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Single-Engine Piston

1970 BAC MK5A PROVOST

$120,000 fyiEstimate $220,000–$225,500 How this estimate is built

Starts from the median asking price of 3236 comparable Single-Engine Piston listings ($275,000), then adjusts for:

  • Year -31 vs comparable listings -20.0%
  • Garmin GTN 750Xi (uncommon in comps) +3.5%
  • Modern GPS navigator (uncommon in comps) +3.0%
  • Market supply: 2 for sale of 2 FAA-registered -5.0%

Shown as a range. An estimate from asking-price comparables and FAA supply data — not an appraisal.

1970
N287XW
XW287
1
42A
📍 Rockford, Illinois
Ozark Aerosports LLC
Per the FAA aircraft registry (public record)

Overview

Make / ModelBAC MK5A PROVOST
TypeSingle-Engine Piston
Airframe time
Avionics / GPSGarmin GTN 750Xi
Avionics / TransponderGarmin GTX 345
ADS-BYes
AnnualMarch 2026
InspectionAnnual
Garmin GPS ADS-B

Description

7288 Hours TTSNEW

Modifications

Drop Tanks installed US standard oxygen system Smoke System Ejection Seats (Cold) Solid state Inverter 2 Seat Pack Parachutes Included

Avionics

Garmin GTN-750xi GPS/ NAV/ COM Garmin GTX-345 Transponder Garmin GTR-200 COM Garmin GMA-240 Audio Control Panel Garmin G-5 Electric Flight Instrument Garmin G-5 Electric Flight Instrument Garmin GMU11 Magnetometer Garmin GA35 WAAS GPS Antenna

General

Year1970
ManufacturerBAC
ModelMK5A PROVOST
Registration #N287XW
Serial NumberXW287
ConditionUsed
Based at42A
Total Time7,288
Number of Seats2

Avionics

ADS-B EquippedYes
Avionics/RadiosGarmin GTN-750xi GPS/ NAV/ COM Garmin GTX-345 Transponder Garmin GTR-200 COM Garmin GMA-240 Audio Control Panel Garmin G-5 Electric Flight Instrument Garmin G-5 Electric Flight Instrument Garmin GMU11 Magnetometer Garmin GA35 WAAS GPS Antenna

Additional Equipment

Additional EquipmentDrop Tanks installed US standard oxygen system Smoke System Ejection Seats (Cold) Solid state Inverter 2 Seat Pack Parachutes Included

Inspection Status

Inspection StatusTransponder check completed March 2026 Annual Inspection completed February 2026 Completed Logs Since 2018 No known accident history Aircraft flown by early British Demo Team, Red Pelicans PERFORMANCE SPECS: Specification BAC Jet Provost T.5 Engine 1 × Armstrong Siddeley Viper Mk.202 turbojet Thrust 2,500 lbf (11.1 kN) Crew 2 (side-by-side seating) Length 34 ft 0 in (10.36 m) Wingspan 35 ft 4 in (10.77 m) Height 10 ft 2 in (3.10 m) Empty Weight 4,888 lb (2,222 kg) Max Takeoff Weight 9,200 lb (4,173 kg) Maximum Speed 440 mph (382 kt / 708 km/h) at 25,000 ft Cruise Speed ~390 mph Range 900 mi (780 nm / 1,450 km) Service Ceiling 36,750 ft Rate of Climb 4,000 ft/min Wing Loading 32.7 lb/ft² The Rolls Royce Viper is an excellent engine used in many civilian and military applications. Manuals and support are excellent. Contact Courtesy Aircraft to schedule an inspection- located at 42A SPECIFICATIONS SUBJECT TO VERIFICATION UPON INSPECTION