1998 Cessna 208, C208 Pilots Operating Handbook (POH)
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TEMPORARYRE'VISION
208PHTR03
3 FEBRUARY 2004
for
, CESSNA MODEL 208 SERIES
PILOT'S OPERATING HANDBOOKS
" and
FAA ,APPROVED AIRPLANE
FLIGHT MANUALS
THIS TEMPORARY REVISION REVISES FUEL QUANTITY VERSUS
DEPTH INFORMATION WHEN USING THE DIPSTICK REQUIRED
BY CAB04-1 ON BOTH LEFT AND RIGHT WING L.EADING EDGE
IN THE PILOT'S OPERATING HANDBOOK.
(
INSERT THE , PROVIDED LIST OF TEMPORARY REVISIONS, AND
( ,r-" THE TEMPORARY REVISION INTO THE PILOT'S OPERATING
( HANDBOOK ' IN ACCORDANCE WITH ' THE FILING
,INSTRUCTIONS IN EACH REVISION.
For Training Purposes Only
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For Training Purposes Only
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LIST OF TEMPORARY REVISIONS
for ..
CESSNA MODEL 208 SERIES
PILOT'S OPERATING HANDBOOKS
and
FAA APPROVED AIRPLANE
FLIGHT MANUALS
3 February 2004
208PHTR .
208PHTR03
For Only
LIST OF
TEMPORARY REVISIONS
MODEL (
(
Pilot's Operating Handbook
All Cessna Model208,Series
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Following is the List of Temporary Revisions that may be inserted into this " (
Pilot's Operating Handbook. . i (
Insert this page opposite the first page of the Log of Effective Pages in the
front of the Pilot's Operating Handbook.
TEMPORARY MANUAL
ISSUE
REVISION SECTION/
DATE
NUMBER TOPIC
20BPHTROl
CANCELLED CANCELLED
REPLACED BY REPLACED BY
208PHTR02 208PHTR02
208PHTR02 2ILlMITATIONS
23 September
2003
208PHTR02 3/EMERGENCY
23 September
PROCEDURES
2003
208PHTR02 4/NORMAL
23 September
PROCEDURES
2003
208PHTR02 51
23 September
PERFORMANCE
2003
208PHTR03 4/NORMAL
3 February
PROCEDURES
2004
TEMPORARY REVISION 208PHTR03
APPROVED BY
'AA APPROVED UNDER FAR 21SUBPART J
rl\lj Ceqn. Aircraft Co
0010g81100 Option' Authonzalion 00A·230428-Ce
SERVICE
BULLETIN
REFERENCE
NO
REFERENCE
CAB03-11Rl
CAB03-11Rl
CAB03-11Rl
CAB03-11Rl
CAB04-1
DATE'OFAPPROVAL.3 E=eeRUAAY
For Train!og Purposes Only
3 February 2004
208PHTR
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Cessna 208
MODEL SERIES .
Description of Change:
Filing Instructions:
PILOT'S OPERATING HANDBOOK
TEMPORARY REVISION
Section 4, NORMAL PROCEDURES
Insert this temporary revision into the Pilot's
Operating Handbook.
( In Section 4, NORMAL PROCEDURES, insert the temporary revIsion
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pages adjacent to . the ·current Pilot's Operating Handbook Section 4 pages
. containing' the information that is shown in this temporary revision.
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For Training Purposes Only
3 February 2004
208PHTR03
I This Page Intentiona.lly Left Blank I
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For Training Purposes Only
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I This Page Intentionally Left Blank I
For Training Purposes Only
PILOT'SOPERATING HANDBOOK
TEMPORARY REVISION
Cessna 208
MODEL SERIES
SECTION 4 - NORMAL PROCEDURES
CHECKLIST PROCEDURES
PREFLIGHT INSPECTION
0LEFT WING Leading Edge
A WARNING
It is essential in cold weather to remove even small
accumulations of frost, ice, or snow from the wing and
control surfaces. Also, make sure the control surfaces
contain no internal accumulations of ice or debris.
Prior to any flight in icing ' conditions, check that
pitot/static source and stall warning heaters are warm
to touch after turning pitot/static and stall heat switches
on for 30 seconds, then off. Make sure the pitot covers
are removed.
1. Wing Strut Deice Boots -- CHECK for tears, abrasion and cleanliness.
2. Wing Tie-Down -- DISCONNECT.
3. Wing Deice Boots -- CHECK for tears, abrasions and cleanliness.
4. Stall Warning Vane -- CHECK freedom of movement, audible warning
and warmth. (For aircraft equipped with a stall warning ground
disconnect switch, check audible warning with elevator off forward
stop).
5. PitoVStatic Tube -- CHECK security, openings for stoppage and
warmth. ,
6. Landing and Taxi Lights CHECK condition and cleanliness.
7. Fuel Quantity -- USE DIPSTICK required by CAB04-1 to check fuel
level. See Figure TC-l for fuel quantity versus depth.
A CAUTION
Fuel gages may indicate incorrect fuel quantity.
8. Fuel Filler Cap -- SECURE.
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9. Outboard Fuel Tank Sump Quick-Drain Valve (if installed and airplane
parked with one wing low on a sloping ramp) -- DRAIN (using fuel
sampler) to check for water, sediment, and proper fuel before each
flight and after each refueling. If water is observed, take further (
samples until clear. Take repeated samples from all fuel drain points ( . (,
until all contamination has been removed. \.
10; NaVigation and Strobe Lights -- CHECK for condition and cleanliness.
3 February 2004
208PHTR03
For Training Purposes Only
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"' --
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Cessna 208
MODEL SERIES · .
Universal XL
Fuel Gage Fuel Quantity
Gage Scale
Gal lbs
0.50 87.4 585
0.75 91 .1 610
1.00 94.7 634
1.25 98.2 658
1.50 101.8 682
1.75 105.2 705
2.00 108.6 727
2.25 111.9 750
2.50 115.1 771
2.75 118.3 793
3.00 121.5 814
3.25 124.5 834
3.50 127.5 855
3. 75 130.5 874
4.00 133.4 894
4.25 136.2 912
4.50 138.9 931
4.75 141.6 949
5.00 144.3 966
5.25 146.8 984
5.50 149.3 1000
5. 75 151 .8 1017
6.00 154.1 1Q33
6.25 156.5 1048
6.50 158.7 1053
160.9 1078
7.00 163.0 1092
7.25 165.0 1106
Figure TC-1. Measure
PILOT'S OPERATING HANDBOOK
TEMPORARY REVISION
Generic Fuel
Gage - Inches Fuel Quantity
ncnes
Gal . Lbs
0. 50 88.4 592
0.75 92.6 . 621
1.00 96.7 648
1.25 100.8 675
1.50 104.7 702
1.75 108.6 727
2.00 112.4 753
2.25 116.1 7 78
2.50 119.7 802
2.75 123.2 826
3.00 126.7 849
3. 25 130.1 871
3.50 133.4 894
3.75 136.G 915
4.00 139.7 936
4.25 142.8 956
4.50 145.7 976
4.75 148.6 996
5.00 151.4 1015
5.25
154.1 .
1033
5.50 156 .. 8 1050
5.75 159.3 1068
6.00 161.8 1084
6.33 · 165.0 1105
d Fuel Depth vs Fuel Quantity
For Training P\Jrposes On'y
3 February 2004
208PHTR03
PILOT'S OPERATING HANDBOOK
TEMPORARY REVISION
MODEL 208 '
(
VRIGHT WING Leading Edge
A WARNING
It is essential in cold weather , to remove even small
accumulations of frost, ice, or snow from the wing and
control surfaces. Also, make sure the control surfaces
contain no internal accumulations of ice or debris.
1. Navigation and Strobe Lights -- CHECK condition and cleanliness.
2. Fuel Quantity -- USE DIPSTICK required by QAB04-1 to check fuel
level. See Figure TC-1 for fuel quantity verSus depth.
A CAUT10N
Fuel gages may indicate incorrect fuel quantity.
3. F'uel Filler Cap-- SECURE.
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4. Outboard Fuel Tank Sump Quick-Drain Valve (if installed and airplane
parked with , one wing low on a sloping ramp) -- DRAIN (using fuel
sampler) to check for water, sediment, and proper fuel before each
flight and after each refueling. If water is ' observed, take further
samples until clear. Take repeated samples from all fuel drain points
until all contamination has been removed. (
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5. PitoVStatic Tube -- CHECK security, . openings 'for stoppage , and
warmth.
6. Landing and Taxi Lights CHECK conditibn cleanliness.
7. Wing Deice Boots-- CHECK for tears, and cleanliness.
8. Radome -- CHECK condition and security. :' \ .
9. Wing Tie-Down -- DISCONNECT. '
10 .. Wing Strut Deice Boots -- CHECK for tears, abrasion,and cleanliness.
11 . Inboard Fuel Tank Sump and External Sump Quick-Drain Valves --
DRAIN (using fuel sampler) to check for water, sediment, arid proper
fuel before each flight and after each refueling. If water is observed.
take further samples until clear. Take repeated samples from aliluel
drain pOints until all contamination has been removed.
12. Main Landing Gear -- CHECK proper tire inflation and gear condition.
3 February 2004
208PHTR03
For Training Purposes Only
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Full Search Facility
Print one or all pages of your manual
$30.99
$40.99
The Cessna 208 C208 675HP 1998 POH Cessna Caravan manual, updated to 2004, is available in PDF format. It is compatible with all versions of Windows, Mac, and Linux. This manual is printable and provides instant high-speed access. Adobe is required to view the manual.
