AIRCRAFT FLIGHT
MANUAL
BRISTELL B23
Document No.: ADXC-73-001-AFM
Non-approved page
Revision: A2
1-8
Date of Issue: 15.04.2021
1.4
Descriptive data
− CS-23 Level 1 aircraft (formally CS-VLA)
− Day and Night VFR operation
− Maximum Take Off Weight 750kg
− Side-by-side seating
− Low wing monoplane
− Conventional cruciform design
− All aluminium airframe, composite canopy frames
− Power plant
o
Engine Rotax 912 S3
▪
Without airflow cap
▪
BRM exhaust
▪
BRM Airbox (carbon)
▪
BRM Engine interface ring-mount
▪
ROTAX oil cooler and tank
– oil system without thermostat
▪
ROTAX coolant radiator
– coolant system with thermostat
o
Propeller MTV-34-1-A/175-200
▪
Hydraulic governor P-110-051/A
− Fuel system
o
Fuel tanks in wing leading edge with strainer pick up
o
Left/Right/OFF fuel selector
o
Mechanical engine pump
o
Electric fuel pump with check valve bypass
o
Gascollator (water trap and filter)
o
Fuel return line (left tank only)
o
Fuel flow sensing
− Landing gear
o
Fixed tricycle
o
MLG composite spring type with differential hydraulic braking
o
NLG welded steel design steered (two push/pull cable on
excentre) and combined hydraulic/spring damper
− Control system
o
Elevator and Aileron pushrod system
o
Rudder cable / pulley system
o
Electric actuated trim for pitch and roll
o
Anti-Servo tab on pitch control
− Luggage
o
Luggage compartments in cabin (15kg)
o
Luggage compartments in wings (2 x 20kg each)
− AEPS (if installed – optional equipment)
o
BRS-6-1350 (ASTM compliant) on forward RHS fuselage
