Cessna 182Q 1979 Owner's manual

PILOT'S OPERATING HANDBOOK
and
FAA APPROVED AIRPLANE FLIGHT MANUAL
"' CESSNA AIRCRAFT COMPANY I
I1979 MODEL
182Q I
THIS DOCUMENT MUST BE
CARRIED IN THE AIRPLANE
AT ALL TIMES.
Serial No. /f;z {;; 7 ('70
Registration No. IV 97" 9{,
C - G.\ '\ r-
THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE
FURNISHED TO THE PILOT BY CAR PART 3AND CONSTITUTES
THE FAA APPROVED AIRPLANE FLIGHT MANUAL.
COPYRIGHT ©1978
CESSNA AIRCRAFT COMPANY
WICHITA, KANSAS, USA
D1141-13PH-RPC-2.000-8/78
1 OCTOBER 1978

THIS MANUAL WAS PROVIDED FOR THE AIRPLANE
IDENTIFIED ON THE TITLE PAGE ON J/ -/ J' 77' .
SUBSEQUENT REVISIONS SUPPLIED BY CESSNA
AIRCRAFT COMPANY MUST BE PROPERLY IN-
SERTED.
4
TLL
:tZ'b /vf7~L~/
CESSNA AIRCRAFT COMPANY, PAWNEE DIVISION'

CESSNA
MODEL 182Q
CONGRATULATIONS
CONGRATULATIONS ••••
Welcome to the ranks of Cessna owners! Your Cessna has been designed and
constructed to give you the most in performance, economy, and comfort. It is our desire that
you will find flying it, either for business or pleasure, a pleasant and profitable experience.
This Pilot's Operating Handbook has been prepared as a guide to help you get the most
pleasure and utility from your airplane. It contains information about your Cessna's
equipment, operating procedures, and performance; and suggestions for its servicing and
care. We urge you ~o read it from cover to cover, and to refer to it frequently.
Our interest in your flying pleasure has not ceased with your purchase of a ~essna.
World-wide, the Cessna Dealer Organization backed by the Cessna Customer Services
Department stands ready to serve you. The following services are offered by most Cessna
Dealers:
• THE CESSNA WARRANTY, which provides coverage for parts and labor, is available at
Cessna Dealers worldwide. Specific benefits and provisions of warranty, plus other
important benefits for you, are contained in your Customer Care Program book,
supplied with your airplane. Warranty service is available to you at authorized Cessna
Dealers throughout the world upon presentation of your Customer Care Card which
establishes your eligibility under the warranty.
•FACTORY TRAINED PERSONNEL to provide you with courteous expert service.
•FACTORY APPROVED SERVICE EQUIPMENT to provide you efficient and accurate
workmanship.
• A STOCK OF GENUINE CESSNA SERVICE PARTS on hand when you need them.
• THE LATEST AUTHORITATIVE INFORMATION FOR SERVICING CESSNA AIR-
PLANES, since Cessna Dealers haveall of the Service Manuals and Parts Catalogs, kept
current by Service Letters and Service News Letters, published by Cessna Aircraft
Company.
We urge all Cessna owners to use the Cessna Dealer Organization to the fullest.
A current Cessna Dealer Directory accompanies your new airplane. The Directory is
revised frequently, and a current copy can be obtained from your Cessna Dealer. Make your
Directory one of your cross-country flight planning aids; a warm welcome awaits you at
every Cessna Dealer.
1 October 1978 i

PERFORMANCE-
SPECIFICATIONS
CESSNA
MODEL 182Q
PERFORMANCE -SPECIFICATIONS
880NM
6.2 HRS
1095 NM
9.7 HRS
1010 FPM
16,500 FT
705 FT
1350 FT
2960 LBS
_____ J
2950 LBS
590 FT
1350 FT
1700 LBS
1754 LBS
56 KNOTS i
50 KNOTS
1260 LBS
1206 LBS
200 LBS
16.9
12.8
92
GAL.
12 QTS
0-470-U
82 IN.
. Range
Time
. Range
Time
SPEED:
Maximum at Sea Level 148 KNOTS
Cruise, 75% Power at 8000 Ft 144 KNOTS
CRUISE: Recommended lean mixture with fuel allowance for
engine start, taxi, takeoff, climb and 45 minutes
reserve at 45% power.
75% Power at 8000 Ft ....
88 Gallons Usable Fuel
Maximum Range at 10,000 Ft
88 Gallons Usable Fuel
RATE OF CLIMB AT SEA LEVEL
SERVICE CEILING ....
TAKEOFF PERFORMANCE:
Ground Roll . . . . . .
Total Distance Over 50-Ft Obstacle
LANDING PERFORMANCE:
Ground Roll ..........
Total Distance Over 50-Ft Obstacle
/ STALL SPEED (CAS):
." Flaps Up, Power Off
Flaps Down, Power Off
MAXIMUM WEIGHT:
Ramp .
Takeoff or Landing . .
STANDARD EMPTY WEIGHT:
Skylane .
Skylane II .
MAXIMUM USEFUL LOAD:
Skylane .
Skylane II .
BAGGAGE ALLOWANCE
WING LOADING: Pounds/ Sq Ft
POWER LOADING: Pounds/HP
FUEL CAPACITY: Total
OIL CAPACITY . . . . . . .
ENGINE: Teledyne Continental
230 BHP at 2400 RPM
PROPELLER: Constant Speed, Diameter
ii 1 October 1978

CESSNA
MODEL 182Q
COVERAGE/REVISIONS/
LOG OF EFFECTIVE PAGES
COVERAGE
The Pilot's Operating Handbook in the airplane at the time of delivery from Cessna Aircraft
'Jmpany contains information applicable to the 1979 Model 182Q airplane designated by the serial
number and registration number shown on the Title Page of this handbook.
REVISIONS
Changes and/or additions to this handbook will be covered by revisions published by Cessna
Aircraft Company. These revisions are distributed to all Cessna Dealers and to owners of U. S.
Registered aircraft according to FAA records at the time of revision issuance.
Revisions
should be examined immediately upon receipt and incorporated in this handbook.
NOTE
It is the responsibility of the owner to maintain this handbook in acurrent
status when it is being used for operational purposes.
Owners should contact their Cessna Dealer whenever the revision status of their handbook is in
question.
Arevision bar will extend the full length of new or revised text and/or illustrations added on new
or presently existing pages. This bar will be located adjacent to the applicable revised area on the
outer margin of the page.
All revised pages will carry the revision number and date on the applicable page.
The following
Log of Effective Pages provides the dates of issue for original and revised pages, and
ii5ting of all pages in the handbook. Pages affected by the current revision are indicated by an
3sterisk (*)
preceding the pages listed.
LOG OF EFFECTIVE PAGES
Dates of issue for original and revised pages are:
Original 1 October 1978
NOTE
Refer to Section 9Table of Contents
for supplements applicable to optional
systems.
6-1 1 October 1978
6-2 Blank 1 October 1978
6-3 thru 6-13 1 October 1978
6-14 Blank 1
October 1978
6-15
thru 6-25 1 October 1978
6-26 Blank 1 October 1978
7-1 thru 7-40 1 October 1978
8-1 1 October 1978
8-2 Blank 1 October 1978
8-3 thru 8-14 1 October 1978
9-1 thru9-3 1 October 1978
9-4 Blank 1 October 1978
Page Date
Title 1
October 1978
Assignment Record 1 October 1978
i
thru iv 1 October 1978
1-1 thru 1-8 1 October 1978
2-1 1 October 1978
2-2 Blank 1 October 1978
2-3 thru 2-11 1 October 1978
2-12 Blank 1
October 1978
3-1 thru 3-9 1 October 1978
3-10 Blank 1
October 1978
3-11
thru 3-18 1 October 1978
4-1 thru 4-21 1 October 1978
4-22 Blank 1 October 1978
5-1 1 October 1978
5-2 Blank 1 October 1978
5-3 thru 5-25 1 October 1978
5-26 Blank 1 October 1978
1 October 1978
Page Date
iii

TABLE OF CONTENTS
CESSNA
MODEL 182Q
f .
iv
TABLE OF CONTENTS
SECTION
GENERAL 1
L1MITATIONS 2
EMERGENCY PROCEDURES 3
NORMAL PROCEDURES 4
PERFORMANCE 5
WEIGHT & BALANCE/
EQUIPMENT LIST 6
AIRPLANE &SYSTEMS
DESC
RI PTI ONS 7
AIRPLANE
HANDLING,
SERVICE & MAINTENANCE 8
SU PPLEMENTS
(Optional Systems Description
& Operating Procedures) 9
1 October 1978

CESSNA
MODEL 182Q
SECTION 1
GENERAL
TABLE OF CONTENTS
SECTION 1
GENERAL
Page
Three View
Introduction
Descriptive Data
Engine
Propeller
Fuel ...
Oil
Maximum Certificated Weights
Standard Airplane Weights ..
Cabin And Entry Dimensions .
Baggage Space and Entry Dimensions
Specific Loadings .
Symbols, Abbreviations And Terminology
General Airspeed Terminology And Symbols
Meteorological Terminology .
Engine Power Terminology . . . . . . . .
Airplane Performance And Flight Planning Terminology
Weight And Balance Terminology . . . . . . . . . . .
1
October 1978
1-2
1-3
1-3
1-3
1-3
1-3
1-4
1-4
1-5
1-5
1-5
1-5
1-5
1-5
1-6
1-7
1-7
1-7
1-1

SECTION 1
GENERAL
CESSNA
MODEL 182Q
2a._o"-----------J
1.-------
9'-3" MAX.
PIVOT POINT
Wing span shown with strobe lights
installed.
Maximum height shown with nose
gear depressed, as far as possible
and flashing beacon installed.
1. Oi mensions shown are based on
standard empty weight and proper
nose gear and tire inflation.
NOTES:
4. Wheel base length is 66 1/2".
5. Propeller ground clearance is 10 718".
6. Wing area is 174 square feet.
7. Minimum turning radius (*pivot
point to outboard wing tip) is 27'-0".
@
* *
PIVOT POINT
l--
36'-0"
'I
~~
----
1------9'-0"--_
J
Figure 1-1. Three View
1-2 1 October 1978

CESSNA
MODEL 182Q
INTRODUCTION
SECTION 1
GENERAL
This handbook contains 9 sections, and includes the material required
to be furnished to the pilot by CAR Part 3. It also contains supplemental
data supplied by Cessna Aircraft Company.
Section 1 provides basic data and information of general interest. It
also contains definitions or explanations of symbols, abbreviations, and
terminology commonly used.
DESCRIPTIVE DATA
ENGINE
Number of Engines: 1.
Engine Manufacturer: Teledyne Continental.
Engine Model Number: 0-470-U.
Engine Type: Normally-aspirated, direct-drive, air-cooled, horizontally-
opposed, carburetor-equipped, six-cylinder engine with 470 cu. in.
displacement.
Horsepower Rating and Engine Speed: 230 rated BHP at 2400 RPM.
PROPELLER
Propeller Manufacturer: McCauley Accessory Division.
Propeller Model Number: C2A34C204/90DCB-8.
Number of Blades: 2.
Propeller Diameter, Maximum: 82 inches.
Minimum: 80.5 inches.
Propeller Type: Constant speed and hydraulically actuated, with a low
pitch setting of 15.00 and a high pitch setting of 29.40(30 inch station).
FUEL
Approved Fuel Grades (and Colors):
100LL Grade Aviation Fuel (Blue).
100 (Formerly 100/130) Grade Aviation Fuel (Green).
Total Capacity: 92 gallons.
Total Capacity~a.c.l} .. Tank: 46 gallons.
Total Usable: ;138 gallons,-,
.......... -. __ ._ ....._ ... _~-
1 October 1978 1-3

SECTION 1
GENERAL
NOTE
CESSNA
MODEL 182Q
To ensure maximum fuel capacity when refueling and
minimize cross-feeding when parked on a sloping surface,
place the fuel selector valve in either LEFT or RIGHT
position.
OIL
Oil Grade (Specification):
MIL-L-6082 Aviation Grade Straight Mineral Oil: Use to replenish
supply during first 25 hours and at the first 25-hour oil change.
Continue to use until a total of 50 hours has accumulated or oil
consumption has stabilized.
NOTE
The airplane was delivered from the factory with a corro-
sion preventive aircraft engine oil. This oil should be
drained after the first 25 hours of operation.
Continental Motors Specification MHS-24 (and all revisions thereto),
Ashless Dispersant Oil: This oil must be used after first 50 hours
or oil consumption has stabilized.
Recommended Viscosity for Temperature Range:
SAE 50 above 4°C (40°F).
SAE 10W30 or SAE 30 below 4°C (40°F).
NOTE
Multi-viscosity oil with a range of SAE 10W30 is recom-
mended for improved starting in cold weather.
Oil Capacity:
Sump: 12 Quarts.
Total: 13 Quarts (if oil filter installed).
MAXIMUM CERTIFICATED WEIGHTS
Ramp: 2960 lbs.
Takeoff: 2950 lbs.
Landing: 2950 lbs.
I
1-4 1
October 1978

CESSNA
MODEL 182Q
SECTION 1
GENERAL
Weight in Baggage Compartment:
Baggage Area "A" (or passenger on child's seat) - Station 82 to 108: 120
lbs. See note below.
Baggage Area "B" and Hatshelf-Station 108 to 136: 80 lbs. See note
below.
NOTE
The maximum combined weight capacity for baggage
areas A and B, including the hatshelf, is 200 lbs. The
maximum hatshelf load is 25 lbs.
STANDARD AIRPLANE WEIGHTS
Standard Empty Weight, Skylane: 1700 lbs.
Skylane II: 17541bs.
Maximum Useful Load, Skylane: 12601bs.
Sky lane II: 1206 lbs.
CABIN AND ENTRY DIMENSIONS
Detailed dimensions of the cabin interior and entry door openings are
illustrated in Section 6.
BAGGAGE SPACE AND ENTRY DIMENSIONS
Dimensions of the baggage area and baggage door opening are
illustrated in detail in Section 6.
SPECIFIC LOADINGS
Wing Loading: 16.9 lbs./ sq. ft.
Power Loading: 12.8 lbs./ hp.
SYMBOLS, ABBREVIATIONS AND
TERMINOLOGY
GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS
KCAS Knots Calibrated Airspeed is indicated airspeed corrected
for position and instrument error and expressed in knots.
Knots calibrated airspeed is equal to KT AS in standard
atmosphere at sea level.
KIAS Knots Indicated Airspeed is the speed shown on the
airspeed indicator and expressed in knots.
1 October 1978 1-5

SECTION 1
GENERAL
KTAS
V
NE
,&1,.
,SO,-
'V
CESSNA
MODEL 182Q
Knots True Airspeed is the airspeed expressed in knots
relative to undisturbed air which is KCAS corrected for
altitude and temperature.
Manuevering Speed is the maximum speed at which you
may use abrupt control travel.
Maximum Flap Extended Speed is the highest speed
permissible with wing flaps in a prescribed extended
position.
Maximum Structural Cruising Speed is the speed that
should not be exceeded except in smooth air, then only with
caution.
Never Exceed Speed is the speed limit that may not be
exceeded at any time.
Stalling Speed or the minimum steady flight speed at
which the airplane is controllable.
Stalling Speed or the minimum steady flight speed at
which the airplane is controllable in the landing configu-
ration at the most forward center of gravity.
Best Angle-of-Climb Speed is the speed which results in
the greatest gain of altitude in a given horizontal distance.
Best Rate-of-Climb Speed is the speed which results in the
greatest gain in altitude in a given time.
METEOROLOGICAL TERMINOLOGY
OAT
Standard
Tempera-
ture
Pressure
Altitude
1-6
Outside Air Temperature is the free air static temperature.
It is expressed in either degrees Celsius or degrees Fah-
renheit.
Standard Temperature is 15°C at sea level pressure alti-
tude and decreases by 2°C for each 1000 feet of altitude.
Pressure Altitude is the altitude read from an altimeter
when the altimeter's barometric scale has been set to 29.92
inches of mercury (1013 mb).
1 October 1978

CESSNA
MODEL 182Q
ENGINE POWER TERMINOLOGY
SECTION 1
GENERAL
BHP
RPM
Brake Horsepower is the power developed by the engine.
Revolutions Per Minute is engine speed.
MP
Manifold Pressure is a pressure measured in the engine's
induction system and is expressed in inches of mercury
(Hg).
AIRPLANE PERFORMANCE AND FLIGHT PLANNING
TERMINOLOGY
Demon-
strated
Crosswind
Velocity
Usable Fuel
Unusable
Fuel
GPH
NMPG
g
Demonstrated Crosswind Velocity is the velocity of the
crosswind component for which adequate control of the
airplane during takeoff and landing was actually demon-
strated during certification tests. The value shown is not
considered to be limiting.
Usable Fuel is the fuel available for flight planning.
Unusable Fuel is the quantity of fuel that can not be safely
used in flight.
Gallons Per Hour is the amount of fuel (in gallons)
consumed per hour.
Nautical Miles Per Gallon is the distance (in nautical
miles) which can be expected per gallon of fuel consumed
at a specific engine power setting and/ or flight configura-
tion.
g is acceleration due to gravity.
WEIGHT AND BALANCE TERMINOLOGY
Reference
Datum
Station
Arm
Moment
1 October 1978
Reference Datum is an imaginary vertical plane from
which all horizontal distances are measured for balance
purposes.
Station is a location along the airplane fuselage given in
terms of the distance from the reference datum.
Arm isthe horizontal distance from the reference datum to
the center of gravity (C.G.) of an item.
Moment is the product of the weight of an item multiplied
1-7

SECTION 1
GENERAL
Center of
Gravity
(C.G.)
C.G.
Arm
C.G.
Limits
Standard
Empty
Weight
CESSNA
MODEL 182Q
by its arm. (Moment divided by the constant 1000 is used in
this handbook to simplify balance calculations by reduc-
ing the number of digits.)
Center of Gravity is the point at which an airplane, or
equipment, would balance if suspended. Its distance from
the reference datum is found by dividing the total moment
by the total weight of the airplane.
Center of Gravity Arm is the arm obtained by adding the
airplane's individual moments and dividing the sum by
the total weight.
Center of Gravity Limits are the extreme center of gravity
locations within which the airplane must be operated at a
given weight.
Standard Empty Weight is the weight of a standard air-
plane, including unusable fuel, full operating fluids and
full engine oil.
Basic Empty Basic Empty Weight is the standard empty weight plus the
Weight weight of optional equipment.
Useful
Load
Maximum
Ramp
Weight
Maximum
Takeoff
Weight
Maximum
Landing
Weight
Tare
1-8
Useful Load is the difference between ramp weight and the
basic empty weight.
Maximum Ramp Weight is the maximum weight approved
for ground maneuver. (It includes the weight of start, taxi
and runup fuel.)
Maximum Takeoff Weight is the maximum weight ap-
proved for the start of the takeoff run.
Maximum Landing Weight is the maximum weight ap-
proved for the landing touchdown.
Tare is the weight of chocks, blocks, stands, etc. used when
weighing an airplane. and is included in the scale read-
ings. Tare is deducted from the scale reading to obtain the
actual (net) airplane weight.
1 October 1978

CESSNA
MODEL 182Q
SECTION 2
LIMITATIONS
TABLE OF CONTENTS
Introduction . . . . . . . .
Airspeed Limitations
Airspeed Indicator Markings
Power Plant Limitations
Power Plant Instrument Markings
Weight Limits . . . . . .
Center Of Gravity Limits . ','
Maneuver Limits ....
Flight Load Factor Limits
Kinds Of Operation Limits
Fuel Limitations . - .
Other Limitations
Flap Limitations
Placards .....
1 October 1978
SECTION 2
LIMIT ATIONS
Page
2-3
2-4
2-4
2-5
2-6
2-6
2-7
2-7
2-7
2-7
2-8
2-8
2-8
2-9
2-1/ (2-2 blank)

CESSNA
MODEL 182Q
INTRODUCTION
SECTION 2
LIMITATIONS
Section 2 includes operating limitations, instrument markings, and
basic placards necessary for the safe operation of the airplane, its engine,
standard systems and standard equipment. The limitations included in
this section and in Section 9 have been approved by the Federal Aviation
Administration. Observance of these operating limitations is required by
Federal Aviation Regulations.
NOTE
Refer to Section 9 of this Pilot's Operating Handbook for
amended operating limitations, operating procedures,
performance data and other necessary information for
airplanes equipped with specific options.
NOTE
The airspeeds listed in the Airspeed Limitations chart
(figure 2-1) and the Airspeed Indicator Markings chart
(figure 2-2) are based on Airspeed Calibration data shown
in Section 5 with the normal static source. If the alternate
static source is being used, ample margins should be
observed to allow for the airspeed calibration variations
between the normal and alternate static sources as shown
in Section 5.
Your Cessna is certificated under FAA Type Certificate No. 3A13 as
Cessna Model No. 182Q.
1
October 1978 2-3

SECTION 2
LIMITATIONS
AIRSPEED LIMITATIONS
CESSNA
MODEL 182Q
Airspeed limitations and their operational significance are shown in
figure 2-1.
SPEED
KCAS
KIAS REMARKS
VNE Never Exceed Speed 172
179
Do not exceed th is speed in
any
operation.
V
NO
Maximum Structural
139 143
Do not exceed this speed
Cruising Speed
except in smooth air, and
then
only with caution.
VA
Maneuvering Speed:
2950 Pounds 109 111 Do not make full or abrupt
2450 Pounds
99
100
control movements above
1950 Pounds
89
89
this speed.
VFE
Maximum Flap Extended
Speed:
To 10
0Flaps 137
140
Do not exceed these speeds
100-
40
0Flaps
95
95
with the given flap settings.
Maximum Window Open 172
179
Do not exceed this speed with
Speed
windows open.
Figure 2-1. Airspeed Limitations
AIRSPEED INDICATOR MARKINGS
Airspeed indicator markings and their color code significance are
shown in figure 2-2.
2-4 1 October 1978

CESSNA
MODEL 182Q
SECTION 2
LIMIT ATIONS
MARKING
KIAS VALUE
SIGNIFICANCE
OR RANGE
White Arc
45 - 95
Full Flap Operating Range.
Lower
limit is maximum weight VSoin
landing
configuration. U~r limit
is maximum speed permissible with
flaps extended.
Green
Arc 48 -143 Normal Operating Range.
Lower limit
~.
is maximum weight Vs at most forward
C.G. with flaps retracted.
Upper limit
is maximum structural cruising speed.
Yellow Arc 143 -179 Operations
must be conducted with
caution and only in smooth air..
Red Line 179
Maximum speed for all operations.
Figure 2-2. Airspeed Indicator Markings
POWER PLANT LIMITATIONS
Engine Manufacturer: Teledyne Continental.
Engine Model Number: 0-470-U.
Engine Operating Limits for Takeoff and Continuous Operations:
Maximum Power: 230 BHP.
Maximum Engine Speed: 2400 RPM.
Maximum Cylinder Head Temperature: 460°F (238°C).
Maximum Oil Temperature: 240°F (116°C).
Oil Pressure, Minimum: 10 psi.
Maximum: 100 psi.
Propeller Manufacturer: McCauley Accessory Division.
Propeller Model Number: C2A34C204/90DCB-8
Propeller Diameter, Maximum: 82 inches.
Minimum: 80.5 inches.
Propeller Blade Angle at 30 Inch Station, Low: 15.0°.
High: 29.4°.
1
October 1978 2-5

SECTION 2
LIMITATIONS
CESSNA
MODEL 182Q
POWER PLANT INSTRUMENT MARKINGS
Power plant instrument markings and their color code significance
are shown in figure 2-3.
RED LINE
GREEN ARC
YELLOW ARC
RED LINE
INSTRUMENT
MINIMUM
NORMAL CAUTION
MAXIMUM
LIMIT
OPERATING
RANGE
LIMIT
Tachometer - - - 2100 ----2400
RPM
2400 RPM
Manifold Pressure - - - 15-23 - - - ---
in. Hg
Oil Temperature - - -
100° - 240°F
-- -
240°F
Cylinder Head - - -
200° - 460°F
-- -
460°F
Temperature
Oil
Pressure
10 psi 30-60 psi -- - 100 psi
Carburetor
Air
--- - - -
-15° to 5°C
- - -
Temperature
Suction - - -
4.5-5.4 - - -- - -
in. Hg
Fuel
Quantity
E---- - - ---
(2.0 Gal. Unusable
Each Tank)
Figure 2-3. Power Plant Instrument Markings
WEIGHT LIMITS
Maximum Ramp Weight: 2960lbs.
Maximum Takeoff Weight: 2950lbs.
Maximum Landing Weight: 2950lbs.
Maximum Weight in Baggage Compartment:
Baggage Area" A" (or passenger on child's seat) - Station 82 to 108: 120
lbs. See note below.
Baggage Area "B" and Hatshelf- Station 108 to 136: 80lbs. See note
below.
2-6 1
October 1978