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时间:2010-08-10 16:22来源:蓝天飞行翻译 作者:admin
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The Patience Prayer:
Lord, grant me patience. And, I want it NOW!

Nothing makes a person more productive
than the last minute.

Tennis scores go from 0 to 15 to 30 to 40.
Sometimes growing older seems the same.

Many problems don’t exist until a government
agency is created to solve them.

Middle age: When your children tell you
you’re driving too slowly and your parents tell
you you’re driving too fast.
ATP-56(B)
Part 5 Annex H
_____________________________________________________________________
PART 5 – ANNEX H
National Annex - Germany
1. Introduction. Germany operates two tanker types. The PA 200 Tornado in a buddy/ buddy
tanker configuration and the Airbus A310-MRTT.
2. Tanker Aircraft Types
2.1. PA 200 Tornado (buddy/buddy)
a. AAR Equipment. The PA 200 TORNADO can be fitted with a Sargent Fletcher buddybuddy
refuelling pod at the centreline fuselage station. The extended hose has a length of 15.2 m
(50 ft). To open the refuelling valve the hose has to be pushed back in approximately 2 m (6 ft);
however, the forward limit is reached when only 2 marker rings remain visible. During refuelling
operations, hose tension is maintained automatically. The diameter of the drogue is 710 mm.
Recommended closing speed for contact is 3 – 4 KIAS, but is not to exceed 7 KIAS. If contact
speed is in excess of 7 KIAS the possible resulting hose-whip may break off the receivers probe
tip or in an extreme case, damage the tankers refuelling equipment or airframe. Diagrams of the
Tornado refuelling equipment is at Appendix 1.
b. Refuelling Heights and Speeds. Tanker operations are cleared for altitudes from sea
level up to 28,000 ft. Optimum altitude band for refuelling is 5,000 ft to 20,000 ft. The speed
range is from 230 to 320 KIAS/0.75 Mach with an optimum speed of 270 KIAS.
c. Maximum Transferable Fuel. 5,500 kg (12,000 lb) under optimum conditions, but not
more than 3,400 kg (7,500 lb) per contact.
d. Fuel Transfer Rate. Transfer rate is 300 kg/min (650 lbs/min) to 600 kg/min (1,300
lbs/min), depending on receiver aircraft.
e. Regulated Fuel Pressure. Fuel pressure at the drogue is regulated to 50 ± 5 psi.
f. Fuel Types Available for AAR. Primary fuel is F-34. F-35 and F-40 are cleared as
alternative fuels
g. Receiver Types Certified. See Appendix 7.
h. Lighting. A set of three coloured lights each side of the pod’s tail-cone act as indicators to
the receiver for the following:
Amber The hose is extended and the pod system is ready for receiver
engagement and fuel transfer.
Green Fuel is flowing from the pod to the receiver aircraft.
Steady Red Do not make contact. The hose may be winding or trailing.
Flashing Red Break contact immediately.
Three floodlights, located at the pod’s tail, illuminate the underside of the tankers fuselage when
the hose unwinds.
_____________________________________________________________________
Part 5 H-1 Jan 07
ATP-56(B)
Part 5 Annex H
_____________________________________________________________________
i. Mark Facilities. The aircraft is fitted with strobe lighting and is capable of fuel dump.
j. Dimensions. See aircraft drawing at Appendix 2.
k. RV Aids. The aircraft has the following radio, navigation and RV aids:
(1) VHF, UHF, HF and HQII radios.
(2) Tacan, Doppler and LINS/GPS.
(3) Air-to-Air Tacan (DME only).
l. Limitations
(1) Maximum operating time with the hose extended is 45 min. If an interval of 15 min or
more is expected between a series of contacts, the hose will be rewound and the pod shut
down.
(2) Only 3 complete hose extension/retraction cycles per hour are permitted.
(3) Tanker airspeed changes, with hose extended, must be kept within 10 KIAS. For speed
changes greater than 10 KIAS, the hose needs to be rewound and then trailed at the new speed.
Receiver aircraft must stay clear of the hose during this operation.
(4) HF transmissions by the tanker are not permitted when receiver aircraft are within 150 ft
(50 m) tanker.
2.2. Airbus A310 MRTT
a. AAR Equipment. The aircraft is equipped with two under wing mounted AAR pods located
about 3,5 m (12 ft) from the wing tips. The FRL MK 32B-907E pod incorporates an MA 4
coupling and a fixed drogue type. Hose length is 24 m (79 ft) at full trail. To attain fuel flow, the
hose must be pushed in at least 2 m (7 ft), which is marked by the beginning of a white 1,5 m
(5 ft) wide band. Until the end of the second white band fuel will flow, equalling a total optimum
refuelling range of 6 m (20 ft). For reference purpose, four additional white bands of 0,3 m (1ft)
 
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