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 05FDEA02719Skin · chafedLOWER FUSELAGE, FORWARD CARGO DOOR CUT-OUT AFT LOWER SIDE BETWEEN LONGERON 40R AND 41R, FOUND CHAFED SKIN = ABA7030-1. CARRIED OUT REPAIR AS PER SRM 53-50-00.Aug 30, 2005 · N597FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 04FDEA01641Pseu · defectiveGEAR UNSAFE ON PRIMARY AND SECONDARY INDICATIONS WITH LANDING GEAR UP. RIGHT MAIN LANDING GEAR DOOR LINK AND BRACKET ASSEMBLY ADJUSTMENT/TEST CARRIED OUT AS PER AMM 32-34-05-5. PROXIMITY SWITCH ELECTRONICS UNIT REMOVED & REPLACED, OPERATIONAL TEST CARRIED OUJun 8, 2004 · N597FE · Doug MD11 · Landing Gear Position and WarningSDR 04FDEA01625Target · brokenRIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED PRIMARY AND SECONDARY WITH GEAR UP. PERFORMED QRH PROCEDURE AND RESTRICTED SPEED TO 230 KTS. ON POSTFLIGHT FOUND TARGET BROKEN. REMOVED AND REPLACED RT MLG TARGET AS PER AMM 32-34-05-4. PROXIMITY SENSOR & THE TARGETJun 6, 2004 · N597FE · Doug MD11 · Landing Gear Position and WarningSDR 04FDEA01279Structure · corrodedTAIL TANK - NR 28L BARREL NUT BORE CORROSION REMOVAL EXCEEDED LIMIT. COMPLIED AS PER FEDEX EA 1-5510-76711 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - AD 2003-22-08.May 17, 2004 · N597FE · Doug MD11 · Horizontal Stabilizer Miscellaneous StructureSDR 04FDEA01267Frame · damagedUPPER CARGO COMPARTMENT, RIGHT UPPER FRAME ASSY AT STA 1681 FOUND DAMAGED. UPPER CARGO COMPARTMENT, RIGHT UPPER FRAME ASSY AT STA 1681 CARRIED OUT REPAIR ON DAMAGED AREA AS PER SRM 53-30-00 VOL I FIG 1. FOR REPETITIVE INSPECTION TRACKING, REFER TO FEDEX EA 1May 14, 2004 · N597FE · Doug MD11 · Fuselage Main, FrameSDR 04FDEA01236Seat Track · dentedMAIN CARGO DECK STA 810 LEFT HAND SEAT TRACK REF X=27.5 SEAT TRACK DENTED. DENTED SEAT TRACK AT MAIN CARGO DECK STA 810 LEFT HAND SIDE X=27.5 REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I.May 12, 2004 · N597FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01241Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE CORROSION REMOVED AS PER CM 57-44-08 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0502. ORIGINAL THICKNESS =May 12, 2004 · N597FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 04FDEA01237Hinge Bracket · corrodedRIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA FOUND CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CM 57-44-09 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0503 SHT 2.May 12, 2004 · N597FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 04FDEA01243Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP I/B HINGE - ACTUATOR O/B LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE ACTUATOR O/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187, FINAL DIA 1.221 INCH, AND REPMay 12, 2004 · N597FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 04FDEA01242Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP I/B HINGE - ACTUATOR I/B LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE ACTUATOR I/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187 INCH, FINAL DIA 1.221 INCH, ANMay 12, 2004 · N597FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 04FDEA01240Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP I/B HINGE - SPOTFACE AT BARREL NUT AREA FOUND CORRODED. LEFT FWD O/B FLAP I/B HINGE SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CMM 57-44-08 PG 402-407, ORIG THK 0.382 INCH, MATERIAL REMOVED 0.002 INCH, REMAINING THK 0.3May 12, 2004 · N597FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 04FDEA01239Hinge Bracket · corrodedRIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE FOUND CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 PG 402-407, ORIG DIA 1.187 INCH, FINAL DIA 1.220 INCHMay 12, 2004 · N597FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 04FDEA01238Hinge Bracket · corrodedRIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE FOUND CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED, FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187 INCH, FINAL DIA 1.220 INCMay 12, 2004 · N597FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 04FDEA01212Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0503 SHT 2 AMay 10, 2004 · N597FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 04FDEA01189Hinge Bracket · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL 2. ORIG DIA 1.062 INCH, FINAL DIA 1.189 INCH AND REPAIRED AS PER FEDEX EA May 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01213Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE I/B ACTUATOR LUG HOLE CORROSION REMOVED, FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 PG 402-407 ORIG DIA 1.187 INCH, FINAL DIA 1.221 INCH ANDMay 10, 2004 · N597FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 04FDEA01211Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE O/B ACTUATOR LUG HOLE CORROSION. REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 PG 402-407 ORIG DIA 1.187 INCH, FINAL DIA 1.221 INCH ANMay 10, 2004 · N597FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 04FDEA01206Hinge · corrodedRIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR O/B LUG HOLE FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR O/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187, FINAL DIA 1.222, AND REPAIRMay 10, 2004 · N597FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 04FDEA01205Hinge · corrodedRIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR I/B LUG HOLE FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR I/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187, FINAL DIA 1.221, AND REPAIRED May 10, 2004 · N597FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 04FDEA01204Hinge · corrodedRIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUNT SPOTFACE FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUNT SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0502 SHEET 2. ORIGINAL THICMay 10, 2004 · N597FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 04FDEA01203Hinge · corrodedRIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, SPOTFACE AT BARREL NUT AREA FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0502 SHEET 2. May 10, 2004 · N597FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 04FDEA01202Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.503 MATERIAL REMOVED: 0.002 REMAINING THICKMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01201Hinge · corrodedRT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.094. REPAIRED AS PER EA 1-5750-75954, LT AND RT OMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01200Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.487 MATERIAL REMOVED: 0.003 REMAINING THICKNEMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01199Hinge · corrodedRT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.093 FINAL DIAMETER: 1.126 AND REPAIRED AS PER FEDEX EMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01198Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.410 MATERIAL REMOVED: 0.004 REMAININGMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01197Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND REPAIRED AS PER FEDEMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01196Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.397 MATERIAL REMOVED: 0.001 REMAINING TMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01195Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND REPAIRED AS PER FEDMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01194Hinge · corrodedRT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.514, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0.513 AMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01193Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.093 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT ANDMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01191Hinge · corrodedRT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.093, FINAL DIA 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RTMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01192Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.500, MATERIAL REMOVED 0.002, REMAINING THICKNESS 0.498May 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01190Hinge · corrodedRT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.406, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0.4May 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01188Hinge · corrodedRT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR LUG SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.406, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0.405 AMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01187Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.502 MATERIAL REMOVED: 0.002 REMAINING THICKNESMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01186Hinge · corrodedLT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.094 AND REPAIRED AS PER FEDEX EAMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01185Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.500 MATERIAL REMOVED: 0.008 REMAINING THICKNESMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01184Hinge · corrodedLT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.093 FINAL DIAMETER: 1.127 AND REPAIRED AS PER FEDEX EA 1May 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01183Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.391 MATERIAL REMOVED: 0.002 REMAINING THMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01182Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND REPAIRED AS PER FEDEXMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01181Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.222 AND REPAIRED AS PER FEDEXMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01180Hinge · corrodedLT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.405, MATERIAL REMOVED 0.003, REMAINING THICKNESSMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01179Hinge · corrodedLT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.223 AND REPAIRED AS PER FEDEX May 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01178Hinge · corrodedLT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.505, MATERIAL REMOVED 0.002, REMAINING THICKNESS 0.503 ANMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01177Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.095 AND REPAIRED AS PER FEDEX EA 1-5750-74315. LT AND RMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01176Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.502, MATERIAL REMOVED 0.004, REMAINING THICKNESS 0.498 AMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01175Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.093, FINAL DIA 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT ANDMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01174Actuator · corrodedLT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.405, MATERIAL REMOVED 0.002, REMAINING THICKNESS 0.403May 10, 2004 · N597FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01173Actuator · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT ANMay 10, 2004 · N597FE · Doug MD11 · Trailing Edge Flaps
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