Hawker Siddeley HS.748 / Avro 748 Andover Aircraft Aeroplane Manuals Collection
This is a comprehensive, curated collection of technical documentation for the Hawker Siddeley HS.748 and its military Andover variants — one of Britain's most capable and enduring regional turboprops. Spanning flight operations, maintenance, structural repair, illustrated parts, and pilot notes, this collection provides the essential reference library for operators, restorers, historians, and A&P mechanics working with this aircraft.
Definitive Collection with Free Lifetime Updates
This is a living collection that we continuously expand and refine. As we acquire additional HS.748 / Avro 748 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 Avro 748 was conceived in the late 1950s by A.V. Roe & Co. (Avro) as a rugged, economical short-haul turboprop for regional and feeder routes — particularly suited to semi-prepared and short runways. The prototype first flew on 24 June 1960, and the type entered service with Indian Airlines in 1961. When Avro was absorbed into the Hawker Siddeley Group, the aircraft was redesignated the Hawker Siddeley HS.748.
Powered by two Rolls-Royce Dart turboprops — typically the RDa.7 Mk 534-2 or Mk 535-2 delivering 1,700 kW (2,280 ehp) each — and fitted with 4-bladed Dowty Rotol constant-speed, fully-feathering reverse-pitch propellers, the HS.748 was optimised for STOL performance. Its large Fowler flaps, low-wing pressurised cabin, and robust undercarriage made it ideal for operations in Africa, South America, Southeast Asia, and the Indian subcontinent. The Series 2A (MTOW 21,092 kg / 46,500 lb) became the definitive production standard, with a cruise speed of approximately 244 knots (452 km/h).
The military Andover variant (HS.780 / Andover C Mk.1) introduced a rear loading ramp and a distinctive kneeling main undercarriage that lowered the fuselage for direct cargo loading — a significant tactical logistics capability. The Andover CC Mk.2 served as a VIP transport with the RAF. Both variants are documented in this collection through their respective Pilot's Notes.
Over 380 HS.748s were built, serving with more than 50 operators worldwide. The type remains in limited service today, and its documentation is actively sought by restoration teams, type clubs, and aviation historians. The EASA Type Certificate (TCDS A.397) covers all civil variants.
Manuals Included in This Collection
- Avro / BAe / Hawker Siddeley 748 Aircraft Training Manual
- Avro / BAe / Hawker Siddeley 748 Series 2A Model 345 Aircraft Type Specification Manual
- Avro / BAe / Hawker Siddeley 748 Series 2A Model 283 Aircraft Weight and Load Manual
- Avro / BAe / Hawker Siddeley 748 Series 2A Aircraft Flight Manual
- Avro / BAe / Hawker Siddeley 748 Series 2A Aircraft Maintenance Manual
- Avro / BAe / Hawker Siddeley 748 Series 2A Aircraft Illustrated Parts Catalog Manual
- Avro / BAe / Hawker Siddeley 748 Series 2A Aircraft Structural Repair Manual — 1961
- Avro / BAe / Hawker Siddeley 748 Aircraft Service Bulletins Manual
- A.V. Roe Avro 748 Aircraft Series 2 Type Record General Data Manual
- A.V. Roe Avro Andover CC Mk.2 Aircraft Pilot's Notes Manual
- A.V. Roe Avro Andover C Mk.1 Aircraft Pilot's Notes Manual
This collection spans the full operational lifecycle of the HS.748 and Andover family — from initial type specification and weight & balance data through to structural repair, illustrated parts, and military variant pilot notes. Coverage includes Series 2A civil variants (Models 283 and 345) and both Andover military marks.
Engineering Norms and Standards
The HS.748 was designed to British Civil Airworthiness Requirements (BCAR) and military equivalents, with a fail-safe structural philosophy emphasising ease of maintenance and accessibility — all servicing points were positioned at shoulder height to eliminate the need for access platforms. Military variants were built to Air Publication (AP) standards. The EASA TCDS A.397 defines the current certification basis for all civil variants, including CG ranges, weight limits, and propeller RPM restrictions (continuous operation between 8,500 and 9,500 RPM is prohibited). Ground running requires the aircraft to face into wind within 60° when wind velocity exceeds 15 knots. Known engineering bulletins address hydraulic system cold-weather sensitivities, axle nut wear, and gust lock system modifications introduced following the 1979 Sumburgh accident investigation.
Format and Delivery
All manuals are supplied as high-resolution PDF files, optimised for both on-screen reference and print use. Files are delivered instantly upon purchase via secure download link. Documents are clearly named and organised by type for straightforward navigation across the collection.
Disclaimer
All documents in this collection are provided for historical reference and research purposes only. They do not constitute current airworthiness data. For active maintenance and operations, always consult the current Type Certificate holder and applicable regulatory authority. All trade names and designations remain the property of their respective owners. Copyright © Sicuro Publishing.