N529FE

Service difficulty reports · 240

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 = 'N529FE' 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 FDEA201111235011Fitting · looseVERTICAL STABILIZER RT SIDE BANJO FITTING AFT SIDE FOUND LOOSE. R & R FASTENER IAW EA 1-5530-154251, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 23, 2011 · N529FE · Doug MD11F · Vertical Stabilizer, Attach FittingsSDR FDEA201111235005Seat Track · corrodedCORROSION ON SEAT TRACK CROWN AND CHANNEL AT BS 1059 -1079 X=-8. REPAIRED IAW SRM 53-00-52, FIG 201, REVISION 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 23, 2011 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201103311256Pump · leakingTOTAL LOSS OF NR 2 HYD. FOUND UPPER RUDDER NON REV PUMP SHUTOFF VALVE LEAKING. REPLACED VALVE . REPLACED BOTH NR 2 ENG DRIVEN PUMP CASE DRAIN FILTERS. NO CONTMINATION NOTED. FOUND FLUID IN NR2 RESERVIOR AND BOTH CASE DRAIN FILTERS. RAN NR 2 ENG HYD PUMPSMar 31, 2011 · N529FE · Doug MD11F · Hydraulic Pump (Electric/Engine), MainSDR FDEA201002090377Access Door · missingON POST FLT WALKAROUND FOUND ACCESS DOOR MISSING FROM LT WING INBD T/E FAIRING, DOOR IS 541CL AND IS SHOWN ON MM 06-35-00-0, FIG 12/SHEET 1. REPLACED ACCESS DOOR MISSING FROM LT WING INBD T/E FAIRING IAW SRM 51-00-00.Feb 9, 2010 · N529FE · Doug MD11F · DoorsSDR FDEA200911244139Skin · corrodedCABIN - RT STA 1210, XCW = -107 CTR WING UPPER PANEL FOUND CORROSION. REPAIRED IAW EA NR 1-5710-135667, THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REVISION 108.Nov 24, 2009 · N529FE · Doug MD11F · Wing, Center BoxSDR FDEA200911244138Skin · corrodedCABIN - RT STA 1229, XCW = -105 CTR WING UPPER PANEL FOUND CORROSION. REPAIRED IAW EA NR 1-5710-135667, THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 108.Nov 24, 2009 · N529FE · Doug MD11F · Wing, Center BoxSDR FDEA200911244137Frame · chafedCABIN - LT STA 1741 BETWEEN LONGERON 11 LT AND LONGERON 12 LT FOUND CHAFED. REPAIRED IAW SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 42. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT AS IAW SRM 5Nov 24, 2009 · N529FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200903291096Engine · power lossENG NR 3 FLAMED OUT IN FLIGHT. FL 320. LOUD BANG & SHUDDER WITH HIGH EGT INDICATION. DUMPED 59K LBS OF FUEL. LOUD COMPRESSOR STALL SOUND AND LOOKS LIKE EGT WENT TO 680 DEG C. ENGINE APPEARED TO ROLL BACK. HE CONSIDERED A RESTART BUT HIGH EGT PROMPTED SHUTDOWMar 29, 2009 · N529FE · Doug MD11F · Engine (Turbine/Turboprop)SDR 08FDEA02011Skin · crackedRT WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT CUT-OUT TOP INBOARD AND OUTBOARD CORNER FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.May 28, 2008 · N529FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA02010Frame · dentedAFT CABIN AT APPROXIMATELY STATION 1721 LEFT SIDE LONGERON 12 LEFT FOUND FRAME DENTED. CARRIED OUT REPAIR AS PER SRM 53-30-00, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.May 28, 2008 · N529FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA02009Frame · dentedAFT CABIN AT APPROXIMATELY STATION 1761 LEFT SIDE LONGERON 12 LEFT FOUND FRAME DENTED. BS 1761 LT LONGERON 12 LT FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00, FIG.1, VOL.I. DUE TO CAT B REPAIR, INITIAL INSPECTION TO BE CARRIED OUT AT 14,500 CYCLE, WITH REPETMay 28, 2008 · N529FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA02008Frame · dentedAFT CABIN AT APPROXIMATELY STATION 1701 RIGHT SIDE LONGERON 12 RIGHT TO LONGERON 13 RIGHT FOUND FRAME DENTED. AFT BS 1701 FRAME RT LONGERON 12 TO 13 RT CARRIED OUT REPAIR AS PER SRM 53-30-00, FIG.1, VOL.I. DUE TO CAT B REPAIR, INITIAL INSPECTION TO BE CARRMay 28, 2008 · N529FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA02007Doubler · crackedLEFT WING, LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACKED. REMOVED CRACKED RIB DOUBLER AS PER SRM 51-31-01, VOL. II. FABRICATED NEW RIB DOUBLER AS PER DRAWING ARB3954. INSTALLED NEW RIB DOUBLER AT LT WING LEADING EDGE AT XOS 667 AS PER SRM 51-33-01, VOMay 28, 2008 · N529FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA02006Skin · crackedLEFT WING ANTI-ICE TELESCOPIC DUCT DOOR CUT OUT CORNER FOUND CRACKED AT STATION XOS 464 AND XOS 470. REPAIR CARRIED OUT AS PER SRM 57-10-00, FIG.43, VOL.I AND EA 1-5710-122715, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.May 28, 2008 · N529FE · Doug MD11F · Wing, Plate/SkinSDR 07FDEA00356Skin · damagedDURING ACCOMPLISHING EO, NEW EXTERNAL SKIN (P/N ADA 7030Y1) FOUND WITH 2 MISDRILLED HOLES AND 11 EXTRA HOLES BEING TRANSFERRED AFTER TRANSFERRED HOLES FROM EXISTING EXTERNAL HOLES AT STA 853 TO STA 875, L-37R TO L-41R. REPAIR CARRIED OUT PER STEP 31 AND 32 OFFeb 7, 2007 · N529FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 07FDEA00344Hinge · corrodedCENTER CARGO DOOR HINGE ASSY FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.040" REMAINING THK 0.300". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLFeb 6, 2007 · N529FE · Doug MD11 · Fuselage, Door HingeSDR 07FDEA00343Hinge · corrodedCENTER CARGO DOOR HINGE AT FUSELAGE AREA FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10-00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.028" REMAINING THK 0.312". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02.Feb 6, 2007 · N529FE · Doug MD11 · Fuselage, Door HingeSDR 07FDEA00342Hinge · corrodedAFT CARGO DOOR HINGE AT FUSELAGE SIDE FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10-00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.020" REMAINING THK 0.320". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REFeb 6, 2007 · N529FE · Doug MD11 · Cargo/Baggage DoorsSDR 07FDEA00341Hinge · corrodedAFT CARGO DOOR HINGE ASSY FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG.14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.035" REMAINING THK 0.305". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFeb 6, 2007 · N529FE · Doug MD11 · Fuselage, Door HingeSDR 07FDEA00340Hinge · corrodedFWD CARGO DOOR HINGE FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG.14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.025" REMAINING THK 0.315". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFIED MAJOR Feb 6, 2007 · N529FE · Doug MD11 · Fuselage, Door HingeSDR 07FDEA00339Hinge · corrodedFWD CARGO DOOR HINGE AT FUSELAGE AREA FOUND WITH CORROSION. CORROSION ON FUSELAGE CARGO DOOR HINGE ASSY REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10-00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.021" REMAINING THK 0.319". HINGE REMOVED AND NFeb 5, 2007 · N529FE · Doug MD11 · Fuselage, Door HingeSDR 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 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 FittingsSDR 06FDEA04276Rib · crackedFOUND CENTER LANDING GEAR WHEEL WELL RT BULKHEAD FWD RIB CUTOUT SUSPECT CRACKED. CENTER LANDING GEAR WHEEL WELL R/H BULKHEAD FWD RIB CUTOUT REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.Dec 19, 2006 · N529FE · Doug MD11 · Fuselage Main, BulkheadSDR 06FDEA04275Rib · crackedCENTER LANDING GEAR WHEEL WELL LT BULKHEAD FWD RIB CUTOUT SUSPECT CRACKED. CRACKED RIB CUTOUT REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Dec 19, 2006 · N529FE · Doug MD11 · Fuselage Main, BulkheadSDR 06FDEA04274Seat Track · corrodedFWD CABIN SEAT TRACK RIGHT FLANGE AND CROWN UPPER SURFACE FOUND CORROSION AT STA 800-840, RBL 27.5. REMOVED AS PER SRM 51-31-01 VOL.II AT STA 745 TO STA 869 X=27.5 R/H. NEW SEAT TRACK FABRICATED AS PER DRAWING ADA 7321-519, FASTENER HOLES PICKED UP AS PERDec 19, 2006 · N529FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04273Hinge Bracket · corrodedRHW O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57- 44-08 PG. 612-615 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.441" O/B 0.425" REMAINING THK I/B 0.438 O/B 0.432" MATERIAL Dec 19, 2006 · N529FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA04272Hinge Bracket · corrodedRHW O/B FLAP I/B HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG 602-607 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.469" O/B 0.486" REMAINING THK I/B 0.460" O/B 0.481" MATERIAL REMODec 19, 2006 · N529FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA04271Hinge Bracket · corrodedLHW O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. LT FWD O/B FLAP O/B HINGE BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PG. 402-408 AND FOUND WITHIN DRAWING ARC 0503 LIMIT. ORIGINAL THK I/B 0.498" O/B 0.Dec 19, 2006 · N529FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA04270Hinge Bracket · corrodedLHW O/B FLAP O/B HINGE (WING SIDE), LOWER ATTACHMENT I/B BORE FOUND CORRODED. LT FWD O/B FLAP O/B HINGE LOWER MOUNT I/B BORE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG. 402-408. ORIGINAL THK 0.518" FINAL 0.591" MAXIMUM ALLOWABLE 0.584Dec 19, 2006 · N529FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA04268Hinge Bracket · corrodedLHW O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. LT FWD O/B FLAP I/B HINGE BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 PG. 612-615 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.445" O/B 0.Dec 18, 2006 · N529FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA04267Hinge Bracket · corrodedLHW O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. LT FWD O/B FLAP I/B HINGE LOWER MOUNT SPOTFACE CORROSION REMOVED AS PER CMM 57- 44-08 PG. 602-607 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.476" O/B 0.476" REMDec 18, 2006 · N529FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA04266Hinge Bracket · corrodedLHW O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57- 44-08 PG. 602-607 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.476" O/B 0.476" REMAINING THK I/B O.473" O/B 0.473" MATERIAL REMOVDec 18, 2006 · N529FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA04265Hinge Bracket · corrodedLHW O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57- 44-08 PG. 602-607 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.476" O/B 0.476" REMAINING THK I/B 0.473" O/B 0.473" MATERIAL REMOVDec 18, 2006 · N529FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA04264Hinge Bracket · corrodedLHW O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57- 44-08 PG. 602-607 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.476" O/B 0.476" REMAINING THK I/B 0.473" O/B 0.473" MATERIAL REMOVDec 18, 2006 · N529FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA04263Skin · dentedFWD CARGO DOOR CUTOUT AFT DOOR JAMB FX SKIN WITH DENT AT L-32R TO L-35R. DAMAGED AREA TRIMMED AS PER SRM 53-50-00 FIG.16 VOL.I. REPAIR DOUBLER FABRICATED AND INSTALLED AS PER 53-50-00 FIG.16 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Dec 18, 2006 · N529FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA04207Panel · corrodedHORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 02 CORROSION REWORK FOUND EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1. REPAIRED AS PER EA 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Dec 10, 2006 · N529FE · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR 06FDEA04206Skin · gougedCTR CARGO DOOR CUTOUT FUSELAGE SKIN ON AFT DOOR JAMB FOUND WITH SCRATCHES ON L-38R TO L-40R. SCRATCHES ON CENTER CARGO DOOR CUTOUT AFT JAMB OF FUSELAGE SKIN L38R TO L40R REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 16 VOL.I. REPAIR CLASSIFIED AS MAJOR PER Dec 10, 2006 · N529FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA04202Panel · corrodedHORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 19 CORROSION REWORK FOUND OUT OF LIMIT PER EO 1-5510-7-5000 D1 PT1. REPAIRED AS PER EA 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Dec 9, 2006 · N529FE · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR 06FDEA04201Frame · damagedLEFT FWD TAILCONE FRAME ALIGNMENT PIN HOLE (CTR POS) ELONGATED. DAMAGED FRAME AT L/H FWD TAILCONE REMOVED AS PER SRM 51-31-01 VOL.II. HOLES ON NEW FRAME PICKED-UP AS PER SRM 51-31-01 VOL.II AND DWG AKC 7520. NEW FRAME AT L/H FWD TAILCONE INSTALLED AS PEDec 9, 2006 · N529FE · Doug MD11 · Aerodynamic FairingsSDR 06FDEA04170Frame · crackedRT FWD TAILCONE FRAME ALIGNMENT PIN HOLE (CTR POS) FOUND WITH CRACK. REPAIRED AS PER SRM 53-00-01 FIG.9 VOL. I AND SRM 53-30-00 FIG.12 VOL.I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Dec 4, 2006 · N529FE · Doug MD11 · Aerodynamic FairingsSDR 06FDEA04169Tank · corrodedCABIN, UNDER FLOOR AREA, OVERWING TANK TOP SURFACE STA 1360 X=-75.0 (RT) FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 57-00-01 FIG.1A VOL.I. ORIGINAL THK 0.076" REMOVED 0.007" REMAINING THK 0.069" AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG.12 VODec 4, 2006 · N529FE · Doug MD11 · Fuselage Main, Structure
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