N578FE

Service difficulty reports · 364

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 = 'N578FE' 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 08FDEA04512Longeron · corrodedCENTER CARGO BETWEEN LT STA 5-123 TO 1541 LONGERON 48 HAS CORROSION. REMOVED AND FOUND EXCEED LIMITS AS PER SRM 53-00-01 FIGURE 4 VOLUME I. ORIGINAL THICKNESS = 0.130", MATERIAL REMOVED = 0.060 INCH, MATERIAL REMAINING = 0.070 INCH, LONGERON FABRICATED AS Oct 23, 2008 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 08FDEA04511Longeron Splice · corrodedCENTER CARGO, BETWEEN LEFT STA 5-53 TO 5-73 LONGERON 48 SPLICE FOUND CORRODED. CENTER CARGO BETWEEN LEFT STA 5-53 TO 5-73 LONGERON 48 SPLICE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIGURE 4 VOLUME I. ORIGINAL THICKNESS = 0.125 INCH, Oct 23, 2008 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 08FDEA04510Skin · cracked04 FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HFEC INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS = 690 AND STA XORS = 700. RIGHT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS = 690 AND STA XORS = 700, 04 FASTEOct 23, 2008 · N578FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA04509Skin · cracked08 FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HFEC INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS = 690 AND STA XORS = 700. LEFT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS = 690 AND STA XORS = 700, 08 EACH FASTOct 23, 2008 · N578FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA04496Longeron · corrodedCENTER CARGO, BETWEEN LT STA 5-32 TO 5-53 LONGERON 46 FOUND CORRODED. REPAIR CARRIED OUT IAW EA 1-5310-122603. CORROSION REMOVED AND FOUND EXCEED LIMITS IAW SRM 53-00-01. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Oct 23, 2008 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 08FDEA04495Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER ATTACH OUTBOARD HOLE AFT MATING SURFACE FOUND WITH CORROSION. CORROSION REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 23, 2008 · N578FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04494Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER ATTACH OUTBOARD HOLE FORWARD MATING SURFACE FOUND WITH CORROSION. CORROSION REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 23, 2008 · N578FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 08FDEA04493Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER ATTACH INBOARD HOLE AFT MATING SURFACE FOUND WITH CORROSION. CORROSION REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 23, 2008 · N578FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 08FDEA04492Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER ATTACH INBOARD HOLE FORWARD MATING SURFACE FOUND WITH CORROSION. CORROSION REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 23, 2008 · N578FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04491Hinge Bracket · chafedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT UPPER ATTACH OUTBOARD HOLE FOUND WITH SCORING MARK. SCORING REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 23, 2008 · N578FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04490Hinge · chafedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT UPPER ATTACH INBOARD HOLE FOUND WITH SCORING MARK. SCORING REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 23, 2008 · N578FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA04489Longeron · crackedCENTER CARGO, LEFT STA 5-21 LONGERON 41 FOUND EXISTING REPAIR SPLICE FITTING CRACKED. REPAIR SPLICE AT CENTER CARGO LT BS 5-21 LONGERON 41 REMOVED AND REPLACED AS PER SRM 51-33-01. SPLICE FABRICATED AS PER SRM 53-10-00. SPLICE PROCTECTED AND PAINTED AS PEOct 22, 2008 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 08FDEA04472Longeron · crackedCENTER CARGO, LEFT STA 1701 LONGERON 50 FOUND CRACKED. FABRICATED AS PER EA 1-5310-122601. INSTALLED AS PER SRM 53-10-00. FABRICATED AS PER DRAWING AFA7772. LONGERON REMOVED AND REPLACED AS PER SRM 53-10-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Oct 22, 2008 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 08FDEA04471Support Fitting · crackedDURING OPEN HOLE HFEC INSPECTION, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 8 O'CLOCK POSITION) AT HOLE NR D. CARRIED OUT REPAIR AS PER EA 1-5310-125561. THIS REPAIR CLASSIFIED AS MAJOR AOct 22, 2008 · N578FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA04470Support Fitting · crackedDURING OPEN HOLE HFEC INSPECTION, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 UPPER WEB FIRST LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 3 O'CLOCK POSITION) AT HOLE NR C. CARRIED OUT REPAIR AS PER EA 1-5310-125561. THIS REPAIR CLASSIFIED AS MAJOR AOct 22, 2008 · N578FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA04469Support Fitting · crackedDURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 REMOVED AND REPLACED AS PER SRM 51-31-Oct 22, 2008 · N578FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA04468Support Fitting · crackedDURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES NR A AND NR C. CARRIED OUT REPAIR AS PER SRM 53-50-00. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 22, 2008 · N578FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA04467Support Fitting · crackedDURING OPEN HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. CARRIED OUT REPAIR AS PER SRM 53-50-00. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2Oct 22, 2008 · N578FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA04466Fitting · crackedDURING OPEN HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLES NR A AND NR D. CARRIED OUT REPAIR AS PER SRM 53-50-00. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 22, 2008 · N578FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 07FDEA02110Longeron · damagedFUSELAGE, CAC COMPARTMENT AT STA 6-100, LONGERON 40L FOUND LONGERON WITH FREEZE PLUG INSTALLED. [06-19-07] REPAIR CARRIED OUT AT FUSELAGE - CAC COMPARTMENT AT STA 6-100, LONGERON 40L AS PER SRM 53 -10-00 FIGURE 2 VOLUME I.Jun 12, 2007 · N578FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 07FDEA02109Splice · damagedAFT CARGO RT L38, STA 1865 FOUND SPLICE DAMAGED. [06-18-07] REPAIR CARRIED OUT AS PER SRM 51-33-01 VOLUME II AND DRAWING AFA7105. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Jun 12, 2007 · N578FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 07FDEA02083Skin · misrepairedAPPROXIMATELY AT STA 6-100, LONGERON 43L FOUND EXISTING REPAIR. EXISTING REPAIR AT STA 6-100, LONGERON 43L EVALUATED AND FOUND NOT CARRIED OUT AS PER SRM 53-20-00 FIG 2 VOL I. REPAIR CARRIED OUT AS PER FEDEX EA 1-5330-112421A - FUSELAGE, PLATES AND SKIN, EJun 7, 2007 · N578FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 07FDEA02082Skin · misrepairedAPPROXIMATELY AT STA 6-100, LONGERON 40L FOUND EXISTING REPAIR. EXISTING REPAIR AT STA 6-100, LONGERON 40L EVALUATED AND FOUND NOT CARRIED OUT AS PER SRM 53-20-00 FIG 2 VOL I. REPAIR CARRIED OUT AS PER FEDEX EA 1-5330-112421A - FUSELAGE, PLATES AND SKINS, Jun 7, 2007 · N578FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 07FDEA02080Seat Track · noneEXISTING REPAIR, REF EA NR 1-5310-85955, TITLE: FUSELAGE, MAINFRAME, SEAT TRACK SPLICE REPAIRS Y=1781, X=27.50, 47.5 AND -27.5. EXISTING REPAIR EVALUATED AND FOUND ACCOMPLISHED AS PER FEDEX EA NR 1-5310-85955, TITLE: "FUSELAGE - MAIN FRAME, SEAT TRACK SPLICE Jun 7, 2007 · N578FE · Doug MD11F · Fuselage Main, StructureSDR 07FDEA02079Skin · noneAPPROXIMATELY BETWEEN STA 790-808, LONGERON 4L-5L FOUND EXISTING REPAIR. REPAIR CARRIED OUT AT APPROXIMATELY BETWEEN STA 790-808, LONGERON 4L-5L AS PER 53-20-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. THIS SDR SUBMITTED IN ERROR- AJun 7, 2007 · N578FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 07FDEA02084Floorbeam · noneEXISTING REPAIR, FUSELAGE STA 6-50 FLOORBEAM REPAIR AT RT BUTT LINE 60", AS SEEN FROM THE FWD LOWER CARGO COMPARTMENT, REPAIR REQUIRES EVALUATION. EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-00-01 FIGURE 8 VOLUME I. REPAIR CLASSIJun 7, 2007 · N578FE · Doug MD11 · Fuselage Main, Floor BeamSDR 07FDEA02086Plate · damagedCENTER CARGO STA 1841 STEP FORWARD WALL FOUND PLATE DAMAGED. [06-18-07] REPAIR CARRIED OUT AS PER SRM 53- 00-01 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Jun 7, 2007 · N578FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 07FDEA02081Skin · corrodedRT EXTERIOR SKIN UNDERNEATH BODY FAIRING AREA FOUND CORROSION AT SEVERAL PLACES FROM STA 1941-2164. [06-18-07] REPAIR CARRIED OUT AS PER SRM 53-20-00 FIGURE 13 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 7, 2007 · N578FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 07FDEA02069Skin · noneEXISTING REPAIR, RT WING I/B FLAP UPPER SURFACE FOUND EXISTING PATCH AT XIFH 283, YIFH 30. EXISTING REPAIR AT RT WING I/B FLAP UPPER SURFACE XIFH 283, YIFH 30, EVALUATED AND FOUND ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MAJOJun 4, 2007 · N578FE · Doug MD11F · Wing Main, Frame StructureSDR 07FDEA02067Skin · noneEXISTING REPAIR, RT WING I/B FLAP UPPER SURFACE FOUND EXISTING PATCH AT XIFH 168, YIFH 64. EXISTING REPAIR AT RT WING I/B FLAP UPPER SURFACE XIFH 168, YIFH 64, EVALUATED AND FOUND ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MAJOJun 4, 2007 · N578FE · Doug MD11F · Wing Main, Frame StructureSDR 07FDEA02066Skin · noneEXISTING REPAIR, RT WING I/B FLAP UPPER SURFACE FOUND EXISTING PATCH AT XIFH 157 YIFH 64. EXISTING REPAIR AT RT WING I/B FLAP UPPER SURFACE XIFH 157, YIFH 64, EVALUATED AND FOUND ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MAJORJun 4, 2007 · N578FE · Doug MD11F · Wing Main, Frame StructureSDR 07FDEA02064Skin · noneEXISTING REPAIR, LT WING I/B FLAP UPPER SURFACE FOUND WITH EXTERNAL PATCH AT XIFH 216 YIFH 70. EXISTING REPAIR AT LT WING I/B FLAP UPPER SURFACE XIFH 216, YIFH 70, EVALUATED AND FOUND ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS Jun 4, 2007 · N578FE · Doug MD11F · Wing Main, Frame StructureSDR 07FDEA02063Skin · noneEXISTING REPAIR, CTR CARGO, AFT DOOR JAMB EXTERIOR FOUND EDGE PATCH. EXISTING REPAIR AT CTR CARGO, AFT DOOR JAMB EXTERIOR EDGE PATCH EVALUATED AND FOUND ACCOMPLISHED AS PER SRM 53-50-00 FIGURE 17 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. THISJun 4, 2007 · N578FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 07FDEA02070Frame · noneEXISTING REPAIR, UPPER CARGO COMPARTMENT, LT SIDEWALL STRUCTURE FRAME AT STA 1701, L-12L, FOUND WITH REPAIR DOUBLER. EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-Jun 4, 2007 · N578FE · Doug MD11 · Fuselage Main, FrameSDR 07FDEA02068Skin · damagedEXISTING REPAIR, RT WING I/B FLAP UPPER SURFACE FOUND EXISTING PATCH AT XIFH 217 YIFH 65. EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 4, 2007 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA02065Skin · damagedEXISTING REPAIR, LT WING I/B FLAP UPPER SURFACE FOUND WITH EXTERNAL PATCH AT XIFH 233 YIFH 17. EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 4, 2007 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA02054Spar Cap · corrodedRIGHT WING, TRAILING EDGE REAR SPAR UPPER CAP FOUND CORRODED AT XORS 1038. [06-18-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-109902. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 4, 2007 · N578FE · Doug MD11F · Wing SparSDR 07FDEA02039Skin · damagedEXISTING REPAIR, DOUBLER PATCH FOUND ON LT WING L/E AT XIS247. REPAIR CARRIED OUT AT DOUBLER PATCH ON LT WING L/E AT XIS247 AS PER FEDEX EA NR 1- 5710-112420, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Jun 1, 2007 · N578FE · Doug MD11F · Wing Main, Frame StructureSDR 07FDEA02038Spar Cap · corrodedRIGHT WING, TRAILING EDGE REAR SPAR LOWER CAP FOUND CORROSION AT XORS 1054. [06-18-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-109898. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.May 31, 2007 · N578FE · Doug MD11 · Wing SparSDR 07FDEA02037Spar Cap · corrodedRIGHT WING, TRAILING EDGE REAR SPAR LOWER CAP FOUND CORROSION AT XORS 1067. [06-19-07]May 31, 2007 · N578FE · Doug MD11 · Wing SparSDR 07FDEA02036Hinge · corrodedRIGHT WING, O/B FLAP O/B HINGE AFT FAIRING AFT STRUT FWD BOLT HOLE FOUND CORROSION. [06-18-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-109897. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.May 31, 2007 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA02035Seat Track · corrodedUPPER CARGO COMPARTMENT, SEAT TRACK RBL 75 CORRODED AT STA 1301 TO STA 1361. [06-18-07] REPAIR CARRIED OUT AT UPPER CARGO COMPARTMENT, SEAT TRACK RBL 75, STA 1267 TO STA 1391 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER May 31, 2007 · N578FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02034Skin · crackedLEFT WING, NR 1 LEADING EDGE SLAT I/B EDGE FOUND CRACK NEAR ALIGNMENT PIN HOLE. REPAIR CARRIED OUT PER FEDEX EA 1-5710-109891. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.May 31, 2007 · N578FE · Doug MD11 · Leading Edge DevicesSDR 07FDEA01992Stringer · crackedCTR CARGO: UNDER FLOOR STA 1821, RT X=56 FOUND STRINGER JOINT END CRACKED. [06-19-07] REPAIR CARRIED OUT AT CTR CARGO: UNDER FLOOR STA 1821, STRINGER S43R JOINT END AS PER SRM 51-33-01 VOLUME II.May 29, 2007 · N578FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 07FDEA01991Hinge Fitting · crackedRIGHT WING, O/B FLAP I/B HINGE FITTING FOUND CRACK AT STA XOF 556. [06-18-07] RIGHT WING - O/B FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATIONAL TEST CARRIED OUT AS PER AMM 27-50-00-5, FOUND SATIS.May 28, 2007 · N578FE · Doug MD11F · Trailing Edge FlapsSDR 05FDEA04427Angle · damagedDURING ACCOMPLISHMENT OF LEFT LOWER AUXILIARY TANK CAP ANGLE. REPAIR FOUND 1 FASTENER HOLE ELONGATED. REPAIR CARRIED OUT AT ONE (01) EACH FASTENER WITH ELONGATED HOLE AT LEFT LOWER AUXILIARY TANK CAP ANGLE AS PER FEDEX EA NR 1-5310-90694, TITLE: "FUSELAGE Dec 31, 2005 · N578FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA04316Web · puncturedCENTER CARGO LEFT HAND STATION 1841 X= 40 AFT WEB FOUND PUNCTURED. WEB REMOVED AND REPLACED WITH NEW FABRICATED WEB AS PER DRAWING AGA7170 AND INSTALLED AS PER SRM 51-31-01 VOLUME II.Dec 15, 2005 · N578FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA04297Longeron · corrodedCENTER CARGO STATION 5-123 TO STATION 1541 LONGERON 48 RIGHT FOUND CORRODED. CTR CARGO COMPARTMENT STATION 5-123 TO STATION 1541 LONGERON 48 RIGHT, REPAIR CARRIED OUT AS PER SRM 53-10-00 FIG 2 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Dec 14, 2005 · N578FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 05FDEA04296Longeron · corrodedCENTER CARGO COMPARTMENT STATION 1561 TO STA 1581 LONGERON 48 LEFT HAND FOUND CORRODED. CTR CARGO COMPARTMENT STATION 1561 TO STA 1581 LONGERON 48 LT REPAIR CARRIED OUT AS PER SRM 53-10-00 FIG 2 VOL I . REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Dec 14, 2005 · N578FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 05FDEA04213Fitting · corrodedUPON REMOVAL OF CLG SHOCK STRUT ASSY FOUND LT TRUNNION SUPPORT FITTING FWD MOUNTING HOLE, SHEAR PIN HOLE & AFT MOUNTING HOLE WITH CORROSION. LT TRUNNION SUPPORT FITTING FORWARD MOUNTING HOLE, SHEAR PIN HOLE, AND AFT MOUNTING HOLE CORROSION REMOVED AND REPAIR Dec 9, 2005 · N578FE · Doug MD11 · Fuselage, Landing Gear Attach Fittings
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