N616FE

Service difficulty reports · 267

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 = 'N616FE' 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 FDEA2018091432510Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER BARREL NUT HOLE BORE CORROSION. HINGE UPPER BARREL NUT HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T034Sep 13, 2018 · N616FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091432509Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342161 P1 STEP 2A AND INSTALLED AS PSep 13, 2018 · N616FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091432508Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS EPR CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342161 P1 STEP 2A AND INSTALLED AS PSep 13, 2018 · N616FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091432507Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342163 P1 STEP 2A AND INSTALLED AS PSep 13, 2018 · N616FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091432506Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342163 P1 STEP 2A AND INSTALLED AS PSep 13, 2018 · N616FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091432505Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION. HINGE PIVOT HOLE BORE (NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342163 P1 STEP 2B AND STSep 13, 2018 · N616FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091432497Hinge · corrodedRT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-132149 C PART 5 STSep 13, 2018 · N616FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2018091432496Hinge · corrodedRT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-132149 C PART 5 STSep 13, 2018 · N616FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2018091432495Hinge · corrodedLT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-132148 C PART 5 STSep 13, 2018 · N616FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2018091432494Hinge · corrodedLT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1- 5750-132148 C PART 5 SSep 13, 2018 · N616FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2018091432504Doubler · crackedLT WING, ALONG NR 6 SLAT LOCATION, ALONG XOS 789, LT LEADING EDGE FORMER ATTACHED DOUBLER CRACKED. LEADING EDGE FORMER ATTACHED DOUBLER, REMOVED AND REPLACED AS PER SRM 51-31-01-0G AND SRM 51-33-01-0G, DOUBLER PART NUMBER: ARB3954-7 FABRICATED AS PER DRAWING ASep 13, 2018 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018091432502Skin · cracked05EA FASTENER HOLES (NR 6, 7, 15, 34 & 35) FOUND CRACK INDICATION DURING OPEN HOLE HFEC INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. SKIN REPAIR CARRIED OUT AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR CLASSISep 13, 2018 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018091422458Angle · chafedCABIN MAIN DECK CARGO EXISTING REPAIR ANGLE FRAME LONGERON 24 LEFT AT STA 535 LEFT HAND FRAME FOUND CHAFFING MARK. REPAIR ANGLE LEFT HAND FRAME REPAIRED AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 12, 2018 · N616FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201809112450Skin · crackedLT WING LEADING EDGE BOTTOM SURFACE AROUND STA XOS =787.5 FOUND CRACK. REPAIR CARRIED OUT AS PER EA 1-5730-T0342355 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 11, 2018 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018091172374Skin · crackedLEFT HAND WING NR 8 SLAT OUTBOARD EDGE INTERIOR LOWER SURFACE AREA FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 57-40-01-2R REPAIR 3 FIGURE 201 AT STA XOS 1180.5 AND PER EA 1-5750-T0342354 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 7, 2018 · N616FE · Doug MD11F · Leading Edge DevicesSDR FDEA201809062370Skin · crackedNR 1 AIR CONDITIONING COMPARTMENT DOOR CUT OUT STA 587, L-32L AFT UPPER CORNER AREA FOUND CRACK. CRACK REPAIRED AS PER SRM 53-20-15-2R FIG 201 REPAIR 3, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 6, 2018 · N616FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA2018090542343Angle · chafedMAIN DECK CARGO EXISTING REPAIR ANGLE FRAME, LONGERON 20L AT STA 535 LEFT HAND FRAME FOUND CHAFFING MARK. EXISTING REPAIR ANGLE FRAME REPAIRED AS PER SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 4, 2018 · N616FE · Doug MD11F · Fuselage Main, FrameSDR FDEA2018090542342Seat Track · crackedMAIN DECK CARGO SEAT TRACK AT STA 635, X = 8.5 FOUND CRACK. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM EXISTING SPLICE STA 625 TO STA 665, X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 4, 2018 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018090542341Door Frame · crackedMAIN DECK CARGO LEFT HAND NR 3 DOOR AFT DOOR JAMB WEB AT STA 1315.420 FOUND CRACK. DOOR JAMB WEB REPAIRED AS PER SRM 53-40-15-2R FIGURE 201 REPAIR 3 FROM STA 1305.25 TO STA 1315.420. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10.Sep 4, 2018 · N616FE · Doug MD11F · Fuselage Main, StructureSDR FDEA2018090532340Skin · crackedDURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT HAND WING FIXED LEADING EDGE ACCESS DOOR CUTOUT CORNERS, FOUND 01 EACH CRACK AT CORNER 11 APPROXIMATELY 0.3 INCH IN LENGTH. ACCESS DOOR CUTOUT STA XOS 610 CARRIED OUT REPAIR AS PER SRM 57-Sep 3, 2018 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201807301851Sensing Element · failedAT CRUISE W NR 2 ANTI-ICE ON PER MEL. RECVD NR 2 ANTI-ICE OFF ALERT WITH ENGINE NR 2 A-ICE DUCT HAS FAILED. DIVERTED. INTERROGATED ESC VIA CFDS, NO FAULT FOUND ON CURRENT FAULT BUT GOT ANTI-ICE VLV FAULT ON FAULT. REPLACED D1-90 AND D1-91 SENSING ELEMENT FOR PJul 30, 2018 · N616FE · Doug MD11F · Air Intake Anti/De-Ice SystemSDR FDEA201804080930Light · no testEMERGENCY LIGHT SYSTEM TEST FUNCTION INOPERATIVE.Apr 8, 2018 · N616FE · Doug MD11F · Emergency LightingSDR FDEA201803300807Warning Light · illuminatedDURING AN EMERGENCY LIGHT TEST, RECEIVED AN EMERGENCY LIGHT BATTERY 1 LOW LEVEL 1 MESSAGE. PERFORMED AN EMERGENCY LIGHT BATTERY ADJUSTMENT AND TEST IAW AMM 33-51-01-5. OPS CHECKED GOOD.Mar 30, 2018 · N616FE · Doug MD11F · Emergency LightingSDR FDEA201802240483Battery · warning messageDURING A PREFLIGHT EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW. PERFORMED EMERGENCY LIGHT TEST 3 CONSECUTIVE TIMES IAW MM 33-51-01-5. ALL GOOD IAW WRI 30-30/6329. SUSPECT MISC FAILING AND GENERATING SPURIOUS LOW BATTERYFeb 24, 2018 · N616FE · Doug MD11F · Emergency LightingSDR FDEA201802200440Power Supply · inoperativeWITH EMER LT SWITCH IN ARM POS AND TEST BUTTON PUSHED, GET EMER LT BAT1 LO ALERT. EMER LT TEST DOES NOT DISPLAY. EMER LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY REF AMM 33-51-01-4. OPS CHECKS GOOD.Feb 20, 2018 · N616FE · Doug MD11F · Emergency LightingSDR FDEA201802180431Anti-Ice Valve · failedLEVEL 1 ENGINE ANTI-ICE OFF ALERT DURING CLIMB OUT, WITH ANTI-ICE NR 2 ENGINE SELECTED. ALSO HAD AN ANTI-ICE DISAGREE ON SELECTOR. REMOVED AND REPLACED THE NR 2 ENGINE ANTI -ICE VALVE IAW AMM 30-22-01-4. ADJUSTMENT AND TESTED GOOD IAW AMM 30-22-00-5-1.Feb 18, 2018 · N616FE · Doug MD11F · Engine Anti-Icing SystemSDR FDEA201802180430Anti-Ice Valve · failedHAD A LEVEL 1 ENGINE ANTI-ICE OFF ALERT DURING CLIMB OUT. WITH ANTI-ICE NR 2 ENGINE SELECTED. REMOVED AND REPLACED THE NR 2 ENGINE ANTI -ICE VALVE IAW AMM 30-22-01-4. ADJUSTMENT AND TESTED GOOD IAW AMM 30-22-00-5-1. ENGINE RUN PERFORMED.Feb 18, 2018 · N616FE · Doug MD11F · Engine Anti-Icing SystemSDR FDEA201802200431Warning System · activatedHAD LEVEL 1 ENG ANTI-ICE OFF ALERT ON CLIMB OUT WITH A/I ENGINE 2 SELECTED. ALSO HAD A/I DISAGREE ON SELECTOR.Feb 18, 2018 · N616FE · Doug MD11F · Air Intake Anti/De-Ice SystemSDR FDEA201706141645Skin · damagedON POST FLIGHT, FOUND THE LT WING UPPER SKIN PEELED BACK BETWEEN INBD AILERON AND OTBD FLAP. REMOVED DAMAGED AREA. FABRICATED A REPAIR IAW SRM 57-50-01-2R, FIGURE 203, REPAIR 6.Jun 14, 2017 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201611043827Slide · detachedL1 DOOR SLIDE FELL OUT. REMOVED AND REPLACED L1 SLIDE IAW AMM 25-61-01-4.Nov 4, 2016 · N616FE · Doug MD11F · Escape SlideSDR FDEA201609153246Seat Track · corrodedMAIN DECK BS 725 - 765, X 8.5 SEAT TRACK ASSEMBLY FOUND CORRODED. CORRODED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 665 TO STA 765 X=8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 15, 2016 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609153245Doubler · crackedRIGHT WING EXTERIOR, FOUND FIXED LEADING EDGE LOWER FORWARD DOUBLER AT XOS 547 CRACKED. CRACKED DOUBLER REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER PER SRM 51-31-01-0G. NEW DOUBLER FABRICATED PER DWG #ARB2933 REV 'T'. REPAIR CLASSIFIED AS MAJOR PER GMMSep 15, 2016 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201609143234Seat Track · corrodedMAIN DECK BS 1541 - 1561 X -8.5 SEAT TRACK FOUND WITH CORROSION. CORRODED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1531 TO STA 1591 X=-8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 14, 2016 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609143233Seat Track · corrodedMAIN DECK BS 1831, X 27 SEAT TRACK FOUND WITH SURFACE CORROSION. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1811 TO STA 1884 X=27 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 14, 2016 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609143228Seat Track · damagedMAIN DECK BS 685, X -8.5 SEAT TRACK FOUND WTH DAMAGED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 665 TO STA 765 X=-8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 14, 2016 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609143227Doubler · crackedLEFT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 665 FOUND CRACKED. BEADED DOUBLER REPAIRED PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 14, 2016 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201609143226Doubler · crackedLT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 731 FOUND CRACKED. CRACKED BEADED DOUBLER REPAIRED PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 14, 2016 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201609143225Doubler · crackedLEFT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 766 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR NR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 14, 2016 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201609143224Doubler · crackedLEFT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 770 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR NR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 14, 2016 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201609143223Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 792 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR NR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 14, 2016 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201609143222Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 665 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR NR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 14, 2016 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201609143221Doubler · crackedLEFT WING FIXED LEADING EDGE LOWER FORWARD DOUBLER AT XOS 489 FOUND CRACKED. R & R WITH NEW FABRICATED DOUBLER IAW SRM 51-31-01-0G. NEW DOUBLER FABRICATED IAW DWG ARB2933 REV-T. REPAIR CLASSIFIED AS MAJOR IAW GMM 6- 2-100.Sep 14, 2016 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201609143220Doubler · crackedLEFT WING FIXED LEADING EDGE LOWER FORWARD DOUBLER AT XOS 547 FOUND CRACKED. R & R WITH NEW FABRICATED DOUBLER IAW SRM 51-31-01-0G. NEW DOUBLER FABRICATED IAW DWG ARB2933, REV-T. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 14, 2016 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201609093155Doubler · chafedFORWARD CARGO STA 895.700 BETWEEN LONGERON L-40R TO L-41R DOOR JAMB EXISTING REPAIR DOUBLERS FOUND CHAFED. FORWARD CARGO STA 895.700 BETWEEN LONGERON L40R TO LONGERON L41R DOOR JAMB EXISTING REPAIR DOUBLERS CHAFED MARKS REPAIRED IAW EA NR 1-5330-T0311886B, PTSep 9, 2016 · N616FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201609093156Trunnion · crackedNOSE LANDING GEAR WHEEL WELL RT TRUNNION SUPPORT FITTING SUSPECT CRACKED BS 595. REPAIRED IAW SRM 53-10-14-2R, FIG 202, REPAIR 2.Sep 9, 2016 · N616FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201606292179Door · stuckDURING PREFLIGHT, R-1 DOOR WOULD NOT OPEN.Jun 29, 2016 · N616FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201606141996Limit Switch · malfunctionedRIGHT FORWARD PASSENGER DOOR WILL CLOSE, BUT WILL NOT OPEN ELECTRICALLY. R & R GIRT BAR LIMIT SWITCH AND POWER INTERLOCK SWITCH IAW AMM 52-11-02-5. OPS CHECK GOOD. ACFT OK FOR SERVICE.Jun 14, 2016 · N616FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201512194044Switch · malfunctionedENROUTE, AT :50 MINUTES INTO FLIGHT, RECEIVED LVL 2 AVIONICS AIR FLOW OFF. AS SOON AS QRH WAS REFERENCED LVL 2 WENT OUT. CONTROLLER PUT AVIONICS FAN IN OVERRIDE. WHEN THAT HAPPENED LVL 2 WENT OUT, LVL 1 AVIONICS FAN OVRD ON. SAT COMM WITH GOC & MX. AIR TUDec 19, 2015 · N616FE · Doug MD11F · Air Distribution SystemSDR FDEA201510153230Door · missingDURING POST FLIGHT WALK AROUND, FOUND THE NR 1 OTBD THRUST REVERSER BLOCKER DOOR MISSING & ATTACH STRUCTURE BROKEN. ALSO TRANS COWL DAMAGED FROM DOOR. INSTALLED NR 1 ENG LT OTBD TRANSLATING COWL IAW M 78 3116 41. THE 3 LOWER BLOCKER DOORS ARE INSTALLED UP Oct 15, 2015 · N616FE · Doug MD11F · Engine Thrust ReverserSDR FDEA201506282109Bottle · leakingON ACFT ARRIVAL FOUND L1 DOOR SLIDE BOTTLE EMPTY. R&R BOTTLE PER AMM 25-61-01-4.Jun 28, 2015 · N616FE · Doug MD11F · Escape Slide
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