Gulfstream V Training Captain's Questions and Answers
FlightSafety KSAV
- Cockpit Preflight Inspection
- Exterior Preflight Inspection
- APU Starting
- Before Starting Engines
- Bleed Air Panel
- Temperature Control Panel
- Cabin Pressure Control Panel
- Windshield Heat
- Anti Ice Heater
- Windshield Blower
- Cowl and Wing Anti Ice
- Fuel System Panel
- L/R Main Tru
- Cabin Galley Master
- Cabin Window Heat
- PWR XFR Unit (PTU)
- Aux Pump
- Cockpit Light Master Control
- Crank/Start Master
- Side Consoles
- Instrument Panel
- Pedestal
- Engine Ground Start
- After Starting Engines
- Taxi Before Takeoff
TAXI BEFORE TAKEOFF
- In the unlikely event that you make the wrong turn during taxi out, what is the minimum taxi strip required to complete a 180° turn?
- 62 feet
- What is the Minimum Turning Circle Diameter required to avoid striking other aircraft or obstruction while executing a 180° turn?
- 112 feet
- What is Wing Growth?
- Wing Growth is the fact that some swept wing aircraft's wing making a larger arch outside the width of the wing when you execute a taxi turn while locking the inside brakes.
- Does Wing Growth effect the GV?
- Yes the GV Wing will arch 2 feet 4 inches outside of it’s normal straight ahead path while making a taxi turn and holding the inside brake.
- Just prior to Line-Up, you select INHIBIT on the eyebrow panel to inhibit tones. What message tones will not be inhibited when the INHIBIT Switch is selected?
- All Red MESSAGES and Amber CAT II INVALID, and COUPLED DATA INVALID
- Why does the Weather Radar go into Forced Standby on landing?
- So you don’t accidentally microwave a ground guide.
- How can the Weather Radar be taken out of Forced Standby if you want to take a quick look at the weather prior to takeoff?
- Press the TGT Button 4 times in 3 seconds.
- Is there any simple way to remember how to navigate through the Quick Reference Handbook tabs?
- Yes, everything is listed in alphabetical order in the messages and also in the Tabs. However, you can also quickly find Abnormal / Emergencies by remembering a few simple things about the aircraft:
- Tab 1 The GV is an electrical aircraft; therefore electrical malfunctions are in this tab.
- Tab 2 Two engines, everything associated with engine malfunctions is listed here.
- Tab 3 Three places where fires can be extinguished along with fire detection problems.
- Tab 4 Four flight control surfaces and associated malfunctions.
- Tab 5 Hydraulic Pumps and associated malfunctions.
- Tab 6 Six landing gear wheels and associated malfunctions.
- Tab 7 Seven Bleed Air Ducting, overheats and associated malfunctions.
- IN the QRH Tab 4, Page 5 (03-13-21 JAMMED AILERONS) # 6. What does the following statement mean? "Flight Spoilers Hydraulic Power Requirements......CONSIDER BASED ON AMOUNT OF FLIGHT SPOILER DEPLOYMENT".
- Turn OFF the SPOILER CONTROL on the Center Console if the FLIGHT SPOILERS become uncontrollable with the Aileron Jammed Up. Recall, the Flight Spoilers will augment the Roll Control when the Ailerons move more than 1/2°. With the Ailerons › 1/2° the Flight Spoilers will deploy that much further up to a max of 47°.
- In the QRH Tab 4, Page 14 (03-13-91 AILERON HOPS ACTIVATION). What does the following statement mean? "IF HARDOVER CONDITION IS DETERMINED TO BE CORRECTABLE OR CORRECTED":
- What were you doing prior would be an operable phrase. If you were in Moderate to Severe Turbulence, you might consider pulling and resetting the appropriate circuit breakers. However, if your were in smooth air, you might leave it alone without pulling and resetting the circuit breakers. Recall, the Aileron HOPS has a ½ second delay before activation. Therefore, if you are flying at 206 Knots and are moving the roll control from stop to stop, the HOPS should not activate.
- In the QRH Tab 7, page 10-11(03-22-20 SMOKE IN BAGGAGE COMPARTMENT, AFT GALLEY OR LAVATORY, ITEM 8): ,How long should you press and hold the "HOT MIKE" on the Jump Seat Audio Control Panel for it to activate the Audio Panel on the Smoke Evacuation Valve Panel forward of the Baggage Compartment Internal Door?
- 2 Seconds.
- In the QRH Tab 4, page 1 (03-12-00 FAILURE OF FLAP / STABLIZER SYNCHORONIZATION) Which part of the checklist is for Flaps and which part is for the Stabilizer?
-
- If you have a Flap Malfunction which would be indicated by amber messages:
- FLAP ASYMMETRY
- FLAP CMD INVALID
- FLAPS FAILED
- If you have a Stabilizer Malfunction which would be indicated by amber messages:
- FLAP / STAB IND OP
- FLAP / STB MISCOMPARE
- FLP / STB SYNC FAIL
- STABLIZER FAILED
- If you have a Flap Malfunction which would be indicated by amber messages:
- How do we obtain VREF -----APPROPRIATE TO CONFIGURATION as depicted in QRH Tab 4, page 2, (03-12-30 PARTIAL OR JAMMED FLAPS LANDINGS)?
- Display Controller, FLT/REF page, in lower right-hand corner of display.
- Where does the Display Controller obtain inputs to calculate correct Vref speeds?
- SAT, Pressure Altitude, Aircraft Weight and FLAP HANDLE POSITION.
- Can we obtain the Vref speed anywhere else?
- Yes, in the back of the QRH in LANDING PERFORMANCE 04-10-20 LANDING SPEED SCHEDULE
This article is included in Gulfstream Contract Pilot Services' resource library strictly for your convenience. The information in this article is provided without guarantee or warranty, and is subject to change without notice. The information is the opinion of the writer, and may not reflect the opinion(s) of Gulfstream Contract Pilot Services or it's associates. The information should not be relied upon as advice to help you with your specific issue. We recommend that you discuss the specific facts of your situation with a qualified professional before making any personal or business decisions.

