N615FE

Service difficulty reports · 469

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 = 'N615FE' 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 FDEA2018051801192Seat Track · corrodedBS 1880 RBL 27.5 SEAT TRACK FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED FROM BS 1811 TO 1887 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WASMay 8, 2018 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018051801191Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 693. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 8, 2018 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018051801190Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER WAS FOUND CRACKED AT XOS 705. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 8, 2018 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018051801189Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 762. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 8, 2018 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018051801188Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER WAS FOUND CRACKED AT XOS 616. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 8, 2018 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018051811187Seat Track · damagedCARGO TRACK CROWN DAMAGED AT 5-10, X= 27.5 UPPER CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 8, 2018 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201801290271O-Ring · leakingTWO HOURS 20 MINUTES INTO FLT, THE HYD 3 OFF WITH 2.5 GALLONS ON CONFIGURATION OF GEAR HYD 3 FAILED. TROUBLESHOT IAW FIM 29-10-08, HYD QTY LEVEL 1.8 IN SYS 3, FOUND A LARGE AMOUNT OF HYD FLUID LEAKING FROM TAIL. AFTER FURTHER INVESTIGATION. FOUND TJan 29, 2018 · N615FE · Doug MD11F · Hydraulic System, MainSDR FDEA201711113235Duct · crackedLEVEL 2 ENG 2 ICE DUCT FAIL WARNING AFTER T/O PASSING 3000', PER QRH SHUT DOWN NR 2 ENG AND RETURNED TO BASE. DISCOVERED THAT THE DUCT GOING AFT IS CRACKED.Nov 11, 2017 · N615FE · Doug MD11F · Engine Anti-Icing SystemSDR FDEA201708112190Light · inoperativeR1 DOOR SLIDE PRESS TO TEST INDICATOR IS INOP. REMOVED AND REPLACED EMERGENCY SLIDE PRESS TO TEST LIGHT BULBS AS REQUIRED. OPS CHECKED NORMAL PER MM 25-61-04-5. OK FOR SERVICE.Aug 11, 2017 · N615FE · Doug MD11F · Emergency EquipmentSDR FDEA201706141637Pseu · failedUPON RAISING THE GEAR AFTER TAKEOFF, THE LEFT MAIN GEAR DID NOT SHOW UP SAFE. THE PRIMARY AND SECONDARY INDICATORS BOTH INDICATED RED UNSAFE. CHANGED THE PROXIMITY SWITCH ELECTRONIC UNIT.Jun 14, 2017 · N615FE · Doug MD11F · Landing Gear Retraction/Extension SystemSDR FDEA201612064346Computer · failedON TAKEOFF ROLL AT 80 KTS HAD "ALT" MISCOMPARE ALERT AND REJECTED TAKEOFF. COMPLIED WITH QRH. ALERT CLEARED AT 60 KTS. ATTEMPTED SECOND TAKE OFF WITH SAME RESULTS AND A MOMENTARY LEVEL 1 WINDSHEAR DETECT FAIL MESSAGE. COMPLIED WITH QRH AND TAXIED BACK TO RDec 6, 2016 · N615FE · Doug MD11F · Autopilot ComputerSDR FDEA201607122366Spring · brokenL-1 DOOR UPPER LINING SLIDING CLOSEOUT PANEL SPRING BROKEN AND PANEL DAMAGED. NO RESTRICTION, IAW 25-23-23-2 L1 DOOR UPPER LINING SLIDING CLOSEOUT PANEL SPRING BROKEN AND PANEL DAMAGED. REMOVED L1 DOOR SLIDING CEILING AND EXIT LIGHT PANEL ASSY IAW MM 25-23-Jul 12, 2016 · N615FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201607122368Terminal · overheatedFUME EVENT, CAPTAIN AND BOTH JUMPSEATING PILOTS SMELLED STRONG ELECTRICAL BURNING ODOR ON ARRIVAL AT AIRCRAFT. 3RD WRITE-UP OLD DISCREPANCY: 615-24-00-0003950. ACCOMPLISHED GVI OF FLIGHT DECK WINDOWS, FOUND L1 WINDOW UPPER CTR TERMINAL STRIP HAS EVIDENCE OFJul 12, 2016 · N615FE · Doug MD11F · Windshield/Door Rain/Ice RemovalSDR FDEA201607032243Light · brokenL1 DOOR FOLLOWER CEILING PANEL EMERGENCY EXIT LIGHT FRAME ASSY BROKEN.Jul 3, 2016 · N615FE · Doug MD11F · Emergency LightingSDR FDEA201605231720Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE BRACKET, WING SIDE, SIDE ATTACH SURFACE FOUND CORROSION. REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.402", LOWER 0.378", MATERIAL REMOVED: UPPER 0.010", LOWER 0.010" AND REMAINING THICKNESS: UPPER 0.392", LOWER 0May 23, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605231719Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE BRACKET, WING SIDE, SIDE ATTACH SURFACE FOUND CORROSION. REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.392", LOWER 0.353", MATERIAL REMOVED: UPPER 0.010", LOWER 0.010" AND REMAINING THICKNESS: UPPER 0.382", LOWER May 23, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605221713Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.313", FINAL HOLE DIA: 1.326" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BMay 22, 2016 · N615FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201605221712Hinge Bracket · corrodedRIGHT WING INBD FLAP OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.250", FINAL HOLE DIA: 1.285" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BMay 22, 2016 · N615FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201605221711Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.2834", FINAL HOLE DIA: 1.315" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABMay 22, 2016 · N615FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201605221710Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.250", FINAL HOLE DIA: 1.315" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRMay 22, 2016 · N615FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201605221709Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SPOT FACE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.408", MATERIAL REMOVED: FWD 0.008", AFT 0.025", REMAINING THICKNESS: 0.375" ANMay 22, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605221708Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.584", FINAL HOLE DIA: 0.613" AND MAXIMUM ALLOWABLE HOLE DIA: 0.584". NEW May 22, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605221707Hinge Bracket · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.584", FINAL HOLE DIA: 0.612" AND MAXIMUM ALLOWABLE HOLE DIA: 0.584". NEWMay 22, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201685Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.248", FINAL HOLE DIA: 1.252" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201684Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.249", FINAL HOLE DIA: 1.252" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201683Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM57-44-08. EXISTING HOLE DIA: 0.709", FINAL HOLE DIA: 0.727" AND MAXIMUM ALLOWABLE HOLE DIA: 0.709". NEW SMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201682Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.709", FINAL HOLE DIA: 0.727" AND MAXIMUM ALLOWABLE HOLE DIA: 0.709". NEW May 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201680Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, PIVOT BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM57-44-08. EXISTING HOLE DIA: 2.311", FINAL HOLE DIA: 2.316" AND MAXIMUM ALLOWABLE HOLE DIA: 2.3135". NEW REPAIR BUSHING FAMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201679Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE FOUND CORROSION. NR 8 HOLE CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.219", FINAL HOLE DIAMETER 1.224" & MAXIMUM ALLOWABLE HOLE DIMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201678Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORROSION. NR 8 HOLE CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.218", FINAL HOLE DIAMETER 1.224" & MAXIMUM ALLOWABLE HOLE DIMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201677Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SPOT FACE FOUND CORROSION. REWORKED & FOUND EXCEEDED LIMIT IAW MM 57-44-09. EXISTING THICKNESS 0.421", MATERIAL REMOVED, FWD FACE 0.009" & AFT FACE 0.009", REMAINING THICKNESS 0.4May 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201676Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH SPOT FACE FOUND CORROSION. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.399", MATERIAL REMOVED 0.009", REMAINING THICKNESS 0.390" & MINIMUM ALLOWABLE THIMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201675Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. NR 3 HOLE CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.581", FINAL HOLE DIAMETER 0.589" & MAXIMUM ALLOWABLE HOLE DIAMMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201674Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. HOLE 3 CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.596", FINAL HOLE DIAMETER 0.598" & MAXIMUM ALLOWABLE HOLE DIAMETEMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605181657Skin · crackedRIGHT WING FIXED LE SKIN CUT OUT, AT STATION 659.7174, TRACK 10, CORNER 13, FOUND CRACK APPROX 3/16 INCH IN LENGTH. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.May 18, 2016 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605181656Longeron · corrodedCENTER CARGO COMPARTMENT, STATION 1701 - 1721 RT SIDE, LONGERON 49R, FOUND CORRODED. CARRIED OUT REPAIR IAW EA 1-5310-T0325527 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 53103729 FOR WORK DETAILS.May 18, 2016 · N615FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 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 FDEA201605161605Skin · tornRIGHT WING OTBD FUEL DUMP ISLAND, UPPER SKIN FWD EDGE FOUND TORN AT STATION XOFH 799.865. CARRIED OUT REPAIR IAW EA 1-5730-T0325572 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 57303742 FOR WORK DETAILS.May 16, 2016 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605161604Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 1288, X=8.5, FOUND CROWN DAMAGED. REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 1263 - 1312, X= 8.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 16, 2016 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201605161603Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 1288, X=-8.5, FOUND CROWN DAMAGED. REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 1263 - 1312, X=-8.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 16, 2016 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201605161602Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 1288, X=-47.5, FOUND CROWN DAMAGED. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 1248 TO 1312, X = -47.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 16, 2016 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201605161601Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 5 - 7, X= 47.5, FOUND CROWN DAMAGED. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 5-0 TO 5-23, X=47.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 16, 2016 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201605161600Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 5 - 7, X=-47.5, FOUND CROWN DAMAGED. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 5-0 TO 5-63, X = -47.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 16, 2016 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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