Boeing MD-11F

Service difficulty reports · 31,320

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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 = 'MD11F'
  ORDER BY difficulty_date DESC"

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SDR IPXA2016060604308Bulkhead Web · corrodedINSPECTION TYPE:3C, FORWARD CARGO COMPARTMENT AFT BULKHEAD WEB IS CORRODED AT BS 6-73.5 ABOVE LONGERON 42 RT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT CHORD IAW DWG ADA7667 AND SRM 51-35-01.May 17, 2016 · N257UP · Doug MD11F · Fuselage Main, BulkheadSDR IPXA2016060604304Skin · corrodedINSPECTION TYPE:3C, CENTER WING UPPER AFT SKIN HAS CORROSION ABOVE STR 5 AND 6 AT BS XCW =- 113. REPAIRED IAW EA 011-5730-A6270, REV I/R AND EO MD11-5730-60877-A.May 17, 2016 · N257UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016060304196Door Frame · crackedINSPECTION TYPE: 3C, AFT CARGO DOOR AFT FRAME LOWER LIGHTNING HOLE IS CRACKED. REPAIRED AFT CARGO DOOR AFT FRAME LOWER LIGHTNING HOLE IAW EA 011-5231-01-A6284 AND EO MD11-5230-60907-A.May 17, 2016 · N257UP · Doug MD11F · Cargo/Baggage DoorsSDR IPXA2016053104045Intercostal · crackedINSPECTION TYPE: 3C, FWD CARGO COMPARTMENT AT BS 6-10 TO 6-30, INTERCOSTAL BETWEEN LONGERON 42R-43R IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL AT BS 6-10 TO 6-30 LONGERON 42R TO 43R IAS DWG ACA7049 AND SRM 51-33-01.May 17, 2016 · N257UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016053104043Intercostal · crackedINSPECTION TYPE:3CFWD, CARGO AT BS 655 TO 675 LONG 42R-43R, INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL AT BS 655 TO 675 LONGERON 42R-43R IAW DWG ACA7049 AND SRM 51-35-01.May 17, 2016 · N257UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016052904000Longeron Splice · crackedINSPECTION TYPE:3C, LONGERON SPLICE FITTING IS CRACKED IN FWD. CARGO COMPARTMENT AT BS 869, LONGERON 35 LT. R & R CRACKED LONGERON 35 LT SPLICE FITTING AT BS 869 IAW DWG ADA8423 AND SRM 51-33-01.May 17, 2016 · N257UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201605171649Skin · crackedON WALK AROUND, FOUND RT WING LE CRACK, APPROX 3.5" AT INBD SIDE OF NR 6 SLAT. REPAIRED IAW EA 1-5730-T0325373 PART 1 & 2.May 17, 2016 · N583FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605171648Doubler · crackedRIGHT WING FIXED LE COMPARTMENT, AT STATION XOS 795, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.May 17, 2016 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605171647Doubler · crackedRIGHT WING FIXED LE COMPARTMENT, STATION XOS 768, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR AS IAW GMM 6-2-100.May 17, 2016 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605171646Doubler · crackedRIGHT WING FIXED LE COMPARTMENT, AT APPROX STATION XOS 697, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.May 17, 2016 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605171645Doubler · crackedRIGHT WING FIXED LE COMPARTMENT, AT STATION XOS 665, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.May 17, 2016 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605171644Doubler · crackedRIGHT WING FIXED LE COMPARTMENT, AT STATION XOS 656, BEADED DOUBLER FOUND CRACKED. REPAIR CLASSIFIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.May 17, 2016 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605171643Doubler · crackedRIGHT WING FIXED LE COMPARTMENT, AT STATION XOS 614, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.May 17, 2016 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605171642Doubler · crackedLEFT WING FIXED LE COMPARTMENT AT APPROX STATION XOS 545, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.May 17, 2016 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605171641Doubler · crackedLEFT WING FIXED LE COMPARTMENT AT APPROX STATION XOS 675, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 17, 2016 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605171640Fitting · corrodedLEFT WING, OTBD FLAP VANE HORN FITTING B FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.915", WIDTH: 0.621". FINAL SIZE: LENGTH 1.0395", WIDTH: 0.7395", MAXIMUM ALLOWABLE SIZE: LENGTH 0.9May 17, 2016 · N595FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201605171639Fitting · corrodedLEFT WING, OTBD FLAP VANE HORN FITTING C FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.918", WIDTH: 0.653". FINAL SIZE: LENGTH 1.019", WIDTH: 0.718", MAXIMUM ALLOWABLE SIZE: LENGTH 0.940May 17, 2016 · N595FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201605171638Fitting · corrodedLEFT WING, OTBD FLAP VANE HORN FITTING D FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.858", WIDTH: 0.598", FINAL SIZE: LENGTH 0.9495", WIDTH: 0.649", MAXIMUM ALLOWABLE SIZE: LENGTH 0.940May 17, 2016 · N595FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201605171637Hinge · corrodedRIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE OTBD BORE CORROSION. CORROSION REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING DIA: 1.282", FINAL DIA: 1.315", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW May 17, 2016 · N595FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201605171636Hinge · corrodedRIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE INBD BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING DIA: 1.283", FINAL DIA: 1.315". MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IMay 17, 2016 · N595FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201605171635Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 1.282", FINAL DIA: 1.288", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLEDMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171634Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 1.250", FINAL DIA: 1.254", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED BY MACHINING AMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171633Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.708", FINAL DIA: 0.722". MAXIMUM ALLOWABLE DIA: 0.709". SHOULDER BUSHING FABRICATED BY MACHIMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171632Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.708", FINAL DIA: 0.722". MAXIMUM ALLOWABLE DIA : 0.709". SHOULDER BUSHING FABRICATED BY MACHMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171631Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.943", FINAL DIA: 0.953". MAXIMUM ALLOWABLE DIA: 0.944". REPAIRED BUSHING, FABRICATED BY MACMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171630Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.251 INCH, FINAL DIAMETER 1.254 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH;. REPAIRED BUSHING, FAMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171629Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.382 INCH, FINAL DIAMETER 0.410 INCH & MAXIMUM ALLOWABLE DIAMETER 0.391 INCH. RMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171628Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE CORROSION. CORROSION HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.382 INCH, FINAL DIAMETER 0.410 INCH & MAX ALLOWABLE DIAMETER 0.391 INCH. REPAIREDMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171627Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE 3 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.598 INCHES, FINAL DIAMETER 0.604 INCHES, MAX ALLOWABLE DIAMETER 0.584 INCHES. REPMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171626Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE 3 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.598 INCHES, FINAL DIAMETER 0.604 INCHES, MAX ALLOWABLE DIAMETER 0.584 INCHES. REPMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171625Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT INBD HOLE BORE CORROSION. CORROSION HOLE NR 2 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.944 INCHES, FINAL DIAMETER 0.951 INCHES, MAX ALLOWABLE DIAMETER 0.944 INCHES. REPMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171624Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE OTBD BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING DIAMETER 1.222 INCH, FINAL DIAMETER 1.237 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRED BUSHING, FABRICAMay 17, 2016 · N595FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201605171623Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE INBD BORE CORROSION. CORROSION AT HOLE INBD BORE REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING DIAMETER 1.2235 INCH, FINAL DIAMETER 1.237 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRMay 17, 2016 · N595FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201605171622Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 1.218 INCH, FINAL DIAMETER 1.226 INCH & MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. REPAIMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171621Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE. BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 1.252 INCH, FINAL DIAMETER 1.255 INCH & MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. REPMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171620Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING THICKNESS 0.437 INCHES, MATERIAL REMOVED FWD SIDE 0.006 INCHES, AFT SIDE 0.016 INCHES, REMAINING THICMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171619Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-48-08. EXISTING DIAMETER 0.708 INCHES, FINAL DIAMETER 0.731 INCHES, MAX ALLOWABLE DIAMETER 0.709 INCHES. RMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171618Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 0.727 INCHES, FINAL DIAMETER 0.731 INCHES & MAX ALLOWABLE DIAMETER 0.709 INCHES. REPAIR BUSHINMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171617Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, UPPER MOUNT HOLE OTBD BORE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 0.942 INCHES, FINAL DIAMETER 0.950 INCHES & MAX ALLOWABLE DIAMETER 0.944 INCHES. REPAIR BUSHING FABRICATMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171616Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08, EXISTING DIAMETER 0.627 INCHES, FINAL DIAMETER 0.629 INCHES & MAX ALLOWABLE DIAMETER 0.621 INCHES. REPAIR BUSHINGMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171615Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, FWD MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 6 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.2805 INCH, FINAL DIAMETER 1.284 INCH & MAX ALLOWABLE DIAMETER 1.254 INCH. REPAIREMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171614Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.256 INCH, FINAL DIAMETER 1.259 INCH, MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRED BMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171613Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBOARD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.252 INCH, FINAL DIAMETER 01.259 INCH, MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171612Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.665 INCHES, FINAL DIAMETER 0.677 INCHES & MAX ALLOWABLE DIAMETER 0.667 INCHES. REPAIR BUSHING FABMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171611Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.390 INCHES, FINAL DIAMETER 0.407 INCHES, MAX ALLOWABLE DIAMETER 0.391 INCHES. REPAIR BUSHINMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171610Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.390 INCHES, FINAL DIAMETER 0.407 INCHES, MAX ALLOWABLE DIAMETER 0.391 INCHES. REPAIREDMay 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605171609Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.582 INCH, FINAL DIAMETER 0.597 INCHES. MAX ALLOWABLE DIAMETER 0.584 INCHES. SHOULDER May 17, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2016061204517Skin · corrodedINSPECTION TYPE:3C, AFT FUSELAGE SKIN HAS CORROSION BETWEEN BS 2125 TO 2163 AND BETWEEN LONG. 33 RT TO 35 RT. REPAIRED CORRODED FUSELAGE SKIN AT SAID LOCATION IAW VT-SAA EA 011-5330-01-A6277 REV I/R AND MD11-5330-61031-A.May 16, 2016 · N257UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016060804365Seat Track · damagedINSPECTION TYPE:3C, MAIN CABIN CENTER SEAT TRACK HAS AN ELONGATED HOLE AT BS 565. REPAIRED SEAT CENTER SEAT TRACK AT BS 565 IAW VT-SAA EA011-5310-01-A6265, REV. I/R AND EO MD11-5310-60986-A.May 16, 2016 · N257UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2016060704327Structure · corrodedINSPECTION TYPE:3C, AFT CARGO COMPARTMENT AT BS 1902 TO 1967 ABOVE LONGERON 42 RT, T-CHORD HAS CORROSION. REMOVED, FABRICATED AND REPLACED T-CHORD IAW DWG. AGA3857 AND SRM 51-31-01.May 16, 2016 · N257UP · Doug MD11F · Fuselage Main, Structure
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