American Champion 8KCAB Technical specifications

AIRPLANE FLIGHT MANUAL - MODEL 8KCAB
IFM-605
FAA APPROVED
Page l of31
REVISED: 6-17-2013
AMERICAN CHAMPION AIRCRAFT CORPORATION
ROCHESTER, WI 53167
FAA Approved
Airplane Flight Manual
American Champion Model 8KCAB
Lycoming AEI0-390-A1B6
This flight manual applies to 8KCAB aircraft beginning with serial number 1116-2012 and
up equipped with a Lycorning
AEI0-390-AlB6 engine, MTV-15-B-C/C193-25 propeller
and 4-2139 alurninum gear legs.
REGISTRATION NUMBER:
OG"-A>(T
SERIAL NUMBER: 1132-2013
THIS MANUAL IS PART OF THE REQUIRED EQUIPMENT
AND MUST REMAIN IN THE AIRPLANE AT ALL TIMES.
This AFM distinguishes F AA approved data from unapproved data by noting "F AA
APPROVEp" in the upper right hand corner of each page containing such FAA approved
data. Additional informafion
is provided by Arnerican Champion Aircraft Corporation and
is included as unapproved sections of the manual.
APPROVED: f ~ 11 J1!f ZL. ~
For: 1 Timothy Smyth ~
Manager, Chicago Aircrafr.edt'ification Office
Date: FEB ®3 ltHS
Record of Revisions
Revision
By
Description Date Pages Affected
New
JJB Original Issue 12-1-2012 All
A JJB Was ICAO Annex 16, Vol. I, App. 6 6-17-2013 1 and 19
Neues Wiegebaltt
8.Spt..2017
e
EAR

AJRPLANE FLIGHT MANUAL - MODEL 8KCAB
FM-605 FAA APPROVED
Page 2
of3 I
ISSUED: 12-1-2012
1.0
1.1
1.2
1.3
1.4
1.5
1.6
1.7
1.8
1.9
1.10
1. I1
1.12
1.13
1.14
2.0
2.1
2.2
2.3
2.4
2.5
2.6
2.7
2.8
2.9
2.10
2.11
2.12
2.13
2.14
2.15
Table of Contents
Operating Limitations.„.„ .... „.„ „. „ .. „ ............... „. „ „ „ „ .......... „ „. „„ ........ „ ....... „. 4
Airspeed Lirnitations .......„„ „
•. „.„ .. „ „.„....„........„...„ ... „. „. „. „ .... „ .... „.......... 4
Airspeed Indicator Markings .„„ „ „. „ ..... „ .. „.„ ••. „ ......... „ „. „. „ ......... „......„ ... „ 4
Powerplant Lirnitations.„.....„
•• „............................„ .. „ ....... „...............„ .. „ •.. „ 5
Powerplant Instrument Markings .. „ ................... „ ..... „„. „. „ ••• „„........„ •••.••.•• „ 5
Miscellaneous Instrument Markings.......................„ ... „...„ ............. „ .•••.. „ .... „ 5
Weight Limits...„ ...... „.„ .. „.....„...„...............„ .•• „....„ .... „... „.„.„ ..... „ ... „.„ ..... 5
Center of Gravity Limits...„„...„ .. „. „. „ •••. „....„........„ •••• „„ „„ .„ .. „........ „„ ...... 6
Maneuver Limits ..........„. „. „ „ ...... „ .. „„ .. „ .. „ „ .... „... „ „„„.„.„ ..... „ „ ........ „ .... „ 6
Flight Load Factor Limits.„ „. „. „....„ .... „. „ ...•.... „ ...... „ ... „. „„ „„ „ .. „ „ ......•...... 7
Kinds
of Operation .......... „. „ „. „ .. „ ...... „ ... „ „ .... „.... „„ „.......„„ „. „...„ •.........•.. 8
Fuel Limitations .........„..... „„ .. „ .• „ .. „.............................„..„ .. „ „. „ „„ ...•......•.. 8
Outside Air T emperature Limits ........„„ „ „. „.„ ........ „ „ •.•... „ „ „.„....„ ..• „ ......... 8
Types of Surface „ ..... „ „ ... „ .. „ .. „...................„.„ .„ ............. „. „.....„......„....„ „ 8
Required Placards...„ .... „. „ .. „„........„„ ....... „.„. „ „ .... „ „...„„ „ .. „„ .. „.....„....„ .. 8
Emergency Procedures .. „. „ .. „. „„„...„ ............... „ ..... „.....„ „.„ ... „....„ „ .. „. „...... 10
Emergency Airspeeds „ .. „ „ .. „ „ ... „.....„„ •...... „ .... „ .. „.„„ .. „ ... „....„....„....„„ .. 10
Engine Failure During TakeoffRoll.„ .. „ ....•.. „......„.....„..... „„ .. „.„ .... „.„ .. „ .. 10
Engine Failure Irnrnediately After Takeoff .. „... „. „....„ „.„ „...„ „.„.........„...... 10
Engine Failure During Flight (Restart Procedure) .„.„„„ „. „.„.„ „. „...„...„.„.. 10
Precautionary Landing With Power ..........„.„....„.........„ .... „.„....„„.....„.„... 10
Forced Landing without Engine Power „„ .. „.„ .. „.„„„ .. „„„„ .. „„„ ... „.„.„ ... „. 11
Engine Fire - Start .„„. „ .. „.„.„.„ .. „.„ .. „.„ ... „ .. „.......„ .. „ .. „„ .. „„„„„ ... „.„ ..... 11
Engine Fire - Ground .....„ .. „.... „„ ....„.....„.....„...„........„ .. „„ .. „„ .... „ .. „„.„„. 11
Engine Fire - In Flight ......„ „„„ „ .... „ .. „....„...„..................„„„.............„ .. „ .. 11
Electrical System Malfunction „ ...... „. „„......„.„............„......„ „. „......„.„ .. „ .. 12
Electrical
System Fire.„„...„„... „. „„....„ .. „...„ .. „.„.......„ .. „ ..... „„........„....... 12
Emergency Exits ...„„...„„.....„.„ .. „ .. „.„......„.......„...„.„„...„...„ .. „ •••.••• „..... 12
Loss of Governor Control .. „.„.„ ... „.„.„ ...... „.„„ .. „ .. „ ... „„ ... „.„ ..... „„„.„ ...„ 12
Fuel
Pressure Loss ..........„... „. „ .. „.„...„......„ .. „.„.............„„.......„.............. 12
Spin Recovery .........„..... „„ ... „.„„„ ........................„... „....„.....„.................. 12
3.0
3.1
3.2
3.3
3.4
3.5
3.6
3.7
3.8
3.9
3.10
3.11
Normal Procedures .„ ......„ .. „„„.„ ... „.„„.„.„ ......„.....„.........„.... „„ .. „.......„..... 13
Pre-Flight Check (See Page 14)„„ ......„ ..... „....„.............„ .. „ ... „........ „.„ ....„ 13
Pre-Start Check ...........„.„...„ „. „.„.„....„ .... „....„............„ ... „...„ .. „.............. 14
Engine
Start „ „....„ „........„......„„ .... „....„...........................„.„..........„ .. „..... 15
Cockpit (Before Flight) ...„ .. „.„ „ .. „. „ „ „ „...„„.......„.....„....„.„„„....„....„ ..... 16
Engine
Run-Up ..... „.„„ .....„ .. „.......„....„....„ .•..•••••••••.•.• „ .. „ .. „ .. „......„ .. „ ...•. 16
Takeoff (Normal) „...„.......................„....„....„......„.....„ .. „.„ .. „„ .. „ .. „ .. „„ ... 16
Takeoff (Short Field)...„ „ .. „ ... „. „.....„ .. „„........„. „.....„ .. „„ .. „„ „. „.... „.„ „ .... 16
Clirnb ...„....„...
„.„ .. „ .. „..... „.„.„ .. „...„..... „„.„ .......„........ „.„ ..... „„„„„„„ ..... 16
Cruise ..........„ .. „„ ...........„ .. „ .. „„.„ .. „....................... „.„ .. „......„.................. 17
Landing (Normal)...„.....„.....„
.. „............„.....„ .... „...„......„...... „.„„ .. „.„ ...... 17
Landing
(Short Field) ..........„ .. „ „.....„ .. „ „........... „. „.......„ .. „ .. „„ .. „ „ •....••.• „ 17

AIRPLANE FLIGHT MANUAL - MODEL 8KCAB
FM-605 FAA APPROVED
Page 3
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ISSUED: 12-1-2012
3.12
3.13
3.14
3.15
3.16
3.17
3.18
3.19
3.20
3.21
3.22
4.0
4.1
4.2
4.3
4.4
4.5
4.6
4.7
4.8
Balked Landing ..............„.............„.............„........................................„........ 17
After Landing ............„.......
„. „„ .. „„.......„„.......................„...................„........ 17
Shut Down and Securing Aircraft „„ „„„„„„„„„„„„„„„„„ „. „„„„„„„„„„„„ „. 18
Alternate Air „„ „. „. „ „. „. „„„„ „ „. „ „. „„ .. „ „. „„„„„„...... „. „. „„ „. „„ „. „„„„. „. „. 18
Fuel Pump „„„„ „. „. „ „. „ „. „„„„ „. „ „. „ „. „„„„„„„„„ „. „. „„ .. „„ „. „„„„„„„„ „. „. 18
Detuning.„..................................„„ ....„...............„.........................„.....„......... 18
Acrobatic Operation .. „„„„„ .. „„ „„„„ „. „„„„„„„„.„„„„ .. „ „. „. „„„„„ „. „„„„„„18
Spins................................................................................................................. 19
Maximum Demonstrated Crosswind „„„„„„„„„„„„„. „„„„„ „. „„„„„„„„„„ „. 19
Turbulence Penetration Speed „„„„„„„„„„„„„„„„„„„„„„„„„„„„„„„„„„„ „. 19
Noise Characteristics .......„..........„ .... „......„.....„...........„.............„ .. „ ... „........ 19
Performance Information .....„......„ .. „....„ ... „.......„..........................„......„„........ 20
Airspeed Calibration .„ ....„.......„ .. „....„ .. „............................................„.....„„.20
Stalling Speeds„ ... „ ... „....„...........„....„ .. „.....„...................„....................„.„ ... 20
Best Glide Speed and Distance „ .. „ .. „....„„..........................„ .. „.„.........„.„..... 20
Climb Rate and Gradients................................................................................ 21
TakeoffDistance ..........„....„.....„„.....„ ... „ ... „....................„.............. „-„.„ .. „.„21
Time, Fuel, and Distance to Climb „„„„„„„„„„„„„„„„„„„„„„„„„„„„„„„„„22
Cruise Performance ... „.....„.......................... „. „............................„.............. „. 23
Landing Distance ........................„.........„....„....„„...........„„......... „. „.....„...... 24
5.0 Loading Information ..............................„
.. „............................„.......... „. „. „......„ 25
5.1
5.2
5.3
5.4
Weight and Balance .....„...........„.„ .. „....„.„„„ .. „ .. „........„........„.„ .. „.„„„ .. „ ... 25
Moment and Loading.......„ .. „ ... „.„........„....„ ... „„.....„...„.................„............ 25
Equipment„.... „ .. „............„„.......„ ... „ ... „.„ .. „ ... „......„........„....„.„.„ .. „........... 25
Equipment List.................„ .. „.........„....................................................„......... 28

AIRPLANE FLICHT MANUAL -MODEL 8KCAB
FM-605
1.0 Operating Limitations
FAA APPROVED
Page 4
of 31
ISSUED: 12-1-2012
This section contains operating limitations, instrument markings, and placards necessary
for the safe operation
ofthe airplane. The Federal Aviation Administration has approved
the operating limitations section. Observance
of these operation limitations is required by
Federal Aviation Regulations.
1.1 Airspeed Limitations
Speed CAS IAS Remarks
(mph) (mph)
Never Exceed 200 207 Do not exceed this speed in any
VNE
operation
Maximum Structural Cruising 160 162 Do not exceed this speed except
V
No
in smooth air and then only with
caution
Normal Category Maneuvering 110 110 (1950lb)
Do not make füll or
VA
abrupt control movements above
this speed
Acrobatic Category Maneuvering 134 135 (1800lb)
Do not make füll or
VA
abrupt control movements above
this speed
1.2 Airspeed lndicator Markings
Marking Value or Range Significance
(mph)
Green Are 58-160
Normal operating range, extends
from
power-off stall speed (Vs1)
to maximum structural cruising
speed
(VNo)
Yellow Are 160-200 Operate with caution and only in
smooth air, extends from
maximum structural cruising
speed (V
No) to never exceed
speed
(VNE)
Red Radial Line 200
Maximum speed for all
operations, never exceed speed
(VNE)

AIRPLANE FLICHT MANUAL -MODEL 8KCAB
FM-605 FAA APPROVED
Page 5
of 31
ISSUED: 12-1-2012
1.3 Powerplant Limitations
Engine Lycoming AEI0-390-A1B6
Engine Operating Limits 2700 rpm (210 hp) for all operations
Oil Pressure Minimum 25 psi, Maximum 100 psi
Fuel Pressure Minimum
14 psi, Maximum 45 psi
Propeller
MT Propeller MTV-15-B-C/C193-25
Diameter: 75.75 to 76.25 in
Fuel Grades
100 (Green) or IOOLL (Blue)
Oil Grades Lycoming SI-1014
1.4 Powerplant Instrument Markings
Tachometer Green Are
Red Radial
Manifold Pressure Red Radial
Cylinder Head Temperature Green Are
Red Radial
Oil Temperature Green Are
Red Radial
Oil Pressure Green Are
Yellow Are
Red Radial
Fuel Pressure Green Are
Red Radial
1.5 Miscellaneous Instrument Markings
Accelerometer
Vacuum Gauge
Fuel Quantity
1.6 Weight Limits
Normal Categorv
Gross Weight
Maximum Baggage
Acrobatic Category
1 Gross Weight
1 Maximum Baggage
Green Are
Yellow Are
Red Radial
Green Are
Red Radial
Red Radial
1950 lb
100 lb (71.0 in aft of datum)
1800 lb
Baggage Prohibited
500-2700 rpm
2700 rpm
29 in-Hg
200°-465° F
465° F
100°-235° F or 120°-235° F
235° F
60-100 psi
25-60 psi
25 psi, 100 psi
14-45 psi
14 psi, 45 psi
-1.52 to 3.8 g
-5.0 to -1.52 g, 3.8 to 6.0 g
-5.0 g, 6.0 g
3.5 to 5.0 in-Hg
3.5 in-Hg, 5.0 in-Hg
E (1.5 Gallon Each Tank)

AIRPLANE FLIGHT MANUAL -MODEL 8KCAB
FM-605
1. 7 Center of Gravity Limits
Normal Categoa
FAA APPROVED
Page 6 of31
ISSUED: 12-1-2012
Center of Gravity Range +14.7 in to +18.5 in at 1950 lb
Reference Datum
Acrobatic
Catego!}'.
Center of Gravity Range
Reference Datum
1.8 Maneuver Limits
Normal Catego!}'. Maneuvers
+11.5 in
to +18.5 in at 1550 lb or less
Straight line variation between points given
Wing Leading Edge
+13.5 in to +18.5
in at 1800 lb
+11.5 in to +18.5
in at 1550 lb or less
Straight line variation between points given
Wing Leading Edge
No acrobatic maneuvers, including spins, are authorized.
Acrobatic
Categoa Maneuvers
The following maneuvers are approved. Variations
and combinations ofthe maneuvers
are also approved, provided that the speed and load factor limitations are not exceeded.
Tailslides and lomcevaks are not approved.
Proper use and application of controls and rnaneuvering load factors are essential to speed
control. Improper and/or inadequate application
of maneuvering load factors rnay result
in rapid acceleration resulting in unsafe flight situations.
Maneuver Aresti Symbol Entry Speed Remarks
IAS (mph)
---
Enter Full Power, Pull or Push: ± 4 G
il
; ' ' ' ' Speed at Top: 50
MPH
Loop -Up , ' 140
' '
' ' Exit Pul! or Push: ± 4 G
' ,
·--~~'"<...--~~---!
Speed at Exit: 140 MPH
Enter 70 MPH or Slower, Power Off
; ' '
·--o--<
Pul! or Push: -± 4 G
, '
'
Loop -Down ' 70 Speed at Bottom: 150 MPH
' '
' ,
... __ „ ...
Full Power, Pull or Push: ± 4 G
Exit 50 MPH
ImmeIman
:j
145
Enter Full Power, Pull: +4 G
Exit 50MPH
--- .... , Enter 70
MPH or Slower, Power Off
English Bunt ' 70 Push: -4 G
'
,
1-----'"
Exit 150 MPH

AIRPLANE FLIGHT MANUAL -MODEL 8KCAB
FM-605
.Maneuver Aresti Symbol Entry Speed
IAS (mph)
d
~
1
1
1
Hammerhead 1 140
1
1
·--J
1---
Slow or )
Barrel Roll •
~
1 • 1 130
Snap Roll
~
·-----·-----<
90
Inside -
Outside
()<J_
140
Eight •
Vertical Roll -
s·
Up
180
.__,
1
Vertical Roll -1
1
--1- 60
Down 1
1
1
'----<
Spin -----i
·--t
Upright or i
~
Stall
Inverted 1
:
'----<
---1
1.9 Flight Load Factor Limits
Enter
Exit
FAA APPROVED
Page 7
of31
ISSUED: 12-1-2012
Remarks
Full Power, Pull or Push: ± 4 G
Speed at Turn: 40 MPH
Pull
or Push: ± 4 G
140 MPH
Use Smooth Application of Controls
No Full or Abrupt Control Movements
Above Maneuvering Speed
(VA)
Enter 90 MPH or Slower, Full Power
Exit: 90 MPH
Enter Full Power, Pull: +4 G
Begin Outside Eight 140
MPH
Push: -4 G
Exit 140 MPH
Enter Pull: + 4 G to Vertical Up
Push: -2 G to Level Upright
Exit 50MPH
Enter 60 MPH or Slower, Power - Idle
Push: -2 G to Vertical Down
Pull: 4 G to Level Upright
Exit 150
MPH
Recover with Full Opposite Rudder and
Positive Movement ofthe Stick to
Neutra! Until Rotation Stops -Then
Neutralize Rudder and Smoothly
Recover from Dive to Level Flight.
Free Release
ofControls is NOT
Adequate for Spin Recovery; Positive
Movement of Controls is Required.
The limit load factors are not to be exceeded during any flight condition.
Normal Category
The Normal Category limit load factors are +3.8g and -1.52g. Normal Category limit
load factors are indicated by the ends
of the green arc on the accelerometer.
Acrobatic Category
The Acrobatic Category limit load factors are +6.0g and -5.0g. Acrobatic Category limit
load factors are indicated by the red radial lines on the accelerometer. Load factors
within the yellow arc are permitted in the Acrobatic Category only. The accelerometer
is
required for Acrobatic Category operations.

AIRPLANE FLICHT MANUAL -MODEL SKCAB
FM-605
1.10 Kinds of Operation
FAA APPROVED
Page 8 of31
ISSUED: 12-1-2012
Only VFR, day or night, operation is approved. Equipment listed in the Aircraft
Equipment List as
"R" is required to be installed and operational for VFR day or night
flight. Flight into
known icing conditions is prohibited.
1.11 Fuel Limitations
Left and Right Wing Tanks
Total Fuel: 43.0 Gallons; 21.5Gallons
per tank
Useable Fuel: 40.0 Gallons; 20.0 Gallons per tank
Unusable Fuel: 3 .0 Gallons; 1.5 Gallons per tank
A header tank provides fuel for
2. 0 minutes of inverted flight. One minute of positive G
flight is required to completely refill the header tank.
1.12 Outside Air Temperature Limits
Adequate powerplant cooling has been demonstrated for outside air temperatures below
120°F. Remove oil cooler covers when outside air temperature exceeds 40°F.
1.13 Types of Surface
Operations may be conducted from hard surface, grass, gravel, or similar surfaces.
Performance allowances shall be made in accordance with Sections 4.5 and 4.8.
1.14 Required Placards
In Full View
of Pilot
"MANEUVERING SPEED 110 MPH (96 KNOTS) CAS
DEMONSTRATED CROSSWIND VELOCITY 20 MPH (17
KNOTS)"
"SOLO FROM FRONT SEAT ONL Y. NO ACROBATIC MANEUVERS, INCLUDING SPINS,
APPROVED
IN NORMAL CATEGORY. DA Y OR NIGHT VFR OPERATION ONL Y. FLIGHT IN
KNOWN ICING.PROHIBITED. TO RECOVER FROM NORMAL OR INVERTED SPIN, USE FULL
OPPOSITE RUDDER AND NEUTRALIZE ELEVATOR."
"THIS AIRPLANE MUST BE OPERATED AS ANORMAL OR ACROBATIC CATEGORY
AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF
PLACARDS, MARKINGS AND MANUALS. MARKINGS AND PLACARDS (EXCEPT
ACCELEROMETER MARKINGS) REFER TO NORMAL CATEGORY ONLY. SEE AIRPLANE
FLIGHT MANUAL FOR ACROBATIC CATEGORY INFORMATION, WEIGHT AND BALANCE
INFORMATION AND OTHER OPERATING LIMITATIONS."
"NO SMOKING"
"MAGNETIC COMPASS MAY DEVIATE AS MUCH AS 30° WITH PITOT HEA TON" (Heated Pitot)
"SEAT BACK RESTRAINER CABLE MUST BE CONNECTED BEFORE FLIGHT UNLESS
CONTROL STICK
IS REMOVED"

AIRPLANE FLIGHT MANUAL -MODEL 8KCAB
FM-605
In Baggage Compartment
"MAXIMUM BAGGAGE 100 LBS"
On Forward Left Side Window
"DO NOT OPEN ABOVE 130 MPH"
F AA APPROVED
Page 9
of 31
ISSUED: 12-1-2012
"ALTERNATE EMERGENCY EXIT, UNLATCH- FORCE FORWARD PORTION PAST STOP"
On Emergency Door Release
"EMERGENCY DOOR RELEASE, PULL PIN -PULL HANDLE"
Adjacent to Fuel Gauge
"FUEL IN TANK WHEN GAUGE READS 'E' (EMPTY) CANNOT BE SAFELY USED IN FLIGHT"
Above Fuel ShutoffRod
"FUEL 40 GAL USEABLE -DOWN ON"
Adjacent to Fuel Cap
"AVGAS 100 OCTANE 20 GALLONS"
Adjacent to Strohe Light Switch
"TURN OFF STROBE LIGHTS WHEN TAXIING IN VICINITY OF OTHER AIRCRAFT OR DURING
FLIGHT THROUGH CLOUD, FOG, OR HAZE. STANDARD POSITION LIGHTS TOBE ON FOR
ALL NIGHT OPERATIONS."
On Front Seat Rear Leg
"REAR SEAT PIN 7-1500 OR 7-1501 AND REARCONTROL STICK PIN 4-1711 REQ'D WITH THIS
SEAT INSTALLATION" (Adjustable Front Seat)
On Rear Control Stick
"REAR STICK PIN 4-1711" (Adjustable Front Seat)
On Rear Seat Front Leg
"REAR SEAT PIN 7-1500" or "REAR SEAT PIN 7-1501" (Adjustable Front Seat)

AIRPLANE FLIGHT MANUAL -MODEL 8KCAB
FM-605
2.0 Emergency Procedures
2.1 Emergency Airspeeds
Page 10 of3 l
ISSUED: 12-1-2012
Engine Failure After Takeoff.„.„ .. „ .. „ ... „.„„.„.„„ ... „„.„„„„.„„„„ .. 76 mph IAS
Best Glide
(1950lb)„„„„.„„„„„„„„„„„„„„„„„„„„„„„„„„„„„. 70 mph IAS
(1800lb)„„„„„„„„„„„„„„„„„„„„„„„„„„„„„„„
„. „. 68 mph IAS
(1650lb)„„„„„„„.„„„ .. „.„„„.„ ...„„„..... „.„„„„„„„ .. 65 mph IAS
Precautionary Landing with Engine
Power„„„„ .... „„.„„„„„„„„„„. 76 mph IAS
Forced Landing without Engine Power „„„.„„„„„„„„.„ ... „„„„.„ ... 76 mph IAS
2.2 Engine Failure During TakeoffRoll
1) Throttle -idle
2) Brakes -apply
3) Mixture -idle cut-off
4) Ignition switches -
off
5) Master switch - off
2.3 Engine Failure Immediately After Takeoff
If possible land on rernaining runway or land ahead. Do not atternpt to reverse course.
1) Airspeed - 76 mph IAS
2) Mixture -idle cut-off
3) Fuel valve -
off
4) Ignition switches - off
5) Master switch - off
2.4 Engine Failure During Flight (Restart Procedure)
1) Airspeed -80 mph IAS
2) Throttle - Yz travel
3) Alternate air -on
4) Mixture -rich
5) Propeller -füll forward
6) Fuel valve -on
7) Master -on
8) Fuel
pump - on
9) Ignition switches -on
10) Starter -engage (if propeller is stopped)
2.5 Precautionary Landing With Power
1) Speed -76 rnph IAS
2) Master switch - off
3) Door -unlatch prior to touchdown
4) Touchdown -tail low