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2001 Beechcraft Beechjet 400A

BEECHCRAFT BEECHJET 400 · Systems Description

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Overview

This document provides detailed specifications and information about the Beechcraft Beechjet 400A aircraft, including its systems, maintenance notes, and interior features. It highlights the aircraft's capabilities, configurations, and current status as of October 2024.

  • Seating for 8 passengers
  • ADS-B Out / TCAS II Version 7.1 installed
  • Belted lavatory included
  • Maximum take-off weight increased to 16,300 pounds
  • IFA Inspection Program incorporated
  • Total hours since new: 6,589:09
  • Cabin features a four-place club seating arrangement
  • Overall Matterhorn white exterior with black stripes

Document

Source

Originally published by website-files.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
·
Systems Description
Year
·
2001
File size
·
3.0 MB
Publisher
·
website-files.com
Language
·
en

Specifications & performance

Extracted from this document.

Specifications

Cabin width (ft)
·
4.92
Cabin height (ft)
·
4.75
Cabin length (ft)
·
15.6
Basic empty weight (lb)
·
10720
External baggage cu (ft)
·
26
Internal baggage cu (ft)
·
30
Maximum usable fuel (gal)
·
733
Maximum landing weight (lb)
·
15700
Maximum take off weight (lb)
·
16300
Maximum zero fuel weight (lb)
·
13000

Performance

Ferry range (nm)
·
1519
Service ceiling (ft)
·
45000
About this document
What is the 2001 Beechcraft Beechjet 400A?

The 2001 Beechcraft Beechjet 400A is a systems description for the BEECHCRAFT BEECHJET 400, dated 2001.

Where does the 2001 Beechcraft Beechjet 400A come from?

This copy of the 2001 Beechcraft Beechjet 400A was originally published by website-files.com and is hosted on Sprinkle as a free, searchable reference copy.

What year was the 2001 Beechcraft Beechjet 400A published?

The 2001 Beechcraft Beechjet 400A — the BEECHCRAFT BEECHJET 400 systems description on file — is dated 2001.

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In this document

Aircraft Overview

The Beechcraft Beechjet 400A is a business jet with a maximum take-off weight of 16,300 pounds and a seating capacity for 8 passengers.

Engines

Equipped with two Pratt & Whitney JT15D-5 engines, with total hours since new of 8,779:44 for the left engine and 10,425:07 for the right engine.

Interior Features

The cabin features a center four-place club seating arrangement, two forward-facing aft seats, and a belted lavatory, along with an in-flight information system.

Exterior Specifications

The aircraft is painted overall in Matterhorn white with black stripes.

Avionics

The aircraft is equipped with a Collins Pro Line 4 EFIS, dual VHF communication radios, and various other advanced avionics systems.

Maintenance Notes

The aircraft is under an IFA Inspection Program, with various inspection types scheduled for future dates.

Full document text

The information contained in this document is confidential, privileged and only for the information of the intended recipient and may not be used, published or redistributed. 2001 Beechcraft Beechjet 400A Aircraft specification S/N RK-0318 Reg. OK-BII W O R T H A T T E N T I O N HIGHLIGHTS Seating for 8 Passengers ADS-B Out / TCAS II Version 7.1 Installed Belted Lavatory Increased Maximum Take-Off Weight to 16,300 pounds Incorporated IFA (Increase Flight Activity) Inspection Program IFA-D Inspection Performed 7/2024 Aircraft Brokerage & Asset Advisory sales@jetron.aero | +421 903 425 746 | www.jetron.aero 2001 Beechcraft Beechjet 400A A I R F R A M E Total Hours Since New 6 589:09 (As of October 01, 2024) Total Cycles Since New 5 094 (As of October 01, 2024) Certification Date April 2001 Current location Prague (Czech Republic) E N G I N E S Description Pratt & Whitney JT15D-5 Pratt & Whitney JT15D-5 Serial number PCE-100182 PCE-100361 Total Hours Since New 8 779:44 10 425:07 (As of October 01, 2024) Total Hours Since Overhaul 561:114 854:25 Cycles Since New 7 652 8 735 (As of October 01, 2024) Left Right Aircraft Brokerage & Asset Advisory sales@jetron.aero | +421 903 425 746 | www.jetron.aero 2001 Beechcraft Beechjet 400A I N T E R I O R Number of passengers 8 Passenger configuration Cabin configuration Centre four-place club seating arrangement, two forward facing aft seats, aft facing forward seat by the door and belted lavatory Cabin equipment Airshow in flight information system with a single display in the forward bulkhead, three pull-out tables, two 12 volt DC outlets Notes Extended galley storage area, cockpit and cabin separated by sliding hard pocket door Aircraft Brokerage & Asset Advisory sales@jetron.aero | +421 903 425 746 | www.jetron.aero 2001 Beechcraft Beechjet 400A INTERIOR TOUR Aircraft Brokerage & Asset Advisory sales@jetron.aero | +421 903 425 746 | www.jetron.aero 2001 Beechcraft Beechjet 400A E X T E R I O R Base paint color(s) Overall Matterhorn white Stripe color(s) Black stripes Aircraft Brokerage & Asset Advisory sales@jetron.aero | +421 903 425 746 | www.jetron.aero 2001 Beechcraft Beechjet 400A Aircraft Brokerage & Asset Advisory sales@jetron.aero | +421 903 425 746 | www.jetron.aero 2001 Beechcraft Beechjet 400A A V I O N I C S Type of Unit Description EFIS (Electronic Flight Instrument System) Collins Pro Line 4 (4-Tube) RTU (Radio Tuning Unit) Dual RTU-870C VHF Communication Radios Dual VHF-422C ADC (Air Data Computer) Dual ADC-850D AHC (Attitude Heading Computer) Dual AHC-85E Radar Receiver/Transmitter Single Rockwell Collins RTA-854 ADF (Automatic Direction Finder) Single ADF-462 EGPWS (Enhanced Ground Proximity Warning System) Allied Signal Mark V FMS (Flight Management System) Dual Collins AMS 5000 Navigation Radios Dual VIR-432 TCAS (Traffic Collision Avoidance System) Single TTR-921 TCAS II with 7.1 Compensation Unit Dual ICU-85 CVR (Cockpit Voice Recorder) L3 FA2100 Transponder with Enhanced Surveillance Dual TDR-94D Mode S RA (Radio Altimeter) Single Rockwell Collins ALT-55B DME (Distance Measuring Equipment) Dual DME-442 GPS sensor (Global Positioning System) Single Rockwell Collins GPS-4000S FDR (Flight Data Recorder) Single Fairchild F1000 DAU (Data Acquisition Unit) Collins Aerospace DAU-650 ELT (Emergency Location Transmitter) Artex C406-1 ADS-B Out Installed under SB-34-4154 Aircraft Brokerage & Asset Advisory sales@jetron.aero | +421 903 425 746 | www.jetron.aero 2001 Beechcraft Beechjet 400A M A I N T E N A N C E N O T E S Incorporated IFA (Increase Flight Activity) Inspection Program Inspection Type Last performed Next Due A 6 421:01 6 821:01 B 6 421:01 7 221:01 C 6 421:01 8 021:01 D 6 421:01 9 621:01 W E I G H T S Maximum Take Off Weight 16 300 lb Maximum Landing Weight 15 700 lb Basic Empty Weight (As of July 11, 2024) 10 720 lb Maximum Zero Fuel Weight 13 000 lb Maximum Usable Fuel 733 gal B A S I C A I R C R A F T C H A R A C T E R I S T I C S Cabin Height 4.75 ft Cabin Length 15.6 ft Cabin Width 4.92 ft Internal Baggage 30 cu ft External Baggage 26 cu ft Service Ceiling 45 000 ft Ferry Range 1 519 nm sales@jetron.aero | +421 903 425 746 www.jetron.aero Specifications, descriptions, terms, and pricing are provided as introductory information only. Interested parties should rely upon their own inspections and examinations of the aircraft and its records. This introductory information is subject to changes and/or correction, and does not constitute representations or warranties by JETRON s.r.o. or its clients. This material does not represent a binding offering, and the aircraft is subject to prior sale and/or withdrawal from the market at any time. JETRON s.r.o. neither warrants the information’s accuracy nor assumes any responsibility or legal liability for any loss or damage, including, (but not limited to) incidental, special or consequential loss, whatsoever and howsoever arising, either in contract or tort (including negligence), to any party arising out of their reliance or alleged reliance upon it, without limit. Make Offer A S K I N G P R I C E