1. Field Length Limiting Take-Off Mass (FLLTOM) is a limiting factor on short runways.

2. Field Length Limiting Take-Off Mass (FLLTOM) decreases with higher flap/slat setting.

Operation                Twin Turbojet

Certificated Take-Off Flap Settings     5° and 15°

Field length available            2400 m

OAT                    -10° C

Pressure Alt.                7000 ft

PMC                    ON

A/C                    Auto

Packs                    ON

Anti-ice                OFF

Wind                    Zero

Runway Gradient            Zero

The Max. Take-off Mass is:

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1. Take-Off from RWY 24, TORA 2200 m, take-off path over flat terrain, 5 KT tailwind: Max Allowed Take-Off Mass 78.4 t

2. Take-Off from RWY 06, TORA 2300 m, take-off over 230 ft obstacle at 4200 m, 5 KT headwind: Max Allowed Take-Off Mass 77.3 t

The stated limitations for the runways are...

With the following information given, determine the tyre-speed limited take-off mass:

Runway 06, Airport Elevation: 1500 ft

QNH 1013 hPa, OAT: +35°C, W/V: 060/12

Take-Off configuration: Flaps 15

Tyre rating: 210 MPH

Power Management Computer (PMC): ON

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With the following information given, find V1, VR and V2 speeds for a MRJT aeroplane:

Airport Elevation 1000 ft, RWY 24, slope 1% UP

QNH 1013 hPa, OAT +15°C, W/V: 240/35 kt

TOM: 60700 kg, Flaps 5

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With the numbers from the annex showing a Regulated Take-Off Mass (RTOM) Table for runway 05L from position VB, and with the information given below, find the Regulated Take-Off Mass (RTOM) for departure:

OAT +12°C, Wind 050/05, QNH 1015 hPa

Anti-Ice (ENG only) OFF, Packs OFF

Quick line-up, Runway WET

(Do NOT interpolate, instead, use the most conservative numbers)

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With the numbers from the annex showing a Regulated Take-Off Mass (RTOM) Table for runway 05L from position VB, and with the information given below, find the Regulated Take-Off Mass (RTOM) for departure:

OAT +3°C, Wind 050/15, QNH 993 hPa

Anti-Ice (ENG only) ON, Packs OFF

Quick line-up, Runway WET

(Do NOT interpolate, instead, use the most conservative numbers)

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With the numbers from the annex showing a Regulated Take-Off Mass (RTOM) Table for runway 05L from position VB, and with the information given below, find V1, VR, and V2 speeds for a reduced thrust take-off:

OAT -2°C, Wind 050/05, QNH 1033 hPa

Anti-Ice (ENG only) ON, Packs ON

Assumed/FLEX T°: 59°C, Quick line-up, Runway WET

Take-off mass (TOM): Max Take-Off Mass (MTOM)

(Do NOT interpolate, instead, use the most conservative numbers)

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With the numbers from the annex showing a Regulated Take-Off Mass (RTOM) Table for runway 05L from position VB, and with the information given below, find the assumed/FLEX temperature and v-speeds:

OAT +12°C, Wind 050/16, QNH 1008 hPa, 

Anti-Ice (ENG only) OFF, Packs OFF, 

Quick line-up, 

Take-Off Mass 71480 kg.

(Do NOT interpolate, instead, use the most conservative numbers)

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With regard to the information given below, and assuming taxi distance is negligible, what would be the minimum turn-around time according to brake cooling schedule?

Landing mass: 50000 kg, Runway 24, Wind 060/04

approach with VREF 128 kt, correct for wind component minus 50% of headwind / plus 150% for tailwind, 

Airport Elevation 1000 ft, QNH 1013 hPa, OAT +25°C

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With regard to the information given below, and assuming taxi distance is negligible, what would be the minimum time between a rejected take-off and another take-off run?

Take-off mass: 55000 kg

Brakes-on-speed for rejected take-off: 100 kt

Retardation: Maximum braking and reverse thrust

Airport Elevation: 2500 ft, Wind VAR/02, QNH 1013 hPa, OAT -10°C

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With the information given below, determine the maximum permissible net mass allowing clearance from highest relevant obstacles:

Min. off-route pressure altitude: 16400 ft

Temperature: ISA + 5

ANTI-ICE ALL OFF

A/C AUTO (HIGH)

With the information given below, determine (1) time travelled, (2) ground distance and (3) fuel burned for drift-down after engine failure:

Drift-down (pressure altitudes): from 37000 ft to 20000 ft, 

Gross Mass at engine failure 51500 kg, 

Temperature ISA+20, 75 kt headwind, 

ENG WING ANTI-ICE OFF, A/C AUTO(HIGH)

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Why does the 35000 kg Gross Mass net Drift-Down curve start at approximately 4 min at FL370?

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Operation        Twin-Jet

Elevation        2000 ft

QNH            1013 hPa

Landing Mass        50000 kg.

Flap Setting        For Min. Landing Distance

Runway condition    Dry

Max. tailwind        15 kt

Max. headwind        50 kt

Anti-skid         Inoperative

To land with the most adverse wind condition, the Required Field Length is:

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With the information given below, determine the Climb-Limited Landing Mass:

Airport:

Elevation 3000 ft, QNH 1013 hPa, Temperature +20°C,

Configuration:

Flaps 30, A/C AUTO, ENGINE and WING ANTI-ICE ON.

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With the masses listed in the annex, what would be the maximum performance-limited landing mass to ensure compliance with applicable operational requirements for Commercial Air Transport?

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With the masses listed in the annex, what would be the maximum performance-limited landing mass to ensure compliance with applicable operational requirements for Commercial Air Transport?

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With the information given below, select the flap setting(s) that provide staying within limits given in the landing mass configuration table in the annex:

Structural-Limited Landing Mass: 79560 kg

Estimated Landing Mass: 65400 kg

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