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Hunting Percival Jet Provost & BAC Strikemaster Aircraft Manuals Collection

This is a comprehensive, curated collection of official technical publications covering the Hunting Percival P.84 Jet Provost and its combat-capable derivative, the BAC 167 Strikemaster. From the earliest T.1 prototype to the Mk.5A and the export Strikemaster Mk.83, this collection spans the full operational and instructional life of Britain's most successful jet trainer family — bringing together illustrated parts catalogs, aircrew manuals, maintenance publications, flying instructor handbooks, flight reference cards, and engine servicing notes into a single authoritative digital archive.

Definitive Collection with Free Lifetime Updates

This is a living collection that we continuously expand and refine. As we acquire additional Jet Provost and Strikemaster documentation, technical bulletins, or variant-specific materials, we update this collection and provide free lifetime updates to all purchasers. Your one-time purchase guarantees access to all future additions and improvements to this collection.

Historical Note

The Hunting Percival P.84 Jet Provost emerged in the early 1950s as Britain's answer to the challenge of all-through jet training — the concept that student pilots could progress from first flight to advanced instruction entirely on jet aircraft, without the intermediate step of a piston-engine trainer. The prototype XD674 first flew in June 1954, mating the wing structure of the piston-engine Percival Provost to a new fuselage lengthened by 3 feet to accommodate the Armstrong Siddeley Viper Mk.102 turbojet. Early trials at RAF Boscombe Down revealed pleasant handling characteristics, though the initial long stalky undercarriage was redesigned for production models, along with refined fuselage lines and a switch from pneumatic to hydraulic systems for landing gear, flaps, and air brakes.

Production variants progressed through the T.1, T.2, T.3, and T.3A — each incorporating aerodynamic refinements including leading-edge extensions at the wing roots and a ventral fin — before the definitive T.4 introduced the Bristol Siddeley Viper Mk.202, delivering approximately 40% more thrust than the T.3's engine. The T.Mk.5 and Mk.5A followed with pressurised cockpits and further performance improvements, achieving a maximum speed of 440 mph at 25,000 ft and a service ceiling of 36,750 ft. The airframe was stressed to +6g / -2.5g, with a NACA 23015 (modified) wing section at the root and NACA 4412 (modified) at the tip, set at 6° dihedral and 3.5° root incidence for inherent training stability.

The BAC 167 Strikemaster — developed from the Jet Provost T.Mk.5 — transformed the trainer into a capable light attack and counter-insurgency (COIN) platform. Powered by the Rolls-Royce Viper Mk.535 producing 3,410 lb.s.t., the Strikemaster offered a maximum speed of 418 knots at 18,000 ft, a service ceiling of 40,000 ft, and a rate of climb of 5,250 ft/min. Four underwing hardpoints carried up to 3,000 lb of ordnance. The aircraft served with the air forces of Saudi Arabia, New Zealand, Oman, Ecuador, Kenya, Kuwait, Singapore, and Sudan, among others. The RNZAF Mk.88 variant was later subject to wing fatigue restrictions, while Omani aircraft received armour plating for low-level operations. All variants were equipped with Martin-Baker Mk.4 ejection seats.

Manuals Included in This Collection

  • Percival Jet Provost Mk.4 — Illustrated Parts Catalog
  • Percival Jet Provost — Aircraft Maintenance Manual: Electrical Systems (AP 101B-2303-1B)
  • Percival Jet Provost — General and Technical Manual, AP 4560A Vol I (1955)
  • Percival Jet Provost T Mk.3A — Aircrew Manual (AP 101B-2303A-15, March 1975)
  • Percival Jet Provost T2 & T4 — Flying Instructor's Handbook, AP 3225 D (1962)
  • Percival Jet Provost Mk.5 & Mk.5A — Flight Reference Cards, AP 101B-2305-14 (1976)
  • BAe/BAC Strikemaster Mk.83 — Illustrated Parts Catalog, Book 1
  • BAe/BAC Strikemaster Mk.83 — Illustrated Parts Catalog, Book 2
  • BAE BAC 145 Mk.55 — Pilot's Notes (Sudan Air Force, November 1968)
  • Bristol Siddeley Viper Series 8 in Provost Aircraft — Instructional Notes, Issue 3 (Gas Turbine School, Bristol Siddeley Engines Limited, Ansty, Coventry)

This collection covers the full variant spectrum from the early T.1/T.2 through the T.3A, T.4, Mk.5/5A, and the export Strikemaster Mk.83 and Mk.55, with documentation dating from 1955 through 1976. The engine servicing notes provide an authoritative technical reference for the Viper Series 8 powerplant as installed in the Provost airframe, covering 15 sections from leading particulars and limitations through to preservation and storage.

Engineering Norms and Standards

The Jet Provost family was designed and maintained to British military airworthiness standards, with Air Publications (AP) forming the backbone of the technical documentation system. Key engineering parameters include: Viper Mk.102 (1,750 lbf) and Viper Mk.202 (2,500 lbf) engine data; pneumatic-to-hydraulic system conversions on production models; Centralized Warning Panel and oxygen system installations on later marks; and structural reinforcement of the main wing spar for higher-speed operations. The Strikemaster introduced the Rolls-Royce Viper Mk.535 (3,410 lbf), with critical handling notes on engine spool-up below 55% RPM, a Fatigue Index multiplication factor of 1.9 for civil operators, and spinning limitations requiring empty tip tanks and internal fuel not exceeding 1,600 lbs. The Bristol Siddeley Viper Series 8 engine limitations include: Take-off RPM 13,800 (100% ±5%), Max JPT 725°C; Max Continuous 13,300 RPM (95%), JPT 655°C; Ground Idling 5,500 ±200 RPM.

Format and Delivery

All manuals are delivered as high-resolution PDF files, optimised for both on-screen reference and print. Instant download upon purchase — no shipping, no waiting.

Disclaimer

These publications are provided for historical reference and research purposes. They do not constitute current airworthiness documentation. Operators of airworthy aircraft must consult current approved data from the relevant authority. Copyright © Sicuro Publishing.

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