Appendix A Figure C-20 MU-2B B, D (-10), F (-20), G (-30)
CROSSWIND LANDING
DEMONSTRATED
CROSSWIND
ALL MODELS TAKEOFF 22 KCAS LANDING 18 KCAS
• WIND WIND
AIRCRAFT WILL BE FLOWN DOWN AN EXTENSION OF
THE RUNWAY CENTER LINE WITH DRIFT CORRECTION
ESTABLISHED SUFFICIENTLY IN ADVANCE TO PERMIT
CENTER LINE TO BE FLOWN WITH ONLY MINOR
COORDINATED CORRECTIONS INCREASE Vref FOR CROSSWIND LANDING BY ONE-
HALF THE STEADY WIND SPEED PLUS ONE-HALF THE GUST SPEED NOT TO EXCEED Vref PLUS 10 KCAS.
• WIND
PRIOR TO TOUCHDOWN, THE UPWIND WING IS LOWERED AND SMOOTHLY MODULATED. OPPOSITE
RUDDER IS APPLIED SO THAT AIRCRAFT PATH CONTINUES DOWN RUNWAY CENTERLINE. THE
AIRCRAFT SHOULD NOT BE ALLOWED TO DEVELOP ANY TENDENCY TO DRIFT DOWNWIND.
NOTE: RUDDERS CENTERED BEFORE NOSE WHEEL TOUCHDOWN. SPOILERS INTO WIND AS NECESSARY
TO KEEP WINGS LEVEL WIND A-119
Appendix A Figure C-21 MU-2B B, D (-10), F (-20), G (-30)
ILS, LPV, RNP, LNAV/NAV APPROACH IF FLAPS 5° INSTALLED. A/S 130 KCAS (B, D), COMPLETE DESCENT AND APPROACH 130 KCAS (F NOT MOD S/R10), 140 KCAS CHECKLISTS. A/S 150 KCAS (140 KCAS MIN) (F MOD S/R10), 140 KCAS (G) MIN) REVIEW APPROACH PLATE. RADIOS: TUNE (40-50% TORQUE, 25-32 PSI) & IDENTIFY. CHECK FINAL APPROACH FIX ALTITUDE MARKER BEACON RECEIVER "ON" A/S 140/130 KCAS, MIN. (20-25% TORQUE, 13-16 PS/) DESCEND 500 FPM TO PROCEDURE TURN OR OTHER APPROACH SEGMENT ALTITUDE.
A/S 140/130 KCAS.
(25%-30% TORQUE LANDING APPROACH SPEEDS VIe B. B+. D. F. C 16-20 PSI) FLAPS 20° (1.3 V$1) FLAPS 40° (1.5 V$1) WEIGHT 8880 B+, D L128 B+, D 7,000 94 7,500 94 95 LANDING ASSURED, GEAR DOWN, 8,000 100 97 101 101 FLAPS 20 APPROACHING 101 103 100 104 GLIDESLOPE (ONE DOT BELOW G/S) 101 104 103 107 A/S 120 KCAS MIN.
106 103 109 108 9,500 105 10,000 108 COMPLETE LANDING CHECKLIST
10.260 109 117 (APPROX 25% TORQUE, 16 PSI) MISSED APPROACH: CONTINUE WITH DH FINAL CHECK. FLAPS 20° (OR 40°) IF DESIRED, BELOW 120 KCAS)
MISSED APPROACH
PROFILE THRESHOLD: (10%-20% TORQUE, 10-13 PSI) Vref 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-120
Appendix A Figure C-22 MU-2B B, D (-10), F (-20), G (-30)
TWO ENGINE MISSED APPROACH
COMPLETE AFTER
TAKEOFF CHECKLIST
ACCELERATE TO
DESIRED CLIMB SPEED A/S130 KCAS (F, NOT MOD S/R10) 140 KCAS (F, MOD S/R10), 130 KCAS (B, D), 140 KCAS (G)
• FLAPS UP AFTER GEAR IS FULLY RETRACTED, IF FLAPS 20° RETRACT FLAPS TO 5° (IF INSTALLED).
INCREASE PITCH TO APPROX. 10°,
MISSED APPROACH GO- PITCH UP 8° AND SELECT AROUND. MAX POWER. FLAPS 20° IF 40° 20° FLAPS 113 KCAS MIN. IF 5° POSITIVE RATE, GEAR UP, IF FLAPS 120 KCAS MIN (G), PREVIOUSLY SELECTED 125 KCAS MIN (B, D, F) MAP A-121
Appendix A Figure C-23 MU-2B B, D (-10), F (-20), G (-30)
ONE ENGINE INOPERATIVE ILS, LPV, RNP, LNAVIVNAV APPROACH A/S 140/130 KCAS, (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 (G), 135 KCAS MIN (F), 130 KCAS MIN (B,D). (APPROX 70% TORQUE, 45 FLAPS 5° (IF INSTALLED) A/S 140/130 KCAS MIN.
PSI) IDENTIFY. CHECK FINAL APPROACH FIX ALTITUDE, REVIEW APPROACH PLATE. RADIOS: TUNE & (50%-60% TORQUE, 32-40 PSI) MARKER RECEIVER "ON®
WARNING DO NOT ATTEMPT A GO-AROUND WITH FLAPS 5°. DESCEND 500 FPM (40-50% TORQUE, 26-32 PSI)
GEAR DOWN BELOW 400' AGL OR AFTER MISSED APPROACH:
20° FLAPS ARE CONTINUE WITH ENGINE OUT SELECTED. MISSED APPROACH PROFILE LANDING ASSURED, CHECK GEAR
DOWN APPROACHING GLIDE
SLOPE (ONE DOT BELOW G/S) CAUTION A/S 140 KCAS (130 KCAS MIN).
DO NOT USE SINGLE DH
ENGINE REVERSE LANDING CHECK THRUST WITH THE (50-55% TORQUE, 32-38 PSI)
SIMULATED FAILED ENGINE POWER LEVER RUNWAY IN SIGHT, FINAL CHECK. FLAPS 20°.
ABOVE FLIGHT IDLE. SLOWING TO CROSS THRESHOLD AT A/S 110 KCAS (G), 105 KCAS (F), 100 KCAS (B, D).
COMPLETE LANDING CHECKLIST, RUDDER TRIM CENTERED. HOLD BALL IN CENTER WITH RUDDER.
CHECK FINAL LANDING CONFIGURATION.
OPERATING ENGINE POWER TOUCHDOWN, OPERATING
LEVER START (GROUND ENGINE POWER LEVER
IDLE), CHECK PROP BETA, SLOWLY RETARD TO FLIGHT
REVERSE AND BRAKES AS IDLE STOP REQUIRED.
A-122
Appendix A Figure C-24 MU-2B B, D (-10), F (-20), G (-30)
ONE ENGINE INOPERATIVE MISSED APPROACH
B, D /F/ G A/S 150 KCAS, COMPLETE FLAP SETTING Vxse (KCAS) Vyse (KCAS) AFTER TAKEOFF CHECKLIST UP 130 / 135 / 140 135 / 150 / 150 5° 115 / 130 / 130 120 / 140 / 140 20° 100 / 125 / 125 105 / 130 / 135 A/S 130 KCAS (F, NOT MOD S/R10), 140 KCAS (F, MOD S/R10), 130 KCAS (B, D), 140 KCAS (G) FLAPS UP*, PITCH APPROX. 10° TO 13°.
AFTER GEAR IS FULLY RETRACTED, AND OBSTRUCTIONS ARE CLEARED, IF FLAPS 20° ADJUST PITCH TO ACCELERATE TO Vyse.
(IF FLAPS 5° INSTALLED) RETRACT FLAPS TO 5°, PITCHAPPROX. 10° A/S 130 KCAS (F, NOT MOD S/R10), 140 KCAS (F, MOD S/R10), 130 KCAS (B, D), 140 KCAS (G) PITCH TO MAINTAIN Vse 125 KCAS MIN, APPROX 8° PITCH, FLAPS 20°, APPROX 10-13° PITCH, FLAPS 5ª. IF 20° FLAPS 113 KCAS MIN.
IF 5° FLAPS 120 KCAS (G) MIN. 125 KCAS (B, D, F) 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 C-24a) A-123
Appendix A Figure C-25 NOTE MU-2B B, D (-10), F (-20), G (-30)
EITHER THIS PROCEDURE, OR ALTERNATELY PROFILE C-25a NONPRECISION STRAIGHT-IN APPROACH MUST BE DEMONSTRATED.
COMPLETE DESCENT AND APPROACH CHECKLISTS. IF FLAPS 5° INSTALLED. A/S (20%-25% TORQUE, 13-16 PSI) A/S 150 KCAS (140 KCAS MIN) REVIEW APPROACH PLATE. RADIOS: TUNE & IDENTIFY. CHECK FINAL NOT MOD S/R10), 140 KCAS (F, 130 KCAS (B, D), 130 KCAS (F, DESCEND 500 FPM TO PROCEDURE TURN OR OTHER APPROACH APPROACH FIX CROSSING ALTITUDE MOD S/R10), 140 KCAS (G), SEGMENT ALTITUDE.
(40%-50% TORQUE, 25-32 PSI) LANDING APPROACH SPEEDS Vref B, B+, D, F.G FLAPS 20° (1.3 V81) FLAPS 40° (1.5 V$1 WEIGHT 94 94 96 94 95 90 99 100 100 97 101 10 103 101 103 100 104 104 106 106 A/S 140 KCAS (130 KCAS MIN) 8,930 103 107 (25%-30% TORQUE, 16-20 PSI)
9.000 106 103 109 109 9,435 108 112 9,500 105 112 10,000 108 115 LANDING ASSURED, CHECK
10.260 109 117 GEAR DOWN, FLAPS 20°
APPROACHING FIX INBOUND, MAP COMPLETE A/S 120 KCAS MIN. LANDING CHECKLIST MISSED APPROACH: GO- MDA A/S 120 KCAS MIN, (25%-30% TORQUE, 16-20 PSI) AROUND, MAX POWER, 800-1000 FPM DESCENT ROTATE TO 8°. *VDP
CONTINUE WITH TWO A/S 120 KCAS MIN.
VISUAL DESCENT POINT *VDP APPROACH PROFILE ENGINE MISSED (APPROX 50% TORQUE, 32 PSI) AN APPROACH FINAL CHECK. SELECT FLAPS 40° (IF DESIRED, BELOW 120 KCAS
CONSTRUCTED WITH A
VDP SHOULD HAVE THE AIRCRAFT CROSS THE TOUCHDOWN: POWER LEVERS RETARD TO FLIGHT IDLE STOP, THEN MDA AT OR BEYOND POWER LEVERS RETARD TO START. (GROUND IDLE). CHECK BOTH THE VDP. PROPS BETA. REVERSE AND BRAKES AS REQUIRED.
A-124
Appendix A Figure C-25a NOTE MU-2B B, D (-10), F (-20), G (-30)
EITHER THIS PROCEDURE,
OR ALTERNATELY PROFILE NONPRECISION STRAIGHT-IN APPROACH C-25 MUST BE **OPTIONAL USE OF CONTINUOUS DESCENT FINAL APPROACH (CDFA) DEMONSTRATED.
IF FLAPS 5° INSTALLED. A/S (20%-25% TORQUE, 13-16 PSI) 130 KCAS (B, D), 130 KCAS (F DESCEND 500 FPM TO PROCEDURE COMPLETE DESCENT AND APPROACH CHECKLISTS. NOT MOD S/R10), 140 KCAS (F TURN OR OTHER APPROACH A/S 150 KCAS (140 KCAS MIN) REVIEW APPROACH MOD S/R10), 140 KCAS (G), SEGMENT ALTITUDE.
PLATE. RADIOS: TUNE & IDENTIFY. CHECK FINAL (40%-50% TORQUE, 25-32 PSI)
APPROACH FIX CROSSING ALTITUDE LANDING APPROACH SPEEDS Vref B, B+, D, F,G FLAPS 20° (1.3 V$1) FLAPS 40° (1.5 VS1) WEIGHT 7,000 94 7,500 95 96 95 95 99 100 8,000 95 90 100 97 101 10 103 105 8,500 101 103 100 104 106 105 8,490 8,930 9,000 9,435 101 103 1065 103 108 104 107 109 112 109 CAUTION - STEPDOWN FIXES **DURING ALL APPROACHES, (25%-30% TORQUE, 16-20 PSI) A/S 140 KCAS (130 KCAS MIN) 9,500 105 112 USE CDFA THAT MEETS ALL 10,000 10,260 109 108 115 117 ALTITUDE CONSTRAINTS LANDING ASSURED, CHECK GEAR 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, 16-20 PSI) MISSED APPROACH MUST BE WHEN USING CDFA METHOD. MISSED APPROACH: MDA 800-1000 FPM DESCENT DDA. DESCENT BELOW MDA EXECUTED UPON REACHING POWER, PITCH TO 8°. CONTINUE WITH TWO GO-AROUND, MAX *VDP (APPROX 50% TORQUE, 32 PSI) A/S 120 KCAS MIN.
DURING MISSED APPROACH ENGINE MISSED
NOT AUTHORIZED APPROACH PROFILE FINAL CHECK
CHECK FINAL LANDING CONFIGURATION *VDP
VISUAL DESCENT POINT AN APPROACH TOUCHDOWN: POWER LEVERS RETARD TO FLIGHT IDLE STOP, THEN POWER LEVERS RETARD TO START (GROUND IDLE), CHECK BOTH CONSTRUCTED WITH AVDP PROPS BETA. REVERSE AND BRAKES AS REQUIRED.
SHOULD HAVE THE AIRCRAFT
CROSS THE MDA AT OR BEYOND THE VDP.
A-125
Appendix A Figure C-26 NOTE MU-2B B, D (-10), F (-20), G (-30)
EITHER THIS ONE ENGINE INOPERATIVE STRAIGHT-IN NONPRECISION APPROACH
PROCEDURE, OR
ALTERNATELY PROFILE C-26b MUST BE A/S 140/130 KCAS, (20-25% TORQUE DEMONSTRATED. 13-16 PSI) DESCEND 500 FPM TO PROCEDURE TURN ALTITUDE.
FLAPS 5°, (IF INSTALLED) (50%-60% TORQUE, 32-40 PSI)
COMPLETE DESCENT AND APPROACH CHECKLISTS. A/S 150 KCAS, 140 KCAS MIN (G), 135 KCAS MIN (F), 130 KCAS MIN (B, D), (APPROX 70% TORQUE, 45 PSI) REVIEW APPROACH PLATE. RADIOS: TUNE & IDENTIFY.
CHECK FINAL APPROACH FIX CROSSING
ALTITUDE *VDP VISUAL DESCENT POINT A/S 140 KCAS (130 KCAS MIN.) (40%- CONSTRUCTED WITH A VDP AN APPROACH CONTINUE WITH ENGINE OUT MISSED APPROACH: 50% TORQUE, 26-32 PS/) FLAPS 5° (IF INSTALLED)
SHOULD HAVE THE MISSED APPROACH PROFILE AIRCRAFT CROSS THE MDA A/S140 KCAS (130 KCAS MIN) AT OR BEYOND THE VDP. *VDP (20-30% TORQUE, 13-20 PSI) 800-1000 FPM DESCENT WARNING MAP MDA A/S140 KCAS (130 KCAS MIN) DO NOT ATTEMPT A GO-AROUND WITH (50-60% TORQUE, 32-40 PSI)
GEAR DOWN BELOW 400' AGL OR AFTER WHEN RUNWAY IN SIGHT, LANDING ASSURED, GEAR DOWN, FLAPS 20° FLAPS ARE 20°, SLOWING TO CROSS THRESHOLD AT 110 KCAS (G), 105 KCAS (F), SELECTED. 100 KCAS (B, D). BEFORE LANDING CHECKLIST COMPLETE CAUTION FINAL CHECK.
DO NOT USE SINGLE CHECK FINAL LANDING CONFIGURATION CAUTION ENGINE REVERSE GEAR EXTENSION TIME.
THRUST WITH THE APPROXIMATELY SIMULATED FAILED TOUCHDOWN, OPERATING ENGINE POWER LEVER SLOWLY RETARD 17 SECONDS G ENGINE POWER TO FLIGHT IDLE STOP. THEN POWER LEVER START (GROUND IDLE), 15 SECONDS B, D, F LEVER ABOVE FLIGHT CHECK PROP BETA, REVERSE AND BRAKES AS REQUIRED.
IDLE.
A-126
Appendix A Figure C-26a LANDING APPROACH SPEEDS Vref B, B+, D, F, G FLAPS 20° (1.3 Vs1) FLAPS 40° (1.5 Vs1) WEIGHT B+, D B+, D G 7,000 92 92 93 94 94 7,500 95 95 96 94 98 98 99 8,000 98 98 100 97 101 101 103 8,500 101 103 100 104 106 8,490 101 104 8,930 103 107 9,000 106 103 109 9,435 108 112 9,500 105 10,000 108 10,260 109 A-127
Appendix A Figure C-26b MU-2B B, D (-10), F (-20), G (-30)
ONE ENGINE INOPERATIVE STRAIGHT-IN NONPRECISION APPROACH **OPTIONAL USE OF CONTINUOUS DESCENT FINAL APPROACH (CDFA) NOTE A/S 140 KCAS (130 KCAS MIN). (20-25% TORQUE, EITHER THIS PROCEDURE, OR 13-16 PS/) FLAPS 5° (IF INSTALLED). DESCEND ALTERNATELY PROFILE C-26 500 FPM TO PROCEDURE TURN ALTITUDE OR MUST BE DEMONSTRATED. OTHER APPROACH SEGMENT ALTITUDE FLAPS 5°, (50%-60% TORQUE, 32-40 PSI)
COMPLETE DESCENT AND APPROACH CHECKLISTS. A/S 150 KCAS, (140 KCAS MIN (G)) (135 KCAS MIN (F)) (130 KCAS MIN (B, D)) (APPROX 70% TORQUE, 45 PSI) REVIEW APPROACH PLATE. RADIOS: TUNE & IDENTIFY.
CHECK FINAL APPROACH FIX CROSSING
ALTITUDE A/S 140 KCAS (130 KCAS MIN.)
(40%-50% TORQUE, 26-32 PSI) *VDP CAUTION - STEPDOWN FIXES FLAPS 5° (IF INSTALLED).
VISUAL DESCENT POINT CONSTRUCTED WITH A VDP AIRCRAFT CROSS THE MDA SHOULD HAVE THE AN APPROACH **DURING ALL APPROACHES, USE CDFA THAT MEETS ALL ALTITUDE CONSTRAINTS LANDING ASSURED, CHECK GEAR INBOUND, LANDING CHECKLIST COMPLETE A/S 120 KCAS MIN. DOWN, APPROACHING FIX AT OR BEYOND THE VDP. **DERIVED DECISION ALTITUDE (DDA) A/S140 KCAS (130 KCAS MIN) (20-30% TORQUE, MDA 13-20 PSI), BEGIN CALCULATED DESCENT RATE
WARNING AT FAF DO NOT ATTEMPT A MISSED APPROACH: *VDP
GO-AROUND WITH CONTINUE WITH
GEAR DOWN BELOW ENGINE OUT 400' AGL OR AFTER MISSED APPROACH FINAL CHECK., FLAPS 20°, CHECK FINAL LANDING CONFIGURATION, 20° FLAPS ARE PROFILE SLOWING TO CROSS THRESHOLD AT 110 KCAS (G), 105 KCAS (F), SELECTED. 100 KACAS (B,D).. BEFORE LANDING CHECKLIST COMPLETE 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 H-14Ò
Appendix A Figure C-27 MU-2B B, D (-10), F (-20), G (-30)
CIRCLING APPROACH AT WEATHER MINIMUMS COMPLETE DESCENT AND APPROACH CHECKLISTS. A/S 150 COMPLETE DESCENT AND KCAS (140 KCAS MIN (G)), (135K CAS MIN (F)), (130 KCAS MIN (B, APPROACH CHECKLISTS.
D)). (APPROX 70% TORQUE, 45 PSI) REVIEW APPROACH PLATE.
RADIOS: TUNE & IDENTIFY. CHECK FINAL APPROACH FIX
CROSSING 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 MISSED APPROACH: GO-AROUND, MAX TOUCHDOWN, RETARD POWER LEVERS TO FLIGHT IDLE STOP, THEN POWER LEVERS RETARD TO START (GROUND IDLE), CHECK BOTH PROPS BETA, REVERSE AND BRAKES AS POWER, PITCH TO 8°. REQUIRED.
CONTINUE WITH TWO
ENGINE MISSED APPROACH PROFILE THRESHOLD:
*EN CORD (20% TORQUE, 13 PSI) Vref CHECK SINK RATE A/S 140 KCAS (130 KCAS MIN.) 500-600 FPM APPROX 50% TORQUE 32 PSI,
NOT BELOW CIRCLING
MINIMUM DESCENT ALTITUDE FINAL CHECK FLAPS 20° OR 40° CHECK
FINAL LANDING
CONFIGURATION LANDING APPROACH SPEEDS Vref B. B+, D. F. G CATCORD TO MAINTAIN AS REQUIRED *MAX BANK SLOWING TO Vref WEIGHT 7,000 92 FLAPS 20° (1.3 Vs1) B+. D 92 93 G 94 FLAPS 40° (1.5 Vs1) B+. D E 94 ' ,300 PSI) A/S 120 KCAS MIN, 500-600 FPM DESCENT (20-25% TORQUE, 13-16
7.500 95 95 96 94 98 98 99 100
8.000 98 98 100 97 101 10 103 103 8,500 101 103 100 104 106 106 8,490 101 104
8.930 103 107
9.000 106 103 109 109
9.435 108 112 9,500 105 LANDING ASSURED, DO NOT DESCEND
10.000 108 CHECK GEAR DOWN, UNTIL WITHIN 30° OF 10,260 109 FLAPS 20° COMPLETE RUNWAY CENTERLINE
LANDING CHECKLIST A-129
Appendix A Figure C-28
WARNING MU-2B B, D (-10), F (-20), G (-30) DO NOT USE CDFA APPROACH
ONE ENGINE INOPERATIVE CIRCLING APPROACH AT WEATHER MINIMUMS PROCEDURES DURING ENGINE
OUT CIRCLING APPROACH
COMPLETE DESCENT AND PROCEDURES APPROACH CHECKLISTS.
CAT C 121 - 140 KCAS 1.7NM CAT D 141 - 165 KCAS 2.3NM APPROACH SHOULD BE FLOWN WITH 5° ** NOTE: ENGINE OUT CIRCLING FLAPS AND GEAR UP. WHEN LANDING MISSED APPROACH: CONTINUE WITH ENGINE OUT GEAR UP, FLAPS 5°, FROM APPROACH: A/S 140 KCAS A/S 110 KCAS (G), A/S 105 KCAS (B, D, F) ASSURED, GEAR DOWN, FLAPS 20°, SLOWING TO
MISSED APPROACH
PROFILE 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 20° A/S 110 AS MANTAN KCAS (G), A/S 105 KCAS (F). 100 KCAS (B, D) A/S 140K (130K MIN.) CAT C OR D CHECK SINK RATE (APPROX 70% TORQUE, 45 PSI) 500-600 FPM
NOT BELOW CIRCLING MINIMUM
DESCENT ALTITUDE) FINAL CHECK. FLAPS 20°,
CHECK FINAL LANDING TO MAINTAIN AS REQUIRED MAX BANK A/S 125 KCAS MIN. CONFIGURATION.
CAT C OR D 30° COMPLETE LANDING
CHECKLIST
CAUTION WARNING CHECK DESCENT
DO NOT USE SINGLE DO NOT ATTEMPT A PROFILE, LANDING ENGINE REVERSE GO-AROUND WITH CHECK FLAPS 5° (IF ASSURED, GEAR DOWN, THRUST WITH THE GEAR DOWN BELOW INSTALLED.) DO NOT CHECK SINK RATE 500- SIMULATED FAILED 400' AGL OR AFTER DESCEND UNTIL WITHIN 600 FPM ENGINE POWER LEVER 20° FLAPS ARE 30° OF RUNWAY