Closed Test Flashcards
A WARNING is
Operating procedures, techniques, etc., that may result in personal injury or loss of life if not carefully followed.
ref: TO 1C-130(h)J-1 pg: iv
a CAUTION is
Operating procedures, techniques, etc., that may result in damage to equipment if not carefully followed.
ref: TO 1C-130(h)j-1 pg: iv
a NOTE is
Operating procedures, techniques, etc., that are considered essential to emphasize.
ref: TO 1C-130(h)j-1 pg: iv
the maximum recommended gross weight for landing is…..and corresponds to a landing rate of sink of ….
142,000 lbs: 540 fpm
ref: TO 1c-130(h)j–1 pg: 1-2
for landings with rates of sink from 300 to 540 fpm, tanks 1 and 4 must have….of fuel or less and a main tank total fuel limit of….
7,323 lbs; 23,000 to 28,000 lbs
ref: TO1c-130(h)j-1 pg 1-3
which of the following distribution requirements define primary fuel management?
A)tanks no. 1 and no4 always contain 500 to 1,000 pounds more fuel per tank than tanks no. 2 and no. 3, except when total usable fuel is less than 6,000 pounds
B) than main tanks are full, except for fuel used for taxi, takeoff, and climb; but not less than 7,060 pounds in tanks no1 and no4 and not less than 6,400 pounds in tanks no2 and no3, when the external and/ or auxiliary tanks contain usable fuel
C) fuel unbalance is within the limits specified by the airspeed limitations and fuel unbalance limits of TO 1c-130(h)j-1
D)ALL OF THE ABOVE
ref: to 1c-130(h)j-1 pg: 1-4
what are the maximum landing gear and landing light extended speeds?
168 kias; 250 kias
ref: TO 1C-130(H)J-1 Pg: 1-7
What is the maximum airspeed for 50% flaps?
183 KIAS
ref: TO 1C-130(H)J-1 Pg: 1-7
Maximum airspeed if encountering severe turbulence is…., and maximum tire speed (knots ground speed) for hte nose wheel is….
181 KIAS; 139 KTS
ref: TO 1C-130(H)J-1 Pg: 1-8 and 1-9
nose wheel turn limits include which of the following?
20 degrees left or right of center mark at taxi speed higher than 5 knots
ref: TO 1C-130(H)J-1 Pg: 1-9
static propeller feathering is limited to ….cycles (feather to reverse and back to feather). feathering is limited to ….commands (fire handle pulled or prop control to feather). upon reaching either of these limits, no further static propeller feathering cycles or feathering commands should be attempted until the engine has been started and run for at least 10 minutes above LSGI.
2; 4
ref: TO 1C-130(H)J-1 Pg: 1-13
if the aircraft is not pointed into the wind +/-45 degrees and the crosswind component is >15 kts but <35 kts:
do not exceed 2,500 HP until airplane speed is greater than 35 knots
ref: TO 1C-130(H)J-1 Pg: 1-13
the apu must be on speed and warmed up a minimum of….prior to selecting OPEN on the APU bleed air valve. (normal procedures)
1 minute
ref: TO 1C-130(H)J-1 Pg: 1-14
