C&L Aerospace|Aircraft Specifications
Beechcraft Beechjet 400A · Weight And Balance
Overview
This document provides detailed specifications for the Beechcraft Beechjet 400A, specifically for aircraft serial number RK-197. It includes critical information such as operating weights, engine details, landing gear specifications, and avionics configuration. The document is intended for pilots, maintenance personnel, and aviation enthusiasts who require precise data for operational and maintenance purposes. Key metrics such as maximum take-off weight, landing weight, and fuel capacity are outlined to assist in weight and balance calculations and operational planning.
- Maximum Take-Off Weight: 16,100 lbs
- Maximum Landing Weight: 15,700 lbs
- Maximum Zero Fuel Weight: 13,000 lbs
- Basic Operational Empty Weight: 10,585 lbs
- Fuel Capacity: 4,912 lbs
Document
Source
Originally published by cla.aero. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Weight And Balance
- Year
- 2017
- Pages
- 2
- File size
- 248 KB
- Publisher
- cla.aero
Common. Rarer than 24% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Beechcraft Beechjet 400A.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Aircraft Specifications
The Beechjet 400A has a maximum take-off weight of 16,100 lbs and a maximum landing weight of 15,700 lbs. The maximum zero fuel weight is 13,000 lbs, and the basic operational empty weight is 10,585 lbs. The aircraft has a fuel capacity of 4,912 lbs.
Engine Details
The aircraft is equipped with two JT15D-5 engines, with serial numbers PCE-JA-0162 and PCE-JA-0161. Each engine has a total time of 3,677.3 hours and 3,510 cycles. Time since overhaul for both engines is 39.1 hours, with 25 cycles since overhaul.
Landing Gear Specifications
The landing gear includes main and nose landing gear with specific cycle remaining details. The left and right main landing gear shock struts have 3,998 cycles, with 1,002 cycles remaining. The nose landing gear shock strut also has 3,998 cycles with 1,002 cycles remaining.
Inspection Status
The document outlines the inspection status for the aircraft, including the last performed times and remaining hours for various inspections. For example, the last complete A inspection was performed at 4,363.9 hours, with 160.9 hours remaining until the next inspection.
Avionics Configuration
The avionics suite includes various Collins systems such as the APS 850 autopilot, VHF-422A communication radios, and a 3-tube EFIS. The document lists the specific models and quantities of each avionics component installed.
Full document text
C&L Aerospace|Aircraft Specifications 6 September 2017 A/C Model: Beechjet 400A RK-197 1 A/C Model: BEECHJET 400A A/C Serial Number: RK-197 Number of Seats: 8 Date of Build: 1998 Avionics: Collins A/C Total Time: 4,403.0 Hours Country of Registration: USA A/C Total Cycles: 3,998 Cycles Registration Number: N940VA Aircraft Location: Salt Lake City, Utah #1 Position Serial Number JT15D-5 Engine PCE-JA-0162 Total Time 3,677.3 Total Cycles 3,510 Time Since Overhaul 39.1 Cycles Since Overhaul 25 #2 Position Serial Number JT15D-5 Engine PCE-JA-0161 Total Time 3,677.3 Total Cycles 3,510 Time Since Overhaul 39.1 Cycles Since Overhaul 25 L/H Main Landing Gear CSO Cycles Remaining R/H Main Landing Gear CSO Cycles Remaining Shock Strut 3,998 1,002 Shock Strut 3,998 1,002 Side Strut 3,998 1,002 Side Strut 3,998 1,002 Nose Landing Gear CSO Cycles Remaining Shock Strut 3,998 1,002 Drag Strut 3,998 1,002 C&L Aerospace|Aircraft Specifications 6 September 2017 A/C Model: Beechjet 400A RK-197 2 Inspection Status Hourly Last Performed Time Remaining Complete A (200 HR) 4363.9 160.9 Complete B (400 HR) 4190.5 187.5 Complete C (1200 HR) 4190.5 987.5 Complete D (2400 HR) 5K initial not yet due 597.0 Configuration Number of Location of Galley 1 FWD Number and Location of Lavatory 1 FWD Number of Crew Seats 2 Cockpit Aircraft Paint Scheme White – Tan/Black Stripe TCAS Yes TAWS Yes Operating Weight Avionics Maximum Take-Off Weight 16,100 lbs Maximum Landing Weight 15,700 lbs Maximum Zero Fuel Weight 13,000 lbs Basic Op. Empty Weight 10,585 lbs Fuel Capacity 4,912 lbs Nomenclature Manufacturer Model Qty ACARS Not installed Not installed 0 Autopilot w/ Yaw Damper Collins APS 850 1 VHF Comm. Collins VHF-422A 2 VOR/ILS Collins VIR-432 2 DME Collins DME-422 2 TCAS Computer Collins TTR-920 1 ADF Collins ADF-462 1 FMS W/ 4000A GPS Collins FMS-5000 2 3-Tube EFIS Collins 3-TUBE EFIS 1 Radar Collins RTA-854 1 HF Collins - 1 Radio Altimeter Collins ALT 55B 1 ATC (Mode S) Collins TDR-94D 2 CVR Fairchild A-100S 1 RMI Collins SDU-640B 1 TAWS Allied Signal - 1