Limitations

Question 1

AIRSPEED LIMITATIONS - Airframe

Answer 1

V_{MO (S.L. to 27,600 ft}) … 320 KIAS

M_{MO (above 27,600 ft)}… 0.80 Mach

Question 2

AIRSPEED LIMITATIONS - Flaps

Answer 2

V_FE/V_FO (S.L. to 20,000 ft)

(Flaps 10) …… 200 KIAS

(Flaps 20) ….. 200 KIAS

(Flaps DN) ….. 170 KIAS

Question 3

AIRSPEED LIMITATIONS - Landing Gear

Answer 3

V_LE……………… 200 KIAS

V_{LO (Extend)} … 200 KIAS

V_{LO (Retract)}… 180 KIAS

Question 4

AIRSPEED LIMITATIONS - Speed Brakes

Answer 4

M_SB………. NO LIMIT

V_SB……….. NO LIMIT

Question 5

AIRSPEED LIMITATIONS - Tires

Answer 5

V_TIRE……. 165Knots (True Ground Speed)

Question 6

AIRSPEED LIMITATIONS - V_MCA

Answer 6

V_MCA

(Flaps Up)………….. 104 KIAS

(Flaps 10) …………… 100 KIAS

(Flaps 20) …………… 96 KIAS

(Flaps DN)……………. 93 KIAS

Question 7

ENGINE LIMITS % RPM

N2 — Takeoff, Max Cont… ___% RPM

N1 — Takeoff, Max Cont… ___% RPM

N1 — Transient………………. ___% RPM

Answer 7

N₂— _{Takeoff, Max Continuous}… 98.8% RPM

N₁— _{Takeoff, Max Continuous}… 105.2% RPM

N₁— _Transient…………………….. 106.4% RPM

Question 8

ENGINE LIMITS - ITT TEMP (°C)

Max Continuous… ___°C

Takeoff……………….. ___°C ( __ Minutes)

Transient…………….. ___°C ( __ sec)

Start……………………. ____°C ( __ sec)

Answer 8

Max Cont … 805°C

Takeoff……… 820°C (5 Minutes)

Transient….. 835°C (10 sec)

Start………….. 1000°C (15 sec)

Question 9

ENGINE LIMITS OIL (°C/PSI)

Oil Temp for Starting ………………. –_ to __°C

Oil Temp takeoff and max cont thrust … __–__°C

Oil Press at Idle RPM……………………… __–___ psi

Oil Press takeoff and max cont thrust….. __–__ psi

Answer 9

Oil Temp

Starting ................... –40 to 135°C

Takeoff and max cont thrust ... +10 to 135°C

**Oil Press **

at Idle RPM ..................... 35 to 100 psi

takeoff and max cont thrust<sub></sub>...  45 to 90 psi

Question 10

WIND LIMITS FOR ENGINE STARTS

Answer 10

Tailwind Max…………. 15 KIAS

Crosswind Max……… 25 KIAS

Question 11

STARTER LIMITS

(Battery or External Power Assisted Start)

Answer 11

Motoring of engine is limited to TWO Start Attempts, with engine clearing after the first Attempt as follows.

20seconds…………….. ON

30 seconds …………… OFF

20 seconds……………. ON _{for engine clearing}

30 seconds …………… OFF

20seconds…………….. ON

2 hours…………………… OFF

Question 12

EXTERNAL POWER LIMITS

Answer 12

Volts …. 28.0–28.4

Amps … 400 Amps (Continuous)

        / 1000 Amps (Momentary)

Question 13

GENERATOR LIMITS

Ground Operation (Each Generator)

Answer 13

Maximum Amps… 325 Amps

Question 14

GENERATOR LIMITS

In-Flight Operation

Answer 14

One or Both Generators (to FL410)

Max Amps................. 325 Amps

One Generator (to FL290 in Icing Cond)

Max Amps ................ 400 Amps

Question 15

STRUCTURAL LIMITATIONS

Ramp

Takeoff

Landing

Zero Fuel

Answer 15

Maximum Weights:

Ramp ……….. 12,591 lbs

Takeoff………. 12,500 lbs

Landing …….. 11,600lbs

Zero Fuel …. 10,000 lbs

Question 16

FUEL LIMITS

Approved Fuels

Temps

Answer 16

Approved Engine Fuels (unlimited use)

Jet A, Jet A-1, JP-8

Fuel Temperature (°C)

Minimum….. –40°C

Maximum….. 43°C

Question 17

ICING LIMITATIONS - Max Temp / Time

Answer 17

Max Temp (°C)…… +10°C (ground ops)

Max Time (sec)….. 30 Seconds

Question 18

ICING LIMITATIONS - Must be ON below ____ ˚C

Answer 18

Temp (°C) ……… When operating in visibile moisture and 5°C or Colder (engines / wings)

Max 30sec Wing anti-ice ON, at Take-off Thrust, prior to Brake Release.

Question 19

ICING LIMITATIONS - Holding Min Speed. Flaps

Answer 19

Holding in Icing Conditions

Is prohibited below 160 KIAS.

Must have flaps UP

Question 20

AUTO PILOT LIMITATIONS

Answer 20

1. Coupled VOR approaches; using a VOR as the NAV source, are prohibited.
2. Do not use the auto pilot below 200 ft. above terrain during approach operations or below 500 ft. above the terrain during all other operations.
3. Maximum angle for NAV capture is 90°.

Question 21

EFIS LIMITATIONS - How many Adaptive Flight Displays must be operated in normal mode for takeoff?

Answer 21

All Adaptive Flight Displays must be operated in normal mode for takeoff

Question 22

VNAV LIMITATIONS

Answer 22

1. VNAV altitudes must be displayed on the MFD or CDU when utilizing VNAV for flight guidance.
2. Use of VNAV while conducting a missed approach procedure is prohibited.

Question 23

TAKEOFF AND LANDING OPERATIONS

Max. Airfield Elevation (Pressure Altitude) …. ____ ft

Ambient Temperature (°C) ……………… –__°C to ____°C

Maximum Tailwind (Component)
for Takeoff and Landing......................... \_\_ Kts

Maximum Fuel Imbalance

for Takeoff/Landing… ___ lbs

Answer 23

Max. Airfield Elevation (Pressure Altitude) …. 9,400 ft

Ambient Temperature (°C) … –40°C to ISA +37°C

Maximum Tailwind (Component)
for Takeoff and Landing.......... 10 Kts

Maximum Fuel Imbalance

for Takeoff/Landing… 200 lbs

Question 24

ENROUTE OPERATIONS

Maximum Operating Altitude… _____ ft

Ambient Air Temperature (°C)… –__°C to _____°C

Maximum Fuel Imbalance ……… ___ lbs

Yaw Damper ……………………………. _______

Answer 24

Max Operating Altitude … 41,000 ft

Ambient Air Temp (°C) … –65°C to ISA +37°C

Max Fuel Imbalance ……… 200 lbs

Yaw Damper ………………….. Operable and On