Specifications for Beechcraft Beechjet 400A
Beechcraft Beechjet 400A · Specifications
Overview
This document provides detailed specifications for the 1999 Beechcraft Beechjet 400A, including performance metrics, engine specifications, avionics, and maintenance status. It is intended for potential buyers and aviation professionals interested in the operational capabilities and current condition of the aircraft. Key performance figures such as maximum takeoff weight, cruise speeds, and range are highlighted, along with detailed engine hours and maintenance history. The document also lists the avionics suite and additional equipment installed on the aircraft, ensuring that prospective buyers have a comprehensive understanding of the aircraft's features and performance.
- Ramp Weight: 16,500 lbs
- MTOW: 16,300 lbs
- Max Landing Weight: 15,700 lbs
- Max Cruise Speed: 468 knots
- NBAA Range: 1,457 nautical miles
- Service Ceiling: 45,000 feet
- Engine TBO: 625.3 hours (LH), 406.4 hours (RH)
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Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at s3.amazonaws.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Specifications
- Year ·
- 1999
- Pages ·
- 6
- File size ·
- 1.9 MB
- Copy found at ·
- s3.amazonaws.com
What is the Specifications for Beechcraft Beechjet 400A?
The Specifications for Beechcraft Beechjet 400A is a specifications for the Beechcraft Beechjet 400A, dated 1999.
How many pages is the Specifications for Beechcraft Beechjet 400A?
The copy of the Specifications for Beechcraft Beechjet 400A on file runs 6 pages.
What year was the Specifications for Beechcraft Beechjet 400A published?
The Specifications for Beechcraft Beechjet 400A — the Beechcraft Beechjet 400A specifications on file — is dated 1999.
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In this document
Performance Specifications
The Beechcraft Beechjet 400A has a ramp weight of 16,500 lbs and a maximum takeoff weight (MTOW) of 16,300 lbs. The maximum landing weight is 15,700 lbs, and the maximum zero fuel weight (MZFW) is 13,000 lbs. It can achieve a maximum cruise speed of 468 knots and a recommended cruise speed of 430 knots. The NBAA range is 1,457 nautical miles, and the service ceiling is 45,000 feet.
Engine Specifications
The aircraft is powered by two Pratt & Whitney JT15D-5 engines. The left engine has 7,277.6 hours and 5,794 cycles, while the right engine has 7,496.6 hours and 6,074 cycles. The time between overhaul (TBO) for the left engine is 625.3 hours and for the right engine is 406.4 hours. The hours since last inspection (HIS) are 1,212.4 for the left engine and 1,346.48 for the right engine.
Avionics and Equipment
The Beechjet 400A is equipped with a Collins Proline II EFIS with three tubes, dual Collins VHF-422C radios, and a comprehensive suite of navigation and communication equipment. This includes dual Collins VIR-432 navs, a Collins FCS-850 flight director, and a Collins APS-4000 autopilot. The aircraft is also equipped with ADS-B, TCAS II, and an EGPWS.
Maintenance Status
The aircraft has undergone a D-check, completed last year, and is on the CAMP maintenance tracking system. The next A-check is due in 89.9 hours, the B-check in 288.9 hours, the C-check in 1,088.9 hours, and the D-check in 2,288.9 hours. The airframe has a total of 7,539.4 hours and 6,142 landings.
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Full document text
PERFORMANCE Ramp Weight 16500 MTOW 16300 Max Landing Weight 15700 MZFW 13000 Max Cruise Speed 468 NBAA Range 1,457 Rec. Cruise Speed 430 Service Ceiling 45,000 ON CAMP 2 YEAR OLD PAINT RVSM COMPLIANT ADSB COMPLIANT D-CHECK COMPLETED LAST YEAR For SALE 1999 BEECHJET 400A Please call for more information TRIPP WACKER, BROKER 386-517-7216 R YAN AVIATION INC. SPECIFICATIONS YEAR 1999 MANUFACTURER: BEECHCRAFT MODEL 400A SERIAL NUMBER RK-222 REGISTRATION N482RK AIRFRAME (ON CAMP SYSTEM) TOTAL AIRFRAME HOURS 7539.4 TOTAL LANDINGS 6142 ENGINE SPECIFICATIONS TYPE: JT15D-5 SERIAL NUMBERS: LH ENGINE HOURS 7277.6 LH ENGINE HOURS 7496.6 LH ENGINE CYCLES 5794 LH ENGINE CYCLES 6074 ENGINE TBO 625.3 ENGINE TBO 406.4 HOURS SINCE HIS 1212.4 HOURS SINCE HIS 1346.48 HOURS SINCE OVERHAUL 2974.6 HOURS SINCE OVERHAUL 3193.44 AVIONICS / RADIOS - EFIS: Collins Proline II with 3 tube - VHF COM: Dual Collins VHF-422C VHF (8.33 COM spacing) - NAV: Dual Collins VIR-432 - AUDIO PANEL: Dual DB Systems DB-438 - FLIGHT DIRECTOR: Collins FCS-850 - AUTOPILOT: Collins APS-4000 - TRANSPONDER: Dual Collins TDR-94D with Mode S - ADF: Collins ADF-462 - DME: Dual Collins DME-422 - RMI: Dual Collins SDU-640A - RADAR: Collins TRW-850 - RADIO ALTIMETER: Coillins ALT-55B - CVR: L3 Communications 30 min CVR - FMS: Dual Collins AMS-5000 - GPS: Dual Collins GPS-4000 - HF King KHF-950 - TCAS: Collins TCAS-94 (TCAS II/Change 7) - DFDR: L3 Communications F1000 Flight Data Recorder - EGPWS: Honeywell MK5 with Windshear - ELT: Artex 406 - ADSB ADSB EQUIPPED, ALSO EQUIPPED WITH FLIGHTSTREAM-210 ADDITIONAL EQUIPMENT PERFORMANCE - Rhor Thrust Reversers Lights Ramp Weight 16500 - Vapor Cycle Air Conditioning MTOW 16300 - Logo Lights Max Landing Weight 15700 - Flitefone VI MZFW 13000 - B&D Cabin Display Max Cruise Speed 468 - RVSM SB NBAA Range 1,457 - 20 Degree Flaps Rec. Cruise Speed 430 - Flightstream 210 Bluetooth ADSB Service Ceiling 45,000 EXTERIOR 2 year old paint INSPECTION STATUS A CHECK DUE IN 89.9 - No Damage History B CHECK DUE IN 288.9 - Airframe on CAMP system C CHECK DUE IN 1088.9 D CHECK DUE IN 2288.9 MAINTENANCE 1999 BEECHJET 400A PCE-JA0213 (L) PCE-JA0211(R) ENGINES OVERHAULED BY P&W ENGINE SERVICES MAY/JUNE 2014 ALL TIMES SUBJECT TO VERIFICATION