曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
units AOA maximum) for the drop. The banner should
be dropped in wings-level flight at a minimum aircraft
altitude of 1,000 feet AGL. The chase aircraft should
ensurea dequatec learancee xistsb etweent heb annera nd
ground obstacles during approach to the drop zone and
provide calls to assist in lineup. Release is normally
called by the tower when the banner is over the center
of the drop zone. Release is accomplished by lowering
the tailhook. In most cases, the banner will hit down
9-5 ORIGINAL
NAVAIR 01.Fl4AAD-1
range of the release point. However, high-wind conditions
may require the tow aircraft to adjust the release
point to avoid downwind travel ofthe banner. Following
banner release, the tailhook should be raised.
9.3.3.5 Shipboard Banner Drop. The tow aircraft
should extend its flaps and reduce airspeed (140 to 160
KIAS, 12 units AOA maximum) for the drop. The banner
should be dropped in a clear area in wings-level
flight at a minimum altitude of 1,000 feet MSL. If a clear
area is not available, the banner should be dropped approximately
1 mn abeam the port side of the carrier.
Release is called by the air officer when the banner is
over the drop zone. Banner release is accomplished by
lowering the tailhook.
When the tailhook is lowered for banner release,
ensure that the balance ball is centered
or slightly right (IeA yaw). If any right yaw
is present, tow cable/tailhook entanglement
is possible.
9.3.3.6 Banner Release Failure. If the arresting
hook fails to extend, the banner cannot be released. In
this case, the following procedure is recommended:
1. In gunnery range (or other cleared area) descend
to low altitude, extend flaps, slow to 140 to 160
KIAS, 12 units AOA maximum and descend to
100 to 200 feet AGL. This will drag banner off on
ground (or water). Have escort pilot confirm that
banner breaks off on ground collision, and determine
length of remaining tow cable.
[ WARNING 1
The escort pilot must remain well clear of the
remaining cable. The last 25 percent of the
remaining cable will flail unpredictably.
2. If 100 feet or greater remaining tow cable length
is confirmed by escort pilot, plan to touch down
1,000 to 1,500 feet long, runway length permitting.
Every effort must be made by the tow pilot
not to drag the remaining tow cable across
lines, fences, or other obstacles because of
property damage that will result.
Note
The long touchdown should be carefully
plannedb ecausel ong-field arrestmentis impossible.
9-6
NAVAIR 01-Fl4AAD-1
9.4 FUEL MANAGEMENT SYSTEM OPERATIONAL CHECK
The following fuel management system operational check can be used by flightcrews to perform a check of the
fuel transfer system, including FUEL FEED switch, WlNG/EXT TRANS switch, sump tank interconnect valve,
foselage motive flow isolation valves, low-level thermistors, and box-beam vent valves. In addition, the procedure
tests for proper functioning of the automatic electrical controls in the fuel feed system. The tinal four procedures
(steps5 through 8) can best be performed in a shore-basede nvironment where minimum fuel on deck requirements
are not as restrictive.
PROCEDURES COMMENTS
Initial conditions:
FWDlR 8 AFT/L - 3,000 pounds (approximately)
Ensure 4,500 pounds on tapes for operation of FEED
switch.
L 8 R FEED - 1,500 to 1,750 pounds (full)
UR WINGS - Empty (0 to 200 pounds)
TOTAL - 6,000 pounds (approximately)
1. WING/EXT TRANS switch -OFF. 1. Switch should not move until automatic interconnect
occurs. Verifies proper automatic electrical operation.
2. FUEL FEED switch - FWDlR
Monitor 500~pound split, AFT/L high.
2. Verifies sump tank interconnect valve open via
manual operation and aft fuselage motive flow valve
shut off.
3. FUEL FEED switch - AFT/L 3.
Monitor 500~pound split, FWDIR high.
Same as step 2 except forward fuselage motive flow
valve shut off.
4. FUELFEEDswitch - NORM
Verify FWD/R high split remains constant.
4. Verifies system returns to isolated mode with no leaks.
5. f.l.l;;;~NG/EXT TRANS switch returns 5. Verifies cell No. 2 or 5 tow-level thermistor’s proper
operation to trigger automatic interconnect
function.
AFT/L - 1,700 f200 pounds. or
FWDlR - 2,100 f200 pounds.
6. Monitor tapes/feeds for system balancing. 6. Verifies sump tank interconnect valve opens via
automatic operation and L/R box-beam vent valves
N&S
open. Verifies proper operation of FWDlAFT motive
systems.
Balancing normally begins 6 tog minutes
after WING/EXT TRANS switch returns to
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F-14D 飞行手册 Flight Manual 2(47)
