2001 Beechjet 400A Private Jet (OK-BII) (SOLD)

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.

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Description

AIRFRAME
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)

ENGINES
Type: Pratt & Whitney JT15D-5 / Pratt & Whitney JT15D-5
Serial Numbers: 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)

AVIONICS
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

INTERIOR
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 & 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 & cabin separated by sliding hard pocket door

EXTERIOR
Base paint color(s) Overall Matterhorn white
Stripe color(s) Black stripes

MAINTENANCE NOTES (Inspection Type: Last Performed / Next Due)
Incorporated IFA (Increase Flight Activity) Inspection Program
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

WEIGHTS
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

BASIC AIRCRAFT CHARACTERISTICS
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