This comprehensive archive brings together twelve original technical publications covering the Hawker Siddeley AV-8A and AV-8C Harrier — the first-generation V/STOL jets operated by the United States Marine Corps (USMC) and the Royal Air Force. From cross-servicing guides and airframe maintenance manuals to flight reference cards and structural repair documentation, this collection spans the full operational and engineering lifecycle of one of aviation's most revolutionary aircraft.

Definitive Collection with Free Lifetime Updates: This is a living collection that we continuously expand and refine. As we acquire additional AV-8A / AV-8C Harrier 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 Hawker Siddeley Harrier entered service with the Royal Air Force in 1969 as the world's first operational fixed-wing V/STOL combat aircraft. Its revolutionary Rolls-Royce Pegasus engine — with four rotating thrust-vectoring nozzles — enabled vertical takeoff, short-field operations, and the unique in-flight manoeuvre known as VIFF (Vectoring In Forward Flight). The USMC acquired the Americanized AV-8A variant (equivalent to the RAF's GR.Mk 1/GR.Mk 3) beginning in 1971, operating it from both land bases and amphibious assault ships. In 1979, 47 AV-8A airframes were upgraded to AV-8C standard, incorporating a Radar Warning Receiver (RWR), integrated flare/chaff dispensers, Lift Improvement Devices (LIDS), and structural life-extension modifications. The AV-8A/C series was powered by the Rolls-Royce Pegasus Mk 103 (F402-RR-401/403 in US service), rated at 21,500 lbf (95.6 kN) of thrust, with water injection providing short-duration thrust augmentation during V/STOL operations. Despite its demanding handling characteristics — earning the nickname "Widow-Maker" in early USMC service — the Harrier proved the viability of V/STOL combat aviation and directly led to the development of the AV-8B Harrier II.

Manuals Included in This Collection

• Hawker Siddeley Harrier GR Mk 1, 1A and 3 Aircraft Cross Servicing Guide — Air Publication 101B-0603-12, 1972
• Hawker Siddeley Harrier Engineering Aircraft Technical Brochure
• Hawker Siddeley Harrier Sky Jump Aircraft Technical Brochure — 1979
• Hawker Siddeley Harrier T Mk 8 Aircraft Airframe Maintenance Manual — Air Publication 101B-0608-1B, 1995
• Hawker Siddeley Harrier GR Mk 3 Aircraft Airframe Illustrated Parts Catalog — Air Publication 101B-0603-3A, 1979
• Hawker Siddeley Harrier New Weapon Aircraft Technical Brochure — 1969
• Hawker Siddeley Harrier GR Mk 3 and T Mk 4 Aircraft Flight Reference Cards — A.P. 101B-0603 & -4, 1984
• BAe / Hawker Siddeley / McDonnell Douglas AV-8A Aircraft Flight Manual — 1973
• BAe / Hawker Siddeley / McDonnell Douglas Mk.50 (AV-8A) Aircraft Service Manual — A.L. 47, 101B-00601-1, 1970
• BAe / Hawker Siddeley / McDonnell Douglas AV-8A / TAV-8A / AV-8C Aircraft Maintenance Manual — General Aircraft Information
• BAe / Hawker Siddeley / McDonnell Douglas AV-8A / TAV-8A / AV-8C Aircraft Structural Repair Manual with Illustrated Parts Breakdown — 01-AV8A-3-2.1
• BAe / Hawker Siddeley / McDonnell Douglas AV-8A / TAV-8A / AV-8C Aircraft Structural Repair Manual with Illustrated Parts Breakdown — 01-AV8A-3-2.2

This collection spans documentation from 1969 through 1995, covering the GR Mk 1, GR Mk 1A, GR Mk 3, T Mk 4, T Mk 8, AV-8A, TAV-8A, and AV-8C variants. Together, these publications provide an authoritative technical reference for the first-generation Harrier family across both RAF and USMC service.

Engineering Norms and Standards

The AV-8A/C series was governed by USMC and US Navy military airworthiness standards, with airframe documentation issued under the 01-AV8A series of technical orders. RAF documentation followed the Air Publication (AP) system under the 101B-0603 and 101B-0608 series. The Rolls-Royce Pegasus Mk 103 (F402-RR-401/403) was rated at 21,500 lbf thrust with a nozzle rotation range of 0° to 98.5°. Performance standards were defined in the AV-8A Standard Aircraft Characteristics (SAC) sheet of November 1972, specifying a maximum speed of 730 mph (635 knots) at sea level, service ceiling of 51,200 ft, and a combat radius of 230 miles with a 4,400 lb payload. Aerodynamic modeling was conducted by McDonnell Douglas (MDC Reports A1410 and A1400) and NASA (TM 88376), with V/STOL dynamics studied by the Naval Air Development Center (NADC Report 77024-30).

Format and Delivery

All manuals are delivered as high-resolution PDF files, optimized for both screen viewing and printing. Files are organized by document number and variant for easy navigation. Instant download upon purchase — no shipping required.

Disclaimer

These documents are provided for historical reference and research purposes only. They do not constitute current airworthiness guidance. Always consult the current Type Certificate holder and applicable regulatory authorities for operational use. Trade names and designations are the property of their respective owners. Copyright © Sicuro Publishing.