N351SD

Bell UH-1H Iroquois (UH-1H)

Bell Helicopter (Bell Textron Inc.)

2 Hours

Duration of Flight

276 NM

Range

124 MPH

Max Speed

N351SD

Gallery

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Aircraft Class
Aircraft Class
Under 12,500lbs
Max passengers
Max passengers
15
Range
Range
276 NM
Service Ceiling
Service Ceiling
19400 ft
Duration of Flight
Duration of Flight
2 Hours
Max Speed
Max Speed
124 MPH

Basic Information

Year Manufactured1968
LocationQuetta, Pakistan (operated under jurisdiction of U.S. Department of State transfer)
Registration NumberN351SD
OwnershipPakistan Ministry of Interior (Air Wing) — operated following U.S. Dept. of State transfer
Serial Number10713

Airframe

Data valid as of 2008-02-08
AFTT (hrs)
Current
N/A
Flight
N/A
Est.
N/A
Landings/Cycles
Current
N/A
Flight
N/A
Est.
N/A
Nautical Miles
Current
N/A
Flight
N/A
Est.
N/A
No flights

No flight history available

Flight records for this aircraft have not been tracked yet.

AI Summary

Fact-checked by AI

Bell UH-1H Iroquois (UH-1H)

Overview

Documented as N351SD and registered in association with U.S. Department of State transfer activity at Patrick AFB on 2008-02-08; subsequently supplied to Pakistan Ministry of Interior Air Wing (operating identity HY-10).

Specifications

  • Engines: 1× T53-L-13 (Lycoming/Honeywell) (1400 lbf each)
  • Range: 276 nm
  • Cruise: 114 kts
  • Seats: 15
  • Ceiling: 19400 ft

Operations & Cabin

Utility / troop transport configuration, up to 15 seats (bench/side-facing military layout typical)

Model & Market Context

This entry covers rotorcraft airframe N351SD, a Bell UH-1H Iroquois built in 1968 with manufacturer serial number 10713. The helicopter is operated by the Pakistan Ministry of Interior (Air Wing) — operated following U.S. Dept. of State transfer and was placed under their jurisdiction in Quetta, Pakistan after the documented transfer. Registration for the aircraft is US, and its operational history for this airframe includes the notable diplomatic transfer arrangement under which it was supplied. Valuation and specific condition assessments for this individual airframe are Not published.

This airframe is fitted in a utility / troop transport configuration with a typical bench and side-facing military layout accommodating up to 15 occupants, optimized for personnel movement and internal load flexibility. Avionics fit are consistent with UH-1H utility operators of comparable vintage—basic flight instruments and mission radios appropriate for transport and liaison duties—while specific avionics lists for this serial are Not published. Based at Quetta under the operating authority noted above, typical missions for N351SD would include internal security transport, personnel insertion/extraction, logistics support, and short-range liaison flights within Pakistan, exploiting a cruise speed of 114 kts and a maximum practical mission radius given a 276 nm range. Maintenance considerations for this airframe reflect UH-1H norms: adherence to T53-L-13 powerplant service intervals, airframe corrosion control for older examples, and parts logistics influenced by legacy Bell supply chains.

The Bell UH-1H Iroquois family occupies a long-established niche as a rugged, versatile utility rotorcraft valued for troop transport and general utility roles. Powered by the reliable T53 series, the type competes functionally with other medium utility helicopters of its era rather than modern turbine designs; contemporary alternatives include later-model utility helicopters for buyers seeking greater payload or modern avionics. For operators and prospective buyers, maintenance history, availability of T53-L-13 components, and export/import/regulatory status following a U.S. Department of State transfer are primary considerations for operational continuity and resale.

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