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be assignedin subareasN. o interpolationi s allowed.
1. Unqualified - 0.0
2. Conditionally Qualified - 2.0
3. Qualified - 4.0.
To determine the numerical grade for each area and
the overall grade for the flight, add all the points assignedt
o the subareasa ndd ivide this sum by the number
ofs&areasgraded.Theadjectivegradeshallthenbe
determined on the basis of the following scale.
1. O.Oto2.19-Unqualified
2.2.2 to 2.99 -Conditionally Qualified.
3. 3.0 to 4.0 - Qualified.
Example (add subarea numerical equivalents):
4+2+4+2+4 16
5
= r = 3.20 or Qualified
39.8.2 Flnal Grade Determination. The final
NATOPSevaluationgmdeshallbethesameasthegrade
assigned to the flight evaluation. An evaluee who receives
an Unqualified on any ground examination or the
flight ~aluati~shallbeplaced~~Unq~li~~s~~
until a grade of Conditionally Qualified or Qualified is
achieved on a reevaluation.
39.9 APPLICABLE PUBLICATIONS
The NATOPS flight manual contains the standard
operations criteria for F-14D aircraft. Publications regarding
environmental procedures peculiar to shorebased
and shipboard operations and tactical missions are
listed below:
1. F-14D tactical manuals
2. NWPS
3. NATOPS Air Refueling Manual
4. Air TratFo Control NATOPS Msnual
5. LocalAirOperationsManual
6. Carrier Air Operations Manual.
39.10 NATOP!5EVALUAT0NQUEgTiON BANK
The following bank of questions is intended to assist
theunitNATOPS instructor-evaluatorin thepreparation
of ground e xaminations and to provide an abbreviated
study guide. The questions from the bank may be combined
with locally originatedq uestionsin tbe preparation
of ground examinations. The closed-book examination
will consist of not less than 25 questions nor more than
75 questions. The time limit for the closed-book examination
is 1 hour and 30 minutes. The requirements for
the open-book examination are the same as those for the
closed-book examination, except there is no time lit.
ORIGINAL 39-4
NAVAIR 01.F14AAD-1
NATOPS EVALUATION QUESTION BANK
1. Thea imraftw eighsa ppmximately includingtr appedti u& oi&B unP, iloke ndR IO.
2. Theaircraftis inlongthandhasawingspanof at2ood in oversweep.
3. TheL INLET andR LNLETc autionli ghtsi ndicate
4. Duringn ormals ystemo perationt,h e statuso f AICSr ampc ontroli s as follows:
SPEED RampH ydraulicP ower
Mc0.35 ON/OFF Restrainebdy
M 0.35 to 0.5 ON/OFF commanded
M>O.S ON/OFF Pmgrammeads a timtion of
5. An AICSf ailuret hat causeisll uminationo f anI NLET and/orR AMPc autionli ghtr esultsin the following:
SpeedR ange RampR esultant
M > 0.9
6. Duringt he AICSp ortiono f OBC,s imulatedv ariantf light conditionsc yclet he through
theirf ull rangeo f operationin about- secondsT. hise xercisetsh e
and ensures
7. Operationo f theL andR AICS is completelyin dependent
a. True
b. False
8. AICSa nti-iceis availableb etween Macha nd Mach.
9. With theg earh andled owna ndo neo r momr ampsn ot in the stowp ositiont,h er ampl ightw ill be illuminated.
a. True
b. False
10. The installedth rust of the Fl lo-GE-400e ngineis
MAXAA.
poundsa t MRT and poundsa t
11. In SEC mode,b oth main enginef uel flow and compressoVr SVsa m scheduled
, andf an speedis liited by the
12. A 3percenti ncreasein windmillr pm canb e achievedby selecting
by the
13. Nonemergencsye lectiono f the SECm odes houldb ep erformedin
I
39-5 ORIGINAL
NAVAIR 01.F14AAD-1
14. The augmenter fan temperatam control system regulates five parameters of the engine to provide stall-free
operation for any rate of throttle movement thmughout the flight envelope. These parameters are:
a.
d.
e.
15. The engine electrical control subsystemi s poweredb y an engine gearbox-mounted( ac or dc) alternatort hat
contains separatew indings, which ale:
a.
C.
d
16. What are the two power sources for fan speed limiting7
a.
b.
17. The backup ignition is powered by the aircraft
18. Autorelight logic is provided by the
19. What are the throttle interlocks at the military power detent?
bus.
a.
b.
C.
20. Autothmttle may be preflight ground t&cd on deck either in
Indications that a malfonction exists in the autothrottle system are
21. Lit oil pressure readings
a. MRT psi
b. Mium at IDLE psi
or
or
ORIGINAL 39-6
NAVAIR 0%FWAADI
22. An engines tall with no overtemperaturew ill illuminate the appropriateS TALL WARNING light in both PRl
and SEC mode.
a. True
　
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