N602FE

Service difficulty reports · 506

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 = 'N602FE' 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 FDEA201607032238Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 755, X=47.5 FOUND CRACKED AS MARKED. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 3, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607032237Bushing · corrodedLT WING OUTBOARD FLAP VANE FITTING 'B' BUSHING HOLE CORROSION. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.935" X 0.650", FINAL HOLE SIZE: 1.0325" X 0.740", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OJul 3, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607032236Bushing · corrodedLEFT WING OTBD FLAP VANE FITTING C, BUSHING HOLE CORRODED. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.856" X 0.597", FINAL HOLE SIZE: 0.997" X 0.704", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OVERSIJul 3, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607032235Bushing · corrodedLT WING OTBD FLAP VANE FITTING D, BUSHING HOLE, CORRODED. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.876" X 0.580", FINAL HOLE SIZE: 0.953" X 0.660", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OVERSIZJul 3, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607032234Beam · corrodedCABIN MAIN DECK CARGO COMPARTMENT. R3 DOOR PLUG NR 7 LOWER DOOR BEAM DAMAGED.Jul 3, 2016 · N602FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201607032233Floor Support · corrodedMAIN DECK, AFT CABIN RT FLOOR SUPPORT AT STA 1887 -STA 2007, X=-57 FOUND CORROSION AS MARKED.Jul 3, 2016 · N602FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201607032232Hinge Bracket · corrodedLEFT WING OTBD FLAP, FLAP SIDE, INBD AFT HINGE PIVOT INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT CMM 57-52-04. EXISTING HOLE: DIA 1.154", FINAL HOLE: DIA 1.217", MAXIMUM ALLOWABLE HOLE: DIA 1.150". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA1Jul 3, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607012220Skin · crackedTWO CRACK INDICATIONS APPROXIMATE 2.0 INCHES IN LENGTH FOUND DURING X-RAY INSPECTION AT STA 6-0, LONGERON SPLICE 4R AFT SECTION EDGE.Jul 1, 2016 · N602FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201607012219Hinge · corrodedLEFT HAND WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE LOWER MOUNT OUTBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.706", FINAL HOLE DIA: 0.728", MAXIMUM ALLOWABLE HOLE DIA: 0.709". REPAIR BUSHING FABJul 1, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607012218Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE LOWER MOUNT INBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE: DIA 0.706", FINAL HOLE: DIA 0.728", MAXIMUM ALLOWABLE HOLE: DIA 0.709". REPAIR BUSHING FABRICATEDJul 1, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607012217Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE UPPER MOUNT OUTBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.950", MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICAJul 1, 2016 · N602FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR FDEA201607012216Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE UPPER MOUNT INBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.950", MAXIMUM ALLOWABLE HOLE DIA: 0.944", REPAIR BUSHING FABRICATEDJul 1, 2016 · N602FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR FDEA201607012215Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE PIVOT HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 2.311", FINAL HOLE DIA: 2.317", MAXIMUM ALLOWABLE HOLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTAJul 1, 2016 · N602FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR FDEA201607012214Hinge · corrodedRIGHT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE: DIA 1.330", FINAL HOLE: DIA 1.336", MAXIMUM ALLOWABLE HOLE: DIA 1.220". OVERSIZE BUSHING FABRICATED Jul 1, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607012213Hinge · corrodedRIGHT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT INBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE: DIA 1.330", FINAL HOLE: DIA 1.336", MAXIMUM ALLOWABLE HOLE: DIA 1.220". OVERSIZE BUSHING FABRICATED IAW Jul 1, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607012212Hinge · corrodedLEFT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.294", FINAL HOLE DIA: 1.327", MAXIMUM ALLOWABLE HOLE DIA: 1.220", OVERSIZE BUSHING FABRICATED ANDJul 1, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607012211Hinge · corrodedLEFT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT INBOARD HOLE BORE CORRODED. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM57-52-03. EXISTING HOLE DIA: 1.294", FINAL HOLE DIA: 1.327", MAXIMUM ALLOWABLE HOLE DIA: 1.220". OVERSIZE BUSHING FABRICATEDJul 1, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607012210Bracket · corrodedLEFT HAND WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE ACTUATOR OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.219", FINAL HOLE DIA: 1.235" MAXIMUM ALLOWABLE HOLE DIA: 1.220". OVERSIZE BUSHING FABRICATJul 1, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201606302203Seat Track · corrodedMAIN DECK CARGO RT FLOOR SEAT TRACK AT STA 492, X=-27.5, FOUND CORROSION AS MARKED.Jun 30, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201606302202Seat Track · damagedMAIN DECK CARGO LT FLOOR SEAT TRACK AT STA 1801, X= 47.5. FOUND CROWN DAMAGED AS MARKED.Jun 30, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201606302201Seat Track · damagedMAIN DECK CARGO LT FLOOR SEAT TRACK AT STA 5-27, X= 47.5. FOUND CROWN DAMAGED AS MARKED.Jun 30, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201606302200Seat Track · damagedMAIN DECK CARGO LT FLOOR SEAT TRACK AT STA 1259, X= 47.5, FOUND CROWN DAMAGED AS MARKED.Jun 30, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201606302199Seat Track · damagedMAIN DECK CARGO RT FLOOR SEAT TRACK AT STA 5-53, X=-47.5. FOUND CROWN DAMAGED AS MARKED.Jun 30, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201606302198Floorbeam · corrodedCENTER CARGO FLOORBEAM UPPER SURFACE FOUND WITH CORROSION AT STA 1701, X=-18 TO X=-24.Jun 30, 2016 · N602FE · Doug MD11F · Fuselage Main, Floor BeamSDR FDEA201606292189Hinge · corrodedLT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, EXISTING HOLE DIA: 1.249", FINAL HOLE DIA: 1.252" MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLEDJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292188Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE D: 0.420", FINAL HOLE D: 0.423", MAXIMUM ALLOWABLE HOLE D: 0.391". REPAIR BUSHING FABRICATED AND INSTALLED IJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292187Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.420", FINAL HOLE: DIA 0.423", MAXIMUM ALLOWABLE HOLE: DIA 0.391". REPAIR BUSHING FABRICATED AND INJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292186Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE SURFACE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.400", MATERIAL REMOVED: 0.006", FWD FACE; 0.023", AFT FACE, REMAINING THICKNESS: 0.371". MINIMUJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292185Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.419", MATERIAL REMOVED: 0.006", FWD FACE; 0.006", AFT FACE, REMAINING THICKNESS: 0.389". MINIMUM Jun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292184Hinge · corrodedLT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.614", FINAL HOLE DIA: 0.620", MAXIMUM ALLOWABLE HOLE DIA: 0.584". REPAIR BUSHING FABRICATED IAW EA: 1Jun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292183Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.614", FINAL HOLE DIA: 0.620", MAXIMUM ALLOWABLE HOLE DIA: 0.584". REPAIR BUSHING FABRICATED IAW EAJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292182Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.946". MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICATED AND INSTAJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292181Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.946". MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICATED BY MACHJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292180Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE PIVOT HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 2.311". FINAL HOLE DIA: 2.316". MAXIMUM ALLOWABLE HOLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTALLED IAWJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606282177Screw · defectiveCABIN DOOR WOULD NOT ARM AT PUSHBACK. FOUND DOOR CABLE BRACKET LOOSE. REPLACED HARDWARE FOR BRACKET. L1 DOOR OPS CK GOOD AND ARMS. REF AMM 52-11-02-6, FOUND DOOR CABLE BRACKET LOOSE. REPLACED HARDWARE FOR BRACKET. L1 DOOR OPS CK GOOD & ARMS, REF AMM 52-1Jun 28, 2016 · N602FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201606141999Cover · unsecureLEFT ENTRANCE DOOR, L1 WILL NOT ARM, JAMMED LEVER. RESECURED SLIDE COVER IAW MM 25-61-15-4. OPS CHECK GOOD, ACFT OK FOR SERVICE.Jun 14, 2016 · N602FE · Doug MD11F · Emergency EquipmentSDR FDEA201606041827Block · wornINTERMITTENT SLAT DISAGREE ON APPROACH, WENT AROUND. FOLLOWED QRH, NO SLAT & FLAPS 28 DEGREE LANDING. 194 WAS APPROACH SPEED. R & R FWD ATTACH NR 12 BOLT & ATTACHING HARDWARE IAW AMM. R & R L4B SLAT POSITION SENSOR IAW AMM 27-84-03-4. SENSOR STILL REQUIREJun 4, 2016 · N602FE · Doug MD11F · Leading Edge DevicesSDR FDEA201604061146Girt Bar · out of adjustLEFT CABIN DOOR SLIDE WILL NOT ARM WHEN CLOSED. READJUSTED GIRT BAR IAW MM 52-10-01-2. PERFORMED TEST IAW RMM 52-10-01-2.Apr 6, 2016 · N602FE · Doug MD11F · Emergency EquipmentSDR FDEA201603090875Pump · leakingAPPROXIMATELY 50 MINUTES INTO FLIGHT, ANNUNCIATION, HYD 3 OFF. HYD 3 SYS SHOWED 2.0 AT THAT TIME. LEVEL CONTINUED TO DECREASE UNTIL 0.0. RECEIVED ANNUNCIATION, HYD 3 FAIL. USED ALTERNATE GEAR EXTENSION. TROUBLE SHOT ITEM & FOUND LEAK COMING FROM INBD STMar 9, 2016 · N602FE · Doug MD11F · Hydraulic Pump (Electric/Engine), MainSDR FDEA201601270362Girt Bar · out of adjustL1 DOOR EMER SLIDE GIRT BAR WOULD NOT ENGAGE IN DOOR JAMB. UPON INSPECTION, FOUND GIRT BAR DISENGAGED FROM ITS LOCATOR PIN ON SLIDE PACK. RE-CENTERED GIRT BAR, PERFORMED OPERATIONAL TEST OF L1 DOOR SLIDE IAW AMM 52-10-01-2. TESTED OK ACFT OK FOR SERVICE.Jan 27, 2016 · N602FE · Doug MD11F · Emergency EquipmentSDR FDEA201601030010Packing · deterioratedHYD 1 OFF, LEVEL 1 ALERT 2, 30 HOURS INTO FLIGHT AT FL 380, HYD SYS 1 INDICATING 2.8 GALS. FOUND HYD LEAK AT SYS 1 PRESS TRANSDUCER. FURTHER TROUBLESHOOTING FOUND PACKING DETERIORATED AT FITTING SIDE, REMOVED SYS 1 PRESS TRANSDUCER. R & R PACKING ON FITTINGJan 3, 2016 · N602FE · Doug MD11F · Hydraulic System, MainSDR FDEA201511063504Girt Bar · out of positionUNABLE TO ARM L1 DOOR. REPOSITIONED L1 GIRT BAR IAW AMM 52-10-01-2. ACFT OK FOR SERVICE.Nov 6, 2015 · N602FE · Doug MD11F · Emergency EquipmentSDR FDEA201501030013Power Supply · failedDURING EMER LIGHT TEST, GOT A LEVEL 1 EMER LIGHT BATTERY 1 LOW ALERT. REPLACED EMER EXIT LIGHT POWER SUPPLY IAW MM 33-51-01-4 & TESTED OK PER AMM 33-51-01-5.Jan 3, 2015 · N602FE · Doug MD11F · Emergency LightingSDR FDEA201409232734Arming Lever · obstructedL1 DOOR SLIDE ARM LEVER IS DIFFICULT TO MOVE TO THE ARM POSITION AMM SMP. FOUND CORN NUT DEBRIS IN GIRT BAR TO DOOR FRAME AREA, REMOVED DEBRIS & GND TESTED NORMAL IAW MM.Sep 23, 2014 · N602FE · Doug MD11F · Emergency EquipmentSDR FDEA201408062086Skin · damagedTO COMPLY WITH WORK CARD T1-5750-T0302286 PART 2 TITLE WINGS, FLIGHT SURFACES, RT INBD FLAP SKIN DAMAGE. INSTALL PERMANENT REPAIR. EA 1-5750-T0302286 PART 2 TITLE: "WINGS-FLIGHT SURFACES - RT INBD FLAP SKIN DAMAGE" HAS BEEN COMPLIED WITH. REPAIR CLASSFIED Aug 6, 2014 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201407291995Skin · dentedRIGHT WING INBD FLAP UPPER SURFACE FOUND NUMEROUS DENTS. REPAIRED IAW EA 1-5750-T0309945B PT1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.Jul 29, 2014 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201407231926Doubler · crackedRIGHT WING LE LOWER ACCESS COMPARTMENT BEADED DOUBLER FOUND CRACKED XORS 695 DURING OTBD SLAT DRIVE CABLE INSPECTION. REPAIRED IAW SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 56 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.Jul 23, 2014 · N602FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201407201872Skin · crackedLEFT FUSELAGE NR 1 AIR CONDITIONING COMPARTMENT DOOR CUT OUT UPPER AFT CORNER SKIN FOUND CRACK ABOUT 1 INCH IN LENGTH. DOOR CUTOUT UPPER AFT CORNER SKIN CARRIED OUT REPAIR AS PER SRM 53-20-15 REPAIR 3 FIGURE 201 REV 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2Jul 20, 2014 · N602FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201401110084Seal · leakingFUEL STREAMING FROM BOTTOM OF NR 1 ENGINE. LEAK COMING FROM BETWEEN NR 1 ENG FUEL PUMP & HEAT EXCHANGER. R & R SEAL BETWEEN FUEL PUMP & FUEL OIL HEAT EXCHANGER. WET MOTOR, NO LEAKS NOTED. RAN NR 1 ENGINE NO LEAKS NOTED IAW MM 73-12-01-4-1 & JRH. DURING Jan 11, 2014 · N602FE · Doug MD11F · Engine Fuel DistributionSDR FDEA201401050021Light · inoperativeR1 DOOR PRESS TO TEST LAMP INOPERATIVE. R & R BULBS IAW AMM CHAPTER 25-61-04-4. OPERATIONS CHECKED GOOD.Jan 5, 2014 · N602FE · Doug MD11F · Emergency Equipment
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