THRUSH S2R-H80 - Page 5

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