N588FE

Service difficulty reports · 346

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 = 'N588FE' 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 FDEA201012204729Cargo Track · corrodedMAIN DECK CARGO TRACK AT STATION 1665, 'X' = -27.5 FOUND CORRODED. REPAIRED BY SECTIONAL CARGO TRACK REPLACEMENT FROM STA 1631 TO STA 1671, 'X' = -27.5 IAW SRM 53-00-52, FIG 201 REPAIR 1, REV 45. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Dec 20, 2010 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012204726Skin · crackedRT WING FIXED L/E SLAT TRACK NR12 CUT OUT INBD LOWER FOUND CRACKED. REPAIR CARRIED OUT AT RT WING L/E SLAT TRACK NR12 CUT OUT INBD LOWER AREA IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 45. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 111.Dec 20, 2010 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201012204725Skin · crackedLT WING FIXED L/E SLAT TRACK NR12 CUT OUT FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIG 201, REV 45. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.Dec 20, 2010 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201012204724Access Panel · crackedRT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6. FOUND 12 EA FASTENER HOLES WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSP. REPAIR CARRIED OUT IAW DWG SG11570004 REV A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.Dec 20, 2010 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201012204723Access Panel · crackedLT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6. FOUND 04 EACH FASTENER HOLES WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSP. REPAIR CARRIED OUT IAW DWG SG11570004, REV A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.Dec 20, 2010 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201012204722Longeron Splice · crackedMAIN DECK - DURING HFEC INSP, LONGERON 3, RT SPLICE FITTING AT STA 6-100, FOUND 02 EACH CRACKED APPROX 0.5 INCH. CRACKED SPLICE FITTING AT STA 6-100. R & R IAW SRM 51-31-01, REV 45. NEW LONGERON SPLICE FITTING FABRICATED IAW DOUG DWG A6A7112 REV A. REPAIR CDec 20, 2010 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201012204721Frame · deformedMAIN DECK CARGO FRAME AT STA 1661, LONGERON 12 LT FOUND DEFORMED. MAIN DECK CARGO - DEFORMED FRAME AT STA 1661, LONG 12 LT REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2 REV 45. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE AT 9,500 CYCLES,Dec 20, 2010 · N588FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201012174714Vane · delaminatedLT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. R & R IAW AMM 27-50-22-4 REV 69.0. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5, REV 69.0 FOUND SATISFACTORY.Dec 17, 2010 · N588FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201012164709Spar Cap · corrodedLEFT WING REAR SPAR LOWER CAP, ACCESS THROUGH PANEL NR541FB, 8 IN OTBD OF JACK POINT FOUND CORROSION. REMOVED IAW SRM 51-31-01, REV 45 AND REPLACED WITH A FABRICATED STRAP IAW SRM 51-34-01, REV 45. STRAP FABRICATED IAW DWG ARB2615 REV D. FUEL LEAK CHECK Dec 16, 2010 · N588FE · Doug MD11F · Wing SparSDR FDEA201010063960Control Unit · failedDURING DESCENT, FSS DISCHARGED LIGHT ILLUMINATED. COMPLIED WITH EA EA 1-2620-141430 AND EA 1-2623-1441 28. OK. REMOVED AND REPLACED FIRE CONTROL UNIT, BOTH SENSOR BARS AND SURROGATE FIRE DETECTION UNIT AND WIRING HARNESS ON PENTRATOR 13.Oct 6, 2010 · N588FE · Doug MD11F · Fire DetectionSDR FDEA201009293790O-Ring · missingNOTICED NR 2 ENGINE OIL AT 7 QTS. LOSING APPROX 1 QT IN 20 MINUTES. DIVERTED. ENROUTE OIL QTY DECREASED TO 2 QTS & OIL PRESS STARTED TO DECREASE. ENGINE SHUTDOWN. EMERGENCY DECLARED. LANDING UNEVENTFUL. ISOLATED LEAK TO NR 2 ENG LOWER INBD HYD PUMP DRISep 29, 2010 · N588FE · Doug MD11F · Turbine Engine Oil SystemSDR FDEA200911103921Line · leakingLOST HYD 3 FLUID AT LEVEL OFF ALT. THE LOSS WAS RA PID BEFORE PUMPS COULD BE SECURE. ALT GEAR WAS EXT ENDED. UNABLE TO GET CTR FEAR DOWN. LANDED APPROX 15000 NR OVERWEIGHT. PUMPED 9000 NR OF FUEL. FOUND HYD LINE IN RT W/W BETWEEN NR 3 HYD RES C/L/G CNTL Nov 10, 2009 · N588FE · Doug MD11F · Hydraulic System, MainSDR FDEA200906182141Line · burstO2 LINE BEHIND 1ST OBSERVERS MASK BURST. ALL 3 OXYGEN SYS DEPLETED. COMPLIED WITH EA 1-3510-132815, DOC PART NR 1. INSTALLED CAP AND LEAKED CHECKED. REINSTALLED NR1 OBSERVER OXY MASK STORAGE BOX. CONNECTOR PLUG UNSECURED. REMOVED AND REPLACED NR 2 AND NRJun 18, 2009 · N588FE · Doug MD11F · Crew Oxygen SystemSDR FDEA200904011131Skin · misrepairedRIGHT WING INBOARD FLAP ASSEMBLY UNDER-SURFACE, EXISTING DOUBLER REPAIR FOUND AT LOWER SEGMENT AFT EDGE, STA XIFH 270. FOUND NOT CONFORM TO SRM REPAIR. RT INBD FLAP ASSY REMOVED AND REPLACED AS PER AMM 27-50-20-4 REV. 62. ADJUSTMENT AND TEST CARRIED OUT FOUApr 1, 2009 · N588FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200903301103Skin · misrepairedAGING INSPECTION, EXISTING REPAIR FOUND ON LT WING NR 4 SLAT LOWER SURFACE STA XOS= 602. EXISTING REPAIR ON LT WING NR 4 SLAT LOWER SURFACE STA XOS=602 EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM REPAIR. NR 4 SLAT ASSEMBLY REMOVED, REPLACED AND OPERATIONAMar 30, 2009 · N588FE · Doug MD11F · Leading Edge DevicesSDR FDEA200903301102Skin · misrepairedAGING INSPECTION, EXISTING REPAIR FOUND ON LT WING NR 2 SLAT LOWER SURFACE STA XIS= 325. EXISTING REPAIR ON LT WING NR 2 SLAT LOWER SURFACE STA XIS= 325 EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM REPAIR. LT WING NR 2 SLAT LOWER SURFACE STA XIS= 325 SKIN Mar 30, 2009 · N588FE · Doug MD11F · Leading Edge DevicesSDR FDEA200903301101Skin · misrepairedRIGHT WING, INBOARD AILERON ASSY UPPER SURFACE, EXISTING DOUBLER REPAIR FOUND AT LEADING EDGE STA XIA 328. RIGHT WING, INBOARD AILERON ASSY UPPER SURFACE, EXISTING REPAIR FOUND NOT IN ACCORDANCE WITH SRM REPAIR. RIGHT WING INBOARD AILERON ASSY UPPER SURFACE Mar 30, 2009 · N588FE · Doug MD11F · Wing, Control SurfacesSDR FDEA200903281093Structure · misrepairedAFT CARGO DOOR INTERNAL STRUCTURE FOUND WITH EXISTING REPAIR. AFT CARGO, DOOR INTERNAL STRUCTURE EXISTING DOUBLER EVALUATED, FOUND NOT IN ACCORDANCE WITH SRM REPAIR. AFT CARGO, DOOR INTERNAL STRUCTURE REPAIR CARRIED OUT AS PER EA 1-5280-127811. REPAIR CLAMar 28, 2009 · N588FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA200903281092Door · misrepairedCENTER CARGO, DOOR FOUND WITH EXISTING REPAIR. CENTER CARGO, DOOR EXISTING REPAIR EVALUATED AND FOUND THAT IT DOES NOT CONFORM TO SRM REPAIR IN CHAPTER 52. COMPLIED WITH EA 1-5230-127808, CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV 107. EO NR 1-510Mar 28, 2009 · N588FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA200903281091Skin · misrepairedFUSELAGE, EXISTING REPAIR DOUBLER FOUND AT RT STA 860 TO STA 865 STRINGER 34R TO 35R. FUSELAGE, EXISTING REPAIR DOUBLER AT RT STA 860 TO STA 865 STRINGER 34R TO 35R. EVALUATED AND FOUND TO BE NOT IN ACCORDANCE WITH THE SRM. COMPLIED WITH EA 1-5310-127807. Mar 28, 2009 · N588FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200903251034Skin · misrepairedFUSELAGE, EXISTING REPAIR DOUBLER AT RT STA 1781 STRINGER 49R TO 50R. FUSELAGE, EXISTING REPAIR DOUBLER AT RT STA 1781 STRINGER 49R TO 50R FOUND REPAIR DOES NOT CONFORM TO SRM. FUSELAGE STA 1781 STRINGER 49R TO 50R CARRIED OUT REPAIR AS PER MD-11 SRM 53-20-0Mar 25, 2009 · N588FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200903251035Frame · dentedRT STA 1721 LONGERON 12 FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG I VOL. I REV. 40. REPETITIVE INSPECTION REQUIRED INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL. I REV. 40. REPAIR CLAMar 25, 2009 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA200903241024Skin · misrepairedFUSELAGE, EXISTING REPAIR DOUBLER FOUND AT LT STA 730 TO STA 760 STRINGER 37L TO 39L. FUSELAGE, EXISTING REPAIR DOUBLER FOUND AT LT STA 730 TO STA 760 STRINGER 37L TO 39L. FOUND NOT IN ACCORDANCE TO SRM REPAIR. FUSELAGE LT STA 730 TO STA 760 STRINGER 37L TMar 24, 2009 · N588FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200903241023Tee Fitting · corrodedLT WING OTBD FLAP VANE TEE FITTING NR 4 FROM INBD TRACK ATTACH BORE FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-128667. CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.Mar 24, 2009 · N588FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200903241022Vane · corrodedLT WING OTBD FLAP VANE T-FITTING NR 1 FROM INBD TRACK ATTACH BORE FOUND CORRODED. COMPLIED WITH EA 1-5750-128666. CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.Mar 24, 2009 · N588FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200903220995Seat Track · corrodedCABIN, RT STA 5-43 TO STA 5-83 X= -8.5, SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. 1 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.Mar 22, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903220994Seat Track · corrodedCABIN, LT STA 1371 TO STA 1381 X= 75, SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. 1 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.Mar 22, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903220993Seat Track · corrodedCABIN, LT STA 1491 TO STA 1501 X= 8.5, SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107Mar 22, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903220992Seat Track · corrodedCABIN, RT STA 1381 TO STA 1481 X= -8.5, SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107Mar 22, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903220991Seat Track · corrodedCABIN, LT STA 1341 TO STA 1361 X= 75, SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.Mar 22, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903220990Vertical Support · crackedAFT FUSELAGE LOWER COMPARTMENT RT VERTICAL STIFFENER AT APPROX STA 2007 UPPER EDGE FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 53-00-01 FIG. 9 VOL. I REV. 40. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.Mar 22, 2009 · N588FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200903210989Seat Track · corrodedCABIN, LT STA 1331 X= 75 SEAT TRACK FOUND CORRODED. SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.Mar 21, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903210988Seat Track · corrodedCABIN, LT STA 1325 TO STA 1381, X= 8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107Mar 21, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903210987Seat Track · corrodedCABIN, RT STA 1305 X= -8.5 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.Mar 21, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903210986Seat Track · corrodedCABIN, RT STA 1279 TO STA 1299, X= -8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.Mar 21, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903210985Seat Track · corrodedCABIN, LT STA 1299 TO STA 1309, X= 75 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.Mar 21, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903210984Bracket · damagedLT WING OTBD FLAP OTBD FWD HINGE SIDE LINK BARREL NUT HOLE FOUND CORRODED. COMPLIED WITH EA 1-5750-127792. CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.Mar 21, 2009 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200903210983Seat Track · corrodedCABIN, RT STA 1401 TO STA 1426, X= -8 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.Mar 21, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903210982Seat Track · corrodedCABIN, LT STA 1401 TO STA 1461, X= 8 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.Mar 21, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903200977Doubler · crackedCENTER LANDING GEAR WHEEL WELL RT KEEL BEAM WEB FWD DOUBLER FOUND CRACKED. DOUBLER REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.Mar 20, 2009 · N588FE · Doug MD11F · Fuselage Main, KeelSDR FDEA200903200976Doubler · crackedCENTER LANDING GEAR WHEEL WELL LT KEEL BEAM WEB FWD DOUBLER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.Mar 20, 2009 · N588FE · Doug MD11F · Fuselage Main, KeelSDR FDEA200903200975Mount · corrodedRT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT OTBD HOLE FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-127785. CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.Mar 20, 2009 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200903200974Mount · corrodedRT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT INBD FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-127785. CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.Mar 20, 2009 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200903190970Spar Cap · crackedCRACK INDICATION APPROXIMATELY 1 INCH LENGTH FOUND ON THE LT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGES OF UPPER REAR SPAR CAP. REPAIRED AS PER SRM 55-20-00 FIG. 3 VOL. I REV. 40. CATEGORY 'B' REPAIR INITIAL INSPECTION TO BE CARRIED OUT AT 5400Mar 19, 2009 · N588FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA200903190969Spar Cap · crackedCRACK INDICATION APPROXIMATELY 1 1/4 INCH LENGTH FOUND ON THE RT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGES OF UPPER REAR SPAR CAP. CARRIED OUT REPAIR AS PER SRM 55-20-00 FIG. 3 VOL. I REV. 40. CATEGORY 'B' REPAIR INITIAL INSPECTION TO BE CARRIEMar 19, 2009 · N588FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA200903190968Seat Track · crackedCABIN, LT STA 695 TO STA 735, X= 8.5 SEAT TRACK FOUND CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 665 TO STA 745 X= 8.5 AS PER SRM 53-70-00 FIG. I VOL. I REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.Mar 19, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903190967Seat Track · corrodedCABIN,LT STA 415 TO STA 475. X= 107 SEAT TRACK FOUND CORROSION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.Mar 19, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903190966Seat Track · corrodedCABIN, LT STA 1521 TO STA 1531 X=8 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1411 TO STA 1531 X= 8 AS PER SRM 53-70-00 FIG. I VOL. I REV 40. REPAIR CLASSIFIED AS MAJOR AS PER REV. 107.Mar 19, 2009 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903180946Frame · dentedCABIN, LT STA 1701 LONGERON FRAME DOUBLER FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIG. I VOL. I REV. 40. REPETITIVE INSPECTION REQUIRED INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL. I Mar 18, 2009 · N588FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200903180945Frame · dentedCABIN, RT STA 1741 LONGERON 12 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I REVISION 40. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 Mar 18, 2009 · N588FE · Doug MD11F · Fuselage Main, Frame
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