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Old 10th Nov 2004, 02:07
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downwind
 
Join Date: Aug 1998
Location: australia
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Guy's:

My 2 cents worth!!!!!

MISSED APPROACH/GO-AROUND – ONE ENGINE INOPERATIVE

1. PF “GO-AROUND FLAP 1” (SIMULTANEOUSLY SELECT TO/GA AND MAX CONT THRUST) LOOKING FOR APPROX 12.5° BODY ANGLE
2. PNF “POSITIVE RATE”
3. PF “GEAR UP, CHECK THRUST” PNF “THRUST SET”
4. PF “HDG SELECT” @ 400 AGL
5. ACCELARATION ALT 1000 FT AGL
6. LIMIT BANK ANGLE TO 15 DEGREES UNTIL MANEUVERING COMPLETE
7. ACCELERATE TO FLAP RETRACTION SPEED BY REPOSITIONING THE COMMAND SPEED TO MANEUVERING SPEED FOR THE DESIRED FLAP SETTING

THE MISSED APPROACH WITH AN ENGINE INOPERATIVE SHOULD BE APPLISHED IN THE SAME MANNER AS A NORMAL MISSED APPROACH EXCEPT USE FLAPS 1 FOR THE GO-AROUND FLAP SETTING. AFTER TO/GA IS ENGAGED, THE AFDS INITIALLY COMMANDS A GO-AROUND ATTITUDE, THEN TRANSITIONS TO MAINTAIN COMMAND SPEED AS THE RATE OF CLIMB INCREASES. THE PILOT MUST CONTROL YAW WITH RUDDER AND TRIM. SOME RUDDER PRESSURE MAY BE REQUIRED EVEN WITH FULL RUDDER TRIM. SELECT MAXIMUM CONTINUOUS THRUST WHEN FLAPS ARE RETRACTED.

ENGINE FAILURE DURING MISSED APPROACH/GO-AROUND

1. PF “GO-AROUND FLAP 15” (SIMULTANEOUSLY SELECT TO/GA AND MAX CONT THRUST) LOOKING FOR APPROX 12.5° BODY ANGLE
2. PNF “POSITIVE RATE”
3. PF “GEAR UP, CHECK THRUST” PNF “THRUST SET”
4. PF “HDG SELECT” @ 400 AGL
5. ACCELARATION ALT 1000 FT AGL
6. LIMIT BANK ANGLE TO 15° UNTIL MANEUVERING COMPLETE
7. ACCELERATE TO FLAP RETRACTION SPEED BY REPOSITIONING THE COMMAND SPEED TO MANEUVERING SPEED FOR THE DESIRED FLAP SETTING

IF AN ENGINE FAILS DURING GO-AROUND, PERFORM NORMAL GO-AROUND PROCEDURES. VERIFY MAXIMUM GO-AROUND THRUST IS SET. MAINTAIN FLAPS 15, VREF 30 OR 40 + WIND CORRECTIONS (5 KNOTS MINIMUM) SPEED AND LIMIT BANK ANGLE TO 15° UNTIL INITIAL MANEUVERING IS COMPLETE AND A SAFE ALTITUDE IS REACHED. ACCELERATE TO FLAP RETRACTION SPEED BY REPOSITIONING THE COMMAND SPEED TO MANEUVERING SPEED FOR THE DESIRED FLAP SETTING AND ADJUSTING PITCH. RETRACT FLAPS ON THE NORMAL FLAP/SPEED SCHEDULE.

THE MISSED APPROACH WITH AN ENGINE INOPERATIVE SHOULD BE ACOMPLISHED IN THE SAME MANNER AS A NORMAL MISSED APPROACH EXCEPT USE FLAPS 1 FOR THE GO-AROUND FLAP SETTING. AFTER TO/GA IS ENGAGED, THE AFDS INITIALLY COMMANDS A GO-AROUND ATTITUDE, THEN TRANSITIONS TO MAINTAIN COMMAND SPEED AS THE RATE OF CLIMB INCREASES. THE PILOT MUST CONTROL YAW WITH RUDDER AND TRIM. SOME RUDDER PRESSURE MAY BE REQUIRED EVEN WITH FULL RUDDER TRIM. SELECT MAXIMUM CONTINUOUS THRUST WHEN FLAPS ARE RETRACTED.

ENGINE FAILURE ON FINAL APPROACH

IF AN ENGINE FAILURE SHOULD OCCUR ON FINAL APPROACH WITH FLAPS IN THE LANDING POSITION, THE DECISION TO CONTINUE THE APPROACH OR EXECUTE A GO-AROUND SHOULD BE MADE IMMEDIATELY. IF THE APPROACH IS CONTINUED, RETRACT THE FLAPS TO 15 AND ADJUST THRUST ON THE OPERATING ENGINE. SPEED SHOULD BE INCREASED TO 15 KNOTS OVER THE PREVIOUSLY SET FLAPS 30 OR 40 VREF. THIS IS EQUAL TO AT LEAST VREF FOR FLAPS 15.
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