Limitations

Question 1

RVSM Required Equipment List

Answer 1

Equipment, Requirements:
Autopilot(1), Must be operational
Altitude Alerting System, Must be operational
Altitude Reporting Transponder (2),
One must be operational
Air Data Computers (2),
Two must be operational

Question 2

Maximum Taxi and Ramp Weight

Answer 2

75,250 lbs.

Question 3

Maximum Takeoff Weight

Answer 3

75,000 lbs.

Question 4

Maximum Landing Weight

Answer 4

67,000 lbs.

Question 5

Effect of landing gear retraction on CG position is:

Answer 5

Negligible.

Question 6

Max airport pressure altitude for takeoff and landing is:

Answer 6

8,000 feet

Question 7

Max operating altitude is

Answer 7

41,000 feet

Question 8

Max ambient air temperature approved for for takeoff is:

Answer 8

ISA +35C

Question 9

Minimum ambient temperature approved for takeoff is:

Answer 9

-40C

Question 10

Cowl Anti-Ice, Ground Operations

Answer 10

Must be on when OAT is 10C or below AND visible moisture in any form is present (such as fog with visibility of 1,500 meters (1mile) or less, rain, snow, sleet and ice crystals.

WHEN operating on runways, ramps or taxiways where surface snow, ice standing water or slush is present.

Question 11

Cowl Anti-Ice, Flight Operations

Answer 11

Must be on when in icing conditions, or ice is annunciated by the ice detection system.

EXCEPT when SAT is -40 or below

Question 12

Define Icing Conditions (in-flight)

Answer 12

Icing conditions exist in-flight at a TAT of 10C or below, and visible moisture in any form is encountered (such as clouds, rain, snow, sleet or ice crystals), except when the SAT is -40C or below.

Question 13

Wing Anti-Ice, Ground Operations

Answer 13

Must be on for takeoff when the OAT is 5C or below AND visible moisture in any form is present (such as fog with visibility of 1,500 meters (1mile) or less, rain, snow, sleet or ice crystals)

AND/OR the runway is contaminated with surface snow, slush, or standing water.

Question 14

Wing Anti-Ice, Ground Operations – When Type II or Type IV anti-icing fluids have been applied:

Answer 14

Wing anti-ice system must only be selected on, if required, just prior to thrust increase for takeoff.

Question 15

Wing Anti-Ice, Flight Operations

Answer 15

The wing anti-ice system must be on (EXCEPT when SAT is -40C or below) when:
Ice is annunciated by the ice detection system
In icing conditions and the airspeed is less than 230 KIAS

DO NOT HOLD IN ICING CONDITIONS WITH SLATS/FLAPS EXTENDED.

Question 16

Supercooled Large Droplet Icing

Answer 16

Continued operations in areas where SLD icing conditions exist is prohibited.

Wing and cowl anti-icing systems must be on in SLD icing conditions.

Leave icing conditions when side window icing occurs.

Question 17

How are SLD icing conditions indicated?

Answer 17

SLD icing conditions are indicated by ice accretion on the flight deck side windows.

Question 18

Cold Weather Ops

Answer 18

Take-off is prohibited with frost, ice, snow or slush adhering to any critical areas (wings, upper, fuselage, horizontal stabilizer, vertical stabilizer, control surfaces and engine inlets)

Takeoff is permitted with frost adhering to:
Upper surface of the fuselage if it is possible to distinguish surface features.
Max 1/8in layer of frost on the underside of the wing that is caused by cold soaked fuel.

Question 19

Runway Slopes

Answer 19

Max runway slopes approved for takeoff and landing are: +2% uphill and -2% downhill

Question 20

Max tailwind component approved for takeoff and landing is

Answer 20

10knots

Question 21

Ozone Concentration

Answer 21

Airplane operations prohibited on routes where ozone concentrations exceed:

.25 ppm by volume, sea level equivalent, at any time above FL320

.1 ppm by volume, sea level equivalent, time-weighted average during any 3 hour interval above FL270.

Question 22

Engines

Answer 22

General Electric CF34-8C5B1

Question 23

Engines High PWR Schedule Switchlight

Answer 23

Use of the Engines High PWR schedule switchlight is prohibited.

Question 24

ITT Ground Start Temp Limit

Answer 24

815C

Question 25

Oil Pressure Ground Start Limit

Answer 25

182PSI, 95PSI after 10min Should show + value during start and may peak beyond 182PSI. Oil pressure may be greater than 95PSI for a max of 10 minutes.

Question 26

Engine Op Limits

Answer 26

Normal takeoff power and max power (two engines) is limited to 5 minutes. APR power (one engine) is limited to 10 minutes. ITT must be below 120C before attempting to ground start engine.

Question 27

Continuous Engine Ignition must be used during:

Answer 27

Takeoffs and landings on contaminated runways Flight through moderate or heavier intensity rain Flight through moderate or heavier intensity turbulence. Flight in the vicinity of thunderstorms.

Question 28

Reduced (FLEX) Takeoff Thrust for takeoff is NOT authorized when:

Answer 28

Wing and/or cowl anti-ice bleeds are in use Runway is contaminated with standing water, slush, snow or ice* Warnings or forecasts of windshear or downdrafts exist (including LLWAS advisories) Antiskid system is inoperative The engine cannot achieve full rated thrust** *FLEX thrust may be used for takeoff on wet runways, provided the flight crew selects "WET" runway performance data on the FMS MCDU **GoJet utilizes a FAA-approved engine trend monitoring program, which continuously monitors engine parameters, and alerts maintenance when an engine begins to approach its deterioration limits. this program ensures compliance with rated thrust limitation, above.

Question 29

3-13.13.3 (Engine Start times) PG 17

Answer 29

See tablet.

Question 30

The max permissible fuel imbalance between the contents of left wing tank and right wing tank are:

Answer 30

During takeoff: 300 lbs | all other phases of flight: 800 lbs

Question 31

Takeoff with a fuel load in excess of 500 lbs in the center tank is not permitted unless:

Answer 31

each main wing tank is above 4,400 lbs OR | each main wing tank is less than 4,400 lbs consult AFM limitations.

Question 32

Minimum fuel quantity for go-around is:

Answer 32

600 lbs per wing tank (airplane level) and assuming a max airplane climb altitude of 10deg nose up.

Question 33

APU starter motor duty cycle is limited to:

Answer 33

Not more than 3 starts/start attempts in 1 hour. A two minute delay must be observed between cranking attempts to allow for cooling of starter and starter contactor and APU fuel drainage.

Question 34

VFE

Answer 34

Max flap extension speed. ``` Flaps 1 / 230KIAS Flaps 8 / 230KIAS Flaps 20 / 230KIAS Flaps 30 / 185KIAS Flaps 45 / 170KIAS ```

Question 35

VLO

Answer 35

Max gear extension/retract speed. Extension: 220KIAS Retraction: 200KIAS

Question 36

VLE

Answer 36

Max gear extended speed: 220KIAS (down and locked)

Question 37

Turbulence Penetration Speed

Answer 37

Max airspeed for turbulence penetration is 280KIAS or .75 Mach (whichever is lower)

Question 38

Minimum Operating Speed Limit

Answer 38

Intentional speed reduction below onset of stall warning, as defined by stick shaker operation is prohibited unless a lower speed is specifically authorized for flight test or training operations.

Question 39

Windshield Wiper Operations

Answer 39

Must not be operated above 250KIAS If wiper has failed in a non-parked position, airplane speed must not exceed 250KIAS.

Question 40

Maneuvering Limit Load Factors

Answer 40

Flaps Retracted: -1.0 to 2.5 G Flaps Extended: 0.0 to 2.0 G **Avoid unnecessary and large side-slip maneuvers during low speed high altitude cruise.

Question 41

Max Relief Differential Pressure (A/C & Pressurization)

Answer 41

8.7PSI

Question 42

Max Negative Differential Pressure (A/C & Pressurization)

Answer 42

-0.5PSI

Question 43

During taxi, takeoff and landing, the pressure differential must not exceed:

Answer 43

0.1PSI

Question 44

The airplane must be completely depressurized prior to:

Answer 44

Opening any of the airplane doors.

Question 45

To preclude possible crew and/or passenger ear damage:

Answer 45

use of the EMERG DEPRESS switch above 15,000 feet is prohibited.

Question 46

Max altitude for single pack operations is:

Answer 46

31,000 feet

Question 47

What does QRH Volume 1 contain?

Answer 47

Max allowable flight duration at altitude in accordance with 14CFR 25.832 (a)(2)

Question 48

Autopilot minimum use height: Takeoff

Answer 48

Minimum Use Height: 600 feet AGL

Question 49

Autopilot minimum use height: Non-Precision Approach

Answer 49

Airport elevation 4,000 feet approved | Minimum use height: 400 feet AGL

Question 50

Autopilot minimum use height: Precision Approach (Glidepath 3.5deg)

Answer 50

Airport elevation 4,000 feet approved | Minimum Use Height: 80 feet AGL

Question 51

Autopilot minimum use height: Precision Approach (Glidepath > 3.5deg, <= 4.0deg)

Answer 51

Airport elevation 4,000 feet prohibited | Minimum Use Height: 120 feet AGL

Question 52

ADC Source and flight in RVSM airspace

Answer 52

The ADC source coupled to the active autopilot must be the same as that coupled to the ATC Transponder during flight in RVSM airspace.

Question 53

Permissible AC Electrical System Loads

Answer 53

Individual AC generator loading must not exceed: 0 to 41,000 feet: Main Generator (each) 40kVA 0 to 41,000 feet: APU Generator 40kVA

Question 54

In-Flight, Max permissible continuous load on each TRU is:

Answer 54

120 amps

Question 55

Ground Operation, Protect CRT displays

Answer 55

Max permissible time for ground operations with DC power is 5 minutes.

Question 56

Circuit Breaker Reset (in-flight)

Answer 56

A circuit breaker must not be reset or cycled unless doing so is consistent with explicit procedures specified in the Airplane Flight Manual or unless PIC deems necessary for safe completion of the flight.

Question 57

Slats/Flaps

Answer 57

Enroute use of slats/flaps is prohibited. Flight with slats/flaps extended at altitudes above 15,000 feet is prohibited.

Question 58

Flight Spoilers

Answer 58

Flight spoilers must not be extended in-flight below an altitude of 300 feet AGL. To ensure adequate maneuver margins, flight spoilers must not be extended in-flight at air speeds below the recommended approach speed plus 10KIAS.

Question 59

Stall Protection

Answer 59

Both stall protection system switches must remain on for all phases of light.

Question 60

Thrust Reversers

Answer 60

Approved for ground use only. Intended for use during full stop landings Go-around not to be attempted after activating thrust reversers Takeoff with thrust reverser icons or EICAS warning and/or caution message displayed is prohibited. Below 75KIAS, reverse thrust must be less than 60% N1 Backing up using reverse thrusters is prohibited.

Question 61

Taxi Lights

Answer 61

Must be switched off whenever airplane is stationary in excess of 10 minutes

Question 62

Wheel brake cooling limitations

Answer 62

There must be sufficient time to allow brake cooling between a rejected takeoff and subsequent takeoff to make sure there is enough brake energy to bring the aircraft to a stop in the event of another rejected takeoff.

Question 63

Nose Wheel Steering System (Towbarless Towing)

Answer 63

Towbarless towing is prohibited unless performed in compliance with Airplane Maintenance Manual towbarless towing requirements.

Question 64

When setting MDA marker on the barometric altimeter using the DH/MDA knob on the altitude reference panel the next highest 10-foot increment must be:

Answer 64

selected if the altitude is not at a 10-foot increment.

Question 65

TCAS (Authorized, action after TCAS RA)

Answer 65

Authorized to deviate from ATC clearance in order to comply with TCAS resolution advisory (RA) command. Notify dispatch after compliance with TCAS RA.