Name: North American FJ Fury - Comprehensive Aircraft Manuals Collection
Brand: Online Aviation Library
Price: 60.00 EUR
Availability: InStock

North American FJ Fury - Comprehensive Aircraft Manuals Collection

€60,00

North American FJ Fury — Comprehensive Aircraft Manuals Collection

This primary-source digital collection brings together authentic flight handbooks, supplemental flight handbooks, illustrated parts breakdowns, maintenance instructions, and inspection requirement handbooks covering all four variants of the North American FJ Fury — from the straight-wing FJ-1 to the fully redesigned FJ-4B. These are original U.S. Navy technical publications, preserved as issued, spanning the entire operational life of America's first carrier-based jet fighter series.

Manuals Included in This Collection:

FJ-1 Fury

Flight Handbook — Navy Model FJ-1 Aircraft

FJ-2 Fury

Flight Handbook — Navy Model FJ-2 Aircraft
Illustrated Parts Breakdown — Navy Model FJ-2 Aircraft (incomplete archival copy)

FJ-3 / FJ-3M Fury

Flight Handbook — Navy Model FJ-3 Aircraft — AN 01-60JKC-1
Supplemental Flight Handbook — Navy Models FJ-3 • FJ-3M Aircraft — NAVAER 01-60JKC-501A, 1 February 1956 (Revised 1 November 1956) — CONFIDENTIAL, to be used in conjunction with AN 01-60JKC-1
Handbook Inspection Requirements — Intermediate and Major, Navy Models FJ-3, -3M Aircraft — NAVAER 01-60JKC-507, 1 June 1958 (supersedes NAVAER 01-60JKC-507 dated 1 July 1957)
Handbook Inspection Requirements — Daily and Preflight, Navy Models FJ-3, -3M Aircraft — NAVWEPS 01-60JKC-6, 15 November 1960 (supersedes NAVAER 01-60JKC-6 dated 1 March 1959 revised 15 October 1959)

FJ-4 / FJ-4B Fury

Flight Handbook — Navy Models FJ-4 • FJ-4B Aircraft — NAVAER 01-60JKD-501, 1 October 1957 (supersedes NAVAER 01-60JKD-501 dated 1 January 1957 revised 1 July 1957) — to be used in conjunction with Supplemental Flight Handbook NAVAER 01-60JKD-501A
Supplemental Flight Handbook — Navy Models FJ-4 • FJ-4B Aircraft — NAVAER 01-60JKD-501A, 1 October 1957 (Revised 1 February 1959) — CONFIDENTIAL, to be used in conjunction with NAVAER 01-60JKD-501
Illustrated Parts Breakdown — Navy Models FJ-4 • FJ-4B Aircraft — NAVAER 01-60JKD-504, 1 April 1958 (Revised 1 July 1959) — Revision Notice edition
Handbook Inspection Requirements — Intermediate and Major, Navy Models FJ-4, -4B Aircraft — NAVWEPS 01-60JKD-7, 15 November 1960 (supersedes NAVAER 01-60JKD-7 dated 1 March 1959)
Handbook Inspection Requirements — Daily and Preflight, Navy Models FJ-4, -4B Aircraft — NAVWEPS 01-60JKD-6, 15 November 1960 (supersedes NAVAER 01-60JKD-6 dated 1 March 1959)
Handbook Maintenance Instructions — Navy Model FJ-4B Aircraft — NAVAER 01-60JKE-502, Table of Contents, 1 August 1957 (Revised 1 November 1958) — Revision Notice edition

Engineering & Operational Background

The engineering and operational history of the North American FJ Fury series represents a critical bridge in early naval jet aviation, evolving from the straight-wing FJ-1 to the highly advanced, swept-wing transonic FJ-4. The primary technical documentation, engineering profiles, and performance data across these variants reveal significant developments in design and operation.

Aerodynamic & Design Evolution: The FJ-1 was designed as a straight-wing, thick-bodied monoplane — aerodynamic reports noted it quickly became subsonic-limited, which led to a shortened deployment life as swept-wing data became available. To survive carrier approach requirements, the FJ-2 and FJ-3 introduced a 35° wing sweep; later FJ-3 variants added camber to the underside of the leading edge to significantly stabilize low-speed handling. The FJ-4 featured a complete wing overhaul — a much thinner, highly tapered airfoil with a reduced thickness ratio to decrease high-speed drag, increasing internal fuel storage capacity by 50%.

Engine Technical Notes: The FJ-1 was powered by an Allison J35-A-2 turbojet producing roughly 3,820–4,000 lbf of dry thrust, with an 11-stage axial compressor and multi-can combustion system. The FJ-2 transitioned to the General Electric J47-GE-2 (borrowed from the F-86 Sabre program) to handle the increased weight of navalization gear. The FJ-3 and FJ-4 upgraded to the Wright J65 turbojet — a licensed version of the British Armstrong Siddeley Sapphire — boosting output to 7,700 lbf. Fleet technical notes warned about early J65 lubrication system vulnerabilities under severe catapult-launch accelerations.

Handling & Stability: Navalizing a land-based fighter for carrier operations required deep stability interventions. NACA spin tunnel and handling studies forced engineers to add leading-edge slats and modified control surfaces to address the poor low-speed lift profile of swept wings. Flight testing of the FJ-2 and FJ-3 identified tracking issues caused by an excessive downward engine thrust angle — corrected in the FJ-4 by leveling the fuselage design. The FJ-1 also featured a specialized nosewheel strut allowing the aircraft to "kneel" nose-down to save storage space aboard carriers.

Performance Growth Across Variants:

Maximum Speed: 475 knots (FJ-1) → 590 knots (FJ-4B)
Service Ceiling: 32,005 ft (FJ-1) → 46,800 ft (FJ-4B)
Max Takeoff Weight: 15,600 lbs (FJ-1) → 23,700 lbs (FJ-4B)
Maximum Range: 1,301 nm (FJ-1) → 2,020 miles (FJ-4B)
Primary Armament: Six .50-cal machine guns (FJ-1) → 4× 20mm cannons / Bullpup missiles (FJ-4B)