N628FE

Service difficulty reports · 234

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 = 'N628FE' 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 FDEA201903140604Seat Track · crackedMAIN DECK FLOOR SEAT TRACK AT STATION 755 X = 47.5 FOUND CRACKED. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 FROM STATION 725 TO STATION 785 X = 47.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2Mar 14, 2019 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201903140602Seat Track · crackedMAIN DECK FLOOR SEAT TRACK AT STATION 635 X = 27.5 FOUND CRACKED. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT FROM STATION 625 TO STATION 645 X = 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-Mar 14, 2019 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201903140603Seat Track · crackedMAIN DECK FLOOR SEAT TRACK AT STATION 755 X = -27.5 FOUND CRACKED. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT FROM STATION 745 TO STATION 783 X = -27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6Mar 14, 2019 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201903130584Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 5-6 X= -8.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT AS PER SRM 53-00-52-2R FIGURE 201 REPAIR1 FROM STATION 1531/5-0 TO STATION 5-23 X= -8.5. REPAIR CLASSIFIED AS MAJOR PEMar 13, 2019 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201903130582Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1491 X = - 47.5 FOUND CORROSION AS MARKED. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT FROM STATION 1471 TO STATION 5-0 X = -47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS Mar 13, 2019 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201903130585Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 5-6 X = 8.5 FOUND CROWN DAMAGED AS MARKED. MAIN DECK FLOOR SEAT TRACK REPAIR CARRIED OUT BY SECTIONAL REPLACEMENT FROM STATION 1531 / 5-0 TO STATION 5-23 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIMar 13, 2019 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201903130583Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 1351 X = -8.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK REPAIR CARRIED OUT BY SECTIONAL REPLACEMENT FROM STATION 1311 TO STATION 1391 X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PMar 13, 2019 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2019040512571Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 6-40 X = -8.5 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPALCEMANT AT STATION 1129 / 6-0 TO STATION 6-60 X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR1. REPAIR CLASSIFIED AS MAJMar 12, 2019 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2019031420569Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1019 X= 8.5 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT AT STATION 1009 TO STATION 1029 X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMMMar 12, 2019 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201903120570Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 869 X = 8.5 FOUND CORROSION. MAIN DECK FLOOR CARRIED OUT SEAT TRACK REPAIR BY SECTIONAL REPLACEMENT FROM STATION 849 TO STATION 909 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR AS PER GMMar 12, 2019 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201902200459Anti-Ice Valve · malfunctionedPDIS 628 30-10 7458 20FEB19 MSP FACT U LOGPAGES:3042522 DURING DESCENT RECIEVED LEVEL 2 WING A-ICE RIGHT DISAG R/I 20FEB19 09:50 MSP U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 3290278-1 CPN: 3000067 POS: NR 2 SRL: 417 TAG NR: 9C8178Feb 20, 2019 · N628FE · Doug MD11F · Airfoil Anti/De-ice SystemSDR FDEA2018082982216Smoke Detector · false activationINTERMITTENT CAB SMOKE WARNING THROUGOUT FLIGHT AND TAXI-IN. WARNING STAYED ON FOR ABOUT 1 SECOND. R&R NR 9 SMOKE DETECTOR, NOW TEST GOOD REF MM 26-15-01-4.Aug 28, 2018 · N628FE · Doug MD11F · Smoke DetectionSDR FDEA201804050873Trunnion · corrodedCORROSION WAS FOUND ON THE LT MLG TRUNION FAYING SURFACE. BORE HOLES ALSO HAD CORROSION. EA 1-3210-T0339350 ISSUED FOR REPAIRS. REPAIRED THE LT MLG A FRAME IAW SRM 57-20-14-2R, AND EA 1-3210-T0339350, PART 2.Apr 5, 2018 · N628FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201705141415Longeron · corrodedAFT CARGO BAY, BS 1954, LONGERON 45R FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01-0G AND FOUND OUT OF LIMITS IAW SRM 53-00-00-2R, FIGURE 205. REPLACEED THE LONGERON IAW EA 1-5310- T0333344, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 14, 2017 · N628FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201705141414Longeron · corrodedAFT CARGO BAY BS 1954, LONGERON 44R FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01-0G AND FOUND OUT OF LIMITS IAW SRM 53-00-00-2R, FIGURE 205. REPLACED THE LONGERON IAW EA1-5310-0333281, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 14, 2017 · N628FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201705141413Cargo Track · damagedMAIN DECK CARGO TRACK CROWN AREA FOUND DAMAGED BS 1215, RBL 75.25. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.May 14, 2017 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201705141411Skin · crackedONE CRACK FOUND APPRROXIMATELY .500 INCH IN LENGTH ON THE LT WING FIXED LEADING EDGE SLAT ACTUATOR ACCESS DOOR FORWARD INBD CORNER AT XOS 490. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 17. CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.May 14, 2017 · N628FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201705141410Skin · crackedONE CRACK FOUND APPRROXIMATELY .250 INCH IN LENGTH ON THE RT WING FIXED LEADING EDGE, FUEL ACCESSS DOOR FORWARD INBD CORNER AT XOS 610. REPAIRED IAW SRM 57-40-01-2R FIGURE 201 REPAIR 18. CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.May 14, 2017 · N628FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201705141422Cargo Track · corrodedMAIN DECK CARGO TRACK CORRODED AT BS 1617, RBL 75.25. CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1591 - 1651 IAW SRM 53-00-52, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED ASMay 14, 2017 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201705141421Cargo Track · corrodedMAIN DECK CARGO TRACK CORRODED BS 1597, RBL 75.25. THE CORROSION FOUND TO EXCEEDED THE LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMay 14, 2017 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201705141418Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 625 - 627 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15 .THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 14, 2017 · N628FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201705141417Doubler · crackedLEFT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 633 - 636 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 14, 2017 · N628FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201705141412Frame · dentedMAIN DECK CARGO, FRAME DENTED AT BS 1721, LONGERON 12L. REPAIRED IAW SRM 53-00-07-2R, FIG 201, REPAIR 2.May 14, 2017 · N628FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201705101385Doubler · crackedRIGHT WING LEADING EDGE CAVITY AT XOS 614, BEADED DOUBLER CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 10, 2017 · N628FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201703190958Slat System · malfunctionedDURING FINAL, SHORTLY AFTER SELECTING FLAPS 15, RECEIVED A LEVEL 2 SLATS DISAGREE & SPEED FOOT WENT UP TO APROXIMATELY 205. PERFORMED MISSED APPROACH AND FOLLOWED QRH. RECONFIGURED FOR SECOND APPROACH WITHOUT INCIDENT. EXTENDED LEADING EDGE SLATS AND PERMar 19, 2017 · N628FE · Doug MD11F · Leading Edge Slat Control SystemSDR FDEA201608303081Button · defectiveDURING PREFLIGHT, R1 DOOR ESCAPE SLIDE LIGHT DOES NOT TEST. REPLACED RT DOOR SLIDE PRESSURE LENS BUTTON. OPS CHECKS NORMAL IAW MM 25-61-04.Aug 30, 2016 · N628FE · Doug MD11F · Escape SlideSDR FDEA201510293403Tire · blownAFTER TOUCHDOWN ON LANDING ROLLOUT BELOW 60 KTS, NR 9 TIRE FAILURE ALERT. FOUND NR 9 TIRE BLOWN. R & R NR 9 & 10 TIRE IAW MM CHP 32-41-01-4. INTERROGATED CFDS NO ANTI-SKID FAULTS FOUND. PERFORMED ANTI-SKID RTS IAW MM CHP 32-45-01-5. PERFORMED AUTO BRAKE ROct 29, 2015 · N628FE · Doug MD11F · TireSDR FDEA201507032148Seat Track · crackedFORWARD CARGO FLOOR SEAT TRACK FOUND CRACKED AT STATION 635 X = 8.0. CRACKED SEAT TRACK AT FORWARD CARGO FLOOR STA 635 X= 8.5 CARRIED OUT REPAIR AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 3, 2015 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201507032147Seat Track · crackedFORWARD CARGO FLOOR SEAT TRACK FOUND CRACKED AT STATION 635 X= 47.5. CRACKED SEAT TRACK AT FWD CARGO FLOOR STA 635 X=47.5 REPAIRED AS PER MD11 SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 3, 2015 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201507032146Seat Track · crackedFORWARD CARGO FLOOR SEAT TRACK FOUND CRACKED AT STATION 695 X= -8.0. CRACKED SEAT TRACK AT CABIN BETWEEN STA 624 STA 745 X= -8.5 CARRIED OUT REPAIR IAW SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6.2-100.Jul 3, 2015 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201507032143Seat Track · damagedCABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA AT STATION 765, X = 75.25 FOUND DAMAGED. DAMAGED SEAT TRACK CROWN AT MAIN DECK CARGO COMPARTMENT STA 765, X = 75.25 CARRIED OUT REPAIR I.A.W SRM 53-00-52-2R REPAIR 1, FIGURE 201. REPAIR CLASSIFIED MAJJul 3, 2015 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201507032145Seat Track · crackedCABIN SEAT TRACK FOUND CRACKED AT BS 755 X -8. REPAIR IAW SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 3, 2015 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201507032144Seat Track · crackedCABIN SEAT TRACK FOUND CRACKED AT BS 635 X -8. REPAIRED IAW SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 3, 2015 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201507012131Wire · damagedFOUND 14 TWISTED WIRES, OUTER PROTECTIVE INSULATION BADLY DETERIORATED AT ABOUT BS 495 - 555 FLOOR AREA. R & R IAW SWPM 20-10-01. CONTINUITY CHECKED IAW WDM 22-16-02, WDM 27-66-01, WDM 28-48-01, WDM 52-71-02, WDM 73-33-01, WDM 29-31-01 & WDM 79-33-01 FOUND SJul 1, 2015 · N628FE · Doug MD11F · Auto Flight System WiringSDR FDEA201506292116Fitting · crackedRIGHT OTBD FLAP, INBD FWD HINGE, OTBD SIDE LOAD FITTING CRACKED. REMOVED AND REPLACED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 29, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201506282108Hinge Bracket · corrodedRIGHT INBD FLAP, OTBD AFT HINGE, OTBD PIVOT HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-52-03. REPAIR ACCOMPLISHED IAW EA1-5750-T0318614 PART 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 28, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201506282107Hinge Bracket · corrodedRIGHT INBD FLAP, OTBD AFT HINGE, INBD PIVOT HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-52-03. REPAIR ACCOMPLISHED IAW EA 1-5750-T0318614 PART 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 28, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201506282106Hinge · corrodedLEFT INBD FLAP, OTBD AFT HINGE PIVOT, OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING DIAMETER, HALF HINGE LUG 1.281 INCH, STRAP 1.220 INCH, FINAL DIAMETER, HALF HINGE LUG 1.326 INCH, STRAP 1.326 INCH, MAXIMUM Jun 28, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201506282105Hinge · corrodedLEFT INBD FLAP, OTBD AFT HINGE PIVOT, INBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HALF HINGE LUG 1.252 INCH, STRAP 1.220 INCH, FINAL HALF HINGE LUG 1.284 INCH, STRAP 1.284 INCH & MAXIMUM ALLOWABLE 1.220 INCJun 28, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201506282104Hinge · corrodedLEFT OTBD FLAP, OTBD AFT HINGE PIVOT, OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-04. EXISTING 1.141 INCH, FINAL 1.152 INCH & MAXIMUM ALLOWABLE 1.150 INCH. REPAIR ACCOMPLISHED IAW EA 1- 5750-T0318605 PART 1. REFER TO WJun 28, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201506262085Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7, REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING 0.0713 INCH, FINAL= 0.719 INCH & MAXIMUM ALLOWABLE= 0.709 INCH. SHOULDER BUSHING FABRICATED BY MACHJun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201506262084Hinge · corrodedRIGHT WING, OTBD LAP OTBD FWD HINGE LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING 0.0711 INCH, FINAL= 0.715 INCH, MAXIMUM ALLOWABLE= 0.709 INCH. SHOULDER BUSHING FABRICATED BY MACHINIJun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201506262082Bracket · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIAMETER = 1.210 INCH, FINAL DIAMETER = 1.247 INCH, MAXIMUM ALLOWABLE= 1.220 INCH. REPAIR BUSHING FABRIJun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201506262081Bracket · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE ACTUATOR INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 1.218 INCH, FINAL DIAMETER = 1.247 INCH, MAXIMUM ALLOWABLE =1.220 INCH. REPAIR BUSHING FABRICATJun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201506262080Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE PIVOT HOLE BORE CORROSION. CORROSION AT HOLE NR 4 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 2.313 INCH, FINAL DIAMETER = 2.316 INCH & MAXIMUM ALLOWABLE DIAMETER = 2.3135 INCH. REPAIR BUSHING FABJun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201506262079Repair · chafedCABIN MAIN DECK CARGO COMPARTMENT LT STATION 535, LONGERON 19L FRAME EXISTING REPAIR FOUND CHAFED. EXISTING REPAIR PARTS AT MAIN DECK CARGO COMPARTMENT LT STATION 535, LONGERON 19L ON FRAME REMOVED. NEW REPAIR CARRIED OUT IAW SRM 53-20-07-2R REPAIR 1 FIGURJun 26, 2015 · N628FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201506262078Repair · chafedCABIN MAIN DECK CARGO COMPARTMENT LT STATION 535, LONGERON 24L FRAME. EXISTING REPAIR FOUND CHAFED. EXISTING REPAIR REMOVED. NEW REPAIR CARRIED OUT IAW EA 1-5310-TO318700 P 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100. REFER TO WRI 53102075 FOR WORK DETAILSJun 26, 2015 · N628FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201506262077Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE LOWER BARREL NUT HOLE BORE CORROSION. CORROSION AT HOLE NR 7. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING 0.387 INCH, FINAL 0.405 INCH, MAXIMUM ALLOWABLE IS 0.391 INCH. REPAIR BUSHING FABRICATED BY MACHINJun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201506262076Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE UPPER BARREL NUT HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING IS 0.387 INCH, FINAL IS 0.405 INCH, MAXIMUM ALLOWABLE IS 0.391 INCH. REPAIR BUSHING FABRICATED BY MAJun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201506262074Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT OTBD HOLE HAS SURFACE CORROSION. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR SHIM FABRICATED & INSTALLED IAW EA1-5750-T0318565 P1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Jun 26, 2015 · N628FE · Doug MD11F · Trailing Edge Flaps
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