1991 Boeing B737-500 VIP: Cabin – view along centre aisle

1991 Boeing B737-500 VIP: Club seating – conference table

1991 Boeing B737-500 VIP: Dining / work tables

1991 Boeing B737-500 VIPUSA

Photograph 1: 1991 Boeing B737-500 VIP
Photograph 2: Cabin – view along centre aisle
Photograph 3: Club seating – conference table
Photograph 4: Dining / work tables
Photograph 5: Aft cabin
Photograph 6: VIP lavatory
Photograph 7: Rear quarter

Boeing B737-500 VIP

Under offer

VIP business-class cabin for 44 passengers – approx. 4,000 nm range with centre tank

Year: 1991
Total time: 37,136 h
Location: USA
Price: Price on request

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Overview

1991 Boeing 737-500, MSN 24645, powered by two CFM56-3C1 turbofans. A VIP business cabin seats 44 passengers, 16 forward and 28 aft, and left, right and additional centre fuel tanks give a range of approximately 4,000 nm. Newly applied paint livery. The aircraft is currently in preservation.

44-seat VIP business cabin, 16 / 28
Approx. 4,000 nm range with centre tank
Fresh paint livery, newly applied
TCAS 7.1 and EGPWS equipped
ADS-B Out, Wi-Fi server capable
CFM56-3C1 engines, ICAO Stage III

Specification

Airframe

Type: Boeing 737-500
MSN: 24645
Total time: 37,136.27 h
Total cycles: 54,412
Configuration: 16 forward / 28 aft, 44 seats

Date of manufacture: 26 June 1991
Registration: N972EX (United States)
Noise compliance: ICAO Stage III
Location: United States
Times as of: 11 March 2025

Maintenance status

Item	Status
Maintenance programme	MSG-3 routine checks
Last C check	22 February 2024
Next C check due	22 August 2025
Current status	In preservation
Landing gear overhaul (10 years)	Last July 2017, next due July 2027

Weights and performance

Engines: 2 × CFM56-3C1
Max take-off weight: 116,500 lb
Max landing weight: 110,000 lb

Max zero fuel weight: 102,500 lb
Range: approx. 4,000 nm
Fuel: LH, RH and additional centre tank

Weights are as stated in the specification compiled from the seller's documentation and the range is approximate; both are provided for information purposes only. Actual figures vary with configuration, weight, temperature and altitude; the Aircraft Flight Manual and current weight-and-balance report govern.

Engines

Two CFM56-3C1 turbofans – times and cycles since new as of 11 March 2025, with the cycles remaining to each engine's first life limiter.

Engine 1: 37,754.67 h; 29,669 cycles
Engine 2: 44,195.67 h; 38,114 cycles
Engine 1 limiter: 1,156; cycles to LPT stage 2 disk
Engine 2 limiter: 1,601; cycles to HPC / HPT rotor

Item	Engine 1	Engine 2
Engine type	CFM56-3C1	CFM56-3C1
Serial number	857385	724952
Total time	37,754.67 h	44,195.67 h
Total cycles	29,669	38,114
Cycles remaining to first limiter	1,156	1,601
Lowest life limiter	LPT stage 2 disk	HPC / HPT rotor

APU

APU: Honeywell GTCP36-280B
Serial number: P-40108

Total cycles: 44,512

Landing gear

Position	Part number	Serial number	Next overhaul
Nose	65-73762-21	T5264P2553	July 2027
Main left	65-73761-127	MC05089P2553	July 2027
Main right	65-73761-128	MC05090P2553	July 2027

All gear overhauled July 2017 on a 10-year interval.

Avionics

Flight deck

TCAS 7.1, EGPWS and ADS-B Out

Rockwell Collins, Honeywell and Smiths avionics suite with 8.33 kHz VHF and ELS / EHS transponders.

ADS-B Out

Smiths flight management computer (P/N 168925-07-01)
Rockwell Collins TTR-921 TCAS 7.1
Honeywell windshear / EGPWS (965-0976-020-219-219)
Rockwell Collins weather radar (P/N 622-5132-106)
Rockwell Collins VHF COM, 8.33 kHz (P/N 822-1044-004)
Rockwell Collins ATC transponders, ELS / EHS (P/N 822-1338-003)
Airworks CDSS
L3 Communications micro QAR
Artex C406-1 fixed ELT
Artex ME406 portable ELT

Additional equipment

ADS-B Out
GFI
Wi-Fi server capable
LH, RH and additional centre fuel tanks
Two crew plus jumpseat
Fresh paint livery, newly applied

Interior

VIP business cabin, 44 seats (16 forward, 28 aft), in beige leather with navy piping. Club seating with conference table, burl-wood tables, powered seats and a VIP lavatory.

Exterior

Fresh paint livery, newly applied.

Specifications and descriptions are provided solely as introductory information and do not constitute representations or warranties. Verification of specifications remains the sole responsibility of the purchaser. The aircraft is subject to prior sale, lease, or removal from the market without notice. See our standard terms and conditions.

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