{"product_id":"mcdonnell-fh-1-phantom-manuals-collection","title":"McDonnell FH-1 Phantom — Pilot's Handbook \u0026 Engine Manuals Collection","description":"\u003ch3\u003eMcDonnell FH-1 Phantom — Primary-Source Documentation Collection\u003c\/h3\u003e\n\u003cp\u003eThe McDonnell FH-1 Phantom (originally designated XFD-1) holds a defining place in naval aviation history as the United States Navy's first purely jet-powered carrier-borne fighter aircraft. Its maiden flight on 26 January 1945 marked the threshold between the piston era and the jet age aboard American carriers. This collection assembles the original factory and military technical publications that governed the aircraft's operation, maintenance, and powerplant overhaul.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocuments in This Collection\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAN 01-245FA-1 — Pilot's Handbook for Navy Model FH-1 Airplanes\u003c\/strong\u003e\u003cbr\u003eDated 15 May 1949 \/ Revised 1 September 1949. Supersedes AN 01-245FA-1 dated 15 June 1948 \/ Revised 1 July 1948. Published under authority of the Secretary of the Air Force and the Chief of the Bureau of Aeronautics. Covers system checklists, emergency procedures, performance limits, and cockpit operating data.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAN 02B-110AA-2 — Handbook of Service Instructions for Models J30-P-20 and J30-WE-20 Aircraft Engines\u003c\/strong\u003e\u003cbr\u003eDated 15 June 1950 \/ Revised 1 March 1951. Supersedes AN 02B-110AA-2 dated 15 February 1950. Covers scheduled servicing, inspection intervals, and field-level maintenance procedures for the Westinghouse J30 axial-flow turbojet.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAN 02B-110AA-3 — Handbook of Overhaul Instructions for Models J30-P-20 and J30-WE-20 Aircraft Engines\u003c\/strong\u003e\u003cbr\u003eSupersedes AN 02B-110AA-3 dated 15 July 1948 \/ Revised 1 July 1949. Covers depot-level disassembly, inspection, repair, and reassembly procedures for the J30 powerplant.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eAerodynamic Profile \u0026amp; Geometry\u003c\/h3\u003e\n\u003cp\u003eThe FH-1 employed an aerodynamically conservative straight-wing layout, optimizing low-speed lift performance essential for unassisted carrier takeoffs and arrested landings.\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Area:\u003c\/strong\u003e 273.74 sq ft (25.43 m²) — low wing loading profile\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eHigh-Lift Devices:\u003c\/strong\u003e Split-flap systems to reduce stall margins in carrier landing configuration\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Fold System:\u003c\/strong\u003e Electrically actuated — span reduced from 40 ft 9 in to 16 ft 3 in for hangar deck stowage\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003ePowerplant — Westinghouse J30\u003c\/h3\u003e\n\u003cp\u003eThe FH-1's propulsion integration was its most pioneering engineering feature. Twin Westinghouse J30-WE-20 (originally designated 19XB-2B) axial-flow turbojet engines were buried within the thickened wing roots, eliminating the aerodynamic drag penalties of underwing pod installations. Tailpipes were canted slightly outward to protect the aluminum monocoque aft fuselage from thermal degradation.\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eStatic Thrust:\u003c\/strong\u003e 1,600 lbf (7.1 kN) per engine at max military RPM\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eHandling \u0026amp; Stability\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eEmpennage:\u003c\/strong\u003e Horizontal tailplane with distinct dihedral angle — specifically implemented to clear control surfaces from jet exhaust wash\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eControl System:\u003c\/strong\u003e Standard mechanical cable, pulley, and push-rod connections — no hydraulic boost; heavy stick forces at max dive limits\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePilot Visibility:\u003c\/strong\u003e Cockpit positioned far forward of the wing leading edge — exceptional over-the-nose visibility on carrier glide paths\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003ePerformance Data\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\n\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eValue\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Velocity\u003c\/td\u003e\n\u003ctd\u003e505 mph (813 km\/h) at 30,000 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruising Velocity\u003c\/td\u003e\n\u003ctd\u003e248 mph (399 km\/h)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eInitial Climb Rate\u003c\/td\u003e\n\u003ctd\u003e4,230 ft\/min (21.5 m\/s)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e41,100 ft (12,500 m)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Range\u003c\/td\u003e\n\u003ctd\u003e1,400 miles (2,300 km) with centerline belly tank\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e6,683 lb (3,031 kg)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Takeoff Weight\u003c\/td\u003e\n\u003ctd\u003e12,035 lb (5,459 kg)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/p\u003e\n\u003cp\u003e⚠️ \u003cstrong\u003eRegulatory Notice:\u003c\/strong\u003e Under FAA 14 CFR § 43.13 and EASA Part-M, any mechanic performing maintenance on an active aircraft must use current, manufacturer-approved revision-controlled data. This archival document does not satisfy that requirement.\u003c\/p\u003e\n\u003cp\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53731507929435,"sku":null,"price":40.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-4-square-prototype-takeoff.png?v=1786108159","url":"https:\/\/onlineaviationlibrary.com\/products\/mcdonnell-fh-1-phantom-manuals-collection","provider":"Online Aviation Library","version":"1.0","type":"link"}