Gulfstream GVII

Eddie sez:

Keep in mind that the driftdown procedure is designed to extract the maximum amount of foward distance from the airplane with an engine failed at high altitude, regardless of who is below you. If you are not alone in your block of airspace, does it really make sense to jeopardize the lives of hundreds of lives on a large airline passenger jet for the sake of the few siting behind you? On the other hand, if you can driftdown safely, there are techniques to do this safely. Unlike previous Gulfstreams, the driftdown charts are not where you suspect they are. Go to the Airplane Operating Manual, Performance section.

Everything here is from the references shown below, with a few comments in an alternate color.

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AOM Procedure

[AOM, §05-06-10, ¶1]

  1. Driftdown data are provided as a function of altitude and weight at the time of an engine failure. The driftdown performance is shown for temperatures of ISA and ISA+20°C. For temperature less than ISA, temperature corrections are provided at the bottom of the ISA table.

  2. Driftdown Procedure

  3. (1) To attain the driftdown performance shown, the recommended driftdown procedure described below must be followed.

    (a) At the failure of one engine, Maximum Continuous Thrust is set and held on the operating engine during any deceleration, if required to reduce the speed to the entry descent Mach. Any deceleration should be performed at the initial altitude before the start of descent.

    (b) The descent Mach number should be maintained until the calibrated speed is intercepted. The calibrated speed is then held down to the final driftdown altitude (identified as “Cruise Altitude”).

    (c) At the final driftdown altitude, a 200 FPM rate of climb capability will be possible at Maximum Continuous Thrust at the “Start Cruise” Calibrated Airspeed shown. The “Start Cruise” Calibrated Airspeed shown is the single engine, Long Range Cruise speed at the final driftdown altitude.

    (d) Moderate thrust reductions are required at the “Cruise Altitude” to stabilize at the “Start Cruise” Calibrated Airspeed.


Your first priority after an engine failure at high altitude is to keep the airplane flying. To do that you increase power on the operating engine while adding rudder to keep the airplane in coordinated flight. Disengaging the autothrottles and pushing the operating engine power lever full forward takes care of the thrust. You shouldn't need more than rudder trim to take care of the yaw.

The next decision is speed. How slow do you want to let the airplane decelerate before starting down. You obviously want to keep above stall speed, otherwise the flight control computers will take that decsion from you. Stay above the yellow band, of course. How much room do you have? A lot:


Photo: G500 Reference Stall Speed, AFM, §05-01-01, figure 12
Click photo for a larger image

Normal high altitude cruise speeds should normally be at least 0.85M which will give you 229 KCAS at FL450 on an ISA day. So you can get considerably slower. But should you?


Photo: G500 Engine Out Driftdown, AOM, §05-06-00, figure 1, sheet 1
Click photo for a larger image

As you can see from the Operating Manual engine-out driftdown table, the optimal speed for driftdown can be very near or even equal to your cruise speed. So if you want to extract as much forward distance as possible, you might need to start down immediately. But if you are in congested airspace, that might be the wrong decision. With your margin over stall speed, you can be assured that you don't have to fly the driftdown speed immediately. Furthermore, you flight planning is probably based on an immediate descent to driftdown altitude heading to your equal time point alternate. (You need to check with your flight planning service provider to be sure.) See the See Also list below for more about these considerations.

Gulfstream GVII-G500 Aircraft Operating Manual, Revision 4, August 29, 2019

Gulfstream GVII-G500 Airplane Flight Manual, Revision 4, August 29, 2019