N657FE

Service difficulty reports · 180

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 = 'N657FE' 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 FDEA201506262055Floor Panel · crackedMAIN CARGO DECK BETWEEN FRAME 58 & 60, Y450 & Y953 FLOORBOARD HAS PUNCTURED & CRACKED. R & R FLOOR PANEL IAW AMM 53-10-23-04. NEW FLOOR PANEL FABRICATED ON T15 1147411 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Jun 26, 2015 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201506252054Floor Panel · crackedMAIN CARGO DECK BETWEEN FRAME 55 & 57.1, -Y 450 & -Y 953 FLOORBOARD HAS CRACKS. R & R FLOOR PANEL IAW AMM 53-10-23-04. NEW FLOOR PANEL FABRICATED ON T15 1147413 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Jun 25, 2015 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201506252053Floor Panel · crackedMAIN CARGO DECK BETWEEN FRAME 60 & 62, -Y 1456 & -Y 1959 FLOORBOARD HAS PUNCTURED. R & R FLOOR PANEL IAW AMM 53-10-23-04. NEW FLOOR PANEL FABRICATED ON T15 1147348 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Jun 25, 2015 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201506252052Floor Panel · crackedMAIN CARGO DECK BETWEEN FRAME 62 & 65, -Y 450 & -Y 953 FLOORBOARD HAS CRACKS. R & R FLOOR PANEL IAW AMM 53-10-23-04. NEW FLOOR PANEL FABRICATED ON T15 1147346 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Jun 25, 2015 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201506252051Floor Panel · crackedMAIN CARGO DECK FLOOR PANEL BETWEEN -Y 952 & -Y 450 & BETWEEN FRAME 30 & 34 IS CRACKED AT CHS ATTACH POINT. R & R FLOOR PANEL IAW AMM 53-10-23-04. NEW FLOOR PANEL FABRICATED ON T15 1147414 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Jun 25, 2015 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201506252050Floor Panel · damagedMAIN CARGO DECK BETWEEN FRAME 58 & 60, -Y 450 & -Y 953 FLOORBOARD HAS PUNCTURED & CRACKED. R & R FLOOR PANEL IAW AMM 53-10-23-04. NEW FLOOR PANEL FABRICATED ON T15 1147349 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Jun 25, 2015 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201506252049Floor Panel · crackedMAIN CARGO DECK FLOOR PANEL BETWEEN -Y952 & -Y450, BETWEEN FRAME 47 & 51 IS CRACKED AT CHS ATTACH POINT. R & R FLOOR PANEL IAW AMM 53-10-23-04. NEW FLOOR PANEL FABRICATED ON T15 1147417 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Jun 25, 2015 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201506252048Floor Panel · crackedMAIN CARGO DECK BETWEEN FRAME 60 & 62, -Y450 & -Y953 FLOORBOARD HAS CRACKS. R & R FLOOR PANEL 252 UH AT FRAME 60 TO 62 IAW AMM 53-10-23-04. NEW FLOOR PANEL FABRICATED ON T15 1147347 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Jun 25, 2015 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201506252047Floor Panel · crackedMCD FLOOR PANEL BETWEEN -Y952 & -Y450, BETWEEN FRAME 43 & 47 IS CRACKED AT CHS ATTACH POINT. R & R FLOOR PANEL IAW AMM 53-10-23-04. NEW FLOOR PANEL FABRICATED ON T15 1147416 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Jun 25, 2015 · N657FE · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201506252046Floor Panel · crackedMAIN CARGO DECK BETWEEN FRAME 65 & 69, -Y 953 & -Y 1456 FLOORBOARD HAS PUNCTURES & CRACKED. R & R IAW AMM 53-10-23-04. NEW FLOOR PANEL FABRICATED ON T15 1147345 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.Jun 25, 2015 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201506252045Floor Panel · crackedMAIN CARGO DECK BETWEEN FRAME 57.1 & 58, -Y 450 & -Y 953 FLOORBOARD HAS CRACKS. R & R FLOOR PANEL 252 GF AT FRAME 57.1 TO 58 IAW AMM 53-10-23-04. NEW FLOOR PANEL FABRICATED ON T15 1147412 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Jun 25, 2015 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201506242017Floor Panel · crackedMCD FLOOR PANEL BETWEEN -Y952 & -Y450, AND FRAMES 38.2 & 40 FOUND CRACKED. R & R THE FLOOR PANEL IAW AMM 53-10-23-01. MAJOR REPAIR.Jun 24, 2015 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201506242018Floor Panel · crackedMCD FLOOR PANEL BETWEEN -Y952 & -Y450, AND FRAMES 38.2 & 40 FOUND CRACKED. R & R THE FLOOR PANEL IAW AMM 53-10-23-01. MAJOR REPAIR.Jun 24, 2015 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201408212284Beam · lack of lubeLANDING GEAR WOULD NOT RETRACT IN SYS 1 OR 2 AFTER TAKEOFF. LUBE LT & RT MAIN GEAR BOGIE BEAMS & PERFORMED SEVERAL GEAR SWINGS WITH NO DEFECTS NOTED IAW AMM.Aug 21, 2014 · N657FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201404280877Rib · corrodedLEFT MLG RIB NR 5 HAS CORROSION IN BORE & FWD & AFT FACES. REPAIRED IAW EA 6-5710-T0307716 P1.Apr 28, 2014 · N657FE · Airbus A300F4605R · Wing, Landing Gear Attach FittingsSDR FDEA201404280876Rib · corrodedRIGHT RIB NR 5 HAS CORROSION IN BORE, FWD & AFT FACES. REPAIRED IAW EA 6-5710-T0307716 P2.Apr 28, 2014 · N657FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201401220163Seat Track · corrodedMAIN DECK CARGO FRAME 45 - 54 Y1456 SEAT TRACK CORRODED. PERFORMED SPLICE REPAIR IAW EA 6-5310-T0305630 P1.Jan 22, 2014 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201401150098Seat Track · damagedRAMP REPORTED SEAT TRACK ROBE DAMAGED FRAME 20. FLOOR TRACK SECURES MAIN DECK DOOR FWD ENTRANCE SIDE GUIDE. CUT OUT DAMAGED SEAT TRACK SECTION IAW SRM 53-10-16 FIG 201A FABRICATED REPAIR IAW SRM 53-10-16 FIG 201A. INSTALLED REPAIR IAW SRM 53-10-16 FIG 201Jan 15, 2014 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201401020003Crossbeam · crackedAVIONICS COMPARTMENT, CROSSBEAM NLG FRAME 15A WEB FACE AT ATTACHMENT FITTING OF RACK 107VU FOUND CRACKED. DRILLED FASTENER HOLES TO ALL THE REPAIR PARTS PER A300-600F SRM51-40-40 APPLIED PAINT PER A300-600F SRM51-75-21 INSTALLED REPAIR PARTS PER A300-600FJan 2, 2014 · N657FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201401010001Frame · crackedMAIN DECK FR 21, STRINGER 8 - 9 RT FRAME DEFORMED AT THE DOUBLER AREA. REMOVED DOUBLER AND FOUND CRACK ON FRAME. REPLACED FRAME PROFILE AND DOUBLER PER SRM 51-40-21.Jan 1, 2014 · N657FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201310222583Pivot · lack of lubeLANDING GEAR FAILED TO RETRACT. FOUND RT GEAR STIFF AND NOT POSITIONING CORRECTLY. LUBRICATED RT BOGIE BEAM PIVOT POINTS AND LINKS IAW SMP. GEAR IS FREE AND TILTS NORMALLY. PERFORMED GEAR SWINGS SEVERAL TIMES, GEAR OPERATES NORMALLY IN BOTH SYSTEMS IAW MM 3Oct 22, 2013 · N657FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201112215397Selector Valve · failedON INITIAL T/O ROLL, HAD FULL LT RUDDER AND ACFT WAS VEERING RT AT ABOUT 10 PERCENT DIVERGENCE FROM CENTER LINE. LOW SPEED R.T.U (L40 KTS). ON TAXI RETURN TO LINE, TILLER WAS NOT SMOOTH AND HAS A PROGRESSIVELY BAD "RATCHETY" FEEL, INSTEAD WITH RESISTANCE WDec 21, 2011 · N657FE · Airbus A300F4605R · Landing Gear Steering SystemSDR FDEA201111164933Floor Panel · damagedAFT CARGO FLOOR PANEL NR 152WF DAMAGED. FLOOR PANEL REMOVED AND REPLACED AS PER AMM 53-10-33-4 REVISION 52.0. NEW FLOOR PANEL FABRICATED AS PER DWG SRZ25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Nov 16, 2011 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111094833Floor Panel · damagedFORWARD CARGO COMPARTMENT FLOOR PANEL NR 131LG FOUND DAMAGED. FLOOR PANEL R & R IAW AMM 53-10-29-4, REV.52. NEW FLOOR PANEL FABRICATED IAW DWG: SRZ -25-005- REV: J, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 9, 2011 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111094832Floor Panel · damagedFORWARD CARGO COMPARTMENT FLOOR PANEL NR132LG FOUND DAMAGED. FLOOR PANEL R & R IAW AMM 53-10-29-4, REV 52.0. NEW FLOOR PANEL FABRICATED IAW DWG SRZ25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 9, 2011 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111084790Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR LT SEAT TRACK, Y =1959 AT FRAME 38.2 FOUND WITH CORROSION AT FLANGE. CORROSION REMOVED IAW SRM 51-74-10, REV 21. MATERIAL REMOVED 0.040 INCH MATERIAL. REMAINED 0.038 IN ORIGINAL MATERIAL THICKNESS 0.078 INCH AND FOUND OUT Nov 8, 2011 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111084789Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR LT SEAT TRACK, Y =1456 AT FRAME 58 FOUND WITH CORROSION AT FLANGE. REPAIR CARRIED OUT IAW SRM 53-10-16, FIG 201, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 8, 2011 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111084788Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR LT SEAT TRACK, Y= 1959 AT FRAME 40 FOUND WITH CORROSION AT FLANGE. CORROSION REMOVED IAW SRM 51-74-10, REV 21. MATERIAL REMOVED 0.039 INCH MATERIAL REMAINED 0.041 INCH MATERIAL THICKNESS MEASURED 0.080 INCH AND FOUND OUT OF Nov 8, 2011 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111084787Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR LEFT SEAT TRACK, Y=1456 AT FRAME 54.1, FOUND WITH CORROSION AT FLANGE. CORROSION REMOVED IAW SRM 51-74-10, REV 21 MATERIAL REMOVED 0.040 INCH MATERIAL REMAINED 0.038 INCH ORIGINAL THICKNESS 0.078 IN AND FOUND OUT OF LIMIT IAWNov 8, 2011 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111074773Mount · corrodedNR 2 PYLON FORWARD MOUNT INBD AFT BOLT HOLE SPOT FACE FOUND CORRODED. REPAIRED IAW EA 6-5450-155829. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 7, 2011 · N657FE · Airbus A300B4622R · Nacelle/Pylon, Attach FittingsSDR FDEA201111054760Skin · dentedSKIN, FRAME 10, STRINGER 25, DENT FOUND. REPAIRED IAW WRI 53002442.Nov 5, 2011 · N657FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201111054759Hinge · crackedAVIONICS COMPARTMENT ACCESS DOOR RT HINGE ARM FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 52-41-14, FIG 201, REV 21. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 113.Nov 5, 2011 · N657FE · Airbus A300F4605R · Fuselage, Door HingeSDR FDEA201111054758Hinge · crackedAVIONICS COMPARTMENT ACCESS DOOR LT HINGE ARM FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 52-41-14 FIG 201, REV 21. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 113.Nov 5, 2011 · N657FE · Airbus A300F4605R · Fuselage, Door HingeSDR FDEA201111054757Floor Panel · dentedBULK CARGO COMPARTMENT, FLOOR PANEL NR161GF FOUND DENTED ON SEVERAL LOCATIONS. FLOOR PANEL R & R IAW AMM 53-10-35-4, REV 52.0. NEW FLOOR PANEL FABRICATED IAW DWG SRZ 25-011, REV D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 5, 2011 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111054756Floor Panel · corrodedBULK CARGO COMPARTMENT, FLOOR PANEL NR161HF FOUND CORRODED ON LOWER AND UPPER SURFACE. R & R IAW AMM 53-10-35-4, REV 52.0. NEW FLOOR PANEL FABRICATED IAW DWG SRZ 25-011, REV D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 5, 2011 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111054755Floor Panel · corrodedBULK CARGO COMPARTMENT, FLOOR PANEL NR161AF FOUND CORRODED ON LOWER SURFACE. R & R IAW AMM 53-10-35-4, REVISION 52.0. NEW FLOOR PANEL FABRICATED IAW DWG SRZ25-011. REV D REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 5, 2011 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111054754Floor Support · corrodedMAIN DECK FORWARD UTILITY, LT FLOOR AREA CORROSION FOUND ON FLOOR SUPPORT STRUCTURE, Y = 700 BETWEEN FRAME 11A AND FRAME 13A. CORROSION REMOVED IAW SRM 51-74-10 REV 21. MATERIAL REMOVED 0.051 INCH, MATERIAL REMAINED 0.029 INCH, ORIGINAL MATERIAL THICKNESS 0Nov 5, 2011 · N657FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201111014707Crossbeam · crackedCROSSBEAM 29, -Y680, -Z190 FOUND CRACKED. REPAIRED IAW NR 6-5310-155828. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 1, 2011 · N657FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201111014706Crossbeam · crackedAFT CARGO COMPARTMENT CROSSBEAM 64, -Y1150, -Z240 FOUND CRACKED. REPAIRED IAW EA 6-5310-155835. REPAIR CLASSIFIED AS MAJOR IAW REV 113.Nov 1, 2011 · N657FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201111014705Crossbeam · crackedFWD CARGO COMPARTMENT CROSSBEAM 31, Y1705, -Z210 FOUND CRACKED. REPAIRED IAW SRM 53-10-15, FIG 212 REVISION 21. CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100, REV 113.Nov 1, 2011 · N657FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201111014704Crossbeam · crackedFWD CARGO COMPARTMENT CROSSBEAM 30, Y1710, -Z210 FOUND CRACKED. REPAIRED IAW SRM 53-10-15, FIG 212, REV 21. CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100, REV 113.Nov 1, 2011 · N657FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201111014702Seat Track · corrodedMAIN DECK CARGO FLOOR, SEAT TRACK- Y1959 AT FR28 RT FOUND WITH CORROSION ON FLANGE AREA. REPAIRED IAW SRM 53-10-16 FIG 201, REV 21. CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100, REV 113.Nov 1, 2011 · N657FE · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111014701Seat Track · corrodedMAIN DECK CARGO FLOOR, SEAT TRACK- Y953 FR57 CORROSION FOUND ON FLANGE. CORROSION REMOVED IAW SRM 51-74-10, REV 21 MATERIAL REMOVED 0.041 INCH. MATERIAL REMAINED 0.039 INCH, ORIGINAL THICKNESS 0.080 INCH AND FOUND OUT OF LIMIT IAW SRM 53-10-16, FIG 102, REVNov 1, 2011 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001110082Slide · damagedR1 DOOR SLIDE DAMAGED DUE TO DOOR OPENED WHILE ACFT WAS PRESSURIZED. SLIDE REMOVED FROM DOOR. FRAME 13A IS BUCKLED BETWEEN BEAM 1 AND 3 FWD OF R1 DOOR. PREPARATION FOR FERRY FLIGHT FOR REPAIR, DAMAGE ACCEPTAPLE FOR FERRY FLIGHT IAW ABOVE EA.Jan 11, 2010 · N657FE · Airbus A300F4605R · Escape SlideSDR FDEA200906112036Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK NR 5 LT, 6 INCHES FWD OF FR 54 HAS A WORN SCALLOP. CUT OUT DAMAGE SECTION OF SEAT TRACK AND INSTALLED SEAT TRACK REPAIR - CTR SECTION FLOORBEAM RAIL SPLICING METHOD AT SEAT TRACK NR 5LT BETWEEN FR 52 AND FR 54 IAW SRM 53-Jun 11, 2009 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200906102013Skin · bentBULK CARGO DOOR EXTERIOR SKIN TOP FWD CORNER BENT AND CRACKED, I INCH LENGTH REMOVED DAMAGED SECTION OF CORNER AND INSTALLED OUTER CORNER REPAIR ON BULK CARGO DOOR TOP FWD CORNER IAW SRM 52-34-00,FIG 204, PAGE 233/234.Jun 10, 2009 · N657FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA200906091965Skin · gougedRT INBD FLAP UPPER SURFACE HAS 2 EA DENTS--1. 48 INCHES FROM INBD, 16 " FROM L/E, 2" X 1.5" X .043" 2. 47" FROM INBD, 27" FROM L/E, 1" X 1" X .031" REPAIRED 2 EA GOUGES IAW SRM 57-50-00, FIG 206 SHEET 1.Jun 9, 2009 · N657FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA200906051941Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK NR 3 LT BETWEEN FR 77 AND FR 78 HAS 1 SQ INCH OF CORROSION REMOVED LEVEL 1 CORROSION. CUT OUT DAMAGED SECTION OF SEAT TRACK AND INSTALLED SEAT TRACK SPLICE REPAIR AT TRACK NR 3 LT BETWEEN FR 77 AND FR 80 IAW SRM 53-10-16Jun 5, 2009 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA05014Skin · chafedLT WING CENTER FLAP T/E UPPER SKIN 6" UP FROM T/E 3" INBD OF OTBD EDGE 2 EA GOUGES 1ST = .3 X .059 X .010 2ND = .5" X .3" X .013" REPAIRED DAMAGE IAW EA 6-5730-110528 REF PART 1 ITEM 3 REPAIR OF DAMAGE AERAS 1 AND 2 BLENDED AREAS AND CHECKED FOR CRACKS, NO CDec 7, 2007 · N657FE · Airbus A300F4605R · Trailing Edge FlapsSDR 07FDEA04371Regulator Valve · failedDURING TAKEOFF ROLL BELOW APPROX 60 KNOTS ENG NR 1 REV PRESSURIZED AT APPROX 80 PERCENT N1. REJECTED TAKEOFF. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 08OCT07. REACTIVATED NR 1 REVERSER, PERFORMED OPS CHECK, NO DEFECTS NOTED. RSep 28, 2007 · N657FE · Airbus A300F4605R · Engine Thrust Reverser
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