COMMERCIAL PILOT 2025-26 NAVIGATION

(REFER TO FIGURE 17.) WHICH ILLUSTRATION INDICATES THAT THE AIRPLANE SHOULD BE TURNED 150 LEFT TO INTERCEPT THE 360 RADIAL AT A 60 ANGLE INBOUND?. 1. 2. 3.

GIVEN: TRUE COURSE 345 TRUE HEADING 355 TRUE AIRSPEED 85 KT GROUND SPEED 95 KT DETERMINE THE WIND DIRECTION AND SPEED. 095 and 19 knots. 113 and 19 knots. 238 and 18 knots.

GIVEN: WIND 175 AT 20 KTS DISTANCE 135 NM TRUE COURSE 075 TRUE AIRSPEED 80 KTS FUEL CONSUMPTION 105 LB/HR DETERMINE THE TIME EN ROUTE AND FUEL CONSUMPTION. 1 hour 28 minutes and 73.2 pounds. 1 hour 38 minutes and 158 pounds. 1 hour 40 minutes and 175 pounds.

HOW SHOULD THE PILOT MAKE A VOR RECEIVER CHECK WHEN THE AIRCRAFT IS LOCATED ON THE DESIGNATE CHECKPOINT ON THE AIRPORT SURFACE?. set the OBS on 180 plus minus 4; de CDI should center with a FROM indication. set the OBS on the designated radial. the CDI must center within plus or minus 4 of the radial with a FROM indication. with the aircraft headed directly toward the VOR and the OBS set to 000, the CDI should center within plus or minus 4 of that radial with a TO indication.

WHEN USING A VOT TO MAKE A VOR RECEIVER CHECK, THE CDI SHOULD BE CENTERED AND THE OBS SHOULD INDICATE THAT THE AIRCRAFT IS ON THE. 090 radial. 180 radial. 360 radial.

GIVEN: PRESSURE ALTITUDE 12,000 FT TRUE AIR TEMPERATURE +50 FROM THE CONDITIONS GIVEN , THE APPROXIMATE DENSITY ALTITUDE IS. 11,900 feet. 14,130 feet. 18,150 feet.

GIVEN: TRUE COURSE 105 TRUE HEADING 085 TRUE AIRSPEED 95 KTS GROUND SPEED 87 KTS DETERMINE THE WIND DIRECTION AND SPEED. 020 and 32 knots. 030 and 38 knots. 200 and 32 knots.

TRUE COURSE MEASUREMENTS ON A SECTIONAL AERONAUTICAL CHART SHOULD BE MAADE AT A MERIDIAN NEAR THE MIDPOINT OF THE COURSE BECAUSE THE. values of isigonic lines chenge from point to point. angles formed by isogonic lines and lines of latitude vary from point to point. angles formed by lines of longitude and the course line vary from point to point.

AN AIRCRAFT 60 MILES FROM VOR STATION HAS A CDI INDICATION OF ONE-FIFTH DEFLECTION, THIS REPRESENTS A COURSE CENTERLINE DEVIATION OF APPROXIMATELY. 6 miles. 2 miles. 1 mile .

(REFER TO FIGURE 17.)WHICH ILLUSTRATION INDICATES THAT THE AIRPLANE WILL INTERCEPT THE 060 RADIAL AT 60 ANGLE INBOUND, IF THE PRESENT HEADING IS MAINTAINED?. 6. 4. 5.

IF FUEL CONSUMPTION IS 14.7 GALLONS PER HOUR AND GROUNDSPEED IS 157 KNOTS, HOW MUCH FUEL IS REQUIRED FOR AN AIRPLANE TO TRAVEL 612 NM. 58 gallons. 60 gallons. 64 gallons.

AN AIRPLANE DEPARTS AN AIRPORT UNDER THE FOLLOWING CONDITIONS: AIRPORTS ELEVATION 1000 FT CRUISE ALTITUDE 9500 FT RATE IF CLIMB 500 FT /MIN AVERAGE TRUE AIRSPEED 135 KTS TRUE COURSE 215 AVERAGE WIND VELOCITY 290 AT 20 KTS VARIATION 3W DEVIATION -2 AVERAGE FUEL SONSUMTION 13 GAL/HOR DETERMINE THE APPROXIMATE TIME, COMPASS HEADING, DISTANCE, AND FUEL CONSUMED DURING THE CLIMB. 14 minutes, 234, 26 NM, 3.9 gallons. 17 minutes, 224, 36 NM, 3.7 gallons. 17 minutes, 242, 31 NM , 3.5 gallons.

WHEN NAVIGATING USING ONLY VOR/DME BASED RNAV, SELECTION OF A VOR NAVAID THAT DOES NOT HAVE DME SERVICE WILL. result in loss of RNAV capability. have no effect on navigation capability. not impact navigation provided enough of the GPS is operating.

IF AN AIRPLANE IS CONSUMING 95 POUNDS OF FUEL PER HOUR AT A CRUISING ALTITUDE OF 6,500 FEET AND GROUNDSPEED IS 173 KNOTS, HOW MUCH FUEL IS REQUIRED TO TRAVEL 450 NM?. 248 pounds. 265 pounds. 284 pounds.

(REFER TO FIGURE 17.) WHICH IS TRUE REGARDING ILLUSTRATION 4, IF THE PRESENT HEADING IS MAINTAINED? THE AIRPLANE WILL. cross the 060 radial at a 15 angle. intercept the 240 radial at a 30 angle. cross the 180 radial at a 75 angle.

WHEN MUST AN OPERACIONAL CHECk ON THE AIRCRAFT VOR EQUIPMENT BE ACCOMPLISHED TO OPERATE UNDER IFR? WITHIN THE PRECEDING. 30 days or 30 hours of flight time. 10 days or 10 hours of flight time. 30 days.

(REFER TO FIGURE 17) WHICH STATEMENT IS TRUE REGARDING ILLUSTRATION 2, IF THE PRESENT HEADING IS MAINTAINED? THE AIRPLANE WILL. cross the 180 radial at 45 angle outbound. intercept the 225 radial at 45 angle. intercept the 360 radial at a 45 angle inbound.

TO TRACK INBOUND ON THE 215 RADIAL OF A VOR STATION, THE RECOMMENDED PROCEDURE IS TO SET THE OBS TO. 215 and make heading corrections toward the CDI needle. 215 and make heading correction away from the CDI needle. 035 and make heading corrections toward the CDI needle.

WHEN CHECKING THE COURSE SENSITIVITY OF A VOR RECEIVER, HOW MANY DEGREES SHOULD THE OBS BE ROTATED TO MOVE THE CDI FROM CENTER TO THE LAST DOT ON EITHER SIDE?. 5 to 10. 10 to 12. 18 to 20.

AVERAGE TRUE AIRSPEED 160 KTS TRUE COURSE 145 AVERAGE WIND VELOCITY 080 AT 15 KTS VARIATION 5 E DEVIATION -3 AVERAGE FUEL CONSUMPTION 14 GAL/HR DETERMINE THE APPROXIMATE TIME, COMPASS HEADING , DISTANCE, AND FUEL CONSUMED DURING THE CLIMB. 14 minutes, 128, 35 NM, 3.3 gallons. 16 minutes, 132, 41 NM, 3.7 gallons. 16 minutes, 128, 32 NM, 3.8 gallons.

AN AIRPLANE DESCENDS TO AN AIRPORT UNDER THE FOLLOWING CONDITIONS: CRUISING ALTITUDE 7,500 FT AIRPORT ELEVATION 1,300 FT DESCENDS TO 800 FT AGL RATE OF DESCEND 300 FT/MIN AVERAGE TRUE AIRSPEED 120 KTS TRUE COURSE 165 AVERAGE WIND VELOCITY 240 AT 20 KTS VARIATION 4 E DEVIATION -2 AVERAGE FUEL CONSUMPTION 9.6 GAL/HR DETREMINE THE APPROXIMATE TIME, COMPASS HEADING, DISTANCE, AND FUEL CONSUMED DURING THE DESCENT. 16 minutes, 168, 30 NM , 2,9 gallons. 18 minutes, 164, 34 NM , 3.2 gallons. 18 minutes, 168, 34 NM , 2.9 gallons.

IF AN AIRPLANE IS CONSUMING 12.5 GALLONS OF FUEL PER HOUR AT A CRUISING ALTITUDE OF 8,500 FEET AND THE GROUNDSPEED IS 145 KNOTS, HOW MUCH FUEL IS REQUIRED TO TRAVEL 435 NM?. 27 gallons. 34 gallons. 38 gallons.

TO TRACK OUTBOUND ON THE 180 RADIAL OF A VOR STATION , THE RECOMMENDED PROCEDURE IS TO SET THE OBS TO. 360 and make heading corrections toward the CDI needle. 180 and make heading corrections away from the CDI needle. 180 and make heading corrections toward the CDI needle.

GIVEN: PRESSURE ALTITUDE 5,000 FT TRUE AIR TEMPERATURE +30C FROM THE CONDITIONS GIVEN, THE APPROXIMATE DENSITY ALTITUDE IS. 7,200 feet. 7,800 feet. 9,000 feet.

WHICH SITUATION WOULD RESULT IN REVERSE SENSING OF A VOR RECEIVER?. flying a heading that is reciprocal to the bearing selected on the OBS. setting the OBS to a bearing that is 90 from the bearing on which the aircraft is located. failing to change the OBS from the selected inbound course to the outbound course after passing the station.

WHAT PROCEDURE COULD A PILOT USE TO NAVIGATE UNDER VFR FROM ONE POINT TO ANOTHER WHEN GROUND REFERENCES ARE NOT VISIBLE?. dead reckoning. pilotage. VFR is not allowed in the circumstances.

GIVEN: DISTANCE OFF COURSE 9 MI DISTANCE FLOW 95 MI DISTANCE TO FLY 125 MI TO CONVERGE AT THE DESTINATION, THE TOTAL CORRECTION ANGLE WOULD BE. 4°. 6°. 10°.

WHICH DATA MUSTE BE RECORDED IN THE AIRCRAFT LOKBOOK OR OTHER RECORD BY A PILOT MAKING A VOR OPERATIONAL CHECK FOR IFR OPERATIONS?. VOR name or identification, place of operational check, amount of bearing error, and date of check. date of check, place of operational check, bearing error ,and signature. VOR name or identification, amount of bearing error , date of check, and signature.

WHEN THE CDI NEEDLE IS CENTERED DURING AN AIRBONE VOR CHECK, THE OMNIBEARING SELECTOR AND THE TO/ FROM INDICATOR SHOULD READ. within 4° of the selected radial. within 6° of the selected radial. 0° to, only if you are due south of the vor.

FOR IFR OPERATIONS OFF ESTABLISHED AIRWAYS, ROUTE OF FLIGHT PORTION OF AN IFR FLIGHT PLAN SHOULD LIST VOR NAVIGATIONAL AIDS WHICH ARE NO MORE THAN. 40 MILES APART. 70 MILES APART. 80 MILES APART.

GIVEN: PRESSURE ALTITUDE 7,000 FT TRUE AIR TEMPERATURE +15°C FROM THE CONDITIONS GIVEN, THE APPROXIMATE DENSITY ALTITUDE IS. 5,000 feet. 8,500 feet. 9,500 feet.

AN AIRPLANE DESCENDS TO AN AIRPORT UNDER THE FOLLOWING CONDITIONS: CRUISING ALTITUDE 10,500 FT AIRPORT ELEVATION 1,700 FT DESCENDS TO 1,000 FT AGL RATE OF DESCENT 600 FT /MIN AVERAGE TRUE AIRSPEED 135 KTS TRUE COURSE 263° AVERAGE WIND VELOCITY 330° AT 30 KTS VARIATION 7° E DEVIATION +3° AVERAGE FUEL CONSUMPTION 11.5 GAL/HR DETREMINE THE APPROXIMATE TIME, COMPASS HEADING, DISTANCE, AND FUEL CONSUMED DURING THE DESCENT. 9 minutes ,274°, 26 nm, 2.8 gallons. 13 minutes, 274°, 28 nm,2.5 gallons. 13 minutes, 271°, 26 nm, 2.5 gallons.

WHAT IS THE MAXIMUM BEARIN ERROR (+ OR-) ALLOWED FOR AN OPERATIONAL VOR EQUIPMENT CHECK WHEN USING AN FAA- APPROVED GROUND TEST SIGNAL?. 4° degrees. 6° degrees. 8° degrees.

GIVEN: PRESSURE ALTITUDE 6,000 FT TRUE AIR TEMPERATURE +30°F FROM THE CONDITIONS GIVEN, THE APPROXIMATE DENSITY ALTITUDE IS. 9,000 feet. 5,500 feet. 5,000 feet.

AS AIR TEMPERATURE INCREASES, DENSITY ALTITUDE WILL. decrease. increase. remain the same.

AN AIRPLANE DESCENDS TO AN AIRPORT UNDER THE FOLLOWING CONDITIONS: CRUISING ALTITUDE 6,500 FT AIRPORT ELEVATION 700FT DESCENDS TO 800 FT /AGL RATE OF DESCEND 500FT/MIN AVERAGE TRUE AIRSPEED 110KTS TRUE COURSE 335° AVERAGE WIND VELOCITY 060° AT 15 KTS VARIATION 3° W DEVIATION +2° AVERAGE FUE CONSUMPTION 8.5 GAL/HR DETERMINE THE APPROXIMATE TIME, COMPASS HEADING, DISTANCE, AND FUEL CONSUMED DURINGTHE DESCENT. 10 minutes,348°, 18 NM , 1.4 gallons. 10 minutes, 355°, 17 NM , 2.4 gallons. 12 minutes, 346°, 18 NM , 1.6 gallons.

IF AN AIRCRAFT IS CONSUMING 9.5 GALLONS OF FUEL PER HOUR AT A CRUISING ALTITUDE OF 6,000 FEET AND THE GROUNDSPEED IS 135 KNOTS, HOW MUCH FUEL IS REQUIRED TO TRAVEL 420 NM?. 27 gallons. 30 gallons. 35 gallons.

(REFER TO FIGURE 17) WHICH ILLUSTRATION INDICATES THAT THE AIRPLANE WILL INTERCEPT THE 060 RADIAL AT A 75° ANGLE OUTBOUND , IF THE PRESENT HEADING IS MAINTAINED?. 4. 5. 6.

IF AN AIRPLANE IS CONSUMING 14.8 GALLONS OF FUEL PER HOUR AT A CRUISING ALTITUDE OF 7,500 FEET AND THE GROUNDSPEED IS 167 KNOTS, HOW MUCH FUEL IS REQUIRED TO TRAVEL 560 NM?. 50 gallons. 53 gallons. 57 gallons.

IF FUEL CONSUMPTION IS 80 POUNDS PER HOUR AND GROUNDSPEED IS 180 KNOTS, HOW MUCH FUEL IS REQUIRED FOR AN AIRPLANE TO TRAVEL 460 NM?. 205 pounds. 212 pounds. 460 pounds.