Boeing MD-11F

Service difficulty reports · 31,320

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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"

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SDR IPXA2016040701789Floor Panel · delaminatedINSPECTION TYPE:2C, MAIN DECK FLOOR PANEL WSP0825-19 DELAMINATED. REMOVED FABRICATED AND INSTALLED REPLACEMENT FLOOR PANEL IAW DWG WSP0825 AND MD11-5320-27386-C.Mar 31, 2016 · N256UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2016040701788Floor Panel · delaminatedINSPECTION TYPE:2C, MAIN DECK FLOOR PANEL WSP 0825-41 DELAMINATED. REMOVED FABRICATED AND INSTALLED REPLACEMENT FLOOR PANEL IAW DWG WSP0825 AND 5320-27386-C.Mar 31, 2016 · N256UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2016040701787Floor Panel · delaminatedINSPECTION TYPE:2C, MAIN DECK FLOOR PANEL, WSP 0825-50 DELAMINATED. REMOVED FABRICATED AND INSTALLED REPLACEMENT FLOOR PANEL IAW DWG WSP0825 AND MD11-5320-27386-C.Mar 31, 2016 · N256UP · Doug MD11F · Fuselage Floor PanelSDR FDEA201603311124Stiffener · crackedAGEING ACFT, UPON REMOVAL OF STIFFENER AT LT WING LE STATION XOS 542, FOR ACCESS FOUND CRACKED. REFER SNRM N00744. R&R STIFFENER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 31, 2016 · N594FE · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2016041702220Floor Panel · corrodedINSPECTION TYPE:2C, RCB FLOOR PANEL WSP0785-502 CORRODED ON UPPER SURFACE BS 475-500, X=27 -36. REPAIRED NOTED FLOOR PANEL IAW EA 011-5320-01-A6206, REV IR AND EO MD11-5320-60498-A.Mar 30, 2016 · N256UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2016041702219Floor Panel · corrodedINSPECTION TYPE:2C, RCB FLOOR PANEL WSP 0785-501 CORRODED ON UPPER SURFACE BS 475-500 X=19 - 27. REPAIRED NOTED FLOOR PANEL IAW EA 011-5320-01-A6206, REV IR AND EO MD11-5320-60498-A.Mar 30, 2016 · N256UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2016033101455Line · leakingENGINE FAIL LIGHT ON T/O ROLL. REJECT ACCOMPLISHED DUE TO ENGINE MONITORING DATA SHOWING LOW PB PRESSURE NR 2 ENGINE, PERFORMED ENGINE CHECK 3, PB SENSE LINES. FOUND NR 2 ENGINE PB FLEX, PN 51U78 HAS SEVERE AIR LEAK. REPLACED LINE, PERFORMED ACCEL/DECEL TESTMar 30, 2016 · N296UP · Doug MD11F · Engine (Turbine/Turboprop)SDR IPXA2016033101436Indicator · inoperativeRIGHT SLIDE PRESSURE TO TEST LIGHT INOPERATIVE. R & R PRESSURE INDICATOR REMOTE KIT IAW AMM 25-61-04,Mar 30, 2016 · N273UP · Doug MD11F · Escape SlideSDR FDEA201603301119Power Supply · inoperativeEMERGENCY LIGHT BATTERY 1 LOW. R & R EMER EXIT LIGHTS POWER SUPPLY IAW 33-51-01-5. OPERATIONS CHECKED NORMAL AT THIS TIME. OK FOR SERVICE.Mar 30, 2016 · N617FE · Doug MD11F · Emergency LightingSDR FDEA201603301118Skin · crackedONE EACH FASTENER HOLE NR 6 FOUND CRACK INDICATION, DURING OPEN HOLE HFEC INSPECTION, AT LT WING LOWERS SKIN ACCESS DOOR CUT OUT, BETWEEN STATION XORS 690 - XORS 700. REPAIRED IAW SRM 57-20-02-2R FIG 201 REPAIR 5. INITIAL INSPECTION TO BE CARRIED OUT AT 2,000Mar 30, 2016 · N612FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201603291095Skin · damagedAGEING ACFT, EXISTING REPAIR AT LT WING, INBD FLAP LOWER SEGMENT, UPPER SKIN STATION, XIFH 153.30 - XIFH 195.30. EXISTING REPAIR EVALUATED & FOUND REPAIR SKIN WITH NEW DAMAGE. REPAIR CARRIED OUT IAW SRM 57-00-01 REPAIR 2 FIG 201. REPAIR CLASSIFIED AS MAJOR Mar 29, 2016 · N594FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201603291115Girt Bar · obstructedL1 DOOR SHOWS OPEN ON STATUS PAGE WHEN CLOSED & SLIDE ARMED. CLEARED DEBRIS FROM GIRT BAR AREA. OPERATIONS CHECKED IAW MM 52-11-02-2. OK FOR SERVICE.Mar 29, 2016 · N583FE · Doug MD11F · Emergency EquipmentSDR FDEA201603291113Skin · corrodedAFT ACCESSORY COMPARTMENT, RT SKIN WITH ANCHOR NUT ATTACH, FWD OF STATION 2164, FOUND CORROSION. SKIN REPAIRED PER SRM 53-70-01-2R FIG 201 REPAIR NR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Mar 29, 2016 · N612FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201603291112Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORRODED. REWORKED FOUND EXCEEDED LIMITS IAW CMM 57-52-04. EXISTING HOLE DIAMETER 1.193", FINAL HOLE DIAMETER 1.196, MAXIMUM ALLOWABLE HOLE DIAMETER 1.15". NEW REPAIR BUSHINGMar 29, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603291111Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.190", FINAL HOLE DIAMETER 1.225" & MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR Mar 29, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603291110Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.215", FINAL HOLE DIAMETER 1.250", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABRMar 29, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603291109Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.255", FINAL HOLE DIAMETER 1.285", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABMar 29, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603291108Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.257", FINAL HOLE DIAMETER 1.283", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABRIMar 29, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603291107Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE, FOUND CORRODED. CORROSION REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.248", FINAL HOLE DIAMETER 1.283", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUMar 29, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603291106Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.216", FINAL HOLE DIAMETER 1.226 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220Mar 29, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603291104Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.704", FINAL HOLE DIAMETER 0.737 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.709".Mar 29, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603291103Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, UPPER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.957", FINAL HOLE DIAMETER 0.961 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.944".Mar 29, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603291102Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.222", FINAL HOLE DIAMETER 1.228 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220Mar 29, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603291101Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.284", FINAL HOLE DIAMETER 1.289 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220Mar 29, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603291097Frame · chafedCABIN MAIN DECK CARGO COMPARTMENT, FRAME CHAFED AT RT STATION 535, LONGERON 24R. REPAIRED IAW SRM 53-20-07-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 29, 2016 · N594FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201603291096Frame · chafedCABIN MAIN DECK CARGO COMPARTMENT, FRAME CHAFED AT RT STATION 535, LONGERON 19R. REPAIRED IAW SRM 53-20-07-2R FIG 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 29, 2016 · N594FE · Doug MD11F · Fuselage Main, FrameSDR IPXA2016042902738Seat Track · corrodedINSPECTION TYPE:2C, MAIN CABIN SEAT TRACK HAS CORROSION BS 495, RBL 36. R & R MAIN CABIN SEAT TRACK BS 439 TO BS 515 AT RBL 36 IAW DWG DAC WSP0826 AND SRM 51-31-01.Mar 28, 2016 · N256UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2016041702221Barrier · crackedINSPECTION TYPE:2C, RIGID CARGO BARRIER WALL HAS A CRACK AT NR 10 FITTING INNNER LOWER CLOSE OUT AREA BS 488 X=72.5 ACCOMPLISHED CRACK REPAIR ON RCB INNER LOWER CLOSEOUT AREA BS 488 X=-72.5 IAW EA 011-5310-01-A6188, REV I/R AND EO MD11-5310-60517-A.Mar 28, 2016 · N256UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016041001908Structure · corrodedINSPECTION TYPE:2C, 2 AREAS OF CORROSION ON RCB FWD SKIN AND ALONG LOWER SURFACE AT X=79. REPAIRED NOTED CORROSION IAW EA 011-5310-01-A6189, REV IR AND EO MD11-5310-60402-A.Mar 28, 2016 · N256UP · Doug MD11F · Fuselage Main, StructureSDR FDEA201603281090Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.588", FINAL HOLE DIAMETER 0.596 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.584".Mar 28, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603281089Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.588", FINAL HOLE DIAMETER 0.596 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.584".Mar 28, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603281088Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SURFACES, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING THICKNESS: 0.412", MATERIAL REMOVED 0.002" & MINIMUM ALLOWABLE THICKNESS 0.423". NEMar 28, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603281087Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD. STUD ATTACH SURFACES FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING THICKNESS 0.420", MATERIAL REMOVED: 0.010" & MINIMUM ALLOWABLE THICKNESS 0.423". NMar 28, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603281086Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44- 08. EXISTING HOLE DIAMETER 0.720", FINAL HOLE DIAMETER 0.737 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.7Mar 28, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603271084Skin · damagedAGEING ACFT, EXISTING REPAIR AT FWD CARGO, FUSELAGE DOOR CUT OUT, FWD JAMB SKIN STATION 895.7, LONGERON 40RT - 41RT. EXISTING REPAIR EVALUATED & FOUND DAMAGED. REPAIR CARRIED OUT IAW EA 1-5330-T0324500A P 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFEMar 27, 2016 · N594FE · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016041502159Doubler · corrodedINSPECTION TYPE:2C, INTERNAL DOUBLER CORRODED BEYOND ALLOWABLE LIMITS, BS 1159, L51 - L52L . REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG NAA6254, SRM 51-21-01, 51-35-01.Mar 27, 2016 · N256UP · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201603271081Doubler · crackedLEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 614. CARRIED OUT REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 27, 2016 · N612FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201603271080Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 830, X=-8.5 FOUND CORROSION. CORRODED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 785 - 907, X = -8.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 27, 2016 · N612FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201603271079Doubler · crackedRIGHT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT XOS 613. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 27, 2016 · N612FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201603271078Doubler · crackedLEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT XOS 543. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 27, 2016 · N612FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201603271077Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE, FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.220", FINAL HOLE DIAMETER 1.223 & MAX ALLOWABLE HOLE DIAMETER 1.220". NEW RMar 27, 2016 · N612FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201603271075Slide Raft · defectiveREPEAT WRITE UP. R1 ESCAPE SLIDE BOTTLE PRESS LIGHT ILLUMINATED DURING CRUISE FLIGHT. FOUND INTERMITTENT CONTINUITY ON ELEC JACK COMING FROM SLIDE RAFT. R & R R1 DOOR SLIDE RAFT. BOTTLE PRESS PTT LIGHT OPERATIONS CHECKED NORMAL.Mar 27, 2016 · N606FE · Doug MD11F · Escape SlideSDR IPXA2016032801318Battery Pack · dischargedDURING COCKPIT PREFLIGHT TEST OF EMERGENCY LIGHT SYS, DISPLAYED "EMERGENCY LIGHT BATTERY 1 LOW, LEVEL 1 ALERT. PERFORMD OPS CK OK IAW MM 33-51-01, P 501.Mar 27, 2016 · N290UP · Doug MD11F · Emergency LightingSDR FDEA201603261076Control Panel · looseUNABLE TO CLOSE DOOR L1. ON ARRIVAL DOOR OPERATED NORMALLY. FOUND INTERIOR CONTROL PANEL LOOSE. OPENED CONTROL PANEL & INSPECTED. NO DEFECTS OR DAMAGE NOTED. SECURED PANEL & OPERATIONS CHECKED NORMAL.Mar 26, 2016 · N583FE · Doug MD11F · Passenger/Crew DoorsSDR IPXA2016041502162Skin · crackedINSPECTION TYPE:2C, RT FIXED L/E EXTERIOR SKIN PANEL 616ET CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PANEL IAW DWG ARB2386 AND SRM 51-31-01.Mar 25, 2016 · N256UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2016041802303Fitting · corrodedINSPECTION TYPE:2C, RCB FLOOR FITTING HAS CORROSION ALONG UPPER EDGES. ACCOMPLISHED BLEND REPAIR ON RCB FLOOR FITTING BS 488 X=8.5 IAW EA 011-5310-01-A6203, REV I/R AND EO MD11-5340-60492-A.Mar 25, 2016 · N256UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2016041802318Fitting · damagedINSPECTION TYPE:C2, RIGID CARGO BARRIER FLOOR FITTING NR 8 HAS AREAS OF EDGE DAMAGE. REPAIRED DAMAGED RCB FLOOR FITTING NR 8 IAW EA 011-5310-01-A6205, REV A AND EO MD11-5340-60491-A.Mar 25, 2016 · N256UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2016041802316Fitting · corrodedINSPECTION TYPE:2C, RCB FLOOR FITTING HAS CORROSION ALONG UPPER EDGES. ACCOMPLISHED BLEND REPAIR ON RCB FLOOR FITTING BS 488 X=27.5 IAW 011-5310-01-A6203, REV I/R AND EO MD11-5340-60492-A.Mar 25, 2016 · N256UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2016041802314Fitting · corrodedINSPECTION TYPE:C2, RIGID CARGO BARRIER FLOOR FITTING NR 7 HAS AREAS OF CORROSION ALONG UPPER EDGES. REPAIRED CORRODED RCB FLOOR FITTING NR 7 IAW EA 011-5310-01-A6205 REV A AND EO MD11-5340-60491-A.Mar 25, 2016 · N256UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2016041802304Fitting · corrodedINSPECTION TYPE:C2, RIGID CARGO BARRIER FLOOR FITTING NR 6 HAS AREAS OF CORROSION ON UPPER EDGES. REPAIRED CORRODED RCB FLOOR FITTING NR 6 IAW EA 011-5310-A6205, REV A AND EO 5340-60491-A.Mar 25, 2016 · N256UP · Doug MD11F · Fuselage Main, Attach Fittings
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