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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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 OUSDR 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 TARGETSDR 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.SDR 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 1SDR 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.SDR 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 =SDR 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.SDR 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 REPSDR 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, ANSDR 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 0.3SDR 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 INCHSDR 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 INCSDR 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 ASDR 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 SDR 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 ANDSDR 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 ANSDR 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 REPAIRSDR 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 SDR 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 THICSDR 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. SDR 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 THICKSDR 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 OSDR 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 THICKNESDR 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 ESDR 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 REMAININGSDR 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 FEDESDR 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 TSDR 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 FEDSDR 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 ASDR 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 ANDSDR 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 RTSDR 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 0.498SDR 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 0.4SDR 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 ASDR 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 THICKNESSDR 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 EASDR 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 THICKNESSDR 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 1SDR 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 THSDR 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 FEDEXSDR 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 FEDEXSDR 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 THICKNESSSDR 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 SDR 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 ANSDR 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 RSDR 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 ASDR 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 ANDSDR 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 0.403SDR 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 AN
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