Beechcraft MUSKETEER 19 Install guide

0
4
SECTION
1
S
SECTION
2
SECTION
3
SECTION
4
SECTION
5
SECTION
6
169
-59001
S
F
Reissued
:
March,
1974
Qeechcraft
MUSKETEE
R
19,
19A,
131
9
23,
A23,
A23A,
B23,
C2
3
24,
A24,
A24R
SPORT
150
B1
9
SUNDOWNER
180
C2
3
SIERRA
A24
R
SIERRA
200
B24R,C24R
SHOP
MANUAL
General
Informatio
n
Servicing
and
Lubrication
Disassembly,
Assembly
and
Maintenanc
e
Electrical
Wiring
Diagram
s
Periodic
Inspection
Schedule
Overhaul
and
Replacement
Schedule
PUBLISHED
BY
PARTS
AND
SERVICE
OPERATION
S
BEECH
AIRCRAFT
CORPORATIO
N
WICHITA,
KANSAS
6720
1
U.S
.A
.
IGAMA
169
-59001
SF
6
Revised
:
December
29.
197
8
U
I-

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8o'37'
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Title
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1975
A
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December
29, 1978 3-19 thru 3-37
Origina
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l
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197
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29,
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3-56 Origina
l
2-18
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F2
December
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3-58k
F2
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21
,
1976
2-21
thru 2-22
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29,
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,
1976
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thru
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A

.
.
ALPHABETICAL
kNDX
A
B
Adj
list
IOC
U
B5and
137
Heading
Loc
k
/Navigation
Couple
r
System
.
.
Illus
.
3-3
6
Fuel
Injection
System
3-56
[die
Speed
And
Mixture 3-5
6
Parking Brake
..
3-5
1
Voltage
Regulator
.
.
3-6
1
Ailero
n
And
Rudder
Rigging
.
3-14
,
Illus
.
3-12,
3-13, 3-15,
3-22
,
3-2
3
Centering
Cable
Modification
.
3-16
Centering
Sprin
g
Rigging
3-16,
Illus
.
3-1
3
Installation
.
3-i
l
Removal
3-1
1
System
3-1
1
Aircraf
t
Dimensions
Of
1-2,
1-3
1-4,
1-
5
Finish
Cleaning
- . .
2-18
Hoisting
.3-2,
Illus
.
3-12
Leveling
3-
2
Storage
3-53
Air
Fillet
-
Central
..
.l-9,2-16
A
Gyro
Instrument
.
1-9,2-1
8
Induction
.
1-7, 1-9,
2-l6A,
Illus
.
2-17
Alternator
Troubleshooting
.
3-6
1
Anchoring
The
Aircraft
.
.
.24
Approved
Spark
Plugs
.
2-1
7
Engine
Oils
.
. .
2-2
3
Autopilot
BEECHCRAFT
New-Matic
3-28
,
Plus
. 3-34
Troubleshooting
Guide
-
3-28
Bleeding
(Cont'd
)
Landing
Gear Hydraulic
System
.
.
.
.
34
9
Brake
Bleeding
Dual
System
.
3-S
I
Gravity Bleeding
.
3-50
Lining
Wear
Limits
.
1-7,3-50
Parking
Adjustment
3-5
1
Pressure
Bleeding
.
3-S
I
Servicing
-
. .
1-7,2-1
0
System
Bleeding
.
.
.
3-SO
Brush
Replacement
Guide
.
.1-
8
B5
and
B7
Heading
Loc
k
/Navigation
Coupler
System
Adjustment
-
Illus
.
3-36
B7
System
Block
Diagram
- . . .
Illus
.
3-35
C
Cabin
Door
Latch
Rigging
.
3-53
Cabin
Window
Replacement
3-5
3
Cable
Modification
,
Aileron
Centering
-
3-16
Cable
Temperature
Tension
Graph
3-15
Cable,
Trim
Replacement
.
3-18
Carburetor
Heat
Contro
l
and Mixture
Contro
l
Cables
Installation
.
.
3-5
4
Centering
Spring,
Contro
l
Column
-
3-16,
1111
.1s .
3-13
Central
Air
Filter,
Gyr
o
Itistrunient
. .
.
1-9,
2-18
Chart
Consumable
Materials
.
2-2
2
Spaik Plug
-
-
-
2-17
Chec
k
I
lard
Landing
. .
3-40
A
Magneto
3-58
Cleanin
g
Aircraft Finish
2-18
Engine 2-18
Engine
Air
Intak
e
Filter
-
1-7, 1-9,
2-16A
,
Illus
.
21
7
Exterior
2-18
Interior
2-18
Plastic
Windows
2-1
8
Consumable
Materials
Chart
2-22
Contact
Point
Clearance
,
Magneto
1
-
6
Control
Column
Centerin
g
Spring
3-16,
Illus .
3-13
Quadrant
Rigging
. .
3-54
B
:
Balancing
The
Control
Surfaces
.
.
3
-25,
Illus
.
3
-2
6
Battery
Servicing
. .
-
.
2-16
Bearing
Replacement,
Nos
e
Strut
.-
3
-41,
Illus
.
341
BEECIICRAFT
New
-Mati
c
Autopilot
.
3
-28,
Illus
.
3-34
BLECIICPAFT
Supplementar
y
Publications
. . .
.
1
-14
Blade
Repair,
"
Pro'
tici
3
-59,
Illus
. 3
-60
itteedmng
Brake
System
3
-50
Dual
Brakes
.
. .
.
3
-51
C
Control (Cont'd
)
Surface
Balancing
. .
3-25
,
Hums
.
3-26
Surface
Travel
. .
1-
8
Syste
m
Rigging
Rudder
-
.
3-20
Rigging,
Stabilator
-
3-18
,
thus
.
3-19
Throttle
Rigging
.
.
.
3-54
,
Illus .
3-54
Converting
Wheels
2-11,
Illus
.
2-12
Corrosion
Preventative
Maintenanc
e
Of
Magnesium
3-38,
344
B
Coupler
Syste
m
B5
and
137
Headin
g
Lock/Navigation
Ad
-
justmemi
t .
....
.....................
....
.....................
....
...........
.3-3
6
Cowling
Modification
-
.
3-55
D
Diagra
m
Block,
B5 System
.
.
3-3
5
Elecincal
Wiring
. . .
.4-
1
Lubrication
...
2-2
1
Servicing
Points
2-13,
2-11,
2-I
S
Stations
2-
2
Dimensions
01
'
Airciati
.l-2,
1-3,
1-4,
1-
5
Door,
Cahimi
I m
tclr
Rigging
.
3-53
Dtfii+Brake
Bleeding
. .
3
.5
1
F
Electric
Flap
3
-24
Rigging
3
-25
Electric
St
:mhilator
Trim
Tab
Actuator
- .
3
-I
6A,
tIles
.
3-16
Electric
Tab
Actuato
r
Installation
.
3
-17,
IHuc
.
3-17
Magnetic
Clutc
h
Installation
3
-17,
lllus
3
-17
Removal
3
-17,
lllua
.
3-17
Renioval
..
3
-17,
JIlu'
3
-17
Torque
Test
3-17
Electric
Trim
Tab
Moto
r
And
Clutch
Assembl
y
Installation
3
-17,
Illus
.
3
-1
6
Removal
3-16A,
Illus
.
3
-16
Electric
Wiring
Diagrams
.
.4
-I
Empennage
.
3
-I
6A,
Illus
.
3-18
Engin
e
Air
Intake
Filter
('leaning
1
-7, 1-9,
2
-l6A
,
Illus
.
2-17
F6

E
Engin'
Cont'd)
Cleaning
.
2-18
Firing
Order
1-
6
,eneral
Information
-
1-
6
Idle
Speed
1-
7
Installation
- -
-
3-54
B
Mount
Preservation
-
-
2-1
8
Oil
Approved
-
2-2
3
Capacity
-
-
1-9,2-10
Filter
- -
1-9,2-1
0
Pressure
1-
7
Preservation
,
-
.
-
3-5
3
Removal
--------------------------------3-54
A
Exhaust
System
. . -
-
3-5
4
Exterior
Cleaning
-
. .
2-18
External
Power
- .
-
.
2-16
F
Fiberglass
Repair
- -
. -
3-59
Film
Gyro
Instrument
Centra
l
Air
-
.1-9,2-16
A
Oil
1-9,2-1
0
Service
Air
intake
.
-
1-7,
1-9,2-16
,
Illus .
2-17
Finishes,
Paint
-
.
-
.
2-19
Firing
Order,
Engine
. .
-
1-
6
Fitting
Torque
Values,
Fue
l
System
1-10,2-6
Flap
Electric
"
3-2
4
Rigging
-
3-2
1
Installation
-
-
3-2
1
Removal
3-2
1
Rigging
3-2
1
Fiared
Fittings,
Lubricatio
n
01
.2-6,
Illus
.
2-6
A
Fuel
Cel
l
Installation
.
3-1
1
Removal
-----------------------------------3-1
0
F
nd
Grades
1-
7
Futi
injection
System
- -
3-5
5
Adjustment
- . -
.
3-56
Troubleshooting
-
.3-55,3-6
3
Dirt in
System
. .
3-55
Fuel Control Leakage
3-5
5
Fuel Quantity
Transmitte
r
Removal
and
Installation
3-1
1
Fuel
Syste
m
I
are
Fitting
Torqu
e
Values
.
. -
1-10,2-
6
Schematic
.
Illus
.
2-7,
2-8,
2-9
ALPHABETICAL
INDEX
F
Fuel
System
(Cont'd)
Selector
Valve
3
-57
Servicing
1
-7,2
-5
Strainers
1
-9,2
-5
Fuel
Tank
Repair
-
-
-
Illus
. 3
-9
Resealing
-
3
-10,
Illus
.
3
-1
0
G
Gear
Bleeding Hydrauli
c
System
-. --
34
8
Housing
to
Pi
n
Measurement
340,
Illus .
34
0
Installatio
n
Main
Landing
-
.
.
3-37
Retractable
.
. -
34
2
Nose
Landing
- . -
3-38
Retractable
..
3-44
Knee
Pin
Servicing
-
1-9,2-1
1
Remova
l
Main
Landing
.
-
3-3
7
Retractable
- -
3-42
Nose
Landing
..
3-3
8
Retractable
. .
34
4
Rigging
-
.
. -
3-44
k
Servicin
g
Up-lock,
Main
-
-
Illus
;
34
6
General
Informatio n
Brake
Lining
Wear
Limits
.
1-
7
Control
Surface
Travel
.
1-
8
Engine
1-
6
Firing
Order, Engine
-
1-
6
Fuel
Grade
1-
7
Idle
Speed, Engine
. .
.
1-
7
Induction
Air
Filter
-
1-7, 1-9 ,
2-16,
Illus
.
2-17
Magnet
o
Contact
Point
Clearance
1-
6
Timing
1-
6
Motor
Brush
Replacemen
t
Guide
-----------------------------------1-
8
Oil
Capacity,
Engine 1-9,2-10
Filler
-
. -
1-9,2-1
0
Pressure
-------------------------------1-
7
Power
Plant
1-
6
Servicing
-------------------------------------1-
8
Stall
Warning
Switch
-
.1-
8
Suction
Relief
Valve
1-8,2-1
6
Table
of
Torques
. .
-
1-
9
Goodyear
Wheels
and
Brakes
,
Replacing
- - - -
2-1
1
Graph,
Cable
Temperatur
e
Tension
3-1
5
Gravity
Bleeding,
Brakes
.
3-50
G
Ground
Handlin
g
Anchoring
2-
4
Jacking
-
.
-
2-3,
Illus
.
2-
3
Parking
Brakes
-
- .
-
2-
4
Towing
24,
Illus
.
2-
4
Guide
,
Autopilot,
Trouble
-
shooting
-
--
3-28
Lamp
Replacement
-
-
2-20
Gyro
Instrument
Filte
r
Servicing
- . -
1-9,2-1
8
H
Hard
Landing
Check
3
-40A,3
-44
A
Heater
Muffler
. - .
-
2
-17
Heating
and
Ventilation
.
-
2-17
Hoisting,
Aircraft
-
3
-2,
Illus
.
3
-2
Housing
to Pi
n
Measurement,
Gear
. .
3
-40,
Illus
.
3-40
Hydraulic
System,
0
Landing
Gear
..
3-48
,
Illus
.
34
7
Landing
Gear
,
Bleeding
.
.
-
.
34
9
Leak
Test
. . .
-
3-48
Pump
Illus
.
3-48A
,
348B,
348C
Idle
Speed
and
Mixture
Adjustment
- - -
3-56
Engine
1-
7
Induction
Air
Filter
. .
-
1-
7
Inspection
Schedule
,
Periodic
--------------------------------------5-
1
Installatio
n
Aileron
3-1
1
Electric
Tab
Actuator
-
3-17
,
Illus .
3-1
7
Engine
-----------------------------------3-54
B
Flap
3-2
1
Flared
Fittings 2-6,
Illus
.
2-6
A
Fuel
Cell
-----------------------------------3-I
I
Magnetic
Clutch 3-17,
Illus
.
3-17
Main
Gear
Side
Brace
-
342
B
Main
Landing
Gear,
Fixed 3-37
Main
Landing
Gear
,
Retractable
.
- .
34
2
Nose Gear
Drag
Brace
.
3-4
4
Nose
Landing
Gear,
Fixed 3-3
7
iv
FB

ALPHABETICAL
INDE
X
0
/
L
Landing
Gear,
Retractable
(Cont'd
)
Corrosion
Preventativ
e
Maintenance
3
-4
6
Hydraulic
System
3
-48,
Illus
.
3
-42A,
3
-4
7
Bleeding
. .
3
-4
9
Leak
Test,
Extension
System
3
-48,
Illus
.
3
-4
7
Leak
Test,
Retract
Syste
m
3
-48,
lIlus
.
342A,
3
-47
Pump
Overhaul
.
3
-48
,
Illus
.
3
-48A,
3
-48B,
3
-48C
Main
Installation
. .
3
-42B
Removal
3
-42B
Main Gear
Side
Brace
Installation
3
-42B
Removal
-
.
3
-42B
Nose
Installation
-3
-44
Removal
3
-4
4
Nose
Gear
Drag
Brace
Removal
.
3
-44
Replacement
3
-4
4
Rigging
3
-44,
Illus
.
3
-43, 345,
3
-4
6
Safety
System
3
-42B
Shock
Absorber
Dis
c
Replacement
3
-40,3
-44
Landing
Gear
Safety
Switch
Adjustment
. -
.
3
-50
Landing
Gear
Warning
Horn
Switch
Adjustment
- -
3
-50
Leading
Edge
Repair
,
Wing
. .
3
-5,
Illus
. 3
-6
Leak
Test
Hydraulic
System
. .
348
Leveling
Aircraft
3
-2
Lubrication
Diagram
.
.
.
2
-21
M
Installation
(Cont'd
)
Nose
Landing
Gear
,
Retractable
...
3-4
4
Propeller
.
-
3-58A,
Illus
.
3-5
9
Rudder
-------------------------------------3-2
0
Stabilator
. .
. .
3-1
8
Stabilator
Tab
.
. .
3-l6
A
Strobe
Light
3-3
7
Vertical
Stabilizer
.
3-20
,
Illus
.
3-21,3-2
4
Windshield
-
.
.
.
3-5
2
Wing
-
.
.
.
3-3,Illus
.3
4
Installing
New
Landin
g
Gear
Strut
To
Wing
. .
3-3
9
Installing
New
Strut
Adapter
t
o
Wing
34
0
Interconnect
Syste
m
Modification
. . .
-
3-1
6
Rigging
3-14
,
Illus
.
3-12,
3-13,
3-15,
3-22,3-2
3
Interior
Cleaning
.
.
.
2-1
8
J
Jack
Pad
Installation
. .
-
2
-3,
Illus
.
2
-3
Jacking
2
-3,
Illus
. 2
-3
K
Knee
Pin
Servicing
-
-
1
-9,2
-11
L
I
Lamp
Replacement
Guide
.
2
-20
Landing
Gear,
Fixed
Corrosion
Preventativ
e
Maintenance
- .
3
-38
Hard
Landing
Check
.
3-40A
Installing
New
Landing
Gear
Strut
to
Wing
. -
3
-39
Knee
Pin
Servicing
.
1
-9,2
-11
Main
Installation
.
.
.
3
-37
Removal
.
.
3
-37
Nose
Installation
-
.
-
3
-38
Removal
3
-38
Nose
Strut
Bearin
g
Replacement
3
-41,
Illus
.
34
1
Shock
Absorber
Rubber
Dis
c
Replacement
340,
Illus
.
34
0
Torque
Knee
Pin
An
d
Bushings
-
.
.
3
-38
Wheel
Aligning
3
-38,
Illus
.
3
-3
9
Landing
Gear,
Retractable
.
34
2
F6
M
Magnetic
Clutc
h
Installation
.
3-17,
Illus
.
3-1
7
Removal
-
3-17,
Illus
.3-1
7
Torque
Test
-
.
. .
3-1
7
Magnet
o
Checks 3-5
8
Contact
Point
Clearance
.1-
6
Timing
.
. -
1-6,3-5
8
Troubleshooting
-
-
-
3-6
4
Magnetos
.
..
3-57,
Illus
.
3-5
7
Main
Gear,
Fixe
d
Corrosion
Preventativ
e
Maintenance
- .
3-3
8
Hard
Landing
Check
.
3-40A
Main
Gear,
Fixed
(Cont'd
)
Installation
-
.
-
.
3-3
7
Installing
New
Strut
Adapte
r
To Wing
. . .
3-4
0
Knee
Pin
Servicing
-
1-9,2-1
1
Removal
3-3
7
Shock
Absorber
Rubber
Dis
c
Replacement
340,
Illus
.
3-4
0
Torque
Knee
Pi
n
and
Bushings
. .
3-3
8
Wheel
Aligning
3-38,
Illus
.
3-3
9
Main
Gear,
Retractabl
e
Corrosion
Preventativ
e
Maintenance
.
-
34
6
Installation
-
.
.
-
3-42
B
Removal
. . .
3-42B
Rigging
3-44A,
Illus
.
34
3
345,3-4
6
Shock
Absorber
Dis
c
Replacement
- -
34
4
Side Brac
e
Installation
-
- .
342
B
Removal
- - .
3-42
B
Maintenanc
e
Rudder
Torque
Tube
-
3-5
1
Materials
Chart
,
Consumable
2-2
2
Measurement
,
Housing
to
Pin
3-40,
Ill
us
.
34
0
Mixture
and
Idle
Spee
d
Adjustment
- - - -
3-5
6
Mixture
Control
and
Carbureto
r
Heat
Control
Cable
s
Installation
.
-
3-5
4
Modificatio
n
Aileron Centering
Cable
3-1
6
Cowling
3-5
5
Rudder/Ailero
n
Interconnect
. .
3-1
4
Motor
Brush
Replacemen
t
Guide
1-
8
Muffler,
I[eater
. . .
-
2-17
N
Nose
Gear,
Fixed
Corrosion
Preventativ
e
Maintenance
.
-
3
-38
Installation
. - - -
3
-38
Knee
Pin
Servicing
.
1
.9,2
-11
Removal
3
-38
Shock
Absorber
Rubber
Dis
c
Replacement
340,
Illus
.
340
Strut
Bearin
g
Replacement
341,
Illiis
.
341
V

ALPHABETICAL
INDE
X
N
Torque
Knee
Pin
And
Bushings
.
3-38
Nose
Gear, Retractabl
e
Corrosion
Preventativ
e
Maintenance
3-46
Drag
Brace
Removal
3-44
Replacement
3-4-
4
Installation
3-4
4
Removal
3-44
Rigging
.
3-44A,
Illus .
3-43
,
3-45,3-4
6
Shock
Absorber
Dis
c
Replacement
. .
3-4
0
Nose
Strut
Bearing
s
Replacement
3-41,
Illus
.
3-4
1
0
Oil
Approved
Engine
.
2-2
3
Capacity
- . . .
1-9,2-10
-ingc
... .
1-9,2-10
I
lite
r
General Information
1-8,
1-
9
Servicing
.
1-9,2-1
0
Pressure,
Engine
.
.
. .
1-
7
System
Servicing
1-9,2-1
0
Overhaul and
Replacemen
t
Schedule
6-
1
P
Paint Finishes
2-19
Parking
Brake
.
..
2-4,3-5
1
PeriudL
Inspection
Schedule
5- 1
Pitot
And
Static
Syste
m
Servicing
. .
2-16,
illus .
2-12
Piasu
.
Window
Cleaning
2-18
Point
Clearance,
Magnet
o
Contact
1-
6
Po,ve
Plant,
Genera
l
Information
1-
6
Pow .'i
Supply,
Strobe
Ligh
t
Installation
3-37
Removal
3-37
Preservatio
n
Ighie
3-53
briginc
Mounts
.
2-1
8
Rjhbcr
Seals
. .
2-1
8
Press
u
Brake
Bleeding
...
3-51
P
Pressure
(Cont'd
)
Engine
Oil
1- 7
Recommended
Tire
.
1
.8,2-1
1
Propelle
r
Blade
Repair
.
3-59,
Illus
.
3-6
0
Installation
.
3-58A,
Illus .
3-5
9
Removal
.
.
3-SSA,
Illus
.
3-59
Publications,
Supplementar
y
BEECHCRAFT
1-1
4
Vendor
1-1
2
R
Regulator,
Troubleshooting
.
3-6
1
Relief Valve,
Suction
1-8, 1-9,
2-16
Remova
l
Aileron
3-1
1
Electric
Ta
b
Actuator
3.16A,
Illus
.
3-16
Magneti
c
Clutch
3-17
.
Illus
.
3-17
Engine
--.
3-54
A
Flap 3-2
1
Fuel
Cell
3-10
Main Gear
Side
Brace
.
3-42
B
Main
Landing
Gear
,
Fixed
.
.
. .
.3-3
7
Main
Landing
Gear
,
Retractable
. .
.
3-42
B
Nose Gear Drag
Brace
.
3-4
4
Nose
Landing
Gear
,
Fixed
.
. .
.
3-3
8
Propeller
. .
3.58A,
thus
. 3-59
Rudder
3-20
Stabilator
. . . .
3-18
Stabilator
Tab
.
.
.
3-16
Strobe
Light
. . - .
3-37
Vertical Stabilizer
. .
3-20,
A
Rigging (Cont'd
)
Aileron
Centering
Spring
3-16
,
Illus
.
3-13
Cabin
Door
Latch
.
.
3-53
Engine
Controls
.
.
3-54
Throttle
Control
.
3-54
,
Illus
.
3-59
Quadrant
Control
.
3-5
4
Flap
3-2
1
Electric
. .
.
3-2
5
Landing
Gear
.
.
3-44
A
Rudder/Aileron
Interconnec
t
System
3-1
4
Illus
.
3-12, 3-13,
3-15,3-22
,
3-23
Rudder
System
.
.
.
3-20
Stab
it
ato
r
Control
System
.
.
3-18
,
Illus
.
3-19
Trim
Ta
b
System
3-20,
Illus
.
3-19
Royalite
Repair
.. . .
3-60
Rubber
Seal
Preservation
.
2-18
Rudde
r
And
Aileron
Rigging
.
3-14
,
Illus
.
3-1
2
Installation
. -
3-20
Removal
3-20
Rigging
3-20
Torque
Tube
Maintenance
3-5
1
Rudder/Aileron
Interconnec
t
Modification
. .
.
3-16
S
Safety
System,
Landing
Gear
3-42B
Schedule
-
Overhaul
And
Replacement
6-
I
Periodic
Inspection
.
-
.5-
I
Schemati
c
Fuel
System
Illus .
2-7, 2-8, 2-
9
Screen,
Suction
Relie
f
Valve
1-9,2-1
6
Selector
Valve,
Fuel 3-57
Servicin
g
Battery
2-16
Brakes
.
.
. .
1-7,2-1
0
Engine Air
Intake
Filter 1-7
,
1-9,2-16,
Illus .
2-1
7
External
Power
. .
.
2.1
6
Fuel
System
.
. .
1-7,2-
5
Gyro
Instrument
Filter
.
1-9
,
2-1
8
Induction
Air
Filter
.
1-7,
1-c)
.
2-16,
Illus
.
2-1
7
Illus
. 3
-2
1
Windshield
- .
.
.
3-52
Wing
. . . .
3-2,
Illus
.
3-
4
Repair of
Fiberglass
. .
-
3-5
9
Repair
of
Royalite
-
.
.
3-60
Replacemen
t
And
Overhaul
Schedule
.
.6-
I
Cabin
Window
. .
.
3-5
3
Guide,
Lamp
. .
.
2-20
Replacing
Goodyear
Wheels
and
Brakes
With
Cleveland
.
2-1
1
Resealing
Fuel
Tanks
-
.
3-10
,
III
us
.
3-10
Retractable
Landing
Gear
.
3-42
Riggin
g
Aileron
And
Rudder
-
3-14
,
Illus
.
3-12, 3-13, 3-15, 3-22,
3-23
.
Vi
F6

ALPHABETICAL
INDE
X
e
Servicing
(Cont'd)
S S T
a
Landing
Gear
.
1-9,
2-1
1
Oil
Change
.
.
1-9,2-10
Filter
. .
.
1-9,2-1
0
System
. .
. .
2-10
Pitot
And
Stati
c
System
.
2-16,
Illus
.
2-12
Points
Diagram
2-13,2-14,
2-15
Suction
Relief
Valv
e
Screen
.
.
,
1-9,2-1
6
Tires
1-8,2-1
0
Vacuum
System
2
.16,
Thus
.
2-16
Wheel
Bearings
.
.
.
-
1-
9
Shock
Absorber
Rubber
Disc
Replacement
3-40,
Illus
.
3-4
0
Spark
Plug
Chart
. .
,
2-16
Special
Tools
,
....
..
......
..
....
.2-
3
Stabilato
r
Control
Syste
m
Rigging
.
3-18,
Illus .
3-1
7
Electric
Tab
Actuato
r
Installation
3-17,
Illus
.
3-17
Removal
3-17,
Illus
.
3-1
7
Installation
.
3-18
Removal
3-18
Tab
Installation
3-16
A
Tab
Removal
. . .
3-16
A
Trim
Tab
Motor
and
Clutc
h
Assembl
y
Installation
3-17,
Illus
.
3-16
Removal
3-16A,
Illus
.
3-16
Trim
Tab
Syste
m
Rigging
-
3-20,
Illus .
3-19
Stall
Warning
Sensin
g
Switch
.-
.
.
1-8,3-52,
Illus
.
3-52
Stations
Diagram
2-2
Storage,
Aircraft
-
3-5
3
Strainer,
Fuel
-
1-9,2-
5
Strobe Ligh
t
Power
Suppl
y
Installation
.
3-37
Removal
- .
3-37
Wing
Installation
- .
3-37
Removal
-
-
3-37
Wiring 3-37
Suction
Relief
Valve
.
1-8,
1-9,
2-1
6
o
Fl
Switch
Adjustment,
Landing
Gear
Safety
3-50
Switch
Stall
Warning
Sensing
-
1
-7,
3
-52,
Illus
.
3-52
T
Tab
Actuator
Installation
,
Electric
-
3-17,
Illus
.
3-17
Actuator Removal
,
Electric
-
3-17,
thus
. 3.17
Installation,
Stabilator
-
3-16
A
Removal,
Stabilator
.
.
3-16
A
Table
Of
Torques
.1-
9
Tank
Repair,
Fuel
. .
Illus
.
3-
9
Temperature
Tension
Graphs,
Cable 3-15
Test,
Lea
k
Hydraulic
System
, -
3-48
Throttl
e
Control Rigging
3-54,
Illus .
3-54
Timing
Magneto
...
1-6,
3-58
Tire Pressure
.
2-1
1
Tire
Servicing
. .
1-8,2
.11
Tools,
Special
3
Torque
Chart,
Fuel
Syste
m
Fitting
- .
.
.
1-10,2-6
Torque
Test,
Magnetic
Clutch 3-17
Torques,
Table
Of
. . . .
1-
9
TorquingBolts
inShear
-
.
1-1
1
Towing
. - .
2-4,
Illus .
2-4
Transistor
Regulator
,
Troubleshooting
.
.
.
3-6
1
Transmitter, Fuel
Quantity
Removal
and
Installation
3-1
1
Travel,
Control
Surface
-
. -
1-
8
Trim
Tab
Cable
Replacement
3-18
Rigging
- .
3-20,
Illus
.
3-19
Troubleshootin
g
Alternator
- .
.
.
3-6
1
Fuel
Injection
System
.
3-6
3
Dirt
In
System
. .
3-5
5
Fuel Control
Leakage
3-55
Guide, Autopilot
. .
3-28
Magnetos
- . . .
3-64
Troubleshooting
(Cont'd)
Transistor
Regulator
.
3-61
U
Up
-lock,
Main
Gear
. .
Illus
.
3
-46
V
Vacuum
System,
Servicing
.
2-16A,
Illus
.
2-1
6A
Valve,
Fuel
Selector
-
. .
3-37
Valve,
Suction
Relief
1-8, 1-9,
2-16
Vendor
Publications
1
.12
Vertical
Stabilize
r
Installation
-
3-20,
Illus
.
3-21
,
3-24
Removal
. .
3-20,
Thus
.
3-2
1
Ventilation,
Cabin
.
-
2-17
Voltage Regulator 3-60
Adjustment
.
.
3-6
1
w
Warning
Horn
Switch
Adjustment
,
Landing
Gear
3.50
Wear
Limits,
Brake
Linings
. .
.
.
1-7,
3-50
Whee
l
Aligning
-
-
3-38,
Illus
.
3-39
Bearing
.
Servicing
.
.
-
1-
9
Conversion
2-11,
Illus .
2-12
Window
Cleaning
- -
2-1
8
Windshield
Installation
-
3-52
Removal
3-52
Wing
Fuel
Tank
Repair
-
Illus
.
3-
9
Installation
-
-
3-3,
Illus
.
3-
4
Leading
Edg
e
Repair
.
3-5,
Illus
.
3-
6
3-7,
3.8
Removal
Illus
.
3-
4
Strobe
Ligh
t
Installation
3-3
7
Removal
-
.
-
3-3
7
Wiring
Diagrams,
Electrical
-
.4-
1
VII

GENERAL
INFORMATION
0
1
1
0
0

.
SECTION
I
GENERAL
INFORMATIO
N
This
section
includes
a three
view
drawing,
general
information
in
chart
form,
on
servicing,
maintenance
and
rigging
and
a
vendor
publications
list
.
a
0
0
0
1
-
1
-
!
r1
;
c
4

25'
0'
**
25'
1
.25'
25'l'
&
AFTER)
3
.50
15.5
6'
4
o
6'4"
62'
**
11'
23
.07-4
S
Figure
1.1.
Dimensions
of
Aircraft
(M-1 thru
M
-1284
and
MB
-1
thru
MB
-480
)
1
-2
10'
8"

25'
1
.25
"
nr,
AU
*
48
4
13
0
12
.5
-6'
4--
-
---
-
-1
/_
6'
45'
*
6'
5"
ill 101,
Figure
1
-2
.
Dimensions
of
Aircraft
(MA
-1
thru
MA
-363)
SOU
23
-607
.5
1
-3

NOTE
Baggage
door
and
LH
and
RH
cabin
door
standard
on
M1362
and
after,
and
MB
-521
and
after
I
7 5
"
25'
-8
.5"
2
.
75'
23-607-6
A
Figure
1
-3.
Dimensions
of
Aircraft
(M
-1285
and
after,
MA
-364
and
after
and
MB
-481
and
after
)
1
-4

.
0
*765
/
\\
***
74
0
"
76O
'
12'
-8"
'
0
Figure
1
-4
.
Dimensions
of
Aircraft
(MC
-2
and
after
)
F2
1
-5

POWER
PLAN
T
ENGIN
E
Airplane
Manufacturer
Number
Horsepowe
r
23
Lycoming
0-320-D2B
160 (v
2700
RP
M
A23
and
A23A
Continental
10-346-A
165
iJ
2700
RP
M
B23
Lycoming
0-360-A20
180
(Q 2700
RP
M
C23
Lycoming
0-360-A2G
180
@
2700
RP
M
0-360-A4G
180
@
2700
RP
M
0-360-A4J
180
@
2700
RP
M
9
Lycorning
0-320-E2B
ISO
@
2700
RP
M
0-320-E2C
150
@
2700
RP
M
19A
Lycoming
0-320-E2C
150
2700
RP
M
B
l9
Lycorning
0-320-E2C
150
92700
RP
M
0-320-E3D
150
2700
RP
M
24
Lycoming
10-360-A2B
200
@
2700
RP
M
Equipped
with constant
speed
propeller
10-360-Al
B
200
@
2700
RP
M
A24
Lycoming
I0-36fl-A2B
200
@
2700
RP
M
Equipped
with
constant
speed
propeller
10-360-AIB
200
@2700
RP
M
A24R
Lycoming
10-360-A
lB
200
@2700
RP
M
10-360-AID
200
@2700
RP
M
B24R
Lycorning
10-360-A
l
B6
200
@2700
RPM
I
U24R
1
.yeuining
10-360-A
1136
200
01
2700
RPM
FIRING
ORDER
1
-3-2
-4
MAGNETO
TIMING
Airplane
Degrees
BTC
(Before
top
center
of
23,
9,
l9A,
24,
B23,
number
I
cylinder)
C23, B19,
A24and
A24R,
B24R
(MC
-2
thru
MC-388
and
MC
-393)
25°
A23,
A23A
24°
t
0°
-2°
B24R
-
C24R
.
(MC
-389
and
after
.
cxecpi
MC
-3)3l
20°
MAGNETOCONTACT
POINT
CLEARANC
E
Airplane
"E"
Gap
Main
Retar
d
A23, A23A
0°
±
.4
.018
±
.006
018
±
.00
6
23,
19,
19A,
24
15°
±
2°
.016
±
.003
.016
±
.006
B23,
*C23 *B19 A24,
A24R
B-
-14R
.
(24R
*Serials
MB
-540,
MB
-553
and
after,
M
-1672,
M
-l673,
M
-1674,
M
-l676,
M
-l677,
M
-1678
,
M
-tY,
M
-1682,
M
-l684,
M
-l686,
M
-1687,
M
-1688,
M
-1693,
M
-1698,
M
-1702,
M
-
1703
,
M
-1705
and
alter
utilize
Slick
4000
series
magnetos
which
are
considered
non
-servicable
1
-6
F2
0
0
.1
W

-
-
POWER
PLANT
(ont'd
)
OIL
PRESSUR
E
Airplane
Minimum
Idling
Normal
Operating
A23
and
A23A
10
psi
30
to
60
ps
i
23,
19,
19A,
B
l9,
25
psi
60
to
90
ps
i
B23 and
C2
3
24,
A24,
A24R
25
psi
65
to
90
ps
i
[124R
and
C24R
INDUCTION
AIR
FIL
TE
R
The
filter
must
be cleaned
daily
when
operating
in
dusty
conditions
.
When
operating
in
othe
r
than dusty
conditions,
clean
as
required
.
The
required
maximum
time
for
servicing
is
25
hours
.
IDLE
SPEE
D
.
S
23,
A23,
A23A,
B23,C23
.
24,A24,A24R
.B24R
.C24R
650
rpm
19,
19A and
B19
550
rpm
FUEL
SYSTE
M
FUEL
GRADE
Airplane
M-l, M-2,
M
-4
thru
M
-554,
M
-1095
and
after
M-3. M
.555
thru
M
-109
4
MA
-1
thru
MA
-368
Grad
e
91/96 octane
-blue,
100
octane
Low
Lead-blue
100/130
octane
-
green
100/130
octane -green
,
IOU
octane
Low
Lead
-
blue
100/130
octane
-
green
IOU
octane
Low
Lead
-
blu
e
MB-1
and
afte
r
MC-2
and
after
80/87
octane
-
re
d
IOU
octane
Low
Lead
-
blue
100/130
octane
-
gree
n
IOU
octane
Low
Lead
-
blu
e
MISCELLANEOU
S
BRAKE
DISC
AND
LINING
WEAR
LIMITS
Replace
linings
if
space
between
disc
MB-I
through
MB-52
1
and
the
flat
surface
of
the
housing
is
M-1 through
M-136
1
.312
(5)16)
inch
.
MA-1
through
MA-36
8
Minimum
brake
disc
thickness
is
.225 inch
MC-2
through
MC-9
7
Minimum
lining
thickness
is
.107
inch
MB-522
and
afte
r
above
the
rivet
.
M-1362and
afte
r
Minimum
brake
disc
thickness
is
.205 inch
MC-98
and
after
and
any
aircraft
that
hav
e
converted
from
Goodyea
r
to
Cleveland wheels an
d
brakes
.
F2
1
-7

MI
SCELLANEOUS
(C*it'd)
SUCTION
RELIEF
VAL
VE
Set
at
5
.0
inches
Hg. a
t
2000
rpm
.
STALL
WARNING
SWITCH
Adjust
5 to 7
mph
before
a
complete
stall
.
S
CONTROL
SURFACE
TRA
VEL
Flap
0° Full
U
p
30°
Full
Down
(M-l
thru
M
-554
)
35°
Full
Down
(M
-555
and
after,
MA
-1
thru
MA
-368,
MB-i
and
after
and
MC
-2
and
after
)
Aileron
20° ±
2° Up
10°
±
2°
Dow
n
Rudder
25°
±
2°
Right
25° ±
2°
Lef
t
Stabilator
15°
±
2° Up
2°
±2°
i0
Down
Stabilator
Tab
*2°
±
10
Up
*150
2°
-1°
Down
(With
Stabilator
in
Neutral)
**i°
+
1°
-1/2°
Up
±
2
°
.10
Dow
n
U
*Ml
thru
M
-1412
and
M
.!415,
M
-1419,
M
-1423,
M
-1439
&
M
-l447
;
MA
-1
thru
MA
-368
;MB
-I
thru
MB
-557
;
MC-2
thru
MC-i
50 eXcept
MC-l08
.
**.j43
and
after
except
M
-1415,
M
-14i9,
M
-1423,
M
-i439
&
M
-1447
;
MB
-558
and
after
;
MC
-l08,
MC
-l5
1
and
after
.
MOTOR
BRUSH
REPLACEMENT
GUIDE
Starter
23,
A23
and
A23A.
.25
in .
minimum
req
.
19,
19A,24,
B23,
C23,
.30
in .
minimum
req
.
B19,
A24,
A24R
.
B24R
and
C241(
Generator
.25
in .
minimum
req
.
Alternator
.25
in .
minimum
req
.
Tab
Actuator
Every
1000
operating
hrs
.
Motor
or
10,000
flight
lirs
.
SER
VICE
Tire
(inflation)
Aircraft
Standard
Size
Optional
Size
(15
X
6D0-6)
(17.50
X6
.00
.6)
23,
A23,
A23A
19,
19A,
1323,
C23,
B19
40
psi
(Nose
and
Main)
20
to
22
Psi
(Nose and
Main)
24,
A24
60
psi
(Nose
and
Main)
26
to
30
psi
(Nose
and
Main)
A24R,
B24R
.
C24R
Nose
Main
35
psi
(14.20
X
5
.00
-5)
32
psi
(17.50
X
6
.00 .6)
Oil
Filter
(Replace)
50
hours
(on
serials
M
-555
through
40,
M
-1
094
equipped
with
Continental
engines
)
I
1
-8
F2

- -
MISCELLANEOUS
(Cnt'd)
jj
SERVICE
(Corit'd)
Induction
Air
Filter
(Replace)
300
hrs
.
or
sooner
if
conditions
warrant
Induction Air
Filter
(Clean)
25
hrs
.
or
sooner
if
conditions
warrant
Instrument Air
Filter
50
hrs
.
(If
central
air
filter
is
not
installed)
Gyro
Instrument
Central
Air
Filter
(Replace)
Suction
Relief
Valve
Screen
(Clean)
Fuel
System
Screens
and
Strainers
(Clean)
Wheel
Bearings
(Lubricate)
Landing
Gear
Knee
Pins
(Lubricate)
ENGINE
500
hrs
.
100
hrs
.
100
hrs
.
or
sooner
if
conditions
warrant
100
hrs
.
25
hrs
.
or
sooner
if
conditions
warrant
TABLE
OF
TORQUE
S
Engine
mount
to firewall
Engine
Lordmounts
to
engine
supports
Oil
filter
center
stud
(Continental
engine)
Oil
filter
center
stud
(Lycoming
engine)
Spark
plugs
Continental
engines
Lycorning
engine
s
PROPELLE
R
Propeller
mounting
bolts
M-
l
thru
M
-554,
MB-1
thru
MB
-474
M
-555
and
after
and
MB
-475
and
after
MA-
I
and
after
with
fixed pitch
propeller
Propeller
mounting
nuts
MA
-I
and
after,
with
constant
speed
propeller
arid
MC
-2
and
after
325
1
-
0
-
20
inch
pound
s
475
±25
inch
pound
s
180
to
216
inch
pound
s
240
to
280
inch
pound
s
360
to
420
inch
pound
s
320
to
380
inch
pound
s
300
inch
pound
s
740
to
780
inch
pound
s
720
to
780
inch
pound
s
660
to
720
inch
pounds
1
-9

-
TABLE
OF
TORQUES
(Oont'd)
-
FUEL
SYSTEM
Fuel
strainer retainer
bolt
25
inch
pounds
as
stamped
on
straine
r
AIR
FRAME
Wing
attachment
bolts
See
Wing
Installation
in
Section
3
Stabilator
mounting
bolts
AN
bolts
50
to
70
inch
pounds
NAS
bolts
90
to
110
inch
pounds
Vertical
stabilizer
spar
bolts
50
to
70
inch
pound
s
WRENCH
TORQUE
FOR
TIGHTENING
HOSE
END
FITTING
AN
D
AN8
18
NUT
(POUND
INCH)
HOSE
ASSEMBLIE
S
(POUND
INCH
)
TUBING
ALUMINUM-ALLO
Y
CD
TUBING
FLARE
STEELTUBIN
G
INCHES
ANDIOO6I
or
AND10078
FLARE
AND1006
1
MINIMUM
MAXIMUM
MINIMUM
MAXIMUM
MINIMUM
MAXIMU
M
1/8
--
"
--
-
3/16
"
--
"
--
90 100 70 100
114
40
65
135
150 70 120
5/16
60 80
180
200
85 18
0
3/8
75
125
270
300 100
25
0
1/2
150
250
450
500 210 42
0
5/8
200
350 650
700 300
48
0
3/4
300 500
900
1000
500
850
1
500 700 1200
1400
700 1150
1-1/4
600
900
---
--
-
1-1/2
600900
---
--
-
1-3/4
--
"
---
---
--
-.-
2
--- --- ---
---
--
-
Fuel
System
FittingTorque
Values
0
.
1
S
0\1
1
-10

TORQUING
FINE
THREAD
SERIES
BOLTS
LOADED
IN
SHEA
R
TORQUE
LIMITS
RECOMMENDED
(INCH-POUNDS)
MAXIMUM
ALLOWABL
E
TORQUE
(INCH-POUNDS
)
SIZE
AN365
and
AN310 AN364
and
AN320
AN365
and
AN310 AN364
and
AN32
0
Nuts Nuts
Nuts
Nut
s
Column
1
Column
2
Column
3
Column
4
8-36
12-15
7-9
20
1
2
10-32 20-25
12-15
40
25
1/4-28
50-70 30-40
100 6
0
5/16-24
100-140
60-85
225
14
0
3/8-24
1,60-190
95-110
390 24
0
7/16-20
450-500 270-300 840 50
0
1/2-20
480-690
290-410
1100
66
0
9/16-18
800-1000
480-600 1600 96
0
5/8-18
1100-1300
660-780
2400
140
0
3/4-16
2300-2500
1300-1500
5000
300
0
7/8-14
2500-3000
1500-1800
7000
420
0
1-14
3700-5500 2200-3300 10000
600
0
1-1/8-12
5000-7000 3000-4200
15000
900
0
1-1/4-12
9000-11000
5400-6600
25000
15000
The
above
values
apply
to Class
3
threads,
cadmium
plated
and
nonlubricated
.
TORQUING
COARSE
THREAD
SERIES
BOLTS
LOADED
IN
SHEA
R
TORQUE
LIMITS
RECOMMENDED
MAXIMUM
ALLOWABL
E
(INCH-POUNDS)
TORQUE
(INCH-POUNDS
)
SIZE
AN365
and
AN310
AN364
and
AN320
AN365
and
AN310
AN364
and
AN32
0
Nuts Nuts Nuts
Nut
s
Column
1
Column
2
Column
3
Column
4
8-32
12-15
7-9
20 12
10-24 20-25
12-15
35
2
1
1/4-20
40-50
25-30
75
4
5
5/16-18
80-90
48-55
160
10
0
3/8-16
160-185
95-110
275
17
0
7/16-14
235-255
140-155
475 28
0
1/2-13
400-480 240-290
880
52
0
9/16-12
500-700
300-420 1100 65
0
5/8-11
700-900
420-540
1500
90
0
3/4-10
1150-1600
700-950 2500 150
0
7/8-9
2200-3000
1300-1800
4600
270
0
1-8
3700-5000
2200-3000
7600
450
0
1-1/8-8
5500-6500
33004000
12000
720
0
1-1/4-8
6500-8000
4000-5000
16000 1000
0
The
above
values
apply
to
Class
3
threads,
cadmium
plated
and
nonlubricated
.
1
-11

SUPPLEMENTARY
PUBLICATIONS
.
-
Following
is
a
list
of
publications
providing
servicing,
overhaul and
parts
information
on
various
componentson
the
BEECHCRAFT
19,
23
and
24,
which
you may
obtain
to
supplement
the
BEECHCRAFT
Shop
Manual,
In
most
instances
you
should obtain
the
publications
directly
from
the
manufacturer
or
his
distributor
.
Only
a
few,
such
as
engine
manuals
and
Beech
supplementary
publications,
are
available
from
Parts
and
Service
Operations,
Beech
Aircraft
Corporation
.
Those which
are
so
available are
listed
in
the
current
Publications
Price
List,
Since
a
wide
variety
of
radio
equipment
is
available
and
because
radio
manufacturers normally supply
parts
and
servicing
manuals
with each
set,
radio
publications
have not been
included
in
the
list
.
As
publications
on
additional
components
become
available,
they
will
be
added
to
this
list
of
publications
.
VENDOR
PUBLICATIONS
ENGINES
Operator's
Manual,
0
-320-E2B
or
E2C
engine,P/N
60297-16;
Lycorning
Division,
AVCO
Mfg.
Corp
.,
652
Oliver
St .,
Williamsport,
Penn
.,
17701
Operator's
Manual,
0
-320-D2B
engine,
PIN
60297
-16;
Lycoming
Division,
AVCO
Mfg
.
Corp
.,
652
Oliver
St .,
Wi!liamsport,
Penn
.,
17701
Operator's
Manual, 10
-360-AIB
r
A2B
engine,
PIN
60297
-12
;
Lycoming
Division,
AVCO
Mfg.
Corp
.,
652
Oliver
St .,
Williamsport,
Penn.,
17701
Operator's
Manual,
0
-360-A2G
engine,
PIN
60297
-12,
Lycorning
Division,
AVCO
Mfg
.,
Corp
.,
652
Oliver
St .,
Williamsport,
Penn
.,
17701
.
Overhaul
Manual,
0
-320,
0
-360
and
10
-360
series
engines,
P/N
60294-7; Lycoming
Division,
AVCO
Mfg.
Corp
.,
652
Oliver
St
.,
Williamsport,
Penn
.,
17701
0
Illustrated
Parts
Catalog,
0
-320
series
engines,
P/N
PC
-103,
Lycoming
Division,
AVCO
Mfg.
Corp
.,
652
Oliver
St
.,
Williamsport,
Penn
.,
17701
Illustrated
Parts Catalog,
0-360
series
engines,
P/N
PC
-106
;
Lycoming
Division,
AVCO
Mfg.
Corp
.,
652
Oliver
St .,
Williamsport,
Penn
.,
]770l
Illustrated
Parts
Catalog 10
-360
series
engines,
P/N
PC
-106
;
Lycoming
Division,
AVCO
Mfg.
Corp
.,
652
Oliver
St .,
Williamsport,
Penn
.,
17701
Operation
and
Maintenance
Manual,
10
-346
-A
engine,
P/N
X30029
;
Continental
Motors
Corp
.,
205 Market
St .,
Muskegon,
Mich
.,
49440
Maintenance
and Overhaul
Manual,
10
-346
-A
engine,
P/N
X30027
;
Continental
Motors
Corp
.,
205
Market
St .,
Muskegon,
Mich
.,
49440
Illustrated
Parts
Catalog,
10
-346
-A
engine,
P/N
X30028
;Continental
Motors
Corp
.,
205
Market
St
.,
Muskegon,
Mich
.,
49440
MAGNETOS
Service
Parts
List,
S
-200
series,
Form
L-528-2;
Scintilla
Division,
Bendix
Aviation
Corp
.,
Sherman
Ave
.,
Sidney,
New
York
Installation,
Maintenance
and Operation
Instructions,
S
-200
series,
Form
L
-526 -2
;
Scintilla
Division,
Bendix
Aviation
Corp
.,
Sherman
Ave
.,
Sidney,
New
York
Service
Parts
List,
S
-1200
series,
Form
L
-608
-1
;
Scintilla
Division,
Bendix
Aviation
Corp
.,
Sherman
Ave
.,
Sidney,
New
York
0
1
-12
I
-
This manual suits for next models
15
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