Extra questions Flashcards
Why is correct loading (weight and balance) important?
Ensure aircraft stability and controllability
High stall speed, high TO/Landing speed, Longer distance required
Poor climb performance
Less manoeuvrability
High fuel consumption, less range and endurance
Adding weight CG limit: 120 – 130 Current CG: 126 Current Wt: 5000kg Additional weight of 120kg to baggage area (160)?
CG is 126.8
Removing weight CG limit: 120 – 130 Current CG: 125 Current Wt: 6200kg Removing weight of 70kg from baggage area (150)?
124.7
Moving weight W x d = w x D CG limit: 120 – 130 Current CG: 133 Current Wt: 5500kg How much weight to be moved from baggage area 170 to area 60 to ensure CG is within limit?
150kg
BEW = 1000kg/arm 1500mm aft of datum Payloads separated Row 1 – 150kg/1000mm Row 2 – 130kg/1800mm Baggage compartment – 20kg/2100mm Fuel load – 70kg/1400mm
Loaded CG position?
1477.4mm
To correct for a CG aft of its rear CG limit, you could?
A. Unload passengers from front seats
B. Move light passengers in the front row to empty rear-most seats
C. Move heavy passengers in the rear-most seats to most forward seats
C
What are Factors affecting take-off performance.
Weight, Density (temperature), Runway condition, Runway surface, Runway slope
Wind
State ISA conditions
Pressure – 1013.2 hPa Temperature – 15’C Pressure lapse rate – 1hPa/30 ft Temperature lapse rate – 2/c per 1000ft Air is assumed to be dry
how do you calculate Pressure Altitude ?
1013 – Actual pressure
= Pressure diff x 30ft per hPa
= Height change + aerodrome elevation
= PA
how do you calculate Calculate Density Altitude?
Actual temp – ISA temp at PA
= Temp difference x 120 (ft per ‘C)
= Height change + PA
= DA
Given the aerodrome elevation is 820ft/QNH 1007hPa/ Temperature 18’C. Aerodrome DA is?
PA = 1013 – 1007 = 6hpa x 30 = 180 ft + 820ft = 1000 ft DA = 18’ – 13’ = 5’C x 120 = 600 ft + 1000 = 1600ft
What is a drift? How is it determined (Which side)? What affects it?
Drift is the angular difference between aircraft heading and track.
Drift is determined by the side of the tail is on.
Factors: Strength of wind, wind direction, TAS of aircraft
Different types of times. Time zone
LMT, UTC, Zulu, GMT (Longitude degree and time)
The wind on an area is 080’T. The magnetic equivalent if the variation is 7’E is?
The wind on an area is 080’T. The magnetic equivalent if the variation is 7’E is?
073’M
(VARIATION EAST, MAGNETIC LEAST VARIATION WEST, MAGNETIC BEST)
An aircraft is scheduled to depart an aerodrome located on 090’E meridian at 1500UTC on 24th May. What is the date and time, in six-figure, of departure in LMT?
LONGITUDE EAST, UTC LEAST LONGITUDE WEST, UTC LESS 360’ per 24 hours, 15’ per hour 90 ÷ 15 = 6 hours Therefore, 1500 + 6 hours = 2100 242100