kpayne on VMOFRWIN702 with $$_JOB

Section 61.68

14 CFR Ch. I (1-1-19 Edition)

(v) Must be accomplished in an aircraft of the same category and class,
and type, as applicable, as the aircraft
in which the practical test is to be conducted or in a flight simulator that - 
(A) Represents an aircraft of the
same category and class, and type, as
applicable, as the aircraft for which the
authorization is sought; and
(B) Is used in accordance with an approved course conducted by a training
center certificated under part 142 of
this chapter.
(4) The flight time acquired in meeting the requirements of paragraph
(c)(2)(ii)(B) of this section may be used
to meet the requirements of paragraph
(c)(2)(ii)(A) of this section.
(d) Practical test procedures. The practical test consists of an oral increment
and a flight increment.
(1) Oral increment. In the oral increment of the practical test an applicant
must demonstrate knowledge of the
following:
(i) Required landing distance;
(ii) Determination and recognition of
the alert height or decision height, as
applicable, including use of a radar altimeter;
(iii) Recognition of and proper reaction to significant failures encountered
prior to and after reaching the alert
height or decision height, as applicable;
(iv) Missed approach procedures and
techniques using computed or fixed attitude guidance displays and expected
height loss as they relate to manual
go-around or automatic go-around, and
initiation altitude, as applicable;
(v) Use and limitations of RVR, including determination of controlling
RVR and required transmissometers;
(vi) Use, availability, or limitations
of visual cues and the altitude at which
they are normally discernible at reduced RVR readings including - 
(A) Unexpected deterioration of conditions to less than minimum RVR
during approach, flare, and rollout;
(B) Demonstration of expected visual
references with weather at minimum
conditions;
(C) The expected sequence of visual
cues during an approach in which visibility is at or above landing minima;
and

(D) Procedures and techniques for
making a transition from instrument
reference flight to visual flight during
a final approach under reduced RVR.
(vii) Effects of vertical and horizontal windshear;
(viii) Characteristics and limitations
of the ILS and runway lighting system;
(ix) Characteristics and limitations
of the flight director system auto approach coupler (including split axis
type if equipped), auto throttle system
(if equipped), and other Category III
equipment;
(x) Assigned duties of the second in
command during Category III operations, unless the aircraft for which
authorization is sought does not require a second in command;
(xi) Recognition of the limits of acceptable aircraft position and flight
path tracking during approach, flare,
and, if applicable, rollout; and
(xii) Recognition of, and reaction to,
airborne or ground system faults or abnormalities, particularly after passing
alert height or decision height, as applicable.
(2) Flight increment. The following requirements apply to the flight increment of the practical test - 
(i) The flight increment may be conducted in an aircraft of the same category and class, and type, as applicable, as the aircraft for which the authorization is sought, or in a flight
simulator that - 
(A) Represents an aircraft of the
same category and class, and type, as
applicable, as the aircraft in which the
authorization is sought; and
(B) Is used in accordance with an approved course conducted by a training
center certificated under part 142 of
this chapter.
(ii) The flight increment must consist of at least two ILS approaches to
100 feet AGL, including one landing and
one missed approach initiated from a
very low altitude that may result in a
touchdown during the go-around maneuver;
(iii) All approaches performed during
the flight increment must be made
with the approved automatic landing
system or an equivalent landing system approved by the Administrator;
(iv) If a multiengine aircraft with the
performance capability to execute a

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