# N430GT: 2006 Boeing 747-4H6F - Status: Valid registration - Airframe: [Boeing 747-4H6F](https://openairdocs.org/model/boeing-747-4h6f) (registry code 13848BW, 660 seats) - Engine: [Pratt & Whitney Canada JT15D-5R](https://openairdocs.org/engine/pratt-whitney-canada-jt15d-5r) (registry code 52285) - Data sheets: [TCDS E25EA](https://openairdocs.org/tcds/E25EA) (Pratt & Whitney Canada Corp.) (OpenAirDocs) - Serial number: 28434 - Year built: 2006 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 17, 2024 - Certificate issued: May 16, 2024 - Expires: May 31, 2031 - Mode S code: A523C6 - Registered owner: [Atlas Air Inc](https://openairdocs.org/faa-owner/ATLAS%20AIR%20INC) - Location: [White Plains, NY](https://openairdocs.org/faa-place/NY/White%20Plains) - Owner type: Corporation - Owner's area on the map: 41.0329° N, 73.7648° W: Placed by OpenAirDocs at the center of ZIP code 10601, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=430GT - Page: https://openairdocs.org/aircraft/N430GT From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 1 in force ### Matched by airframe (Boeing 747-4H6F) None in force. ### Matched by engine (Pratt & Whitney Canada JT15D-5R) - [AD 2008-24-10](https://openairdocs.org/ad/2008-24-10): Fuel Control Hydro Mechanical Unit (HMU) P3 servo · Pratt & Whitney Canada JT15D-5, JT15D-5B, JT15D-5F and 1 more. Effective Jan 2, 2009 ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N430GT. ## FAA accident and incident reports None matched to N430GT. ## Service difficulty reports (14) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UIEA2025122001354](https://openairdocs.org/sdr/UIEA2025122001354), Dec 19, 2025: ADC. FAULTED. IAS 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 - [SDR UIEA2025092101242](https://openairdocs.org/sdr/UIEA2025092101242), Sep 21, 2025: PUMP. ILLUMINATED. HYD 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 - [SDR UIEA2025090401160](https://openairdocs.org/sdr/UIEA2025090401160), Sep 3, 2025: FMC. FAULTED. ONE 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 F - [SDR UIEA2025090201151](https://openairdocs.org/sdr/UIEA2025090201151), Aug 31, 2025: WINDOW. LEAKING. R2 WINDOW HAS HIGH WIND NOISE. THE HIGHER THE AIRCRAFT CLIMBS, THE LOUDER THE NOISE BECOMES(

APPLIED FILLER TO LOWER LH AND RH WINDOW FRAME CORNER ON R2 POSIT - [SDR UIEA2025080501090](https://openairdocs.org/sdr/UIEA2025080501090), Aug 5, 2025: MANIFOLD. DAMAGED. FLIGHT 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 & - [SDR UIEA2025031400334](https://openairdocs.org/sdr/UIEA2025031400334), Mar 23, 2025: BULKHEAD WEB. CRACKED. DURING ACCOMPLISH EO 4453C449_CS LH CLOSEOUT PANEL REPLACEMENT FOUND I/B SIDE CANTED PRESSURE BULKHEAD WEB FASTENER HOLE CRACKED.(

WORK ACCOMPLISHED CABIN STA 1000 LBL 33 SEAT TRACK REPAIR CARRIED OUT IAW B747-400F SRM 53-00-52 FIG 201 REV 103 AN - [SDR UIEA2025031900358](https://openairdocs.org/sdr/UIEA2025031900358), Mar 23, 2025: STIFFENER. CORRODED. FWD CARGO COMP STIFFENER AT STA 1000 LBL 26 BWL 110 FOUND CORRODED.(

WORK ACCOMPLISHED IAW EN# 1021-25 REV 0. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025031900359](https://openairdocs.org/sdr/UIEA2025031900359), Mar 23, 2025: LONGERON. CRACKED. DURING HFEC INSPECTION, FOUND CRACK AT LONGERON EXTENSION FITTING STA 1480 LHS & RHS APPROX CRACK LENGTH = 0.6" RHS AND 0.4" LHS AS MARKED.(

WORK ACCOMPLI - [SDR UIEA2025031900360](https://openairdocs.org/sdr/UIEA2025031900360), Mar 23, 2025: SUPPORT FITTING. OBSTRUCTED. DURING 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 LO - [SDR UIEA2025031900362](https://openairdocs.org/sdr/UIEA2025031900362), Mar 23, 2025: RUB STRIP. OBSTRUCTED. DURING 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 - [SDR UIEA2024081500831](https://openairdocs.org/sdr/UIEA2024081500831), Aug 17, 2024: SKIN. DENTED. DENT AT RH WING FLAP LOWER SURFACE 58" FROM INBD END(

INSTALLED FABRICATED DOUBLER AT RH WING FLAP LOWER SURFACE 58" FROM INBD END AND 27" FROM LOWER T/E IAW - [SDR UIEA2024081500830](https://openairdocs.org/sdr/UIEA2024081500830), Aug 17, 2024: SKIN. DENTED. SEVERAL DENTS AT LH WING INBD MID FLAP LOWER SURFACE(

INSTALLED, FABRICATED DOUBLER ON LH WING MID FLAP IAW SRM 51-70-10-212-0 PAR 20B TABLE 208. NO FURTHER D - [SDR UIEA2024081600835](https://openairdocs.org/sdr/UIEA2024081600835), Aug 17, 2024: RUB STRIP. GOUGED. LH WING #5 SPOILER LOWER SKIN T/E RUB STRIP GOUGED(

ACCOMPLISHED PERMANENT REPAIR ON #5 SPOILER LOWER SKIN IAW B747 SRM 51-70-10-2R & 57-70-02-2R-1. NO FU ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Boeing 747-4H6F aircraft: https://openairdocs.org/model/boeing-747-4h6f/aircraft.md - The Pratt & Whitney Canada JT15D-5R engine: https://openairdocs.org/engine/pratt-whitney-canada-jt15d-5r.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.