N602FE

Service difficulty reports · 506

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 = 'N602FE' 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 04FDEA02976Support · corrodedLT WING - INBOARD FLAP VANE, OUTBOARD SUPPORT FITTING INBOARD HOLES (03 OFF) ARE CORRODED AND OUTBOARD HOLES FWD AND CENTER ARE CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. SUPPORT FITTING REPLACED AS PER AMM27-50-24 AND FUNCTIONAL TEST CARRIED OUT AS PER Oct 22, 2004 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02975Support Fitting · corrodedLT WING INBOARD FLAP VANE INBOARD SUPPORT FITTING INBOARD HOLES (03 OFF) ARE CORRODED AND OUTBOARD AFT HOLE IS CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. SUPPORT FITTING REPLACED AS PER AMM27-50-24 AND FUNCTIONAL TEST CARRIED OUT AS PER AMM 27-50-00-860-Oct 22, 2004 · N602FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02969Splice · crackedMAIN DECK - ATTIC AREA STA 5-116 LONGERON 9R LONGERON SPLICE FOUND CRACK. NEW LONGERON SPLICE FABRICATED AS PER DWG A5A7112. CRACKED LONGERON SPLICE REMOVED & REPLACED AS PER SRM 51-31-01 VOL 2.Oct 22, 2004 · N602FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA02968Longeron Splice · crackedMAIN DECK - ATTIC AREA STA 1538 LONGERON 6R LONGERON SPLICE FOUND CRACK. NEW LONGERON SPLICE FABRICATED AS PER DWG NR A5A7112. CRACKED LONGERON SPLICE REMOVED & REPLACED AS PER SRM51-33-01 VOL 2.Oct 22, 2004 · N602FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 04FDEA02977Tee Fitting · corrodedRIGHT HAND WING, INBOARD FLAP VANE INBOARD SUPPORT FITTING, INBOARD AFT HOLE CORRODED AND OUTBOARD HOLE (03 OFF) CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. RIGHT HAND WING, INBOARD FLAP VANE INBOARD SUPPORT FITTING, REMOVED AND REPLACED AS PER AMM 27-50-2Oct 22, 2004 · N602FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02967Spar Cap · corrodedEMPENNAGE, UPPER VERTICAL STAB AT FWD CTR SPAR APPROX BETWEEN ZFR 300 TO 340 RT SKIN EXTERIOR SURFACE FOUND CORRODED. EMPENNAGE, UPPER VERTICAL STAB AT FWD CTR SPAR APPROX BETWEEN ZFR 300 TO 340 RT SKIN EXTERIOR SURFACE CORROSION AREA REPAIRED AS PER FEDEX EAOct 22, 2004 · N602FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR 04FDEA02974Vane · corrodedLT WING IB FLAP VANE, IB TEE FITTING BORES HAVE CORROSION AND AFT HOLE IS NOT WITHIN EO LIMITS. CORROSION REMOVED AS PER SRM 51-21-01 VOL2 AND REPAIRED AS PER FEDEX EA 1-5750-81571.Oct 22, 2004 · N602FE · Doug MD11F · Leading Edge DevicesSDR 04FDEA02973Fitting · corrodedRT WING IB FLAP VANE, OB TEE FITTING BORE HOLES HAVE CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 AND REPAIRED AS PER FEDEX EA 1-5750-81570.Oct 22, 2004 · N602FE · Doug MD11F · Leading Edge DevicesSDR 04FDEA02966Structure · corrodedEMPENNAGE, UPPER VERTICAL STAB AT AFT CTR SPAR APPROX ZFR 564 RT EXTRUSION. EXTERIOR SURFACE FOUND CORRODED. CORROSION REPAIRED AS PER FEDEX EA 1-5530-81578.Oct 22, 2004 · N602FE · Doug MD11F · Ventral StructureSDR 04FDEA02965Structure · corrodedEMPENNAGE, UPPER VERTICAL STAB AT REAR SPAR ZFR 510 RT EXTRUSION, EXTERIOR SURFACE FOUND CORRODED. REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA NR 1-5530-81577.Oct 21, 2004 · N602FE · Doug MD11F · Elevator StructureSDR 04FDEA02964Spar · corrodedEMPENNAGE, UPPER VERTICAL STAB AT BETWEEN FWD CTR SPAR TO AFT CTR SPAR ZFR 328.0 LT SKIN EXTERIOR SURFACE FOUND CORRODED. CORROSION REMOVED & WITHIN LIMIT AS PER SRM55-00-01VOL1.Oct 21, 2004 · N602FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR 04FDEA02962Spar · corrodedEMPENNAGE, UPPER VERTICAL STAB AT FRONT SPAR BERWEEN ZFR 400.681 TO 424.219 LT EXTRUSION EXTERIOR SURFACE FOUND CORRODED. FOUND WITHIN LIMIT AS PER FEDEX EA #1-5530-81581.Oct 21, 2004 · N602FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR 04FDEA02963Spar · corrodedEMPENNAGE, UPPER VERTICAL STAB AT BETWEEN FWD CTR SPAR TO AFT CTR SPAR, ZID 92.50 LT SKIN EXTERIOR SURFACE FOUND CORRODED. CORROSION AREA REPAIRED AS PER FEDEX EA 1-5530-81582.Oct 21, 2004 · N602FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR 04FDEA02961Spar · corrodedEMPENNAGE, UPPER VERTICAL STAB AT FRONT SPAR BETWEEN ZID 92.50 TO ZFR 424.219 LT SKIN EXTERIOR SURFACE FOUND CORRODED. REMOVED & REPAIRED AS PER FEDEX EA 1-5530-81581.Oct 21, 2004 · N602FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR 04FDEA02960Spar · corrodedEMPENNAGE, UPPER VERTICAL STAB AT AFT CTR SPAR BERWEEN ZFR 389.681 TO 424.219 LT EXTRUSION EXTERIOR SURFACE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5530-81580.Oct 21, 2004 · N602FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR 04FDEA02955Cowling · crackedENG NR 2 LT HAND T/R COWL AT UPPER SLIDER TRACK END CRACKED. ENG NR 2 LEFT HAND T/R COWL UPPER SLIDER TRACK REPAIRED IAW ROHR AERO SERVICES - ASIA ENGINEERING REPAIR NR 'RASA-040560'. (WITH FAA FORM 8130-3, TRACKING 5586, J009768-000).Oct 20, 2004 · N602FE · Doug MD11 · Engine Thrust ReverserSDR 04FDEA02957Frame · crackedENG NR 1 LEFT HAND T/R COWL TOP AT FORWARD FRAME FOUND CRACKED. FRAME CRACKED REPAIR AS PER DRAWING SRZ78-002.Oct 20, 2004 · N602FE · Doug MD11F · Engine Thrust ReverserSDR 04FDEA02956Cowling · crackedENG NR 3 LEFT HAND T/R COWL AT UPPER SLIDER TRACK END FOUND CRACKED. UPP SLIDER TRACK REPAIRED AS PER FAA FORM 8130-3 TRACKING NR 5590 (J009773-000).Oct 20, 2004 · N602FE · Doug MD11F · Engine Thrust ReverserSDR 04FDEA02935Fitting · crackedRIGHT HAND WING FOUND OUTBOARD FLAP INBOARD STOP FITTING CRACKED, DURING DVI. STOP FITTING REMOVED & REPLACED AS PER SRM51-31-01VOL2 & SRM 51-33-01 VOL2.Oct 15, 2004 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02932Seat Track · corrodedFORWARD CABIN, MOST OUTBOARD LEFT SIDE SEAT TRACK AT APPROX STA 430-450 FOUND TOP SURFACES WITH CORROSION. SNRM N0083, FORWARD CABIN, STA 430-450 MOST OUTBOARD LEFT SIDE SEAT TRACK. CORROSION REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II AND SRM 51-33-01 VOct 14, 2004 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 03FDEA00794Hinge · crackedSNRM N1069 : LT WING FOUND LT OUTBOARD FLAP, INBOARD AFT HINGE FITTING TO FLAP LOWER AFT, FWD MOST HOLE QTY 01 EACH WITH SUSPECTED CRACK. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MMay 22, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00690Structure · corrodedHORIZONTAL STAB CENTER BOX RT 31R BORE EXISTING BUSHING REMOVED FOUND SIDEWALL AND BEARING SURFACE WITH CORROSION. REAM BORE TO 1.181 INCH MAX CORROSION STILL PRESENT ON SIDEWALL SURFACE. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69213 - STABILIZERS - HORIMay 7, 2003 · N602FE · Doug MD11 · Horizontal Stabilizer StructureSDR 03FDEA00689Structure · corrodedHORIZONTAL STAB CENTER BOX LT 31L BORE EXISTING BUSHING REMOVED FOUND BORE SIDEWALL AND BEARING SURFACE WITH CORROSION. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69213 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/REPAIR.May 7, 2003 · N602FE · Doug MD11 · Horizontal Stabilizer StructureSDR 03FDEA00793Hinge · corrodedRT WING, OUTBOARD FLAP, OUTBOARD FWD HINGE WITH ACTUATOR HOLES CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69243 WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS.May 5, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00724Hinge · corrodedRT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE TO FLAP LOWER SURFACE WITH HOLES FLAP SIDE QTY 4 EACH CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69251 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.May 5, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00857Hinge · damagedHFEC INDICATION FOUND IN INBOARD & OUTBOARD PIVOT HOLE BORE SURFACE ON OUTBOARD FLAP, OUTBOARD HINGE (FLAP SIDE) RT WING. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-66421 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE AFT SUPPORT BORE CORRODED.May 4, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00722Hinge · corrodedLT WING, FOUND OUTBOARD FLAP, OUTBOARD HINGE WING SIDE LINK ATTACHMENT HOLE LOCATION QTY 2 EACH CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69243 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LH & RH OUTBD FLAP OUTBD HINGE BRACKET REPAIRS.Apr 30, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00720Hinge · corrodedLT WING: O/B FLAP I/B HINGE ATTACHMENT TO FLAP LOWER AFT HOLE (2 EACH) FOUND CORRODED. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MM 27-50-00-5, FOUND SATIS. COMPLIED WITH FEDEX EAApr 30, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00719Hinge · corrodedLT WING, FOUND OUTBOARD FLAP, OUTBOARD HINGE FLAP SIDE AT FLAP LOWER SURFACE AFT HOLE QTY 2 EACH WITH CORROSION. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MM 27-50-00-5, FOUND SATISApr 30, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00718Hinge · corrodedLT WING, FOUND OUTBOARD FLAP, OUTBOARD HINGE FLAP SIDE AFT HOLES LOCATION QTY 2 EA WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69244 WINGS- TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBD FLAP HINGE BRACKET - STRUT REPAIR.Apr 30, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00717Hinge · corrodedLT WING, FOUND OUTBOARD FLAP, INBOARD HINGE FITTING FLAP SIDE TO FLAP MOUNTING HOLES LOCATION CORRODED. CORROSION ON LH WING, O/B FLAP I/B HINGE FITTING FLAP SIDE TO FLAP MOUNTING HOLES REMOVED AS PER SRM 51-21-01, VOL II. AND SRM 51-31-01, VOL II. REPAIR Apr 30, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00716Hinge · corrodedLT WING, FOUND OUTBOARD FLAP, INBOARD HINGE FITTING, FLAP SIDE TO FLAP MOUNTING HOLES LOCATION QTY 6 EACH CORRODED. CORROSION ON LH WING , O/B FLAP I/B HINGE FITTING, FLAP SIDE TO FLAP MOUNTING HOLES REMOVED AS PER SRM 51-21-01 VOL II & SRM 51-31-01 VOL IIApr 30, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00715Structure · corrodedO/B FLAP O/B HINGE ATTACHMENT TO FLAP (LOWER FWD HOLE, 5 EACH) FOUND CORRODED. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MM 27-50-00-5, FOUND SATIS. COMPLIED WITH FEDEX EA 1-5750Apr 30, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00714Hinge · corrodedLT WING: OUTBOARD FLAP INBOARD HINGE ATTACHMENT TO FLAP LOWER FWD HOLE (4 EACH) FOUND CORRODED. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MM 27-50-00-5, FOUND SATIS. COMPLIED WITHApr 30, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00712Structure · corrodedRT WING, FOUND OUTBD FLAP, INBOARD MOST HINGE LOCATION FLAP SIDE MOUNT HOLES QTY. 5 EACH LOCATION WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69251 WINGS- OUTBOARD FLAP HINGE FIIRINGS OVERSIZE HOLES- REPAIR.Apr 30, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00713Hinge Fitting · corrodedRT WING FOUND OUTBOARD FLAP, INBOARD MOST HINGE FITTING FLAP SIDE, AFT MOST HOLE LOCATION QTY. 1 EACH OUTBOARD MOST FACE WITH CORROSION. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69246 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RH OUTBOARD FLAP/IApr 30, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00659Structure · corrodedHORZ STABILIZER CENTER BOX LT NR 1 BARREL NUT HOLE FOUND WITH CORROSION. REAM BORE UP TO 1.549 INCH CORROSION STILL PRESENT ON THE SIDE OF BEARING SURFACE. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69213 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BOApr 29, 2003 · N602FE · Doug MD11 · Horizontal Stabilizer StructureSDR 03FDEA00637Spar Cap · corrodedLT WING, FOUND WING REAR SPAR UPPER CAP UPPER SURFACE WITH CORROSION FROM XORS 830 TO XORS 1090. OUTER LT WING/REAR SPAR TRAILING EDGE - LT REAR SPAR UPPER CAP REPAIRED FROM XORS 830 TO XORS 1090 AS PER FEDEX EA 1-5720-69229, SRM 57-20-00 FIG. 16 VOL. I ANApr 29, 2003 · N602FE · Doug MD11 · Wing SparSDR 03FDEA00640Rib · crackedRT WING, FOUND OUTBOARD FLAP, INBOARD STOP BOLT SUPPORT ISLAND WITH CRACK. REMOVED AND REPLACED AS PER 51-31-01 VOL. I.Apr 29, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00649Spar · corrodedLT WING FOUND REAR SPAR LOWER CAP WITH CORROSION AT XORS 1090.Apr 29, 2003 · N602FE · Doug MD11 · Wing SparSDR 03FDEA00795Flap Track · chafedLT WING OUTBOARD FLAP INBOARD TRACK (ON WING)FOUND WITH CHAFING MARKS. TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD FLAP TRACK REPAIRED AS PER EA 1-5750-69241.Apr 28, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00721Hinge · corrodedLT WING: O/B FLAP O/B HINGE (WING SIDE) LWR ATTACHMENT TO WING REAR SPAR FOUND WITH HOLE (2 EACH) CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69243 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRSApr 28, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00645Structure · corrodedLT WING OUTBOARD FLAP INBOARD HINGE ATTACHMENT TO WING REAR SPAR LOWER FITTING BORE HOLE (2 EACH) FOUND CORRODED. CORROSION ON LH WING OUTBOARD FLAP INBOARD HINGE ATTACHMENT TO WING REAR SPAR LOWER FITTING BORE HOLE ( 2 EACH )AREA REMOVED AND FOUND WITHIN LIApr 28, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00641Structure · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT BORE HOLE FOUND CORRODED.Apr 28, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00642Structure · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR ATTACH POINT BORE HOLE (2 EACH) FOUND CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69243 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LH AND RH OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAApr 28, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00643Structure · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) UPPER ATTACHMENT TO WING REAR SPAR HOLE (2 EACH) FOUND CORRODED. CORROSION ON LH WING, OUTBD FLAP, OUTBD HINGE (WINGSIDE) UPPER ATTACHMENT TO WING REAR SPAR HOLES (2 EACH) AREA REMOVED AS PER CMM 57-44-09 Apr 28, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00644Structure · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) UPPER ATTACHMENT FITTING TO WING REAR SPAR BORE HOLE (2 EACH) CORRODED. CORROSION ON LT WING OUTBOARD FLAP INBOARD HINGE (WINGSIDE) UPPER ATTACHMENT FITTING TO WING REAR SPAR BORE HOLES (2 EACH) REMOVED AND REApr 28, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00646Structure · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) FITTING BORE HOLE FOUND CORRODED. CORROSION ON LH WING OUTBOARD FLAP INBOARD HINGE (WINGSIDE) FITTING PIVOT BORE HOLE REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-44-08 FIG. 401.Apr 28, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00647Structure · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) ACTUATOR FITTING (2 EACH) BORE HOLE FOUND CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69242 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIRS.Apr 28, 2003 · N602FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA00648Structure · corrodedLT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT BORE HOLE FOUND WITH CORROSION. SURFACE CORROSION ON LT WING INBOARD FLAP OUTBOARD HINGE PIVOT BORE HOLE REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-44-07, FIG. 401.Apr 28, 2003 · N602FE · Doug MD11 · Trailing Edge Flaps
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