Boeing MD-11F

Service difficulty reports · 31,317

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 FDEA202202250372Pipe · noneLEVEL 2 HYD 1 FAIL DURING CLIMB OUT. HYDRAULIC 1 RESERVOIR QUANTITY INDICATED 0.0 ON THE HYDRAULIC SYNOPTIC. REPAIRED HYDRAULIC LINE USING RYNGLOK METHOD. REF MD-11 AMM 20-10-01-2. LEAK AND OPS CHECKS GOOD. REF Feb 25, 2022 · N583FE · Doug MD11F · Hydraulic Power SystemSDR FDEA202202250370None · leakingPDIS 601 29-02 3869 24FEB22 HNL FACT U HYD 3 ELEV OFF LEVEL 1 APPROX 10 MINUTES AFTER TAKEOFF. HYD 3 LEVEL AT 4.0 AND DECREASING. THEN MOMENTARY HYD 3 OFF LEVEL 1 FOLLOWED BY HYD 3 FAIL LEVEL 2 WITH HYD 3 AT 0.0. COMPLIED WITH QRH, RETURNED TFeb 25, 2022 · N601FE · Doug MD11F · Hydraulic Power SystemSDR FDEA202202230364None · failedL1 DOOR REMOTE PRESSURE INDICATOR PUSH TO TEST LIGHT INOP FOUND SWITCH INSIDE OF REMOTE PRESS SWITCH WAS BAD. REPLACED REMOTE PRESS SWITCH AND WORKS NORMAL.Feb 23, 2022 · N592FE · Doug MD11F · Emergency EquipmentSDR IPXA2022031179985Channel · corrodedINSPECTION TYPE:4CCENTER CARGO ROLLER CHANNEL IS CORRODED BETWEEN STA. 5-123/1531 AND 1701 AT X= -33.REPAIRED CORRODED CENTER CARGO ROLLER CHANNEL BETWEEN STA. 5-123/1531 AND 1701 AT X= -33 IAW VT-SAA EA 011-5350-01-A9504 REV. I/R AND UPS EO MD11-5320-83106-A.Feb 23, 2022 · N278UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2022031179984Channel · damagedINSPECTION TYPE:C4CENTER CARGO ROLLER CHANNEL IS CORRODED BETWEEN STA. 5-103 AND 5-123 AT X= -33.REPAIRED CORRODED CENTER CARGO ROLLER CHANNEL BETWEEN STA. 5-103 AND 5-123 AT X= -33 IAW VT-SAA EA 011-5350-01-A9504 REV. I/R AND UPS EO MD11-5320-83106-A. (MAJOR)Feb 23, 2022 · N278UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2022031079941Hinge Fitting · noneINSPECTION TYPE:4CL/H I/B ELEVATOR HAS A CHAFE DAMAGED ON THE HINGE FITTING.REPAIRED CHAFE ON HINGE FITTING IAW VTSAA EA 011-5520-01-A9502 REV I/R AND UPS EO MD11-5520-83074-A. (MINOR)Feb 23, 2022 · N278UP · Doug MD11F · Elevator Control SystemSDR IPXA2022031079938Spar · corrodedINSPECTION TYPE:C4L/H UPPER WING T/E REAR SPAR HAS CORROSION BETWEEN STA XORS=675.5 TO XORS=754.5REMOVED, REPAIRED THE CORROSION ON L/H UPPER WING T/E REAR SPAR IAW VTSAA EA 011-5710-01-A9503 REV I/R AND UPS MD11-5710-83089-A. (MINOR)Feb 23, 2022 · N278UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2022030879878Slat · damagedINSPECTION TYPE:C4L/H WING #2 SLAT T/E LWR SURFACE O/B EDGE RUBSTRIP IS DAMAGED AT STA XIS=358.005REMOVED, REPAIRED THE DAMAGED ON L/H #2 SLAT T/E RUBSTRIP IAW VTSAA EA 011-5754-01-A9499 REV I/R AND UPS EO MD11-5750-83102-A (MINOR)Feb 23, 2022 · N278UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2022030779835Skin · gougedINSPECTION TYPE:1CLT WING FIXED L/E SKIN GOUGE AT XW 290.5.REMOVED,FABRICATED AND REPLACED GOUGED SKIN IAW MD-11 SRM 51-31-01 ND DWG ARB2386-5 (MINOR).Feb 23, 2022 · N278UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2022030479714Fitting · noneINSPECTION TYPE:1CLH HORIZONTAL STAB ELEVATOR #3 ACTUATOR HINGE SUPPORT FITTING IS CHAFE AT STA XE=122.REPAIRED CHAFED HINGE SUPPORT FITTING IAW VT-SAA EA 011-5510-01-A9501 REV I/R AND UPS EO MD11-5550-83032-A (MINOR).Feb 23, 2022 · N278UP · Doug MD11F · Empennage Flight Control Surfaces, Attach FittingsSDR IPXA2022022879541Skin · noneINSPECTION TYPE:1CLT WING SKIN AROUND ACCESS 536AB CRACK.REPAIRED CRACKED SKIN AROUND ACCESS 536AB IAW MD-11 SRM 57-20-02 REPAIR 5 FIG 201 (MINOR).Feb 23, 2022 · N278UP · Doug MD11F · Wing Miscellaneous StructureSDR 9WGA2022022251201None · noneDISCREPANCY: LOST AUTO PILOT #1, LOST FLIGHT DIRECTOR#1 AND LOST NAVIGATION #1. CORRECTIVE ACTIONS: RTS 22-01-10-741-801 ACCOMPLISHED, ALL TESTS PASSED. FLIGHT DIRECTOR VISIBLE REF AMM 22-10-00-001 AND NAVIGATION TEST PER AMM 22-23-01, OPS CHECK SATIS. NO COMPFeb 22, 2022 · N512JN · Doug MD11F · Autopilot SystemSDR IPXA2022031079950Skin · crackedINSPECTION TYPE:1CCENTER FUSELAGE L-3 DOOR FORWARD JAMB INNER SKIN CRACK BETWEEN STA.1250.75 AND STA, 1256.75.REPAIRED L-3 DOOR FORWARD JAMB INNER SKIN BETWEEN STA.1250.75-1256.75 IAW VT-SAA EA 011-5310-01-A9498 REV I/R AND UPS EO MD11-5310-83008-A BY P.LAU (AFeb 22, 2022 · N278UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2022030579761Stringer · crackedINSPECTION TYPE:C4UPPER CTR AUX TANK HAS CRACK ON A INCOMING SPLCE REPAIR ON STRINGER 48 REPAIR ZEE AT SPLICE LOCATION STA XCW-17 AND XCW=17.REMOVED,FAB, REPAIRED THE CRACK ON STRINGER 48 REPAIR ZEE AT STA XCW=-17 AND XCW=17 IAW VTSAA EA 011-5710-01-A9491 REV Feb 22, 2022 · N256UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2022030579759Stringer · crackedINSPECTION TYPE:C4CTR UPPER AUX TANK HAS A INCOMING SPLICE REPAIR WITH 3EA CRACK ON STRINGER 47 REPAIR ZEES AT SPLICE LOCATION STA XCW=46.5 AND XCW=17.0 AND XCW=17.0 AND BETWEEN XCW=-17.0 AND XCW=-46.5 AND XCW=-81.0 .REMOVED, FAB, REPAIRED THE 3EA CRACK ON STRFeb 22, 2022 · N256UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2022030579756Stringer · crackedINSPECTION TYPE:4CCENTER UPPER AUX TANK HAS INCOMING SPLICE REPAIRS ON STRINGER 50 WITH 2EA REPAIR ZEES AT SPLICE LOCATION XCW=17.0 AND XCW=-17.0 AND BETWEEN STA XCW=-17.0 AND XCW=-46.5 WITH CRACK DAMAGE.REMOVED,FAB,REPLACED, THE CRACK ON 2EA REPAIR ZEES SPLICFeb 22, 2022 · N256UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2022030279611None · noneINSPECTION TYPE:C4MAIN CARGO DECK AT LONGERON 15L TEE-ANGLE IS CRACK AT STA 1341.REMOVED, FAB, REPLACED CRACK TEE-ANGLE IAW MD11 DWG AEA7568 AND MD11 SRM 51-31-01 AND 51-33-01. (MINOR)Feb 22, 2022 · N278UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2022030279612Web · crackedINSPECTION TYPE:4CL-3 DOOR JAMB WEB/ INNER SKIN IS CRACKED AT STA. 1307 & Z= -18.REPAIRED CRACKED L-3 DOOR JAMB WEB/ INNER SKIN AT STA. 1307 & Z= -18 IAW SRM 53-40-15 REPAIR 3 FIG. 201. (MAJOR)Feb 22, 2022 · N278UP · Doug MD11F · Fuselage Main, Attach FittingsSDR 9WGA2022022141201Tail Cone · departedCLIMBING THROUGH 4000 FEET AIRCRAFT HAD AN AIRFRAME VIBRATION. ENGINE PARAMETERS WERE INDICATING NORMAL. AT ARRIVAL MAINTENANCE REPS IDENTIFIED #2 ENGINE MAINTENANCE PLATFORM DOORS DAMAGED. REMOVED TAIL CONE REFERENCE MD-11 AMM 53-52-00. REPLACED DAMAGED TAILFeb 21, 2022 · N412SN · Doug MD11F · Nacelle/Pylon StructureSDR FDEA202202210365Support · corrodedCENTER CARGO COMP: FLOOR SUPPORT AT STA 1781 LBL 8 UNDER FLOOR PANEL 183LG HAVE SIGNS OF CORROSION REMOVED AND REPLACED FLOOR SUPPORT AFA 7115-25 AT CENTER CARGO COMPARTMENT STA 1781 LBL 8 REF. SRM 51-31-01-0G AND SRM 51-33-01-0GFeb 21, 2022 · N528FE · Doug MD11F · Standard Practices/StructuresSDR IPXA2022022379327None · failedINSPECTION TYPE:NA**EMERGENCY DECLARED**REC'D PRIORTY LANDING PATTERN**NO EMERG ACTION ON GRD, A/C LANDED W/OUT INCIDENT**AIR SYS 2 AND AIR SYS 1 BOTH FAILED WITHIN A MINUTE OR SO OF EACH OTHER. ALSO RECEIVED LEVEL 2 "TAIL A-ICE DISAG"PERFORMED RTS OF PNEAUMATFeb 21, 2022 · N255UP · Doug MD11F · Pneumatic Indicating SystemSDR FDEA202202210333Life Raft · failedAFTER LANDING CABIN DOOR 1L MISTAKENLY OPENED WITH EMERGENCY HANDLE. RAFT FELL OUT BUT DID NOT INFLATE. REMOVED 1L DOOR SLIDE RAFT AND INSTALLED 10 MAN LIFE RAFT P/N 5A3210-40621 AS PER MEL 52-10-03-03. PLEASE INSTALL CREW STAIR AT 1R DUE 1L DOOR AND Feb 21, 2022 · N615FE · Doug MD11F · Life RaftSDR IPXA2022030379685None · corrodedINSPECTION TYPE:1CLH O/B FLAP I/B HINGE BRACKET ASSEMBLY LUG HOLE CORRODED AT STA.XW 486.403.REPAIRED CORRODED BRACKET ASSY LUG HOLE IAW VT-SAA EA 011-5753-01-A9490 REV I/R AND UPS EO MD11-5740-82979-A (MINOR).Feb 19, 2022 · N256UP · Doug MD11F · Wing, Attach FittingsSDR IPXA2022030779799Longeron · corrodedINSPECTION TYPE:4CCENTER CARGO LONGERON 49 L/H IS CORRODED BETWEEN STA. 5-113 TO 5-123/1531.REPAIRED CORRODED LONGERON 49L BETWEEN STA. 5-103 TO 5-123/1531 IAW VT-SAA EA 011-5310-01-A9496 REV. I/R AND UPS EO MD11-5310-83065-A. (MAJOR)Feb 18, 2022 · N256UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2022022779458Longeron · noneINSPECTION TYPE:C4CTR CARGO BILGE AREA AT STA 1541 HAS CORROSION ON LONGERON 52.REMOVED,FAB AND REPLACED CORRODED LONGERON 52 IAW DWG AFA7762 AND SRM 51-33-01. (MINOR)Feb 18, 2022 · N256UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2022030479717Skin · corrodedINSPECTION TYPE:4CR/H WING UPPER SURFACE HAS 3EA AREA OF CORROSION BETWEEN STA XORS 480.25 AND XORS 538.49 AND BETWEEN STRINGER 12 AND STRINGER 13.REMOVED, REPAIRED CORROSION AT 3EA AREA IAW VTSAA EA 011-5730-01-A9497 REV I/R AND UPS EO MD11-5730-83050-A (MINOFeb 17, 2022 · N256UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2022022479366Stiffener · noneINSPECTION TYPE:1CLH MLG 3RD VERTICAL STIFFENER CRACK AT LWR END WHEEL WELL.REMOVED AND REPLACED CRACKED STIFFENER IAW MD-11 SRM 51-35-01 AND 51-33-01 (MINOR).Feb 17, 2022 · N256UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2022021879131Sleeve · damagedINSPECTION TYPE:SV#1 ENG. I/B T/R HAS DAMAGED L/E AT 3 OCLOCK POSTIONREMOVED AND REPLACED #1 ENG. I/B T/R SLEEVE IAW MD 11 AMM 78-31-22-00-868 AND AMM 78-31-22-400-868 PN. 221-0503-524 AND SN. 318Feb 17, 2022 · N279UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2022021879150Landing Gear · noneATB SDR FILED OPEN*NO EMERG DEC'D* A/C LANDED W/OUT INCIDENT*AFTER T/O ON INTIAL CLIMB OUT, RAISED GEAR THEN GOT" LANDING GEAR" AURAL WARNING. ALL GEAR INDICATORS SHOWED UP GEAR. T/S 31-51-22-00 BLOCK 8 TO EXAMINE CONNECTOR P1-1111. PERFORMED RINGS OUTS FOR Feb 17, 2022 · N279UP · Doug MD11F · Landing Gear Position and WarningSDR IPXA2022030579762Cap · corrodedINSPECTION TYPE:C4L/H UPPER SURFACE REAR SPAR UPPER CAP HAS CORROISON BETWEEN STA XORS 521.5 TO XORS 541.REMOVED,REPAIRED THE CORROSION ON THE REAR SPAR UPPER CAP IAW VTSAA EA 011-5710-01-A9495 REV I/R AND UPS EO MD11-5730-83064-A. (MINOR)Feb 16, 2022 · N256UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2022022779460Skin · noneINSPECTION TYPE:INCENTER WING BOX UPPER SKIN HAS CORROSION AT STR 15 AND XCW=-81.REMOVED,REPAIRED CORRODED CTR WING BOX UPPER SKIN IAW VTSAA EA 011-5710-01-A9487 REV I/R AND UPS EO: MD11-5730-82934-A. (MINOR)Feb 16, 2022 · N256UP · Doug MD11F · Wing, Plate/SkinSDR FDEA202202160303Splice · crackedCENTER CARGO - STATION 5-113 TO STATION 1541 LONGERON 41 LEFT LONGERON SPLICE FOUND CRACKED. CENTER CARGO - STATION 5-113 TO STATION 1541 LONGERON 41 LEFT CRACKED LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01-0G . LONGERON SPLICE FABRICATED BYFeb 16, 2022 · N576FE · Doug MD11F · Fuselage Main, StructureSDR FDEA202202160322Seat Track · corrodedMAIN CARGO - STA 1368 LBL 50 - SEAT TREACK LOBE HAS CORROSION ON THOP & BOLLOM SIDE OF TRACK (MARKED) MAIN CARGO, STA 1368, LBL 50, SEAT TRACK ATTACH LOBE REPAIR PERFORMED IAW MD 11 SRM 53-00-52-2R REPAIR 5. *MAJOR REPAIR*Feb 16, 2022 · N649FE · Doug MD11F · Fuselage Main, StructureSDR FDEA202202160306None · noneAT 16:25 ZULU MOCC MESSAGED US IN FLIGHT ADVISING US THAT HYD #3 QTY SHOWED 5.8 GALLONS. HYD 3 CONTINUED TO LEAK DOWN UNTIL HYD 3 ELEV OFF ILLUMINATED AND THEN HYD 3 LOW QTY ILLUMINATED. FOUND CENTER LANDING GEAR BRAKE R/H UPPER GLAND Feb 16, 2022 · N529FE · Doug MD11F · Hydraulic Power SystemSDR IPXA2022021779114Light · inoperativeINSPECTION TYPE:N/AEMERGENCY PWR OFF LIGHT IS INOPRELAMPED EMERGENCY PWR OFF LIGHT IAW BOEING SWPM 20-84-18 OPS CHK GOODFeb 16, 2022 · N282UP · Doug MD11F · Emergency LightingSDR FDEA202202150637Duct · delaminated#2 ENG INLET DUCT LH UPR EXT SKIN HAS DELAM AT PREVIOUS REPAIR. MRKD 30 IN FWD OF PNL 361EL REPAIRED PREVIOUSE REPAIR ON #2 ENG INLET DUCT EXTERNAL SKIN ON L/H SIDE 30 INCH FWD OF PANEL 361EL PER SRM 51-62-01-0G PAR.10.J PG.44.Feb 15, 2022 · N649FE · Doug MD11F · Powerplant SystemSDR IPXA2022022579420Web · noneINSPECTION TYPE:1CTAILCONE RH PATIO DOOR WEB (CRACK) DAMAGE UNDER WORK PLATFORM.REPAIRED TAILCONE RH DOOR CRACKED WEB IAW SRM 52-00-00 AND DWG AKC 7861 (MINOR).Feb 15, 2022 · N256UP · Doug MD11F · Service DoorsSDR IPXA2022022779462Intercostal · noneINSPECTION TYPE:C4R/H WHEEL WELL LWR FWD BRAKE ACCUMLATOR INTERCOSTAL IS CRACK.REPAIRED CRACK INTERCOSTAL IAW MD-11 SRM 53-40-12 REPAIR 3 AND SRM 51-33-01 PG8 (MINOR)Feb 15, 2022 · N256UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2022021679058Light · inoperativeINSPECTION TYPE:N/A**SUPPLEMENTAL SDR** EMERGENCY LIGHTS INOP. DEFER EMERGENCY LIGHTS IAW MEL 33-50-4. DMP C/W INSTALLED PLACARD ASSIGNED M772946 TRIED REPLACING POWER SUPPLY, NO HELP. REF MM 33-50-00-700-802. ORIGINAL IS INSTALLEDREVERSED DMP T/S PER WDM 33-5Feb 15, 2022 · N264UP · Doug MD11F · Emergency LightingSDR IPXA2022021679064None · noneINSPECTION TYPE:NA** ATB SDR FILED** NO EMERGENCY DEC'D**A/C LANDED W/OUT INCIDENT** LEVEL 2 "AIR SYS 3 PRES LO" AIR TURN BACK DUE TO ICING COND AT DEST.R&R HIGH STAGE MANIFOLD PRESSURE SENSOR PER AMM 36-12-04-000-801, OPS CHECK, SYSTEM CHECK NORMAL, FOB BEFOFeb 15, 2022 · N270UP · Doug MD11F · Pneumatic Distribution SystemSDR FDEA202202141237Skin · chafedL/H WING FIXED L/E SKIN HAS SHALLOW WEAR FROM SLAT CONTACT BETWWEN SLAT TRACK #1 AND #3. MRKD REPAIRED L/H WING FIXED L/E SKIN FROM SLAT CONTACT BETWWEN SLAT TRACK #1 AND #3 PER MD11 SRM 57-40-02-2R FIG 201 REPIAR 4 SHEET 4.Feb 14, 2022 · N649FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202202140450None · noneCENTER CARGO, STA 1801-1821, LONGERON 46R, AT SLPICE AREA, AFT OUTBOARD VERTICLE SIDE OF LONGERON HAS A CRACK. REPLACED CRACKED LONGERON 46R FROM STA 1811 TO 1828 AND FABRICATED NEW SPLICE REF SRM 53-00-05-2R REPAIR 1 FIGURE 201 AND 202 SHEET 1, 2, AND 3 AFeb 14, 2022 · N649FE · Doug MD11F · Standard Practices/StructuresSDR FDEA202202140293Frame · noneMAIN DECK CARGO COMPARTMENT , LEFT HAND STATION 535 LONGERON 24 LEFT FRAME ATTACHED REPAIR ANGLE FOUND CHAFFED. MAIN DECK CARGO COMPARTMENT LEFT HAND STATION 535 LONGERON 24 LEFT FRAME REPAIR ANGLE CHAFFED REMOVED AND FOUND EXCEEDED LIMIT PER SRM 53-00-00-Feb 14, 2022 · N576FE · Doug MD11F · Fuselage Main, StructureSDR FDEA202202140292Frame · noneMAIN DECK CARGO COMPARTMENT LEFT HAND STATION 535 LONGERON 19 LEFT FRAME ATTACHED REPAIR ANGLE FOUND CHAFFED. MAIN DECK CARGO COMPARTMENT LEFT HAND STATION 535 LONGERON 19 LEFT FRAME REPAIR ANGLE CHAFFED REMOVED AND FOUND EXCEEDED LIMIT PER SRM 53-00-00-2Feb 14, 2022 · N576FE · Doug MD11F · Fuselage Main, StructureSDR FDEA202202130287Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM57-50- 02-2RFeb 13, 2022 · N575FE · Doug MD11F · Wing, Control SurfacesSDR FDEA202202130286Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM57-50- 02-2RFeb 13, 2022 · N575FE · Doug MD11F · Wing, Control SurfacesSDR FDEA202202130289Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM57-50- 02-2RFeb 13, 2022 · N575FE · Doug MD11F · Wing, Control SurfacesSDR FDEA202202130288Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM57-50- 02-2RFeb 13, 2022 · N575FE · Doug MD11F · Wing, Control SurfacesSDR FDEA202202130283Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM57-44-08. REPAIR SHIM FABRICATED AND INSTALLED AFeb 13, 2022 · N575FE · Doug MD11F · Wing, Control SurfacesSDR FDEA202202130284Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM57-44-08 AND FOUND LOWER FACE EXCEED LIMIT BASE Feb 13, 2022 · N575FE · Doug MD11F · Wing, Control Surfaces
Back to Boeing MD-11F