Grumman American AG-5B Tiger Pilot Operating Handbook

-.T'

rs

J

PILOT'S

OPERATING

HANDBOOK

AND

FAA

APPROVED

FLIGHT

MANUAL

TIGER AG-5B

Appr.

By;

Meager

:lanta

Federal

Atlanta,

AMERICAN

THIS

REOUIRED BY

THE

AND

ADDITIONAL

BY

THE

Thlft No.l« Hendboek.

revlaed

Aircraft Aviation

GA

MANUFACTURED

GENERAL

HAHOBOOK

INCLUDES

TO

BE

rURHlSHED

EESERAL

AVIATION

INFORHATION

HANUEACTURER.

hftndbdok

Be«tii

Specification for

leeued

Kebruarr

Septenber

1.

ral

Aviation

ification

inistration

OAMA

1984.

THE

REOULATIONS

PlloCe

TO

upcciflcatlon

IS,

AIRC^IAF'T

Serial Registration

Type

HATCRIAL

THE

PILOT

PROVIDED

Operetln?

197S

Administration

Office

No.

Certificate

and

A

BY

CORPORATION

10102

No.

American

P.

0.

Greenville

Mississippi

N592SM~

No.

Box

A16EA

General

5757

38703

-JM-

Revision

Aircraft

9

Date:

NOVEMBER

REVISED:

DEC

1,

18

1991

ORIGINAL

ISSUE

SECTION

GENERAL

1

Paragraph

No.

1.1

1.3

1.5

1.7

1.9

1.11

1.13

1.15

1.17

1.19

1.21

1.23

li25

General

Introduction

Three

View

Engine

Propeller

Fuel

Oil

Maximum

Typical

Cabin

Dimensions

Baggage

Specific

Symbols,

TABLE

Drawing

Certified

Airplane

Compartment

Loadings

Abbreviations,

Weights

OF

CONTENTS

Dimensions

and

Terminology.

Page

No.

1-1

1-2

1-3

1-3 1-3

1-4

1-4 1-4

1-5

1-6

NOVEMBER

REVISED:

1,

1991

ORIGINAL

ISSUE

REPORT:

POH-AOAC-1

1-i

INTENTIONALLY

LEFT

BLANK

REPORT:

1-ii

P0H-A6AC-1

ORIGINAL

ISSUE

AMERICAM AG~5B

TIGER

GENERAL

AIRCRAFT

CORPORATION

SECTION

GENERAL

1

1.1

GENERAL

Section 1 of

owners

contains a glossary

throughout

1.3

INTRODUCTION

This

Pilot's

an

operating

to

be

furnished

additional

the

FAA

This

handbook

competent

directives,

It

is

not

training

kept

in a current

The

handbook

provided

limitations normal

access

Procedures

present

of

the

paragraph

being

"Intentionally

this

and

operators

the

information

Approved

flight intended

manual

with a "finger-tip'

procedures,

to

information

Section

an

instant

handbook

numbers,

manual

manual.

Operating

guide

to

Airplane

is

not instruction,

applicable

and

status.

has

been

and

emergency

have

contains

of

AG-5B

of

symbols,

Handbook

for

the

pilot.

pilot

provided

Flight

designed

federal

to

be a guide

should

not

divided

that

been

Left

procedures

may

furnished

made

numbers,

Blank".

performance

has

reference

figure

SECTION

GENERAL

aircraft.

by

as a substitute knowledge

air be

into

tab

and

be

to

by

1

information

abbreviations

is

the

by

Manual.

for

used

divider

required

the

The

designed

It

includes

Federal

the

manufacturer

of

regulations

basic

for

numbered

for

have

other

item

been

sections

with a red

section.

deliberate

numbers,

of

general

end

of

this

and

terminology

for

maximum

the

Aviation

current flight

operational

(arabic)

in

material

Regulations

and

for

adequate

airworthiness

or

advisory

instruction

reference.

placed

to

tab

omission

and

sections

provide

divider

pages

quick

flight. Provisions

interest

section

utilization

required

constitutes

and

circulars.

purposes

ahead

of

easier

The

Emergency

to

for

expansion

of

certain

noted

used

or

unless

each

The

the

to

as

and

a

as

ORIGINAL

ISSUE

REPORT:

POH-AGAC-1

1-1

SECTION

GENERAL

1.5

THREE

1

VIEW

DRAWING

AMERICAN

ira"

GENERAL

AIRCRAFT

7*7"

CORPORATION AG-SB

TIGER

REPORT:

1-2

POH-AGAC-1

Figure

l-l

Three

View

Drawing

ORIGINAL

ISSUE

AMERICAN AG-SB

1.7

TIGER

ENGINE

GENERAL

AIRCRAFT

CORPORATION

SECTION

GENERAL

1

Number Engine

Engine

Maximum

1.9

Number Propeller Propeller

Number

Propeller

1.11

Fuel

Total

of Manufacturer

Model

Type

PROPELLER

of

FUEL

Grade

Capacity

Usable

Engines

Number

Continuous

Engine

Propellers Manufacturer Model

Blades

Diameter

Type

Fuel

Speed

Numbers

Power

(No

Further

Reduction

Permitted)

Aviation

Normally

Horizontally

Grade

Four

360

1A76EM8S10-0-61 1A76EM8S10-0-63 1A76EM8S10-0-65

100/lOOLL(Blue)

0-360-A4K

Aspirated

Air

Direct

Cubic

Sensenich

76

Fixed

52.6

51.0

Lycoming

Opposed

Cylinder

Cooled

Drive

Inches

180

BHP

2700

RPM

inches

Pitch

Gallons

2

ORIGINAL

ISSUE

REPORT:

POH-AGAC-1

1-3

SECTION GBNERAIi

1.13

Oil

First

Oil

After

AVERAGE

AIR

ALL

ABOVE

30

TO

0

TO

BELOW

Total

1.15

1

OIL

Grade:

50

Hours

Grade:

50

Hours

AMBIENT

TEMPERATURE

TEMPERATURES

80

DEGREES

60

DEGREES

90

DEGREES

70

DEGREES

10

DEGREES

Oil

MAXIMUM

of

Capacity

CERTIFIED

Operation

F.

STRAIGHT

MIL-L-6082B

HEIGHTS

SAE

AMERICAN

MINERAL

60

50

40

30

20

GENERAL

Straight

Ashless

AIRCRAFT

Mineral

Oil

Dispersing

ASHLESS

MIL-L-22851

SAE

15W50

SAE

40

SAE

40,

30

SAE

CORFORATION

AG-SB

MIL-L-6082

MIL-L-22851

DISPERSANT

OR

60

OR

SAE

40

OR

SAE

30

OR

20W30

8

Quarts

TIGER

20W50

50

20W40

Maximum

Maximum Maximum Maximum

1.17

TYPICAL

Standard

Useful

REPORT:

1-4

Takeoff Landing

Weight

Empty

Load;

POH-AGAC-1

Weight Weight

in

Baggage

AIRPLANE

Weight

Normal

Utility

(Normal (Normal

(Utility (Utility

HEIGHTS

(No

Category

Category) Category)

Compartment

Optional

Equipment)

ORIGINAL

2400 2400 2050 2050

120

1398

1002

652

Lbs.

Lbs. Lbs.

Lbs.

Lbs. Lbs.

ISSUE

lUfERICAN

AG-5B

1.19

TIGER

CABIN

GENERAL

DIMENSIONS

AIRCRAFT

CORPORATION

SECTION

GENERAL

1

Width

Length

Height

Entrance

1.21

BAGGAGE

Width

Length

Height

Entrance

1.23

SPECIFIC

Wing

Loading

Power

Loading

Width

Height

COMPARTMENT

LOADINGS

DIMENSIONS

40 50

46 34

29 35

30

24 12

17.1

13.3

Inches Inches

Inches Inches Inches

Inches Inches

Lbs/Ft^

Lbs/HHP

ORIGINAL

ISSUE

REPORT:

POH-AGAC-1

1-5

SBCTIOH GENERAL

1.25

1

Synbols,

Abbreviations,

AMERICAN

and

Terainclogy

GENERAL

AIRCRAFT

CORFORATION AG-5B

TIGER

AIRSPEED

KCAS

KIAS

KTAS

Vf£

Vno

SYMBOLS

AND

TERMINOLOGy

Knots

Calibrated

corrected expressed

standard

Knots

airspeed

Knots

temperature.

Maneuvering

application

overstress

Maximum

the speed

fully

Maximum limit

the

air.

Never

indicator,

exceeded.

atmosphere

Indicated

indicator,

True

Flap

white

the

extended.

Structural

of

the

speed

Exceed

for

position

in

knots.

Airspeed

Speed

of

full

the

airplane.

Extended

arc

on

is

Speed

the

yellow

should

the

airplane

that

and

KCAS

at

sea

expressed

is

KCAS

is

the

available

Speed

airspeed

can

be

Cruising

arc

not

marked

speed

limit

is

the

indicated

instrviinent

is

equal

level.

is

the

speed

in

knots.

corrected

maximum

speed

control

marked

indicator,

flown

with

Speed

the

airspeed

exceeded

that

marked

on

be

by a red

to

by

the

line

may

airspeed

error, KTAS

in

shown

on

for

altitude

at

which

will

not

the

upper

is

the

wing

by

the

indicator,

except

on

the

never

a

the

end

highest

flaps

lower

in

smooth

airspeed

be

and

of

is

Vg'

*

REPORT:

1-6

Stalling

the

speed

limit

POH-AGAC-1

speed

airplane

is

marked

of

the

—

(clean)

is

controllable

on

the

green

arc.

is

the

minimum

with

airspeed

speed

the

flaps

indicator

at

up.

as

the

ORIGINAL

which

This

lower

ISSUE

AMERICAN

AG-SB

TXGER

GENERAL

AIRCRAFT

CORPORATION

SECTION

GENERAL

1

HETROLOGICAL

OAT

STANDARD TEMPERATURE

PRESSURE

ALTITUDE

ENGINE

BHP

RPM

AIRPLANE

DEMONSTRATED

CROSSWIND

COMPONENT

POWER

PERFORMANCE

Stalling the

airplane

speed

is

limit

of

Best

Angle

the

greatest

Best

Rate

the

greatest

time.

TERMINOLOGY

Outside

15

degrees

The

altitude

scale

set

TERMINOLOGY

Brake

Horse

Revolutions

turning.

TERMINOLOGY

The

velocity

adequate

landing

test.

speed

(dirty)

is

marked

the

white

of

Climb

gain

of

Climb

gain

Air

Temperature

Celsius

read

at

29.92

Power

per

of

control

was

actually

is

controllable

on

the

arc.

in

speed

in

(59

from

inches

is

Minute

the

of

the

airspeed

Speed

is

altitude

is

altitude

is

free

degrees

an

altimeter

of

the

power

is

the

crosswind

the

airplane

demonstrated

minimum

with

the

indicator

the

speed

per

distance

the

speed

in

the

air

static

Fahrenheit).

mercury.

with

developed

speed

the

component

during takeoff

during

speed

at

flaps

down.

as

the

which

results

traveled.

which

shortest

results

temperature.

the

barometric

by

the

engine

for

which

certification

which

This

lower

in

possible

engine.

is

and

in

ORIGINAL

ISSUE

REPORT:

POH-AGAC-1

1-7

SBCTIOH GENERAL

1

AMERICAN

GENERAL

AIRCRAFT

CORPORATION AG-5B

TIGER

USABLE

UNUSABLE

GPH

WEIGHT

REFERENCE DATUM

STATION

ARM

MOMENT

C.G.

ARM

C.G.

LIMITS

STANDARD EMPTY

WEIGHT

FUEL

AND

The

Gallons

consumed

A

the

BALANCE

An

distances

A

REFERENCE

quantity

Per

unit

of

force

TERMINOLOGY

imaginary

location

expressed

The

horizontal

CENTER

airplane.

The

arm. 1000

Center

would

REFERENCE

by

The

WEIGHT

The

can

The

fluids,

OF

product

IN TO

of

balance

the

TOTAL

quotient

of

extreme

be

operated

weight

of

fuel

of

fuel

Hour

by

aooeleration

of

are

as

DATUM.

GRAVITY

THIS REDUCE

Gravity

DATUM

the

engine

is

the

engine.

gravity.

reference

measured

along

the

distance,

distance

of

the

HANDBOOK

THE

if

suspended.

is

WEIGHT

of

the

airplane.

C.G.

locations

at a given

of a standard

oil,

available

that

the

rate

equivalent

from

for

airplane's

from

of

an

Item

weight

ALL

NUMBER

is

the

found

of

the

TOTAL

and

unusable

for

cannot

at

which

weight

longitudinal

in

inches,

the

or

location

of

an

item

MOMENTS OF

DIGITS.

point

at

It

by

is

dividing

airplane.

MOMENTS

within

weight.

airplane

flight.

be

used

fuel

to

that

all

horizontal

and

balance

from

REFERENCE

multiplied

HAVE

which

DISTANCE

the

divided

which

with

fuel.

in

is

produced

the

in

BEEN

an

TOTAL

by

the

full

flight.

being

purposes.

axis

DATUM

to

the

by

DIVIDED

airplane

from

MOMENT

the

airplane

operating

by

the

its

BY

the

TOTAL

REPORT:

1-8

POH-AGAC-1

ORIGINAL

ISSUE

AMERICAN AG-SB

BASIC

WEIGHT

USEFUL

GROSS

TARE

6BHBRAL

TIGER

EMPTY

LOAD

WEIGHT

AIRCRAFT

The

STANDARD

EQUIPMENT.

The

difference

WEIGHT.

The

maximum

The

weight

weighing

readings.

obtain

an

CORPORATION

EMPTY

weight

of

chocks,

an

airplane,

Tare

accurate

WEIGHT

between

to

is

subtracted

weight.

plus

GROSS

which

blocks,

that

is

the

WEIGHT

the

airplane

stands, included

from

WEIGHT

and

etc.

in

the

scale

the

is

OF

used

the

SECTION

GENERAL

OPTIONAL

BASIC

EMPTY

certified.

when

scale

reading

1

to

ORIGINAL

ISSUE

REPORT:

POH-AGAC-1

1-9

SECTION

GENERAL

1

AHERICAN

GENERAL

AIRCRAFT

CORPORATION

AG-SB

TIGER

REPORT:

1-10

FOH-AGAC-1

INTENTIONALLY

LEFT

BLANK

ORIGINAL

ISSUE

SECTION

LIMITATIONS

2

Paragraph

No.

2.1

2.3

2.5

2.7

2.9

2.11

2.13

2.15

2.17

2.19

2.21

2.23

2.25

General

Airspeed Airspeed

Power

Plant

Power

Plant Weight Center

Maneuver

Flight Kinds

of

Fuel

Limitations

Noise

Level

Placards

TABLE

Limitations Indicator

Limitations

Instrument Limitations of

Gravity

Limits

Load

Factor

Operations

OF

CONTENTS

Markings

Limitations

Limits

Page

No.

2-1

2-1 2-2

2-2

2-3 2-4 2-4

2-5

2-5 2-6

2-6 2-6

2-7

NOVEMBER

REVISED:

I,

1991

ORIGINAL

ISSDE

REPORT:

POH-AGAC-1

2-i

SBCTIOM

LIMITATIONS

2

AHBRICAH

GENERAL

AIRCRAFT

CORPORATION

AG-SB

TJGBR

REPORT:

2-ii

POH-AGAC-1

INTENTIONALLY

LEFT

BLANK

ORIGINAL

ISSUE

aMERICAN

AG-5B

ZIGBS

GBNBRAL

AIRCRAFT

CORPORATION

SECTION

LIMITATIONS

2

2.1

GENERAL

This

section

placards

limitations

Aviation

2.3

AIRSPEED

SYMBOL

v„

V.W

1

v„

presents

necessary

contained

Administration.

LIMITATIONS

NEVER

MAXIMUM

CRUISING

MANEUVERING

(2,400

MAXIMUM

the

for

EXCEED

STRUCTURAL

pounds)

FLAP

CANOPY

Figure

operating

the

in

this

SPEED

EXTENDED

OPEN

2-1

SECTION

LIMITATIONS

limitations,

safe

section

Airspeed

2

operation

are

Limitations

instrument

of

the

approved

KCAS

174

143

113

104

113

markings

airplane.

by

the

KIAS

172

142

112

103

112

and

The

Federal

ORIGINAL

ISSUE

REPORT:

POH-AGAC-1

2-1

SECTION

LIHITATXONS

2.5

AIRSPEED

2

INDICATOR

MARKINGS

AMERICAN

GENERAL

AIRCRAFT

CORPORATION

AG-SB

TIGER

2.7

POWER

Number Engine Engine

Maximum

MARXZNO

WHITE

GREEN

YELLOW

RED

Figure

PLANT

of

Engines Manufacturer Model

Number

Power

Engine

Speed

ARC

LINE

2-2

LIMITATIONS

KIA8

53-103

56-142

142-172

172

Airspeed

EZILANATION

FLAP

OPERATING

lower

limit

landing

upper

speed

flaps

NORMAL

The

weight

the

limit

Structural

Operations

conducted

then

Never

configuration.

limit

permissible

extended.

OPERATING

lower

stalling

flaps

is

the

only

exceed

Indicator

RANGE.

is

the

RANGE.

limit

is

speed

up.

The

Maximum

cruising

must

be

in

smooth

with

caution.

speed.

Mtirlcings

in

the

maximum

with

maximum

upper

Speed.

air

The

with

The

and

Lycoming

0-360-A4K

180

2700

BHP

RPM

REPORT:

2-2

POH-AGAC-1

ORIGINAL

ISSUE

AMERICAN AG-SB

TIGER

Fuel

Grade

Oil

Grade:

Oil

Grade:

Number

Propeller

of

Propeller

2.9

POWER

GENERAL

Propellers

Manufacturer

Model

AIRCRAFT

Numbers

Diameter

PLANT

INSTRUMENT

(No

CORPORATION

Further

MARKINGS

Straight

Reduction

Aviation

Mineral

(First

Ashless

(After

50 Dispersing 50

Permitted)

Grade

Oil

Hours

1A76EM8S10-0-61 1A76EM8S10-0-63 1A76EM8S10-0-6S

SECTION

LIMITATIONS

100

LL{Blue)

MIL-L-6082B

of

Operation)

MIL-L-22851

of

Operation)

Sensenich

76

2

1

Inches

ORIGINAL

ZMSTRnMEMT

TACHOMETER

(RFM)

OZL

(PSZ)

TEMPERATURE

(DEGREES

FUEL

(Paz)

CYLZNOER

TEMPERATURE

(DEGREES

VACUUM

(Hg.)

ISSUE

PRESSURE

OZL

PRESSURE

Figure

HEAD

RED

LZME

25

F)

0.5

F)

2-3

Power

YELLOW

ARC

25-55

—

Plant

GREEN

ARC

2250

To

2700

55-95

80-245

0.5-8

150-400

4.6-5.4

Instrument

YELLOW

ARC

95-115

Meurkings

REPORT:

RED

LZME

2700

115

245

8

500

POH-AGAC-1

2-3

SECTION LIHITATI0N8

2.11

WEIGHT

2

LIMITATIONS

AMERICAN

GENERAL

AIRCRAFT

CORPORATION

AG-SB

TIGER

Maximum

Maximum Maximum

Maximum

2.13

NORMAL

1920

2400

UTILITY

1920

2050

NOTES:

(1)

(2)

\

(3)

Gross

Takeoff

Landing

Ramp

Weight

CENTER

CATEGORY

WEIGHT

Lbs.

CATEGORY

WEIGHT

LBS.

Lbs.

Straight

Limits

50

inches

firewall.

It

is

insure

POH for

Weight;

Weight Weight

Weight;

in

Baggage

OF

GRAVITY

line

variation

are

given

forward

the

responsibility

that

the

proper

Normal

Utility

Normal

Utility

Compartment

LIMITATIONS

in

inches

of

airplane

loading

Category

FORWARD

between

the

is

instructions).

81.00

89.00

81.00

83.17

aft

of

front

of

the

properly

LIMITS

points

face

given.

Reference

of

the

airplane

loaded

Datxua

lower

owner

(see

2400 2050

2400 2400 2408

2058

120

AFT

LIMITS

92.50

AFT

LIMITS

85.32

which

is

the

located

of

pilot

portion

and

Section 6 of

Lbs. Lbs.

Lbs.

Lbs. Lbs. Lbs. Lbs.

the

this

to

REPORT:

2-4

POH-AGAC-1

ORIGINAL

ISSUE

AMERICAN

AG-SB

2.15

GENERAL

TIGER

MANEUVER

LIMITS

AIRCRAFT

CORPORATION

SECTION

LIMITATIONS

2

NORMAL

Authorized

Uauthorized

UTILITY

Maneuver

Chandelles

Lazy

Steep

Stalls

SPINS

INTENTIONAL

2.17

NORMAL

Flaps Flaps

CATEGORY

Eights

Turns

(Except

FLIGHT

Up

Down

CATEGORY

Maneuvers:

Whip

SPINS

LOAD

ARE

FACTOR

Stalls)

PROHIBITED

LIMITS

Any

Maneuver

Stalls

Chandelles,

more

All

(Except

than

acrobatic

prohibited

Incidental

Whip

And

60

degrees

maneuvers

Recommended

Stalls),

Steep

of

To

Normal

Lazy

Turns

bank)

including

Entry

Slow

Deceleration

+3.8/

+3.5

Flying, Eights,

(with

spins

Speed

112

112 112

-1.52g

KIAS

KIAS KIAS

not

UTILITY

Flaps

ORIGINAL

Up

Down

CATEGORY

ISSUE

REPORT:

+4.4/

+3.5

POK-AGAC-1

-1.76g

2-5

SECTION

LIMITATIONS

2.19

KINDS

The

Standard

the

appropriate

91

installed,

2

OF

OPERATIONS

AG-5B

is

approved

navigation

the

airplane

AMERICAN

for

and

is

Day

communication

approved

and

for

GENERAL

Night

equipment

IFR

operations.

AIRCRAFT

VFR

operations.

required

CORFORATION

AO-SB

TXGER

by

With

FAR

NOTE:

2.21

Total

2.23

The

been this airport.

above

Administration FAR

This

applicable

The

FUEL

LIMITATIONS

Capacity

Usable

NOISE

noise

level

made

by

airplane

The

has

36,

Noise

aircraft

AG-SB

LEVEL

been

to

is

Fuel

of

the

Federal

should

above

verified

in

noise

Standards

model

this

type.

not

approved

this

airplane

Aviation

be

acceptable

statement

level Aircraft

is

in

for

is

Administration

or

not

by

compliance

withstanding

and

test

flight

Type

flight

72.4

into

dB(A).

unacceptable

approved

conducted

and

Airworthiness

with

all

by

known

icing

No

determination

that

the

for

the

noise

the

in

FAR

36

conditions.

52.6

51.0

noise

operation

Federal

accordance

noise

level

Aviation

Certification.

standards

Gallons

has

at

any

stated

with

of

REPORT:

2-6

POH-AGAC-1

ORIGINAL

ISSUE

AMERIC2UI AG-SB

2.25

On

the

THE

MARKINOS

CONTAIN WITH CATEGORY.

COMPLIED

CATEGORY THE

PILOT'S

NORMAL

DESIGN NO

ACROBATIC

UTILITY

DESIGN

REAR

ACROBATIC

HAKBUVBR

CHAHDELLES LAZY STEEP

STALLS

SPINS

THIS

MIGHT

THIS

KNOWN

GENERAL

TIGER

PLACARDS

Left

OPERAXINO

WHEN

OTHER

WITH

OR

CATEGORY-

MANEUVERING

CATEGORY-

MANEUVERING

SEAR

MUST

MANEUVERS

EIGHTS

TURNS

(EXCEPT

PROHIBITED

MRPLAMB

MHEM

AIRPLANE

ICING

Side

AND

PLACARDS

OPERATING

WHEN

IN

THE

OPERATING

MANEUVERS

NOT

WHIP

IS

EQUIPPED

CONDITIONS.

AIRCRAFT

Panel:

LIMITATIONS

THIS

OPERATING

UTILITY

HANDBOOK

SPEED

INCLUDING

SPEED

BE

OCCUPIED

ARB

LIMITED

STAU.S)

APPROVED

IN

IS

NOT

CORPORATION

IKSXALLBD

AIRPLANE

LIMITATIONS

CATEGORY

V^

ACCORDANCE

APPROVED

NBICB

THIS

112

FOR

SPINS

KNOTS

TO

ZN

KD8I

AIRPLANE

ARE

KNOTS

THE

VFR,

THIS

BE

IN

WHICH

CONTAINED

APPROVED

IAS

FOLLOWING:

ENTRY

SLOW

IFR,

WITH

FOR

AIRPLANE

COMPLIED

TEE

MHST

IN

IAS

FLIGHT

NORMAL

BE

THIS

IN

SPEED

112

112 112

DECELERATION

DAY

FAR

91.

INTO

AMD

KNOTS

KNOTS KNOTS

SECTION

LIMITATIONS

lAB

2

FOR

FLIGHTS

SEAT

OCCUPANTS

BAGGAGE-CARGO,

CHECK

BALANCE

ORIGINAL

TIRE

NOSE

MAIN

WEIGHT

PRESSURE

25

35

ISSUE

LBS.

WITH

&

REAR

AND-OR

REPORT:

POH-AGAC-1

2-7

SBCTIOH

LIMITATIOHS

On

the

2

Instrument

Panel:

AMERICAN

GENERAL

AIRCRAFT

CORPORATION AG-SB

TIGER

On

the

TURN

OR

In

Baggage

120

FOR SEE

NO

On

Rear

INSTRUCTIONS

CAUTION:

HAY

CAUSE

CLOSE

SUBTRACT

Instrument

OFF

HAZE,

POUNDS

ADDITIONAL WEIGHT

HEAVY

Seat

340

POUNDS

DISTRIBUTE

FOR

BALANCE

OPERATING

FLASHING

VISUAL

CANOPY

80

6

WHEN

KNOTS

FEET

Panel

STROBE TAKI

WITH

Compartment:

MAKIMUM

LOADING

AND

BALANCE

OBJECTS

Base:

NO

PASSENGERS

MAKIMUM

ADDITIONAL

SEE

DATA

AND

HANDBOOK

BEACON

DISORIENTATION

USING

FROM

(If

IN

CLOUD,

STROBE

BAGGAGE

ON

HAT

(Visible

EVENLY

LOADING

WEIGHT

PILOT'S

ALTERNATE

IAS

ALTITUDE

Strobe

FOG

OFF

INSTRUCTIONS DATA

SHELF

With

CARGO

AND

IN

ABOVE

CLOUDS

ABOVE

Lights

Rear

87

STATIC

KNOTS

86

are

Seat

AIR

IAS

KNOTS.

Installed)

Back

Upright)

REPORT:

2-8

POH-AGAC-1

ORIGINAL

ISSUE

AMERICAN

AG-SB

On

Baggage

TO

SLroE

TIGER

OPEN

GENERAL

Door:

DOOR

HANDLE

AIRCRAFT

FROM

FORWARD

CORPORATION

INSffiE

SECTION

LIMITATIONS

2

Interior-

IJNLOCK

UNLATCHED

On

the

Inside

t

Under

Rear

—BEFORE

SEAT

TURNED

Adjacent

FLAG

112 NO

FLIGHT

Seat

NO

STEP

BACK

DOWN

THIS

INDICATES

Canopy

KNOTS

Base

FLIGHT—

MUST

TO

AREA

to

Canopy

COPY

Rail:

IAS

MAX

WITH

(Visible

BE

COVER

WITH

CANOPY

Lock:

CANOPY

OPEN

With

OPEN

BEYOND

Rear

TO

THIS

Seat

HERE

POINT

Back

Upright)

ORIGINAL

ISSUE

REPORT:

POH-AGAC-1

2-9

SECTION

LIMITATIONS

Aft

of

MIN

26.3

19.0

On

the

LEFT

25.5

2

Fuel

U.S.

Fuel

FUEL

U.&

Tank

Caps:

FUEL

100/100

GAL.

Selector

^

GAL.

LL

TOTAL

TO

Valve:

RIGHT

2S.5

U.S.

OCX

TAB

FUEL

CAP.

GAL

AMERICAN

GENERAL

AIRCRAFT

CORPORATION AG-SB

TJGEK

On

Glare

On

Throttle

REPORT:

2-10

BOTH

Shield:

NO

FRICTION

POH-AGAC-1

OFF

SMOKING

Quadrant:

ADJ

FUEL

SELECTOR

ORIGINAL

ISSUE

SECTION

3

Paragraph

No.

3.1

General

3.3

Airspeeds

3.5

Emergency

3.7

Amplified

3.9

Engine

3.10

Air

3.11

Smoke

3.12

System

3.13

Glide

3.14

Landing

3.15

Spins

Failure

Start

and

Failures

Emergencies

EMERGENCY

for

Emergency

Procedures

Emergency

Fire

TABLE

Operations

Checklist

Procedures

PROCEDURES

OF

CONTENTS

Page

No.

3-1

3-4

3-6

3-7

3-8

3-9 3-10

HOVEMBrR

REVIS70N:

1,

1991

ORIGINAL

ISSUE

REPORT:

P0H-A6AC-1

3-1

INTENTIONALLY

LEFT

BLANK

REPORT:

3-ii

P0H-A6AC-1

ORIGINAL

ISSUE

Grumman American AG-5B Tiger Pilot Operating Handbook

Specifications and Main Features

Frequently Asked Questions

User Manual