CAL Stage Maneuvers

Question 1

Minimum LZ size for a single MV-22

Answer 1

170 x 170 feet

Question 2

During CAL takeoff maintain a departure path to clear the highest obstacle by a minimum of

Answer 2

25ft

Question 3

Recommended hover page setup for CALs

Answer 3

AUTO 35CHARTRNG 0.25ZOOM 2.0INBD MFD

Question 4

When should you initiate crosswind turn after takeoff

Answer 4

200ft AGL

Question 5

How should slope takeoffs be accomplished

Answer 5

The nacelle setting should put the fuselage parallel to the slope.For upslope, nacelles should be forward of vertical For downslope, nacelles should be aft of vertical

Question 6

How should cross slope takeoffs be accomplished

Answer 6

Cyclic input should be into the slope so that downslope gear comes off the deck first

Question 7

80 Jump Takeoff

Answer 7

1. Apply brakes2. Set nacelles to 80 degrees 3. Set trim to 1” aft4. Add full power in 2-3 seconds5. 75 degree nacelle and normal takeoff once clear of obstacles

Question 8

Where should intended point of landing be

Answer 8

Forward third of the LZ

Question 9

CONV Mode CAL Pattern

Answer 9

1. Extend 0.5 nm upwind and execute the crosswind turn using 20 degree AOB turn2. Fly downwind at 300ft AGL, 80 KCAS3. Extend 20 degrees past the abeam position, then turn to arrive at the 90 at 300ft AGL, 80 KCAS4. At 90 adjust the nacelles to 85 degrees to decelerate5. At the 45 nacelles should be 88-92 degrees6. Roll out on final at 150ft, 50 KGS, 0.3 nm straightaway 7. Execute a no hover landing

Question 10

PNF Callouts during CONV Pattern

Answer 10

Excessive ground speed after glideslope interceptGreater than 93 degrees nacelle below 25ft AGLExcessive descent rateExcessive lateral drift approaching touchdown

Question 11

Deceleration point for tactical approaches

Answer 11

3 miles at 220 KGS, Add or subtract 0.1 nm for every 10 knots above or below 220 KGS

Question 12

When is a straight in tactical approach used

Answer 12

When the ingress heading from the IP to the LZ is within +/- 45 degrees of the final approach course

Question 13

Straight in Tactical Approach Procedures

Answer 13

1. Intercept the final approach course at or beyond 5 nm, at 220 KGS, 300ft AGL2. At 3 nm: Reduce power to 20% Qm, Autobeep at 170 KCAS, and initiate conversion and descent to 200ft AGL 3. At 1.5 nm should be at 150 KGS and continue to slow at 10 KGS per 0.1 nm, to arrive at 1 nm at 100 KGS.4. At 0.5 nm: 200ft AGL, 70 KGS, 80-85 nacelle5. Descend to intercept glideslope at 150ft AGL, 50 KGS, and 0.3 nm straightaway

Question 14

PNF FDP Duties on downwind During straight in tactical training pattern

Answer 14

Turn on Altitude Capture, Speed Capture, and set the inbound course

Question 15

PNF FDP duties at 3 nm Qm Straight in Tactical Approach

Answer 15

Speed Command - OFF

Question 16

PNF FDP duties at 170 KCAS on Straight in Tactical Approach

Answer 16

Altitude command - OFF

Question 17

PNF duties prior to intercepting the inbound course at or beyond 5 nm During Straight in Tactical Approach

Answer 17

Set HOLD for: HDG, ALT, and SPEED, and verify that either DIRECT or FPLN ARM is on MFD accunciators

Question 18

When is the 180 degree offset tactical approach used

Answer 18

When the ingress heading from the IP to the Conversion Point is between 135-225 degrees of the final approach course for the LZ

Question 19

Where is the conversion point for a 180 degree offset approach

Answer 19

1.5 nm slant range from the LZ at a 1 nm offset

Question 20

180 degree offset approach

Answer 20

1. Approach the conversion point at 300ft AGL, 220 KCAS2. At the Conversion point reduce power to 20% Qm3. Autobeep at 170 KCAS4. Abeam the LZ execute a converting turn 5. Execute gear down and Landing Checks during the turn6. Roll out on 0.5 nm final at 70 KGS, 80-85 nacelle

Question 21

When is the 90 degree offset tactical approach used

Answer 21

When the final approach course is 45-135 degrees from the ingress course

Question 22

Where is the Conversion point for a 90 degree offset approach

Answer 22

2 nm slant range from the LZ at a 1 nm offset

Question 23

90 degree offset approach

Answer 23

1. Approach the conversion point at 300ft AGL, 220 KCAS2. At the Conversion point reduce power to 20% Qm3. Autobeep at 170 KCAS, just prior to initiating turn4. Initiate converting turn when waypoint needle is 20-30 degrees above the abeam position 5. Execute gear down and Landing Checks during the turn6. Roll out on 0.5 nm final at 70 KGS, 80-85 nacelle

Question 24

4 critical data points to be scanned on the hover display during RVLs

Answer 24

Rate of descentAirspeedDrift Altitude

Question 25

RVL Procedure

Answer 25

1. Between 0.3-0.2 nm set hover nacelle and descend at 200 fpm2. Descend into obscuration and terminate at 0-5 KGS, 0-3 KGS lateral drift, with 1-3 degrees pitch up 3. Allow the aircraft to settle by reducing power while centering the controls

Question 26

Augmented hover couple landing procedures

Answer 26

1. Set hover nacelle at 0.3 DME and use nose to control closure rate 2. Establish visual glideslope and transition to Hover Page as you descend into obscuration.3. Once in a stable hover use trim release to trim out all control pressures4. After pilot reports stable, PNF selects HVR CPLD and reports hover couple armed (PNF must also toggle to POSITION HOLD on Hover Page)5. Reduce TCL while depressing ALT REF button to set rate of descent of 200-300 fpm until on deck 6. Smoothly pull power to idle and apply brakes

Question 27

PNF mandatory call outs for lateral drift

Answer 27

Greater than 3 kts of lateral drift

Question 28

Descent rate PNF mandatory call out

Answer 28

Greater than 800 fpm during approach or 500 fpm during landing

Question 29

Nacelle setting PNF mandatory call out

Answer 29

Nacelles less than 87 or greater than 93 on final

Question 30

Pitch attitude PNF mandatory call out

Answer 30

Pitch attitude +/- 3 degrees from the horizon

Question 31

Wave off criteria for RVL profile

Answer 31

1. Greater than 15 KGS at 50ft2. Greater than 5 KGS or 300 fpm ROD at 20ft3. Lateral drift greater than 3 KGS4. Pitch greater than 3 degrees from the horizon

Question 32

Wave off criteria for Augmented hover coupled landing

Answer 32

1. ROD greater than 300 fpm2. Greater than 3 KGS