N1116R
Beechcraft 400A Beechjet (400A)
Raytheon Aircraft Company
4 Hours
Duration of Flight
1547 NM
Range
458 MPH
Max Speed

Gallery




Aircraft Overview
At a glance
Basic Information
Year Manufactured
1996
Registration Number
N1116R
Serial Number
RK-116
Ownership
CTB INC
Location
Milford, IN, US
Aircraft Class
12,500 to 20,000lbs
Max Passengers
10
Range
1547 NM
Service Ceiling
45000 ft
Duration of Flight
4 Hours
Max Speed
458 MPH
Mode-S Code
A03324
Registration Country
US
Certificate Issued
May 10, 2004
Airworthiness Date
Sep 21, 1996
Reg. Expiration
Apr 30, 2027
Safety Record
N1116R
None found
No flight history available
Flight records for this aircraft have not been tracked yet.
AI Summary
Beechcraft 400A Beechjet (400A)
Overview
US registration assigned. Airworthiness certificate dated 1996-09-21; FAA certificate issue date 2004-05-10; last FAA registration action 2023-01-22; registration expiration 2027-04-30. Registered owner: CTB INC, Milford, IN.
Specifications
- Engines: 2x Pratt & Whitney Canada JT15D-5 (2900 lbf each)
- Range: 1547 nm
- Cruise: 410 kts
- Seats: 10
- Ceiling: 45000 ft
Operations & Cabin
Executive 6–8 place typical layout; forward galley, belted aft lavatory (operator-dependent) Typical executive leather seating, forward refreshment/galley and enclosed lav; cabin arrangements vary by refurbishment and operator. Avionics: Collins Pro Line 4 (common fit for 400A examples)
Model & Market Context
The airframe bearing tail number N1116R is a 1996-built Beechcraft 400A Beechjet, serial RK-116, manufactured by Raytheon Aircraft Company. The aircraft is recorded as owned by CTB INC, a corporation based in Milford, IN, US, and has a US registration. The build-year and serial identify this example as a mid-1990s production 400A variant, and its last recorded market valuation stands at $1,000,000. Registered ownership and base location have been maintained under the corporate owner in Milford, Indiana.
This airframe is typically outfitted in an executive interior configured for 6–8 passengers in a forward galley and belted aft lavatory arrangement, though final layout is operator-dependent; the cabin description for this specific airframe aligns with the common executive 6–8 place layout. Avionics fit on 400A examples is commonly the Collins Pro Line 4, which provides integrated flight, navigation and communications capabilities for this aircraft. With a cruise speed of 410 kts, a range of 1,547 nm and an operational ceiling of 45,000 ft, the aircraft is suited to short to medium‑range executive missions from its operator base in Milford, Indiana. Maintenance considerations derive from twin Pratt & Whitney Canada JT15D-5 engines and the systems associated with the Pro Line 4 avionics suite for this production year.
As a Beechcraft 400A Beechjet from 1996, this airframe occupies the fixed-wing multi-engine category and offers trans-regional capability driven by its 410 kt cruise and 1,547 nm range. The twin JT15D-5 engines delivering 2,900 lbf each and a certified ceiling of 45,000 ft define its performance envelope. Market and resale considerations for this specific airframe are influenced by its age (1996 build), installed avionics fit, interior configuration, and the recorded valuation of $1,000,000, all of which inform operator maintenance planning and mid-life systems upkeep.