IFR Quick Review Guide Flashcards

1
Q

When is an instrument rating required? 61.51

A
  • -When acting as PIC under IFR or in weather conditions less than prescribed for VFR
  • When carrying passengers for compensation or hire on cross-country flights in excess of 50 NM or at night
  • For flight in Class A airspace
  • For Special VFR between sunset and sunrise
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2
Q

What is the Airplane-Instrument rating minimum aeronautical experience?

A
  • 50 hours X-country PIC time (of which 10 hr in airplane)
  • 40 hours actual or simulated instrument time (of which 15 hrs with CFII)
  • One X-country flight of 250NM along airways or directed by ATC, perform an instrument approach at each airport, 3 different kinds of approaches using navigation system, with a filed IFR flight plan
  • 3 hours instrument flight training in last calendar months prior to practical test
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3
Q

What is the Simulator-Instrument rating minimum aeronautical experience?

A
  • Approved full flight simulator or FTD, if trained by authorized instructor: Max. 30 hrs if completed under part 142, or 20 if not under part 142
  • FAA approved aviation training device, if trained by an authorized instructor: Max 10hrs of instrument time if basic ATD, Max 20 hrs if instrument time if advanced training ATD
  • No more than 20 hrs of total instrument time can be credited in a full flight simulator, FTD or ATD, expect the 30 hrs exception under part 142.
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4
Q

Recency of experience to act as PIC under IFR or wx conditions less than VFR. 61.57(C)

A

6HITS

  • 6 instruments approaches
  • Holding procedures & tasks
  • Intercepting & tracking courses through the use of navigational electronic systems.
  • The above can be completed in a FFS, ATD or FTD provided the device represents the category of aircraft for the instrument rating privileges to be maintained and the pilot performs the tasks and iterations in simulated instruments conditions
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5
Q

Not current looking back 6 months

A
  • You can still log the required “6 HITS” with a safety pilot (under simulated conditions), examiner or instructor.
  • Safety pilot requirements: at least a private pilot with appropriate category and class, have adequate vision forward and to each side of the aircraft, aircraft must have a dual control system.
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6
Q

Not current looking back 12 months. 61.57(d)

A
  • Instrument proficiency check (IPC) by a CFII, examiner, or other approved person is required. Some IPC tasks, but not all, can be conducted in an FTD or ATD.
  • To carry passengers as PIC: 3 takeoffs & landings in category, class and type in the las 90 days (at periods between 1hr after sunset and 1hr before sunrise must be to a full stop)
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7
Q

To act as PIC in the last 24 months

A

Flight review

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8
Q

What information must be recorded to meet recent instrument experience requirements?

A
  • Location & type of each instrument approach accomplished
  • The name of the safety pilot, if required.
  • If using a flight simulator, FTD or ATD: and authorized instructor is present to observe and signs the person’s logbook to verify time and content of the session.
  • for IFR recency requirements: log training device, time and content.
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9
Q

Personal documents required for flight

A
  • Pilot certificate
  • Medical certificate
  • Authorized photo ID (passport, driver’s license, etc)
  • Restricted radiotelephone operator permit (for flights outside the US)
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10
Q

AIRCRAFT DOCUMENTS REQUIRED FOR

FLIGHT

A

A - Airworthiness certificate
R - Registration certificate
R - Radio station license (for flights outside the US)
O - Operating limitations & information (in AFM)
W - Weight & Balance data (aircraft specific)
(§21.5, §91.103, §91.9, §91.203, ICAO Article 29)

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11
Q

AIRCRAFT MAINTENANCE INSPECTIONS

REQUIRED FOR IFR

A

■ A - Airworthiness Directive (AD) required inspections.
(§39)
■ V - VOR check every 30 days. (For IFR; §91.171)
■ I - Inspections: (§91.409)
▷ Annual inspection - 12 Cal. Months (all aircraft).
▷ 100-hour (time-in-service) inspection required if:
□ Carrying a person for hire (other than crew
member), or
□ Flight instructing for hire in an aircraft provided by
the person giving the instruction.
□ “For hire” refers to the person , not the aircraft.
◦ Flight school providing airplane + instructor for hire:
100-hours required
◦ Student-owned aircraft: 100-hours not required.
◦ Rental (no pilot or instructor): 100-hr not required.
□ The 100-hr inspection may be exceeded by up to 10
hours if aircraft is enroute to a place where it can be
done. This additional time must be included in
computing the next 100-hours inspection.
□ An annual inspection can substitute for the 100-hour if
done within 100 hours of time-in-service.
▷ A progressive inspection schedule, if specifically
approved by the FAA, may replace the annual and 100
hour inspections.
■ A - Altimeter, automatic altitude reporting (used by
transponder) & static system every 24 calendar months.
(For IFR in controlled airspace; §91.411)
■ T - Transponder every 24 calendar months. (§91.413)
■ E - ELT (§91.207)
▷ inspected every 12 calendar months.
▷ Battery must be replaced after more than 1 hour of
cumulative transmitter use or if 50% of its useful life
has expired (or, for rechargeable batteries, 50% of the
useful life of charge has expired).
■ S - Supplemental Type Certificate (STC) required
inspections.

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12
Q

PREFLIGHT SELF-ASSESSMENT

A

■ I - Illness - Do I have any symptoms?
■ M - Medication - Have I taken prescription or over-thecounter drugs?
■ S - Stress - Am I under psychological pressure, worried
about finances, health or family discord?
■ A - Alcohol - No drinking within 8 hours. (“8 hours bottle to
throttle”). No more than .04% of alcohol in blood.
■ F - Fatigue - Am I tired / adequately rested?
■ E - Emotion - Am I emotionally upset?
(§91.17, AIM 8-1-1)

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13
Q

PREFLIGHT INFO REQUIRED FOR IFR: (§91.103)

A

■ N - NOTAMs.
■ W - Weather reports and forecasts.
■ K - Known traffic delays as advised by ATC.
■ R - Runway length of intended use.
■ A - Alternatives available if flight cannot be completed as
planned.
■ F - Fuel requirements
■ T - Takeoff and landing performance data.

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14
Q

RISK MANAGEMENT & PERSONAL MINIMUMS

A

■ P - Pilot (general health, physical / mental / emotional state,
proficiency, currency)
■ A - Aircraft (airworthiness, equipment, performance)
■ V - EnVironment (weather hazards, terrain, airports /
runways to be used & other conditions)
■ E - External pressure (meetings, people waiting at
destination, etc.)

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15
Q

DECISION MAKING

A

■ D - Detect that a change has occurred.
■ E - Estimate the need to counter the change.
■ C - Choose a desirable outcome.
■ I - Identify solutions.
■ D - Do the necessary actions.
■ E - Evaluate the effects of the actions

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16
Q

PASSENGER BRIEFING

A

■ S
▷ Seat belts fastened for taxi, takeoff, landing.
▷ Shoulder harness fastened for takeoff, landing.
▷ Seat position adjusted and locked in place
■ A
▷ Air vents location and operation
▷ All environmental controls (discussed)
▷ Action in case of any passenger discomfort
■ F
▷ Fire extinguisher (location and operation)
■ E
▷ Exit doors (how to secure; how to open)
▷ Emergency evacuation plan
▷ Emergency/survival kit (location and contents)
■ T
▷ Traffic (scanning, spotting, notifying pilot)
▷ Talking, sterile flight deck expectations
■ Y
▷ Your questions? Speak up!

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17
Q

TAXI BRIEFING

A

■ A - Assigned / planned runway.
■ R - Route.
■ C - Crossings and hold short instructions.
■ H - Hot spots & Hazards s (e.g., NOTAMs, closed taxiways/
runways, surface condition).

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18
Q

TAKEOFF BRIEFING

A

D - Departure review (e.g. takeoff type, initial heading, first fix &
course, clearance readout).
E - Establish Expectations (e.g., flying pilot, PIC, positive
transfer of controls).
P - Plan / special considerations (e.g., weather, visibility, terrain,
unfamiliar field, inoperative equipment / MELs).
A - Alternate (takeoff alternate, if needed, or return plan)
R - Runway conditions and length.
T - Trouble / Tactics (e.g., rejected takeoff, engine failure).
S - Speak up! Questions / concerns?

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19
Q

IFR FLIGHT PLAN REQUIREMENTS

A

■ Requirement: no person may operate an aircraft in controlled
airspace under IFR unless that person has:
▷ Filed an IFR flight plan; and
▷ Received an appropriate ATC clearance.
■ It is legal to fly IFR in uncontrolled airspace (class G)
without a flight plan or clearance. However, once airborne,
you must remain in uncontrolled airspace until you file a
flight plan and get an ATC clearance to enter the controlled
airspace.
§91.173

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20
Q

How to file an IFR flight plan?

A

▷ FSS
□ by phone (1-800-WX-BRIEF)
■ over the radio (GCO/RCO frequencies)
□ In person.
▷ Online
□ www.1800wxbrief.com (Leido)
□ www.fltplan.com (Garmin)
▷ EFB (e.g., Foreflight)
▷ With ATC (over radio, or phone if no other mean available)
■ File at least 30 minutes prior to estimated departure. Nonscheduled flights above FL230 should be filed at least 4
hours before est. departure time. (AIM 5-1-8)

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21
Q

Flight plan cancelation (AIM 5-1-15)

A

▷ Towered airports - automatically cancelled by ATC upon
landing.
▷ Non-towered airports - Pilot must contact ATC / FCC to
cancel (by radio or phone)
▷ Can cancel anytime in flight if out of IMC and out of
class A airspace.

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22
Q

IFR MINIMUM FUEL REQUIREMENTS §91.167

A
  • Fuel to fly & land to destination airport
  • Thereafter, fuel to fly & land to most distant alternate
  • Thereafter, fuel to fly 45 min at normal cruise speed in still air.
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23
Q

NEED A DESTINATION ALTERNATE?

A

A destination alternate is always required, unless:
■ An instrument approach is published and
available for the destination, AND,
■ For at least 1 hour before to 1 hour after ETA:
▷ Ceiling will be at least 2000’ above airport
elevation; and
▷ Visibility will be at least 3 SM.
§91.169

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24
Q

MIN WX CONDITIONS REQUIRED AT AN AIRPORT

TO LIST IT AS AN ALTERNATE

A

The alternate airport minima published in the
procedure charts, or, if none:
■ Precision approach:
600 ft ceiling and 2 SM visibility.
■ Non-precision approach:
800 ft ceiling and 2 SM visibility.
■ No instrument approach available at the
alternate:
Ceiling & visibility must allow descent from MEA,
approach and landing under VFR.
§91.169

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25
Q

FILING AN ALTERNATE - GPS CONSIDERATIONS

A

■ Equipped with a non-WAAS GPS? You can flight
plan based on GPS approaches at either the
destination or the alternate, but not at both.
■ WAAS Without baro-VNAV? May base the flight
plan on use of LNAV approaches at both the
destination and alternate.
■ WAAS with baro-VNAV? May base the flight plan
on use of LNAV/VNAV or RNP 0.3 at both the
destination and the alternate.
AIM 1-1-17b.5, 1-1-18c.9, 1-2-3d

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26
Q

IFR CRUISING ALTITUDES §91.179

A

Uncontrolled airspace –
Based on magnetic course:
Below FL290
0º-179º ODD thousands (below 18,000’)
or Flight Levels (at or above FL180)
180º-359º EVEN thousands (below 18,000’) or Flight
Levels (at or above FL180)
Above FL290 (in non-RVSM)
0º-179º Flight Levels at 4,000’ increments starting at
FL290 (e.g., FL 290, 330, 370)
180º-359º Flight Levels at 4,000’ increments starting at
FL310 (e.g., FL 310, 350, 390)
Above FL290-FL410 (in RVSM)
0º-179º Odd Flight Levels at 2,000’ intervals starting at
FL290 (e.g., FL 290, 310, 330)
180º-359º Even Flight Levels at 2,000’ intervals starting
at FL300 (e.g., FL 300, 320, 340)

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27
Q

IFR TAKEOFF MINIMUMS (§91.175)

A

No T/O minimums mandated for part 91 operations.
Part 121, 125, 129, 135:
■ Prescribed T/O minimums for the runway, or, if none:
■ 1-2 engines airplanes: 1 SM visibility
■ More than 2 engines: ½ SM visibility

28
Q
DEPARTURE PROCEDURES (DP)
AIM 5-2-9
A

■ Ensures obstacle clearance, provided:
▷ the airplane crossed the departure end of the
runway at least 35 ft AGL,
▷ reaches 400 ft AGL before turning, and
▷ climbs at least 200 Feet per NM (FPNM), or as
published otherwise on the chart.
□ FPNM to feet-per-minute conversion:
fpm = FPNM * Groundspeed / 60
■ Pilots are encouraged to file a DP at night, during
marginal VMC or IMC.

29
Q

Two types of DP

A

▷ Obstacle Departure Procedure (ODP)
□ Provides only obstacle clearance.
□ Graphic ODPs will have “(OBSTACLE)”
printed in the chart title.
□ Printed either textually or graphically.
▷ Standard Instrument Departure (SID)
□ In addition to obstacle clearance it reduces
pilot and controller workload by simplifying
ATC clearances and minimizing radio
communications.
□ Some SIDs may depict special radio failure
procedures.
□ Always printed graphically.

30
Q

DP are also categorized by equipment required:

A

▷ Non-RNAV DP - for use by aircraft equipped with
ground-based navigation (i.e., VOR, DME, NDB).
▷ RNAV DP - for aircraft equipped with RNAV
equipment (e.g., GPS, VOR/DME, DME/DME).
Require at least RNAV 1 performance. Identified
with the word “RNAV” in the title.
▷ RADAR DP - ATC radar vectors to an ATS route,
NAVAID, or fix are used after departure. RADAR
DPs are annotated “RADAR REQUIRED.”
■ You are not required to accept a DP. To avoid
getting one, state “NO SIDs” in remarks section of
flight plan.
■ Transition routes connect the end of the basic SID
procedure to the en-route structure.

31
Q

IFR DEPARTURE CLEARANCE

A

■ C - Clearance limit.
■ R - Route.
■ A - Altitude.
■ F - Frequency (for departure).
■ T - Transponder code.
Clearance void time – The time at which your
clearance is void and after which you may not takeoff.
You must notify ATC within 30 min after the void time if
you did not depart.
“Hold for release” – You may not takeoff until being
released for IFR departure.
Release time – The earliest time the aircraft may
depart under IFR.
Expect Departure Clearance Time (EDCT) – A
runway release time given under traffic management
programs in busy airports. Aircraft are expected to
depart no earlier and no later than 5 minutes from the
EDCT.
Abbreviated departure clearance – “Cleared (…) as
filed (…)”
(AIM 5-2-6)

32
Q

STANDARD TERMINAL ARRIVAL (STAR)

A

■ Serves as a transition between the en route
structure and a point from which an approach to
landing can be made.
■ Transition routes connect en route fixes to the
basic STAR procedure.
■ Usually named according to the fix at which the
basic procedure begins.
■ As with a SID, you can state “NO STARs” in the
remarks section of the flight plan, to avoid getting a
clearance containing a STAR.
■ RNAV STARs require RNAV 1 performance.

33
Q

MIN IFR ALTITUDES (§91.177)

A

■ Except for takeoff or landing, or otherwise authorized
by the FAA, no person may operate an aircraft under
IFR below -
▷ Minimum altitudes prescribed for the flown
segment, or if none:
▷ Mountainous areas: 2,000 ft above the highest
obstacle within a horizontal distance of 4 NM
from the course.
▷ Non-mountainous areas: 1,000 ft above the
highest obstacle within 4 NM from the course

34
Q

DA / H

A

Decision Altitude / Height: the Altitude (MSL) / Height (above runway threshold), on an instrument approach procedure
at which the pilot must decide whether to continue the approach or go around.

35
Q

MAA

A

Maximum Authorized Altitude. Annotated “MAA-17000” (17,000ft as an example) on IFR charts

36
Q

MCA

A

Minimum Crossing Altitude

37
Q

MDA / H

A

Minimum Decent Altitude / Height: The lowest Altitude (MSL) / Height (above runway threshold) to which descent is
authorized on a non-precision approach until the pilot sees the visual references required for landing.

38
Q

MEA

A

Minimum En route Altitude: The lowest published altitude between radio fixes which assures acceptable navigational
signal coverage and meets obstacle clearance requirements. An MEA gap establishes an area of loss in navigational coverage
and annotated “MEA GAP” on IFR charts.

39
Q

MOCA

A
  • Minimum Obstruction Clearance Altitude: Provides obstacle clearance and navigation coverage only up to 22 NM of
    the VOR.
    ▷ If both an MEA and a MOCA are prescribed for a particular route segment, a person may operate an aircraft lower than
    the MEA down to, but not below the MOCA, provided the applicable navigation signals are available. For aircraft
    using VOR for navigation, this applies only when the aircraft is within 22 NM of the VOR. (§91.177)
40
Q

MORA

A

Minimum Off Route Altitude (Jeppesen):
▷ Route MORA provides obstruction clearance within 10NM to either side of airway centerlines and within a 10NM radius at
the ends of airways.
▷ Grid MORA provide obstruction clearance within a latitude / longitude grid block

41
Q

MRA

A

Minimum Reception Altitude

42
Q

MTA

A

Minimum Turning Altitude: Provides vertical and lateral obstacle clearance in turns over certain fixes. Annotated with the MCA X icon and a note describing the restriction.

43
Q

MVA

A

Minimum Vectoring Altitude: The lowest altitude at which an IFR aircraft will be vectored by a radar controller, except as
otherwise authorized for radar approaches, departures, and missed approaches. MVAs may be lower than the minimum
altitudes depicted on aeronautical charts, such as MEAs or MOCAs.

44
Q

OROCA

A

Off Route Obstruction Clearance Altitude: Provides obstruction clearance with a 1,000 ft buffer in non-mountainous terrain areas and 2,000 ft in mountainous areas. OROCA may not provide navigation or communication signal coverage.
*Designated mountainous areas are defined in 14 CFR part 95 by lat / long coordinates.

45
Q

GYROSCOPIC INSTRUMENTS

Two principles of a gyroscope

A

Rigidity in space and precession.

46
Q

GYROSCOPIC INSTRUMENTS

Attitude indicator

A

– operates on the principle of rigidity in space. Shows bank and pitch information. Older AIs may have a
tumble limit. Should show correct attitude within 5 minutes of starting the engine. Normally vacuum-driven in GA aircraft, may be electrical in others. May have small acceleration/deceleration errors (accelerate-slight pitch up, decelerate- pitch down) and roll-out errors (following a 180 turn shows a slight turn to the opposite direction).

47
Q

GYROSCOPIC INSTRUMENTS

Heading indicator

A

operates on the principle of rigidity in space. It only reflects changes in heading, but cannot measure the
heading directly. You have to calibrate it with a magnetic compass in order for it to indicate correctly. HIs may be slaved to a magnetic heading source, such as a flux gate, and sync automatically to the present heading. Normally powered by the vacuum system in on GA aircraft.

48
Q

GYROSCOPIC INSTRUMENTS

Turn indicators

A

operates on the principle of precession.
▷ Turn coordinators show rate-of-turn and rate of roll.
▷ Turn-and-slip indicators show rate-of-turn only.

49
Q

PITOT-STATIC INSTRUMENTS

Altimeter

A

■ An aneroid barometer that shows the height above a given pressure level, based on standard pressure lapse rate of 1000’ per inch of mercury.
■ A stack of sealed aneroid wafers expand and contract with changes in atmospheric pressure received from the static port.
■ A mechanical linkage between the aneroid and the display translates the sensed pressure to an altitude indication.
■ An altimeter setting knob (on a “sensitive altimeter”, which are most aircraft altimeters) allows the pilot to adjust the current pressure to the current altimeter setting published locally (available from ATIS, METAR or ATC).
■ The pressure setting is displayed in the “Kollsman Window” in mb and/or inches of mercury (Hg)
■ In the US, when operating below 18,000’ MSL regularly set the altimeter to a station within 100 NM. Above 18,000’ MSL,
the altimeter should be set to the standard sea level pressure of 29.92” Hg, and operate in Flight Levels (FL).
■ “High to Low - Watch out below!”. Use caution when flying from high pressure to low pressure areas. If altimeter setting is not updated, altitude will indicate higher, causing the pilot to fly lower than desired. Flying from hot to cold areas results in the same error.

50
Q

TYPES OF ALTITUDES

A

■ Indicated altitude – Uncorrected altitude indicated on the dial when set to local pressure setting (QNH).
■ Pressure altitude – Altitude above the standard 29.92. Hg plane. (QNE). Used when flying above the transition altitude
(18,000’ in the US)
■ Density altitude – Pressure alt. corrected for nonstandard temperature. Used for performance calculations.
■ True altitude – Actual altitude above Mean Sea Level (MSL).
■ Absolute altitude – Height above airport elevation (QFE).

51
Q

PITOT-STATIC INSTRUMENTS

VERTICAL SPEED INDICATOR (VSI)

A

■ Indicates rate-of-climb in fpm (accurate after a 6-9 sec. lag), and rate trend (immediately with rate change).
■ A diaphragm inside the instrument is connected directly to the static source.
■ The area outside the diaphragm also receives static pressure, but via a calibrated leak (a restricted orifice).
■ This configuration essentially responds to static pressure change over time.
■ As the diaphragm expands or contracts, a mechanical linkage moves the pointer needle to display the current rate of climb to
the pilot.
■ Instantaneous VSI (IVSI) solves the lag issue with the addition of vertical accelerometers.

52
Q

PITOT-STATIC INSTRUMENTS

A

■ The airspeed indicator measures the difference between impact (ram) air pressure from the pitot tube and ambient pressure from the static port. The result pressure is called dynamic pressure and corresponds to airspeed.
▷ Dynamic Pressure (airspeed) = Impact Pressure – Static pressure.
■ A diaphragm in the instrument receives ram pressure from the pitot tube. The area outside the diaphragm is sealed and
connected to the static port. A mechanical linkage converts the expansion and contraction of the diaphragm to airspeed shown on the display dial.

53
Q

TYPES OF SPEEDS

A

■ Indicated airspeed (IAS) – indicated on the airspeed indicator
■ Calibrated airspeed (CAS) – IAS corrected for instrument & position errors.
■ Equivalent airspeed (EAS) – CAS corrected for compressibility error.
■ True airspeed (TAS) – Actual speed through the air. EAS corrected for nonstandard
temperature and pressure
■ Mach number – The ratio of TAS to the local speed of sound.
■ Ground speed – Actual speed over the ground. TAS corrected for wind conditions.

54
Q

STATIC PORT BLOCKAGE

A

■ Airspeed indicator – Indicates correctly only at the blockage altitude.
▷ Higher altitudes → airspeed indicates lower than it should.
▷ Lower altitudes → Indicates higher than it should.
■ Altimeter – will freeze on the altitude where it was blocked.
■ VSI – freezes on zero.
▷ After verifying a blockage in the static port, you should use an alternate static source
or break the VSI window (in which case, expect reverse VSI information).
■ When using the alternate static source (a lower static pressure is measured):
▷ Airspeed indicator – indicate a faster speed than it should.
▷ Altimeter – indicate higher than it should.
▷ VSI – momentarily show a climb.

55
Q

PITOT TUBE BLOCKAGE

A

The only instrument affected is the airspeed indicator.
■ Ram air inlet clogged and drain hole open? Airspeed drops to zero.
■ Both air inlet and drain hole are clogged? The airspeed indicator will act as an altimeter, and will no longer be reliable.
■ When suspecting a pitot blockage, consider the use of pitot heat to melt ice that may have formed in or on the pitot tube.

56
Q

MAGNETIC COMPASS ERRORS & LIMITATIONS

A
■ D- Deviation
■ V- Variation
■ M- Magnetic dip
■ O- Oscillation
■ N- North/south turn errors -
Northern hemisphere: UNOS Undershoot North/ Overshoot South
■ A- Acceleration errors -
Northern hemisphere: ANDS Accelerate North/ Decelerate South
57
Q

ELECTRONIC FLIGHT INSTRUMENTS

Attitude Heading Reference Systems (AHRS)

A

Provides more accurate and reliable attitude and heading data than traditional separate gyro systems. The first AHRS units were very expensive and relied on laser gyros and flux valves. Today they are based on solid state technologies (no moving parts) and are cheaper, smaller and easier to maintain.

58
Q

ELECTRONIC FLIGHT INSTRUMENTS

Air Data Computers (ADC)

A

replaces the mechanical pitot-static instruments. The ADC receives inputs from the pitot, static and outside temperature ports and computes airspeed, true airspeed, vertical speed and altitude.

59
Q

ELECTRONIC FLIGHT INSTRUMENTS

Flight director

A

computes and displays command bars over the attitude indicator to assist the pilot in flying selected heading,
course or vertical speed

60
Q

ELECTRONIC FLIGHT INSTRUMENTS

Flight Management System (FMS)

A

Receives inputs from various sensors and provides guidance to the autopilot and flight director throughout the flight. The FMS also automatically monitors and selects the most appropriate navigation source for accurate positioning. (GPS, VOR/DME, INS etc.)

61
Q

ELECTRONIC FLIGHT INSTRUMENTS

Electronic Flight Instrument Systems (EFIS)

A

AKA “Glass cockpit”.

62
Q

ELECTRONIC FLIGHT INSTRUMENTS

Primary Flight Displays (PFD)

A

– Displays flight data such as attitude, altitude, airspeed, VSI and heading as well as rate tapes.

63
Q

ELECTRONIC FLIGHT INSTRUMENTS

Multi-Function Displays (MFD)

A

Displays a variety of information such as moving maps, aircraft system status, weather and traffic. It may also be used as a backup for other displays, such as the PFD or EICAS.

64
Q

MINIMUM EQUIPMENT REQUIRED FOR FLIGHT (§91.205)

For VFR day

A

A - Altimeter
T - Tachometer for each engine.
O - Oil temperature indicator for each engine.
M - Manifold pressure gauge for each altitude engine.
A - Airspeed indicator.
T - Temperature gauge for each liquid cooled engine.
O - Oil pressure gauge for each engine.
F - Fuel quantity gauge for each tank.
L - Landing gear position lights (if retractable gear).
A - Anticollision lights (for aircraft certified after March
11, 1996).
M - Magnetic direction indicator (magnetic compass).
E - ELT, if required by §91.207.
S - Safety belt / shoulder harness.

65
Q

MINIMUM EQUIPMENT REQUIRED FOR FLIGHT (§91.205)

For VFR night

A
All VFR day equipment + FLAPS
F - Fuses (spare set).
L - Landing light (if for hire) .
A - Anti-collision lights.
P - Position lights (navigation lights).
S - Source of electrical power (i.e., battery).
66
Q

MINIMUM EQUIPMENT REQUIRED FOR FLIGHT (§91.205)

A

For IFR day: all VFR day equipment + GRABCARD
For IFR night: all VFR day + VFR night + GRABCARD
G - Generator / alternator.
R - Radios. Two-way radio communication & navigational equipment suitable for the route to be flown.
A - Altimeter (sensitive, adjustable for barometric pressure)
B - Ball (slip-skid indicator).
C - Clock. Shows hours, minutes and seconds with sweep-second pointer or digital representation. Installed as part of aircraft equipment.
A - Attitude indicator.
R - Rate-of-turn indicator.
D - Directional gyro (heading indicator).