{"product_id":"mcdonnell-xf-88-voodoo-erection-maintenance-pilot-flight-operating-instructions","title":"McDonnell XF-88 Voodoo — Erection \u0026 Maintenance Instructions + Pilot's Flight Operating Instructions","description":"\u003ch2\u003eMcDonnell XF-88 Voodoo — Primary-Source Technical Documentation\u003c\/h2\u003e\u003cp\u003eTwo original factory-issued manuals for the USAF Model XF-88 Voodoo, manufactured by McDonnell Aircraft Corporation. This archival set covers both ground handling and airborne operations for one of the most significant penetration fighter prototypes of the early jet age — the direct ancestor of the legendary F-101 Voodoo.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDocuments Included\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eMAC Report No. 1033\u003c\/strong\u003e — Handbook of Erection and Maintenance Instructions, USAF Model XF-88\u003cbr\u003e\u003cem\u003eAircraft:\u003c\/em\u003e McDonnell XF-88 Voodoo · \u003cem\u003eContent:\u003c\/em\u003e Erection and maintenance instructions · \u003cem\u003eLength:\u003c\/em\u003e 25 pages · \u003cem\u003eType:\u003c\/em\u003e Military technical handbook\u003cbr\u003eA historical United States Air Force technical manual covering assembly, ground handling, and servicing guidelines for the experimental twin-jet penetration fighter prototype developed by McDonnell Aircraft.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eReport No. 1032\u003c\/strong\u003e — Pilot's Handbook: Flight Operating Instructions, USAF Model XF-88 Aircraft (Preliminary \/ Unclassified)\u003cbr\u003eSerial Nos. 46-525 \u0026amp; 46-526 · MFG Model Designation 36\u003cbr\u003ePowered by two Westinghouse J34-WE-22 turbojet engines (Engine MFG \u0026amp; Model Designation: Westinghouse–24C)\u003cbr\u003eContract W33-038-AC-14582 · Specification S-148\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eEngineering \u0026amp; Aerodynamic Background\u003c\/h3\u003e\u003ch4\u003e1. Aerodynamic Configuration\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003e35-degree swept-back wings with modified high-chord ailerons requiring structural stiffening against wing twist\u003c\/li\u003e\n\u003cli\u003eInitial V-tail design abandoned after wind-tunnel instability findings; replaced with conventional mid-mounted tailplane\u003c\/li\u003e\n\u003cli\u003eSevere nose-down pitch (tucking under) and aileron effectiveness loss at high Mach numbers due to span loading shifts\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003e2. Engine \u0026amp; Airframe Integration\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eTwo Westinghouse turbojets mounted side-by-side in the lower-mid fuselage with wing-root air intakes\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eXF-88:\u003c\/strong\u003e Non-afterburning J34-WE-13 (3,000 lbf each) — deemed underpowered\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eXF-88A:\u003c\/strong\u003e Short-afterburning J34-WE-15 (3,600 lbf each) — +34% baseline thrust\u003c\/li\u003e\n\u003cli\u003eSpring-loaded blow-in auxiliary intake doors added to combat S-duct choking on takeoff\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003e3. Handling, Stability \u0026amp; NACA Flight Research\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eXF-88A introduced an all-moving stabilator for transonic longitudinal authority\u003c\/li\u003e\n\u003cli\u003eSpeed brake deployment restricted at high speed due to severe aft-fuselage buffeting\u003c\/li\u003e\n\u003cli\u003eRoll rate improved 26% via chord expansion; wingtip fuel tanks degraded high-alpha maneuverability\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eXF-88B Propeller Testbed:\u003c\/strong\u003e First prototype fitted with a nose-mounted 2,500 shp Allison XT38 turboprop; evaluated supersonic propeller blades at NACA Langley through 1956, achieving Mach 1.0+ in dives\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003e4. Performance Data\u003c\/h4\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eXF-88 (J34-WE-13)\u003c\/th\u003e\n\u003cth\u003eXF-88A (J34-WE-15)\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Level Speed\u003c\/td\u003e\n\u003ctd\u003e641 mph (1,032 km\/h)\u003c\/td\u003e\n\u003ctd\u003e~700 mph (1,126 km\/h)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Terminal Dive Speed\u003c\/td\u003e\n\u003ctd\u003eSubsonic \/ Transonic\u003c\/td\u003e\n\u003ctd\u003eMach 1.175\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eTime to 30,000 ft\u003c\/td\u003e\n\u003ctd\u003eN\/A\u003c\/td\u003e\n\u003ctd\u003e4.0 minutes\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eInternal Fuel Capacity\u003c\/td\u003e\n\u003ctd\u003e~734 gallons\u003c\/td\u003e\n\u003ctd\u003e834 gallons (bladder cells)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCombat Radius\u003c\/td\u003e\n\u003ctd\u003eUnmet target\u003c\/td\u003e\n\u003ctd\u003e900 miles (1,450 km)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003ch4\u003e5. Engineering Legacy\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eProgram canceled 1950 due to shifting USAF tactical budgets and high afterburner fuel consumption\u003c\/li\u003e\n\u003cli\u003eStructural blueprints and flight test data directly informed the design of the supersonic McDonnell F-101 Voodoo\u003c\/li\u003e\n\u003cli\u003eStaggered wing-root intake and belly exhaust scheme later applied to the F3H Demon and F-4 Phantom II\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\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\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.\u003cbr\u003e\u003cstrong\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/strong\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53731095183707,"sku":null,"price":14.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/xf-88-voodoo-colour-front-on.png?v=1786103741","url":"https:\/\/onlineaviationlibrary.com\/products\/mcdonnell-xf-88-voodoo-erection-maintenance-pilot-flight-operating-instructions","provider":"Online Aviation Library","version":"1.0","type":"link"}