaminatedRIGHT WING INBOARD FLAP VANE LOWER AND UPPER SURFACE FOUND DELAMINATED AT BETWEEN NR 1 AND 2 VANE TRACK AREA. REMOVED AND REPLACED IAW AMM 27-50-22-4, REVISION 64. RT INBD FLAP VANE ADJUSTMENT AND TEST IAW WORK CARD NR E1-5750-7-5003 C3 PART 2.Jul 6, 2009 · N617FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200906302401Fitting · crackedCRACKED INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON FIRST LAYER (SKIN) AT RT SIDE BANJO FITTING, AFT ROW LOWEST NR 4 FASTENER HOLE. REPAIR CARRIED OUT AS PER EA 1-5530-132118, REPAIR CATEGORY B, ACCOMPLISH INITIAL INSPECTIJun 30, 2009 · N617FE · Doug MD11F · Vertical Stabilizer, Attach FittingsSDR FDEA200906302400Fitting · crackedVERTICAL STABILIZER LT NR 4 FWD BANJO FITTING FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 55-20-00 FIGURE 3 VOLUME I, REVISION 40. REPAIR CATEGORY B, DAMAGE TOLERANCE INSPECTION REQUIREMENT INITIAL 5400 CYCLE, REPETITIVE 2700 CYCLE AS PER DRAWING NR SN1Jun 30, 2009 · N617FE · Doug MD11F · Vertical Stabilizer, Attach FittingsSDR FDEA200906272347Hinge Bracket · corrodedCORROSION-BORE OF LT WING OTBD FLAP INBD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT OTBD LUG. REPAIR CARRIED OUT AS PER EA 1-5750-131725, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jun 27, 2009 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200906272346Hinge Bracket · corrodedCORROSION-BORE OF LT WING OTBD FLAP INBD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT INBD LUG. REPAIR CARRIED OUT AS PER EA 1-5750-131725, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jun 27, 2009 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200906272345Hinge · corrodedCORROSION-OTBD BORE OF LT WING OTBD FLAP INBD HINGE (WING MOUNTED) LWR ATTACHMENT. REPAIR CARRIED OUT AS PER EA 1-5750-131725, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jun 27, 2009 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200906272344Hinge · corrodedCORROSION-INBD BORE OF LT WING OTBD FLAP INBD HINGE (WING MOUNTED) LWR ATTACHMENT. REPAIR CARRIED OUT AS PER EA 1-5750-131725, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jun 27, 2009 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200906272343Hinge · corrodedCORROSION-BORE OF LT WING OTBD FLAP INBD HINGE (WING MOUNTED) PIVOT ATTACHMENT. REPAIR CARRIED OUT AS PER EA 1-5750-131725, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jun 27, 2009 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200906272342Hinge · corrodedCORROSION-BORE OF RT WING OTBD FLAP INBD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT INBD. FOUND CORROSION. REPAIR CARRIED OUT AS PER E.A. 1-5750-131726, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jun 27, 2009 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200906272341Hinge Bracket · corrodedCORROSION-BORE OF RT WING OTBD FLAP, OTBD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT INBD LUG. REPAIR CARRIED OUT AS PER E.A. 1-5750-131727, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jun 27, 2009 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200906272340Hinge Bracket · corrodedCORROSION-LWR BORE OF RT WING OTBD FLAP OTBD HINGE (WING MOUNTED) SIDE LINK ATTACHMENT. REPAIR CARRIED OUT AS PER E.A. 1-5750-131727, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jun 27, 2009 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200906272339Hinge Bracket · corrodedCORROSION-UPPER BORE OF RT WING OTBD FLAP OTBD HINGE (WING MOUNTED) SIDE LINK ATTACHMENT. REPAIR CARRIED OUT AS PER E.A. 1-5750-131727, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jun 27, 2009 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200906272338Hinge · corrodedCORROSION-BORE OF LT WING OTBD FLAP OTBD HINGE (WING MOUNTED) FWD ATTACHMENT LUG OTBD. REPAIR CARRIED OUT AS PER E.A. 1-5750-131724. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.Jun 27, 2009 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200906272337Hinge Bracket · corrodedCORROSION-UPPER BORE OF LT WING OTBD FLAP OTBD HINGE (WING MOUNTED) SIDE LINK ATTACHMENT. REPAIR CARRIED OUT AS PER E.A. 1-5750-131724, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jun 27, 2009 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200906272336Hinge Bracket · corrodedCORROSION-LOWER BORE OF LT WING OTBD FLAP OTBD HINGE (WING MOUNTED) SIDE LINK ATTACHMENT. REPAIR CARRIED OUT AS PER E.A. 1-5750-131724 REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.Jun 27, 2009 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200906262326Fitting · crackedVERTICAL STABILIZER RT NR 4 FWD BANJO FITTING FOUND WITH CRACK. REPAIR CARRIED OUT AS PER SRM 55-20-00 FIGURE 3 VOLUME I, REVISION 40. REPAIR CATEGORY B DAMAGED TOLERANCE INSPECTION REQUIREMENT INITIAL 5400 CYCLE, REPETITIVE 2700 CYCLE AS PER DRAWING NR Jun 26, 2009 · N617FE · Doug MD11F · Vertical StabilizerSDR FDEA200906262325Intercostal · crackedRT NR 2 ENGINE INTAKE DUCT (INTERNAL) SUPPORT FRAME AT STA ZFR 2033 FOUND WITH CRACK. REPAIR CARRIED OUT AS PER E.A. 1-5530-132119, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jun 26, 2009 · N617FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA200906262324Support · crackedLT NR2 ENGINE INTAKE DUCT (INTERNAL) SUPPORT FRAME AT STA ZFR 2033 FOUND WITH CRACK. REPAIR CARRIED OUT AS PER E.A. 1-5530-132119, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jun 26, 2009 · N617FE · Doug MD11F · Vertical Stabilizer Miscellaneous StructureSDR FDEA200906262313Skin · crackedCTR LANDING GEAR WHEEL WELL RT SIDEWALL DOUBLER ON CUTOUT CRACKED AT STA 1390. CUTOUT STA 1390 REPLACED AS PER SRM 51-31-01 VOLUME II, REVISION 40 AND SRM 51-33-01 VOLUME II, REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 107.Jun 26, 2009 · N617FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200906242278Web · crackedCRACK INDICATION FOUND ON SECOND LAYER WEB AT 2 O'CLOCK POSITION DURING HFEC OPEN HOLE INSP ON 0.520 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 7 SUPPORT FITTING AT HOLE NR B. MAIN CARGO DOOR LOWER JAMB NO.7 SUPPORT FITTING AT HOLE NO. B SECOND LAYER WEB RJun 24, 2009 · N617FE · Doug MD11 · Fuselage Main, StructureSDR FDEA200906242277Web · crackedCRACK INDICATION FOUND ON FIRST LAYER WEB AT 5 O'CLOCK POSITION DURING HFEC OPEN HOLE INSP ON 0.520 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 7 SUPPORT FITTING AT HOLE NR B. REAMED TO DIAMETER 0.540 INCH IAW SRM 51-31-01 VOLUME II, REVISION 40. REPAIR CARRIEDJun 24, 2009 · N617FE · Doug MD11 · Fuselage Main, StructureSDR FDEA200906242276Web · crackedCRACK INDICATION FOUND ON FIRST LAYER WEB AT 7 O'CLOCK POSITION DURING HFEC OPEN HOLE INSP AT MAIN CARGO DOOR LWR JAMB NR 7 SUPPORT FITTING AT HOLE C. REPAIR CARRIED OUT ON WEB AS PER E.A. 1-5310-132111, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISIONJun 24, 2009 · N617FE · Doug MD11F · Fuselage Main, StructureSDR FDEA200906232241Access Panel · crackedRT WING L/E LOWER ACCESS FOUND CRACKED AT APPROX XOS 612. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I, REVISION 40. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100, REVISION 107.Jun 23, 2009 · N617FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200906232240Stop Fitting · crackedRT WING OTBD FLAP SECONDARY STOP FITTING FOUND CRACKED. STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II, REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 107.Jun 23, 2009 · N617FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200903220996Fuel Tank · venting"TANK WING OVERFILL" AMBER LEVEL 2. COMPLIED WITH RED TABS. VISUALLY CONFIRMED FUEL VENTING FROM CARGO BAY WINDOW. FUEL VENTING FROM OVER TOP OF LT AILERON. RTB WITH FUEL DUMP OF APPROX 90,000 LBS. UNEVENTFUL LDG. NO FUEL VENTING AFTER FUEL DUMP. CREW Mar 22, 2009 · N617FE · Doug MD11F · Fuel StorageSDR FDEA200812235266Pressure Switch · frozenLOW SPEED REJECTED T/O AT 75KT DUE TO LEVEL 2 ENGINE OIL FILTER 3 ALERT. COMPLETED RTO AND OIL FILTER CHECK LISTS. OIL TEMPS WERE ALL AT 65 DEGREES. ACFT COLD SOAKED FROM SITTING IN VERY COLD AIR FOR 2 DAYS. CONTACTED MX AND AGREED THAT PROBLEM WAS MOST LIKEDec 23, 2008 · N617FE · Doug MD11F · Turbine Engine Oil SystemSDR 08FDEA01468Pin · installedAFTER TAKEOFF AND GEAR RETRACTION. CENTER MAIN LANDING GEAR SHOWED RED. EXTENDED GEAR ALL POSITIONS GREEN. DUMPED 30K FUEL. RETURNED TO MEM LANDED UNEVENTFULLY. REMOVED CENTER LANDING GEAR SAFETY LOCK PIN. RETURNED TO SERVICE.Apr 21, 2008 · N617FE · Doug MD11F · Landing Gear SystemSDR 08FDEA00324Chain · failedDURING ESCAPE SLIDE/RAFT OPS CHECK, MED L1 FAILED TO DEPLOY IN EMERGENCY MODE. L1 DOOR AFT DRUM POWER DRIVE ROLLER CHAIN REMOVED AND REPLACED AS PER CMM 52-11-09. EMERGENCY OPERATIONAL TEST CARRIED OUT AS PER AMM 52-11-04-5.Jan 29, 2008 · N617FE · Doug MD11F · Escape SlideSDR 08FDEA00255Hinge · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD HINGE AFT FAIRING STRUT AFT FASTENER HOLE FOUND CORRODED. CORROSION AT LEFT WING OUTBOARD FLAP OUTBOARD HINGE AFT STRUT AFT HOLE REPAIRED AS PER FEDEX EA NR 1-5750-117303, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 24, 2008 · N617FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA00256Support Bracket · corrodedFOUND CORROSION, LT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT INBOARD CENTER FASTENER HOLE. CORROSION REPAIRED AS PER EA 1-5750-117305, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 24, 2008 · N617FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA00254Seat Track · crackedMAIN DECK STA 755, X = 48, SEAT TRACK FOUND CRACKED. CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 24, 2008 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00253Skin · dentedRT WING, INBOARD FLAP LOWER SURFACE FOUND DENTS AT XIFH 192. REPAIR CARRIED OUT AT RT WING INBOARD FLAP LOWER SURFACE DENT AREA AT XIFH 192 AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 24, 2008 · N617FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA00252Strut · corrodedFOUND CORROSION, LT WING OUTBOARD FLAP INBOARD HINGE AFT FAIRING STRUT AFT FASTENER HOLE. CORROSION REPAIRED AS PER EA 1-5750-117306, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 24, 2008 · N617FE · Doug MD11F · Wing Miscellaneous StructureSDR 08FDEA00251Strut · corrodedFOUND CORROSION, LT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING STRUT FORWARD FASTENER HOLE. CORROSION REPAIRED AS PER EA 1-5750-117306, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 24, 2008 · N617FE · Doug MD11F · Wing Miscellaneous StructureSDR 08FDEA00250Support · corrodedFOUND CORROSION LEFT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT INBOARD FORWARD FASTENER HOLE. MINOR CORROSION REPAIRED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER DRAWING ARC1984. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 24, 2008 · N617FE · Doug MD11F · Wing Miscellaneous StructureSDR 08FDEA00226Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE FITTING ARC4009 FORWARD INBOARD FASTENER HOLE FOUND CORROSION. LT WING, OUTBOARD FLAP R & R AS PER AMM 27-50-30-4. FLAP ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-830-805. TEST OF THE FLAP SYSTEM OPERATION/RANGE OF MOJan 22, 2008 · N617FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA00225Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE FITTING ARC4008 OUTBOARD FASTENER HOLE FOUND CORROSION. LT WING, OUTBOARD FLAP R & R AS PER AMM 27-50-30-4. FLAP ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-830-805. TEST OF THE FLAP OPERATION/RANGE OF MOVEMENT CARRIED OUJan 22, 2008 · N617FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA00224Seat Track · corrodedMAIN DECK SEAT TRACK AT STA 1806 LBL 8 FOUND EXFOLIATION CORROSION. MAIN DECK SEAT TRACK REPAIR CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 22, 2008 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00223Skin · crackedRT WING, LEADING EDGE LOWER ACCESS PANEL 618FB INBOARD FORWARD CORNER CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE LOWER ACCESS PANEL 618FB INBOARD FORWARD CORNER AS PER EA 1-5740-117298, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 22, 2008 · N617FE · Doug MD11F · Wing, Plate/SkinSDR 07FDEA02348Element · failedAT SFS DURING PRE-FLIGHT, GOT AIR SYSTEM TEST FAIL. TRIED SECOND TIME WITH SAME ALERT. CALLED MX, THEY TEST AIR SYSTEM AND GAVE OK TO GO. UPON DEPARTURE DURING CLIMB, GOT AVIONICS FAN OVRD PASSING FL230 FOLLOWED SHORTLY BY LEVEL 2 AIR MANF 1 FAIL. FOLLOWEDJul 1, 2007 · N617FE · Doug MD11F · Air Distribution SystemSDR 07FDEA00610Brake · separatedDURING TIRE CHANGE, FOUND THAT NR 1 BRAKE COMING APART REMOVED AND REPLACE NR 1 BRAKE PER AMM 32-43-01-4. OPS AND LEAK CHECK GOOD.Feb 27, 2007 · N617FE · Doug MD11 · BrakeSDR 06FDEA02984Doubler · crackedSNRM N00670: RT WING - STA XOS 641 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED. SNRM N00670: COMPLIED WITH NR 1-5730-100726, TITLE: WINGS - LEADING EDGE BEADED DOUBLER - PERMANENT REPAIR. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 14, 2006 · N617FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA02983Skin · crackedSNRM N00669: RT WING - STA XOS 647 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED. SNRM N00669: COMPLIED WITH FEDEX EA NR1-5730-100726, TITLE: WINGS - LEADING EDGE BEADED DOUBLER - PERMANENT REPAIR. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-10Aug 14, 2006 · N617FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA02973Skin · crackedSNRM N00639: LT WING - STA XOS 639 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED. SNRM N00639: COMPLIED WITH FEDEX EA NR1-5730-100725, TITLE: WINGS - LEADING EDGE BEADED DOUBLER - PERMANENT REPAIR. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-1Aug 14, 2006 · N617FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA02982Doubler · crackedRT WING - STA XOS 701 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED. COMPLIED WITH NR1-5730-103472, TITLE: WINGS, LEADING EDGE BEADED DOUBLER, PERMANENT REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 14, 2006 · N617FE · Doug MD11F · Wing, Plate/SkinSDR 06FDEA2972Doubler · crackedLEFT HAND WING - STA XOS 628 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.Aug 14, 2006 · N617FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA2973Doubler · crackedLEFT HAND WING - STA XOS 639 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.Aug 14, 2006 · N617FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA2974Doubler · crackedLEFT HAND WING - STA XOS 646 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.Aug 14, 2006 · N617FE · Doug MD11 · Wing, Plate/Skin
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