N597FE

Service difficulty reports · 406

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 = 'N597FE' 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 FDEA201910042436Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52Oct 4, 2019 · N597FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201910042435Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-Oct 4, 2019 · N597FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201910042434Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-Oct 4, 2019 · N597FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201910042433Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMMOct 4, 2019 · N597FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201910032430Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TOE EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PAROct 3, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910032429Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, Oct 3, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910032428Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, Oct 3, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910032427Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349923, PART 1, STEP 3B, AND INSTALLED IAW COct 3, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910032426Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349923, PART 1, STEP 3B, AND INSTALLED IAW CMM Oct 3, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910032425Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT BORE FOUND CORRODED. WORKED THE CORROSION AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, PART 1, STEP 3A, AND Oct 3, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910032424Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG BORE WAS FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T034988Oct 3, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910032423Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349887, PARTOct 3, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910032422Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT, OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349887, PART 1, STEP 3B, AND INSTALLED Oct 3, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910032421Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT, INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349887, PART 1, STEP 3B, AND INSTALLED IAW CMOct 3, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910032420Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT, INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349887, PARTOct 3, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2019100322399Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750- T0349884, PART 1, STEP 3A, AND INSTALLED IAW CMM 57Oct 2, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2019100312389Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE LOWER MOUNT, OUTBOARD BORE WAS FOUND CORRODED. THE CORROSION WAS WORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349884, PART 1, STEP 3A, AND INSTALLOct 1, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2019100312388Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE LOWER MOUNT, INBOARD BORE SURFACE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PAROct 1, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910012387Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE BRACKET, INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, POct 1, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2019100312386Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE BRACKET, OUTBOARD LUG BORE WAS FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, POct 1, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2019100312385Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE FITTING OTBD LUG BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PART 1, STEP 3C, Oct 1, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2019100312384Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE ACTUATOR, INBOARD LUG BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PART 1, STEPOct 1, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2019100312383Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 AND EA 1-5750- T0349824, PART 1, STEP 3,Oct 1, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2019100312382Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED IAW CMM 57- 44-09 AND EA 1-5750-T0349824, PART 1, STOct 1, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2019100312381Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORRODED. WORKED THE CORROSION AND FOUND EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 AND EA 1-5750-T0349824, PART 1, STEP 3B, AND SOct 1, 2019 · N597FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201908302045Sensor · malfunctionedAFTER LANDING, RECEIVED A BRAKE DIFF TEMP LVL 1 MESSAGE. BRAKE TEMP ON NR 8 WAS ABOUT 200 COOLER THAN ALL OTHER TEMPS. REMOVED AND REPLACED THE NR 8 BRAKE TEMP SENSOR IAW MM 32-46-01-4. PERFORMED A TEST OF THE BRAKE TEMPERATURE MONITOR AND TIRE PRESSURE INAug 30, 2019 · N597FE · Doug MD11F · Landing Gear Brake SystemSDR FDEA2018120653434Sensor · malfunctionedCRUZ FLT FL320.LEVEL THREE ALERT "AIR MANF #2 FAIL. QRH COMPLIED WITH,AIR SYSTEM REMAINED IN AUTO. AIR SYSTEM #2 27PSI #2 BLEED VALVE OPEN PER TECH PILOT CYCLED "PNEUM PRESS REG VLV ENG #2. PRV CYCLED #2 PNEUMATIC SYST PRESSURE LESS THAN 10PSI, LANDED NDec 5, 2018 · N597FE · Doug MD11F · Pneumatic Indicating SystemSDR FDEA2018082982271Truck · failedON TAXI OUT PVD FELT UNUSUAL VIBRATION WHILE TAXIING. WE SUSPECTED A FLAT TIRE ON THE RIGHT MAIN TRUCK. REMOVED AND REPLACED LT MLG TRUCK ASSEMBLY PER AMM 32-12-20-4.Aug 28, 2018 · N597FE · Doug MD11F · Main Landing Gear Strut/Axle/TruckSDR FDEA201806081440Slat Track · crackedNR 12 RT SLAT TRACK (MOST O/B ON THE NR 5 SLAT) APPEARS TO BE CRACKED FROM L/E OF CUT OUT THROUGH 2 FASTENERS GOING AFT. INSTALLED REPAIR IN REF TO SRM 57-40-02-2R AND PRIMED AND PAINTED REPAIR IN REF TO SRM 51-21-01.Jun 8, 2018 · N597FE · Doug MD11F · Leading Edge DevicesSDR FDEA201803140686Sensor · failedBRAKE DIFF TEMP, LEVEL ONE ALERT CAME ON DURING CLIMB, TIRE NR 8 WHILE READING QRH IT BECAME A LEVEL TWO BRAKE OVERHEAT WITH A TEMP OF 640 DEGREES AT FL 370. DESCENDED TO FL240, SLOWED AND LOWERED THE GEAR IAW QRH. THE TEMP BEGAN TO DECREASE, BUT THE INMar 14, 2018 · N597FE · Doug MD11F · Landing Gear Brake SystemSDR FDEA201802200442Warning System · activatedLVL 2 ANTI SKID L FAIL ON APPROACH, COMPLIED WITH QRH. ANTI-SKID CONTROL VALVE INOP. SYSTEM 1 BRAKE 6 DISABLED. ENSURE PENALIES ARE APPLIED. COMPLIED WITH "M" PROCEDURE. BRAKE INOP KIT INSTALLED ON NR 6 BRAKE.Feb 20, 2018 · N597FE · Doug MD11F · Brake Anti-Skid SectionSDR FDEA201709192616Doubler · crackedLEFT WING FIXED LEADING EDGE LOWER DOUBLER AT XOS 555 FOUND CRACKED. THE DOUBLER WAS REMOVED IAW SRM 51-31-01-0G, AND FABRICATED A NEW DOUBLER IAW DRAWING ARB 2933, REVISION AJ, AND INSTALLED IAW SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6Sep 19, 2017 · N597FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201709182590Seat Track · damagedMAIN DECK CARGO SEAT TRACK CROWN AREA DAMAGED AT STA 5-5, RBL 8.5. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 18, 2017 · N597FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201709172587Intercostal · crackedEMPENNAGE VERTICAL STAB, UPON REMOVAL FOR ACCESS RT CENTER REAR SPAR TO REAR SPAR INTERCOSTAL AT BS 2164 FOUND CRACKED. REPAIRED AS PER EA 1-5530-T0335514, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 17, 2017 · N597FE · Doug MD11F · Vertical Stabilizer Miscellaneous StructureSDR FDEA201709172586Doubler · crackedRIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 789 FOUND CRACKED. DOUBLER REMOVED IAW SRM 51-31-01-0G, AND FABRICATED A NEW DOUBLER IAW DRAWING ARB3954, REVISION K. INSTALLED THE DOUBLER IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 17, 2017 · N597FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201709172585Rib · crackedDURING BORESCOPE INSPECTION, FOUND THE RT WING NR 8 SLAT INNER RIB, XOS 1092 CRACKED. A NEW RIB WAS FABRICATED IAW DRAWING ARB1928 REVISION G. REMOVED AND REPLACED THE RIB IAW SRM 51-35-01-0G, AND EA 1-5750-T0335496, PART 1. THE REPAIR WAS CLASSIFIED AS MSep 17, 2017 · N597FE · Doug MD11F · Leading Edge DevicesSDR FDEA201709152569Skin · crackedDURING HFEC OPEN HOLE INSPECTION ON THE RIGHT WING FUEL TANK LOWER ACCESS PANEL 636AB, FOUND THREE FASTENER HOLES 10, 28 AND 34 CRACKED. REPAIRED IAW SRM 57-20-02-2R, FIGURE 201, REPAIR 5. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 15, 2017 · N597FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201709152568Rib · crackedLEFT WING NR 3 SLAT INNER RIB AT XOS 435.446 FOUND CRACKED. REPAIRED THE RIB IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 7, AND EA 1-5750-T0335618, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 15, 2017 · N597FE · Doug MD11F · Leading Edge DevicesSDR FDEA201709152567Skin · dentedLEFT WING NR 3 SLAT FOUND DENTED AT XOS 435.446. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 11, AND EA 1-5750-T0335618, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 15, 2017 · N597FE · Doug MD11F · Leading Edge DevicesSDR FDEA201709142556Doubler · crackedRIGHT WING FIXED LEADING EDGE LOWER DOUBLER AT XOS 546, FOUND CRACKED. THE DOUBLER WAS REMOVED IAW SRM 51-31-01-0G, FABRICATED A NEW DOUBLER IAW DRAWING ARB 2933, REVISION AJ, AND INSTALLED IAW SRM 51-35-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6Sep 14, 2017 · N597FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201709142555Frame · chafedMAIN DECK CARGO, FRAME WITH AN EXISTING REPAIR FOUND CHAFED AT BS 535, LONGERON 24L. THE REPAIR ANGLE WAS REMOVED IAW SRM 51-33-01-0G. A NEW REPAIR ANGLE WAS FABRICATED IAW SRM 53- 20-07-2R, FIGURE 201, REPAIR 1, AND INSTALLED IAW SRM 53-20-07-2R, FIGURE 2Sep 14, 2017 · N597FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201709142554Frame · chafedMAIN DECK CARGO, FRAME WITH AN EXISTING REPAIR FOUND CHAFED AT BS 535, LONGERON 19L. REMOVED THE REPAIR IAW SRM 51-33-01-0G. A NEW OUTER REPAIR ANGLE, FABRICATED IAW SRM 53-20-07-2R, FIGURE 202, REPAIR 1. THE NEW REPAIR ANGLE WAS INSTALLED IAW SRM 53-20-07Sep 14, 2017 · N597FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201709142553Doubler · crackedLEFT WING FIXED LEADING EDGE LOWER DOUBLER AT XOS 907 FOUND CRACKED. REPAIRED THE LEADING EDGE LOWER AREA IAW SRM 57-40-03-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 14, 2017 · N597FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201709142552Fitting · crackedDURING HFEC INSPECTION AT RT FWD FLANGE LOCATED AT THE UPPER SECTION REAR SPAR CAP OF THE NR 4 BANJO FITTING OF THE VERTICAL STABILIZER, Y=2164 A CRACK WAS FOUND APPROXIMATELY 0.25 INCH LENGTH. REPAIRED IAW EA 1-5530-T0335558, PART 1. THE REPAIR WAS CLASSISep 14, 2017 · N597FE · Doug MD11F · Vertical Stabilizer Miscellaneous StructureSDR FDEA201709132532Frame · dentedMAIN DECK CARGO FRAME DENTED AT BS 1721, LONGERON 12L. REPAIRED THE FRAME IAW SRM 53-00-07-2R, FIGURE 201, REPAIR 2.Sep 13, 2017 · N597FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201709132531Seat Track · crackedMAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 635, LBL 27.5. REPLACED THE SEAT TRACK FROM BS 625 TO 665, LBL 27.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 13, 2017 · N597FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201709132530Seat Track · crackedMAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 635, LBL 47. REPLACED THE SEAT TRACK FROM BS 625 TO 665 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 13, 2017 · N597FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201709132529Cargo Track · crackedMAIN DECK CARGO TRACK FOUND CRACKED AT BS 755, LBL 49. REPLACED THE CARGO TRACK IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 13, 2017 · N597FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201709132528Seat Track · crackedMAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 695, RBL 27.5. REPLACED THE SEAT TRACK FROM BS 665 TO 705 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 13, 2017 · N597FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201709132527Seat Track · crackedMAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 695, RBL 8.5. REPLACED THE SEAT TRACK FROM BS 625 TO 705, IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 13, 2017 · N597FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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