- Registered owner
- Atlas Air Inc
- Location
- Purchase, NY
- Owner type
- Corporation
- Serial number
- 28367
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Certificate issued
- May 8, 2008
- Expires
- August 31, 2027
- Mode S code
- A4F6A5
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 0
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
No ADs matched this aircraft’s modelsADs on appliances, propellers and installed equipment aren’t matched by model; check those separately.
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N419MCMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 747-48EF aircraft
FAA incident reports
No FAA accident or incident reports matched to N419MCMatched 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 747-48EF aircraft
Service difficulty reports · 287
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR UIEA2026071300597None · noneUNABLE TO CARRY OUT LFEC PER WORK CARD 53-F64K-00-01 ON LTH DRAIN MAST CUTOUT UNDER FAIRINGS STD 42L TO 43L AT BS 870 DUE TO NO DOUBLER INSTALLED. ONLY TWO DRAIN MASTS INSTALLED (DIFFERENT FROM THE WORK CARD). PERFORMED HFEC SCAN PER 747 NDT MANUAL D6-7170, SDR UIEA2026072000632Rivet · shearedQTY 01 DENT MARK AND QTY 01 SHEARED RIVET FOUND ON FUSELAGE SKIN FWD OF STA 2598, S26-38R, JACK PAD AREA. SHEARED RIVET ON FUSELAGE SKIN ON FWD OF STA 2598 BETWEEN S-26R AND S-38R EVALUATED AND FOUND STRUCTURALLY ACCEPTABLE TO LEAVE THE DENT AS-IS ALONG WITH SDR UIEA2026072200636Beam · damagedWHILE ACCOMPLISHING SB747-53A2562 R3, FOUND EXISTING PANEL HOLE TOO CLOSE TO NEW BEAM (05EA) AT STA 340. FASTENER INTERFERENCE CONDITIONS WITH HORIZONTAL STIFFENERS ON LHS NOSE WHEEL WELL AT STA 340, WL 130 - WL 170 RECTIFIED WITH THE HORIZONTAL STIFFENER FLA
See all 287 reportsSTCs that may be installed
No STCs matched this aircraft’s modelsSTCs are matched through the model’s type certificate data sheet, and this registry model isn’t matched to one.