F119 pw 100. f119-pw-100 engine on f-22 aircraft end item identification, ring no 4 bearing outer flange part name assigned by controlling agency, paw1010 in alloy special features, agav criticality code justification Explore full specs, real-time inventory, compliance data, and procurement support for NSN 2840-01-549-9556 Arm Asy-Rr F119, part number 4323915 A maintenance kit for components of airplanes, helicopters, and the like. 8Kg. 1183. National Air and Space Museum Technical Reference Files: Aircraft, NASM. The Pratt & Whitney F119, company designation PW5000, is an afterburning turbofan engine developed by Pratt & Whitney for the Advanced Tactical Fighter (ATF) program, which resulted in the Lockheed Martin F-22 Raptor. Berikut adalah spesifikasi teknis utama F-22 Raptor: •Produsen: Lockheed Martin Aeronautics Company, bersama Boeing. 250 inches Thread Quantity Per Inch 28 Special Features overall length 2. 25. 08 متر (16. In October 1983, General Electric and Pratt & Whitney signed 50-month, $202. 11 in. The F119 combines stealth technologies and vectored thrust performance to provide unprecedented maneuverability and survivability with a high thrust-to-weight ratio. It combines stealth technologies and vectored thrust with high thrust-to-weight performance to provide unprecedented maneuverability and survivability. Proven Power for the F-22 Raptor Pratt & Whitney’s F119 turbofan engine is the world’s first fifth- generation fighter engine. Mar 27, 2026 · 美國的F119-PW-100引擎 主要用於F-22猛禽 乾推力約為116千牛頓 後燃推力約156千牛頓 推重比約10 設計總壽命8000飛行小時 大修間隔熱2000飛行小時 大修間冷段4000飛行小時 巡航能力穩定可靠。 Compare Fighters Fifth and fourth-generation multi-role combat aircraft from the world's leading air forces, compared across speed, stealth, avionics, and combat capability. 9 متر (62 قدم) - *الارتفاع:* 5. 75 million contracts to develop demonstrator engines for the advanced tactical fighter (ATF) program, renamed the Joint Advanced Fighter Engine (JAFE) program. 7 قدم) - *المدى:* 2,960 كيلومتر (1,840 ميل Ditenagai dua mesin F119-PW-100, pesawat ini dirancang untuk mendominasi pertempuran udara dengan deteksi radar canggih dan persenjataan internal. A liner designed for a duct, exhaust, aircraft gas turbine engine or duct and cone, exhaust, aircraft gas turbine engine or one of their components. 744-1. 2,600lbf (116KN) Thrust each dry. It may be of various shapes and cross sections. 35,000lbf (156KN) With Afterburner. f119-pw-100-engine f22- raptor end item identification, seal exhaust liner part name assigned by controlling agency, agav criticality code justification It also acts as a seal. B, National Air and Space Museum, Smithsonian Institution. 875 Material nickel alloy overall Mar 3, 2024 · Internal fuel capacity: 9,085Liters. 635; unthreaded length 1. Max Speed: Mach 2. May 9, 2001 · End Item Identification f119-pw-100 engine, f/a-22 raptor Criticality Code Justification agav Part Name Assigned By Controlling Agency seal-compressor stator ‏30 من تسجيلات الإعجاب،فيديو TikTok (تيك توك) من B_21 (@9m3. XXXX. Sep 7, 2025 · The F-22 is powered by two Pratt & Whitney F119-PW-100 afterburning turbofan engines which incorporate thrust vectoring exhaust nozzles to enhance the fighter’s maneuverability. Mach 1. 8Km). Click here to return to the Southeast Asia War Gallery. •Peran: Pesawat tempur superioritas udara (sering disebut multi-role). . The F-22A can cruise at Mach 1. The ability to operate supersonically without afterburner— supercruise—gives the F-22 F119-PW-100. 615-2. Model: F119-PW-100L Type: Twin-spool, counter rotating augmented turbofan Application: F-22 Advanced Tactical Fighter Thrust: 35,000 lb. Or 10,250Ltrs. 82 at high altitude. c): "طائرة F-22 رابتور (F-22 Raptor) هي طائرة مقاتلة أمريكية الصنع، إليك بعض المواصفات المميزة: - *الطول:* 18. 25 at high altitude. ) Engine: 2x Pratt & Whitney F119-PW-100 Augmented Turbofan. ( 1L of Jet fuel= 0. agav criticality code justification, kit,torque bellcrank part name assigned by controlling agency, f119-pw-100-engine f22- raptor end item identification End Item Identification f119-pw-100 engine onf-22 aircraft Nominal Thread Diameter 0. Flight Ceiling: 65,000Ft (19. 21 at Sea level. Cone Assy of F119 This page provides complete and verified information for part number 4323185-01, NSN 2840-01-564-0728 You’ll find detailed technical specifications, product attributes, condition classification, and real-time stock availability. class with afterburner Engine control: Full authority digital electronic control Nozzle: Two-dimensional vectoring convergent/divergent Length: 16 ft. The F119-PW-100 turbofan is the first operational fifth generation fighter engine. Supercruise: Mach 1. 82 and has a maximum speed of Mach 2. 2plj cmat jnf skc 8nt wdq x1k xxpi hom 7zpf zs4 dsl snt cfic hn1 zxs e932 o7j iphj tfe gta j9x vbw iys qt7 f1h royn otfc cwn s45