Mcdonnell Douglas MD-11

Service difficulty reports · 7,956

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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 aircraft_model_key = 'MD11'
  ORDER BY difficulty_date DESC"

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SDR 07FDEA00243Stringer · crackedCRACK FOUND (APPROX. 0.5" LONG) DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF UPPER STRINGER 43 (XORS 565). CRACK ON RIGHT HAND WING TANK AT THE END OF UPPER STRINGER 43 (XORS 565) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIEDFeb 2, 2007 · N624FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00242Stringer · crackedCRACK FOUND (APPROX 3.5" LONG) DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF UPPER STRINGER 10 (XORS 760). CRACK ON RIGHT HAND WING TANK AT THE END OF UPPER STRINGER 10 (XORS 760) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED Feb 2, 2007 · N624FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00241Stringer · crackedCRACK FOUND (APPROX 0.5" LONG) DURING HFEC INSPECTION ON LEFT WING TANK AT THE END OF UPPER STRINGER 37 (XORS 938). CRACK ON LEFT HAND WING TANK AT THE END OF UPPER STRINGER 37 (XORS 938) REPAIRED AS PER FEDEX E.A. 1-5720-105613, REPAIR CLASSIFIED AS MINOR PEFeb 2, 2007 · N624FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00240Stringer · crackedCRACK FOUND (APPROX 3" LONG) DURING HFEC INSPECTION ON LEFT WING TANK AT THE END OF UPPER STRINGER 12 (XORS 642). CRACK ON LEFT HAND WING TANK AT THE END OF UPPER STRINGER 12 (XORS 642) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MFeb 2, 2007 · N624FE · Doug MD11 · Wing, Longeron/StringerSDR UPS07M49237Doubler · crackedINSPECTION TYPE:C LEFT WING L/E LWR COMPT STA XORS 558 FOUND UPPER DOUBLER PANEL CRACKED AS MARKED. LEFT WING L/E LWR COMPT STA XORS 558 UPPER DOUBLER REMOVED PER SRM 51-31-01, V2R 2, R38. REPAIR DOUBLER FILLER ANGLES FAB & HOLES DRILLED PER SRM 57-10-00 -00Jan 23, 2007 · N258UP · Doug MD11 · Wing, Plate/SkinSDR 07FDEA00153Valve · failedON DEPARTURE WHEN WING ANTI-ICE SELECTED ON GOT WING ANTI-ICE DISAGREE AND MOMENTARILY MANIFOLD FAIL. PERFORMED QRH PROCEDURE, REMAINED CLEAR OF ICING CONDITION. WING DISAGREE INDICATION REMAINED. TROUBLE SHOT CARRIED OUT PRECAUTIONARY MEASURE DELTA P SENSOJan 23, 2007 · N582FE · Doug MD11 · Ice DetectionSDR WRLA2007015Battery Pack · dischargedNR 1 EMERGENCY LIGHT PWR SUPPLY HAS A LOW ALERT. REMOVED AND REPLACED BATTERY PACK PER MM 33-51-00. OPS NORMAL.Jan 21, 2007 · N801DE · Doug MD11 · Emergency LightingSDR 07FDEA00147Trunnion · corrodedCENTER LANDING GEAR LT TRUNNION FOUND CORROSION. CTR LANDING GEAR LT TRUNNION FITTING REMOVED & REPLACED AS PER DWG AEA7035 AND SRM 51-31- 01 VOL.II. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Jan 20, 2007 · N590FE · Doug MD11 · Emergency Flotation SectionSDR 07FDEA00146Trunnion · corrodedFOUND CENTER LANDING GEAR LT TRUNNION FWD HOLE FOUND CORROSION.Jan 20, 2007 · N590FE · Doug MD11 · Emergency Flotation SectionSDR 07FDEA00126Seat Track · corrodedM/D CARGO SEAT TRACK (STA 1520, LT, X=8.5) FOUND FLANGE UNDER FLOOR CORRODED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK (STA 1520, LT, X=8.5) AS PER SRM 53-70-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 16, 2007 · N590FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00101Seat Track · corrodedM/D CARGO SEAT TRACK (STA 5/0, LT, X=8.5) FOUND FLANGE UNDER FLOOR PANEL CORRODED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK (STA 5/0, LH, X=8.5) AS PER SRM 53-70-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 15, 2007 · N590FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00100Trunnion · corrodedCENTER LANDING GEAR RT TRUNNION AFT HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR RH TRUNNION AFT HOLE AS PER FEDEX EA 1-5340-105661, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 15, 2007 · N590FE · Doug MD11 · Emergency Flotation SectionSDR 07FDEA00099Structure · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE OUTBOARD CENTER HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107762, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 15, 2007 · N598FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA00098Structure · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE OUTBOARD AFT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5750-107762, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 15, 2007 · N598FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA00097Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE OUTBOARD AFT HOLE FOUND CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 15, 2007 · N598FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA00096Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE INBOARD AFT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 15, 2007 · N598FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA00095Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE INBOARD FORWARD HOLE FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 15, 2007 · N598FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA00094Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD AFT BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED AS PER CMM 57-52- 04. FLAP ADJUSTMENT REFER TO FEDEX EO 1-5720-7-5001 PT2, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 15, 2007 · N598FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA00093Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD CENTER BOLT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 15, 2007 · N598FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA00088Seat Track · damagedSEAT TRACK AT MAIN DECK CARGO AT STA 495-515 X=27.5 RT FOUND EDGE BROKEN OFF. REPAIR CARIED OUT AT MAIN DECK CARGO SEAT TRACK (STA 495-515 X=27.5 RT) AS PER SRM 53-70- 00 FIGURE 4 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 12, 2007 · N590FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00074Skin · crackedRIGHT WING TELESCOPIC DUCT CUTOUT FOUND CRACKED. CRACK AREA ON THE RIGHT WING TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57-10-00 FIGURE 42 VOLUME I AND FEDEX EA NR 1-5710-107767, TITLE: WINGS, RIGHT WING ANTI-ICING TELESCOPIC DUCT DOOR CUTOUT REPAIR. REPAIRJan 11, 2007 · N598FE · Doug MD11 · Wing, Plate/SkinSDR 07FDEA00077Support Fitting · crackedLEFT WING O/B FLAP ARC4012 OUTBOARD SUPPORT FITTING FOUND CRACK. LEFT HAND OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATIS AS PER AMM 27-50-00-5.Jan 11, 2007 · N590FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA00076Angle · crackedRT WING ROOT, CENTER TANK LOWER TEE ANGLE FOUND CRACKED AT STA 1298. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-105590. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 11, 2007 · N590FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 07FDEA00068Frame · dentedCABIN LEFT STA 1661 BETWEEN LONGERON 12 AND LONGERON 14 FRAME FOUND CRACKED. CABIN LEFT STA 1661 BETWEEN LONGERON 12 AND LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYJan 10, 2007 · N598FE · Doug MD11 · Fuselage Main, FrameSDR 07FDEA00067Frame · dentedCABIN, LEFT STA 1641 BETWEEN LONGERON 12 AND LONGERON 14 FRAME FOUND DENT. CABIN, LEFT STA 1641 BETWEEN LONGERON 12 AND LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CJan 10, 2007 · N598FE · Doug MD11 · Fuselage Main, FrameSDR 07FDEA00066Frame · dentedCABIN LEFT STA 1681 BETWEEN LONGERON 12 AND LONGERON 14 FRAME FOUND DENT. CABIN LEFT STA 1681 BETWEEN LONGERON 12 AND LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCJan 10, 2007 · N598FE · Doug MD11 · Fuselage Main, FrameSDR 07FDEA00065Frame · dentedCABIN RIGHT STA 1701 BETWEEN LONGERON 12 TO LONGERON 14 FRAME FOUND DENT. CABIN RIGHT STA 1701 BETWEEN LONGERON 12 TO LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCJan 10, 2007 · N598FE · Doug MD11 · Fuselage Main, FrameSDR 07FDEA00064Frame · dentedCABIN RIGHT STA 1681 BETWEEN LONGERON 12 TO LONGERON 14 FRAME FOUND DENT. CABIN, RIGHT STA 1681 BETWEEN LONGERON 12 TO LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYJan 10, 2007 · N598FE · Doug MD11 · Fuselage Main, FrameSDR 07FDEA00061Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER END-40 (XORS 747) INSIDE LT WING TANK. REPAIR CARRIED OUT AT STRINGER END-40 (XORS 747) INSIDE LT WING TANK AS PER FEDEX EA NR 1-5720-105598, TITLE: "WINGS-STRINGER 40 LEFT CRACK AT WING STATION XORS = 747 - REPJan 9, 2007 · N590FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00062Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER END-13R (XORS 577) INSIDE RT WING TANK. REPAIR CARRIED OUT AT STRINGER END-13 (XORS 577) INSIDE RT WING TANK AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 9, 2007 · N590FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00060Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER END-11 (XORS 704) INSIDE LT WING TANK. REPAIR CARRIED OUT AT STRINGER END-11 (XORS 704) INSIDE LT WING TANK AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 9, 2007 · N590FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00056Structure · crackedLANDING GEAR: LT LDG AT FLIPPER DOOR FWD SIDE FOUND CRACKED. LANDING GEAR, LT LDG AT FLIPPER DOOR FWD SIDE REPAIRED AS PER SRM 52-10-00 VOLUME I, FIGURE 18. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 9, 2007 · N579FE · Doug MD11 · Main Landing GearSDR 07FDEA00063Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER END-14R (XORS 521) INSIDE RT WING TANK. REPAIR CARRIED OUT AT STRINGER END-14R (XORS 521) INSIDE RT WING TANK AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 9, 2007 · N590FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00059Stringer · crackedDURING HFEC INSPECTION, CRACK FOUND AT STRINGER END 14R (XORS 685) INSIDE RT WING TANK. REPAIR CARRIED OUT AT STRINGER END-41R (XORS 685) INSIDE RT WING TANK AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 9, 2007 · N590FE · Doug MD11 · Wing, Longeron/StringerSDR WRLA2007003Oven · smokeMID GALLEY OVEN NR 2 STOPPED WORKING, C/B PULLED. ELECTRICAL SMOKE WAS SENSED ON LEFT SIDE OF VENT, NO SMOKE WAS EVIDENT ALTHOUGH SMELL WAS NOTICEABLE. OPS CHECKED MID OVENS, NO SIGN OF ELECTRICAL SMOKE OR ODOR. COOKED WITH MID GALLEY OVENS FOR MEAL SERVICEJan 8, 2007 · N801DE · Doug MD11 · Buffet/GalleysSDR WRLA2007002Unknown · smokeTO+15 MIN SMOKE & FUMES IN COCKPIT, UNKNOWN SOURCE. COCKPIT DOOR POWER & RECIRC FANS TURNED OFF. SMOKE DISSIPATED SOME. RETURN TO ORIGIN. CHECKED RECIRC FANS, ALL CHECKED GOOD, CHECKED MUX SYSTEM OPS CHECK GOOD. CHECKED WIRING IN OVERHEAD, FOUND NO PROBLEJan 8, 2007 · N277WA · Doug MD11 · Air Distribution SystemSDR 07FDEA00017Skin · corrodedRIGHT WING UPPER SURFACE CORROSION AT XORS 1011. COMPLIED WITH FEDEX E.A.# 1-5710-105601, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 3, 2007 · N579FE · Doug MD11 · Wing, Plate/SkinSDR 07FDEA00006Skin · dentedLT HORIZONTAL STAB LEADING EDGE O/B SECTION NR 331FT FOUND WITH DENT ON O/B EDGE. FOUND OUT OF LIMIT AS PER SRM 55-00-01 VOL. I. DEPTH= 0.080", WIDTH= 2". REPAIR CARRIED OUT AS PER SRM 55-20-00 FIG. 5 VOL. I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Jan 1, 2007 · N529FE · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR 06FDEA04316Frame · crackedDURING PROGRESSION OF REPAIR PER EO 1-5100-7-50001A PT.1 FOUND FRAME CRACKED AT RIGHT I/B NR 1 SLAT AT STA XIS 185.453. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL.II AND SRM 51-33-01 VOL.II. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Dec 26, 2006 · N529FE · Doug MD11 · Leading Edge DevicesSDR 06FDEA04315Skin · damagedDURING FUSELAGE SKIN REPLACEMENT PER EA 1-5330-104764 PT.1 FOUND 01 HOLE SIZE 1/4 AT STA 979 LONGERON 48R, ORIGINAL SIZE 3/16. DIAMETER HOLE ON NEW SKIN PICKED-UP AND 01 EA. FASTENER ON NEW SKIN INSTALLED AS PER SRM 51-35-01 VOL.II. REPAIR CLASSIFIED MAJORDec 26, 2006 · N529FE · Doug MD11 · Fuselage Main, Plate/SkinSDR UPS07M48929Doubler · corrodedINSPECTION TYPE:C CTR CARGO BILGE STA 1664-1677 BETWEEN LONG 52 & 51R, ANTENNA DOUBLERS CORROSION. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL II REV 38. MAT'L REMOVED 0.006 INCH ORG THK 0.063 INCH THK REMAINING 0.057 INCH FOUND WITHIN LIMITDec 20, 2006 · N257UP · Doug MD11 · Fuselage Main, Plate/SkinSDR UPS07M48928Frame · corrodedINSPECTION TYPE:C AFT WASTE TANK BILGE FRAME STA 1978 BETWEEN LONG 48R & 48L AFT SIDE CORROSION. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL I REV 38 MAT'L REMOVED 0.006 INCH THK REMAINING 0.057 INCH ORG THK 0.063 INCH FOUND WITHIN LIMIT AS PER Dec 20, 2006 · N257UP · Doug MD11 · Fuselage Main, FrameSDR 06FDEA04294Support Fitting · crackedCRACK INDICATION FOUND ON SECOND HOLE FROM OUTBOARD ON ARC4009 SUPPORT FITTING LOWER FASTENER HOLE AT 3 O'CLOCK POSITION (LOOKING FWD). RT OUTBOARD FLAP ASSEMBLY REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & OPERATION TEST CARRIED OUT FOUND SATIS ASDec 20, 2006 · N631FE · Doug MD11 · Wing, Attach FittingsSDR 06FDEA04283Hinge Bracket · corrodedLHW I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER E.A.1-5750-106569. ORIGINAL 1.300" FINAL 1.328" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PER E.A. 1-575Dec 19, 2006 · N529FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA04282Hinge Bracket · corrodedLHW I/B FLAP O/B HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. LT FWD I/B FLAP O/B HINGE PIVOT HOLE SPOTFACE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-07 PG. 403-404. ORIGINAL THK I/B 0.491" O/B 0.443" REMAINING THK I/B 0.489" Dec 19, 2006 · N529FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA04281Hinge Bracket · corrodedRHW I/B FLAP O/B HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER E.A. 1-5750-106574 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Dec 19, 2006 · N529FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA04280Hinge Bracket · corrodedRHW O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION HAND CLEANED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04 PG. 621-622. ORIGINAL THK 1.151" FINAL 1.151" MAX. ALLOWABLE THK 1.150". BUSHING FABRICATED AND INSTALLEDDec 19, 2006 · N529FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA04279Hinge Bracket · corrodedRHW I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. RT AFT I/B FLAP O/B HINGE PIVOT I/B BORE CORROSION HAND CLEANED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG. 442-444. ORIGINAL THK 1.2555" FINAL 1.2555" MAXIMIUM ALLOWABLEDec 19, 2006 · N529FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA04278Hinge Bracket · corrodedRT WING I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION HAND CLEANED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG. 442-444. ORIGINAL 1.2555" FINAL 1.2555" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PDec 19, 2006 · N529FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA04277Hinge Bracket · corrodedFOUND RHW O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57- 44-09 PG. 402-408 AND FOUND WITHIN DAC DWG ARC 0503 LIMIT. ORIGINAL THK I/B 0.484" O/B 0.484" REMAINING THK I/B 0.481" O/B 0.481" MADec 19, 2006 · N529FE · Doug MD11 · Wing, Control Surface Attach Fittings
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