Appendix A Figure B-25a NOTE MU-2B J (-35), K (-25), L (-36), M(-26)
EITHER THIS PROCEDURE, NONPRECISION STRAIGHT-IN APPROACH OR ALTERNATELY PROFILE **OPTIONAL USE OF CONTINUOUS DESCENT FINAL APPROACH (CDFA) B-25 MUST BE DEMONSTRATED. COMPLETE DESCENT AND APPROACH CHECKLISTS A/S 150 KCAS, 140 KCAS (J, L, M, K+) MIN, 130 KCAS (K) MIN. A/S 140 KCAS (130 KCAS MIN).
REVIEW APPROACH PLATE. RADIOS: TUNE & IDENTIFY. (20%-25% TORQUE), DESCEND 500 FPM CHECK FINAL APPROACH FIX CROSSING ALTITUDE. TO PROCEDURE TURN OR OTHER **CALCULATE VDA. APPROACH SEGMENT ALTITUDE LANDING APPROACH SPEEDS Vref FLAPS 5°, (IF INSTALLED) A/S 140 KCAS MIN.
FLAPS 20° (1.3 V$1) J,K, L, M FLAPS 40° (1.5 V§1) (25%-30% TORQUE) 93 96 95 100 93 99 100 100 100 103 103 103 1080 103 106 99 106 106 106 109 103 99 109 109 109 108 112 112 106 103 112 112 111 CAUTION - STEPDOWN FIXES A/S 140 KCAS MIN.
115 115 (25%-30% TORQUE) 109 105 115 114 **DURING ALL APPROACHES, 110 117 USE CDFA THAT MEETS ALL 108 110 ALTITUDE CONSTRAINTS LANDING ASSURED, CHECK GEAR 110 119 DOWN, FLAPS 20° APPROACHING
FIX INBOUND, LANDING CHECKLIST COMPLETE A/S 120 KCAS MIN.
**DERIVED DECISION ALTITUDE (DDA) *CAUTION A/S 120 KCAS MIN, (25%-30% TORQUE), MISSED APPROACH MUST BE WHEN USING CDFA METHOD, MISSED APPROACH: MDA BEGIN CALCULATED DESCENT RATE AT FAF EXECUTED UPON REACHING GO-AROUND, MAX *VDP DDA. DESCENT BELOW MDA DURING MISSED APPROACH NOT AUTHORIZED POWER, PITCH TO 8°. CONTINUE WITH TWO APPROACH PROFILE ENGINE MISSED (APPROX 50% TORQUE) A/S 120 KCAS MIN.
FINAL CHECK.
*VDP CHECK FINAL LANDING CONFIGURATION
VISUAL DESCENT POINT AN APPROACH TOUCHDOWN: POWER LEVERS RETARD TO FLIGHT IDLE STOP,
CONSTRUCTED WITH A VDP THEN POWER LEVERS RETARD TO START (GROUND IDLE), CHECK SHOULD HAVE THE AIRCRAFT BOTH PROPS BETA. REVERSE AND BRAKES AS REQUIRED.
CROSS THE MDA AT OR BEYOND THE VDP.
A-91
Appendix A Figure B-26 NOTE MU-2B J (-35), K (-25), L (-36), M(-26)
EITHER THIS ONE ENGINE INOPERATIVE STRAIGHT-IN NONPRECISION APPROACH
PROCEDURE, OR ALTERNATELY PROFILE A/S 140 KCAS (130 KCAS MIN.) (50%-60% TORQUE), B-26b MUST BE FLAPS 5° (IF INSTALLED). DESCEND 500 FPM TO DEMONSTRATED. PROCEDURE TURN ALTITUDE OR OTHER
APPROACH SEGMENT ALTITUDE FLAPS 5°, (IFINSTALLED) A/S 140 KCAS COMPLETE DESCENT AND APPROACH (130 KCAS MIN) CHECKLISTS. A/S 150 KCAS 140 KCAS (J, L), MIN, (50%-60% TORQUE) 135KCAS (K, (M) MIN. REVIEW APPROACH PLATE.
RADIOS: TUNE & IDENTIFY. CHECK FINAL APPROACH FIX ALTITUDE.
A/S 140 KCAS (130 KCAS MIN.)
*VDP FLAPS 5° (IF INSTALLED). (50%-60% TORQUE),
VISUAL DESCENT POINT MISSED APPROACH:
AN APPROACH CONTINUE WITH ENGINE
CONSTRUCTED WITH AVDP OUT MISSED APPROACH AIRCRAFT CROSS THE MDA SHOULD HAVE THE PROFILE A/S140 KCAS (130 KCAS MIN) AT OR BEYOND THE VDP. *VDP (20%-30% TORQUE), 800-1000 FPM DESCENT WARNING MAP A/S140 KCAS (130 KCAS MIN) (50%-60% TORQUE)
DO NOT ATTEMPT A
GO-AROUND WITH
GEAR DOWN BELOW WHEN RUNWAY IN SIGHT, LANDING ASSURED, GEAR DOWN, 400' AGL OR AFTER FLAPS 20°, SLOWING TO CROSS THRESHOLD AT 20° FLAPS ARE 110 KCAS (J, L), 105 KCAS (K, M), SELECTED. BEFORE LANDING CHECKLIST COMPLETE
CAUTION CAUTION FINAL CHECK.
CHECK FINAL LANDING CONFIGURATION GEAR EXTENSION TIME.
DO NOT USE SINGLE APPROXIMATELY ENGINE REVERSE 17 SECONDS J, L, THRUST WITH THE 15 SECONDS K, M.
SIMULATED FAILED ENGINE POWER TOUCHDOWN, OPERATING ENGINE POWER LEVER SLOWLY RETARD LEVER ABOVE FLIGHT IDLE. TO FLIGHT IDLE STOP. THEN POWER LEVER START (GROUND IDLE), CHECK PROP BETA, REVERSE AND BRAKES AS REQUIRED.
A-92
Appendix A Figure B-26a LANDING APPROACH SPEEDS Vref
J, K, L, M FLAPS 20° (1.3 Vs1) FLAPS_40° (1.5 Vs1)
WEIGHT K M K M 7,000 93 96 96 7,500 96 100 93 99 100 100 100 103 96 103 103 103 103 106 100 99 106 106 106 105 106 109 103 99 109 109 109 108 9,435 108 112 9,500 112 106 103 112 112 111 9,955 115 115 10,000 109 105 115 114 10,260 110 117 10,500 108 117 11,000 110 119 11,025 110 119 A-93
Appendix A Figure B-26b MU-2B J (-35), K (-25), L (-36), M(-26)
ONE ENGINE INOPERATIVE STRAIGHT-IN NONPRECISION APPROACH **OPTIONAL USE OF CONTINUOUS DESCENT FINAL APPROACH (CDFA) NOTE A/S 140KCAS (130 KCAS MIN. (50%-60% TORQUE), EITHER THIS PROCEDURE, OR FLAPS 5° (IF INSTALLED). DESCEND 500 FPM TO ALTERNATELY PROFILE B-26 PROCEDURE TURN ALTITUDE OR OTHER MUST BE DEMONSTRATED. APPROACH SEGMENT ALTITUDE FLAPS 5° (IF INSTALLED), 140 KCAS (130 KCAS MIN) COMPLETE DESCENT AND APPROACH (50%-60% TORQUE) CHECKLISTS. A/S 150 KCAS 140KCAS (J, L) MIN, 135KCAS (K, M) MIN. REVIEW APPROACH PLATE RADIOS: TUNE & IDENTIFY. CHECK FINAL APPROACH FIX CROSSING ALTITUDE.
**CALCULATE VDA.
A/S 140 KCAS (130 KCAS MIN.)
*VDP CAUTION - STEPDOWN FIXES (50%-60% TORQUE), FLAPS 5°
VISUAL DESCENT POINT **DURING ALL APPROACHES,
AN APPROACH USE CDFA THAT MEETS ALL LANDING ASSURED, CHECK GEAR DOWN,
CONSTRUCTED WITH A VDP ALTITUDE CONSTRAINTS APPROACHING FIX INBOUND, LANDING SHOULD HAVE THE CHECKLIST COMPLETE A/S 120 KCAS MIN.
AIRCRAFT CROSS THE MDA AT OR BEYOND THE VDP. **DERIVED DECISION ALTITUDE (DDA) A/S140 KCAS (130 KCAS MIN) (20%-30% TORQUE),
MDA BEGIN CALCULATED DESCENT RATE AT FAF
WARNING DO NOT ATTEMPT A MISSED APPROACH: *VDP
GO-AROUND WITH CONTINUE WITH GEAR DOWN BELOW 400% AGL OR AFTER MISSED APPROACH ENGINE OUT FINAL CHECK, FLAPS 20°, CHECK FINAL LANDING CONFIGURATION, 20° FLAPS ARE PROFILE SLOWING TO CROSS THRESHOLD AT 110 KCAS (J, L, 105 KCAS (K, M) BEFORE LANDING CHECKLIST COMPLETE SELECTED.
CAUTION TOUCHDOWN, OPERATING ENGINE POWER LEVER SLOWLY RETARD TO FLIGHT IDLE STOP. THEN POWER LEVER GROUND IDLE, CHECK DO NOT USE SINGLE PROP BETA. REVERSE AND BRAKES AS REQUIRED.
ENGINE REVERSE THRUST WITH THE *CAUTION
SIMULATED FAILED
ENGINE POWER WHEN USING CDFA METHOD, MISSED
LEVER ABOVE FLIGHT APPROACH MUST BE EXECUTED UPON IDLE REACHING DDA. DESCENT BELOW MDA
DURING MISSED APPROACH NOT
AUTHORIZED A-94
Appendix A Figure B-27 MU-2B J (-35), K (-25), L (-36), M(-26)
CIRCLING APPROACH AT WEATHER MINIMUMS COMPLETE DESCENT AND APPROACH CHECKLISTS.
A/S 150KCAS 140 KCAS (J, L) MIN, 135 KCAS (K, M) MIN.
REVIEW APPROACH PLATE. RADIOS: TUNE & IDENTIFY.
CHECK FINAL APPROACH FIX ALTITUDE.
CAT C 121 - 140 KCAS 1.7NM CAT D 141 - 165 KCAS 2.3NM FROM APPROACH: GEAR DOWN, FLAPS 5° (IF INSTALLED), A/S 140 KCAS
TOUCHDOWN, RETARD POWER LEVERS TO FLIGHT IDLE STOP, MISSED APPROACH: THEN POWER LEVERS RETARD TO START (GROUND IDLE),
GO-AROUND, MAX CHECK BOTH PROPS BETA, REVERSE AND BRAKES AS POWER, PITCH TO 8° REQUIRED.
CONTINUE WITH TWO
ENGINE MISSED APPROACH PROFILE THRESHOLD:
(10%-20% TORQUE) AS REQUIRED TO MAINTAIN Vref CHECK SINK RATE A/S 140 KCAS (130 KCAS MIN.) CAT CORD 500-600 FPM (APPROX 50% TORQUE), NOT
BELOW CIRCLING MINIMUM DESCENT ALTITUDE FINAL CHECK. FLAPS 20° OR 40° CHECK LANDING APPROACH SPEEDS Vref FINAL LANDING CONFIGURATION.
WEIGHT FLAPS 20° (1.3 VS1 J,K, L. M FLAPS 40° (1.5 V$1) MY ! CAT C OR D AS REQUIRED TO MAINTAIN MAX BANK SLOWING TO Vref 7,000 7,500 93 95 100 95 93 99 100 96 100 30° A/S 120 KCAS MIN,
8.000 8,500 9.000 100 103 106 103 109 106 103 100 96 99 99 103 106 109 103 106 109 103 106 109 (20%-25% TORQUE), 500-600 FPM
9.435 108 112 DESCENT 9,500 112 106 103 112 112 9 955 115 115
10.000 109 105 115 10 260 110 117 10,500 11.000 11.025 110 110 108 CHECK GEAR DOWN, LANDING ASSURED UNTIL WITHIN 30° OF DO NOT DESCEND FLAPS 20° COMPLETE RUNWAY CENTERLINE
LANDING CHECKLIST A-95
Appendix A Figure B-28 WARNING MU-2B J (-35), K (-25), L (-36), M(-26) DO NOT USE CDFA APPROACH
PROCEDURES DURING ENGINE
ONE ENGINE INOPERATIVE CIRCLING APPROACH AT WEATHER MINIMUMS OUT CIRCLING APPROACH
COMPLETE DESCENT AND PROCEDURES
APPROACH CHECKLISTS CAT C 121 - 140 KCAS 1.7NM CAT D 141 - 165 KCAS 2.3NM ** NOTE: ENGINE OUT CIRCLING APPROACH SHOULD BE FLOWN WITH 5° MISSED APPROACH: FROM APPROACH: FLAPS AND GEAR UP. WHEN LANDING CONTINUE WITH ENGINE OUT GEAR UP, FLAPS 5°, A/S 140 KCAS ASSURED, GEAR DOWN, FLAPS 20°, SLOWING TO MISSED APPROACH A/S 110 KCAS (J, L), PROFILE A/S 105 KCAS (K, M) TOUCHDOWN. OPERATING ENGINE POWER LEVER SLOWLY RETARD TO CAUTION NDA FLIGHT IDLE STOP, THEN POWER LEVER TO START (GROUND IDLE).
CHECK PROP BETA. REVERSE AND BRAKES AS REQUIRED.
ANTICIPATE SWERVE
TOWARD OPERATING ENGINE WHEN ENTERING BETA THRESHOLD FLAPS 20P.
A/S 110 KCAS (J, L), 105 KCAS(K, M) A/S 140 KCAS (130 KCAS MIN.) CHECK SINK RATE (APPROX 70% TORQUE), 500-600 FPM
NOT BELOW CIRCLING
MINIMUM DESCENT ALTITUDE FINAL CHECK. FLAPS 20°,
CHECK FINAL LANDING AS REQUIRED CONFIGURATION.
CAT C OR D TO MAINTAIN MAX BANK 30° COMPLETE LANDING A/S 125 KCAS MIN.
CHECKLIST
CAUTION WARNING
DO NOT USE SINGLE DO NOT ATTEMPT A CHECK DESCENT THRUST WITH THE ENGINE REVERSE GEAR DOWN BELOW GO-AROUND WITH CHECK FLAPS 5°, DO NOT DESCEND UNTIL WITHIN PROFILE, LANDING ASSURED, GEAR ENGINE POWER LEVER SIMULATED FAILED 400' AGL OR AFTER 20° FLAPS ARE 30° OF RUNWAY CENTERLINE DOWN. CHECK SINK RATE 500-600 FPM
ABOVE FLIGHT IDLE SELECTED A-96
Appendix A Figure C-1 MU-2B B, D (-10), F (-20), G (-30) NORMAL TAKE-OFF, 5° OR 20° FLAPS PRIOR TO TAKEOFF, CONSULT THE "WEIGHT FOR
POSITIVE GRADIENT AFTER LIFTOFF AND "SINGLE ENGINE RATE OF CLIMB® CHARTS FOR A/S 140 KCAS (B, D), 150 KCAS THE TAKEOFF FLAP SETTING SELECTED. (F), 155 KCAS (G) MIN.
TORQUE AND EGT LIMITS TAKEOFF SPEEDS AFTER GEAR IS FULLY RETRACTED, IF FLAPS 20° ADJUST PITCH TO ACCELERATE. RETRACT FLAPS TO _FOR TORQUE AND EGT LIMITS 5°. INCREASE PITCH TO APPROX. 10°, 130 KCAS AND TAKEOFF SPEED CHARTS (F, NOT MOD S/R10), 140 KCAS (F, MOD S/R10), COMPLETE AFTER T/O SEE TABULAR CHARTS ON 130 KCAS (B, D), 140 KCAS (G), THEN FLAPS UP. AND CLIMB CHECKLIST REVERSE SIDE OF PROFILE.
NORMAL PITCH.
APPROX 8°- FLAPS 20°, APPROX 10-12° -FLAPS 5°
ACCELERATE TO
DESIRED CLIMB SPEED
POS RATE, NO RUNWAY REMAINING FOR LANDING, GEAR UP.
IF 20° FLAPS 113 KCAS MIN. IF 5° FLAPS 120 KCAS (G), 125 KCAS (B, D, F) MIN.
* TORQUE/PS/ OR TEMP
SET AT MAXIMUM LESS OCCURS FIRST. BETA 10% WHICHEVER VR - ROTATE 13° LIGHTS OUT. RELEASE MAX NOSE UP BRAKES. RAM RISE WILL PITCH
CAUSE TORQUE OR
TEMP TO RISE TO MAXIMUM TAKEOFF POWER DURING * NOTE: IF RUNWAY LENGTH OR TAKEOFF ROLL. OBSTACLE CLEARANCE IS
CRITICAL, SET POWER TO
TORQUE/PSI OR TEMP
MAXIMUM, WHICHEVER OCCURS FIRST. RETARD
POWER LEVERS AS REQUIRED
TO MAINTAIN MAXIMUM
ALLOWABLE TORQUE/PSI OR TEMP.
A-97
Appendix A Figure C-1a
TORQUE LIMITS TAKE OFF SPEEDS B, D 64 PSI FLAPS 5° ROTATE B÷ G F, G 60 PSI (STATIC) 10,800 LES 109 64 PSI (RAM CONDITIONS 5 MINUTES) 10,000 LBS 105 9,920 LBS 108 EGT LIMITS DEPEND ON OUTSIDE AIR TEMPERATURE, 9,500 LBS 107 103 CHECK EGT LIMITS PRIOR TO DEPARTURE. 9,350 LBS 111 111 9,000 LBS 110 110 106 101 8,930 LBS 109 8,000 LBS 107 107 107 104 100 7,500 LBS 106 106 106 102 7,000 LBS 104 104 104 FLAPS 20° B÷ D G 10,800 LBS 105 10,000 LBS 102 9,920 LBS 102 9,500 LBS 101 101 9,350 LBS 104 104 9,000 LBS 103 103 100 100 8,930 LBS 103
8.000 LBS 101 101 101 99 100 7,500 LBS 100 100 100 98 7,000 LBS 99 99 99 B: NOT MODIFIED BY S/B 036 AND S/B 092 B+: MODIFIED BY S/B 036 AND S/B 092 A-98
Appendix A Figure C-2 MU-2B B, D (-10), F (-20), G (-30) TAKE-OFF ENGINE FAILURE - FLAPS 5° OR 20° PRIOR TO TAKEOFF, CONSULT THE "WEIGHT FOR POSITIVE GRADIENT AFTER LIFTOFF® AND "SINGLE ENGINE RATE OF CLIMB CHARTS FOR THE TAKEOFF FLAP SETTING SELECTED. APPROX 300-400 FEET (OBSTRUCTION CLEARANCE). IF FLAPS 20° ADJUST PITCH B, D /F/ G TO ACCELERATE 130 KCAS (B, D), Vyse (F, G) MIN. FLAPS TO 5° IF FLAPS 5° FLAP SETTING Vxse (KCAS) Vyse (KCAS) INSTALLED, PITCHAPPROX. 10° (IF FLAPS 5 NOT INSTALLED, FLAPS UP*, PITCH UP 5° 130 / 155/1 115 / 130 / 130 B/D 135 / 150 / 150 120 / 140 / 140 APPROX. 10° TO 13°.) COMPLETE AFTER TAKE-OFF AND A/S 150 KCAS.
20° 100 / 125 / 125 105 / 130 / 135 ENGINE SHUTDOWN CHECKLIST PITCH TO MAINTAIN Vxse 125 KCAS MIN, APPROX 8° PITCH, FLAPS 20°, APPROX 10°-12° PITCH, FLAPS 5°. MAINTAIN DIRECTIONAL CONTROL WITH RUDDER 140 KCAS (F w/SR 10), A/S 135 KCAS (B, D) AND MINIMUM SPOILER. FAILED ENGINE 135 KCAS (F w/o SR 10), CONDITION LEVER, EMERGENCY STOP; POWER 140 KCAS (G) MIN.
LEVER, TAKE OFF **, TRIM AIRCRAFT FLAPS UP*.
*IF SR 10 NOT INSTALLED,
MAXIMUM FLAP SPEED DURING RETRACTION IS 140 KCAS.
POS RATE, NO RUNWAY REMAINING DURING RETRACTION, PITCH TO FOR LANDING, GEAR UP. MAINTAIN 140 KCAS MAX UNTIL F 20° FLAPS 113 KCAS MIN. IF 5° FLAPS FLAPS UP.
120 KCAS (G) 125 KCAS (B, D, F)
MAKE NORMAL T/O * IF SUFFICIENT RUNWAY CAUTION REMAINS, OR UNABLE TO CLIMB:
GEAR DOWN, REDUCE POWER TO
SIMULATED ENGINE LAND STRAIGHT AHEAD USING FAILURE (NOT LESS THAN 200 FT AGL) A/S APPROPRIATE FOR WEIGHT, 100 KCAS (B, D) MIN 105 KCAS (F) MIN.
110 KCAS (G) MIN, A-99
Appendix A Figure C-3 MU-2B B, D (-10), F (-20), G (-30)
TAKE-OFF ENGINE FAILURE ON RUNWAY
CAUTION
SIMULATED ENGINE FAILURE OR MALFUNCTION
IS TO BE GIVEN BY INSTRUCTOR AT NOT MORE THAN 50% OF ROTATE SPEEDS.
ENGINE FAILS OR CLEAR RUNWAY
MALFUNCTION OCCURS OR EVACUATE
AIRCRAFT AS POWER LEVERS TO GROUND NECESSARY *
DLE, BRAKES AS NECESSARY
REVERSE THRUST AS REQUIRED. USE NOSE WHEEL
STEERING, BRAKES, AND/OR
REVERSE THRUST TO
MAINTAIN DIRECTIONAL NOTIFY TOWER CONTROL. OF ABORT
POWER SET,
BRAKES RELEASED * IF EVACUATING
AIRCRAFT, BOTH
CONDITION LEVERS TO
EMERGENCY STOP AND
CAUTION MASTER SWITCH TO EMERGENCY
DO NOT USE SINGLE
ENGINE REVERSE THRUST
WITH THE SIMULATED
FAILED ENGINE POWER
LEVER ABOVE FLIGHT IDLE.
A-100
Appendix A Figure C-4 MU-2B B, D (-10), F (-20), G (-30)
TAKE-OFF ENGINE FAILURE - UNABLE TO CLIMB
CLASSROOM DISCUSSION OR FTD USE ONLY PRIOR TO TAKEOFF, CONSULT THE "WEIGHT FOR POSITIVE GRADIENT AFTER LIFTOFF® AND "SINGLE ENGINE RATE OF CLIMB® CHARTS FOR THE TAKEOFF FLAP SETTING SELECTED.
PILOT MAKES DECISION TO EITHER
RETURN THE RUNWAY SURFACE OR TO
WARNING FLY BEYOND AIRPORT BOUNDARY TO
DO NOT LET AIRSPEED SUITABLE LANDING AREA
DECELERATE BELOW SINGLE ENGINE AIRSPEED.
105 KCAS (G) 100 KCAS (B, D, F) MIN. ENGINE FAILS
POS RATE, NO RUNWAY REMAINING FOR LANDING, GEAR UP.
IF 20° FLAPS 113 KCAS MIN. IF 5° FLAPS 120 KCAS (G), 125 KCAS (B, D, F) MIN. PROPELLERS BETA, THEN
REVERSE AND BRAKES AS
REQUIRED ROTATE
IF RUNWAY REMAINS OR A LANDING CAN
RELEASE BRAKES POWER SET, SURFACE, CHECK GEAR DOWN, FLAPS SAFELY BE MADE ON THE AIRPORT REMAIN IN TAKE-OFF POSITION, ANTICIPATE SWERVE CAUTION LAND USING SINGLE ENGINE AIRSPEED, POWER ON OPERATING ENGINE AS REQUIRED TO LAND. 100 KCAS MIN (B, D) TOWARD OPERATING ENTERING BETA ENGINE WHEN 105 KCAS MIN( F) 110 KCAS MIN (G) A-101
Appendix A Figure C-5 MU-2B B, D (-10), F (-20), G (-30)
STEEP TURNS
SET HEADING START NORMAL TURN POWER AS BUG TO ROLL REQUIRED. (INCREASE OUT HEADING APPROXIMATELY 10% TORQUE) *CLEAR AREA, 50° BANK GEAR UP, FLAPS ESTABLISHED. PITCH UP, A/S 180 KCAS, UP APPROXIMATELY TRIM A/C 2° TO 3º ORAS
NECESSARY TO MAINTAIN ALTITUDE.
*THIS MANEUVER SHOULD BE PERFORMED IN
BOTH CLEAN AND LANDING CONFIGURATIONS CHECK FOR (USE 130 KCAS FLAPS 20°, GEAR DOWN, FOR A/S AND
LANDING CONFIGURATION) ALTITUDE TRENDS ** NOTE: TURNS WILL
BE DONE THROUGH 360° AS WELL AS 180° REDUCE POWER TO ROLL OUT ON **START ROLL OUT MAINTAIN 180 KCAS HEADING ON ALT. 20° BEFORE ROLL