GE CF6-6D

Service difficulty reports · 1,051

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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 engine_model_key = 'CF66D'
  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 FDEA201008253122Skin · misrepairedRT WING DROOP L/E INBD EXTERIOR SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR AT RT WING DROOP L/E INBD EXTERIOR SURFACE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-00-01 FIG 4, VOL I, REV 96. EA8-5750-143409, REPAIR CLASSIFIED AS MAJOR IAW GMM Aug 25, 2010 · N562FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201008253124Slat · misrepairedRT WING SLAT NR 2 UPPER SURFACE OTBD CORNER FOUND EXISTING REPAIR. EXISTING REPAIR AT RT WING SLAT NR2 UPPER SURFACE OTBD CORNER EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW APPROVED DATA. EXISTING REPAIR REMOVED IAW SRM 51-31-01, VOL II REV 96. NEWAug 25, 2010 · N562FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201008233094Skin · misrepairedRT WING UPPER SURFACE FIXED L/E AT XOS 660 FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT RT WING UPPER SURFACE FIXED L/E XOS 660 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR ACCOMPLISHED IAW EA NR 8-5730-143420, REPAIR CLAAug 23, 2010 · N562FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201008233095Floor Support · misrepairedFWD CARGO - FOUND EXISTING REPAIR ON LONGERON 52 AT STA 808 TO STA 859. EXISTING REPAIR AT FWD CARGO LONGERON 52 STA 808 TO STA 859 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTING REPAIR PARTS REMOVED IAW SRM 51-31-01, VOLUMEAug 23, 2010 · N562FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201008233097Skin · misrepairedRT WING SLAT TRACK NR10 CUTOUT FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT RT WING SLAT TRACK NR10 CUTOUT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. RT WING SLAT TRACK NR10 CUTOUT, REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 68, VOLAug 23, 2010 · N562FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201008233098Skin · misrepairedRT WING FUELING STATION DOOR INBD SIDE FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT RT WING FUELING STATION DOOR INBD SIDE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. RT WING FUELING STATION DOOR INBD SIDE CARRIED OUT REPAIR IAW Aug 23, 2010 · N562FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201008233099Skin · misrepairedFUSELAGE - EXTERIOR SURFACE AT APPROX STA 463 TO STA 475 BETWEEN LONGERON 29 LT AND LONGERON 30 LT FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT FUSELAGE EXTERIOR SURFACE AT APPROX STA 463 TO STA 475 BETWEEN LONGERON 29 LT AND LONGERON 30 LT EVALUATED AND FAug 23, 2010 · N562FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201008233100Skin · misrepairedFUSELAGE - EXTERIOR SURFACE AT APPROX STA 557 TO STA 572 BETWEEN LONGERON 45 LT AND LONGERON 47 LT FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT FUSELAGE EXTERIOR SURFACE AT APPROX STA 557 TO STA 572 BETWEEN LONGERON 45 LT AND LONGERON 47 LT EVALUATED AND Aug 23, 2010 · N562FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201008233102Skin · misrepairedFUSELAGE - EXTERIOR SURFACE AT APPROX STA 1581 TO STA 1601 BETWEEN LONGERON 50 LT AND LONGERON 52 FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT FUSELAGE EXTERIOR SURFACE AT APPROX STA 1581 TO STA 1601 BETWEEN LONGERON 50 LT AND LONGERON 52 EVALUATED AND FOAug 23, 2010 · N562FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201008233103Skin · misrepairedNR3 AIRCON - AFT OF DOOR CUTOUT AT APPROX STA 524 TO STA 540 BETWEEN LONGERON 31 RT AND LONGERON 32 RT FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT NR3 AIRCON - AFT OF DOOR CUTOUT AT APPROX STA 524 TO STA 540 BETWEEN LONGERON 31 RT AND LONGERON 32 RT EVALUATAug 23, 2010 · N562FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201008233105Frame · misrepairedFWD CARGO - EXISTING REPAIR AT CARGO SIDE AFT DOOR JAMB. EXISTING REPAIR AT FWD CARGO, CARGO SIDE AFT DOOR JAMB EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR CARRIED OUT IAW EA 8-5310-143729. TITLE: FUSELAGE - MAIN FRAME - FAug 23, 2010 · N562FE · Doug MD1010F · Fuselage Main, FrameSDR FDEA201008223091Frame · crackedFUSELAGE - FWD AVIONICS COMPARTMENT STA 348 FRAME AT LONGERON 28 RT FOUND CRACKED. FUSELAGE - FWD AVIONICS COMPARTMENT STA 348, FRAME AT LONGERON 28 RT. R & R IAW SRM 51-31-01, VOL II, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.Aug 22, 2010 · N396FE · Doug MD1010F · Fuselage Main, FrameSDR FDEA201008203056Frame · misrepairedFWD CARGO - EXISTING REPAIR AT LOWER FRAME STA 1099, "X" = -38 TO "X" = -48. EXISTING REPAIR AT FWD CARGO LOWER FRAME STA 1099, "X" = -38 TO "X" = -48 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY APPROVED DATA. EXISTING REPAIR FOUND TO BE ACCEPTABAug 20, 2010 · N562FE · Doug MD1010F · Fuselage Main, FrameSDR FDEA201008193045Skin · crackedRT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACKED. RT WING FIXED L/E TELESCOPIC DUCT CUTOUT CRACKED INBD AND OTBD AREA TRIMMED AND REPAIRED IAW EA NR 8-5710-143702, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Aug 19, 2010 · N562FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201008193046Skin · crackedLT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACKED. LT WING FIXED L/E TELESCOPIC DUCT CUTOUT CRACKED AREA ACCOMPLISHED REPAIR IAW EA NR 8-5710-143715, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Aug 19, 2010 · N562FE · Doug MD1010F · Wing Main, Frame StructureSDR FDEA201008193047Skin · misrepairedRT WING SLAT NR4 EXTERIOR SURFACE LWR EDGE FOUND 02 EA EXISTING REPAIRS. 02 EACH EXISTING REPAIRS AT RT WING SLAT NR4 EXTERIOR SURFACE LOWER EDGE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR ACCOMPLISHED IAW EA 8-5750-14371Aug 19, 2010 · N562FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201008173029Seat Track · wornSEAT TRACK AT LBL 48 BETWEEN STA 1630 AND STA 1661 HAS SEVERAL WORN TRACK SCALLOPS. ABRICATED NEW SECTION OF SEAT TRACK ON STAM TRAVELER T10/848877 AND REPAIR PARTS ON TRAVELER T10/848872. REPLACED SEAT TRACK IAW SRM 53-70-00. CLASSIFIED AS A MAJOR REPAIRAug 17, 2010 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201008132994Landing Gear · malfunctionedON INITIAL GEAR EXTENSION ALL 3 WERE UNSAFE ON BOTH PRIMARY & SECONDARY INDICATORS WENT AROUND COMPLIED WITH QRH CYCLED GEAR UP THEN DOWN. GOT 3 GREEN. UNEVENTFUL LANDING. JACKED ACFT IAW MM 07-11-00-2 RETRACTED GEAR OPS CHECK GOOD. UPON EXTENDING LANDINAug 13, 2010 · N68053 · Doug MD1010F · Landing Gear Retraction/Extension SystemSDR FDEA201008122946Hinge Bracket · corrodedLT WING OTBD FLAP, OTBD HINGE, BARREL NUT UPPER BORE HOLE FOUND CORRODED AFTER BUSHING REMOVED. REWORKED IAW EA NR 8-5740-132487, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.Aug 12, 2010 · N372FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201008122950Hinge Bracket · corrodedLT WING SIDE OTBD FLAP, OTBD HINGE, BARREL NUT LOWER BORE HOLE FOUND CORRODED AFTER BUSHING REMOVED. LT WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER BORE HOLE REWORKED AS PER EA 8-5740-132487, BUSHING FABRICATED AND INSTALLED AS PER EA 8-5740-13248Aug 12, 2010 · N372FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201008122951Hinge Bracket · corrodedLT WING SIDE OTBD FLAP, OTBD HINGE, BARREL NUT BORE FOUND CORRODED AFTER BUSHING REMOVED. LT WING SIDE OTBD FLAP, OTBD HINGE BARREL NUT BORE HOLE REWORKED IAW EA 8-5740-132487, BUSHING FABRICATED AND INSTALLED IAW EA 8-5740-132487. REPAIR CLASSIFIED AS MIAug 12, 2010 · N372FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201008122952Hinge Bracket · corrodedRT WING SIDE OTBD FLAP, INBD HINGE UPPER MOUNT FWD FACE FOUND CORRODED. REWORKED IAW EA 8-5740-132488, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.Aug 12, 2010 · N372FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201008122953Hinge Bracket · corrodedRT WING SIDE OTBD FLAP INBD HINGE BARREL NUT SURFACE FOUND CORRODED. RT WING SIDE OTBD FLAP INBD HINGE BARREL NUT SURFACE REWORKED IAW EA 8-5740-132488, REPAIR CLASSIFIED AS MINOR IAWGMM 6-2-100, REV 110.Aug 12, 2010 · N372FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201008122954Hinge Bracket · corrodedRT WING SIDE OTBD FLAP, INBD HINGE, BARREL NUT UPPER BUSHING FOUND CORRODED. BUSHING REMOVED AND FOUND BORE EXCEED LIMIT IAW CMM 57-44-08 REV 50. EXISTING BORE DIAMETER 0.494", MAXIMUM BORE DIA 0.490". BUSHING FABRICATED AND INSTALLED IAW EA 8-5740-132488. REAug 12, 2010 · N372FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201008122955Hinge Bracket · corrodedRT WING SIDE OTBD FLAP INBD HINGE BARREL NUT LOWER BUSHING FOUND CORRODED. BUSHING REMOVED AND FOUND BORE EXCEED LIMIT IAW CMM 57-44-08 REV 50. EXISTING BORE DIA 0.4965", MAXIMUM BORE DIAMETER 0.490". BUSHING FABRICATED AND INSTALLED IAW EA NR 8-5740-132488Aug 12, 2010 · N372FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201008122956Hinge Bracket · corrodedRT WING SIDE OTBD FLAP INBD HINGE AFTER PIVOT POINT BUSHING REMOVED, BORE FOUND CORRODED. BORE FOUND CORRODED RT WING SIDE OTBD FLAP INBD HINGE PIVOT POINT REWORKED IAW EA 8-5740-132488, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.Aug 12, 2010 · N372FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201008122945Skin · misrepairedFUSELAGE - EXISTING REPAIR DOUBLER FOUND AT FUSELAGE SKIN AT LT STA 1541 TO STA 1561, LONGERON 45L. SKIN EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED PER SRM 51-33-01 VOLUME II REVISION 96 AND NEW REPAIR CARRIEDAug 12, 2010 · N383FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201008122948Skin · misrepairedLT WING TIP AFT CAP AT STA XW 930 FOUND EXISTING REPAIR.REPAIR EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED PER SRM 51-31-01 VOLUME II REVISION 96 AND NEW REPAIR CARRIED OUT PER E.A. 8-5730-140434, REPAIR IS CLASSAug 12, 2010 · N383FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201008122966Hinge Bracket · corrodedLT WING SIDE OTBD FLAP INBD HINGE BARREL NUT LOWER BUSHING FOUND CORRODED. LOWER BUSHING REMOVED AND F0UND BORE EXCEED LIMIT AS PER CMM 57-44-08 REVISION 50. EXISTING BORE DIAMETER 0.502", MAXIMUM BORE DIAMETER 0.490". REPAIRED AND INSTALLED BUSHING AS PER EAAug 12, 2010 · N372FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201008122967Hinge Bracket · corrodedLT WING SIDE OTBD FLAP INBD HINGE BARREL NUT UPPER BUSHING FOUND CORRODED. BUSHING REMOVED AND F0UND BORE EXCEED LIMIT AS PER CMM 57-44-08 REVISION 50. EXISTING BORE DIAMETER 0.5045", MAXIMUM BORE DIAMETER 0.490". REPAIRED AND INSTALLED BUSHING AS PER EA 8-57Aug 12, 2010 · N372FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201008122968Hinge Bracket · corrodedLT WING SIDE OTBD FLAP INBD HINGE FWD MOUNT OTBD BUSHING FOUND CORRODED. BUSHING REMOVED AND FOUND BORE EXCEED LIMIT AS PER CMM 57-44-08 REVISION 50. EXISTING BORE DIAMETER 1.259", MAXIMUM BORE DIAMETER 1.254". REPAIRED AND INSTALLED BUSHING AS PER EA 8-574Aug 12, 2010 · N372FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201008122969Hinge Bracket · corrodedLT WING SIDE OTBD FLAP INBD HINGE BARREL NUT SURFACE FOUND CORRODED. HINGE BARREL NUT SURFACE REWORKED AS PER EA 8-5740-132489, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 110.Aug 12, 2010 · N372FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201008122970Hinge Bracket · corrodedLT WING SIDE OTBD FLAP INBD HINGE PIVOT POINT BORE HOLE FOUND CORRODED AFTER BUSHING REMOVED. REWORKED AS PER EA 8-5740-132489, BUSHING FABRICATED AND INSTALLED AS PER EA 8-5740-132489. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 110.Aug 12, 2010 · N372FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201008122971Hinge Bracket · corrodedLT WING SIDE OTBD FLAP INBD HINGE BARREL NUT UPPER BORE HOLE FOUND CORRODED AFTER BUSHING REMOVED. REWORKED AS PER EA 8-5740-132489, BUSHING FABRICATED AND INSTALLED AS PER EA 8-5740-132489. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 110.Aug 12, 2010 · N372FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201008122972Hinge Bracket · corrodedLT WING SIDE OTBD FLAP INBD HINGE BARREL NUT LOWER BORE HOLE FOUND CORRODED AFTER BUSHING REMOVED. REWORKED AS PER EA 8-5740-132489, BUSHING FABRICATED AND INSTALLED AS PER EA 8-5740-132489. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 110.Aug 12, 2010 · N372FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201008122973Hinge Bracket · corrodedLEFT WING SIDE OTBD FLAP INBD HINGE FWD MOUNT OTBD BORE HOLE FOUND CORRODED AFTER BUSHING REMOVED. LT WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT OUTBOARD BORE HOLE REWORKED AS PER EA 8-5740-132489, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISIONAug 12, 2010 · N372FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201008122974Stiffener · crackedCABIN STA 1160 TO 1169 XCW=0 CTR WING TANK UPPER SURFACE STIFFENER FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II REVISION 96. NEW STIFFENER REWORKED FROM S1325739S TEE EXTRUSION 7075-0-0-094" AS PER DRAWING NPB 6072 REVISION AL. REPAIR CLAAug 12, 2010 · N372FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201008122944Hinge Bracket · corrodedLT WING OTBD FLAP OTBD HINGE BARREL NUT SURFACE FOUND CORRODED. LT WING SIDE OTBD FLAP, OTBD HINGE BARREL NUT SURFACE REWORKED IAW EA 8-5740-132487, MATERIAL REMOVED 0.008", REMAINING THICKNESS 0.418". REPAIR EVALUATED AND FOUND REMAINING THICKNESS 0.394"(Aug 12, 2010 · N372FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201008112941Strut · failedON POST FLIGHT, FOUND NOSE GEAR COLLAPSED AND LOWER COLLAR OUT OF SHRUT. REMOVED AND REPLACED NOSE LANDING GEAR ASSY IAW WORK CARD 32T2701. OPS, LEAK & RIG CHECKS NORMAL.Aug 11, 2010 · N68052 · Doug MD1010F · Nose/Tail Landing Gear Strut/AxleSDR FDEA201008102914Hinge · corrodedRT WING OTBD FLAP INBD HINGE PIVOT POINT INBD BORE HOLE FOUND CORRODED. REWORKED IAW EA NR 8-5750-132465, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.Aug 10, 2010 · N372FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201008102916Hinge Bracket · corrodedRT WING SIDE OTBD FLAP OTBD HINGE BARREL NUT FOUND SURFACE CORROSION. REWORKED IAW EA NR 8-5740-132486, SHIM FABRICATED AND INSTALLED IAW EA NR8-5740-132486. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.Aug 10, 2010 · N372FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201008102897Longeron · damagedCTR CARGO - UPON REMOVAL OF EXISTING REPAIR IAW SNRM N01182, EXISTING LONGERON 46R, SPLICE AT STA 1671 FOUND WITH 6 EACH FASTENER HOLES ELONGATED. DAMAGED LONGERON 46R AT CENTER CARGO STA 1671 TRIMMED OUT PER SRM 53-10-00 FIGURE 1 AND 2 VOLUME I REVISION 96Aug 10, 2010 · N383FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201008102896Skin · dentedRT WING INBD FLAP INBD AFT SEGMENT UPPER SURFACE FOUND DENTED AT MID AREA. DENT AREA AT RIGHT HAND WING INBOARD FLAP INBOARD AFT SEGMENT UPPER SURFACE MID SKIN AREA CARRIED OUT DOUBLER REPAIR AS PER SRM 57-10-00 FIGURE 85 VOLUME I, REVISION 96. REPAIR CLAAug 10, 2010 · N396FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201008092895Frame · crackedCABIN RT STA 1781, STR 11R, FRAME FOUND CRACKED. REPAIRED IAW SRM 53-30-00, FIG 5 (SHEET 1) VOL I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110. INITIAL INSP TO BE CARRIED OUT ON 12,000 FLIGHT CYCLES AND REPETITIVE INSP ON 8,000 FLIGHT CYCLES.Aug 9, 2010 · N372FE · Doug MD1010F · Fuselage Main, FrameSDR FDEA201008092880Skin · dentedFUSELAGE SKIN DENTED LT STA 1881 - 1898 AT LONGERON 36L. SIDEWALL PANELS REMOVED TO FOM IAW SRM 51-31-00, VOL II. DISPLACED INSULATION TO FOM IAW AMM 25-20-00. DENT OUT OF LIMITS IAW SRM 53-20-00, VOL I. FABRICATED REPAIR PARTS IAW SRM 53-20-00, FIG 6, VOLAug 9, 2010 · N567FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201008092875Wedge · dentedRT INBD ELEVATOR T/E WEDGE FOUND DENT. RIGHT HAND INBOARD ELEVATOR TRAILING EDGE WEDGE DENT MEASURED AND FOUND EXCEEDED LIMIT AS PER SRM 55-00-01 FIGURE 4 VOLUME I, REVISION 96. DEPTH = 0.089 INCH LENGTH = 1 INCH X 2 INCH. WEDGE REPAIRED AS PER SRM 55-30-00 FAug 9, 2010 · N396FE · Doug MD1010F · Elevator, Plate/SkinSDR FDEA201008072868Skin · delaminatedRT WING NR3 SPOILER PANEL UPPER SURFACE FOUND WITH DELAMINATION. REPAIR CARRIED OUT IAW EA NR8-5770-132457, TITLE: "WINGS - RT WING NR 3 SPOILER DELAMINATION - REPAIR." THIS REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100 REV 110.Aug 7, 2010 · N383FE · Doug MD1010F · SpoilersSDR FDEA201008062849Skin · crackedDURING WALKAROUND CHECK, RT WING ADJACENT TO NR 3 SLAT L/E TELESCOPIC DUCT CUT-OUT UPPER SECTION FOUND CRACKED.Aug 6, 2010 · N372FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201008062866Longeron · misrepairedFWD CARGO - EXISTING REPAIR AT LONGERON 52 FROM STA 979 TO STA 1039. FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED PER SRM 51-35-01 VOLUME II REVISION 96 AND NEW REPAIR CARRIED OUT PER FEDEX E.A. 8-5310-140425, EO 8-5100-Aug 6, 2010 · N383FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201008062848Skin · crackedDURING WALK AROUND CHECK LT WING ADJACENT TO NR 3 SLAT L/E TELESCOPIC DUCT CUT-OUT UPPER SECTION FOUND CRACKED. REPAIR ACCOMPLISHED PER EA 8-5710-140449. REPAIRED CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 110.Aug 6, 2010 · N372FE · Doug MD1010F · Leading Edge Devices
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