- Registered owner
- Atlas Air Inc
- Location
- Purchase, NY
- Owner type
- Corporation
- Serial number
- 33517
- Year built
- 2004
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 25, 2017
- Certificate issued
- July 22, 2021
- Expires
- July 31, 2028
- Mode S code
- A561FD
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 15
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2006 | 1 |
|---|---|
| 2010 | 2 |
| 2011 | 1 |
| 2012 | 8 |
| 2015 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2026 | 1 |
Engine · Pratt & Whitney PW4062A
AD 2026-21-06Engine Fuel and ControlAD 2018-13-02Turbine Engine Combustion SectionAD 2016-08-09HPC 10th stage diskInformation bulletins that may apply · 5
Advisory, not mandatory.
Engine · Pratt & Whitney PW4062A
SAIB 2025-06High Pressure TurbinesSAIB NE-19-02Turbine Engine Compressor Section -- Low-pressure turbine uncontainmentSAIB NE-16-01R1Turbine SectionSAIB NE-15-19Turbine SectionSAIB NE-13-31Turbine Engine Oil System Scavenge Oil Tube Coking and Proper Cleaning at OverhaulHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N446MCMatched 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 747-4B5F aircraft
FAA incident reports
No FAA accident or incident reports matched to N446MCMatched 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 747-4B5F aircraft
Service difficulty reports · 68
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR UIEA2025080901117Engine · vibrationNR 2 ENG EXCESSIVE VIBRATION 4.5 N1. NO CHANGE WHEN THROTTLE REDUCED AT CRUISE LEVEL. VIBRATION FELT THROUGH RUDDER PEDALS. MAX RECORDED 5.0(<P>#2 ENG 2 EACH BALANCE WEIGHT REMOVED, ENG #2 VIB TRIM BALANCE PERFORMED IAW AMM 71-00-00 & AMM 72-31-00. RESULT MAX SDR UIEA2025071800977Bulb · inoperativeLEFT DOOR 1, CEILING FWD EMERGENCY LIGHT (L5735) FOUND INOPERATIVE. REPLACED THE LIGHT BULB FOR L1 DOOR CEILING FWD EMERGENCY LIGHT IAW AMM 33-51-07. OPS TESTED NORMAL.SDR UIEA2025072301010Fitting · crackedONE CRACK WAS FOUND ON BS 1000 INTERCOSTAL LUG FITTING AT RBL 11.33. INTERCOSTAL LUG FITTING REPLACED IAW EO 4453C024, REV.4, PART 7, STEP 3. NO FURTHER DEFECTS NOTED.
See all 68 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.