Cessna Model 208 Series Pilot's Operating Handbook
CESSNA CARAVAN 208 · Pilot's Operating Handbook
Overview
This document is a temporary revision for the Cessna Model 208 Series Pilot's Operating Handbook, specifically addressing updates to fuel quantity versus depth information. It includes instructions for inserting the revision into the handbook and highlights important safety procedures.
- This is a temporary revision dated 3 February 2004.
- It revises fuel quantity versus depth information.
- The revision must be inserted into the Pilot's Operating Handbook.
- It includes a checklist for preflight inspection.
- Warnings are provided for cold weather operations.
- Fuel gauges may indicate incorrect fuel quantity.
- The document is FAA approved under FAR 21 Subpart J.
- It includes a list of previous temporary revisions.
Document
Source
Originally published by aeroelectric.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Pilot's Operating Handbook
- Year ·
- 2004
- File size ·
- 61 MB
- Publisher ·
- aeroelectric.com
- Language ·
- en
What is the Cessna Model 208 Series Pilot's Operating Handbook?
The Cessna Model 208 Series Pilot's Operating Handbook is a pilot's operating handbook for the CESSNA CARAVAN 208, dated 2004.
Where does the Cessna Model 208 Series Pilot's Operating Handbook come from?
This copy of the Cessna Model 208 Series Pilot's Operating Handbook was originally published by aeroelectric.com and is hosted on Sprinkle as a free, searchable reference copy.
What year was the Cessna Model 208 Series Pilot's Operating Handbook published?
The Cessna Model 208 Series Pilot's Operating Handbook — the CESSNA CARAVAN 208 pilot's operating handbook on file — is dated 2004.
Most owners only have the POH. Here's the essential set for the CESSNA CARAVAN 208.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
In this document
Temporary Revision Overview
This section outlines the purpose of the temporary revision and the specific changes made to the Pilot's Operating Handbook.
Normal Procedures
This section includes a checklist for preflight inspection, emphasizing the importance of checking for frost, ice, and snow on wings and control surfaces.
Warnings and Cautions
Warnings regarding cold weather operations and cautions about fuel gauge accuracy are highlighted.
Fuel Quantity Measurement
Instructions for using a dipstick to check fuel levels and a reference for fuel quantity versus depth are provided.
List of Temporary Revisions
This section lists previous temporary revisions and their topics, indicating which revisions have been replaced.
Filing Instructions
Instructions for inserting the temporary revision into the Pilot's Operating Handbook are detailed.
Safety notes
- It is essential to remove frost, ice, or snow from wings and control surfaces in cold weather.
- Ensure control surfaces are free of internal ice or debris.
- Check that pitot/static source and stall warning heaters are warm before flight in icing conditions.
- Fuel gauges may indicate incorrect fuel quantity.
- Drain fuel sumps to check for water and sediment before each flight.
Full document text
( ( ( ( ( ( ' \ ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( 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 ( \0~')' HANDBOOK 'IN ACCORDANCE WITH ' THE FILING ,INSTRUCTIONS IN EACH REVISION. For Training Purposes Only ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( { ( ( "~ ( ( ,( For Training Purposes Only ( ( ( ( ( \ ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( 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 Traini"g' Purpos~s Only LIST OF TEMPORARY REVISIONS MODEL ~eERIES208 (( Pilot's Operating Handbook All Cessna Model208 ,Series ( ( 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 *~_E_ DATE'OFAPPROVAL.3 E=eeRUAAY ~ For Train!og Purposes Only 3 February 2004 208PHTR ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( \..~: . ~ .( ( ( ( ( ( ( ( Cessna 208MODEL 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 ( pages adjacent to .the ·current Pilot's Operating Handbook Section 4 pages . containing' the information that is shown in this temporary revision. ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( For Training Purposes Only 3 February 2004 208PHTR03 IThis Page Intentiona.lly Left Blank I { \\ For Training Purposes Only ( ( ( ( ( ( ( ( ( ( ( \ ( ( ( ( ( ( ( ( ( ( ( . ( ( ( ( ( ( ( (-- " \. ( ( ( ( ( ( o IThis Page Intentionally Left Blank I For Training Purposes Only PILOT'SOPERATING HANDBOOK TEMPORARY REVISION Cessna 208MODEL 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. ( ( ( ( ( ( ( ( 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 ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( "'-- ( ( ( ( ( ( ( ( ( ( ( Cessna 208MODEL 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 6 ~ 75 160.9 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 2.25 116.1 778 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
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3 February 2004 208PHTR03 PILOT'S OPERATING HANDBOOK TEMPORARY REVISION MODEL s~e~~~~ 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. ( ( ( ( ( ( 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. ( ( ( ( ( 5. PitoVStatic Tube -- CHECK security, . openings 'for stoppage , and warmth. 6. Landing and Taxi Lights -~ CHECK conditibn . ~nd cleanliness. 7. Wing Deice Boots-- CHECK for tears, abrasl9~ 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 ( ( ( ( ( i ( \".. { ( ( ( ( TEMPORARY REVISION( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( , i ( ( ( ( ( ( ( ( 208PHTR02 23 SEPTEMBER 2003 for CESSNA MODEL 208 SERIES PILOT1SOPERATINGHANDBOOKS and FAA APPROVED AIRPLANE FLIGHT MANUALS THIS TEMPORARY REVISION REPLACES TEMPORARY . REVISION 208PHTR01 DATED 8 SEPTEMBER 2003 AND REVISES FLAP USAGE INFORMATION IN ·SECTIONS 2, 3, 4 AND 5 OF THE PILOT'S OPERATING HANDBOOK. INSERT THE PROVIDED LIST OF TEMPORARY REVISIONS, AND THE TEMPORARY REVISION INTO THE PILOT'S OPERATING HANDBOOK· IN ACCORDANCE WITH THE FILING INSTRUCTIONS IN EACH REVISION. For Training Purposes Only For Training Purposes Only ( ( ( ( ( ( ( ( ( ( ( ( ( . ( ( ( ( ( ( ( ( ( ,,~ . -.,: ( ( ( ( ( ( ( LIST OF TErv1PORARY REVISIONS ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( for CESSNA MODEL 208 SERIES PILOT'S OPERATING HANDBOOKS and FAA APPROVED AIRPLANE FLIGHT MANUALS 23 September 2003 208PHTR 208PHTR02 For Training Purposes Only LIST. OF TEMPORARY REVISIONS Cessna 208MODEL SERIES . Pilot's Operating Handbook All Cessna Model 208 Series The following List of .Temporary Revisions must be inserted into this Pilot's Operating Handbook. ( Insert this page opposite the first page of the Log of Effective Pages in the frontof the Pilot's Operating Handbook. TEMPORARY MANUAL ISSUE REVISION . . SECTIONI DATE NUMBER TOPIC 208PHTR01 CANCELLED · CANCELLED REPLACED BY REPLACED BY 208PHTR02 .. 208PHTR02 20BPHTR02 2IUMITATIONS 23 September 2003 20BPHTR02 3/EMERGENCY 23 September PROCEDURES 2003 20BPHTR02 4/NORMAL 23 September PROCEDURES 2003 20BPHTR02 51 23 September PERFORMANCE 2003 -. TEMPORARY REVISION 208PHTR02 APPROVED BY FAA APPROVED UNDER FAR 21 SUBPART J The C_ 1.ircr8ft co . Del"llation Option Authoriulion DOA-23042B-CE . ~f-.w; rJ .t;:-J ExIlQlliye Engineer . ~ . ~3 SE..PTEM&R. :l003 For Training Purposes Only 23 September 2003 208PHTR ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ~~ . . '" "-> ( . ( ( ( ( ( ( ( ( ( ( \ ( ( / ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( / Cessna 208MODEL SERIES . Description of Change: Filing Instructions: PILOT'S OPERATING HANDBOOK TEMPORARY REVISION Section 2, LIMITATIONS, . EMERGENCY PROCEDURES, NORMAL PROCEDURES, and PERFORMANCE. Section Section Section 3, 4, 5, Insert this temporary revision into the Pilot's Operating Handbook. In Section 2, LIMITATIONS, insert the temporary revision pages ad ja cent to the current Pilot's Operating Handbook Section 2 pages containing the information that is shown in this -temporary revision. . _In Section 3, EMERGENCY PROCEDURES; insert the temporary revision pages adjacent to the current Pilot's Operating Handbook Section 3 pages containing the information that is shown in this temporary rev i sion. In Section 4, NORMAL PROCEDURES, insert the temporary revision pages adjacent to the current Pilot's Operating Handbook Section 4 pages containing the information that is shown in this temporary revision. In Section 5, PERFORMANCE, insert th e. temporary revision pages adjacent to the current Pilot's Operating Handbook Section 5 pages containing the information that is shown in this temporary revision. Discard any pages of this temporary revision that are not applicable to your model/serial airplane. For Training Purposes Only 23 September 2003 20BPHTR02 IThis Page Intentionally Left Blank I For Training Purposes Only ( ( ( ( ( ( ( ( ( ( { ( \ ( ( ( '( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( (' (' ( /" ~<. '. ~ '"-<.,..~~ Cessna 208MODEL SERIES SECTION 2 • LIMITATIONS OTHER LIMITATIONS FLAP LIMITATIONS U~E OF FLAPS IS PROHIBITED PILOT'S OPERATING HANDBOOK TEMPORARY REVISION The flap motor and STBY flap motor circuit breakers must be pulled and collared. (place a tie wrap or equivalent around the pulled circuil breaker.) • The following placard must be displayed in the cockpit, in clear view 01 the pilot, on the lower right hand portion of the center instrument panel: I· USE OF FLAPS IS PROHIBITED NOTE Use 0° Flap Takeoff and . Landing performance and procedures from Section 5. 23 September 2003 For Training Purposes Only 208PHTRm IThis Page Intentionally Left Blank I For Training Purposes Only ( ( ( . ( ( ( ( ( ( ( ( ( ( ( ( ( " ( ( ( ( ( ( / ( ( ( ( ( ( ( (' \" ( ( ( ( ( ( , (, -- Cessna 208MODEL SERIES SECTION 2 - LIMITATIONS PILOT'S OPERATING HANDBOOK TEMPORARY REVISION 'KINDS OF OPERATION LIMITS This airplane is equipped for day VFR, and may be equipped for night VFR and/or IFR operations and for f1ight-into-known icing conditions. The operating limitations placard reflects the limits applicable at the time of Airworthiness Certificate issuance. The following equipment list identifies the systems and equipment upon which type certification for each kind of operation was ' predicated, These systems and equipment items must be installed and operable for the particular kind of operation indicated. Reference should also be made to the Equipment List furnished with the airplane for additional equipment information. The pilot is responsible for determining the airworthiness of his airplane for each flight and for assuring compliance with curr~nt operating FAR's. REQUIRED EQUIPMENT DAVVFR: Airspeed Indicator (1) Altimeter (1)* Auxiliary Boost Pump System BATIERY HOT And SATIERY OVERHEAT ·Annunciators (NiCad Batteries Only) Elevator Trim System (Manual) Engine Ignition System (Flap Motor Disabled) Flap Position Indicator FUEL PRESS LOW Annunciator Fuel Quantity Indicators (2) Fuel Selectors Off Warning System Generator Inertial Separator System In Indicator Magnetic Compass Ng% RPM Indicator . OIL PRESS LOW Annunciator Oil Pressure Gage Oil Temperature Gage Outside Air Temperature Gage Overspeed (Airspeed) Warning System Overspeed Governor Pilots Operating HandbookiAFM Pitot-Static System (1) . Propeller APM Indicator * NOTE Seat Belts (Each Occupant) Shoulder Harnesses (Front Seats) Slip-Skid Indicator (1) Stall Warning System Torque Indicator ' Trim Position Indicators (3) VolVAmmeter . When a servoed altimeter is installed, a functioning pneumatic altimeter is also required . 23 September 2003 For Training Purposes Only 208PHTA02 IThis Page Intentionally Left Blank I For Training Purposes Only ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( \ ( Cessna 208MODEL SERIES SECTION 3 - EMERGENCY PROCEDURES ENGINE FAILURES PILOT'S OPERATING HANDBOOK TEMPORARY REVISION ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF 1. Airspeed •• 95 KIAS with 0° flaps. 2. Propeller-- FEATHER. 3. Fuel Condition Lever -- CUTOFF. 4. Fuel Shutoff -- OFF (pull out). 5. Fuel Tank Selectors -- OFF (warning horn will sound), 6. Battery -" OFF. 23 September 2003 for Tr~ining Pqrposes Only 208PHTR02 IThis Page Intentionally LeftBlank I For Training Purposes Only ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( (\ ( ( ( ( ( ( ( ( \ ( ( ( ( . "- ( ( ( ( ( ( / Cessna 208MODELSERIES . ' PILOT'S OPERATING HANDBOOK TEMPORARY REVISION SECTION 3 - EMERGENCY PROCEDURES FORCED LANDINGS EMERGENCY LANDING WITHOUT .ENGINE POWER 1, Seats, Seat Belts, Shoulder Harnesses -- SECURE, 2. Airspeed -- 100 KIAS (flaps UP) 3. Power Lever --IDLE. 4. Propeller Control Lever -- FEATHER. 5. Fuel condition Lever -- CUTOFF. 6. Fuel Boost Switch -- OFF. 7. Ignition Switch -- NORM, 8. Standby Power Switch (if installed) -~ OFF. 9. . Non-essential Equipment (if Installed) -- OFF. 10. Fuel Shutoff -- OFF (pull out). 11. Fuel Tank Selectors -- OFF (warning horn will sound). 12. Crew Doors -- UNLATCH PRIOR TO TOUCHDOWN. 13. Ba~tery Switch -- OFF when landing is assured. 14 . Touchdown -- SLIGHTLY TAIL LOW. 15. Brakes -- APPLY HEAVILY. PRECAUTIONARY LANDING WITH ENGINE POWER 1. Seats, Seat Belts, Shoulder Harnesses -- SECURE. 2 . . Wing Flaps -- 0° . 3. Airspeed -- 95 KIAS . 4. Selected Field -- FLYOVER, noting terrain and obstructions. 5. All Electrical Switches (except Battery and Generator) -- OFF. 6. Crew Doors -- UNLATCH PRIOR TO TOUCHDOWN. 7. Generator Switch (if installed) -- OFF. 8. Battery Switch -- OFF. 9. Touchdown -- SLIGHTLY TAIL LOW. 10 . Fuel Condition Lever -- CUTOFF. 11. Brakes -- APPLYHEAVIL Y. 23 September 2003 For Training Purposes Only 208PHTR02 IThis Page Intentionally Left Blank I For Training Purpos~s Only 1 ( ( ( ( ( ( ( ( ( ( ( . ( ( ( ( ( ( ( ( ( ( {' ( ( ( ( ( ( ( ( ( ( 1-- \ , ( ( ( ( ( ( ( ( ( f i ;' 'tit ~~,.,; .,. ··· ' Cessna 208MODEL SERIES SECTION 3 • EMERGENCY PROCEDURES FORCED LANDINGS DITCHING PILOT'S OPERATING HANDBOOK TEMPORARY 'REVISION 1. Radio·· TRANSMIT MAYDAY on 121.5 MHz,giving location and intentions and SQUAWK 7700 if transponder is installed. 2. Heavy Objects in Cabin •• SECURE if passenger is available to assist. 3. Seats, Seat Belts, Shoulder Harnesses •• SECURE. 4. , Wing Flaps •• 0°. , 5. Power·· ESTABLISH 300 FT/MIN DESCENT AT 100 KIAS. 6. Approach·· High Winds .. INTO THE WIND. light Winds, Heavy Swells •• PARALLEL TO SWELLS. 7. FACE •• CUSHION at touchdown with folded coat or similar object. 8. Touchdown •• NO FLARE, maintain descent attitude. 9. Airplane·· EVACUATE. 10. Life Vests and Raft·· INFLATE when outside cabin. 23 September 2003 ForTraining Purposes Only 208PHTRm ( IThis Page Intentionally Left Blank I For Training Purposes Only ( ( ( ( ( ( { \ ( ( ( ( ( ( ( ( ( ( ( ( ' -- - ( ( ( ( / (- , \0,.-".) Cessna 208MODEL SERIES SECTION 3 - EMERGENCY PROCEDURES SMOKE AND FIRE PILOT'S OPERATING HANDBOOK TEMPORARY REVISION ENGINE FIRE IN FLIGHT (Red ENGINE FIRE Annunciator On Or Off) 1. Power Lever -- IDLE. 2. Propeller Control Lever -- FEATHER. 3. Fuel Condition Lever - CUTOFF. 4. Fuel Shutoff -- OFF . 5. Cabin Heat Firewall Shutoff Coritrol-- PULL OFF. 6. Forward Side Vents -- CLOSE. 7. Overhead Vents -- OPEN . 8. Ventilation Fans (if installed) -- ON . 9. , Wing Flaps -- 0°. 10. Airspeed _. 100 KIAS . 11. Forced Landing -- EXECUTE (as described in Emergency Landing Without Engine Power) 23 September 2003 Fpr Training Purposes O"ly , 20ePHTR02 IThis Page ·lntentionaHy Left Blank I For Training Purposes Only ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( \ Cessna 208MODEL· SERIES SECTION 3 .. EMERGENCY PROCEDURES PILOT'S OPERATING HANDBOOK . TEMPORARY REVISION LANDING GEAR MALFUNCTION PROCEDURES LANDING WITH FLAT MAIN TIRE 1. Airplane -- FLY as desired to lighten fuel load. ~. Fuel Selectors _. POSITION ONE SIDE OFF TO LIGHTEN LOAD ON SIDE OF FLAT TIRE (maximum fuel unbalance of 200 pounds). 3. Approach -- NORMAL W flaps). 4. Touchdown .- INFLATED TIRE FIRST. Hold airplane off flat tire as long as possible with aileron control. 5. Directional Control·· MAINTAIN using brake on wheel with inflated tire as required. 23 Septemb er 2003 For TrlliniJlg Purpo!!es Only 208PHTR02 IThis Page Intentionally Left Blank I For Training Purposes Only ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( \ Cessna 208MODEL SERIES · SECTION 3 - EMERGENCYPROCEDURES PILOT'S OPERATING HANDBOOK TEMPORARY REVISION EMERGENCY DESCENT PROCEDURES SMOOTH AIR 1. Seats, Seat Belts, Shoulder Harnesses -- SECURE. 2. Power Lever -- IDLE. 3. Propeller Control Lever -- MAX (full forward). 4. Wing Flaps -- 0°. 5. Airspeed -- 175 KIAS . 23 September 2003 For Training Purposes Only 208PHTRO~ IThis Page Intentionally Left Blank I For Training Purposes Only ( ( ( ( ( ( ( ( ( ( ( . ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ,". ( ( ( ( ( ( ( ( ( ( (' f ' t/ ~"",< Cessna 208MODEL SERIES SECTION 3 - EMERGENCY PROCEDURES PILOT'S OPERATING HANDBOOK TEMPORARY REVISION INADVERTENT OPENING OF AIRPLANE DOORS IN FLIGHT UPPER HALF OF CARGO DOOR OR UPPER HALF OF PASSENGER AIRSTAIR DOOR OPEN (Red DOOR WARNING Annunciator On) . 1. Airspeed -- MAINTAIN LESS THAN 100 KIAS. 2. If available or practical. have a second crew member go aft to close and latch door. 3. If landing is required with door open: a. Approach and Landing NORMAl. LOWER HALF OF PASSENGER AIRSTAIR DOOR OPEN 1. Airspeed -- MAINTAIN 100 KIAS. 2. Flight Controls -- MANEUVER for return for landing. 3. Wing Flaps -- 0°. 4. Approach -- NORMAL. 5. Landing -- SLIGHTLY TAIL LOW; avoid nose high flare. 23 September 2003 For Training Purposes Only 208PHTR02 IThis Page Intentionally left Blank/ For Training Purposes Only ( ( { ( ( ( ( ( ( ( /' ( I I, ( ( ( ( ( ( ( ( ( ( ( ' ( '\ ( ( ( ( ( ( ( ( \ Cessna 208MODEL SERIES SECTION 3 - EMERGENCY PROCEDURES PILOT'S OPERATING HANDBOOK TEMPORARY REVISION LANDING WITHOUT ELEVATOR CONTROL Using power lever and elevator trim control, trim for approximately 500 fpm descent with 0° flaps at 100 KIAS. Then control the glide angle by adjusting power. If required,make small trim changes to maintain approximately 85KIAS as power is adjusted during the approach. The landing ' flare can be accomplished by a gentle power reduction accompanied by nose up trim.' At forward C.G. loadings, it may be necessary to make a small power increase in the final flare stage to bring the nose up and prevent touchdown 'on the nose first. After touchdown, mov.e the powe r lever to idle: 23 September 2003 For Trai"ingPurp(Jses Oply 208PHTR02 IThis Page Intentionally Left Blank I For Training Purposes Only ; ( ( \., ( '-, .~. -, ( ( '. ( ! ( I ( I ( ( ( ( I ( ( ( ( ( ( ( ( ( ( ( ( , ( I Cessna 208 PILOT'S OPERATING HANDBOOK MODEL SERIES . TEMPORARY REVISION SECTION 3 - EMERGENCY PROCEDURES INADVERTENT OPENING OF AIRPLANE DOORS IN FLIGHT If any of the airplane doors should inadvertently. open in flight, the airplane should be slowed to 100 KIAS tei reduce buffeting of the doors. On the Passenger Version, closing the upper cargo door or upper half of the passenger airstair door can be accomplished after airspeed has been reduced by pulling the door forcefully closed and latching the door. If the door cannot be closed · in flight, a landing should be made as soon as practical in accordance with the checklist procedures. On Cargo ·Versions. an open cargo door cannot be closed in flight since the inside of the upper door has no handle. . If any cargo pod doors inadvertently open in flight. the airplane should be slowed to 100 KIAS or less and landed as soon as practical. During the landing. avoid a nose-high flare to prevent dragging an .open rear cargo pod door on the runway. . 23 Septertlber2003 For Training Purposes Only 208PHTRO~ IThis Page IntentionallyLeft Blank I For Training Purposes Only ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( '~ ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( Cessna 208MODEL SERIES SECTION 4 - NORMAL PROCEDURES .PREFLIGHT INSPECTION CD CABIN PILOT'S OPERATING HANDBOOK TEMPORARY REVISION 1. Pilot's Operating Handbook and Other Required Documents -- AVAILABLE IN THE AIRPLANE. 2. Control Locks --REMOVE (DISENGAGE rudder lock, if installed). 3. Parking Brake -- SET . 4. All Switches -- OFF. 5. All Circuit Breakers -- IN. 6. Static Pressure Alternate Source Valve -- OFF (full in) . . 7. Inertial Separator T-Handle -- NORMAL. 8. Standby Flap Motor Switch (Overhead) -- GUARDED NORM. 9. Oxygen Supply Pressure -- CHECK. 10. Oxygen Masks -- CHECK AVAILABLE. 11. Fuel Selector Valves -- CHECK ON and FEEL AGAINST STOPS. 12. Radar -- OFF. 13. Air Conditioner (if installed) -- OFF. 14. inverier Switch (if instaiied) -- OFF. 15. Bleed Air Heat Switch -- OFF . 16. Emergency ' Power Uwer -- NORMAL, and if applicable, copper witness wire present and in t ac t. 17. Trim Controls -- SET. . 18. Fuel Shutoff -- ON. 19. Cabin Heat Firewall Shutoff Control -- CHECK IN . 20 . Battery Switch -- ON . 21 . Avionics Power Switch No. 2 -- ON. Check audibly that avionics cooling fan is operating. 22. Avionics Power Switch No. 2 .- OFF. 23. Fuel Quantity Indicators -- CHECK QUANTITY. 24. Wing Flaps -- UP . . 25 . Pilot/Static and Stall Heal Switches -- ON for 30 seconds, then OFF. (Ensure pitot/static tube covers are removed.) . 26. .Battery Switch -- OFF. CD LEFT SIDE 1. Fuel Reservoir Drain (bottom .of fuselage or left side of .cargo pod) -- 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 (see Section 7 Fuel System Schematic for all nine drain locations) until all contamination has been removed. 23 September 2003 For Training Purpo~es Only 208PHTR02 IThis Pagel{ltentionally Left Blank I ,. \ For Training Purposes Only ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( (