This comprehensive digital collection provides structured technical documentation for the LTV A-7 Corsair II, one of the most effective and longest-serving carrier-based attack aircraft in U.S. military history. The collection includes authentic flight manuals, maintenance instructions, structural repair handbooks, and system-specific technical documentation covering Navy variants (A-7A, A-7B, A-7E, TA-7C) and Air Force variants (A-7D, A-7K, A-7H) spanning 1968 through 1989.

Definitive Collection with Free Lifetime Updates: This is a living collection that we continuously expand and refine. As we acquire additional A-7 Corsair II documentation, technical bulletins, or variant-specific materials, we update this collection and provide free lifetime updates to all purchasers. Your one-time purchase guarantees access to all future additions and improvements to this collection.

Historical Note

The LTV A-7 Corsair II was developed by Ling-Temco-Vought (later Vought Corporation) in response to the U.S. Navy's VAL (heavier-than-air, attack, light) competition of 1963, which sought a replacement for the Douglas A-4 Skyhawk. The Navy's requirements emphasized weapons payload, range, and delivery accuracy over raw speed—a revolutionary departure from the supersonic fighter-bomber trend of the era. Vought's design, based on a shortened and simplified derivative of the F-8 Crusader airframe, won the competition in February 1964.

The prototype YA-7A first flew on September 27, 1965, and the aircraft entered fleet service with VA-147 aboard USS Ranger in October 1967. The A-7 saw its combat debut in December 1967 over Vietnam, where it quickly established a reputation for exceptional accuracy and survivability. The aircraft's advanced AN/APQ-126 radar, sophisticated AN/ASN-90 inertial navigation system, and integrated weapons delivery computer allowed pilots to deliver ordnance with unprecedented precision in all weather conditions—a capability that proved invaluable in the challenging combat environment of Southeast Asia.

Production variants included the A-7A powered by the Pratt & Whitney TF30-P-6 turbofan (199 built), A-7B with the improved TF30-P-8 engine (196 built), A-7C with additional avionics improvements (67 built), and the definitive A-7E powered by the Allison TF41-A-2 turbofan—a license-built Rolls-Royce Spey engine producing 15,000 pounds of thrust (535 Navy aircraft built). The U.S. Air Force adopted the type as the A-7D with the TF41 engine and Air Force-specific avionics (459 built), while the two-seat TA-7C trainer variant (60 built) provided conversion training for Navy and Marine Corps pilots. Export variants included the A-7H for Greece (60 aircraft) and A-7P for Portugal (50 ex-Navy A-7As). Total production exceeded 1,500 aircraft between 1965 and 1984.

The A-7 Corsair II could carry up to 15,000 pounds of ordnance on eight external hardpoints (two fuselage stations and six wing stations), making it one of the most capable attack platforms of its generation. Standard armament included a single M61A1 Vulcan 20mm rotary cannon with 1,000 rounds. The aircraft could deliver a wide variety of weapons including conventional bombs, cluster munitions, laser-guided bombs (with the AN/AVQ-23 Pave Penny laser spot tracker), AGM-45 Shrike and AGM-88 HARM anti-radiation missiles, AGM-65 Maverick air-to-ground missiles, and AIM-9 Sidewinder air-to-air missiles for self-defense.

The Corsair II served with distinction in every major U.S. military operation from Vietnam through Desert Storm. During Operation Desert Storm in 1991, Navy A-7Es and Air Force A-7Ds flew thousands of combat sorties, demonstrating the aircraft's enduring combat effectiveness even after 25 years of service. The type also saw action in Operation Urgent Fury (Grenada, 1983), Operation El Dorado Canyon (Libya, 1986), and Operation Praying Mantis (Persian Gulf, 1988). The A-7's combination of accuracy, reliability, weapons-carrying capability, and survivability made it the benchmark for subsonic attack aircraft and directly influenced the design requirements for the F/A-18 Hornet and A-10 Thunderbolt II.

The A-7 Corsair II remained in active U.S. Navy service until 1991, when it was replaced by the F/A-18 Hornet. Air National Guard units continued flying the A-7D and A-7K until final retirement in 1993, marking nearly three decades of operational service. Greek Air Force A-7H variants served until 2014, making the Corsair II one of the longest-serving jet attack aircraft in history. Today, several A-7 Corsair IIs are preserved in museums and private collections, representing a pivotal chapter in the evolution of precision strike warfare.

Manuals Included in This Collection

• LTV / Vought A-7E "Corsair II" Aircraft Maintenance Instructions Manual - Escape and Survival Systems - 01-45AAE-2-3 - 1969
• LTV / Vought A-7C, A-7E "Corsair II" Aircraft Flight Manual 01-45AAE-1 - 1972
• LTV / Vought A-7A and A-7B "Corsair II" Aircraft Maintenance Manual - Propulsion System - 01-45AAA-2-8 - 1968
• LTV / Vought A-7H Aircraft Pilot's Pocket Checklist Manual 01-45AAH-1B (GR)
• LTV / Vought A-7E "Corsair II" Aircraft Flight Manual 01-45AAE-1 - 1989
• LTV / Vought A-7D Aircraft Flight Aircrew Air Refueling Procedures Manual - T.O. 1-1C-24 - 1978
• LTV / Vought A-7D Aircraft Aircrew Weapon Delivery Manual - (Non-Nuclear) - T.O. 1A-7D-34-1-1 - 1978
• LTV / Vought A-7A and A-7B "Corsair II" Aircraft Flight Manual 01-45AAA-1 - 1971
• LTV / Vought TA-7C "Corsair II" Aircraft Flight Manual 01-45AAF-1 - 1979
• LTV / Vought A-7K Aircraft Aircrew Weapon Delivery Manual - (Non-Nuclear) - 1981
• LTV / Vought A-7D Maintenance Manual - Electrical Power and Light System Manual, AN 01-A7-D-2-11, 1981
• LTV / Vought A-7D Structural Repair Manual, AN 01-A7-D-3, 1985
• LTV / Vought A-7D Maintenance Manual - Flight Control Systems, AN 01-A7-D-2-8, 1976
• LTV / Vought A-7D Maintenance Manual - Landing Gear Systems, AN 01-A7-D-2-7, 1976
• LTV / Vought A-7D Maintenance Manual - Fuel Systems, AN 01-A7-D-2-6, 1986
• LTV / Vought A-7D Maintenance Manual - Power Plant System, AN 01-A7-D-2-5, 1985
• LTV / Vought A-7D Maintenance Manual - Pneudraulic Systems, AN 01-A7-D-2-4, 1975
• LTV / Vought A-7D Maintenance Manual - Mechanical Accessories Systems, AN 01-A7-D-2-3, 1972
• LTV / Vought A-7D Maintenance Manual - Egress and Survival Systems, AN 01-A7-D-2-2, 1976
• LTV / Vought A-7D Maintenance Manual - General Information and Airframe Group Manual, AN 01-A7-D-2-1, 1985
• LTV / Vought A-7D "Corsair II" Aircraft Flight Manual 01-A7-D1 - 1971

This collection provides comprehensive coverage of all major A-7 Corsair II variants, including detailed flight operations, maintenance procedures, system-specific documentation, structural repair techniques, weapons delivery procedures, and air refueling operations. The manuals span the entire operational history from initial Navy deployment through final Air Force service.

Engineering Norms and Standards

Design and Construction: The A-7 Corsair II was designed to U.S. Navy Bureau of Naval Weapons specifications and certified under military airworthiness standards of the mid-1960s. The aircraft featured all-metal semi-monocoque construction derived from the F-8 Crusader but with a shortened fuselage (46 feet 1.5 inches versus 54 feet 3 inches) and simplified high-lift wing design. The wing employed a modified NACA 65A007 airfoil section with a span of 38 feet 9 inches and area of 375 square feet, optimized for subsonic attack operations rather than supersonic performance. The wing incorporated full-span leading-edge slats and trailing-edge single-slotted flaps for excellent low-speed handling and short-field performance. Wing folding mechanisms allowed the outer panels to fold upward hydraulically for carrier storage, reducing span to approximately 23 feet 9 inches.

Powerplant and Propulsion System: Early Navy variants (A-7A, A-7B) were powered by the Pratt & Whitney TF30-P-6 and TF30-P-8 turbofan engines producing 11,350 pounds of thrust, while the definitive A-7E and all Air Force variants (A-7D, A-7K) employed the Allison TF41-A-2 turbofan (license-built Rolls-Royce Spey) producing 15,000 pounds of thrust. The TF41 engine provided significantly improved thrust-to-weight ratio, better fuel efficiency, and enhanced hot-day/high-altitude performance. The engine was mounted on a structural engine frame assembly designed to absorb landing loads and facilitate rapid engine changes for maintenance. Air intake was through a single ventral inlet with a fixed geometry design optimized for subsonic flight regimes. The exhaust nozzle was a simple convergent design without afterburner, consistent with the aircraft's subsonic mission profile.

Performance Specifications: The A-7E achieved a maximum speed of 698 mph (Mach 0.92) at sea level, with a combat radius of 700 nautical miles on internal fuel and 1,100 nautical miles with external tanks. Service ceiling was 42,000 feet. Maximum takeoff weight was 42,000 pounds, with a typical combat weight of 30,000-35,000 pounds depending on weapons load. The aircraft could sustain 6.5g maneuvers at combat weight. Ferry range with maximum external fuel exceeded 2,800 nautical miles. The A-7D had similar performance characteristics with slight variations due to Air Force-specific equipment installations.

Structural Design and Load Factors: The A-7 airframe was designed to withstand load factors of +7.5g and -3.0g at design gross weight, with ultimate load factors of +11.25g and -4.5g (1.5 times limit load per MIL-A-8860 and MIL-A-8861 military specifications). The main landing gear featured robust oleo-pneumatic shock struts designed for carrier arrested landings, with a sink rate capability of 23 feet per second at maximum landing weight. The nose gear was also designed for catapult launches with a maximum end speed of 150 knots. Landing gear track was 9 feet 3 inches. The arresting hook was mounted on the aft fuselage for carrier operations (Navy variants). Fuselage structure consisted of machined aluminum frames and longerons with riveted aluminum skin panels, employing fail-safe design principles with multiple load paths.

Fuel System: Total internal fuel capacity was 1,500 U.S. gallons (10,000 pounds) distributed across fuselage and wing tanks, all equipped with self-sealing bladders and fire-suppression systems. The aircraft could carry two 300-gallon external tanks on inboard wing stations and one 300-gallon centerline tank for a total of 2,400 gallons (16,000 pounds) with external stores. All variants were equipped with aerial refueling capability via a retractable probe on the right side of the fuselage, compatible with Navy and Air Force tanker aircraft. Fuel system pressure was maintained at 35-50 psi by dual engine-driven fuel pumps with electric boost pumps for backup.

Hydraulic and Flight Control Systems: The A-7 employed dual independent hydraulic systems (PC-1 and PC-2) operating at 3,000 psi, providing redundancy for all critical flight control functions. Each system was powered by an engine-driven hydraulic pump with an accumulator for emergency backup. The flight control system was fully powered (no manual reversion) with artificial feel systems to provide appropriate control forces. Controls included conventional ailerons, rudder, and stabilator (all-moving horizontal tail). Leading-edge slats and trailing-edge flaps were hydraulically actuated. The aircraft featured a stability augmentation system (SAS) for improved handling qualities and weapons delivery accuracy.

Avionics and Weapons Systems: The A-7E was equipped with the AN/APQ-126 forward-looking radar for terrain avoidance, navigation, and air-to-ground ranging. The AN/ASN-90 inertial navigation system provided continuous position updates with exceptional accuracy (typical drift less than 1 nautical mile per hour). The central air data computer integrated inputs from the INS, radar, and air data sensors to compute weapons delivery solutions displayed on the head-up display (HUD). The AN/AVQ-23 Pave Penny laser spot tracker pod allowed delivery of laser-guided munitions. The AN/ALR-45 radar warning receiver and AN/ALE-39 chaff/flare dispenser provided defensive countermeasures capability. The A-7D featured Air Force-specific avionics including the AN/APQ-126 radar and similar navigation/attack systems.

Armament and Ordnance: Standard gun armament consisted of one M61A1 Vulcan 20mm six-barrel rotary cannon mounted in the left side of the fuselage with 1,000 rounds of ammunition. Eight external hardpoints provided a maximum ordnance capacity of 15,000 pounds: two fuselage stations (500 pounds each), two inboard wing stations (3,500 pounds each), two intermediate wing stations (3,500 pounds each), and two outboard wing stations (2,500 pounds each). Certified weapons included Mk 80-series general-purpose bombs (Mk 82 500-lb, Mk 83 1,000-lb, Mk 84 2,000-lb), cluster munitions (CBU-52, CBU-58, CBU-87), laser-guided bombs (GBU-10, GBU-12, GBU-16), AGM-45 Shrike and AGM-88 HARM anti-radiation missiles, AGM-65 Maverick air-to-ground missiles, Rockeye cluster bombs, and AIM-9 Sidewinder air-to-air missiles for self-defense.

Electrical System: The electrical system was 115/200-volt AC, 400 Hz, three-phase power generated by two engine-driven 40 kVA generators with a 24-volt DC system for starting and emergency backup. The DC system included a 40-ampere-hour nickel-cadmium battery and transformer-rectifier units for AC-to-DC conversion. The electrical system powered all avionics, flight instruments, lighting, and utility systems.

Manufacturing Standards: Production aircraft were built to U.S. Navy and Air Force military specifications including MIL-A-8860 (airplane strength and rigidity), MIL-A-8861 (airplane strength and rigidity, reliability requirements), and MIL-E-5400 (electronic equipment, general specification). Structural components were fabricated from 2024-T3, 7075-T6, and 7178-T6 aluminum alloys, with 4130 chromoly steel and titanium alloys used for high-temperature and high-stress applications. All fuel system components met self-sealing and crashworthiness requirements per MIL-T-5624 (fuel tank specifications). Quality control procedures ensured interchangeability of parts across the production run and between Navy and Air Force variants where applicable.

Specialized Documentation

Supplemental Type Certificates and Modifications: While the A-7 Corsair II is a military aircraft without a civilian Type Certificate, several examples have been registered under FAA Experimental-Exhibition or Experimental-Research categories for warbird operations and flight test programs. These aircraft typically operate under approved flight manuals and maintenance programs derived from the original military technical orders. Some privately-owned A-7s have received modifications for civilian operation including updated avionics, simplified weapons systems, and enhanced safety equipment.

Service Bulletins and Technical Directives: The A-7 Corsair II is no longer supported by an active Type Certificate holder, as LTV Aerospace was acquired by Northrop Grumman and A-7 production ended in 1984. However, historical Navy Technical Directives, Air Force Technical Orders, and LTV Service Bulletins remain valuable references for museums, warbird operators, and aviation historians. The Hellenic Air Force (Greece) maintained A-7H variants until 2014 and developed extensive maintenance documentation and modification programs that extended the type's service life.

Performance Profiles and Operational Procedures: This collection includes authentic flight manuals with detailed performance charts, takeoff and landing data, fuel consumption tables, weapons delivery profiles, air refueling procedures, and emergency procedures. The Air Force weapon delivery manuals provide comprehensive tactical employment guidance for conventional ordnance delivery in various attack profiles. These documents are invaluable for flight simulator developers, military aviation historians, and researchers studying precision strike tactics and weapons system integration.

Where to Find Additional Documentation

Official Archives: The National Naval Aviation Museum in Pensacola, Florida, and the National Museum of the United States Air Force at Wright-Patterson AFB, Ohio, maintain extensive archives of A-7 Corsair II documentation including technical orders, engineering drawings, and operational records. The Smithsonian National Air and Space Museum also holds significant A-7 technical records and historical materials.

Historical Archives: The A-7 Corsair II community is supported by organizations including the Tailhook Association (for Navy and Marine Corps carrier aviation), the Air Force Association, and various warbird preservation groups. Online resources such as the A-7 Corsair II Association website, military aviation forums, and warbird registries provide community knowledge, historical information, and technical discussions. The Air Force Historical Research Agency (AFHRA) and Naval History and Heritage Command (NHHC) maintain research archives with operational histories, combat reports, and technical documentation.

Specialty Vendors: In addition to Online Aviation Library, several organizations provide A-7 Corsair II historical documentation, research materials, and museum-quality information including the Tailhook Association, various aviation museums with A-7 aircraft in their collections, and military aviation research organizations. These resources can provide additional context for A-7 operations, tactical employment, and historical significance.

Format and Delivery

All manuals are provided as high-resolution PDF files, optimized for on-screen viewing and printing. Files are delivered via secure download link immediately upon purchase. The complete collection is organized in a logical folder structure by variant and document type for easy navigation and reference.

Disclaimer

This item is sold for historical and reference purposes only. These are either original or copies of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. These manuals and blueprints are not meant to be used for current update material for certification/repair, but make an excellent reference for the scholar, collector, modeler, or aircraft enthusiast. For proprietary reasons, we generally only provide civil manuals and blueprints on obsolete aircraft/engines/helicopters. The information is for reference only, and we do not guarantee the completeness, accuracy, or currency of any manuals.

Reference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks, and manufacturer names are the property of their respective owners.

This digital compilation, structure, indexing, and presentation are © Sicuro Publishing.