Beechcraft Baron POH

SENECA

COLLEGE

SCHOOL

OF

AVIATION

FLIGHT

MANUAL

FOR

RAYTHEON

BEECHCRAFT

B58

BARON

VERSION

B1

FOR

CLASSROOM

USE

ONLY

FOR

CLASSROOM

USE

||ay|'|lB0ll

Aircraft

LIST

OF

E|=r=EcT|vE

PAGES

Thislistingcontainsallcurrent

pages

witheffective revision

numberordate. Itshould be used after posting changesto

ensure the manual is complete and up-to-date. A/ways

destroy

superseded

pages

whenyouinsert revisedpages.

Baron® 58/58A

(SerialsTH-1472 andAfter,exceptTH-1476,

TH-1487, TH-1489,andTH-1498)

Pi|ot’s

Operating Handbook

Bhd

FAA

Approved Airplane

Flight Manual

P/N

58-590000-39

Revision

B1 -

June,

2004

TitlePage

....

Logo Page

...

ListOfEffectivePages _ __

LogOf Revisions Revision B1 ReissueB

....

1-1 thru1-24 2-1 thru2-18 2-19

...

2-20 thru 2-36 3-1 thru3-17

..

3-18

...

3-19 thru 3-24 4-1 and4-2

....

4-3thru4-11 _._ 4-12and4-13 4-14 thru 4-32 ._ 4-33 thru 4-40 5-1 thru5-62

..June,2004

Undated _ .Jur-fi 2004

._June,2004

..June,2003

June,2003

June,2003

June,2004

June,2003

June,2003

June,2004

June,2003

June,2004

June,2003

June,2004

June,2003

June,2004

June,2003

1of2

List Of

Effective

Pages

(Cont’d)

2of2

58-590000-39

Revision

B1 -

June,

2004

6-1thru6-24.

...

June, 2003 7-1 thru7-4._

...

...

June,2004 7-5thru7-27. June, 2003 7-28 thru 7-32

...

June, 2004 7-33 thru 7-39

...

June, 2003 7-40 thru 7-52

...

June 2004 8-1thru8-56.

...

June, 2003 9-1 and 9-2. __

...

June, 2003

Supplements

...

....

SeeLog ofSupplements

10-1 thru 10-64

....

...

May, 1994

/¥

||3y|’|lB0ll

Aircraft

Loc.

o|=

Revisions

Baron® 58/58A

(SerialsTH-1472andAfter, ExceptTH-1476,

TH-1487,TH-1489, andTH-1498)

Pilot’s

Operating Handbook

and

FAA

Approved Airplane

Flight

Manual

P/N

58-590000-39

Revision

B1 -

June,

2004

PAGE-

_

-DES;;-PTION

_

_

TitlePage New

LOEP New

LOR New

2-19 RevisedPlacard

3-18 Revised “Electrothermal Propeller Deice System"

4-1and 4-2 Revised Table oiContents

4-12and 4-13 Revised “Before Takeofl" and Shifted Data

4-33thru 4-35 Added“Heater Operation" and revised

"Wind-shield Defogging"

4-36thru 4-40 Shifted Data

7-1thru 7-4 Revised Table ofContents

7-28and 7-29 Revised “Fue| Cells"

7-30thru 7-32 Revised illustrations

7-40 thru 7-5? Revised“LightingSystem", “Environmental

Sys-tem”and ShiftedData

B1

||3y|'|II€0Il

Aircraft Company

INSTRUCTION SHEET

Baron® 58/58A

(SerialsTH-1472thruTH-2124,exceptTH-1476,

TH-1487, TH-1489,and TH-1498)

Pi|ot’s Operating Handbook

and

FAA

Approved

Airplane

Flight Manual

Revision

B2

January

2006

TitlePage

LogoPage

List ofEiiectwePages

1 012 2 of2 LogofRevisions 1 0I2 2of2 2-29 2-30 REMOVE EXISTING PAGE June 2004 June 2004 June 2004 June,2003 June, 2003 PAGE January2006 January2006 January2006 January 2006 January 2006 June, 2003 January, 2006 PIN

58-590000-39

PAGEOR INSERTNEW

SECTION

Instruction

Sheet

(Cont’d)

PIN5§Q?59QQ °°'39~; -Q

Revision_S_Q24¢[Jqhu;ii§y,2006

SPA;§E€6F!

_<

Tjusznr

New

SECTION V_ _ &

37,

f

*'A ~1ii'!§§47?Q6?¥¥7{ §3 >- ¢.

.

JLif?§£@QQ§59

3-a SN JyHé{26b§i“7f` Qéndq§g2QQq I'» <sub>_§=%1i<fv?f'</sub> Q I' » _` 3-21

.

O O 3-22 `9OJdh’éQS`2boé _{%Juhéf§66§S} Qff June,'2003 O.

;€;:5;37

S 7 SS Junegzooa "_ S Ju0é§?955,V 5i .; _, `. V, §_ QlY Y »`VV

f|12 fH||'f¢Q§!i

_Jfii

3

‘if*i@7§1 fi?xi§l`i\‘?T.'iW§i "~ 5; l§Hce;1f_2I1d`¥

54,1-.,.~’V¢5f:»gmfg§> _,¢,$;'= <f=A_,»~v~,< »

OtherP¢!t!§i§

V

¢» ¢ f ;nHf¢éhé f¢V'S¢di or¢ V

.

O ,

v. "Q n, *~

After

A»lO_A l»al~€:arded'A1_iL~Ai§<Qé;,;;§'f2§<¢}'fO,.l~»~',,E3»

gi;

V

Z

||ily|’|ll20ll

Aircraft Company

Qeechclaft

Baron®

58

and

58A

Special

Reduced

Gross

Weight

Configuration

(SerialsTH-1472thruTH-2124,

except

TH-1476, TH-1487,

TH-1489,andTH-1498)

Pilot’s

Operating

Handbook

and

FAA

Approved Airplane

Flight Manual

FAAApproved in the Normal Category based on CAR 3. This

document must be carried inthe airplaneatall times, andbe kept

within reach ofthe pilot duringallflightoperations. This handbook

includesthe material requiredtobe furnishedtothepilotbyCAR3.

Airplane Serial Number:

AirplaneRegistration N

FAAAppro

by:

John

ue/

RaytheonAircraftCompany

DOA-230339-CE

Copyrig ©2006 Raytheon Aircraft Company. Allrightsreserved.

P/N58-590000-39B P/N58-590000-39B2

||8y||lB||ll

Aircraft Company

LIST OF

EFFECTIVE

PAGES

Thislisting containsall currentpageswith effective revision

numberor date. Itshouldbe used afterposting changesto

ensure the manual is complete and up-to-date. A/ways

destroysuperseded pageswhen you insertrevisedpages.

Baron® 58l58A

(Serials TH-1472thruTH-2124,exceptTH-1476,

TH-1487, TH-1489,andTH-1498)

PiIot’s

Operating Handbook

and

FAA

Approved

Airplane

Flight Manual

PIN

_58-590000-39

Revision

B2 -

January,

₂₀₀₆

Title Page

... ...

LogoPage

...

January, 2006 Undated

ListOfEffectivePages

....

January, 2006

Log OfRevisions RevisionB2

...

January, 2006 RevisionB1 June, 2004 ReissueB

...

June, 2003 1-1 thru1-24 .__June, 2003 2-1thru2-18 ._ _June 2003 2-19

.._.._....

...June

2004 2-20 thru 2-29 .__. .June 2003 2-30

..__..._._._

January 2006 2-31thru2-36

....

_June 2003 3-1 thru 3-7 __.. .June 2003 3-8

..._.__._.

January, 2006 3-9thru3-17 _June, 2003 3-18

_..._._

_June, 2004 3-19 and 3-20 _June, 2003 3-21

__.._.._.

_{January, 2006} 1 of 2

ListOfEffective

Pages

(Cont’d) 3-22 thru3-24. 4-1 and4-2. 4-3thru4-11 4-12 and4-13. 4-14 thru4-32. 4-33 thru4-40. 5-1thru5-62. 6-1thru6-6. 6-7

...

6-8thru 6-24. 7-1thru7-4. 7-5thru 7-27. 7-28thru 7-32. 7-33 thru 7-39. 7-40 thru 7-52. 8-1thru 8-34. 9-1 and 9-2.._ Supplements 10-1 thru 10-64

2of2

P/N 58-590000-39 RevisionB2-

January,

2006 2003 2004 2003 2004 2003 2004 2003 2003 2006 2003 2004 2003 2004 2003 2004 2006 2003 June, June, June, June, June, June, June, June, January, June, June, June, June, June, June, January, June,

SeeLog ofSupplements

||ily|'|l|!0Il

Aircraft Company

LOG

OF REVISIONS

Baron® 58l58A

(SerialsTH-1472thruTH-2124,ExceptTH-1476,

TH-1487, TH-1489,and TH-1498)

Pilot’s

Operating Handbook

and

FAA

Approved Airplane

Flight Manual

PIN

58-590000-39

Revision

B2-

January,

2006

TitlePage New

LOEP New

LOR New

2-30 RevisedPlacards

3-8 Revised"AirStart”

3-21 Revised “Loss ofOne Alternator’

6-7 Revised Illustration

8-1thru8-4 Revised Table of Contents

8-5 Revised "IntroductiontoServicing”and

“Publications”

8-7 Revised “Preventive Maintenance that

maybe AccomplishedbyaCertificated

Pilot”

8-12 I Revised "Storage"

8-14 Revised“Fuel CeIls”

8-18 Revised “Batteries”

8-22 Revised “Shimmy Damper" and "Brakes"

PAGE B25

826

832

LogOfRevisions(Cont’d)

PIN58-590000-39 Revision B2-

January"

2006 Revised Revlsed Revised DESCRIPTION

Heating and VentilatingSystem

Alternators Consumable Materials Deleted and Shifted Data

|8-28and 8-29 Revised“ExteriorPainted Surface"

I

I

aylhellll

Aircraft

Loc.

OF

Revisions

Baron® 58/58A

(SerialsTH-1472andAfter,ExceptTH-1476,

TH-1487,TH-1489,andTH-1498)

Pilot’s

Operating Handbook

and

FAA

Approved Airplane

Flight

Manual

P/N

58-590000-39

Revision

B1 -

June,

2004

TitlePage New

LOEP New

LOR New

2-19 RevisedPlacard

3-18 Revised “Electrothermal Propeller Deice System”

4-1 and 4-2 Revised Table ofContents

4-12and 4-13 Revised “BeforeTakeoff"and ShiftedData

4-33thru 4-35 Added“Heater Operation” and revised

“Wind-shield Defogging"

4-36thru 4-40 Shifted Data

7-1 thru 7-4 Revised TableofContents

7-28and 7-29 Revised“FuelCells"

7-30thru 7-32 Revised Illustrations

7-40thru 7-52 Revised“LightingSystem", “Environmental

Sys-tem" and ShiftedData

B1

1of 1

llaylhalbll

Aircraft

B°°°"

B°'°"

58

"

SECTION

|

GENERAL

TABLE OF

CONTENTS

SUBJECT

PAGE

Introduction

.._.,._.._..._..

...

1

-3

Important Notice

...

...

1

-4

Use

ofthe

Handbook

...

...

1-5

Warnings,

Cautions, and Notes

...._...

_..._....1-5

Revising

The Handbook

..._.

...

1

-6

Revision

Service

,.._..._..._..,....

.A_.._...1

-7

Supplements

._...,...

;

..._...._.

...

1

-8

AnmaneFHghtManualSupmemenw

Revision

Record

...,...

ii.

..._..

.,...

1

-9

Airplane

Three

View

...

... 1-10

,s

Ground

Turning

Clearance

...

...

1-11

Descriptive

Data

...

...

1

-12

Engines

...

...

1

-12

Number

oi

Engines

...

_...

1

-12

Engine

Manufacturer

...

...

1

-12

Engine

Model

Number

..._..

...

1

-12

Engine

Type

...

...

1

-12

Horsepower

Rating

...._..._.

...

1

-12

Number

oi

Propellers

...

...

1

-12

Propeller

Manufacturer

...

...

1

-12

Number

of

Blades ...

...

1

-13

Propeller

Type

...

...

1

-13

Pitch

Settings

(30-inch

Station)

...

...

1

-13

Propeller

Diameter ...

...

1

-13

Fuel

...

._...

1

-13

Approved Engine

Fuels ...

...

1

-13

Fuel

Capacity

...

...

1

-13

Standard

System

...

...

1

-13

//-`

Optional

Systems

.._....

..._

1

-14

Engine

Oil

..._.._..._..

..._.

1

-14

June,

2003

1-1

FOR

CLASSROOM

USE

Beech Baron

58

|\3y|'|l¢llll

Aircraft

SECTION

I

GENERAL

TABLE OF CONTENTS

_(C0nt’d)

SUBJECT

Oil

Capacity

...__.__

Specification ..._.._,..

Maximum

Certificated

Weights

..._

PAGE

...1-14

...1-14

...‘|-15

Cabin

and

Entry

Dimensions ..._...,...

...

1

15

Cabin

Baggage Volumes

..._....__,_...

1

15

Specific

Loadings

(At

_{Maximum Take-olf Weight)}

_...

_1-15

Symbols,

Abbreviations and Terminology

...

1-16

General Airspeed

Terminology

...

...

1

16

Meteorological

Terminology ..._..._...i...

...

1

19

Power

Terminology., .,.._...,...,...

_1-20

Engine

Controls

_{and Instruments Terminology ...}

_1-20

Airplane

Performance

and

Flight

Planning Terminology

._.,___._._..__

Weight

_{and Balance Terminology ...}

1-2

FOR

CLASSROOM

USE

ONLY

...1-21

...1-22

||ay"lG|||\

Aircraft

Section

l

Beech Baron

58

_General

INTRODUCTION

The

format

and

contents

of

this

Pilot’s

Operating Handbook and

FAA

Approved Airplane

Flight

Manual

conform

to GAMA

(Gen-eral Aviation

_{Manufacturers Association) Handbook}

Specifica-tion No.

1

through Revision

No.

2,

dated October

18,

1996. Use

of

_this

specification

by

all

manufacturers

will

provide

the

pilot

with

the

same

type

of

_data

in

the

same

place

in

all

handbooks.

Attention

is

called

to

Section

X,

SAFETY INFORMATION.

Ray-theon

Aircraft

feels

that

it is

highly

important

to

have Safety

ln-formation

in

_condensed

form

in

the

hands

of

the

pilots.

The

Safety

information

should

be

read and studied.

Periodic review

will

serve

_as

a

reminder

of

good piloting

techniques.

Use only

genuine Raytheon

Aircraft

or

Raytheon

Aircraft

approved parts obtained

from

Raytheon

Aircraft

approved

sources,

in

connection

with

the

maintenance and

repair

of

Beech airplanes.

Genuine Raytheon

Aircraft

parts

are

produced

and inspected under rigorous

procedures

to

en-sure

airworthiness

and

suitability for

use

in

Beech

airplane applications.

Parts

purchased

from

sources

other

than

Raytheon

Aircraft,

even

if

out-wardly

identical

in

appearance,

may not

have had

the

required

tests

and

inspections

performed,

may

be

different

in

fabrication techniques and

materials,

and

may

be

dangerous

when installed

in

an

airplane.

Salvaged

airplane

parts,

reworked parts obtained

from

non-Raytheon

Aircraft

approved

sources,

or

parts,

components,

or

structural

assemblies,

the

June,

2003

_1-3

FOR

CLASSROOM

USE

Se¢[iQ|»'|

|

Aircraft

General

_{Beech Baron}

₅₈

service

history

of

which

is

unknown or

cannot

be

authenticated,

may

have been subjected

to

unac-ceptable

stresses

or

temperatures

or

have other

hidden

damage,

not

discernible through routine

visual or

usual

nondestructive testing

techniques.

This

may

render

the part,

component,

or

structur-al

assembly,

even though

originally

manufactured

by

Raytheon

Aircraft,

unsuitable

or

unsafe

for

air-plane use.

Raytheon

Aircraft

expressly disclaims any

re-sponsibility for

malfunctions, failures,

damage

or

injury

caused

by

use

of

non-Raytheon

Aircraft

ap-proved

parts.

_

IMPORTANT NOTICE

This

handbook should be read

carefully

by

the

owner

and

the

operator

in

order

to

become

familiar

with

the

operation

of

the

airplane.

_{Suggestions and recommendations have been made}

within

it

to

aid

in

obtaining

maximum

performance

without

sac-rificing

economy.

Be

familiar

with,

and

operate the

airplane

in

accordance

with,

the

Pilot’s

Operating

Handbook and

FAA

Ap-proved

Airplane

Flight

Manual

_and/or

placards

which

are

locat-ed

in

the

airplane.

This

handbook includes

the

_material

_required

to

be

furnished

to

the

pilot by

the

Title 14

Code

of

Federal

Reg-ulations

and

additional information provided

by

the

manufactur-er

and

constitutes

the

FAA

Approved Airplane

Flight

Manual.

As a

further

reminder,

the

owner

and

the

operator should

also

be familiar

with

the Title

14

Code

of

Federal Regulations

appli-cable

to

the

operation and maintenance

of

the

_{airplane, and,}

_as

appropriate

14

CFR

Part

91

_{General Operating and}

Flight

Rules.

Further, the

airplane

must be

operated

and maintained

in

accordance

with FAA

_{Airworthiness Directives which may}

_be

issued

against

it.

1-4

_June,

₂₀₀₃

FOR

CLASSROOM

USE

||3y|'|lEl|ll

Aircraft

section

i

Beech Baron

58

General

The

Title 14

Code

of

Federal

_Regulations

place

the

responsibil-

|

ity

for

the

maintenance

of

this

airplane

on

the

owner

and

the

op-erator,

who

should

ensure

that

all

maintenance

is

done

by

|

qualified

mechanics

in

conformity

with

all

airworthiness

require-ments

established

for

this

airplane.

All

limits,

procedures, safety practices,

time

limits,

servicing,

and

maintenance requirements contained

in

this

handbook are

considered mandatory

for

continued airworthiness and

to

main-

|

tain the

_airplane

in

a

condition

equal

to

that

of its

original

man-ufacture.

Raytheon

Aircraft

Authorized

Outlets can

provide

recommend-

|

ed

modification,

service,

and operating

procedures

issued

by

both

the

FAA

and Raytheon

Aircraft, which

are

designed

to

get

maximum

utility

and

safety

from

the

_airplane.

USE

OF THE HANDBOOK

WARNINGS, CAUTIONS,

AND

NOTES

The

following

definitions apply

to

(WARNINGS), (CAUTIONS),

and

(NOTES) found

throughout

the

handbook:

Operating procedures, techniques,

etc.,

which

could result

in

personal

injury

or

loss

of life

if

not

carefully followed.

Operating procedures, techniques, etc.,

which

could result

in

_damage

to

equipment

if

not

care-fully

followed.

June,

2003

1-5

FOR

CLASSROOM

USE

semioni

llilylhellll

Aircraft

General

_{Beech Baron}

₅₈

NOTE

An

operating procedure, technique, etc.,

which

is

considered

essential

to

emphasize.

REVISING THE

HANDBOOK

The

Pilot's

Operating

Handbook

is

designed

to

facilitate

main-taining

the

documents

necessary

for

the

safe and

efficient

op-eration

of

the

airplane.

The handbook

has

been

prepared

in

loose-leaf

form

for

ease

in

maintenance.

It

incorporates

quick-reference tabs

imprinted

with

the

title

of

each

section.

NOTE

ln

an effort

to

provide

_as

complete

coverage as

possible, applicable

to

any

configuration

of

the

airplane,

some optional equipment has been

in-cluded

in

the

scope

of

the

handbook.

However,

due

to

the variety

of

_{airplane appointments and}

arrangements available,

optional

equipment

de-scribed

or

depicted

herein may not

be

designated

as

such

in

every

case.

Immediately

following

the

Title

Page

is a List

of

Effective

Pages.

A

complete

listing

of all

pages

is

presented

along

with

the

cur-rent

status

of

the material

contained;

i.e.

Original

Issue,

Fleis-sued

or Flevised.

A

reissue

of

the

manual

or

the

revision

of

any

portion

will

_be

_received

with a

new

List

of

Effective

Pages

to

re-place the

previous one. Reference

to

the

List

of

Effective

Page(s)

enables

the

user

to

determine

the

current

issue,

revi-sion,

or

reissue

in

effect for

each

page

in

the

handbook, except

for

the

Supplements

Section.

1-6

_June,

₂₀₀₃

FOR

CLASSROOM

USE

||3y|'|lG0ll

Aircraft

section:

Beech Baron

58

General

When

the

handbook

is

originally

issued, and each

time

it

is

re-vised or

reissued,

a

new

Log

of

_Revisions

_page

is

provided

im-mediately

following

the

List of

Effective

Pages.

All

Log

ol

Revisions

pages

must

be retained

until

the

handbook

is

reis-sued.

A

capital

letter

in

the lower

right

corner

of

the Log

of

Re-visions

page

designates the

Original

lssue

(“A")

or

reissue

("B"

"C",

etc.)

covered

by

the Log

of

Revisions

page.

lf

a

number

fol-lows the letter,

it

designates

the

sequential

revision

(lst,

2nd,

3rd,

etc.)

to

the Original

Issue

or

reissue covered

by

the Log

of

Revisions

page.

Reference

to

the Log

ol

Revisions

page(s)

pro-vides

a

record

of

_changes

_{made since}

the Original

Issue

or

the

latest

_reissue.

That portion

of

a

text or

an

illustration which

has

been revised

by

the addition

of,

or

a

change

in,

information

is

denoted

by a

solid

revision

bar located

adjacent

to

the

area

of

change

and

placed

along the

outside

margin

ofthe

page.

nEv|s|oN

sEnv|cE

The

following

_publications

will

be

provided, at

no

charge,

to

the

registered owner/operator

of

this

airplane:

1.

Reissues and

revisions

of

the

Pilot’s

Operating

Hand-book

and

FAA

Approved Airplane

Flight

Manual.

2.

Original

issues

and

revisions

of

FAA

Approved Airplane

Flight

Manual

Supplements.

3.

Original

issues

and

revisions

of

Raytheon

Aircraft

Service

Bulletins.

The

above

publications

will

be

provided only

to

the

registered

owner/operator

at

the

address

listed

on

the

FAA

Aircraft

Regis-tration

Branch

List

or

the

Raytheon

Aircraft

Domestic/lnterna-tional Owner‘s Notification

Sen/ice

List.

Further,

the

owner/

operator

will

receive

only

those

publications

pertaining

to

the

registered airplane serial

number. For

detailed

information

on

how to

obtain

“Revision

Sen/ice"

applicable

to

this

handbook

or

other Raytheon

Aircraft

Service

Publications,

consult any

Ray-June,

2003

1-7

FOR

CLASSROOM

USE

Segiign

|

Aircraft

General

_Beech

_B8l'OI'l

₅₈

theon

Aircraft

Authorized Outlet

or

refer

to

the

latest

revision

of

Raytheon

Aircraft

Service

Bulletin No.

2001.

Raytheon

Aircraft

expressly

reserves

the

right to

supersede,

cancel,

_{and/or declare obsolete,}

without

prior

notice, any part,

part

number,

kit,

or

publication

referenced

in

this

handbook.

The

owner/operator should always

refer

to

all

supplements

for

possible placards,

limitations,

emergency, abnormal,

normal

and

other operational

procedures

for

proper operation

of

the

airplane

with

optional

equipment

installed.

lt

shall be

the

responsibility

of

the

owner/operator

to

ensure

that the

latest

revisions

of

publications

referenced

in

this

handbook

are utilized

during

operation, sen/icing, and maintenance

of

the

air-plane.

SUPPLEMENTS

When

a

new airplane

is

delivered

from

the factory, the

hand-book

delivered

with

it

contains either

an

STC

(Supplemental

Type Certificate)

Supplement

or

a

Raytheon

Aircraft Flight

Manual

Supplement

for

every installed item requiring

a

supple-ment.

lf

a

new handbook

for

operation

of

the

airplane

is

ob-tained

at

a

later

date,

it is

the

responsibility

of

the

owner/

operator

to

ensure

that

all

_required

STC

Supplements

(as

well

as

weight

and

balance

and other peninent data)

are

transferred

into

the

new

handbook.

1-8

_June,

₂₀₀₃

FOR

CLASSROOM

USE

llaylhellll

Aircraft

secnoni

Beech Baron

58

General

AIRPLANE

FLIGHT

MANUAL

SUPPLE-MENTS

REVISION

RECORD

Section

IX,

SUPPLEMENTS,

contains

the

FAA-approved

Air-plane

Flight

Manual

Supplements,

headed

by

a

Log

of

Supple-ments

page. When new

supplements

are

received

or

existing

supplements

are

revised,

a

new

Log

page

will

_replace

the

pre-vious

one,

since

it

contains

a

listing

of all

_previous

_approvals,

plus

the

new approval.

The supplemental material

will

be added

to

the

Section

in

accordance

with

the

sequence

specified

on

the

Log

page.

NOTE

Upon

receipt

ot a

new or

revised

supplement,

compare

the existing

Log of

Supplements

in

the

handbook

with

the

corresponding applicable

Log

page accompanying

the new or

revised

supple-ment.

lt

may occur

that the Log

page already

in

the

handbook

is

dated

later

than

the Log

page

ac-companying

the

new or

revised supplement.

In

any

case,

retain

the

Log

page

having the

later

date

and discard

the older

Log

page.

June,

2003

1-9

FOR

CLASSROOM

USE

Segtign

|

Aircraft

General

Beech Baron

58

i-i15'11"

W\NG AREA:

199.2

SQ

FT

l

I » I

_{_}

Q

H

A

I

V

!

V

77

DIAMETER

f

,.

Q

37'1O"

4 »

9'»~

0

S

l»a'1‘$-”;|;_1o'4"

1

29'10"

KC

AIRPLANE THREE-VIEW

1-10

_June,

₂₀₀₃

FOR

CLASSROOM

USE

llaylllellll

Aircraft

Section!

Beech Baron

58

General

GROUND TURNING CLEARANCE

,'

_;Q;v;`7

7

I

\

°

RADIUS FOR WING TIP

...

31 FT.

6

IN.

6

RADIUS FOR

NOSE

WHEEL

...

15 FT.

6

IN.

a

RADIUS FOR INSIDE GEAR

...

7FT. 11 IN.

9

RADIUS

FOR

OUTSIDE GEAR

...

17 FT.6 IN.

TURNINGRADIIARE PREDICATED ON THE USE OF PARTIAL BRAKINGACTIONANDDIFFERENTIAL

POWER.

THOOC

020334AA,AI

June,

2003

1-11

FOR

CLASSROOM

USE

secrioni

llaylheoll

Aircraft

General

Beech Baron

58

DESCRIPTIVE

DATA

ENGINES

NUMBER

OF ENGINES

Two

ENGINE

MANUFACTURER

Teledyne Continental

Motors

Corporation

(Mobile,

Alabama)

ENG/NE

MODEL

NUMBER

IO-550-C

ENGINE TYPE

Normally

aspirated,

Foel-injected, direct-drive,

air-cooled,

six-cylinder, horizontally

opposed,

550~cubic-inch

displacement

HORSEPOWER

RATING

300 H.P.

NUMBER

OF

PROPELLERS

Two

PROPELLER

MANUFACTURER

McCauley

Propeller

(Vandalia, Ohio)

(Refer

to

supplement

HPBE58-2 for

airplanes

equipped

with

Harlzell

prope//ers.)

1-12

_June,

₂₀₀₃

FOR

CLASSROOM

USE

na“'|l¢0|\

AiI'CI‘21fI

Section

I

Beech Baron

58

General

NUMBER

OF

BLADES

Three

PROPELLER TYPE

Constant~speed,

variable-pitch,

three-blade

propeller using

a

3AF32C512-(X)

hub

with

(X)-82NEA-5

blades.

NOTE

The

letters

appearing

in

the

place

of

the

(X)

rep-resent

minor

variations

in

the

propeller hub or

blades.

They

do not affect

eligibility

or

inter-changeability.

PITCH

SETTINGS (30-INCH

STA

TION)

Low

...

..._...

15.2°

1

O.2°

Feathered

...

....

8

2.5"

1 0.5°

PROPELLER DIAMETER

77

inches

FUEL

APPROVED ENGINE FUELS

Aviation

Gasoline

Grade

100LL

(blue)

Aviation

Gasoline

Grade

100

(green)

Aviation

Gasoline

Grade

115/145

(purple)

FUEL

CAPACITY

STANDARD

SYSTEM

Total

Capacity

...

....

1

42

Gallons

Total

Usable

...

....

1

36

Gallons

June,

2003

1-13

FOR

CLASSROOM

USE

Segfign

|

Aircraft

General

Beech Baron

58

OPTIONAL

SYSTEMS

Total

Capacity

...

__ _

172

Gallons

Total

Usable

__ _

...

__ _

166

Gallons

or

Total

Capacity

....

. . _.

200 Gallons

Total

Usable

.._..

_ __

194

Gallons

ENGINE OIL

O/L

CAPACITY

Total

_._...

...__

1

2

Ouarts

(each engine)

SPE

CIFICA

T/ON

Use

MIL-L-22851

Ashless Dispersant

Oils

meeting

the

require-ments

of

the

latest

revision

of

Teledyne Continental

Motors

Corporation

Specification

MHS-24B or

current applicable

Tele-dyne

Continental

Sen/ice

Bulletin.

Refer

to

Section

Vlll,

HAN-DLlNG,

SERVICING

AND

MAINTENANCE

for

a

list

of

approved

oils.

Ambient

Air

Single Viscosity

Multiviscosity

Temperature

Grade

Oil

Grade

Oil

Below

5°C

SAE

30 (max.)

15W-50,

20W-50

Above

5°c

sAE so

(min.)

ggwigg'

2°W'5°

When

operating

temperatures

overlap

indicated

ranges, use

|

the lighter

grade

of oil.

1-14

_June,

2003

FOR

CLASSROOM

USE

||ily|'|lBlll\

Aircraft

secuoni

Beech Baron

58

General

MAXIMUM

CERTIFICATED

WEIGHTS

Model 58:

Maximum

Take-ott

Weight

...

5500

Ibs

Maximum

Landing Weight

....

5400

Ibs

Maximum

Ramp

Weight

....

5524 lbs

Model 58A:

Maximum

Take-oft Weight

...

...

4

990 lbs

Maximum Landing

Weight.

. _

...

4990

lbs

Maximum

Ramp

Weight

...

...

5

O14

Ibs

CABIN AND ENTRY

DIMENSIONS

Cabin

Length

...

12

tt

7

in.

Cabin

Width

(max.)

...

...

3

ft 6

in.

Cabin Height'(max.)

...

...

4

tt

2

in.

Fwd Cabin

Door

. . .

...

37

in.

wide

x

36

in.

high

Att Utility

Door

....

...

4 5

in.

wide

x

35

in.

high

CABIN

BAGGAGE

VOLUMES

Aft

Cabin

Compartment

...

....

3 7

cu

ft

Between

Spars

...

....

1

2

cu

ft

Extended Rear Compartment

....

....

1

0

cu

ft

Nose

Compartment

...

....

1

8

cu

ft

SPECIFIC

LOADINGS

(At

Maximum

Take-off

Weight)

Wing

Loading

...

....

2

7.6

ibs/sq

ft

Power

Loading

_ .

....

9.16

lbs/hp

June,

2003

1-15

FOR

CLASSROOM

USE

5e¢u.,,,|

||3y|'|l¢Dll

Aircraft

General

Beech Baron

58

SYMBOLS,

ABBREVIATIONS

AND

TERMI-NOLOGY

The

following

glossary

is

applicable

within

this

handbook.

GENERAL

AIRSPEED TERMINOLOGY

CAS

Calibrated

Airspeed

is

the

indicated

airspeed

of

an

airplane

corrected

for

position

and instrument

error.

Calibrated

airspeed

is

equal

to

true

airspeed

in

standard

atmosphere

at

sea

level.

GS

Ground

Speed

is

the

speed

of

an airplane

relative

to

the

ground.

lAS

Indicated

Airspeed

is

the

speed

of

an

airplane

as

shown

on

the

airspeed

indicator

when

corrected

for

instrument

error.

lAS

values published

in

this

handbook

assume

zero instrument

error.

KCAS

Calibrated

Airspeed

expressed

in

knots.

KIAS

Indicated

Airspeed

expressed

in

knots.

TAS

True

Airspeed

is

the

airspeed

of

an airplane

relative

to

undisturbed

air,

which

is

the

CAS

corrected

for

altitude,

temperature, and

compressibility.

1-16

June,

2003

FOR

CLASSROOM

USE

||8y"lE0l\

Aircraft

section

i

Beech Baron

58

General

VMcA

Vsse

VA VF VFE

June,

2003

Air

Minimum Control

Speed

is

the minimum

flight

speed

at

which

the

airplane

is

directionally

controllable

as

determined

in

accordance

with Title 14

Code

of

Federal

Regulations.

The

airplane

certification

conditions

include

one

engine becoming

inoperative

and

windmilling;

a

5°

bank

towards

the

operative

engine;

take-oft

power

on

operative engine;

landing

gear

up;

flaps

in

take-off position;

and most

rearward

C.G. For

some conditions

of

weight

and

altitude, stall

can

be

encountered

at

speeds

above

VMCA

as

established

by

the

certification

procedure described above,

in

which

event

stall

speed

must

be regarded

as

the

limit of

effective

directional control.

Intentional

One-Engine-inoperative

Speed

is

a speed

above both

VMCA

and

stall

speed,

selected

to

provide

a

margin

of

lateral

and

directional control

when

one

engine

is

suddenly

rendered inoperative.

intentional

failing

of

one

engine

below this

speed

is

not

recommended.

Maneuvering

§peed

is

the maximum

speed

at

which

application

of

full

available

aerodynamic

control

will

not

overstress

the

airplane.

Design Flap

Speed

is

the

highest

speed

permissible

at which wing flaps

may be

actuated.

Maximum

F/ap

Extended

Speed

is

the

highest

speed

permissible

with wing

flaps

in

a

prescribed

extended

position.

1-17

FOR

CLASSROOM

USE

Section

l

General

VLE

V|.o

VNE

VNo

or

Vc

Vs

Vso

Vx

VY

1-18

llaylheull

Aircraft

Beech Baron

58

Maximum

Landing

_Gear

Extended

Speed

is

the maximum

speed

at which

an airplane

can

be

safely

flown with

the

landing

gear

extended.

Maximum

Landing

Gear

Operating

Speed

is

the maximum

speed

at which

the

landing

gear can

be

safely

extended

or

retracted.

Never Exceed

Speed

is

the

speed

limit

that

may not be

exceeded

at any time.

Maximum

Structural

Cruising

Speed

is

the

speed

that

should

not

be

exceeded

except

in

smooth

air

and

then

only with

caution.

Stalling

Speed

or

the minimum

steady

flight

speed

at which

the

airplane

is

controllable.

Stal/ing

Speed

or

the minimum

steady

flight

speed

at which the

airplane

is

controllable

in

the landing configuration.

Best

Angle-of-C/imb

Speed

is

the

airspeed

which delivers

the

greatest

gain

of

altitude

in

the

shortest possible

horizontal

distance.

Best

Rate-of-C/imb

Speed

is

the airspeed

which delivers the

greatest

gain

in

altitude

in

the

shortest

possible

time.

June,2003

FOR

CLASSROOM

USE

llaylheun

Aircraft

season

i

Beech Baron

58

General

METEOROLOGICAL TERMINOLOGY

Flight

in

Icing

Conditions

Indicated

Pressure

Altitude

ISA

OAT

Pressure

Altitude

June,

2003

Flight

when

the

OAT

is

5°C

(41

°F)

or

colder,

and

in

the

presence

of

visible

moisture.

The

number actually read

from

an

altimeter

when

the

barometric

subscale

has

been

set

to

29.92

inches

of

mercury

(1013.2

millibars).

International

Standard

Atmosphere

in

which:

(1)

The

air

is

a

dry

perfect

gas;

(2)

The

temperature

at

sea

level is 15°

Celsius

(59°

Fahrenheit);

(3)

The

pressure

at

sea

level is

29.92

inches

of

mercury (1013.2

millibars);

(4)

The

temperature

gradient

from

sea

level

to

the

altitude

at

which

the

temperature

is

-56.5°C (-69.7°F)

is

-0.00198°C (-0.003566°F) per

foot

and

zero

above

that altitude.

Outside

Air

Temperature

is

the

tree

air

static

temperature, obtained either

from

the

temperature

indicator

(IOAT)

adjusted

for

compressibility

effects,

or

from

ground

meteorological

sources.

Altitude

measured

from

standard sea-level

pressure

(29.92

in.

Hg/1013.2

millibars)

by

a

pressure

(barometric) altimeter.

It

is

the

indicated

pressure

altitude

corrected

for

position

and

instrument

error.

ln

this

handbook, altimeter

instrument errors

are

assumed

to

be zero.

Position

errors

may

be

obtained

from

the

Altimeter

Correction

graphs.

1-19

FOR

CLASSROOM

USE

section

r

Ilaylhellll

Aircraft

General

Beech Baron

58

Station

Actual

atmospheric

pressure

at

field

Pressure

elevation.

Wind

The

wind

velocities

recorded

as

variables

on

the

charts

of

this

handbook

are

to

be

understood

as

the

headwind

or tailwind

components

of

the

reported

winds.

POWER TERMINOLOGY

Cruise

Climb

Power

recommended

for

cruise

climb.

Economy

The

lowest power

setting

for which

cruise

Cruise

power

settings

are

presented.

Maximum

The highest

power

settings

recommended

Cruise

for

cruise.

Recommended

intermediate

power

settings

for

which

Cruise

cruise

power

settings

are

presented.

Take-off

and

Highest power rating not limited

by

time.

To

Maximum

be

used

only for

conditions

which

warrant

Continuous

the

use

of

this

rating.

ENGINE

CONTROLS

AND

INSTRUMENTS

TERMI-NOLOGY

Manifold

Pressure

Gage

Mixture

Control

1-20

An

instrument

that

measures

the

absolute

pressure

in

the

intake manifold

of

an

engine,

expressed

in

inches

of

mercury

(in.

Hg).

This

lever,

in

the idle

cut-off

position,

stops

the

flow

of

fuel

at the injectors

and

in

the

intermediate

through the

full

rich

positions,

regulates

the

fuel

air mixture.

June,

2003

FOR

CLASSROOM

USE

nay|’||B||||

Aircraft

Section

I

Beech Baron

58

General

Propeller

The governor maintains

the

selected_ rpm

Governor

requested

by

the

propeller

control

leverl

Propeller

This lever

requests

the

governor

to

maintain

Control

rpm

at

a selected

value and,

in

the

full

decrease

rpm

position,

feathers

the

propeller.

Throttle

The

lever

used

to

control

the

forced

Control

introduction

of

a

fuel-air mixture

into

the

intake

passages

of

an engine.

Tachometer

An

instrument

that

indicates

the

rotational

speed

of

the

propeller

in

revolutions

per

minute (rpm).

AIRPLANE

PERFORMANCE

AND

FLIGHT

PLANNING

TERMINOLOGY

Accelerate-

The distance required

to

accelerate

an

Stop Distance

airplane

to

a

specified

speed

and,

assuming

failure

of

an engine

at

the

instant

that

speed

is

attained,

to

bring the

airplane

to

a

stop.

Accelerate-Go

The distance required

to

accelerate

an

Distance

airplane

to

a

specified

speed

and,

assuming

failure

of

an

engine

at

the

instant

that

speed

is

attained,

feather

inoperative

propeller

and continue

takeoff

on

the

remaining

engine

to a

height

of

50 feet.

Climb

Gradient

The

ratio

of

the

change

in

height during

a

portion

of

a

climb to

the

horizontal

distance

traversed

in

the

same

time

interval.

June,

2003

1-21

FOR

CLASSROOM

USE

Section

I

General

Demonstrated

Crosswind

Velocity

GPH

MEA

Route

Segment

||3y|'|l¢0ll

Aircraft

B€€C|'l

B8I'0l"l

58

The velocity

ofthe

crosswind

component

for

which

adequate

control

of

the

airplane

during

takeoff

and

landing

was actually

demonstrated

during certification

tests.

The

value

shown

is

not

limiting.

U.S.

Gallons

per

hour.

Minimum

Enroute

IFR

Altitude.

A

part

of

a

route.

Each end

of

that

part

is

identified

by: (1)

A

geographical

location;

or

(2)

A

point at

which

a

definite radio

fix

can

be

established.

WEIGHT AND

BALANCE TEFIMINOLOGY

Airplane

Center

of

Gravity

(C.G.)

Arm

Basic

Empty

Weight

C.G.

Arm

C.G.

Limits

1-22

The

point at which

an airplane

would

balance

it

suspended.

its

distance

from

the

reference datum

is

found

by

dividing

the

total

moment

by

the

total

weight

of

the

airplane.

The

horizontal

distance

from

the

reference

datum

to

the center

of

gravity (C.G.)

of

an

item.

Standard

empty

weight

plus

optional

equipment.

The arm

obtained

by

adding

the

airplane’s

individual

moments and

dividing by

the

sum

of

the total weight.

The

extreme

center

of

gravity

locations

within

which

the

airplane

must

be operated

at

a

given

weight.

June,

2003

FOR

CLASSROOM

USE

||3y|'|'I¢0ll

Aircraft

secriani

Beech Baron

58

_General

Jack Points

Leveling

Points

Loading

Condition

Maximum

Ramp

Weight

Maximum

Take-off

Weight

Maximum

Landing

Weight

Moment

Payload

Reference

Datum

Standard

Empty

Weight

June,

2003

Points

on

the

airplane

identified

by

the

manufacturer

as

suitable

for

supporting

the

airplane

for weighing or

other

purposes.

Those

points which

are

used

during

the

weighing

process

to

level

the

airplane.

That

combination

of

airplane

weight

and

corresponding moment applicable

to

the

various loadings computed

for

weight

and

balance purposes.

Maximum

weight

approved

for

ground

maneuvering (includes

weight

of

start,

taxi,

and

run up

fuel).

Maximum weight

approved

for

the

start

of

the take-off run.

Maximum

weight

approved

for

the

landing

touchdown.

The

product

of

the

weight

of

an

item

multiplied

by

its

arm.

(Moment divided

by a

constant

is

used

to

simplify

balance

calculations

by

reducing the

number

of

digits)

Weight

of

_{occupants, cargo and baggage.}

An

imaginary

vertical

plane

from

which

all

horizontal

distances

are measured

for

balance

purposes.

Weight

of

a

_{standard airplane}

including

unusable

fuel,

full

operating

fluids

and

full

oil

1-23

FOR

CLASSROOM

USE

Section

I

General

Station

Tare

Unusable

Fuel

Useful Load

Usable

Fuel

Zero Fuel

Weight

1-24

llaylheull

Aircraft

Beech Baron

58

A

location along

the

_airplane

_fuselage

usually given

in

terms

of

distance

from

the

reference datum.

The

weight

ol

chocks,

blocks,

stands,

etc.,

used

on the

scales

when weighing

an

airplane.

The

luel

remaining

after

consumption

of

usable

fuel.

Difference

between

Fiamp

Weight,

and

Basic Empty Weight.

That portion

of

the total fuel which

is

avlalable

for

consumption

as determined

in

accordance

with

applicable

regulatory

standards.

Weight

exclusive

of

usable

fuel.

June,

2003

FOR

CLASSROOM

USE

llaylhellll

Aircraft

B°°°"

B“'°"

5°

2%

SECTION

ll LIMITATIONS TABLE OFCONTENTS SUBJECT _PAGE

AhspeedLhnhaHons

... ...2%

Alrspeedindicator Markings... ...2 -4

PowerPlant Limitations ... ... 2 -4

NumberofEngines... ...2 -4

EngineManufacturer ... ...2 -4

EngineModel Number ... ... 2 -4

Engine Type ... ... 2 -5

EngineOperating Limitations ... .._... 2 -5

FuelLimits ... ...2 -5

Approved Engine Fuels ... ...2 -5

~ _{Fuel Capacity ...,... ...2 -5}

StandardFuelSystem... ...2 -5

Optional FuelSystems... ... 2 -6

FuelManagement...t... ...2 -6 OilSpecification ,... ...._...2-6 NumberofPropellers... ...2 -6 PropellerManufacturer ... ...2 -6 NumberofBlades ..._... ...2 -7 PropellerType... ...2 -7

Pitch Settings (30-inch Station) ... ...2 -7

PropellerDiameter... ...2 -7

Power Plant

Instrument

Markings... ...2 -7 OilTemperature ... ...2 -8 OilPressure ... ... 2-8

Fuel Flow... ...2 -8

ManifoldPressure... ...._... 2 -8

Tachometer ...,... ...2 -8

CylinderHeadTemperature ... ...2 -8

f`

Miscellaneous

Instrument

Markings ... ...._... 2 -9

instrumentPressure ..._... ...2 -9

;

@

f.

Bawheon

Mrcraft

seciacn

||

Beech Baron

58

Limitations

Ai/

_{airspeeds quoted}

inthis section

are

indicated

airspeeds

(IAS)

except

as noted and assume

zeroinstrumenterror.

TheIimitationsincludedinthis section havebeen approvedby

the Federal Aviation Administrationand must be

obsewed

in

theoperationofthis airplane.

AIRSPEED

LIMITAT

ONS

SPEED KCAS KIAS REMARKS

NeverExceed 223 223 Do notexceed this speed

(VNE) in anyoperation.

Maximum 195 195 Do not exceed this speed

Structural except in smooth air and

Cruising then onlywithcaution.

(VuoorVc)

Maneuvering 156 156 Donotmaketull or abrupt

(VA) control movements above

thisspeed.

Maximum Flap Do not extend ilaps or

Extension/ operatewithtlaps extended

Emended(VFE) above thisspeed.

Approach (15°) 152 152

FullDown (30°) 122 122

Maximum 152 152 Do not extend, retract or

LandingGear operatewithgear extended

Operating above thisspeed.

Extended(VLQNLE)

Singie-Engine 83 84 Minimum speed tor

MinimumControl directional controllability

Speed aher sudden loss ot

(VMCA) engine.

MaximumWith 174 174 Utility door Oremoval kit

UtiliwDoors must be installed.

Removed

Sectign

||

Mrcraft

Limitations

Beech Baron

58

AIRSPEED

INDICATOR

MARKINGS*

MARKING KCAS VALUEOR KIASVALUEOR SIGNIFICANCE

RANGE RANGE

White Arc 73-122 74~122 FullFlapOperating

Range

WhiteTriangle 152 152 Maximum Flap

Approach Position

15°

BlueRadial 10O 10O Single-Engine Best

Rate-oi-C|imb Speed

Red Radial 83 84 Minimum

Single-EngineControl

(VMCA)

GreenArc 83~ 195 84-195 Nomal Operating

Range

YellowArc 195-22S 195~223 operare waih

ca;

tion,onlyin smoth

air

RedRadial 223 223 Maximumspeedior

ALLoperations

'TheairspeedindicatorismamedinlASvalues.

POWER PLANT LIMITATIONS

NUMBER OF

ENGINES

Two

ENGINE

MANUFACTURER

Teledyne ContinentalMotors Corporation(Mobile,Alabama)

ENGINEMODEL NUMBER

IO-55O-C