Boeing MD-11F

Service difficulty reports · 31,317

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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 FDEA202508131431Seat Track · wornSEAT TRACK AT STATION 6-4 X= -47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 6-4, X= -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK Aug 13, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508131430Seat Track · wornCABIN-SEAT TRACK AT STATION 6-9, X= 27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 6-9, X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TAug 13, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508131429Seat Track · wornCABIN-SEAT TRACK AT STATION 6-4, X= -8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 6-4, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT Aug 13, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508131428Seat Track · wornSEAT TRACK AT STATION 6-4, X= 8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 6-4, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REAug 13, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508131427Seat Track · wornCABIN-SEAT TRACK AT STATION 1541, X= -8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1541, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEATAug 13, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508131426Seat Track · wornCABIN-SEAT TRACK AT STATION 1541 X= 8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1541, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TAug 13, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508131425Seat Track · wornCABIN-SEAT TRACK AT STATION 5-5, X= 47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 5-5, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRAAug 13, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508131424Seat Track · wornCABIN-SEAT TRACK AT STATION 5-11, X= 27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 5-11, X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAAug 13, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508131423Seat Track · wornCABIN-SEAT TRACK AT STATION 5-6, X= -47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 5-6, X= -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TAug 13, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508131422Seat Track · wornCABIN-SEAT TRACK AT STATION 5-5, X= -27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 5-5, X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAAug 13, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508131421Seat Track · wornCABIN-SEAT TRACK AT STATION 1421, X= 47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1421, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEATAug 13, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025081222186Battery · no testPRE FLIGHT, DURING EMER LIGHT TEST GOT €Œ L1 EMER LT BAT 1 LO. ? REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-51-01. REVERSED DMP 33-50-4. OPS CHECK GOOD PER AMM 33-51-01.Aug 12, 2025 · N284UP · Doug MD11F · Emergency LightingSDR IPXA2025081217326Battery · inoperativeEMERGENCY LIGHT TEST SHOWING BAT LO ON EAD. EMERGENCY LIGHTING BATTERY POWER SUPPLY R&R IAW AMM 33-51-01/401. LIGHTS CHECKS SERVICEABLE.Aug 12, 2025 · N273UP · Doug MD11F · Emergency LightingSDR IPXA2025081116757Battery · no testPREFLIGHT DURING EMER LIGHT TEST HAD LEVEL 1 EMER LT BAT 1 LO ILLUMINATE R&RD EMERGENCY LIGHT POWER SUPPLY/ BATTERY AS REQ. OPS CK NORMAL REF. MM 33-51-01 OK FOR SVC PLACARD REMOVED DMP REVERSEDAug 11, 2025 · N288UP · Doug MD11F · Emergency LightingSDR FDEA202508111407Trunnion · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND NOSE LANDING GEAR TRUNNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING AT STATION 583, FOUND 01 EACH CRACK INDICATION PROPAGATE FROM THE SLOT OUT AREA APPROXIMATELY 1/8" LENGTH. LEFT Aug 11, 2025 · N522FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA202508111403Seat Track · wornCABIN-SEAT TRACK AT STATION 889, X= -27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 889, X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEATAug 11, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508111402Seat Track · wornSEAT TRACK AT STATION 889, X= -47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 889, X= -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACKAug 11, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508111401Seat Track · wornCABIN-SEAT TRACK AT STATION 889, X= 27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 869, X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TAug 11, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508111400Seat Track · wornCABIN-SEAT TRACK AT STATION 889, X= 47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 889, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT Aug 11, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508111399Seat Track · wornSEAT TRACK AT STATION 999, X= -8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 999, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK Aug 11, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508111398Seat Track · wornSEAT TRACK AT STATION 999, X= -27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 999, X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACKAug 11, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508111397Seat Track · wornCABIN-SEAT TRACK AT STATION 999 X= 47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 999, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRAug 11, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508111396Seat Track · wornCABIN-SEAT TRACK AT STATION 999 X= 47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 999, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRAug 11, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508111395Seat Track · wornCABIN-SEAT TRACK AT STATION 1089, X= 8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1089, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLAAug 11, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508111394Seat Track · wornCABIN-SEAT TRACK AT STATION 6-30,X= -47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 6-30, X= -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAAug 11, 2025 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508071383Doubler · chafedEXISTING REPAIR AT FUSELAGE SKIN FORWARD CARGO DOOR CUTOUT FORWARD JAMB STATION 895.70 BETWEEN LONGERON 40 RIGHT TO LONGERON 42 RIGHT. EXISTING REPAIR AT FUSELAGE SKIN FORWARD CARGO DOOR CUTOUT FORWARD JAMB STATION 895.70 BETWEEN LONGERON 40 RIGHT TO LONGEAug 7, 2025 · N613FE · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2025080632499Battery · inoperativeEMERGENCY LIGHT BATTERY 1 LOW. REVERSED DMP 33-50-4 AS REQUIRED. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW A.M.M. 33-51-01-000-802/400-802. PERFORMED OPERATIONAL TEST AS PER TASK# 33-51-01-700-802 AND FOUND SATISFACTORY. THIS CLEARS DEFERRAL [TAug 6, 2025 · N288UP · Doug MD11F · Emergency LightingSDR FDEA202508061381Frame · damagedDURING REPAIR INSPECTION, REF WRI 53-10/5099, FOUND DAMAGE TO FRAME AT FR. STA. 374L@X= 38. INSTALLED SKIN DOUBLER, TRIPLER AND FILLER REF MD11 SRM 53-00-01-2R. E. A. 1-5330-T0384438 PT1 AND PT2 .FUSELAGE- PLATES & SKINS- SKI AND FRAME REPAIR AT STA 374, Aug 6, 2025 · N605FE · Doug MD11F · Fuselage Main, FrameSDR IPXA2025080511544Manifold · faulted**ATB**LEVEL 3 AIR MANF 3 FAIL CLIMBING OUT OF 12,000 ALERT AUTO SYSTEM ISOLATED THE #3 BLOCKED AND THEN ALERT CAME BACK. ATB FOUND FAULTS FOR MANIFOLD AND ANTI ICE VALVE IN THE ESC INOP RESET . VERIFIED WITH TELEMETRY THAT THE RIGHT WING ANTI ICE VALVE FAIL Aug 5, 2025 · N257UP · Doug MD11F · Airfoil Anti/De-ice SystemSDR FDEA202508051369Spoiler · damagedPOST FLIGHT WALK AROUND FOUND SPOILER NR 5 DAMAGED ON RIGHT WING. R & R'D RH O/B #5 SPOILER OPS & FUNCTION CHK GOOD. A/C OK FOR SERVICE IAW AMM 27-60-30-4 ANN: 27-60-30-6.Aug 5, 2025 · N607FE · Doug MD11F · SpoilersSDR FDEA202508051368Skin · puncturedRIGHT HAND WING: LOCATED ALONG OUTBOARD SIDE OF #12 SLAT TRACK, RIGHT HAND LEADING EDGE SKIN AREA FOUND PUNCTURED AND DENTED, ALONG XOS 780. REPAIR CARRIED OUT AT RIGHT HAND WING: LOCATED ALONG OUTBOARD SIDE OF #12 SLAT TRACK RIGHT HAND LEADING EDGE SKIN AAug 5, 2025 · N613FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202508041382Skin · ground damageDURING STORM IN DFW , TRUCK CAN PUNCTURED AIRCRAFT . DAMAGE IS 4" LONG BY 2 " WIDE . SEE PICTURES INSTALLED SKIN DOUBLER, TRIPLER AND FILLER REF MD11 SRM 53-00-01-2R. E. A. 1-5330-T0384438 PT1 AND PT2 .FUSELAGE- PLATES & SKINS- SKI AND FRAME REPAIR AT STAAug 4, 2025 · N605FE · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2025080145238Proximity Sensor · faultedDESCENDING THROUGH 17000 W/SPEED EXTENDED, THE RIGHT GEAR HANDLE RED WARNING LIGHT CAME ON,AND STAYED ON. RE-ADJUSTED RH MLG GEAR UP AND DOOR LATCHED PROXIMITY SENSOR IAW AMM 32-61-15. PERFORMED BITE TEST IAW AMM 32-61-15-741-802. TEST GOOD.Aug 1, 2025 · N254UP · Doug MD11F · Landing Gear Position and WarningSDR IPXA2025090125093Pressure Panel · corrodedMAJOR REPAIR. MAIN CABIN AT CENTER WING L/H TUNNEL AT THE PRESSURE PANEL HAS CORROSION. ATA 36-14 CENTER WING UPPER AFT SKIN CORROSION REPAIR BTWN XCW=101.850 AND XCW=110 AT REAR SPAR ACCOMPLISHED IN ACCORDANCE WITH UPS EO-94951-REQ1 REVISION 1 AND VT SAA EAJul 31, 2025 · N274UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2025081524093Pressure Panel · corrodedMAIN CABIN AT CENTER WING L/H TUNNEL AT THE PRESSURE PANEL HAS CORROSION. VERIFIED STEP 7 C/W IAW UPS RII GMM 04-02.Jul 31, 2025 · N274UP · Doug MD11F · Fuselage Main, StructureSDR FDEA202507311344Skin · crackedFUSELAGE EXTERIOR SKIN APPROXIMATE X= 18.955 LEFT HAND STATION 475, FORWARD OF NOSE LANDING GEAR FORWARD DOOR FOUND CRACKED. CRACKED SKIN AT FUSELAGE EXTERIOR APPROXIMATE X= 18.955 LEFT HAND STATION 475 FORWARD OF NOSE LANDING GEAR FORWARD DOOR REPAIRED ASJul 31, 2025 · N613FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 9WGA2025092454671Panel · corrodedCENTER WING UPPER PANELCORRODED AT RH APPROX STA 1219, XCW 16.0, S-16. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT CENTER WING UPPER PANEL RH APPROX STA 1219, XCJul 30, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025092454670Panel · corrodedDURING HEAVY MAINTNENANCE CENTER UPPER PANEL CORRODED AT RH APPROX STA 1204, XCW 24.5 S-18. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH APPROX. STA 1204, XCW 2Jul 30, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025090954652Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER SECTION UPPER PANEL CORRODED AT RT APPROX. STA. 1219, XCW 16.0 S-16. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT CENTER WINGJul 30, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025090954651Panel · corrodedDDURING HEAVY MAINTENANCE CHECK CENTER SECTION UPPER PANEL CORRODED AT RH APPROX STA 1204, XCW 24.5 S-18. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH APPROX. SJul 30, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR FDEA202507301340Power Unit · faultedEMER PWR TST FAIL LEVEL 1 ALERT ILLUMINATED. PER QRH, TURNED EMER PWR SWITCH OFF AND WAITED FOR BAT CHARGING MESSAGE TO GO OUT, THEN TURNED EMER PWR SWITCH ON AND ALL APPEARED NORMAL, UNTIL APU PWR DROPPED OFFLINE AGAIN AND EMER PWR ON LEVEL 1 ALERT ILLUMJul 30, 2025 · N621FE · Doug MD11F · Electrical Power SystemSDR 9WGA2025092354669Panel · corrodedCENTER WING UPPER PANEL CORRODED AT RH APPROX STA 1229, XCW 96.0 AT S-15. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPROX STA 1229, XCW 96.Jul 29, 2025 · N546JN · Doug MD11F · Fuselage Miscellaneous StructureSDR 9WGA2025092354668Panel · corrodedDURING HEAVY MAINTENANCE CENTER UPPER PANEL CORRODED AT RH APPROX STA 1233, XCW 76.5 AT S-14. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1233, XCW 76.5 AT S-14, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MJul 29, 2025 · N546JN · Doug MD11F · Fuselage Miscellaneous StructureSDR 9WGA2025092354667Panel · corrodedCENTER UPPER PANEL CORRODED AT LH APPROX STA 1205, XCW 7.0 S-18. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT LH APPROX STA 1205, XCW 7.0 AT S-18, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MESSAGE: WGN-WGN-25-0035-4C. Jul 29, 2025 · N546JN · Doug MD11F · Fuselage Miscellaneous StructureSDR 9WGA2025090954650Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA 1229, XCW 96.0 AT S-15. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WINJul 29, 2025 · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025090954649Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA 1233, XCW 76.5 AT S-14. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1233, XCW 76.5 AT S-14, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IJul 29, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025090954648Panel · corrodedDURING HEAVY MAINTENENACE CHECK CENTER WING UPPER PANEL CORRDODED AT LH APPROX STA 1205, XCW 7.0 S-18. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT LH APPROX STA 1205, XCW 7.0AT S-18, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MJul 29, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR IPXA202507304352Transmitter · faultedDURING ILS COUPLED APPROACH WITH FLAPS AT 35 AND VERIFIED BY CAPT AND F/O GREEN BOX, TOO LOW FLAPS WARNING WENT OFF TWICE CAUSING GO AROUND. REPLACED RT OTBD FLAP POSITION TRANSMITTER IAW MM 27-54-02-400-801.Jul 29, 2025 · N276UP · Doug MD11F · Trailing Flap Position Indicating SystemSDR IPXA2025081560455Stringer · damagedMAJOR REPAIR, EXISTING REPAIRS IS TIME LIMITED RT WING UPPER STRINGER 6 AT XORS 980.80 REQUIRED PERM. REF EO # 87790-REQ 001. ACCOMPLISHED REPAIR IAW EO-87790-REQ001 REV2 AND VT-SAA EA 011-5700-01-B0550 REV IR.Jul 28, 2025 · N274UP · Doug MD11F · Wing, Longeron/StringerSDR FDEA202507271326Battery · no testEMER LT BATT 1 LOW, NOTED DURING POST FLIGHT WALK AROUND. REMOVED AND REPLACED EMERGENCY POWER LIGHTING BATTERY AS PER MD11 M.M. 33-51-01-4, OPS CHECKS NORMAL. O.K. FOR FLIGHT.Jul 27, 2025 · N607FE · Doug MD11F · Emergency Lighting
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