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N409MC

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2000 Boeing 747-47UF · GE CF6-80 series

Open in FAA registry

© OpenStreetMap
Registered owner
Atlas Air Inc
Location
Purchase, NY
Owner type
Corporation
Serial number
30558
Year built
2000
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
March 31, 2000
Certificate issued
October 13, 2016
Expires
October 31, 2029
Mode S code
A4CF26
Boeing 747-47UFAirframe model · 660 seats · 4 engines · 15 registeredTCDS E13NEEngine · GE CF6-80 series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE CF6-80 model are included below.

On this page

Airworthiness directives that may apply · 61

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1985In forceSuperseded2026
See all 80 ADs

Information bulletins that may apply · 5

Advisory, not mandatory.

NTSB investigations · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

NTSB DCA12WA144Incident · No injuriesForeign investigationMelbourne, AustraliaOn September 9, 2012 a Boeing 747 operated by Atlas Air did not comply with the height and tracking requirements of the BADGR SIX STAR to Melbourne Airport. The investigation is being conducted by the Australian Transport Safety Bureau. www.atsb.gov.auSep 9, 2012 · No damage

FAA incident reports

No FAA accident or incident reports matched to N409MCMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Boeing 747-47UF aircraft

Service difficulty reports · 236

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR UIEA2026082000782Switch · faultedRTO MASTER WARNING AURAL "CONFIG SPOILERS". LOW SPEED RTO 65KTS, RETURNED TO GATE. R & R AUTOMATIC SPEED BRAKE ARM SWITCH IAW AMM 27-62-10/401 AND AIPC 2762-55-01 ITEM 344. PERFORMED OPS CHK, CHKD OK. PERFORMED T/O WARNING TEST IAW AMM 31-51-00-725-024, TEST Aug 20, 2026 · N409MC · Boeing 74747UF · Drag Control SystemSDR UIEA2025112401322Coupler · faultedLEFT/RIGHT HF WILL NOT TRANSMIT. R & R RT & LT HF COUPLER PER AMM 23-11-03 & AIPC 23-11-03-05A. OPS CHK OK. LNov 24, 2025 · N409MC · Boeing 74747UF · Communications System WiringSDR UIEA2025050600588Support Fitting · gougedLH BLG INBOARD TRUNNION VERTICAL SUPPORT FITTING I/B AND O/B SIDE FACE FOUND GOUGE MARK. LH BLG INBOARD TRUNNION VERTICAL SUPPORT FITTING I/B AND O/B SIDE FACE MACHINED AS PER B747-400F SRM 53-40-90 REPAIR 1 REV. 103 AND FOUND WITHIN WORK LIMIT. FOR DETAILS RMay 15, 2025 · N409MC · Boeing 74747UF · Fuselage Main, Attach Fittings
See all 236 reports

STCs that may be installed · 6

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

Engine · GE CF6-80 series

STC SE01543CHReplace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve.Cook Airtomic · Lists CF6-80ASTC SE01478CHInstallation of Cook Airtomic alignment joint p/n AIR 22912.Cook Airtomic · Lists CF6-80C2 SeriesSTC SE00969CHInstall AeroControlex P/N 2605290-001 variable stator feedback control cable.AeroControlex Group TransDigm Inc · Lists CF6-80ASTC SE01471ATReplace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine.Unison Industries · Lists CF6-80C2 SeriesSTC SE00463LAInstall fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220Hi Temp Insulation Inc · Lists CF6-80C2A1STC SA2227SOInstallation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIESRolls Royce, Inc