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1992 BOEING 737-400

Jet

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Posizione dell' Aereomobile:Fort Lauderdale, Florida, Stati Uniti

Mathew McMenamin

Contatto:Mathew McMenamin

Telefono:(954) 684-4680

Fort Lauderdale, Florida, Stati Uniti

(954) 684-4680

Costi di gestione

Generale

Anno

1992

Produttore

BOEING

Modello

737-400

Numero di serie

26279

Registrazione #

N279AD

Condizione

Usati

Descrizione

Maintained by U.S. Marshals Service (JPATS) under FAA oversight 2,060-nautical mile range 156-seat passenger configuration Avionics suite includes TCAS II, DFDR/SSCVR, and triple VHF comm Recent engine installation (Engine#1- Aug 2024) Active CAMP tracking with maintenance logged through April 2026

Struttura velivolo

Tempo totale

64,429.1

Sbarchi totali

33,382

Engine Program

Engine 1 Maintenance Program

Altro

Engine 1

Engine 1 Make/Model

CFM INTERNATIONAL

Engine 1 Time

78,593.1

Motore 1 Note

Model: CFM56-3C1 #1 L/H Engine (ESN 720189) ETT: 78,593.1 CSN: 64,406

Engine 2

Engine 2 Make/Model

CFM INTERNATIONAL

Engine 2 Time

64,406

Motore 2 Note

Model: CFM56-3C1 #2 R/H Engine (ESN 856938) ETT: 46,689.4 CSN: 33,191

Auxiliary Power Unit

APU

Programma APU

Altro

Note APU

Manufacturer: Honeywell Model: GTCP85-129(H) Serial Number: P-35109C TSN: 37,713.1

Avionica

Flight Deck Manufacturer/Model

HONEYWELL

Avionica/Radio

Honeywell Dual Air Data Computers (HG480E1) Dual G.E. Aviation Flight Management Computers (FMC) Honeywell Flight Control Computers (FCC A & B) Honeywell Yaw Damper Coupler Honeywell Engine Vibration Signal Conditioner Dual Honeywell Digital Air Data Assemblies (DAA) Dual Honeywell Inertial Reference Units (IRU) Triple Collins VHF COMM Radios Dual Collins VHF NAV Receivers Dual Collins DME Units Dual Collins EFIS Symbol Generators Dual Collins HF Communication Radios (One Installed) ACSS TCAS Computer ACSS ATC Transponder Motorola SELCAL Decoder Honeywell Autothrottle Computer Logic Air LPV Adapters (Left & Right) Dual Boeing Stall Management Computers Hamilton Cabin Pressure Controller Avtech Remote Electronics Unit (REU) & Aircraft Engineering AIU Honeywell Digital Flight Data Acquisition Unit (DFDAU) OECO Triple Transformer Rectifiers Avionics Instruments Static Inverter ELDEC Battery Charger Boeing Auto Speed Brake Control Unit Boeing APU Control Unit Boeing Engine Accessory Unit Boeing Flap/Slat Position Module Boeing Relay and Switching Modules Crane Anti-Skid Control Unit Dual Honeywell Zone Temperature Controllers Fire Detection and Overheat Detection Systems Aircell Satellite Telephone System

Esteriore

Overall white paint finish offering a neutral base for custom livery Fuselage and airframe in servable condition Cabin windows and cockpit glass noted as intact with no major damage No major external corrosion in maintenance records

Interno

Interiore

Retains original factory flight deck configuration with all core avionics in place Instrumentation and display components reported in functional condition Cabin configuration adaptable for passenger or cargo operations Pressurized fuselage with serviceable cabin window condition Ideal candidate for reconfiguration or interior modernization

Stato Ispezione

Stato di ispezione

MAINTENANCE CAMP-maintained with tracking through April 2026 Currently owned and operated by the U.S> Marshals Service (JPATS) Engine #1 recently installed (August 2024) APU installed in mid-2023 with reliable Honeywell GTCP85-129(H) performance Avionics software and database updates No significant structural corrosion findings reported Logbooks and maintenance documentation available for review MAINTENANCE DUE: Service check: 6/5/2026 1A Check: 6/22/2026 1C Check: 6/7/2026 2C Check: 6/23/2026 3C Check: 6/29/2026 6C Check: 6/7/2026