- Registered owner
- Atlas Air Inc
- Location
- White Plains, NY
- Owner type
- Corporation
- Serial number
- 28434
- Year built
- 2006
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- August 17, 2024
- Certificate issued
- May 16, 2024
- Expires
- May 31, 2031
- Mode S code
- A523C6
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 1
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
Engine · Pratt & Whitney Canada JT15D-5R
AD 2008-24-10Fuel Control Hydro Mechanical Unit (HMU) P3 servoInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N430GTMatched 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 747-4H6F aircraft
FAA incident reports
No FAA accident or incident reports matched to N430GTMatched 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 747-4H6F aircraft
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR UIEA2025122001354Adc · faultedIAS DISAGREE EICAS MSG AFTER T/O & ALT DISAGREE EICAS MSG AT 7000 FT. REMOVED AND REPLACED L/H AIR DATA COMPUTER IAW AMM 34-12-01. PITOT STATIC LEAK CHK OK IAW AMM 34-11-00. ALTIMETER SYSTEM ACCURACY TEST OK IAW AMM 34-41-00. REMOVED AND REPLACED LEFT UPPER PSDR UIEA2025092101242Pump · illuminatedHYD PRESS SYS 1 EICAS CAUTION; HYD QTY LOW EICAS CAUTION, HYD OVHT SYS 1 EICAS, GEAR DOOR CAUTION - BODY GEAR RIGHT DOOR. R & R THE NLG DOOR ACTUATOR PER AMM 32-34-14. OPS & LK CHK GOOD PER AMM 32-34-14. INSTALLED NEW EDP IAW AMM 29-11-05 & IPC 29-11-05-02B.SDR UIEA2025090401160Fmc · faultedONE HOUR, THREE MINUTES INTO FLIGHT, BOTH ND'S HAVE YELLOW MAP FAULT DISPLAYED. NO ROUTE OR MAGENTA LINE SHOWN, EIU SOURCE SEL AND CTR C/B CYCLED. REPLACED LT FMC PER AMM 34-61-01, TESTED GOOD IAW AMM 34-61-00 & IPC 34-61-01.SDR UIEA2025090201151Window · leakingR2 WINDOW HAS HIGH WIND NOISE. THE HIGHER THE AIRCRAFT CLIMBS, THE LOUDER THE NOISE BECOMES(<P>APPLIED FILLER TO LOWER LH AND RH WINDOW FRAME CORNER ON R2 POSITION PER AMM 20-30-01, BOEING TLS 25-0574-02B AND BOEING EID 65B07610 SHEET 5. INSTALLED NEW R2 WINDOSDR UIEA2025080501090Manifold · damagedFLIGHT CREW REPORTED MOMENTARY FIRE WARNING MESSAGE ON EICAS. FOUND DAMAGE TO THE 8TH STAGE MANIFOLD. REPLACED 8TH STAGE MANIFOLD IAW AMM 36-11-01/401 PER 114 & IPC 36-11-05-01B REV 89. PERFORMED NR 2 ENG PNEUMATIC LEAK TEST IAW AMM 71-00-00-705-002-N00. LESDR UIEA2025031400334Bulkhead Web · crackedDURING ACCOMPLISH EO 4453C449_CS LH CLOSEOUT PANEL REPLACEMENT FOUND I/B SIDE CANTED PRESSURE BULKHEAD WEB FASTENER HOLE CRACKED.(<P>WORK ACCOMPLISHED <SPAN>7075T6-0.125" & 7075T6-0.063" </SPAN><SPAN>IAW EN 1014-25 REV 0.</SPAN></P>)SDR UIEA2025031900357Seat Track · corrodedCABIN STA 1000 LBL 33 FOUND SEAT TRACK CORROSION AS MARKED.(<P>CABIN STA 1000 LBL 33 SEAT TRACK REPAIR CARRIED OUT IAW B747-400F SRM 53-00-52 FIG 201 REV 103 AND EN# 1020-25 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025031900358Stiffener · corrodedFWD CARGO COMP STIFFENER AT STA 1000 LBL 26 BWL 110 FOUND CORRODED.(<P>WORK ACCOMPLISHED IAW EN# 1021-25 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025031900359Longeron · crackedDURING HFEC INSPECTION, FOUND CRACK AT LONGERON EXTENSION FITTING STA 1480 LHS & RHS APPROX CRACK LENGTH = 0.6" RHS AND 0.4" LHS AS MARKED.(<P>WORK ACCOMPLISHED IAW EN# 1018-25 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025031900360Support Fitting · obstructedDURING ACCOMPLISH EO 4454A215_CS NACELLE STRUT PW4000 NO.1 & NO.4 OUTER SPRING BEAM SUPPORT FTG. WHILE LOCATE FILLE P/N: 321U2400-5602 AT FASTENER CODE A LOCATION. FOUND TOO CLOSE TO EXISTING BULKHEAD.(<P>WORK ACCOMPLISHED IAW EN# 1013-25 REV 0. NO FURTHER DEFSDR UIEA2025031900362Rub Strip · obstructedDURING PERFORMING LH AND RH RUB STRIP INSTALLATION PER SB 747-53A2721R3/ AD 2013-26-12, FOUND AFT RUB STRIPS INTERFERING WITH EXISTING PROTUDING HEAD FASTENERS ON FUSELAGE SKIN AT BS2517 TO 2628 LH AND RH(<P>WORK ACCOMPLISHED IAW EN# 1019-25 REV 0. NO FURTHER SDR UIEA2024081500831Skin · dentedDENT AT RH WING FLAP LOWER SURFACE 58" FROM INBD END(<P>INSTALLED FABRICATED DOUBLER AT RH WING FLAP LOWER SURFACE 58" FROM INBD END AND 27" FROM LOWER T/E IAW SRM 51-70-10-2R-0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024081500830Skin · dentedSEVERAL DENTS AT LH WING INBD MID FLAP LOWER SURFACE(<P>INSTALLED, FABRICATED DOUBLER ON LH WING MID FLAP IAW SRM 51-70-10-212-0 PAR 20B TABLE 208. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024081600835Rub Strip · gougedLH WING #5 SPOILER LOWER SKIN T/E RUB STRIP GOUGED(<P>ACCOMPLISHED PERMANENT REPAIR ON #5 SPOILER LOWER SKIN IAW B747 SRM 51-70-10-2R & 57-70-02-2R-1. NO FURTHER DEFECTS NOTED</P>)
STCs 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.