Appendix А Figure C-12a
GEAR AND FLAP EXTEND SCHEDULE (F+ AND G+ ARE MODIFIED BY S/R10) GEAR B, D, F, F+: 160 KCAS G, G+: 170 KCAS FLAPS 5° 20° 40° G: NOT MODIFIED BY S/R10 146 KCAS 146 KCAS 120 KCAS G+: MODIFIED BY S/R10 175 KCAS 146 KCAS 120 KCAS F: NOT MODIFIED BY S/R10 140 KCAS 140 KCAS 120 KCAS F+: MODIFIED BY S/R10 175 KCAS 140 KCAS 120 KCAS B, D 140 KCAS 140 KCAS 120 KCAS A-110
Appendix A Figure C-13 MU-2B B, D (-10), F (-20), G (-30)
EMERGENCY DESCENT (HIGH SPEED) *CLEAR AREA, CRUISE POWER LEVERS F/I. NOTE
CONFIGURATION START CONDITION LEVERS T/O DECREASE INDICATED AT ASSIGNED ALTITUDE. AND LAND SYNC OFF. AIRSPEED BY 5 KCAS A/S 150 KCAS MIN. BELOW 250 KCAS, FOR EACH 1,000 FT ABOVE 21,300 FT
SIMULATE EXPLOSIVE
DECOMPRESSION AT DECLARE EMERGENCY ASSIGNED ALTITUDE. OXYGEN MASKS ON. ESTABLISH DESCENT IN A 30° BANK, ACCELERATING TO Vmo (250 KCAS). INITIAL 15-20° NOSE DOWN, REDUCING TO APPROX. 8° NOSE DOWN AS A/S APPROACHES Vmo (250 KCAS).
CHECK 1000 FT *WHILE CLEARING THE AREA, AFTER ESTABLISHING DESCENT, KEEP WINGS ABOVE LEVEL
COORDINATE WITH AIR TRAFFIC CONTROL LEVEL, CONTINUE DESCENT ON STEADY HEADING OFF ALTITUDE TO CLEAR TRAFFIC AT LOWER ALTITUDES. OR AS REQUIRED BY ATC 700 FT ABOVE, START
LEVEL OFF COMPLETE EXERCISE AT ASSIGNED ALTITUDE.
REDUCE SPEED TO 200 KCAS A-111
Appendix A Figure C-14 MU-2B B, D (-10), F (-20), G (-30)
UNUSUAL ATTITUDE RECOVERY (NOSE HIGH) UNLOAD AND INITIATE ROLL TOWARD 60° BANK
USING SPOILER AND RUDDER AND ALLOW NOSE TO
FALL THROUGH THE HORIZON
CAUTION
DO NOT G LOAD WINGS DURING BANKING MANEUVER TO PREVENT AN ACCELERATED STALL.
*IF ATOR NEAR STALL BEFORE RECOVERY, DO NOT USE RUDDER TO INITIATE ROLL.
UPON RECOGNITION OF ANOSE
HIGH UNUSUAL ATTITUDE, WHEN NOSE LOW, ROLL WINGS
POWER TO TAKEOFF LEVEL, REDUCE POWER TO
FLIGHT IDLE, AND COMMENCE A
WINGS LEVEL PULL UP TO A LEVEL FLIGHT ATTITUDE.
*CLEAR AREA
ONCE LEVEL, ADD POWER
TO MAINTAIN LEVEL FLIGHT *WHILE CLEARING THE AREA, COORDINATE
WITH AIR TRAFFIC CONTROL TO CLEAR TRAFFIC BOTH ABOVE AND BELOW YOUR ALTITUDE.
INSTRUCTOR NOTE
THE INSTRUCTOR SHOULD INITIATE THE UNUSUAL ATTITUDE NOT TO EXCEED 30° OF PITCH AND/OR 60° OF BANK AND USE POSITIVE
CONTROL TO TRANSFER CONTROL TO THE
STUDENT FOR RECOVERY A-112
Appendix A Figure C-15 MU-2B B, D (-10), F (-20), G (-30)
UNUSUAL ATTITUDE RECOVERY (NOSE LOW)
UPON RECOGNITION OF ANOSE LOW
UNUSUAL ATTITUDE, REDUCE POWER
TO FLIGHT IDLE, INITIATE A ROLL
TOWARD WINGS LEVEL IF IN A BANK, *CLEAR AREA AND MAINTAIN NOSE LOW PITCH
ATTITUDE WHILE LEVELING WINGS
ONCE WINGS ARE LEVEL IN NOSE LOW
ATTITUDE, COMMENCE A WINGS LEVEL PULL UP TO A LEVEL FLIGHT ATTITUDE.
CAUTION *WHILE CLEARING THE AREA, COORDINATE WITH
AIR TRAFFIC CONTROL THE CLEAR TRAFFIC BOTH ABOVE AND BELOW YOUR ALTITUDE.
DO NOT G LOAD AIRCRAFT UNTIL WINGS
ARE LEVEL TO PREVENT AN ACCELERATED STALL. AND UNEVEN G LOADING ON WING IF AIRSPEED IS ATOR NEAR Vmo, DO NOT
USE ABRUPT CONTROL MOVEMENTS DURING RECOVERY.
ONCE LEVEL, ADD POWER
TO MAINTAIN LEVEL FLIGHT
INSTRUCTOR NOTE
THE INSTRUCTOR SHOULD INITIATE THE UNUSUAL ATTITUDE NOT TO EXCEED 30° OF PITCH AND/OR 60° OF BANK AND USE POSITIVE
CONTROL TO TRANSFER CONTROL TO THE
STUDENT FOR RECOVERY A-113
Appendix A Figure C-16 MU-2B B, D (-10), F (-20), G (-30) NORMAL LANDING (20°or 40° FLAPS) TOUCHDOWN. POWER LEVERS RETARD TO FLIGHT IDLE STOP. THEN RETARD BOTH POWER LEVERS TO START (GROUND IDLE). CHECK BOTH PROPS BETA.
THEN REVERSE AND BRAKES AS REQUIRED.
THRESHOLD (10%-20% TORQUE, 10 -13 PSI) PARALLEL TO RUNWAY MAINTAIN TRACK Vref FINAL CHECK. FLAPS 20° or 40°.
A/S SLOWING TO Vref.
CHECK SINK RATE 500-600 FPM
COMPLETE DESCENT AND APPROACH CHECKLISTS A/S 120 KCAS MIN DESCENT. 500-600 FPM (20%-25% TORQUE, 13-16 PSI) (25-30% TORQUE, 16-20 PSI) A/S 150 KCAS MINIMUM. APPROACH BY STABILIZED FLAPS 5° (IF FLAPS 5° INSTALLED), 130 KCAS 500'agl (B,D,F, NOT MOD S/R 10), 140 KCAS (F MOD S/R 10, G) MINIMUM (40-50% TORQUE, 25-32 PSI) 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 8,000 95 98 95 98 100 96 101 98 101 98 103 99 100 103 LANDING ASSURED, FLAPS 20°, A/S 120-130 KCAS 8,500 101 103 100 104 106 106 GEAR DOWN, 500 FPM SINK RATE 8,490 101 104 COMPLETE LANDING (APPROX 25% TORQUE, 16 PSI) 8,930 103 107 CHECKLIST 9,000 106 103 109 109 9,435 108 112 9,500 105 112
10.000 108 115 10,260 109 117 A-114
Appendix A Figure C-17 MU-2B B, D (-10), F (-20), G (-30)
GO AROUND - REJECTED LANDING
AFTER GEAR IS FULLY RETRACTED, IF ACCELERATE TO FLAPS 20° RETRACT FLAPS TO 5°. DESIRED CLIMB SPEED INCREASE PITCH TO APPROX. 10°, A/S 130 MOD S/R10), 130 KCAS (B, D), 140 KCAS (G) KCAS (F, NOT MOD S/R10), 140 KCAS (F, COMPLETE AFTER T/O AND CLIMB CHECKLIST UP AND SELECT FLAPS 20° IF 40° APPLY MAX POWER, PITCH 8° WHEN LANDING REJECTED, A/S 140 KCAS. FLAPS UP.
PREVIOUSLY SELECTED
POSITIVE RATE GEAR UP, IF FLAPS 20°A/S 113 KCAS MIN NORMAL IF 5° FLAPS APPROACH, 120 KCAS (G) MIN.
STABILIZED AND 125 KCAS (B, D, F) MIN.
CONFIGURED FOR
LANDING A-115
Appendix A Figure C-18 MU-2B B, D (-10), F (-20), G (-30) NO FLAP OR 5° FLAP LANDING (ABNORMAL PROCEDURE)
CAUTION DO NOT SELECT REVERSE AS REQUIRED. CHECK BOTH PROPS BETA. BRAKES AND NOTE: BETA MAY NOTE REVERSE UNTIL NOT BE AVAILABLE UNTIL BELOW 90 KCAS LANDING DISTANCE BELOW 90 KCAS WILL INCREASE
WITH NOSE APPROXIMATELY
WHEEL ON TOUCHDOWN - POWER
GROUND LEVERS SLOWLY RETARD TO FLIGHT IDLE. THEN START (GROUND IDLE).
PARALLEL TO RUNWAY MAINTAIN TRACK THRESHOLD: (20% TORQUE, 12 PS/) NO FLAP Vref. 1.25 Vs1 BUT NOT BELOW 110/115 KCAS (SEE CHART) FINAL CHECK. A/S
SLOWING TO NO FLAP COMPLETE DESCENT Vref. (SEE CHART)
AND APPROACH CHECKLISTS A/S 150 KCAS MINIMUM. APPROACH BY STABILIZED 500'agl (25%-30% TORQUE, 16-20 PSI) CHECK LANDING APPROACH SPEEDS NO FLAP OR 5° FLAP LANDING ASSURED, GEAR DOWN A/S 140 KCAS MIN SINK RATE
COMPLETE LANDING CHECKLIST
FOR LANDING APPROACH
SPEEDS SEE TABULAR CHART ON REVERSE SIDE OF FLAPS 0° OR 5º. A/S 130 KCAS MIN.
PROFILE. 500-600 FPM SINK RATE (APPROX 25%-30% TORQUE, 16-19 PSI) A-116
Appendix A Figure C-18a NO FLAP Vref 1.25 Vs1 (BUT NOT BELOW 110 KCAS (B, B+, D, F) 115 KCAS (G)) USE FOR FLAP UP OR 5° B, B+, D, F, G FLAPS UP FLAPS 5° WEIGHT 7,500 110 110 110 110 110 110 110 110
8.000 113 113 113 114 115 110 110 115 8,490 117 110
8.500 117 117 11 18 117 110 110 110 115 8,930 119 119 110 110
9.000 122 119 114 115 9,435 124 117
9.500 115
10.000 118
10.260 128 120 A-117
Appendix A Figure C-19 MU-2B B, D (-10), F (-20), G (-30)
CAUTION ONE ENGINE INOPERATIVE LANDING
SWERVE TOWARD ANTICIPATE RUDDER, MOVE OPERATING ENGINE WHILE MAINTAINING TRACK WITH OPERATING ENGINE TOUCHDOWN, CAUTION WARNING
OPERATING ENGINE POWER LEVER TO START (GROUND POWER LEVER SLOWLY DO NOT USE SINGLE DO NOT ATTEMPT A
WHEN ENTERING IDLE), CHECK PROP BETA, REVERSE RETARD TO FLIGHT IDLE ENGINE REVERSE GO-AROUND WITH BETA AND BRAKES AS REQUIRED. STOP THRUST WITH THE GEAR DOWN BELOW SIMULATED FAILED 400' AGL OR AFTER APPROXIMATELY ENGINE POWER LEVER 20° FLAPS ARE 1500 FT AGL ABOVE FLIGHT IDLE. SELECTED THRESHOLD: (10%-20% TORQUE 10-13 PSI). Vref. A/S 110 KCAS (G), 105 KCAS (F), 100 KCAS (B, D)
PARALLEL TO RUNWAY MANTAN TRACK CHECK SINK RATE 300-600 FPM FINAL CHECK. FLAPS 20°.
COMPLETE DESCENT AND A/S Vse MIN. (SEE CHART)
APPROACH CHECKLISTS AND COMPLETE LANDING CHECKLIST,
REVIEW SINGLE ENGINE LANDING RUDDER TRIM CENTERED, HOLD
CHECKLIST BALLIN CENTER WITH RUDDER A/S 150 KCAS, 140 KCAS MIN (G), 135 APPROACH BY STABILIZED (APPROX 60%-70% TORQUE, 32-38 PSI) KCAS MIN (F),130 KCAS MIN (B,D) - AS REQUIRED 500'agi CHECK
SINK RATE, 500 - 600
FEET PER
B, D/F/ G MINUTE
FLAPS SO IF FLAPS SPINSTALLED FLAP SETTING UP 130 / 135 / 140 Vxse (KCAS) 135 / 150 / 150 Vvse (KCAS) 130 KCAS MIN (F, NOT MOD A/S 130 KCAS MIN (B, D) 20° 5° 115 / 130 / 130 100 / 125 / 125 120 / 140 / 140 105 / 130 / 135 S/R10), 140 KCAS MIN (F, MOD S/R10), 140 KCAS MIN (G). LANDING ASSURED. CHECK GLIDE PATH, GEAR DOWN.
(APPROX 40% TORQUE, 26 PSI) A-118
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