THRUSH S2R-H80 - Page 2

S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL
REV.
PAGE
DESCRIPTION OF REVISION
BY:
AFM H8001 SINGLE & DUAL COCKPIT Revision C Page ii
FAA APPROVAL DATE: 09/03//2015
LOG OF REVISIONS
NOTE: Re-formatting and correction of typographical errors is not considered revision. True revisions are indicated
by a dark vertical line at the right margin of the line revised.
REV.
PAGE
DESCRIPTION OF REVISION
BY:
IR
ALL
New Document Initial Release.
Melvin D Taylor
Manager Federal Aviation
Administration Aircraft
Certification Office
Atlanta, GA
July 2, 2013
A
A
(cont)
ALL
Cover
ii
v-vi
SECT 1:
pg 6
pg 9
pg 11
pg 12
pg 14
SECT 2:
pg 24
pg 27
pg 28
SECT 4:
pg 59
SECT 5:
pg 66:
pg 72
Added Document Control “# AFM H8001 SINGLE & DUAL COCKPIT” to document.
Replaced the picture to reflect an S2R-H80 model airplane.
Updated Log of Revision to reflect Revision A.
Log of Effective Pages: updated for revised page numbering & all pages affected due to
Document Control # added.
Corrected Sub-section/Paragraph Numeration t/o Section 1.
SECTION 1.5: Changed Max Landing Weight to 7600 Lbs. per FAA Project #
TD12022AT-A.
SECTION 1.11.1: Corrected placard (h) to (…”UNLESS HEADED OUT OF THE
WIND…”). Per FAA request.
Removed placard for SC/SC airplane(“HOPPER RINSE TANK MUST BE FULL WHEN
REAR COCKPIT IS OCCUPIED BY A CREWMEMBER”). Per FAA Request.
SECTION 1.11.2: revised wording for Dual Cockpit/Single Control Placards to alleviate
reference to placard not intended for Single Cockpit/Single Control Aircraft.
SECTION 1.11.2.d: Corrected placard to (…”UNLESS HEADED OUT OF THE
WIND…”). Per FAA request.
Added placard dd, ee, and ff for new fuel filter bypass circuit breaker.
Deleted instructions to check fuel filter bypass as it cannot be done due to location of
the fuel filter. Letter g.
SECTION 1.11.3: Revised wording for Dual Cockpit/Dual Control.
Removed placard (“PASSENGER OR CARGO- 200 LBS. MAX”)
No Substantiation to Designate Rear Cockpit As Cargo Area.
SECTION 1.11.3.h: Corrected placard to (…”UNLESS HEADED OUT OF THE
WIND…”). Per FAA request.
SECTION 1.12: Revised “Kinds of Operations” table to clearly designate front cockpit
instruments; also clearly define required items by coloring.
Added check for the fuel filter bypass light: Press to test.
Added a definition for the “FUEL FILTER BYPASS” light and to land as soon practicable
if illuminated signaling a restricted fuel filter.
SECTION 2.4: Revised “Dry Motoring Run” Definition per GE-H80-100 Operation
Manual 0983302.
SECTION 2.8: Corrected “Note” allowing the engine to stabilize for a period now a
minimum of 5 minutes, was 3 minutes.
SECTION 2.9: Added “Engine Re-Start Procedures On The Ground” per GE-SB-H80-
100-80-0005 Per FAA request.
SECTION 4.5: Added chart for reduced weight takeoff distance, inadvertently omitted
from Revision IR.
SECTION 5.1: Changed Max Landing Weight back to 7600 Lbs. FAA Project #
AT12022AT-A, also referenced in CG range.
SECTION 5.5: Change Max Landing Weight back to 7600 lbs.
Bruce S. Remick
For Manager Federal Aviation
Administration Aircraft
Certification Office
Atlanta, GA
DATED: Aug 5, 2014