McDonnell F4H-1 Phantom II — Primary-Source Technical & Engineering Archive

The 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.

Document Manifest

Aerodynamic Reports

• NASA/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
• Drag and static longitudinal stability profiles across dynamic Reynolds numbers
• Boundary Layer Control (BLC) reports — high-lift flap airflow manipulation studies

Engine Technical Notes

• General Electric J79 turbojet transition notes — J79-GE-2 to J79-GE-8 upgrade documentation
• F4H-1 Air Induction System Manual (F.S.R. 60-4, October 1960, McDonnell Aircraft) — 10-degree and 14-degree automatically controlled variable compression-ramp intake mechanics
• Variable stator compressor notes — adjustable blades optimized for variable-altitude fuel economy
• Hydraulic exhaust nozzle logs — oil-operated variable apertures during afterburner phase

Handling and Stability Studies

• Wing design geometry alterations resolving wing-tip stall anomalies at steep angles of attack
• 12-degree dihedral outer wing tip integration into the dogtooth layout — lateral stability correction
• 23.25-degree tailplane anhedral studies — downward tail angle verification to clear elevators from wing downwash
• Steady-heading/sideslip maneuver evaluations — short period and phugoid dynamic stability modes

Performance Data Sheets

• Standard Aircraft Characteristics (SAC) Sheet — 30 April 1960 — official range, loadout limitations, and speed limits
• NATOPS Flight Manual NAVWEPS 01-245FDA-1 — Navy Model F4H-1 (1 May 1961, Revised 1 July 1961) — BUWEPS Serial Numbers 145311b thru 148410g
• Flight Manual NAVWEPS 01-245FDA-1 — Navy Model F4H-1F (15 March 1962, Revised 15 September 1962) — Published by direction of the Chief of the Bureau of Naval Weapons
• Fuel burn/climb charts — internal fuel quantities vs. external centerline and wing pylon drop tank configurations

Structural Documentation

• F4H-1 Structure Manual (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
• Fuselage nomenclature documents — structural changes across canted and regular fuselage frame stations

Engineering Bulletins & Proposals

• F4H-1A USAF Tactical Fighter Proposal (Report No. 7182, 18 November 1959, Revised 1 January 1960, McDonnell Aircraft) — declassified Group 4 document
• Bureau of Naval Weapons (BuWeps) bulletins — airframe reworks including radar upgrade to Westinghouse AN/APQ-72
• Redesignation directives — May 1961 retroactive designation of first 47 airframes to the developmental F4H-1F standard

Test Pilot Reference

• Phantom Guide — A Guide to the F-4 (July 1983, USAF Test Pilot School, Edwards Air Force Base, California) — operational and handling characteristics reference

This 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.

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