N274CA - 1969 SABRE 60EL

1969

SABRE

60EL

306-37

N274CA

Used

Sabreliner Overview and Summary of Capabilities: The Sabreliner aircraft is a modified version of the North American Rockwell NA 265-60, a medium-range, high-altitude, pressurized twin-jet monoplane. The Sabreliner is best suited for those research missions that require high-altitude operation above 25,000 ft, 7.7 km, or that need to cover large distances in a minimum amount of time. Transceiver - Collins VHF-21A, Receiver – Collins VIR-32 & Collins ADF-60, Collins DME-42

5517.0

Airframe and Engine Specs Total Time: 5,517 hours L/H Engine: 9,588 hours (2371 hours SMOH) R/H Engine: 8,521 hours (2373 hours SMOH) Length: 48.3 feet Wingspan: 44.6 feet Gross Weight: 20,000 lbs Max. Payload: 1,850 lbs (with fuel) Max. Altitude: 43,000 feet Range: 1,300 nm (@ 37,000 ft. cruise) Endurance: 2.5 hours (max with IFR reserve) Speed: 420 KTAS

Two Pratt & Whitney JT12A-8

2371

SMOH

8521

SMOH

Avionics and Other Equipment Specs Transceiver - Collins VHF-21A (qty 2) Receiver – Collins VIR-32 (qty 1) Receiver – Collins ADF-60 (qty 1) DME – Collins DME-42 (qty 2) Flight Computer – Collins 562A-5G (qty 1) Autopilot – Collins 562C-4 (qty 1) Altitude Controller – Collins 590A-3E (qty 2) Audio Controller – Collins 346B-3 (qty 4) GPS – Trimble 2101 (qty 1) Power Supply – PS-823B (qty 1) Instrument Amplifier – Collins 344C-10 (qty 1)

1995

white/green

Gray carpet 6 leather seats (light gray) Crew: 2 pilot, plus 2-4 additional seats

Special features for S/N 306-37: This aircraft was purchased and modified for atmospheric testing by NCAR. Special features include: 1) Air-sampling nose boom; 2) T-39 B/D nose configuration with large radome; 3) two additional static ports and one pilot head; 4) 2-day equipment cabinet on the R/H side between FS143-206; 5) electric power distribution panels at FS206-206; 6) four fuselage hard points located on top centerline at FS154.25, FS202, FS 253, and FS298.5 and 5.8; 7) two wing hard points located in the leading-edge structure at Xf69 and Xf96.5; 8) provisions for wire routing through wing leading edge to tip; 9) cabin set-up with provisions for four seats with O2/air/intercom consoles at each location; 10) one 76.5 cu. Feet O2 bottle in L/H forward cabin behind FS 174; 11) external antenna bay mounted on lower aft fuselage behind FS412.