Appendix A Figure B-21 MU-2B J (-35), K (-25), L (-36), M(-26)
ILS, LPV, RNP, LNAV/NAV APPROACH COMPLETE DESCENT AND APPROACH CHECKLISTS. A/S A/S 140 KCAS MIN. (20%-25% TORQUE), 150 KCAS, 140KCAS (J, L, M, K+) MIN, 130 KCAS (K) MIN, DESCEND 500 FPM TO PROCEDURE REVIEW APPROACH PLATE. RADIOS: TUNE & IDENTIFY. TURN OR OTHER APPROACH SEGMENT
CHECK FINAL APPROACH FIX ALTITUDE, MARKER ALTITUDE BEACON RECEIVER "ON® FLAPS 5°, 140 KCAS MIN (25%-30% TORQUE) LANDING APPROACH SPEEDS Vref
J, K, L, M FLAPS 20° (1.3 V81) FLAPS 40° (1.5 V$1)
WEIGHT K 7,000 A/S 140 KCAS MIN.
105 108 MISSED APPROACH: (25%-30% TORQUE) 10000000 CONTINUE WITH 105 103 112 MISSED APPROACH LANDING ASSURED, CHECK GEAR DOWN, 105 115 114 PROFILE A/S 140 KCAS (J, L, M, K+) 130 KCAS (K) 117 FLAPS 20° APPROACHING GLIDE SLOPE 117 119 (ONE DOT BELOW G/S), A/S 120 KCAS MIN.
COMPLETE LANDING CHECKLIST (APPROX 25% TORQUE) FINAL CHECK. FLAPS 20% (OR 40°) DH IF DESIRED, BELOW 120 KCAS) TOUCHDOWN: POWER LEVERS RETARD TO FLIGHT IDLE STOP. POWER LEVERS RETARD TO START (GROUND IDLE), CHECK BOTH PROPS BETA.
REVERSE AND BRAKES AS REQUIRED.
A-86
Appendix A Figure B-22 MU-2B J (-35), K (-25), L (-36), M(-26)
TWO ENGINE MISSED APPROACH
COMPLETE AFTER
TAKEOFF CHECKLIST
ACCELERATE TO
DESIRED CLIMB SPEED A/S 130 KCAS (K), 140 KCAS (J, L, M),
FLAPS UP AFTER GEAR IS FULLY RETRACTED, A/S 130 KCAS.
IF FLAPS 20° RETRACT FLAPS TO 5° (IF INSTALLED).
INCREASE PITCH TO APPROX. 10°, A/S130 KCAS (K), 140 KCAS (J, L, M) MISSED APPROACH GO- POSITIVE RATE, GEAR UP.
AROUND. MAX POWER. IF 20° FLAPS 113 KCAS MIN.
PITCH UP 8° AND SELECT IF 5° FLAPS 120 KCAS (J, L) MIN, FLAPS 20° IF 40° 125 KCAS (K, M) MIN
PREVIOUSLY SELECTED MAP A-87
Appendix A Figure B-23 MU-2B J (-35), K (-25), L (-36), M(-26)
ONE ENGINE INOPERATIVE ILS, LPV, RNP, LNAV/NAV APPROACH A/S 140 KCAS (130 KCAS MIN.), (50%-60% TORQUE), FLAPS 5°.
DESCEND 500 FPM TO PROCEDURE TURN OR OTHER APPROACH
SEGMENT ALTITUDE
COMPLETE DESCENT AND APPROACH CHECKLISTS. A/S 150 KCAS, 140 KCAS MIN (J, L), 135 KCAS MIN (K,M). REVIEW APPROACH PLATE.
APPROACH FIX ALTITUDE, MARKER RECEIVER RADIOS: TUNE & IDENTIFY. CHECK FINAL FLAPS 5°, 140 KCAS (130 KCAS MIN) (50%-60% TORQUE) "ON° WARNING A/S 140 KCAS (130 KCAS DO NOT ATTEMPT A GO-AROUND WITH MIN.) (50%-60% TORQUE), FLAPS 5°.
GEAR DOWN BELOW MISSED APPROACH:
400' AGL OR AFTER CONTINUE WITH ENGINE OUT 20° FLAPS ARE MISSED APPROACH PROFILE LANDING ASSURED, CHECK GEAR SELECTED. DOWN APPROACHING GLIDE
SLOPE (ONE DOT BELOW G/S), A/S 140 KCAS (130 KCAS MIN).
CAUTION
DO NOT USE SINGLE
ENGINE REVERSE LANDING CHECK THRUST WITH THE DH (50%-55% TORQUE)
SIMULATED FAILED ENGINE POWER RUNWAY IN SIGHT, FINAL CHECK, FLAPS 20°, LEVER ABOVE FLIGHT SLOWING TO CROSS THRESHOLD 110 KCAS (J, L), 105 IDLE. KCAS (K, M). COMPLETE LANDING CHECKLIST. RUDDER TRIM CENTERED. HOLD BALL IN CENTER WITH RUDDER.
CHECK FINAL LANDING CONFIGURATION.
OPERATING ENGINE POWER TOUCHDOWN, OPERATING ENGINE POWER LEVER
LEVER START (GROUND SLOWLY RETARD TO FLIGHT REVERSE AND BRAKES AS IDLE), CHECK PROP BETA, IDLE STOP.
REQUIRED.
A-88
Appendix A Figure B-24 MU-2B J (-35), K (-25), L (-36), M(-26)
ONE ENGINE INOPERATIVE MISSED APPROACH J, K, L, M AFTER TAKEOFF CHECKLIST A/S 150 KCAS, COMPLETE FLAP SETTING Vxse (KCAS) Vyse (KCAS) UP 140 / 135 * 150 / 150 * 5° 130 / 130 * 140 / 140 * A/S 130 KCAS (K), 20° 125 / 125 * 135 / 130 * 140 KCAS (J, L, M),
FLAPS UP *K, M
AFTER GEAR IS FULLY RETRACTED AND OBSTRUCTINS ARE CLEARED, IF FLAPS 20°, ADJUST PITCH TO ACCELERATE TO Vyse, IF FLAPS 5° INSTALLED, RETRACT FLAPS TO 5°. INCREASE PITCH TO APPROX. 10°, A/S130 KCAS (K), 140 KCAS (J, L, M) PITCH TO MAINTAIN Vse MIN, APPROX 8° PITCH, FLAPS 20° APPROX 10-130 PITCH FLAPS 50 F 20PFLAPS 113 KCAS MIN. IF 50 FLAPS 120 KCAS (J, L) MIN. 125 KCAS (K, M) MIN.
COMMENCING MISSED APPROACH, SET MAX POWER. MAINTAIN DIRECTIONAL
CONTROL, RUDDER AND SPOILER AS NECESSARY. GEAR UP.
MAP
WARNING
UNDER CERTAIN COMBINATIONS OF WEIGHT, *IF TRANSITIONING FROM A DESCENT, TEMERATURE AND PRESSURE ALTITUDE, WITH LANDING MAINTAIN PITCH TO MAINTAIN 140 KCAS, GEAR DOWN AND FLAPS 209, SINGLE ENGINE GO RAISE GEAR, THEN 10° PITCH. SOME AROUND MAY NOT BE POSSIBLE AT ALTITUDES OF LESS ALTITUDE LOSS IS TO BE EXPECTED. THAN 400 FEET AGL. (SEE PAGE B-24a) A-89
Appendix A Figure B-25 NOTE MU-2B J (-35), K (-25), L (-36), M(-26)
EITHER THIS PROCEDURE, OR ALTERNATELY PROFILE B-25a NONPRECISION STRAIGHT-IN APPROACH MUST BE DEMONSTRATED.
COMPLETE DESCENT AND APPROACH CHECKLISTS. (20%-25% TORQUE), DESCEND 500 FPM A/S 140 KCAS (130 KCAS MIN).
A/S 150 KCAS 140KCAS (J, L, M, K+), 130 KCAS (K) MIN. REVIEW APPROACH PLATE. RADIOS: TUNE & TO PROCEDURE TURN OR OTHER APPROACH SEGMENT ALTITUDE IDENTIFY. CHECK FINAL APPROACH FIX CROSSING ALTITUDE.
FLAPS 5°, A/S 140 KCAS MIN.
LANDING APPROACH SPEEDS Vref (25%-30% TORQUE)
J,K, L, M FLAPS 20° (1.3 VS1) FLAPS 40° (1.5 V$1) MIL 96 100 103 93 96 103 189 193 100 106 100 99 106 106 109 103 99 109 109 109 A/S 140 KCAS MIN.
108 112 (25%-30% TORQUE) 112 106 103 112 112
9.955 115 115 10,000 109 105 115 10,260 110 117 LANDING ASSURED, CHECK GEAR 10,500 108 DOWN, FLAPS 20° APPROACHING 11,000 11.025 110 110 FIX INBOUND, LANDING CHECKLIST MAP COMPLETE A/S 120 KCAS MIN.
MDA A/S 120 KCAS MIN, (25%-30% TORQUE), MISSED APPROACH: 800-1000 FPM DESCENT POWER, PITCH TO 8° GO-AROUND, MAX *VDP A/S 120 KCAS MIN.
CONTINUE WITH TWO (APPROX 50% TORQUE)
ENGINE MISSED *VDP APPROACH PROFILE AN APPROACH FINAL CHECK. FLAPS 40° (IF DESIRED, BELOW 120 KCAS)
CONSTRUCTED WITH
A VDP SHOULD HAVE THE AIRCRAFT CROSS TOUCHDOWN: POWER LEVERS RETARD TO FLIGHT IDLE STOP,
THE MDA AT OR THEN POWER LEVERS RETARD TO START (GROUND IDLE), BEYOND THE VDP. CHECK BOTH PROPS BETA. REVERSE AND BRAKES AS REQUIRED.
A-90
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