Boeing MD-11F

Service difficulty reports · 31,320

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'MD11F'
  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 FDEA201909222317Skin · corrodedAFT ACCESSORY COMPARTMENT STA 2144 TO STA 2164 RT LONGERON 39 - 43 EXFOLIATION CORROSION ON SKIN AND AROUND NUTPLATES. PERFORMED FUSELAGE SKIN REPAIR IN REF TO SRM 53-70-01, REPAIR # 3.Sep 22, 2019 · N631FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201909202783Spar Cap · corrodedLEFT WING REAR SPAR UPPER CAP. SHOWING LIGHT SURFACE CORROSION ON CAP SURFACE. FROM APPROX. WING STA. XORS1050 - XORS1060 AREA MARKED DOT 60 REPAIRED PER EA 1-5710-T0350190 WING- BASIC WING STRUCTURE- LH WING REAR SPAR UPPER CAP AFT LEG- REWORK.Sep 20, 2019 · N528FE · Doug MD11F · Wing SparSDR FDEA201909202290Computer · faultyON CLIMBOUT BEFORE GEAR RETRACTION, RECEIVED A LEVEL-2 TIRE FAILURE WITH AURAL WARNING. DID NOT RETRACT THE GEAR. RAN QRH FOR LEVEL 2 TIRE FAILURE. DECLARED AN EMERGENCY AND RETURNED TO KEWR. R&R #9 MLG WHEEL TIRE PRESSURE TRANSDUCGER IAW AMM 32-46-03-4 AND R&Sep 20, 2019 · N613FE · Doug MD11F · Landing Gear Brake SystemSDR FDEA2019110792887Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1225 LBL 42-45. STRUCTURE EXFOLIATED. ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.Sep 19, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA2019110792886Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1225 LBL 36-37. STRUCTURE EXFOLIATED. ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.Sep 19, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA2019110792884Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1225 LBL 18-20. STRUCTURE EXFOLIATED. ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.Sep 19, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201909192286Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. RESep 19, 2019 · N584FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201909192285Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPASep 19, 2019 · N584FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201909192284Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPASep 19, 2019 · N584FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201909192283Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAISep 19, 2019 · N584FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201909182754Skin · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1270 AT RBL 105 STRUCTURE EXFOLIATED REPAIRED CORROSION FOUND AT UPPER CARGO COMP UNDER FLOOR AREA NEAR STATION 1270 RBL105 REF E.A 1-5730-T0350234 P1. TITLED "WING-PLATES AND SKINS-CENTER WING- UPPER SKIN-REWORK" ALSep 18, 2019 · N528FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201909182752Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1260 AT RBL 105 STRUCTURE EXFOLIATED. REPAIRED CORROSION FOUND AT UPPER CARGO COMP UNDER FLOOR AREA NEAR STATION 1260 RBL105 REF E.A 1-5730-T0350234 P1. TITLED "WING-PLATES AND SKINS-CENTER WING- UPPER SKIN-REWORK" ASep 18, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201909182704Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1210 AT RBL 105 STRUCTURE EXFOLIATED. REPAIRED UPPER CARGO COMP FLOOR CORROSION AT STATION 1210 RBL105 REF E.A 1- 5730-T0350234 P2. TITLED "WING-PLATES AND SKINS-CENTER WING-UPPER SKIN-REWORK" ALONG WITH JPF ITEMS 1 Sep 18, 2019 · N528FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2019121382687Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1235 AT LBL 106 STRUCTURE EXFOLIATED.Sep 18, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201909182281Relay · unknownLEVEL 1 EMERGENCY PWR ON IN FLIGHT, COMPLIED WITH QRH, ALERT REMAINED ON. DEPLOYED ADG PER QRH WITH MOCC CONCURRENCE CHECKED ASSOCIATED WIRING FROM OVERHEAD ELECTRICAL PANEL TO EPCU AND FROM R2-17 TO R2-5411. NO DEFECTS NOTED. REPLACED R2-17 AND R2-5411. PERFOSep 18, 2019 · N595FE · Doug MD11F · AC Generation SystemSDR 9WGA2019091809Spar · corrodedRT WING OUTBOARD AFT TRAILING EDGE SPAR CORROSION PULLING THRU FASTENERS STA. XORS 433.00- XORS 418.60. NON-ROUTINES 1573, 1574.Sep 18, 2019 · N543JN · Doug MD11F · Wing SparSDR 9WGA2019091808Attach Fitting · corrodedFWD CARGO COMPARTMENT LT SIDE WALL ATTACHMENT FRAME STA. 899, 919, 939 HAS CORROSION. NON-ROUTINES 1514, 1515, 1516. REMOVED AND REPLACED ATTACH FRAMES.Sep 18, 2019 · N543JN · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201909172267Spar · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT PRINCIPAL STRUCTURAL ELEMENT SPAR, LOWER VERTICAL STABILIZER AND FOUND CRACK INDICATION AT RIGHT HAND STATION 2164 FORWARD FLANGE OF THE REAR UPPER SPAR. LOWER VERTICAL STABILIZER AT RIGHT HAND STATION 2164Sep 17, 2019 · N586FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA201909172266Spar · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT PRINCIPAL STRUCTURAL ELEMENT SPAR, LOWER VERTICAL STABILIZER AND FOUND CRACK INDICATION AT LEFT HAND STATION 2164 FORWARD FLANGE OF THE REAR UPPER SPAR. LOWER VERTICAL STABILIZER AT LEFT HAND STATION 2164 FSep 17, 2019 · N586FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA2019102472735Skin · dentedUPPER FUSELAGE RHS, APPROX STA 1761 LONGERON NO. 9, SKIN DENTED, MARKED. REMOVED DENT AND REPAIRED AREA REF SRM 53-00-01-2R FIG. 201 SHEETS 2 AND 3, AND SRM51-31-01.Sep 17, 2019 · N528FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201909172260Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND ORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-52-03. REPAISep 17, 2019 · N584FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201909172259Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND ORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-52-03. REPAIRSep 17, 2019 · N584FE · Doug MD11F · Trailing Edge FlapsSDR IPXA2019091846966Bottle · lowINSPECTION TYPE:N/A L1 DOOR EMERGENCY BOTTLE LOW. SERVICED THE L1 DOOR PNEUMATIC STORAGE SYSTEM.Sep 17, 2019 · N294UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA201909172274Access Panel · crackedRT WING FUEL ACCESS PANEL AT XORS 685-702 HAS 6 EA OPEN HOLES AT 11 T0 12 O'CLOCK AND 5 O'CLOCK POSITIONS (HOLES 8,11,28,31,32 AND 34) WITH CRACK INDICATIONS. REPAIRED 6 EA CRACKED HOLES REF SRM 57-20-02-2R PG 30.Sep 17, 2019 · N528FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201909172273Access Panel · crackedLT WING FUEL ACCESS PANEL AT XORS 700 HAS 2 EA OPEN HOLES AT 5 O'CLOCK POSITION (HOLES 30 AND 31) WITH CRACK INDICATIONS. REPAIRED 2 EA CRACKED HOLES REF SRM57-20-02-2R PG 30.Sep 17, 2019 · N528FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201909162255Smoke Detector · false activationPDIS 592 26-12 3896 14SEP19 MEM FACT U LOGPAGES:2863413 CABIN SMOKE DETECT @ 9000 FT SHGN 14SEP19 11:38 MEM U PERFORMED GVI OF CARGO SMOKE DETORS, ALL DISPLAYED GREEN. PERFORMED OPERATIONAL TEST OF CARGO SMOKE SYSTEM, REF AMM 26-15-1-5. NO Sep 16, 2019 · N592FE · Doug MD11F · Smoke DetectionSDR FDEA2019091762683Doubler · crackedR/H CENTER LANDING GEAR WHEEL WELL FWD KEEL BEAM MACHINE DOUBLER (AEA0526)HAS A CRACK ON THE AFT ANGLE BETWEEN THE FASTENER HOLES. REMOVED AND REPLACED MACHINE DOUBLER IN REF TO DWG AEA0526 AND SRM 51-31-01.Sep 16, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA2019101762676Former · crackedLEFT WING - FORWARD SPAR - SUPPORTING STRUCTURE IS CRACKED AFT/OUTBOARD OF FUELING PANEL (MARKED). STOP DRILLED CRACK AND INSTALLED A .090 REPAIR DOUBLER IAW SRM 57-00-00 FIG 209 SHEET 1.Sep 16, 2019 · N631FE · Doug MD11F · Wing SparSDR FDEA2019101462640Doubler · crackedLEFT CENTER LANDING GEAR WHEEL WELL FWD KEEL BEAM DOUBLER WAS CRACKED ON THE AFT ANGLE BETWEEN THE FASTENER HOLES. REMOVED AND REPLACED PER DWG AEA0526Sep 16, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201909162250Doubler · chafedCABIN MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR FOUND EDGE CHAFED AT LEFT HAND STATION 535, LONGERON 24 LEFT. CABIN - MAIN DECK CARGO COMPARTMENT FRAME AT LEFT HAND LONGERON 24L CARRIED OUT OUTER ANGLE REPAIR IAW SRM 53-20-07-2R. REPAIR CLASSIFIED AS MSep 16, 2019 · N624FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201909162249Doubler · chafedCABIN MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR FOUND EDGE CHAFED AT LEFT HAND STATION 535, LONGERON 19 LEFT. CABIN- MAIN DECK CARGO COMPARTMENT FRAME AT LEFT HAND LONGERON 19 LEFT CARRIED OUT OUTER ANGLE REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-Sep 16, 2019 · N624FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201909162251Finger Doubler · detachedLEFT HAND WING PANEL 541 KB ACCESS UPPER FORWARD AT REAR SPAR AREA FINGER DOUBLER FOUND DETACHED XW 375.340 - XW 400.340. REPAIR CARRIED OUT AT LEFT HAND WING PANEL 541KB ACCESS UPPER FORWARD AT REAR SPAR FINGER DOUBLER AT XW 375.340 - XW 400.340 AS PER SRM 57Sep 16, 2019 · N624FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201909162252Finger Doubler · delaminatedRIGHT HAND WING PANEL 641 KB ACCESS UPPER FORWARD AT REAR SPAR AREA FINGER DOUBLER FOUND DETACHED BETWEEN XW 375.340 - XW 400.340. REPAIR CARRIED OUT AT RIGHT HAND WING PANEL 641KB ACCESS UPPER FORWARD AT REAR SPAR AREA FINGER DOUBLER AT XW 375.340 - XW 400.34Sep 16, 2019 · N624FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2019102812755Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR AREA NEAR STA 1250 RBL 105 STRUCTURE/AROUND FASTNERS SHOWING EXFOLIATTION AREA MARKED DOT 35 REPAIRED CORROSION FOUND AT UPPER CARGO COMP UNDER FLOOR AREA NEAR STATION 1250 RBL105 REF E.A 1-5730-T0350234 P1. TITLED "WING-PSep 15, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA2019109282753Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR AREA, STRUCTURE/AROUND FASTNERS NEAR STA 1240 AT RBL 105 SHOWING EXFOLIATTION AREA MARKED DOT 39 REPAIRED CORROSION FOUND AT UPPER CARGO COMP UNDER FLOOR AREA NEAR STATION 1240 RBL105 REF E.A 1-5730-T0350234 P1. TITLED "WISep 15, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA2019092152703Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1210 RBL 100 STRUCTURE/AROUND FASTNERS SHOWING EXFOLIATTION. AREA MARKED DOT 34 REPAIRED UPPER CARGO COMP FLOOR CORROSION AT STATION 1210 RBL100 REF E.A 1- 5730-T0350234 P2. TITLED "WING-PLATES AND SKINS-CENTER WISep 15, 2019 · N528FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201909152352Tee Fitting · crackedUPPER CARGO COMPT. SUSPECTED CRACK AT RBL 100 STA 1225 ON T-CORD. WHERE AUUPER AUX ENDS AND JOINS CENTER TANK, ABOVE EXISTING REPAIR REPAIRED UPPER CARGO COMPT T-CHORD CRACK AT RBL 100 STATION 1225 REF E.A # 1-5710- T0349985 P1, TITLED "WING-BASIC WING STRUSep 15, 2019 · N528FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2019110752891Skin · corrodedUPPER CARGO COMPT. UNDER FLOOR AREA, STRUCTURE/AROUND FASTNERS NEAR STA 1225 AT LBL 45 SHOWING EXFOLIATTION AREA MARKED DOT 38 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGSep 15, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA2019110752883Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR AREA, STRUCTURE/AROUND FASTNERS NEAR STA 1225 AT LBL 18 SHOWING EXFOLIATTION AREA MARKED DOT 37 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGESep 15, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA2019110752882Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR AREA, STRUCTURE/AROUND FASTNERS NEAR STA 1225 AT CENTER- LINE SHOWING EXFOLIATTION AREA MARKED DOT 36 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- SSep 15, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201909152248Control Unit · inoperativePDIS 625 24-50 3089 15SEP19 SYD FACT U LOGPAGES:3129175 AT TOP OF CLIMB THE RFO WENT BACK AND FOUND THAT THE COURIER COMPARTMENT LIGHTS WOULD NOT COME ON. ON FURTHER INVESTIGATION FOUND MAIN CARGO OVERHEAD LIGHTS ALSO INOP, TOILET WOULD NOT FLUSH, Sep 15, 2019 · N625FE · Doug MD11F · AC Power Distribution SystemSDR FDEA2019112243018Floor Panel · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1321 AT LBL 106 TUNNEL. STRUCTURE EXFOLIATED DOT 16 REMOVED CORROSION, ALODINED AND FR-PRIMED AREA PER SRM 51-21-01-0G. BLEND OUT AREA IS ACCEPTABLE TO USE AS IS REF E.A # T-1-5730-T0349941 P1. WING PLATES AND SKISep 14, 2019 · N528FE · Doug MD11F · Fuselage Floor PanelSDR FDEA2019102142701Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1321 AT RBL 106 TUNNEL STRUCTURE EXFOLIATED DOT 16 REWORKED AREA I.A.W. E.A # 1-5730-T0350534 WING-PLATES AND SKINS-CENTER WING UPPER SKIN PANEL RHS-REWORK.Sep 14, 2019 · N528FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2019101342689Fuel Tank · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1270 LBL 106 IN TUNNEL AREA STRUCTURE/AROUND FASTNERS SHOWING EXFOLIATTION AREA MARKED DOT 29 REMOVED CORROSION, ALODINED AND FR-PRIMED AREA. PER BOEING BLEND OUT AREA IS ACCEPTABLETO USE AS IS REF SRM 57-10-01Sep 14, 2019 · N528FE · Doug MD11F · Fuselage Floor PanelSDR FDEA2019101392686Skin · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1260 LBL 106 IN TUNNEL AREA STRUCTURE/AROUND FASTNERS SHOWING EXFOLIATTION AREA MARKED DOT 28 REPAIRED PER E.A # T-1-5730-T0350159 TITTLED "WING-PLATES AND SKINS-CENTER TANK UPPER SKIN EXFOLIATION SEVERAL LOCATSep 14, 2019 · N528FE · Doug MD11F · Fuselage Floor PanelSDR FDEA2019110742890Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1225 FROM RBL 75 TO NEAR RBL95 STRUCTURE/AROUND FASTNERS SHOWING EXFOLIATTION AREA MARKED DOT 23 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANSep 14, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA2019110742885Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA. 1225 RBL 62 STRUCTURE EXFOLIATED DOT 15 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.Sep 14, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA2019110742881Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1225 LBL 32 SHOWING EXFOLIATION ON STRUCTURE/AROUND FASTNERS AREA MARKED DOT 26 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.Sep 14, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA2019110742880Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1225 FROM RBL 25 TO NEAR RBL45 STRUCTURE/AROUND FASTNERS SHOWING EXFOLIATTION AREA MARKED DOT 25 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANSep 14, 2019 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA2019110742879Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1225 FROM RBL 60 TO NEAR RBL 75 STRUCTURE/AROUND FASTNERS SHOWING EXFOLIATTION AREA MARKED DOT 24 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PASep 14, 2019 · N528FE · Doug MD11F · Fuselage Main, Structure
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