{"product_id":"mcdonnell-douglas-f-4c-f-4d-phantom-ii-technical-documentation","title":"McDonnell Douglas F-4C \/ F-4D Phantom II — Primary-Source Technical Documentation","description":"\u003ch2\u003eMcDonnell Douglas F-4C \/ F-4D Phantom II\u003c\/h2\u003e\u003ch3\u003ePrimary-Source Technical Documentation Collection\u003c\/h3\u003e\u003cp\u003eThe F-4 Phantom II is one of the defining combat aircraft of the Cold War era — a Mach 2+ twin-engine interceptor and fighter-bomber that served as the backbone of USAF tactical aviation from the early 1960s through the Vietnam War and beyond. This collection assembles primary-source USAF Technical Orders, McDonnell Aircraft engineering reports, maintenance manuals, armament systems documentation, and structural repair instructions covering the F-4C and F-4D variants specifically — the two principal USAF Phantom configurations of the 1960s and early 1970s.\u003c\/p\u003e\u003cp\u003eDocuments span airframe, powerplant, avionics, armament, structural repair, and flight control systems — providing the depth of coverage demanded by serious researchers, restorers, historians, and simulation specialists.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDocument Manifest — 11 Primary-Source Documents\u003c\/h3\u003e\u003cp\u003e\u003cstrong\u003e1. T.O. 1F-4C-4-1\u003c\/strong\u003e\u003cbr\u003eIllustrated Parts Breakdown — Airframe (F-4C \/ F-4D)\u003cbr\u003eMcDonnell Aircraft · Change 21 · November 1971\u003cbr\u003e\u003cem\u003eComprehensive airframe parts breakdown with ATA-structured component identification across all major structural assemblies.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003e2. Pilot's J79 Emergency Procedures for the F-4C Installation\u003c\/strong\u003e\u003cbr\u003eGeneral Electric Company\u003cbr\u003e\u003cem\u003eEngine-specific emergency procedures for the J79-GE-15 installation in the F-4C, covering compressor stalls, afterburner malfunctions, and emergency shutdown sequences.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003e3. F-4C \/ F-4D \/ F-4E Armament Systems\u003c\/strong\u003e\u003cbr\u003eMcDonnell Douglas · P.S. 217 · Rev. 1 December 1967\u003cbr\u003e\u003cem\u003eArmament systems documentation covering weapons integration, electrical routing, and delivery configurations across the F-4C, D, and E variants.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003e4. TO 1F-4C-35\u003c\/strong\u003e\u003cbr\u003eNon-Munitions Accessories — Installation, Checkout \u0026amp; Removal (F-4C \/ F-4D \/ F-4E \/ RF-4C)\u003cbr\u003eApril 1972 · Change 24\u003cbr\u003e\u003cem\u003eCovers installation and removal procedures for non-munitions accessories across all principal Phantom variants.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003e5. T.O. 1F-4C-2-8\u003c\/strong\u003e\u003cbr\u003eMaintenance Instructions — Power Plant, F-4C\u003cbr\u003eMcDonnell Aircraft · March 1972 · Change 24\u003cbr\u003e\u003cem\u003eFull maintenance instructions for the J79-GE-15 powerplant installation in the F-4C, including removal, installation, and ground run procedures.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003e6. T.O. 1F-4C-3-1-1\u003c\/strong\u003e\u003cbr\u003eStructural Repair Organizational \u0026amp; Field — General Information (F-4C \/ F-4D \/ F-4E \/ RF-4C)\u003cbr\u003eMcDonnell Douglas · N00019-69-C-0521 · 15 October 1971\u003cbr\u003e\u003cem\u003eStructural repair manual covering organizational and field-level repair procedures for the F-4 series airframe, including wing spar, fuselage, and control surface repair data.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003e7. T.O. 1F-4C-34-1-1CL-1\u003c\/strong\u003e\u003cbr\u003eAircrew Weapons Delivery Checklist (Nonnuclear) — F-4C \/ F-4D \/ F-4E\u003cbr\u003eMcDonnell Aircraft · NOw(A) 64-0001-f · 1 June 1971 · Change 8, 22 February 1973\u003cbr\u003e\u003cem\u003eOperational checklist for nonnuclear weapons delivery procedures, covering all standard delivery modes for the F-4C, D, and E.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003e8. TO 1F-4D-2-16\u003c\/strong\u003e\u003cbr\u003eMaintenance Instructions — Automatic Flight Control System, F-4D\u003cbr\u003eMcDonnell Aircraft · N00019-71-A-0011 · 15 January 1972 · Change 53, 1 October 1989\u003cbr\u003e\u003cem\u003eComprehensive maintenance manual for the AN\/ASA-32H Automatic Flight Control System (AFCS) on the F-4D, covering the three-axis stability augmentation system (pitch, roll, yaw) and Dutch roll damping subsystems.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003e9. Report No. B425\u003c\/strong\u003e\u003cbr\u003eF-4D Gun Module\u003cbr\u003eMcDonnell · 12 January 1965 · Copy No. 28\u003cbr\u003e\u003cem\u003eEngineering report covering the F-4D internal gun module design, integration, and installation specifications.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003e10. Report No. B233\u003c\/strong\u003e\u003cbr\u003eF-4D\/E Gun Pod Installations\u003cbr\u003eMcDonnell · 10 November 1964 · Control No. C-104936 · Copy No. 28\u003cbr\u003eOriginally classified Confidential — Group 4 · Declassified after 12 years\u003cbr\u003e\u003cem\u003eEngineering report on external gun pod installation configurations for the F-4D and F-4E, covering SUU-16\/A and SUU-23\/A pod integration on wing pylons.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003e11. A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1\u003c\/strong\u003e\u003cbr\u003ePerformance Analysis — F-4D Block 37 Phantom II (J79-GE-15)\u003cbr\u003eJ.M. Langeron \/ TOPOLO · Supplementary Reference\u003cbr\u003e\u003cem\u003e⚠️ Supplementary simulation reference document — not an OEM or USAF primary source. Included for performance data cross-reference and flight simulation use only. All aerodynamic values are modelled, not factory-issued.\u003c\/em\u003e\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eAircraft Technical Overview\u003c\/h3\u003e\u003ch4\u003eAerodynamic Configuration\u003c\/h4\u003e\u003cp\u003eThe F-4C\/D features a 45° swept wing with 12° wing-tip dihedral to counter lateral instability, and a 23° anhedral all-moving stabilator positioned to clear the wing's turbulent downwash. Lift augmentation is achieved through leading and trailing edge flaps combined with a Boundary Layer Control (BLC) system — high-pressure engine bleed air blown over the flaps to prevent airflow separation at low speeds, dramatically reducing approach speeds. Roll control relies on small ailerons working in tandem with upper-wing spoilers, intentionally omitting differential aileron control at high angles of attack to mitigate adverse yaw.\u003c\/p\u003e\u003ch4\u003ePowerplant — General Electric J79-GE-15\u003c\/h4\u003e\u003cp\u003eBoth variants are powered by two axial-flow, twin-spool J79-GE-15 turbojet engines. Each powerplant delivers 10,300 lbs dry thrust and 17,000 lbs with afterburner. The 17-stage compressor employs variable stator vanes that actively adjust to optimize airflow across the full Mach envelope, preventing compressor surges. Variable-area convergent-divergent exhaust nozzles modulate continuously to maintain optimal EGT and turbine pressure ratios during afterburner transitions.\u003c\/p\u003e\u003ch4\u003ePerformance Envelope\u003c\/h4\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eMetric\u003c\/th\u003e\n\u003cth\u003eSpecification\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Airspeed\u003c\/td\u003e\n\u003ctd\u003eMach 2.2+ (approx. 1,400 mph at altitude)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruising Speed\u003c\/td\u003e\n\u003ctd\u003e590 mph (513 knots)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eFerry Range\u003c\/td\u003e\n\u003ctd\u003e1,750 miles (external fuel dependent)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003eOver 59,600 feet\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Takeoff Weight\u003c\/td\u003e\n\u003ctd\u003eApprox. 58,000 lbs loaded\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003ePayload Capacity\u003c\/td\u003e\n\u003ctd\u003eUp to 16,000 lbs across 9 hardpoints\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003ch4\u003eAvionics \u0026amp; Engineering Differences — F-4C vs F-4D\u003c\/h4\u003e\u003cp\u003eThe F-4D updated the F-4C's AN\/APQ-100 radar to the AN\/APQ-109 system, adding the AN\/AJB-7 bombing computer and a distinctive Radome Chin Pod hump. Structural wing-spar reinforcements were mandated by early service bulletins to handle extreme G-loads from low-altitude conventional bombing operations over Southeast Asia. Later TCTOs updated electrical routing to support early smart weapons integration including laser-guided bombs and AGM-65 Maverick missiles on inner wing pylons.\u003c\/p\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\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":53703253492059,"sku":null,"price":79.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-2-redo-f-4d-desert-camo-in-flight.png?v=1785634961","url":"https:\/\/onlineaviationlibrary.com\/products\/mcdonnell-douglas-f-4c-f-4d-phantom-ii-technical-documentation","provider":"Online Aviation Library","version":"1.0","type":"link"}