N43GG

Piper PA-34-200T Seneca II (Seneca II)

Piper Aircraft

5 Hours

Duration of Flight

870 NM

Range

204 MPH

Max Speed

N43GG

Gallery

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Aircraft Class
Aircraft Class
Under 12,500lbs
Max passengers
Max passengers
6
Range
Range
870 NM
Service Ceiling
Service Ceiling
25000 ft
Duration of Flight
Duration of Flight
5 Hours
Max Speed
Max Speed
204 MPH

Basic Information

Year Manufactured1976
LocationUnited Kingdom
Registration NumberN43GG
OwnershipSouthern Aircraft Consultancy Inc Trustee
Serial Number34-7670066

Airframe

Data valid as of 2004-06-25
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

Piper PA-34-200T Seneca II (Seneca II)

Overview

Previously UK-registered as G-ROLA; sold and transferred to the US register on 2004-06-25. Involved in a nose-landing-gear collapse on 2005-09-27 (Humberside).

Specifications

  • Engines: 2× Continental TSIO-360-EB (200 lbf each)
  • Range: 870 nm
  • Cruise: 188 kts
  • Seats: 6
  • Ceiling: 25000 ft

Operations & Cabin

6-place light-twin executive/utility layout (club or 1+5 typical)

Model & Market Context

This airframe, N43GG, is a 1976-built Piper PA-34-200T Seneca II with serial number 34-7670066 manufactured by Piper Aircraft. The airframe is held by Southern Aircraft Consultancy Inc Trustee (a corporate owner located in the United Kingdom), creating an ownership profile in which a UK-based trustee holds a US-registered asset. The airframe carries a US registration (US) while ownership is based abroad, a relationship that has implications for registry administration and transnational maintenance logistics. Condition and valuation details are not published for this specific aircraft.

The aircraft is configured as a 6-place light-twin executive/utility layout with a cabin arrangement that supports either a club seating plan or a typical 1+5 executive layout. As a light twin, the airframe is suited to short- to mid-range missions consistent with its 870 nm range and 188 kts cruise, operating in roles from executive transport to utility and light charter. Maintenance planning for this airframe reflects its twin Continental TSIO-360-EB engines and 1976 build year, and operator logistics are influenced by the fact that the owner is based in the United Kingdom while the aircraft remains US-registered, a point occasionally noted in registry and crewing arrangements.

The Piper PA-34-200T Seneca II occupies a performance niche as a light twin offering modest cruise speed and useful ceiling for non-pressurized twin operations, leveraging two turbocharged Continental engines for improved climb and high-altitude capability. Buyers and charter operators seeking a six-seat executive/utility platform often compare this type to contemporaneous light twins; demand and resale considerations for this specific airframe will be affected by its 1976 vintage, engine model, and the international ownership/registration profile. Maintenance cycles, parts availability, and corrosion inspections typical for an aircraft of this era are relevant resale and operational considerations.

Aircraft Comparison

ParameterN43GGN15HDN73LW
Serial Number (MSN)34-767006630-75730-1124
Year Manufactured197619651966
Duration of Flight5 Hours7 HoursN/A
Range870 NM1237 NMN/A
Max Speed204 MPH182 MPHN/A
Aircraft ClassUnder 12,500lbsUnder 12,500lbsUnder 12,500lbs
Service Ceiling25000 ft18000 ft18000 ft
Max Passengers644
Cabin ComfortNo items found.No items found.No items found.

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