S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL
AFM H8001 SINGLE & DUAL COCKPIT Revision B Page v
FAA APPROVAL DATE: 3/19/2015
SECTION 3: EMERGENCY PROCEDURES........................................................................................................30
3.1. INTRODUCTION........................................................................................................................................30
3.2. DEFINITION OF EMERGENCY TERMS....................................................................................................30
3.3. EMERGENCY BASIC RULES ...................................................................................................................30
3.4. MVP-50T ANNUNCIATION LIGHTS..........................................................................................................30
3.5. GROUND ENGINE FIRE............................................................................................................................33
3.6. IN-FLIGHT ENGINE FIRE..........................................................................................................................33
3.7. EMERGENCY HOPPER DUMP.................................................................................................................34
3.8. ELECTRICAL FIRE IN-FLIGHT.................................................................................................................34
3.9. 3.9 ENGINE FAILURE IN-FLIGHT.............................................................................................................34
3.10. ENGINE FLAMEOUT.................................................................................................................................36
3.11. FAILURE OF AUTOMATIC FUEL SCHEDULING.....................................................................................36
3.12. AIR STARTS..............................................................................................................................................37
3.13. ABORTED TAKE-OFF...............................................................................................................................39
3.14. FORCED LANDINGS.................................................................................................................................40
3.15. EMERGENCY EGRESS.............................................................................................................................41
3.16. ELEVATOR TRIM/ RUDDER CENTERING SPRING FAILURE................................................................41
3.17. NOSE BAGGAGE DOOR OPENING IN FLIGHT ......................................................................................41
3.18. LOSS OF HOPPER RINSE BALLAST IN THE DUAL...............................................................................41
3.19. SUSPICION OF HOPPER RINSE TANK LEAKING..................................................................................41
SECTION 4: PERFORMANCE .............................................................................................................................42
4.1. INTRODUCTION........................................................................................................................................42
4.2. AIRSPEED CALIBRATION........................................................................................................................44
4.3. STALLING SPEED VERSUS AIRCRAFT WEIGHT ..................................................................................49
4.4. INSTALLED ENGINE HORSEPOWER......................................................................................................52
4.5. TAKEOFF DISTANCE TO 50 FEET ABOVE GROUND LEVEL ...............................................................57
4.6. CLIMB PERFORMANCE ...........................................................................................................................60
4.7. LANDING DISTANCE FROM 50 FEET ABOVE GROUND LEVEL .........................................................63
SECTION 5: WEIGHT & BALANCE...........................................................................................................................66
5.1. WEIGHT & BALANCE PROCEDURE .......................................................................................................66
5.2. S2R-H80 SINGLE AND DUAL COCKPIT C.G. ENVELOPE.....................................................................67
5.3. WAM - EXAMPLE......................................................................................................................................68
5.5. USING FORWARD BALLAST TO MANAGE AFT EMPTY CG POSITION FOR THE DUAL COCKPIT
CONFIGURATION. ...................................................................................................................................72
