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
ABOVE FLIGHT IDLE SELECTED CENTERLINE A-130
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