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Firestone XR-9 Multi-Cache

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BeardedGentleman: Time to go! Thanks to all who took their time to solve this multi, visit this location and find this cache.
- BG

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Hidden : 5/8/2016
Difficulty:
2 out of 5
Terrain:
2 out of 5

Size: Size:   micro (micro)

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Geocache Description:

BeardedGentleman
presents a geocache:

Firestone XR-9

The Firestone XR-9, also known by the company designation Model 45, was a 1940s American experimental helicopter built by the Firestone Aircraft Company for the United States Army Air Forces. Only two (the military XR-9B and one civil example) were built.

Originally developed by G & A Aircraft with the co-operation of the United States Army Air Forces' Air Technical Service Command, the G & A Model 45B (designated XR-9 Rotocycle by the Army) was a design for a single-seat helicopter of pod-and-boom configuration. It had a fixed tri-cycle landing gear and three-bladed main and tail rotors. Power would have been supplied by a 126 hp (94 kW) Avco Lycoming XO-290-5 engine. The Model 45C (XR-9A) was the same helicopter with a two-bladed rotor. Neither of the two helicopters were built. G & A Aircraft was purchased by Firestone in 1943, and was renamed the Firestone Aircraft Company in 1946.

A revised two-seat design the revised Model 45C (or XR-9B) was built with a three-bladed main rotor and two-seat in tandem. The first aircraft procured by the Army Air Forces in 1946, it was powered by an Avco Lycoming O-290-7 engine and first flew in March of that year.

A civil version, the Model 45D was also built and flown, in anticipation of a postwar boom in aircraft sales. This differed in having the two occupants side-by-side instead of Tandem as in the 45C, and was equipped with a 150 horsepower (110 kW) Lycoming engine. The prototype was demonstrated at the 1946 Cleveland National Air Races. A four-seat Model 50, with twin tail rotors, was also projected, but the predicted sales boom did not materialise, and Firestone closed its aircraft manufacturing division.

General characteristics:

  • Crew: 2
  • Length: 27 ft 0 in (8.23 m)
  • Main rotor diameter: 28 ft 0 in (8.53 m)
  • Height: 8 ft 6½ in (2.60 m)
  • Gross weight: 1750 lb (794 kg)
  • Powerplant: 1 × Avco Lycoming O-290-7 flat-four engine, 135 hp (101 kW) each

Performance:

  • Cruise speed: 80 (approx) mph (129 (approx) km/h)
  • Service ceiling: 10,000 ft (3050 m)

XXXX = Search for the year when the monument was built.

N 45° 38. (XXXX-1657)
E 016° 03. (XXXX-1452)

Additional Hints (Decrypt)

[HR] ...yvwrib bq fgnmvpr, 1 z. [ENG] ...yrsg sebz gur cngu, 1 z.

Decryption Key

A|B|C|D|E|F|G|H|I|J|K|L|M
-------------------------
N|O|P|Q|R|S|T|U|V|W|X|Y|Z

(letter above equals below, and vice versa)