N613FE

Service difficulty reports · 422

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 = 'N613FE' 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 08FDEA04162Attach Fitting · corrodedLEFT WING OUTBOARD FLAP VANE ATTACHMENT FITTING NR 3 FROM INBOARD FOUND CORROSION AFTER REMOVED FROM FLAP. CORROSION REMOVED BY MACHINED AS PER SRM 57-20-00 FIGURE 19 VOLUME I AND EXCEED LIMITS. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 1, 2008 · N613FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04161Attach Fitting · corrodedLEFT WING OUTBOARD FLAP VANE ATTACHMENT FITTING NR 4 FROM INBOARD FOUND CORROSION AFTER REMOVED FROM FLAP. CORROSION REMOVED BY MACHINED AS PER SRM 57-20-00 FIGURE 19 VOLUME I AND EXCEED LIMIT. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 1, 2008 · N613FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04160Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE AFT FITTING AFT BORE HOLE FOUND WITH PITTING CORROSION. FITTING REPAIRED AS PER E.A. NO. 1-5750-122572. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 1, 2008 · N613FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04159Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING ARC1984 INBOARD MID MOUNTING HOLE FOUND CORROSION. FITTING ARC1984 REPAIRED AS PER E.A. NR 1-5750-122571. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 1, 2008 · N613FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04158Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING ARC1984 OUTBOARD AFT MOST MOUNTING HOLE FOUND CORROSION. CORROSION IN AFT MOST MOUNTING HOLE FITTING ARC1984 REPAIRED AS PER E.A. NR 1-5750-122571. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 1, 2008 · N613FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04156Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP OUTBOARD AFT HINGE AFT FITTING AFT BORE HOLE FOUND PITTING CORROSION. FITTING REPAIRED AS PER E.A. 1-5750-122574. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 1, 2008 · N613FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04155Hinge Bracket · corrodedLT WING OUTBOARD FLAP ASSEMBLY INBOARD HINGE BRACKET ARC1984 MOUNTING BORE HOLE OUTBOARD NR 3 FOUND WITH PITTING CORROSION. MOUNTING BORE HOLE OUTBOARD NR 3 BRACKET ARC1984 REPAIRED AS PER E.A. NR 1-5750-122573. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 1, 2008 · N613FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04154Hinge Bracket · corrodedLT WING OUTBOARD FLAP ASSEMBLY INBOARD HINGE BRACKET ARC1984 MOUNTING BORE HOLE INBOARD NR 2 FOUND WITH PITTING CORROSION. INBOARD NR 2 MOUNTING BORE HOLE AT LT WING OUTBOARD FLAP ASSY INBOARD HINGE BRACKET ARC1984 REPAIRED AS PER E.A. NR 1-5750-122573. REPAOct 1, 2008 · N613FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04153Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP ASSEMBLY INBOARD HINGE BRACKET ARC4009 MOUNTING BORE HOLE INBOARD NR 2 FOUND WITH PITTING CORROSION. CORROSION REMOVED AS PER E.O. 1-5750-5008 PART 1. FINAL HOLE DIAMETER = 0.660", MAXIMUM HOLE DIAMETER = 0.660". CORROSION STILL EXIST.Oct 1, 2008 · N613FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04152Beam · crackedMAIN DECK CARGO - DOOR LEFT 3 NR 5 BEAM FORWARD STOP FITTING AREA FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Sep 30, 2008 · N613FE · Doug MD11F · Fuselage Main, StructureSDR 08FDEA04146Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE AFT LOWER OUTBOARD MOUNTING BORE HOLE INNER SURFACE FOUND WITH PITTING CORROSION. CORROSION AT LT WING OUTBOARD FLAP INBOARD FORWARD HINGE AFT LOWER OUTBOARD MOUNTING BORE HOLE REMOVED AND FOUND WITHIN LIMIT AS Sep 30, 2008 · N613FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04102Attach Fitting · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR OUTBOARD ATTACHMENT POINT INBOARD SURFACE FOUND PITTING CORROSION.Sep 29, 2008 · N613FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04100Attach Fitting · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR INBOARD ATTACHMENT POINT INBOARD SURFACE FOUND PITTING CORROSION.Sep 29, 2008 · N613FE · Doug MD11F · Wing, Attach FittingsSDR 08FDEA04099Attach Fitting · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR INBOARD ATTACHMENT POINT INNER SURFACE FOUND PITTING CORROSION.Sep 29, 2008 · N613FE · Doug MD11F · Wing, Attach FittingsSDR 08FDEA04090Attach Fitting · scratchedRIGHT WING OUTBOARD FLAP INBOARD HINGE AFT MOUNTING LOWER OUTBOARD MOUNTING BORE HOLE INNER FACE FOUND WITH SCRATCH MARKS.Sep 29, 2008 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 08FDEA04071Spar Cap · damagedRIGHT WING REAR SPAR UPPER CAP AT STA XORS 676, 875, AND 887 FOUND HOLE ELONGATED. CARRIED OUT REPAIR AS PER EA NR 1-5710-123124. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 26, 2008 · N613FE · Doug MD11F · Wing SparSDR 08FDEA04065Fitting · crackedHFEC INSPECTION CARRIED OUT ON DIAMETER 0.520" HOLES AT MAIN DECK CARGO DOOR NR 7 SPOOL FITTING, FOUND CRACK INDICATION ON HOLE 'B' SECOND LAYER FROM TOP. CARRIED OUT REPAIR AS PER E.A. 1-5310-123123. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 26, 2008 · N613FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA04064Fitting · crackedHFEC INSPECTION CARRIED OUT ON DIAMETER 0.520 INCH HOLES AT MAIN DECK CARGO DOOR NR 6 SPOOL FITTING. FOUND CRACK INDICATION ON HOLE 'B' SECOND LAYER FROM TOP. CARRIED OUT REPAIR AS PER E.A. 1-5310-123123. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 26, 2008 · N613FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA04063Fitting · crackedHFEC INSPECTION CARRIED OUT ON DIAMETER 0.520 INCHES HOLES AT MAIN DECK CARGO DOOR NR 5 SPOOL FITTING, FOUND CRACK INDICATION ON HOLE C AT DOOR JAMB FIRST LAYER. CARRIED OUT REPAIR AS PER EA 1-5310-123123. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 26, 2008 · N613FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA04062Skin · chafedRIGHT WING LEADING EDGE TELESCOPIC DUCT CUT OUT INBOARD DOUBLER FOUND CHAFED. DOUBLER REPAIRED AS PER SRM 57-10-00. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 26, 2008 · N613FE · Doug MD11F · Wing Miscellaneous StructureSDR 08FDEA04060Fitting · crackedHFEC INSPECTION CARRIED OUT ON DIAMETER 0.460 INCH HOLES AT MAIN DECK CARGO DOOR NR 3 SPOOL FITTING, FOUND CRACK INDICATION ON HOLE B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Sep 26, 2008 · N613FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA04058Fitting · crackedHFEC INSPECTION CARRIED OUT ON DIAMETER 0.460 INCH HOLES AT MAIN DECK CARGO DOOR NR 7 SPOOL FITTING, FOUND CRACK INDICATION ON HOLE A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Sep 26, 2008 · N613FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA04057Fitting · crackedHFEC INSPECTION CARRIED OUT ON DIAMETER 0.460 INCH HOLES AT MAIN DECK CARGO DOOR NR 6 SPOOL FITTING, FOUND CRACK INDICATION ON HOLE A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Sep 26, 2008 · N613FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA04054Fitting · crackedHFEC INSPECTION CARRIED OUT ON DIAMETER 0.460 INCH HOLES AT MAIN DECK CARGO DOOR NR 5 SPOOL FITTING, FOUND CRACK INDICATION ON HOLE A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Sep 26, 2008 · N613FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA04052Fitting · crackedHFEC INSPECTION CARRIED OUT ON DIAMETER 0.460 INCH HOLES AT MAIN DECK CARGO DOOR NR 4 SPOOL FITTING, FOUND CRACK INDICATION ON HOLE A, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Sep 26, 2008 · N613FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA04046Fitting · crackedHFEC INSPECTION CARRIED OUT ON DIAMETER 0.460 INCH HOLES AT MAIN DECK CARGO DOOR NR 2 SPOOL FITTING FOUND CRACK INDICATION ON HOLE NR A, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Sep 25, 2008 · N613FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA04044Fitting · crackedHFEC INSPECTION CARRIED OUT ON DIAMETER 0.460 INCH HOLES AT MAIN DECK CARGO DOOR NR 1 SPOOL FITTING FOUND CRACK INDICATION ON HOLE NR A, B, C AND WITH CRACK INDICATION. SPOOL FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED ASSep 25, 2008 · N613FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA04028Doubler · crackedCENTER LANDING GEAR WHEEL WELL, FOUND FORWARD RIGHT LOWER CORNER DOUBLER CRACKED. CRACKED DOUBLER REMOVED AND REPLACED AS PER SRM 51-35-01 AND SRM 51-33-01. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Sep 25, 2008 · N613FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA01538Hose · leakingLEVEL 3 ENG 2 A-ICE DUCT ALERT, COMPLIED WITH QRH, ENG 2 SHUTDOWN. FLIGHT CREW VERBAL REPORTED ALERT CAME ON 45 MINS BEFORE LAND TO NRT. DUCT SENSOR RESISTANCE. PER FIM 30-22-00. FOUND SHORT TO GROUND AT P1-1843, PIN 10 WAS 15KOHM AND PIN 11 WAS 15KOHM. Apr 24, 2008 · N613FE · Doug MD11F · Central WarningSDR 07FDEA01955Seat Track · crackedAFTER CEILING REMOVAL, 1 CRACK FOUND ON SEAT TRACK LOWER SURFACE AT STA 750 LBL 44. [SUP 06-08-07] REPAIR CARRIED OUT AS PER 53- 70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 23, 2007 · N613FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA01946Longeron Splice · crackedAFTER BLANKET REMOVAL FOR WINDOW FRAME INSPECTION, MAIN DECK CARGO COMPARTMENT, RIGHT LONGERON 24R SPLICE STA 5-123 FOUND CRACKED. MAIN DECK CARGO COMPARTMENT - RIGHT HAND LONGERON 24R CRACKED SPLICE STA 5- 123 REMOVED AS PER SRM 51-31-01 VOLUME II. NEMay 22, 2007 · N613FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 07FDEA01928Seat Track · damagedMAIN DECK CARGO COMPARTMENT, SEAT TRACK STA 765 X= 8.5 FOUND BROKEN. [SUP 06-08-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 22, 2007 · N613FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA01920Frame · damagedMAIN DECK CARGO COMPARTMENT, RIGHT MAIN FRAME STA 1661 EXISTING REPAIR DOUBLER AT LONGERON 12R FOUND DAMAGED. MAIN DECK CARGO COMPARTMENT, RIGHT FUSELAGE MAIN FRAME AT STA 1661. DAMAGED EXISTING REPAIR DOUBLER AT LONGERON 12R REMOVED AND REPLACED. REPAIR May 21, 2007 · N613FE · Doug MD11F · Fuselage Main, FrameSDR 07FDEA01919Frame · damagedMAIN DECK CARGO COMPARTMENT, LEFT MAIN FRAME STA 1661 EXISTING REPAIR DOUBLER AT LONGERON 12L FOUND DAMAGED. MAIN DECK CARGO COMPARTMENT, LEFT FUSELAGE MAIN FRAME STA 1661 DAMAGED EXISTING REPAIR DOUBLER AT LONGERON 12L REMOVED AND REPLACED. REPAIR CARRIEDMay 21, 2007 · N613FE · Doug MD11 · Fuselage Main, FrameSDR 07FDEA01921Fitting · corrodedLEFT WING LOWER WINGLET AFT FITTING FWD AND AFT HOLES FOUND CORRODED. [SUP 05-29-07] CORRODED FWD AND AFT HOLES AT LEFT HAND WING LOWER WINGLET ATTACHED AFT FITTING REPAIRED AS PER FEDEX EA 1-5730-111107. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.May 21, 2007 · N613FE · Doug MD11F · Wing, Attach FittingsSDR 07FDEA01862Stringer · crackedLEFT WING, LEADING EDGE CAVITY STRINGER AT XOS 667 FOUND WITH 0.375 INCH CRACK. [SUP 06-08-07] COMPLIED WITH FEDEX EA 1-5710-111105, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM CHAPTER 6-2-100.May 21, 2007 · N613FE · Doug MD11F · Wing, Longeron/StringerSDR 07FDEA01861Skin · crackedRIGHT WING LEADING EDGE WING ANTI-ICE TELESCOPIC DUCT CUT-OUT STA XOS 464 AND STA 469 FOUND CRACKED. [SUP 06-08-07] REPAIRED AS PER SRM 57-10-00 VOLUME I, FIGURE 43. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.May 20, 2007 · N613FE · Doug MD11F · Wing, Plate/SkinSDR 07FDEA01860Skin · crackedLEFT WING TELESCOPIC DUCT CUT-OUT FOUND WITH 0.3125 INCH CRACKED. [SUP 06-08-07] REPAIRED AS PER SRM 57-10-00 VOLUME I , FIGURE 43. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 20, 2007 · N613FE · Doug MD11F · Wing, Plate/SkinSDR 07FDEA01859Trunnion · crackedNOSE LANDING GEAR LEFT TRUNNION FITTING FOUND WITH CRACKED. [SUP 06-08-07] NOSE LANDING GEAR LEFT HAND TRUNNION FITTING CARRIED OUT REPAIR AS PER SRM 53-40- 00 VOLUME I, FIGURE 23 AND FEDEX E.A.1-5310-111106, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 20, 2007 · N613FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR 06FDEA2570Striker · out of adjustPASSING 20,000 FT ON CLIMBOUT VERY LOUD SQUEAL BEGAN FROM UPPER RT SIDE OF CAPT'S SLIDING WINDOW CAN FEEL LARGE AMOUNT OF AIRFLOW AT TOP OF WINDOW. CHANGED CABIN PRESSURE BOTH UP AND DOWN, NO HELP. CHECKED RIG OF CAPT SLIDING WINDOW PER AMM 56-12-01-5. FOUNJul 14, 2006 · N613FE · Doug MD11 · Flight Compartment WindowsSDR 06FDEA0234Skin · chafedLEFT HAND WING - LEADING EDGE SKIN BETWEEN SLAT TRACK NR 6 AND NR 7. FOUND WITH CHAFING MARK. DOUBLER FABRICATED AND INSTALLED AT LEFT HAND WING LEADING EDGE SKIN BETWEEN SLAT TRACK #6 AND #7 AS PER SRM 57-10-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AJan 17, 2006 · N613FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA0153Unknown · unknownEMPENNAGE, TO CARRY OUT FEDEX EA 1-5510-80336 HORIZONTAL STABILIZER AFT STRINGER PANEL ASSEMBLY SPLICE REPAIR. COMPLIED WITH FEDEX EA 1-5510-80336, TITLE: STABILIZERS - HORIZONTAL STABILIZER - AFT STRINGER PANEL ASSEMBLY (P/N: ALC8103-504) SPLICE REPAIR, AIRWJan 11, 2006 · N613FE · Doug MD11 · Empennage StructureSDR 06FDEA0094Frame · wornNR 2 ENGINE, LEFT CORE COWL INTERIOR FRAME (5TH FROM FORWARD) FOUND EXISTING REPAIR STRIP AND FRAME WORN. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL.II.Jan 9, 2006 · N613FE · Doug MD11F · Nacelle/Pylon, Frame/Spar/RibSDR 06FDEA0093Spar Cap · damagedTWO (2) EACH FASTENER HOLE AT LOWER REAR SPAR CAP AT STA XORS 1062, FOUND ELONGATED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5720-94587.Jan 9, 2006 · N613FE · Doug MD11 · Wing SparSDR 06FDEA0092Spar Cap · crackedRIGHT WING, LOWER REAR SPAR CAP AT STA XORS 1048 FOUND WITH APPROX 1.25 INCH CRACKED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5720-94587.Jan 9, 2006 · N613FE · Doug MD11 · Wing SparSDR 06FDEA0091Splice · crackedFUSELAGE, LEFT CENTER ACCESSORY COMPARTMENT, NR37 LONGERON SPLICE BETWEEN STA 6-90 TO STA 1139 FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.Jan 9, 2006 · N613FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 06FDEA0090Structure · dentedUPPER CARGO COMPARTMENT, RIGHT SIDEWALL, DENT AT INNER CHORD FOUND AT STA 1741, LONGERON 12R. REPAIRED AS PER SRM 53-30-00.Jan 9, 2006 · N613FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 06FDEA0089Structure · dentedUPPER CARGO COMPARTMENT, LEFT SIDEWALL, DENT INNER CHORD FOUND AT STA 1741, LONGERON 12L. REPAIRED AS PER SRM 53-30-00.Jan 9, 2006 · N613FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 06FDEA0088Seat Track · crackedFOUND UPPER CARGO COMPARTMENT CRACKED AT SEAT TRACK. CRACKED AT STA 6- 30, X= 47. REMOVED AS PER SRM 51-31-01 VOLUME II. NEW SEAT TRACK REWORKED AND INSTALLED AS PER 53-70-00 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 9, 2006 · N613FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA0087Skin · dentedFOUND LEFT WING, NR 8 SLAT OUTBOARD LEADING EDGE FOUND DENT. REPAIR CARRIED OUT AT LEFT HAND WING, #8 SLAT OUTBOARD LEADING EDGE SKIN AS PER SRM 57-10-00 VOLUME I, FIGURE 5. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.Jan 9, 2006 · N613FE · Doug MD11F · Leading Edge Devices
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