McDonnell Douglas F-4J Phantom II

Primary-Source Technical Documentation Collection — 4 Documents

The F-4J was the definitive US Navy fleet air defense and strike variant of the Phantom II — an extensively upgraded evolution of the F-4B that introduced the AN/AWG-10 pulse-Doppler fire control system, AN/AJB-7 bombing computer, slotted stabilator, drooped ailerons, and the General Electric J79-GE-10 engines with their distinctive extended afterburner variable ejector leaves. Entering service in 1966, the F-4J became the primary fleet interceptor and strike aircraft of the US Navy and Marine Corps through the Vietnam War and into the 1980s, serving with distinction aboard carriers from the Gulf of Tonkin to the Mediterranean.

This collection assembles 4 primary-source NAVAIR publications covering the full operational life of the F-4J — from the 1969 Blue Angels supplemental data through the 1988 final-service pocket checklist — including two distinct change states of the definitive NATOPS flight manual.

Document Manifest — 4 Primary-Source Documents

1. NAVAIR 01-245FDD-1
NATOPS Flight Manual — Navy Model F-4J Aircraft
McDonnell Aircraft · NOw(A)65-0044-f / N00019-73-A-0017 · 15 February 1973
Supersedes NAVAIR 01-245FDD-1 dated 1 June 1971, Changed 15 September 1972
The 1973 edition of the F-4J NATOPS flight manual — the primary operational reference for F-4J crews during the final years of the Vietnam War. Documents the full F-4J systems configuration including the AN/AWG-10 pulse-Doppler fire control system, J79-GE-10 powerplant, and all normal, emergency, and special procedures.

2. NAVAIR 01-245FDD-1
NATOPS Flight Manual — Navy Model F-4J Aircraft
Naval Air Systems Command · 1 May 1975
The 1975 edition with full tabbed index across 11 chapters: Aircraft, Indoctrination, Normal Procedures, Flight Characteristics, Emergency Procedures, All-Weather Operation, Communications Procedures, Weapons Systems, Flight Crew Coordination, NATOPS Evaluation, Performance Data, and Appendix Foldout Illustrations.

3. NAVAIR 01-245FDD-1B
NATOPS Pilot's Pocket Checklist — F-4J/S Aircraft
Naval Air Systems Command · S/N 0801-LP-142-0070 · 1 December 1988
Supersedes NAVAIR 01-245FDD-1B dated 1 May 1975, Changed 1 May 1985
Distribution Statement C — US Government agencies and contractors only
The final-service NATOPS pocket checklist covering both the F-4J and F-4S (the leading-edge slat-equipped upgrade variant). The compact checklist format used by Navy and Marine Corps Phantom crews through the type's retirement from US service.

4. NAVAIR 01-245FDE-1
Flight Operating Difference / Supplemental Data — Navy Model F-4J Aircraft
Flight Demonstration Team Aircraft Configuration — Blue Angels
Naval Air Systems Command · 1 May 1969 / Change 4 – 1 August 1972
One of the rarest documents in the F-4J series — the official supplemental flight data for the F-4J in Blue Angels configuration. Documents systems modifications, performance differences, and operating limitations unique to the Blue Angels display aircraft, including formation flying parameters, smoke system operation, and the precise aerobatic envelope limits flown from 1969 through 1974.

Aircraft Technical Overview

Aerodynamic Configuration

The F-4J retains the core Phantom II aerodynamic architecture — 45° swept wing with 12° wingtip dihedral and 23° anhedral all-moving stabilator — with two key improvements over the F-4B: a slotted stabilator for increased low-speed pitch authority, and drooped ailerons for improved roll control at high angles of attack. Boundary Layer Control (BLC) uses high-pressure engine bleed air over leading and trailing edge flaps to enhance lift coefficients during carrier approaches.

Powerplant — General Electric J79-GE-10

Twin J79-GE-10 axial-flow turbojets, each delivering 11,810 lbs dry thrust and 17,900 lbs with afterburner. Visually distinguished by extended afterburner variable ejector leaves — the “turkey feathers” — which improve afterburner efficiency and reduce infrared signature. Variable stator compressors and a VEN mechanically operated by engine oil pressure minimize EGT spiking during afterburner transitions.

Performance Envelope

Stability & Handling

Three-axis analog Stability Augmentation System (SAS) provides artificial damping to correct high-altitude adverse yaw and Dutch roll oscillations. Primary roll and yaw transitions via trailing-edge ailerons coupled with upper-surface wing spoilers. Spin recoveries demand strict neutral control configurations due to high inertial coupling along the fuselage axis.

⚠️ Regulatory Notice: 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.

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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