{"product_id":"mcdonnell-f4h-1-phantom-ii-primary-source-technical-engineering-archive","title":"McDonnell F4H-1 Phantom II — Primary-Source Technical \u0026 Engineering Archive","description":"\u003ch3\u003eMcDonnell F4H-1 Phantom II — Primary-Source Technical \u0026amp; Engineering Archive\u003c\/h3\u003e\n\u003cp\u003eThe historical technical and engineering records for the McDonnell F4H-1 Phantom II — later redesignated as the F-4A\/B — span vintage wind tunnel tests, early naval operating manuals, and propulsion field notes. This baseline documentation shaped the early development of the Mach 2+ fleet defense interceptor that would go on to define a generation of naval and air force aviation.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\n\u003ch4\u003eAerodynamic Reports\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003eNASA\/NTRS aerodynamic data (ref. NASA Citation 20090023600) — Langley Unitary Plan wind tunnel tests on 1\/20-scale models at supersonic ranges Mach 1.57–2.53\u003c\/li\u003e\n\u003cli\u003eDrag and static longitudinal stability profiles across dynamic Reynolds numbers\u003c\/li\u003e\n\u003cli\u003eBoundary Layer Control (BLC) reports — high-lift flap airflow manipulation studies\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eEngine Technical Notes\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003eGeneral Electric J79 turbojet transition notes — J79-GE-2 to J79-GE-8 upgrade documentation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eF4H-1 Air Induction System Manual\u003c\/strong\u003e (F.S.R. 60-4, October 1960, McDonnell Aircraft) — 10-degree and 14-degree automatically controlled variable compression-ramp intake mechanics\u003c\/li\u003e\n\u003cli\u003eVariable stator compressor notes — adjustable blades optimized for variable-altitude fuel economy\u003c\/li\u003e\n\u003cli\u003eHydraulic exhaust nozzle logs — oil-operated variable apertures during afterburner phase\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eHandling and Stability Studies\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003eWing design geometry alterations resolving wing-tip stall anomalies at steep angles of attack\u003c\/li\u003e\n\u003cli\u003e12-degree dihedral outer wing tip integration into the dogtooth layout — lateral stability correction\u003c\/li\u003e\n\u003cli\u003e23.25-degree tailplane anhedral studies — downward tail angle verification to clear elevators from wing downwash\u003c\/li\u003e\n\u003cli\u003eSteady-heading\/sideslip maneuver evaluations — short period and phugoid dynamic stability modes\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003ePerformance Data Sheets\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003eStandard Aircraft Characteristics (SAC) Sheet — 30 April 1960 — official range, loadout limitations, and speed limits\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNATOPS Flight Manual NAVWEPS 01-245FDA-1 — Navy Model F4H-1\u003c\/strong\u003e (1 May 1961, Revised 1 July 1961) — BUWEPS Serial Numbers 145311b thru 148410g\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlight Manual NAVWEPS 01-245FDA-1 — Navy Model F4H-1F\u003c\/strong\u003e (15 March 1962, Revised 15 September 1962) — Published by direction of the Chief of the Bureau of Naval Weapons\u003c\/li\u003e\n\u003cli\u003eFuel burn\/climb charts — internal fuel quantities vs. external centerline and wing pylon drop tank configurations\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eStructural Documentation\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eF4H-1 Structure Manual\u003c\/strong\u003e (SEDR 148, 1 September 1960, Technical Data Dept. 84) — Handbook of Structural Repair Instructions, NAVWEPS 01-245FDA-3, BIS Aircraft Numbers 145311–145317 and RCVG Aircraft Numbers 146817–146821 and 148252–148275\u003c\/li\u003e\n\u003cli\u003eFuselage nomenclature documents — structural changes across canted and regular fuselage frame stations\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eEngineering Bulletins \u0026amp; Proposals\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eF4H-1A USAF Tactical Fighter Proposal\u003c\/strong\u003e (Report No. 7182, 18 November 1959, Revised 1 January 1960, McDonnell Aircraft) — declassified Group 4 document\u003c\/li\u003e\n\u003cli\u003eBureau of Naval Weapons (BuWeps) bulletins — airframe reworks including radar upgrade to Westinghouse AN\/APQ-72\u003c\/li\u003e\n\u003cli\u003eRedesignation directives — May 1961 retroactive designation of first 47 airframes to the developmental F4H-1F standard\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eTest Pilot Reference\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003ePhantom Guide — A Guide to the F-4\u003c\/strong\u003e (July 1983, USAF Test Pilot School, Edwards Air Force Base, California) — operational and handling characteristics reference\u003c\/li\u003e\n\u003c\/ul\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\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":53729629143387,"sku":"OAL-F4H1-PHANTOM-ARCHIVE","price":39.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-b-overhead-planform.png?v=1786090759","url":"https:\/\/onlineaviationlibrary.com\/products\/mcdonnell-f4h-1-phantom-ii-primary-source-technical-engineering-archive","provider":"Online Aviation Library","version":"1.0","type":"link"}