N279AD - 1992 BOEING 737 400
Aircraft Summary
General
Year
1992
Manufacturer
BOEING
Model
737-400
Serial Number
26279
Registration #
N279AD
Condition
Used
Description
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
Airframe
Total Time
64429.1
Total Landings
33382
Engine Program
Engine Maintenance Program
Other
Engine 1
Engine 1 Manufacturer
CFM INTERNATIONAL
Engine 1 Time
78593.1
Engine 1 Notes
Model: CFM56-3C1
#1 L/H Engine (ESN 720189)
ETT: 78,593.1
CSN: 64,406
Engine 2
Engine 2 Manufacturer
CFM INTERNATIONAL
Engine 2 Time
64406
Engine 2 Notes
Model: CFM56-3C1
#2 R/H Engine (ESN 856938)
ETT: 46,689.4
CSN: 33,191
Auxiliary Power Unit
APU
Yes
APU Maintenance Program
Other
APU Notes
Manufacturer: Honeywell
Model: GTCP85-129(H)
Serial Number: P-35109C
TSN: 37,713.1
Avionics
Flight Deck Manufacturer
HONEYWELL
Avionics/Radios
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
Exterior
Exterior Notes
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
Interior
Interior Notes
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
Inspection Status
Inspection Status
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
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