CESSNA GRAND CARAVAN
C208B
QUICK REFERENCE HANDBOOK
Original
COPY # __
Page 1
Table of Contents
Page Title
Page
Title
1
Table of Contents
29
Normal Checklist
2
Distribution List/Revision and Use Policy
30
Briefing Card
3
List of Effective Pages
31
DG Hazard and Handling Labels
4
Emergency and Abnormal Index
32
DG Hazard and Handling Labels
5
Emergency and Abnormal Index
33
DG Carried by Passengers or Crew
6
Emergency and Abnormal Index
34
DG Carried by Passengers or Crew
7
Airspeeds for Emergency Operation
35
DG Emergency Response Guide
8
Maximum Glide
36
DG Emergency Response Guide
9
Emergency Procedures
37
Annunciator Panel
10
Emergency Procedures
11
Emergency Procedures
12
Emergency Procedures
13
Emergency Procedures
14
Emergency Procedures
15
Emergency Procedures
16
Abnormal Procedures
17
Abnormal Procedures
18
Abnormal Procedures
19
Abnormal Procedures
20
Abnormal Procedures
21
Abnormal Procedures
22
Maximum Takeoff and Climb Torque
23
Takeoff Performance
24
Takeoff Performance
25
Cruise Performance
26
Landing Performance
27
Landing Performance
28
Intercept Procedures
Rev: Original
Date: 06-Nov-2014
C208B Quick Reference Handbook
Page 2
Distribution List
Two copies of the QRH have been issued by Air Serv Limited and Approved by the
Civil Aviation Authority as indicated below:
COPY NO.
ISSUED TO
COPY TYPE
01
Air Serv Limited
Hardcopy
02
CAA - Uganda
Hardcopy
The Chief Pilot shall be responsible for issuing and controlling certified true copies
of the QRH Copy No.1, for use/reference by Air Serv, see listing below:
CERTIFIED
COPY NO.
ISSUED TO
COPY TYPE
01
Operations Library
Hardcopy
02
5X-ASI
Hardcopy
03
5X-ASA
Hardcopy
04
5X-ASB
Hardcopy
05
5X-ASC
Hardcopy
06
5X-ACE
Hardcopy
e-Copy
Director of Operations
Electronic copy held on
server available to all staff
Revision Policy
The Operations Manual indicates that the Chief Pilot issues additions to and revision for any
pages in this document. Upon receipt of any amendments, they are to be incorporated into
the manual immediately and the revision sheet completed and signed.
If any error is found by a user it should be brought to the attention of the Chief Pilot as soon
as possible. If the error is a safety issue, they are to inform the base as soon as practical.
Use Policy
This document is for use by Air Serv operations staff and flight crew and it is used in
conjunction with other Air Serv documents. All performance charts are based on the
approved Pilots Operating Handbook, for the Cessna Grand Caravan (C208B) and have
incorporated additional safety margins as prescribed by Air Serv. It is the PIC’s ultimate
responsibility to ensure the aircraft is operated within the limitations of the Pilots Operating
Handbook and appropriate CAR’s.
Rev: Original
Date: 06-Nov-2014
C208B Quick Reference Handbook
Page 3
Revision List
Revision Date
Pages Amended
Added By
Original
All
Incorporated
List of Effective Pages
Page
Revision Date
Page
Revision Date
1
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3
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4
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7
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27
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8
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Rev: Original
Date: 06-Nov-2014
C208B Quick Reference Handbook
Page 4
EMERGENCY AND ABNORMAL INDEX
AIRSPEEDS FOR EMERGENCY OPERATION ...................................... 7
MAXIMUM GLIDE CHART ....................................................................... 8
EMERGENCY EVACUATION .............................................................. 15A
EMERGENCY DESCENT PROCEDURE ............................................ 14B
ENGINE START MALFUNCTIONS
Hung Start or Hot Start ............................................................. 15B
Ignition Failure .......................................................................... 15B
SMOKE AND FIRE
Engine Fire In Flight
(Red ENGINE FIRE Annunciator ON or OFF) ............................ 9A
Electrical Fire In Flight ................................................................ 9B
Cabin Fire ................................................................................... 9B
Wing Fire .................................................................................. 10A
Cabin Fire During Ground Operations ...................................... 10B
Engine Fire During Ground Start
(Red ENGINE FIRE Annunciator ON Or OFF)..........................10C
ENGINE FAILURES
Engine Failure During Takeoff Roll ...........................................10D
Engine Failure Immediately After Takeoff ................................. 10E
Engine Failure During Flight ..................................................... 11A
Engine Flameout During Flight ................................................. 11B
AIRSTART
Starter Assist (Preferred Procedure) ......................................... 16A
No Starter Assist ...................................................................... 16B
FORCED LANDINGS
Emergency Landing Without Engine Power ..............................16C
Precautionary Landing With Engine Power ............................... 17A
Ditching .................................................................................... 17B
Rev: Original
Date: 06-Nov-2014
C208B Quick Reference Handbook
Page 5
ICING
Weather Conditions That May Be Conductive
To Severe Inflight Icing (As Required By AD 96-09-15) ............19D
Procedures For Exiting Severe Icing Conditions
(As Required By AD 96-09-15) ................................................. 19E
Inadvertent Icing Encounter ...................................................... 20A
Static Source Blockage
(Erroneous Instrument Reading Suspected) ............................. 20B
ENGINE MALFUNCTIONS
Loss Of Oil Pressure
(Red OIL PRESSURE LOW Annunciator ON).......................... 12A
Fuel Control Unit Malfunction In The Pneumatic Or Govern
or Sections (Engine Power Falls Back To Idle) ......................... 12B
Gear Box Contamination
(Amber Chip Detector Annunciator ON) ..................................17C
FUEL SYSTEM MALFUNCTIONS
Loss Of Fuel Pressure
(Amber FUEL PRESS LOW Annunciator ON) ..........................17D
Fuel Flow Interruption To Fuel Reservoir
(Red RESERVOIR FUEL LOW Annunciator ON) .....................12C
Fuel Tank Selector Off During Engine Start
(Red FUEL SELECT OFF Annunciator ON And
Both Fuel Selector Warning Horns Activated) ...........................12D
Fuel Level Low With Single Tank Selected
(Red FUEL SELECT OFF And Amber LEFT Or
RIGHT FUEL LOW Annunciator ON And Fuel
Selector Warning Horn Activated)............................................. 12E
FLAP SYSTEM MALFUNCTIONS
Asymmetric Flap Extension Or Sudden Flap
Retraction On One Side ........................................................... 12F
Flaps Fail To Extend Or Retract ............................................... 18A
LANDING GEAR MALFUNCTIONS
Landing With A Flat Main Tire .................................................. 18B
Landing With A Flat Nose Tire ..................................................18C
Rev: Original
Date: 06-Nov-2014
C208B Quick Reference Handbook
Page 6
ELECTRICAL MALFUNCTIONS
Battery Temperature High
(Amber BATTERY HOT Annunciator On)................................. 19A
Battery Overheated
(Red BATTERY OVERHEAT Annunciator On) ........................ 13A
Voltage Low (Red VOLTAGE LOW Annunciator On) ............... 13B
Generator Malfunction with Standby power (Red VOLTAGE LOW
And/Or Red GENERATOR OFF Annunciators ON) .................. 13B
Inverter Failure (Amber INVERTER INOP Annunciator ON) ..... 19B
Starter Contactor Does Not Disengage After Engine Start
(Amber STARTER ENERGIZED Annunciator ON) ...................19C
Standby Power Malfunction
(STB PWR INOP Annunciator ON)...........................................13C
Electric Trim Malfunction .......................................................... 14A
INADVERTENT OPENING OF AIRPLANE DOORS IN FLIGHT
Upper Half Of Cargo Door Of Upper Half Of Passenger
Airstair Door Open (Red DOOR WARNING Annunciator ON) ..14C
Lowe Half Of Passenger Airstair Door Open.............................14D
Right Or Left Crew Doors Open ................................................ 14E
Cargo Pod Door(S) Open ......................................................... 14F
VACUUM SYSTEM
Vacuum Failure (Red VACUUM LOW annunciator ON) ...........15C
Rev: Or iginal
Date: 06-Nov-2014
C208B Quick Reference Handbook
C-208B EMERGENCY AIRSPEEDS
C208B CESSNA GRAND CARAVAN (675 SHP) WITH PAYLOAD EXTENDER MOD.
Engine Failure After Takeoff:
Wing Flaps Up
100 KIAS
Wing Flaps Down
80 KIAS
Maneuvering Speed:
9000 Pounds
143 KIAS
8750 Pounds
148 KIAS
7500 Pounds
137 KIAS
6250 Pounds
125 KIAS
5000 Pounds
112 KIAS
Maximum Glide:
With Cargo Pod
Without Cargo Pod
9000 Pounds
97 KIAS
99 KIAS
8750 Pounds
95 KIAS
97 KIAS
7500 Pounds
87 KIAS
90 KIAS
6250 Pounds
79 KIAS
82 KIAS
5000 Pounds
71 KIAS
74 KIAS
Precautionary Landing with Engine Power
Flaps Down
80 KIAS
Landing Without Engine Power:
Wing Flaps Up
100 KIAS
Wing Flaps Down
80 KIAS
Rev: Or iginal
Date: 06-Nov-2014
C208B Quick Reference Handbook
Page
7
C-208B EMERGENCY AIRSPEEDS
Page
Maximum Glide Chart
SECTION 3
EMERGENCY PROCEDURES
CESSNA
MODEL 208B G1000
ENGINE FAILURE (Continued)
MAXIMUM GLIDE
Rev: Or iginal
Figure 3-1
Propeller feathering is dependent on circumstances and is at the
discretion of the pilot. However, if engine oil pressure drops below 15
psi, the propeller should be feathered.
If an airstart is to be attempted, follow the checklist procedures. The
Starter Assist procedure is preferred since it results in cooler engine
starts. Successful airstarts (with starter assist) can be achieved at all
airspeeds
normally flown and up to an altitude of
14,000 feet. However,
Date: 06-Nov-2014
C208B Quick Reference Handbook
above 14,000 feet, or with the gas generator RPM below 10%, starting
temperatures tend to be higher and caution is required.
8
C-208B EMERGENCY PROCEDURES
Continued…
SMOKE AND FIRE
WARNING Without electrical power,
A
ENGINE FIRE IN FLIGHT
Red ENGINE FIRE annuciator light ON or OFF
1. Skytrac and ELT Switch..................….ACTIVATE
2. Power Lever ................................................... IDLE
3. Propeller Control Lever ........................ FEATHER
4. Fuel Condition Lever ...............................CUTOFF
5. Fuel Shutoff ..................................................... OFF
6. Cabin Heat Firewall Shutoff Control ....PULL OFF
7. Forward Side Vents ..................................... CLOSE
8. Overhead Vents ............................................. OPEN
9. Ventilation Fans (if installed) ..............................ON
10.Wing Flaps ....................................................20°- 30°
11.Airspeed ................................................ 80-85 KIAS
EMERGENCY LANDING
WITHOUT ENGINE POWER
1. Seats, Seat Belts, Shoulder Harness SECURE
2. Airspeed:
Flaps UP.............................. 100 KIAS
Flaps DOWN ..........................80 KIAS
3. PowerLever .............................................. 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. Nonessential Equipment (if installed) ....... OFF
10. Fuel Shutoff ...............................................OFF
11. Fuel Tank Selectors ......(horn will sound) OFF
12. Wing Flaps(full recommended)AS REQUIRED
13. Crew Doors ................. UNLATCH PRIOR TO
TOUCHCHDOWN
14.Battery Switch (when landing is assured) OFF
15. Touchdown ................... SLIGHTLY TAIL LOW
16. Brakes .................................APPLY HEAVILY
ELECTRICAL or CABIN FIRE
IN FLIGHT
Rev:
1.
2.
3.
4.
5.
6.
7.
Orignal
Skytrac and ELT Warning Switch….ACTIVATE
Battery Switch ............................................ OFF
Generator Switch ............ TRIP and RELEASE
Standby Power Switch (if installed) ............ OFF
Vents ..................................................... CLOSE
Bleed Air Heat Switch ................................ OFF
Fire Extinguisher ............................. ACTIVATE
Date:
06-Nov214
9
all electricallyoperated gyros and engine instruments, fuel boost
pump, annunciator lights, wing flaps and all avionics will
be inoperative Vacuum-driven gyros will still be
operative (For airplanes with a KFC-150 autopilot,
vacuum-driven gyros are the pilot’s horizon gyro and
right-hand directional gyro For airplanes with a KFC250 autopilot, vacuum-driven gyros are the right-hand
horizon and directional gyros)
WARNING
Occupants should use oxygen masks until
smoke clears After discharging an extinguisher within a
closed cabin, ventilate the cabin
IF ELECTRICAL FIRE:
8. Avionics Power Switches ........................... OFF
9. All Other Electrical Switches ...................... OFF
If fire appears out and electrical power is necessary
for continuance of flight:
10. Battery Switch and STBY Power Switch......ON
11. Generator Switch ........ RESET and RELEASE
12.
13.
14.
15.
16.
CB ..... CHECK for faulty circuit; do not reset
Inverter Switch (if installed) ...................... 1 or 2
Radio Switches .......................................... OFF
Avionics Power Switches ............................. ON
Radio and Electrical Switches (one at a time,
with delay after each until short circuit is
localized) ...................................................... ON
17. Vents (when it is ascertained that fire is
completely extinguished)......................... OPEN
18. Bleed Air Heat ........................... ON as desired
If Cabin Fire:
EMERGENCY LANDING WITH
ENGINE POWER
1.
2.
3.
4.
5.
B
Page
6.
7.
8.
9.
10.
11.
12.
13.
14.
Seats, Seat Belts, Shoulder Harness.SECURE.
Wing Flaps .................................................. 10°.
Airspeed ..............................................90 KIAS.
Selected Field ............................... FLY OVER,
*NOTE TERRAIN AND OBSTRUCTIONS
All Electrical Switches (except Battery and
Generator) .................................................. OFF
Wing Flaps . FULL DOWN (on final approach)
Airspeed ...............................................80 KIAS
Crew Doors UNLATCH PRIOR TO TCHDOWN
Skytrac and ELT………………… . ...ACTIVATE
Generator Switch ............ TRIP and RELEASE
Battery Switch ............................................ OFF
Touchdown .................... SLIGHTLY TAIL LOW
Fuel Condition Lever ...........................CUTOFF
Brakes ...................................APPLY HEAVILY
C208B Quick Reference Handbook
10
C-208B EMERGENCY PROCEDURES Page
ENGINE MALFUNCTIONS
A
D
WING FIRE
1.
2.
3.
4.
5.
6.
7.
8.
Skytrac and ELT Warning Switch….ACTIVATE
Pitot/Static Heat Switch .............................. OFF
Stall Heat Switch ........................................ OFF
Strobe Lights Switch .................................. OFF
Navigation Lights Switch ............................ OFF
Landing and Taxi Light Switches ............... OFF
Radar.......................................................... OFF
Ventilation Fans (if installed) ...................... OFF
WARNING Perform a sideslip as required to keep
flames away from the fuel tank and cabin Land the
airplane
B
CABIN FIRE DURING GROUND
OPERATIONS
1.
2.
3.
4.
5.
6.
7.
8.
Power Lever .............................................. IDLE
Brakes ...................................... AS REQUIRED
Propeller Control Lever .................... FEATHER
Fuel Condition Lever ...........................CUTOFF
Skytrac and ELT Warning Switch….ACTIVATE
Battery Switch ............................................ OFF
Airplane ......................................... EVACUATE
Fire .............................................. EXTINGUISH
C
ENGINE FAILURE DURING TAKEOFF
ROLL
1. Power Lever ............................................ BETA
2. Brakes ................................................... APPLY
3. Wing Flaps. ...................................... RETRACT
If airplane cannot be stopped on remaining runway:
4.
5.
6.
7.
8.
Fuel Condition Lever ...........................CUTOFF
Fuel Shutoff ...............................OFF (pull out)
Fuel Tank Selectors ..... OFF (horn will sound)
ISAT and ELT Warning Switch ....... ACTIVATE
Battery Switch ............................................ OFF
E
ENGINE FAILURE IMMEDIATELY AFTER
TAKEOFF
1.
2.
3.
4.
5.
6.
7.
8.
Airspeed ...................... 85 KIAS with 20° flaps
Skytrac and ELT Warning Switch….ACTIVATE
Propeller ........................................... FEATHER
Wing Flaps ...................................FULL DOWN
Fuel Condition Lever ...........................CUTOFF
Fuel Shutoff ................................OFF (pull out)
Fuel Tank Selectors ..... OFF (horn will sound)
Battery ........................................................ OFF
ENGINE FIRE DURING START ON
GROUND
(Red ENGINE IFIRE Annunciator On or Off)
1. Fuel Condition Lever ...........................CUTOFF
2. Fuel Boost Switch ...................................... OFF
3. Starter Switch ....................................... MOTOR
CAUTION Do not exceed the starting cycle limitations;
refer to Section 2 Should the fire persist, as indicated
by sustained inter-turbine temperature, Immediately
close the fuel shutoff and continue motoring.
Rev:
4.
5.
6.
7.
8.
9.
Orignal
Starter Switch ............................................. OFF
Fuel Shutoff ................................OFF (pull out)
ISAT and ELT Alert Switch.............. ACTIVATE
Battery Switch ............................................ OFF
Airplane ......................................... EVACUATE
Fire .............................................. EXTINGUISH
Date:
06-Nov214
C208B Quick Reference Handbook
C-208B EMERGENCY PROCEDURES
A
ENGINE FAILURE DURING FLIGHT
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
Skytrac and ELT Alert Switch…. ..... ACTIVATE
Airspeed ...............................................95 KIAS
Power Lever .............................................. IDLE
Propeller Control Lever .................... FEATHER
Fuel Condition Lever ...........................CUTOFF
Wing Flaps ................................................... UP
Fuel Boost Switch ...................................... OFF
Fuel Shutoff ................................OFF (pull out)
Ignition Switch ........................................ NORM
Standby Power Switch (if installed) ............ OFF
Electrical Load .................................... REDUCE
EMERGENCY LANDING WITHOUT ENGINE POWER
12. Seats, Seat Belts, Shoulder Harness SECURE.
13. Airspeed:
........................................100 KIAS (Flaps UP)
................................... 80 KIAS (Flaps DOWN)
14. PowerLever .............................................. IDLE.
15. Propeller Control Lever ................... FEATHER.
16. Fuel Condition Lever ..........................CUTOFF.
17. Fuel Boost Switch ..................................... OFF.
18. Ignition Switch ....................................... NORM.
19. Standby Power Switch (if installed) ........... OFF.
20. Nonessential Equipment (if installed) ........ OFF.
21. Fuel Shutoff ...............................OFF (pull out).
22. Fuel Tank Selectors ..... OFF (horn will sound)
23. Skytrac and ELT Switch…… .. .….…ACTIVATE
24. Wing Flaps AS REQD (FULL recommended).
Continued on next page…………
25. Crew Doors .................. UNLATCH PRIOR TO
TOUCHCHDOWN
26. Battery Switch OFF when landing is assured.
27. Touchdown ................... SLIGHTLY TAIL LOW.
28. Brakes .................................. APPLY HEAVILY
Page
11
AIRSTART (STARTER ASSIST) FOR NO STARTER
ASSIST REF 15-B
1. Electrical Load .................................... REDUCE
2. Standby Power Switch (if installed) ............ OFF
3. Avionics Power Switches ........................... OFF
4. Ignition Switch ........................................ NORM
5. Air Conditioner (if installed) ........................ OFF
6. Bleed Air Heat Switch ................................ OFF
7. Emergency Power Lever ................... NORMAL
8. Power Lever .............................................. IDLE
9. Propeller Control Lever ......................MIN RPM
10. Fuel Condition Lever ...........................CUTOFF
11. Fuel Shutoff ..................................ON (push in)
12. Fuel Tank Selectors ....... LEFT ON, RIGHT ON
13. Battery Switch .............................................. ON
14. Fuel Boost Switch – .................................... ON
15. AUX FUEL PUMP ON Annunciator .... CHK ON
16. FUEL PRESS LOW Annunciator ...... CHK OFF
17. Altitude .......................... 20,000 feet maximum
18. Starter Switch .............. START and OBSERVE
a.
IGNITION ON Annunciator CHECK ON
b.
Engine Oil Pressure ...........CHECK for
indication
c.
Ng ................................. 12% MINIMUM
19. Fuel Condition Lever ................ LOW IDLE and
OBSERVE
a.
ITT ..... MONITOR (1 090°C maximum)
b.
Ng ................................. 52% MINIMUM
20. Starter Switch ............................................. OFF
WARNING If conditions exist, such as heavy
precipitation or nearly empty fuel tanks, turn the
ignition switch ON.
21. Fuel Boost Switch .................................. NORM
(unless it cycles on and off; then leave ON)
22. Fuel Condition Lever ....................... HIGH IDLE
23. Propeller Control Lever ............... AS DESIRED
24. Power Lever ................................ AS DESIRED
25. Electrical Equipment ................ AS REQUIRED
B
ENGINE FLAMEOUT DURING FLIGHT
If Gas Generator Speed (Ng) Is Above 50%
1. Power Lever .............................................. IDLE
2. Fuel Selectors ...................................BOTH ON
3. Fuel Boost Pump ……………………………..ON
4. Ignition Switch .............................................. ON
5. Skytrac and ELT Warning Switch….ACTIVATE
6. Power Lever ................................ AS DESIRED
7. Ignition Switch ............................................ OFF
If Gas Generator Speed (Ng) is Below 50%:
1.
Fuel Condition Lever ........................CUTOFF
Rev:
Continued….
Orignal
Date:
06-Nov214
C208B Quick Reference Handbook
C-208B EMERGENCY PROCEDURES
Page
12
A
D
LOSS OF OIL PRESSURE
FUEL TANK SELECTOR OFF DURING
ENGINE START
(Red FUEL SELECT OFF Annunciator On
And Both Fuel Selector Warning Horns
Activated)
(Red OIL PRESS LOW Annunciator On)
1. Oil Pressure Gage ........... CHECK oil pressure
indication
If oil pressure gage confirms annunciator warning,
proceed in accordance with Engine Failures
checklists or at the discretion of the pilot and
consistent with safety, continue engine operation in
preparation for an emergency landing as soon as
possible.
B
(Engine Power Falls Back To Idle)
1. Power Lever .............................................. IDLE
2. Emergency Power Lever .......... AS REQUIRED
(maintain 65 Ng minimum during flight)
CAUTION The emergency power lever overrides
normal fuel control functions and results in the direct
operation of the fuel metering valve Utilize slow and
smooth movement of the emergency power lever to
avoid engine surges, and/or exceeding lTT, Ng, and
torque limits
FUEL SYSTEM
MALFUNCTIONS
C
FUEL FLOW INTERRUPTION TO FUEL
RESERVOIR (Red RESERVOIR FUEL LOW
Annunciator On)
1.
2.
3.
4.
5.
Fuel Tank Selectors ....... LEFT ON, RIGHT ON
Fuel Boost Switch ........................................ ON
Ignition Switch .............................................. ON
Skytrac and ELT Warning Switch….ACTIVATE
If RESERVOIR FUEL LOW annunciator
remains illuminated and there is usable fuel in
the wing tanks:
a. Carefully monitor engine gages and FUEL
PRESS LOW annunciator for signs of fuel
starvation
b. Land as soon as possible and determine
cause of RESERVOIR ~ FUEL LOW
warning
Continued…
WARNING If there are signs of fuel starvation, prepare
for a forced landing (as described in Emergency
Landing Without Engine Power)
Orignal
E
FUEL LEVEL LOW WITH SINGLE TANK
SELECTED (Red FUEL SELECT OFF And Amber
FCU MALFUNCTION IN THE PNEUMATIC
OR GOVERNOR SECTIONS
Rev:
1. Left and Right Fuel Tank Selectors .............. ON
Date:
06-Nov214
LEFT Or RIGHT FUEL LOW Annunciators On And
Fuel Selector Warning Horn Activated)
1. Left and Right Fuel Tank Selectors .............. ON
(turning both fuel tank selectors ON will extingush
the red FUEL SELECT OFF annunciator and
silence the warning horn)
FLAP SYSTEM
MALFUNCTION
PROCEDURES
F
ASYMMETRIC FLAP EXTENSION OR
SUDDEN FLAP RETRACTION ON ONE
SIDE
1. Apply aileron and rudder to stop the roll
2. Flap Selector ................................................ UP
3. Airspeed ................SLOW to 100 KIAS or less
4. If both flaps retract to a symmetrical setting:
a. Plan a flaps up landing
b. Refer to Section 5 (notes above landing
performance tables) for increase in
approach speed and landing distance
6. If both flaps cannot be retracted to a
symmetrical setting:
a. Land as soon as practical
b. Maintain a minimum airspeed of 90 KIAS
on the approach and avoid a nose high
flare on landing
C208B Quick Reference Handbook
13
C-208B EMERGENCY PROCEDURES Page
If GENERATOR OFF annunciator is extinguished
ELECTRICAL POWER
and STBY ELECT PWR ON annunciator is
illuminated:
SUPPLY SYSTEM
3. Perform steps 4, 5, and 6 above
MALFUNCTIONS
If GENERATOR OFF annunciator is extinguished
and STBY ELECT PWR INOP annunciator is
illuminated:
A
BATTERY OVERHEATED
(Red BATTERY OVERHEAT Annunciator On) (NiCad Battery Equipped Airplanes Only)
1.
2.
3.
4.
5.
Battery Switch ..................................... CHECK OFF
Generator Switch .....................................................
Standby Power Switch (if installed) .........................
All Electrical System Switches .................................
Bus 1 Pwr and Bus 2 Pwr CBs ................................
(total of 6 circuit breakers)
6. Avionics Switches ....................................................
7.
8.
Standby Power Switch (if installed) ..................................
Avionics Standby Power Switch ………...Lift Switch,
TURN ON
9. Avionics Bus tie Switch ............ LIFT GUARD, TURN ON
10. Reinstate essential electrical systems, exercising caution
not to exceed capacity of standby electrical system
(if installed)
11. ISAT and ELT Alert Switch ............................ CONSIDER
12. As Soon as Practical .............................................. LAND
B
3. STBY PWR Switch ....................... Off, then ON
4. STBY ELECT PWR INOP
Annunciator ..................... Check Extinguished
If STBY ELECT PWR INOP annunciator remains
illuminated:
5. Go to 13C, STNDBY ELECT PWR INOP
ANNUNCIATOR ILLUMINATED
C
STDBY ELECT PWR INOP ANNUNCIATOR
ILLUMINATED:
1. STBY PWR Switch ....................... Off, then ON
2. STBY ELECT PWR INOP
Annunciator ..................... Check Extinguished
If STBY ELECT PWR INOP annunciator remains
illuminated:
GENERATOR FAILURE
(GENERATOR OFF, Red VOLTAGE LOW and/or
STBY ELECT PWR Annunciators On)
1.
Generator Switch ....................... TRIP, then RESET
If primary power is not restored:
2. GEN CONT and GEN FIELD CBs ........ RESET
(If tripped) and repeat step 1.
If GENERATOR OFF annunciator remains
illuminated and STBY ELECT PWR INOP
annunciator is illuminated:
3. STBY PWR Switch .................................... OFF
4. Oil Pressure Gauge................................ Check
CAUTION
An Indication of less than normal or 0 may
indicate failure of the scavenge oil system,
closely monitor engine gauges and oil pressure
for signs of engine failure. Land as soon as
possible
5. Flight......... COMPLETE utilizing primary power
6. ISAT and ELT Alert Switch ........... CONSIDER
3. STBY PWR Switch .................... OFF, then ON.
Check STBY ELECT PWR INOP annunciator
extinguished and STBY ELECT PWR ON
annunciator illuminated.
4. AVIONICS STBY PWR and AVIONICS BUS
TIE Switches ................................................ ON
5. AVIONICS 1 and 2 Switches...................... OFF
6. Volt/Ammeter ............. SELECT ALT and verify
alternator load is 75 amperes or less. REDUCE
LOAD as required to prevent batty discharge.
Continued….
Rev: Original
Date: 06-Nov-2014
C208B Quick Reference Handbook
14
C-208B EMERGENCY PROCEDURES Page
INADVERTENT OPENING
OF AIRPLANE DOORS IN
ELECTRIC TRIM MALFUNCTION
FLIGHT
1. A/P DISC/TRIM INTER Switch…PRESS AND
A
HOLD
2. Elevator Trim Circuit
Breaker(7:10)……...........................PULL OFF
3. Retrim aircraft manually
WARNING
When disconnecting the autopilot after an
electric trim malfunction, hole the control wheel
firmly; up to 45 pounds of force on the control
wheel may be necessary to hold the aircraft
level.
EMERGENCY DESCENT
PROCEDURES
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. Wing Flaps ............................................... FULL
(wing downwash with flaps extended will move the
doors near their normally closed position)
3. If available or practical, have a second crew
member go aft to close and latch door
4. If landing is required with door open:
a. Approach and Landing ............... NORMAL
D
B
LOWER HALF OF PASSENGER AIRSTAIR
DOOR OPEN
ROUGH AIR
1. Seats, Seat Belts, Shoulder Harnesses
........................................................... SECURE
2. Power Lever .............................................. IDLE
3. Propeller Control Lever ...... MAX (full forward)
4. Wing Flaps ................................................... UP
5. Weights and Airspeed:
9062 Pounds .......................................143KIAS
8750 Pounds ......................................148 KIAS
7500 Pounds ......................................137 KIAS
6250 Pounds .......................................125KIAS
5000 Pounds .......................................112KIAS
1. Airspeed .... MAINTAIN LESS THAN 100 KIAS
2. Flight Controls ....... MANEUVER for return for
landing
3. Wing Flaps ............................................... FULL
4. Approach ........................................... NORMAL
5. Landing ......................... SLIGHTLY TAIL LOW
avoid nose high flare
E
RIGHT OR LEFT CREW DOORS OPEN
SMOOTH AIR
1.
2.
3.
4.
5.
C
Seats, Seat Belts, Shoulder Harnesses ..... SECURE
Power Lever ...................................................... IDLE
Propeller Control Lever ................ MAX (full forward)
Wing Flaps ...........................................................10°
Airspeed ..................................................... 175 KIAS
1. Airspeed .... MAINTAIN LESS THAN 125 KIAS
2. Door..................... PULL CLOSED and LATCH
F
CARGO POD DOOR(S) OPEN
Rev:
1. Airspeed .... MAINTAIN LESS THAN 125 KIAS
2. Land ......................AS SOON AS PRACTICAL
a. Approach .................................... NORMAL
b. Landing ...... AVOID A NOSE HIGH FLARE
Orignal
Date:
06-Nov214
C208B Quick Reference Handbook
C-208B EMERGENCY PROCEDURES
AIRCRAFT EVACUATION
Page
15
A
AIRCRAFT EVACUATION CHECKLIST
1.
2.
3.
4.
5.
6.
7.
8.
Park Brake.................................................. SET
Power Lever .............................................. IDLE
Propeller ........................................... FEATHER
Condition Lever ..................................CUT OFF
Standby Power ........................................... OFF
ISAT and ELT Alert Switch............ACTIVATED
Battery Switch ............................................ OFF
All People ...................................... EVACUATE
ABNORMAL STARTS
B
HOT START or HUNG START or IGNITION
FAILURE
1. Condition Lever ..................................CUT OFF
2. Starter Switch ....................................... MOTOR
CAUTION:
Should the fire persist, as possibly indicated by
sustained inter-turbine (ITT) temperature, continue
motoring
CAUTION:
DO NOT exceed starter cycle limitations.
3. Starter Switch ............................................. OFF
4. Battery Switch ............................................ OFF
VACUUM FAILURE
C
VACUUM FAILURE (Red VACUUM LOW
Annunciator ON)
Rev:
1. Vacuum Pressure Gauge ..................... VERIFY
a. If gauge indicates sufficient vacuum,
then continue to monitor situation
b. If gauge indicates no vacuum, then
proceed with partial panel procedures
Note:
For airplanes with KFC-150 or KFC-225
autopilot, vacuum driven gyros are the pilots
horizon gyro and right hand directional gyro
Original
Date:
06-Nov-2014
C208B Quick Reference Handbook
16
C-208B ABNORMAL PROCEDURES
Page
13. Fuel Boost Switch -- ON (check AUX FUEL
AIRSTART
PUMP ON annunciator ON, FUEL PRESS
A
STARTER ASSIST (Preferred Procedure)
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
13.
14.
15.
16.
17.
18.
Electrical Load ....................................... REDUCE
Standby Power Switch (if installed) ............... OFF
Avionics Power Switches .............................. OFF
Ignition Switch ........................................... NORM
Air Conditioner (if installed) ........................... OFF
Bleed Air Heat Switch .................................... OFF
Emergency Power Lever ...................... NORMAL
Power Lever ................................................. IDLE
Propeller Control Lever .........................MIN RPM
Fuel Condition Lever ..............................CUTOFF
Fuel Shutoff .....................................ON (push in)
Fuel Tank Selectors .......... LEFT ON, RIGHT ON
Battery Switch.................................................. ON
Fuel Boost Switch – ........................................ ON
AUX FUEL PUMP ON Annunciator ........ CHK ON
FUEL PRESS LOW Annunciator.......... CHK OFF
Altitude .............................. 20,000 feet maximum
Starter Switch ................. START and OBSERVE
a. IGNITION ON Annunciator ...... CHECK ON
b. Engine Oil Pressure CHECK for indication
c. Ng ....................................... 12% MINIMUM
19. Fuel Condition Lever LOW IDLE and OBSERVE
a. ITT ........... MONITOR (1 090°C maximum)
b. Ng ....................................... 52% MINIMUM
20. Starter Switch ................................................ OFF
WARNING If conditions exist, such as heavy
precipitation or nearly empty fuel tanks, turn the ignition
switch ON.
21. Fuel Boost Switch ...................................... NORM
.... (Unless it cycles on and off; then leave ON)
22. Fuel Condition Lever .......................... HIGH IDLE
23. Propeller Control Lever .................. AS DESIRED
24. Power Lever ................................... AS DESIRED
25. Electrical Equipment .................... AS REQUIRED
B
NO STARTER ASSIST
Rev:
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
Original
Generator Switch ................ TRIP and Release
Standby Power Switch (if installed) ............ OFF
Avionics Power Switches ........................... OFF
Air Conditioner (if installed) ........................ OFF
Bleed Air Heat Switch ................................ OFF
Emergency Power Lever ................... NORMAL
Power Lever .............................................. IDLE
Propeller Control Lever ......................MIN RPM
Fuel Condition Lever ...........................CUTOFF
Fuel Shutoff ..................................ON (push in)
Fuel Tank Selectors ....... LEFT ON, RIGHT ON
Battery Switch .............................................. ON
Date:
06-Nov-2014
LOW annunciator OFF).
14. Ignition Switch -- .......................................... ON
Check IGNITION ON annunciator ON
15. Airspeed ........................... 100 KIAS minimum
(140 KIAS if propeller is feathered)
16. Altitude .......................... 20,000 feet maximum
(15,000 feet if propeller is feathered).
CAUTION Do not attempt a restart without starter assist
if Ng tachometer indicates zero RPM.
17. Ng Indicator ........................... CHECK STABLE
18. Fuel Condition Lever ................ LOW IDLE and
OBSERVE.
a. ITT ........... MONITOR (1 090°C maximum)
b. Ng ....................................... 52% MINIMUM
19. Ignition Switch -- NORM (Ng 52% or above)
unless conditions warrant leaving ON.
WARNING If conditions exist, such as heavy
precipitation or nearly empty fuel tanks, turn the ignition
switch ON.
20. Fuel Boost Switch -- NORM (unless it cycles
on and off); then leave ON
21. Fuel Condition Lever ....................... HIGH IDLE
22. Propeller Control Lever ............... AS DESIRED
23. Power Lever ................................ AS DESIRED
24. Generator Switch ......... RESET and RELEASE
25. Electrical and Avionics Equipment ............... AS
REQUIRED
FORCED LANDINGS
C
EMERGENCY LANDING WITHOUT ENGINE POWER
1. Seats, Seat Belts, Shoulder Harness . SECURE.
2. Airspeed:
........................................ 100 KIAS (Flaps UP)
................................... 80 KIAS (Flaps DOWN)
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. Nonessential Equipment (if installed) ......... OFF.
10. Fuel Shutoff ................................OFF (pull out).
11. Fuel Tank Selectors ....... OFF (horn will sound)
12. Skytrac and ELT Switch…… ... .….…ACTIVATE
13. Wing Flaps .. AS REQD (FULL recommended).
Continued on next page…………
14. Crew Doors .................... UNLATCH PRIOR TO
TOUCHCHDOWN
15. Battery Switch .. OFF when landing is assured.
16. Touchdown .................... SLIGHTLY TAIL LOW.
17. Brakes ....................................APPLY HEAVILY.
C208B Quick Reference Handbook
17
C-208B ABNORMAL PROCEDURES
Page
ENGINE MALFUNCTIONS
A
PRECAUTIONARY LANDING WITH ENGINE
POWER
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
13.
14.
Seats, Seat Belts, Shoulder Harness.SECURE.
Wing Flaps .................................................. 10°.
Airspeed ..............................................90 KIAS.
Selected Field ............................... FLY OVER,
(Note terrain and obstructions).
All Electrical Switches (except Battery and
Generator) .................................................. OFF
Wing Flaps . FULL DOWN (on final approach)
Airspeed ...............................................80 KIAS
Crew Doors UNLATCH PRIOR TO TCHDOWN
Skytrac and ELT………………… . ...ACTIVATE
Generator Switch ............ TRIP and RELEASE
Battery Switch ............................................ OFF
Touchdown .................... SLIGHTLY TAIL LOW
Fuel Condition Lever ...........................CUTOFF
Brakes .................................. APPLY HEAVILY
C
GEAR BOX CONTAMINATION
(Amber CHIP DETECTOR Annunciator On)
1. Engine Gages CAREFULLY MONITOR engine
gages for abnormal oil pressure, oil
temperature or power indications
2. If engine gages are normal, proceed to
destination and determine cause of chip
detector annunciator warning prior to next flight
3. If engine gages confirm chip detector
annunciator warning, proceed in accordance
with Engine Failures checklists or at the
discretion of the pilot and consistent with
safety, continue engine operation in preparation
for an emergency landing as soon as possible
FUEL SYSTEM
MALFUNCTIONS
B
DITCHING
Rev:
1. Radio--TRANSMIT MAYDAY on 121.5 MHz,
giving location and intentions and SQUAWK
7700 if transponder is installed. Select
Emergency Position on Skyrac and ELT.
2. Heavy Objects in Cabin -- SECURE if
passenger is available to assist.
3. Seats, Seat Belts, Shoulder Harnesses
.......................................................... SECURE.
4. Wing Flaps ..................................FULL DOWN.
5. Power -- ESTABLISH 300 FT/MIN DESCENT
AT 80 KIAS.
6. Approach ........... High Winds INTO THE WIND.
7. Light Winds, Heavy Swells -- PARALLEL TO
SWELLS.
8. Skytrac and ELT
Switch………………….ACTIVATE
9. Face -- CUSHION at touchdown with folded
coat or similar object.
10. Touchdown ........ NO FLARE, maintain descent
attitude.
11. Airplane ........................................ EVACUATE.
12. Life Vests and Raft ....... INFLATE when outside
cabin.
WARNING The airplane has not been flight tested in
actual ditching, thus the above recommended
procedure is based entirely on the best judgment of
Cessna Aircraft Company.
Original
Date:
06-Nov-2014
D
LOSS OF FUEL PRESSURE
(Amber FUEL PRESS LOW Annunciator
On)
1. Fuel Boost Switch ........................................ ON
2. If FUEL PRESS LOW annunciator
extinguishes:
a. Carefully monitor fuel quantity and cabin
odor for evidence of a fuel leak
b. Land as soon as practical and determine
cause for motive flow failure before next
flight
3. If FUEL PRESS LOW annunciator and AUX
FUEL PUMP ON annunciator are illuminated:
a. Carefully monitor engine gages for sign of
fuel starvation
b. Land as soon as possible
C208B Quick Reference Handbook
18
C-208B ABNORMAL PROCEDURES
Page
FLAP SYSTEM
LANDING GEAR
MALFUNCTION
MALFUNCTION
PROCEDURES
PROCEDURES
A
FLAPS FAIL TO EXTEND OR RETRACT
B
LANDING WITH FLAT MAIN TIRE
1. Flap Motor and STBY Flap Motor CBs CHECK
IN
2. If flaps still fail to extend or retract:
Earlier Airplanes:
a. Guarded Standby Flap Motor Switch
(Overhead) MOVE GUARD, and
POSITION SWITCH TO STBY
b. Standby Flap Motor Up/Down Switch
(Overhead) UP or DOWN (hold switch
until flaps reach desired position,
except release switch before flaps reach
full up or full down travel)
Later Airplanes:
a. Guarded and Safety-tied Standby Flap
Motor Switch (Overhead) MOVE GUARD,
breaking safety wire, and POSITION
SWITCH TO STBY
b. Guarded and Safety-tied Standby Flap
Motor Up/Down Switch (Overhead) .......
MOVE GUARD, breaking safety wire,
and position switch UP or DOWN (hold
switch until flaps reach desired
position, except release switch before
flaps reach full up or full down travel)
1. Airplane ............................ CONTINUE FLIGHT
(As desired to lighten fuel load).
1. Fuel Selectors ...................................................
............ POSITION ONE SELECTOR OFF TO
LIGHTEN LOAD ON SIDE OF FLAT TIRE
(maximum fuel unbalance of 200 pounds)
2. Approach ................... NORMAL FULL FLAPS)
3. Touchdown ................. INFLATED TIRE FIRST
Hold airplane off flat tire as long as possible
with aileron control
4. Directional Control ...........................MAINTAIN
(Using brake on wheel with inflated tire as
required).
C
LANDING WITH FLAT NOSE TIRE
1. Pax and Bags .......... MOVE AFT (if practical).
Remain within approved CG envelope.
2. Approach ........................................... NORMAL
WITH FULL FLAPS
3. Touchdown ................................... NOSE HIGH
HOLD NOSE-WHEEL OFF LANDING ROLL
4. Brakes ......................... MINIMUM AS NEEDED
CAUTION: With the standby flap system in use,
limit swItches, which normally shut off the primary
flap motor when reaching the flap travel limits, are
electrically inactivated Therefore, the pilot must
release the standby flap motor up/down switch
before the flaps reach their travel limit to prevent
overloading and damage to the flap system
Rev:
3. Guarded Standby Flap Motor Switch Leave
in STBY position until after landing when
maintenance action can be accomplished
Original
Date:
06-Nov-2014
C208B Quick Reference Handbook
19
C-208B ABNORMAL PROCEDURES
Page
STARTER CONTACTOR DOES NOT
ELECTRICAL POWER
DISENGAGE AFTER ENGINE START (Amber
STARTER ENERGIZED Annunciator On)
SUPPLY SYSTEM
1. Battery Switch ............................................ OFF
MALFUNCTIONS
2. Auxiliary Power Unit ... OFF, then DISENGAGE
A
3. Fuel Condition Lever ...........................CUTOFF
ICING
BATTERY TEMPERATURE HIGH
(Amber BATTERY HOT Annunciator On) (Ni-Cad
Battery Equipped Airplanes Only)
1. Battery Switch ............................................ OFF
2. Ammeter .............................................. CHECK
With selector switch in BATT
position
If ammeter shows zero indication:
(1) Annunciator light should extinguish
If ammeter shows charge indication:
(2) Generator Switch .............. TRIP AND
RELEASE
(3) Standby Power Switch (if installed)
.................................................... OFF
(4) All Electrical System Switches ... OFF
(5) Bus 1 Pwr and Bus 2 Pwr Circuit
Breakers ...........................PULL OFF
(total of 6 circuit breakers)
(6) Avionics Switches ....................... OFF
(7) Standby Power Switch (if installed)
...................................................... ON
(8) Avionics Standby Power Switch LIFT
GUARD, TURN ON
(9) Avionics Bus Tie Switch ............LIFT
GUARD, TURN ON
(10) Essential electrical systems .............
....................................... REINSTATE
(Exercise caution not to exceed
capacity of standby electrical
system).
B
INVERTER FAILURE
(Amber INVERTER INOP Annunciator On)
(Airplanes Equipped with KFC-250 Autopilot Only)
1. Inverter Switch ............SELECT other inverter
2. Failed Inverter ....... REPAIR before next flight
If INVERTER INOP Annunciator remains on:
3. Inverter 1 and 2 Circuit Breakers ..... CHECK IN
4. If the left-hand gyros are flagged, the
INVERTER INOP annunciator is correct
5. Disregard left-hand gyros, land as soon as
practical, and repair inverters
C
Rev:
Original
Date:
06-Nov-2014
D
THE FOLLOWING WEATHER CONDITIONS MAY BE
CONDUCIVE TO SEVERE IN-FLIGHT ICING - As
Required by AD 96-09-15, Paragraph (a) (2):
1. Visible rain at temperatures below 0 degrees
Celsius ambient air temperature.
2. Droplets that splash or splatter on impact at
temperatures below 0 degrees Celsius ambient
air temperature.
E
PROCEDURES FOR EXITING THE SEVERE ICING
ENVIRONMENT ............ As Required by AD 96-09-15,
Paragraph (a) (2):
These procedures are applicable to all flight phases
from takeoff to landing. Monitor the ambient air
temperature. While severe icing may form at
temperatures as cold as -18 degrees Celsius,
increased vigilance is warranted at temperatures
around freezing with visible moisture present. If the
visual cues specified in Section 2 Limitations for
identifying severe icing conditions are observed,
accomplish the following:
1. Immediately request priority handling from Air
Traffic Control to facilitate a route or an altitude
change to exit the severe icing conditions in
order to avoid extended exposure to flight
conditions more severe than those for which
the airplane has been certificated.
2. Avoid abrupt and excessive maneuvering that
may exacerbate control difficulties.
3. Do not engage the autopilot.
4. If the autopilot is engaged, hold the control
wheel firmly and disengage the autopilot.
5. If an unusual roll response or uncommanded
roll control movement is observed, reduce the
angle-of-attack.
CONTINUED ON NEXT PAGE……
6. Do not extend flaps during extended operation
in icing conditions. Operation with flaps
extended can result in a reduced wing angle-ofattack, with the possibility of ice forming on the
C208B Quick Reference Handbook
C-208B ABNORMAL PROCEDURES
upper surface further aft on the wing than
normal, possibly aft of the protected area.
7. If the flaps are extended, do not retract them
until the airframe is clear of ice.
8. Report these weather conditions to Air Traffic
Control.
A
INADVERTENT ICING ENCOUNTER
1.
2.
3.
4.
5.
6.
7.
Ignition Switch .............................................. ON
Inertial Separator ............................... BYPASS
Pitot-Static Heat Switch................................ ON
Stall Warning Heat Switch............................ ON
Windshield Anti-ice Switch(es) ............... AUTO
Prop Anti-Ice Switch ................................ AUTO
If Above 20,000 feet ..........................................
a. Airspeed: 160 KIAS or less
b. Altitude: DESCEND to 20,000 feet
or below as soon as practical
8. Flight Path ... Turn back or change altitude to
obtain an OAT that is less conducive to
icing.
9. Ignition Switch ...................................................
.......... OFF- AFTER 5 MINUTES OPERATION
10. Bleed Air Heat Switch and Temp Control .........
.............................................. ON and ADJUST
11. Push Fwd Cabin Heat Contol ............. FULL IN.
12. Defrost Control ............................... FULL OUT
(to obtain max windshield defrost effect).
13. Propeller RPM .......... INCREASE to 1900 RPM
(to minimize ice build-up).
Page
20
WARNING With heavy ice accumulations on the
horizontal stabilizer leading edge, do not extend flaps
while enroute or holding. When landing is assured,
select the minimum flap setting required, not to exceed
20°, and maintain extra airspeed consistent with
available field length. Do not retract the flaps once they
have been extended, unless required for go-around.
Then retract flaps in increments while maintaining 5 to
10 knots extra airspeed.
18. Land on the main wheels first, avoiding a slow
and high flare-out.
19. Missed approaches should be avoided
whenever possible because of severely
reduced climb capability. However, if a goaround is mandatory, make the decision much
earlier in the approach than normal. Apply
takeoff power and maintain 90 to 105 KIAS
while retracting the flaps slowly in small
increments.
B
STATIC SOURCE BLOCKAGE (Erroneous
Instrument Reading Suspected)
1. Static Pressure Alternate Source Valve...PULL FULL ON
NOTE The alternate static source is connected to the
left-hand flight panel instruments only.
2. Refer to Section 5 for airspeed and altimeter
corrections.
3. Autopilot ................... DISENGAGE altitude hold mode
Rev:
CAUTION If excessive vibration is noted, momentarily
reduce propeller RPM to 1600 with the propeller
control, then rapidly move the control full forward.
Cycling the RPM flexes the propeller blades and high
RPM increases centrifugal force, causing ice to shed
more readily
.
14. If icing conditions are unavoidable, plan a
landing at the nearest airport. With an
extremely rapid ice build-up, select a suitable
off airport’ landing site.
15. With an ice accumulation of 1/4 inch or more on
the wing leading edges, be prepared for a
significantly higher power requirement,
approach speed and stall speed and longer
landing roll.
16. If necessary, set up a forward slip for visibility
through the left portion of the windshield during
the landing approach.
17. Use a minimum approach speed of 105 KIAS,
select the minimum flap setting required, and
maintain extra airspeed consistent with
available field length. With ice suspected on the
airframe, or operating at 4°C or less in visible
moisture, Do Not Extend Flaps Beyond 20° for
Landing.
Original
Date:
06-Nov-2014
C208B Quick Reference Handbook
C-208B ABNORMAL PROCEDURES
Page
21
STARTING ENGINE (Auxiliary Power Start)
(24-28 Volt, Minimum 800 Amp and Maximum 1700 Amp
Capacity)
1. Battery Switch - ON.
2. External Power Switch - OFF.
3. Volt/Ammeter - CHECK (20 volts minimum).
4. Battery Switch - OFF.
5. Auxiliary Power Unit - ENGAGE; then ON.
6. External Power Switch - BUS.
7. Volt/Ammeter - CHECK 24 -28.5 Volts.
CAUTION
MAKE SURE THAT THE EMERGENCY POWER LEVER
IS IN THE NORMAL POSITION OR AN OVER
TEMPERATURE CONDITION WILL RESULT DURING
ENGINE START.
8. Battery Switch - ON.
9. External Power Switch - STARTER.
10. Emergency Power Lever - NORMAL (check
EMERGENCY POWER LEVER annunciator OFF).
11. Propeller - CLEAR.
12. Fuel Boost Switch - ON and OBSERVE.
A. AUX FUEL PUMP ON Annunciator - ON.
B. FUEL PRESS LOW Annunciator - OFF.
C. No fuel flow.
CAUTION
IF THE AUXILIARY POWER UNIT DROPS OFF THE LINE,
INIITIATE ENGINE SHUTDOWN
13. Starter Switch- START and OBSERVE
A. IGNITION ON Annunciator – CHECK ON.
B. Engine Oil Pressure – CHECK ON.
C. Ng – STABLE (12% minimum).
14. Fuel Condition Lever – LOW IDLE and OBSERVE.
A. Fuel Flow – CHECK for 90 to 140 pph.
B. ITT – MONITOR (1090 C° maximum, limited to 2 seconds).
CAUTION
• IF ITT CLIMBS RAPIDLY TOWARDS 1090°C, BE
PREPARED TO RETURN THE FUEL CONDITION
LEVER TO CUTOFF.
• UNDER HOT OAT AND/OR HIGH GROUND ELEVATION
CONDITIONS, IDLE ITT MAY EXCEED MAXIMUM IDLE
ITT LIMITATION OF 685°C. INCREASE Ng AND/OR
REDUCE ACCESSORY LOAD TO MAINTAIN ITT WITHIN
LIMITS.
Rev:
C. Ng - 52% MINIMUM.
15. Starter Switch - OFF (check STARTER ENERGIZED
annunciator OFF).
16. Inverter Switch (if installed) - 1 or 2.
17. Engine Instruments - CHECK.
18. External Power Switch - OFF.
19. Auxiliary Power Unit - OFF, then DISENGAGE.
20. Generator - CHECK GENERATOR OFF annunciator OFF
and battery charging.
21. Fuel Boost Switch - NORM (check AUX FUEL PUMP ON
annunciator OFF).
22. Avionics No.1 and No.2 Power Switches - ON.
23. Navigation Lights and Flashing Beacon - ON as required.
24. Suction Gage - CHECK.
25. Cabin Heating, Ventilating and Defrosting Controls – AS
DESIRED.
26. Radios - AS REQUIRED.
Original
Date:
06-Nov-2014
C208B Quick Reference Handbook
Page 22
Air Serv Limited Takeoff & Climb Torque for C208B (675 SHP) with Cargp Pod Installed
Directions: 1.) First number is max takeoff torque (Inerial Seperator in BYPASS, Cabin Heat OFF)
2.) Second number is max climb torque at 1000 ft. AGL assuming 2° C decrease in temperature (Inertial Seperator NORMAL, Cabin Heat OFF)
5° C
10° C
12° C
14° C
16° C
18° C
20° C
22° C
24° C
26° C
28° C
30° C
32° C
34° C
36° C
38° C
40° C
42° C
44° C
46° C
48° C
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
1850
1835
1795
1760
1720
1685
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
1850
1800
1760
1725
1685
1645
1600
1555
1515
1475
1435
1400
1360
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
1835
1815
1780
1745
1715
1680
-----
MAX
MAX
MAX
MAX
MAX
1850
1835
1805
1780
1730
1695
1660
1620
1585
1545
1495
1455
1415
1380
1335
-----
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
1835
1795
1770
1735
1705
1680
-----
-----
MAX
MAX
MAX
1840
1820
1785
1770
1740
1710
1665
1635
1595
1560
1525
1490
1435
1400
1360
1325
-----
-----
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
1835
1810
1775
1755
1725
1695
1665
-----
-----
-----
MAX
MAX
1820
1760
1740
1770
1705
1675
1640
1600
1570
1530
1495
1465
1425
1375
1340
-----
-----
-----
-----
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
MAX
1845
1810
1780
1755
1725
1695
1670
1645
-----
-----
-----
-----
MAX
1790
1745
1705
1680
1640
1640
1610
1575
1535
1505
1465
1435
1405
1360
1320
1280
-----
-----
-----
-----
MAX
MAX
MAX
MAX
MAX
MAX
MAX
1825
1805
1775
1745
1715
1695
1675
1645
1615
-----
-----
-----
-----
-----
MAX
1700
1660
1610
1600
1580
1560
1520
1480
1440
1400
1370
1340
1300
1260
-----
-----
-----
-----
-----
-----
7,000
MAX
MAX
MAX
MAX
1825
1795
1775
1755
1725
1700
1680
1645
1625
1590
1585
-----
-----
-----
-----
-----
-----
8,000
1700
1610
1600
1570
1530
1500
1490
1440
1415
1395
1340
1310
1290
1245
-----
-----
-----
-----
-----
-----
-----
9,000
1620
1560
1520
1500
1460
1440
1410
1380
1350
1320
1290
1260
1240
-----
-----
-----
-----
-----
-----
-----
-----
10,000
1550
1500
1480
1460
1430
1400
1360
1330
1300
1280
1250
1220
-----
-----
-----
-----
-----
-----
-----
-----
-----
11,000
1520
1450
1420
1390
1350
1320
1290
1270
1240
1220
1200
-----
-----
-----
-----
-----
-----
-----
-----
-----
-----
12,000
1430
1360
1340
1310
1280
1260
1230
1210
1180
-----
-----
-----
-----
-----
-----
-----
-----
-----
-----
-----
-----
13,000
1360
1310
1280
1260
1240
1220
1180
1150
1130
-----
-----
-----
-----
-----
-----
-----
-----
-----
-----
-----
-----
1,000
2,000
3,000
4,000
5,000
Climb Torque Only
6,000
Notes:
Takeoff:
1. Takeoff torque on this chart shall be achieved without exceeding 805°C ITT or 101.6% Ng. When ITT exceeds 765°C this power setting is time limited to 5 minutes
2. With cabin heater ON, where altitude and temperature do not permit 1865 ft-lbs for takeoff, decrease torque setting by 65 ft-lbs.
3. With the inertial separator in NORMAL increase torque by 15 ft-lbs
Climb:
4. Climb torque on this chart shall be achieved without exceeding 765°C ITT or 101.6 Ng.
5. With cabin heater ON, decrease torque setting by 80 ft-lbs
6. With the inertial separtor in BYPASS decrease torque by 100 ft-lbs
Rev: Original
06 Nov 2014
Air Serv Limited C-208B Payload Extender Takeoff Performance Chart (Distances in Meters)
WT
Tkof Speed
LBS
Vlof
V50
Alt
Roll
50 ft
Roll
50 ft
Roll
50 ft
Roll
50 ft
Roll
9062
71
86
0
797
891
822
918
846
945
871
971
1000
853
951
879
979
905
1007
940
2000
909
1010
937
1040
964
1069
3000
973
1079
1003
1112
1033
1146
4000
1036
1147
1069
1185
1103
5000
1111
1230
1169
1304
1227
6000
1187
1313
1269
1422
7000
1335
1502
1431
8000
1482
1692
1594
8950
8850
8750
8600
71
70
70
69
85
84
83
82
Press
20 C
Rev: Original
Page 23
Tkof Speed
50 ft
LBS
Vlof
V50
Alt
Roll
50 ft
Roll
50 ft
Roll
50 ft
Roll
50 ft
Roll
896
998
8500
68
81
0
676
745
696
766
717
788
738
809
759
831
1049
976
1091
1000
722
793
744
816
766
839
796
873
826
907
1009
1127
1055
1185
2000
768
840
791
865
814
890
853
936
892
982
1098
1231
1162
1317
3000
822
896
847
924
873
952
926
1019
979
1086
1222
1187
1336
1270
1449
4000
876
952
904
983
932
1014
999
1102
1066
1189
1377
1321
1509
1415
1641
5000
938
1020
985
1078
1033
1135
1109
1236
1185
1337
1351
1532
1456
1683
1560
1833
6000
1000
1087
1067
1172
1134
1257
1219
1371
1303
1485
1640
1528
1778
1652
1974
1775
2171
7000
1121
1234
1200
1339
1278
1444
1378
1588
1477
1732
1857
1705
2023
1848
2266
1990
2509
8000
1242
1382
1333
1506
1423
1630
1537
1805
1651
1979
30 C
35 C
40 C
8400
25 C
30 C
35 C
40 C
50 ft
0
774
863
798
889
822
915
846
940
870
965
0
655
720
675
741
695
761
715
782
736
803
828
920
853
947
879
975
913
1015
947
1056
1000
700
766
721
788
742
810
771
843
800
876
2000
882
978
909
1006
935
1034
980
1090
1024
1146
2000
744
812
766
836
789
859
826
903
864
948
3000
944
1044
973
1076
1003
1108
1065
1190
1127
1272
3000
796
866
821
892
846
919
897
983
948
1047
4000
1005
1110
1038
1146
1070
1182
1151
1290
1231
1398
4000
848
920
875
949
903
979
967
1062
1032
1146
5000
1078
1189
1134
1260
1190
1330
1280
1456
1371
1582
5000
908
984
954
1040
1000
1095
1073
1191
1146
1286
6000
1151
1269
1230
1374
1309
1479
1410
1622
1511
1766
6000
968
1049
1033
1130
1097
1211
1178
1319
1260
1427
7000
1294
1450
1387
1582
1480
1713
1599
1899
1718
2086
7000
1085
1189
1160
1289
1236
1388
1331
1524
1427
1659
8000
1436
1632
1544
1789
1651
1947
1788
2176
1925
2406
8000
1201
1330
1288
1447
1375
1565
1484
1728
1593
1892
67
81
20 C
1000
8300
68
Press
06 Nov.2014
WT
25 C
0
751
835
774
860
797
884
821
909
844
933
0
634
695
653
715
672
735
692
755
712
775
1000
803
890
828
916
852
942
885
981
919
1020
80
1000
677
739
697
761
718
782
746
813
774
845
2000
855
945
881
972
907
1000
950
1053
993
1107
2000
720
783
741
806
763
829
799
871
836
914
3000
915
1008
944
1040
972
1071
1032
1149
1092
1227
3000
770
835
794
861
818
886
867
947
916
1008
4000
975
1072
1006
1107
1037
1142
1115
1245
1192
1348
4000
821
887
847
915
874
943
935
1023
997
1102
5000
1045
1149
1099
1216
1153
1284
1240
1404
1327
1523
5000
879
949
923
1001
967
1054
1037
1145
1107
1235
6000
1116
1226
1192
1325
1268
1425
1365
1562
1462
1698
6000
937
1011
998
1088
1060
1165
1138
1267
1216
1369
7000
1253
1399
1343
1523
1433
1648
1547
1824
1661
2000
7000
1049
1144
1121
1238
1193
1332
1285
1459
1376
1586
8000
1390
1572
1494
1721
1597
1870
1729
2087
1860
2303
8000
1161
1278
1244
1388
1327
1499
1431
1651
1536
1804
0
728
807
750
830
773
854
796
877
818
901
0
616
674
634
693
653
712
672
731
691
751
1000
778
859
802
885
826
910
858
947
890
984
8200
1000
657
716
677
737
696
757
724
787
751
818
2000
828
912
853
939
879
965
920
1016
962
1067
2000
698
759
719
781
740
803
775
843
811
884
3000
886
973
914
1003
942
1034
1000
1108
1057
1183
3000
747
809
770
833
794
858
841
916
888
975
4000
944
1034
974
1068
1005
1102
1079
1200
1153
1298
4000
796
859
822
886
847
913
907
989
966
1065
5000
1012
1108
1064
1173
1115
1237
1199
1351
1283
1465
5000
852
918
895
969
937
1019
1004
1106
1072
1193
6000
1080
1182
1153
1277
1226
1372
1319
1501
1412
1631
6000
908
978
968
1052
1027
1125
1102
1223
1177
1321
7000
1212
1347
1298
1465
1385
1583
1494
1749
1604
1915
7000
1016
1106
1086
1196
1156
1285
1244
1407
1331
1528
8000
1344
1512
1444
1653
1543
1794
1669
1997
1795
2199
8000
1124
1234
1204
1340
1285
1445
1385
1590
1485
1735
0
697
770
718
792
739
814
761
837
783
859
0
597
653
615
671
633
689
652
708
670
726
1000
744
819
767
843
790
867
821
902
851
938
1000
637
694
656
713
675
733
702
762
728
791
8100
66
66
79
78
2000
792
869
816
894
840
920
880
968
920
1016
2000
677
734
697
756
718
777
752
816
786
855
3000
848
927
874
956
900
984
955
1054
1010
1124
3000
724
782
746
806
769
830
815
886
861
942
4000
903
985
932
1017
961
1049
1031
1141
1101
1233
4000
771
830
796
857
820
883
878
956
936
1028
5000
968
1055
1017
1116
1066
1176
1145
1282
1224
1388
5000
826
888
867
936
907
985
972
1068
1037
1151
6000
1032
1125
1101
1214
1171
1303
1259
1423
1347
1544
6000
880
946
937
1016
994
1086
1066
1179
1138
1273
7000
1158
1279
1239
1389
1321
1499
1424
1652
1528
1805
7000
984
1068
1051
1154
1118
1239
1203
1354
1287
1469
8000
1283
1434
1377
1565
1471
1696
1590
1882
1709
2067
8000
1088
1190
1165
1291
1242
1392
1339
1529
1435
1665
Air Serv Limited C-208B Payload Extender Takeoff Performance Chart (Distances in Meters)
WT
Tkof Speed
LBS
Vlof
V50
Alt
Roll
50 ft
Roll
50 ft
Roll
50 ft
Roll
50 ft
Roll
8000
65
78
0
579
631
596
649
613
666
631
684
1000
617
671
635
689
654
708
679
2000
655
710
675
730
695
751
3000
701
756
723
779
744
802
4000
747
802
770
828
794
5000
799
858
839
904
6000
852
913
907
980
7900
7800
7700
65
64
63
77
76
75
Press
20 C
25 C
Rev: Original
Page 24
Tkof Speed
50 ft
LBS
Vlof
V50
Alt
Roll
50 ft
Roll
50 ft
Roll
50 ft
Roll
50 ft
Roll
649
702
7500
62
74
0
491
533
506
547
520
562
534
577
549
592
736
705
764
1000
523
566
538
581
554
597
575
619
596
642
728
788
760
825
2000
554
599
571
615
588
632
615
662
642
692
788
855
833
908
3000
593
636
611
655
629
674
666
716
702
759
853
849
922
905
992
4000
631
674
651
695
671
715
716
771
762
826
878
950
940
1029
1002
1108
5000
675
719
708
756
740
793
791
856
841
918
962
1047
1031
1136
1100
1225
6000
720
765
765
818
810
872
866
941
921
1010
35 C
40 C
Press
06 Nov.2014
WT
30 C
20 C
25 C
30 C
35 C
63
75
50 ft
7000
952
1030
1016
1111
1081
1193
1162
1302
1242
1411
7000
802
858
854
922
907
986
972
1069
1037
1153
8000
1052
1147
1126
1242
1200
1338
1292
1467
1385
1596
8000
884
951
944
1025
1004
1100
1078
1198
1153
1295
0
560
610
577
626
594
643
611
660
628
677
0
475
515
488
528
502
542
516
557
530
571
1000
597
648
615
666
633
684
657
710
682
737
7400
62
1000
505
546
520
561
534
576
555
597
575
619
2000
633
685
653
705
672
725
704
760
735
796
2000
535
578
551
594
567
609
593
638
619
667
3000
678
730
699
752
720
774
762
824
805
875
3000
572
614
590
632
607
650
642
690
677
731
4000
722
774
744
798
767
823
821
889
874
955
4000
609
650
628
670
648
690
691
742
735
795
5000
773
827
810
871
848
915
908
991
968
1066
5000
652
694
683
729
715
764
763
824
811
883
6000
824
880
876
944
929
1008
995
1092
1061
1177
6000
695
737
738
788
781
839
834
905
887
970
7000
920
992
982
1069
1043
1146
1120
1249
1198
1352
7000
774
826
824
887
874
948
936
1027
998
1106
8000
1016
1103
1087
1194
1158
1284
1246
1406
1334
1527
8000
852
915
909
986
966
1056
1038
1149
1109
1241
7300
61
74
0
541
589
558
604
574
620
590
637
607
653
0
458
496
471
509
483
523
497
537
511
551
1000
577
625
594
642
612
659
635
684
658
710
1000
487
527
501
541
515
555
534
576
554
596
2000
612
661
631
680
650
699
680
732
710
766
2000
516
557
531
572
546
587
572
615
597
642
3000
655
703
675
724
695
746
736
794
777
842
3000
551
592
568
609
585
626
619
664
652
703
4000
697
746
719
769
740
793
792
855
843
918
4000
587
626
605
645
624
664
666
714
707
764
5000
746
797
782
839
818
881
876
952
933
1023
5000
628
668
658
702
689
735
735
792
780
848
6000
796
848
846
908
896
969
959
1049
1022
1129
6000
670
710
711
758
753
807
803
869
853
931
7000
887
954
947
1027
1006
1100
1079
1197
1153
1293
7000
745
794
793
852
841
910
900
984
959
1059
8000
979
1060
1047
1145
1115
1231
1200
1344
1284
1458
8000
821
879
875
946
929
1012
997
1100
1065
1187
CONDITIONS:
73
0
525
570
540
585
556
601
572
617
588
633
Flaps 20
Torque Set Per Figure 5-8
1000
559
605
576
622
592
638
615
663
637
687
1900 RPM
Dry, Grass Runway
2000
593
640
611
658
629
676
658
709
687
741
Intertial Separator - BYPASS
Zero Wind
3000
634
681
653
701
673
722
712
768
752
814
Cabin Heat - OFF
ASI Ground Roll x 1.4
4000
675
722
696
744
717
767
767
827
816
888
5000
723
771
758
811
792
852
847
920
902
988
6000
770
820
819
878
868
936
928
1013
988
1089
1 Short Field Takeoff Technique as specified in Section 4
7000
859
922
916
992
973
1062
1044
1154
1114
1247
2 Decrease distances 10% for each 11 knots headwind.
8000
948
1023
1013
1105
1078
1187
1159
1295
1240
1404
0
508
552
523
566
538
581
553
597
568
612
3 Ground roll figures include 15% penalty due to operation on dry, grass runway
1000
541
586
557
602
573
618
595
641
617
664
4 Ground roll & Total distance figures include 3% penalty for inertial separator in bypass
2000
574
619
591
637
608
654
636
685
665
716
5 For operations above 40C and below the temperature operating limitations,
3000
613
659
632
678
651
698
689
742
727
787
4000
653
698
673
720
694
741
741
799
789
857
5000
699
745
733
784
766
823
819
888
872
953
6000
745
792
792
848
839
904
897
977
955
1050
7000
831
890
885
957
940
1024
1008
1112
1076
1200
8000
916
987
978
1065
1041
1143
1119
1247
1196
1350
NOTES:
For operations with tailwinds up to 10 knots, increase distances by 10%
for each 2 knots
7600
40 C
multiply takeoff distances at 40C by 1.2
6 Ground Roll distances include ASL OM specified adjustment of +40%
Air Serv Limited Cruise Performance Charts For C208B with Cargo Pod Installed
Notes:
Page 25
From Section 5 Performance CESSNA MODEL 208B (675 SHP) Rev 23, Figure 5-17 Cruise Performance.
o
1. The highes torque shown for each temperature and RPM corresonds to the max allowable cruise power. Do not exceed this torque, 740 C ITT or 101.6% Ng, whichever occurs first.
2. The lowest torque shown for each temperature and RPM corresponds to the recommended torque setting for best range in zero wind conditions.
3. With the inertial separator in BY-PASS and the power set below the torque limit (1865 ft-lbs), decrease the max cruise torque by 100 ft-lbs. Do not exceed 740oC ITT.
Fuel flow for a given torque setting will increase 15 pph .
4. The propeller setting for cruise shall be 1750 RPM.
5. With the cabin heat on and power wet below the torque limit (1865ft-lbs). Decrease maximum cruise torque by 80 ft-lbs. Do not exceed 740oC ITT. Fuel flow for a given torque setting will be 7 pph
higher.
Altitude
Torque
Temp 'C ft-lbs
2000ft
4000ft
6000ft
8000ft
10000ft
12000ft
Fuel
Flow
PPH
KTAS
Torque
ft-lbs
Fuel
Flow
PPH
KTAS
Torque
ft-lbs
Fuel
Flow
PPH
KTAS
Torque
ft-lbs
Fuel
Flow
PPH
KTAS
Torque
ft-lbs
Fuel
Flow
PPH
KTAS
Torque
ft-lbs
Fuel
Flow
PPH
14000ft
KTAS
Torque
ft-lbs
Fuel
Flow
PPH
KTAS
45
1336
346
145
40
1457
362
151
1335
335
147
35
1573
362
151
1447
335
147
1326
324
149
30
1689
1500
1465
393
365
360
160
151
150
1558
1420
1355
365
341
335
157
151
151
1430
1380
338
330
154
151
1291
311
149
25
1800
1600
1465
369
409
378
163
163
155
1631
1460
1355
375
375
347
161
161
154
1531
1440
1604
338
353
338
156
158
154
1386
1393
320
325
154
152
1254
298
148
20
1910
1700
1465
424
391
356
166
158
148
1704
1500
1355
385
353
331
165
157
150
1632
1500
1360
367
346
325
162
156
149
1481
1325
1255
338
314
302
158
150
150
1342
1320
310
307
154
152
1207
284
147
1285
288
154
11552
269
143
1362
1310
306
298
156
153
1225
280
149
15
10
5
1940
384
156
1837
357
156
1730
345
156
1572
332
162
1426
315
160
1700
427
167
1600
405
168
1550
382
166
1413
351
162
1360
288
150
1458
390
158
1380
367
159
1360
352
158
1290
326
154
1970
1700
1450
430
388
351
167
157
146
1970
1700
1405
425
381
336
170
160
147
1828
1600
1360
396
358
322
169
159
148
1663
1500
1325
364
338
310
165
158
149
1510
1400
1305
334
317
302
161
156
150
1970
388
157
1970
373
159
1899
357
159
1754
335
157
1594
335
166
1441
310
162
1299
283
157
1700
429
166
1700
424
169
1650
409
171
1600
380
168
1450
315
159
1355
279
150
1190
273
153
164
157
151
1372
1295
304
283
158
153
1443
387
156
1398
379
159
1360
363
161
1328
344
159
1300
285
149
0
1970
1700
1435
427
385
345
165
155
144
1970
1700
1390
422
376
331
168
158
145
1970
1700
1360
421
367
319
172
162
146
1844
1700
1330
396
350
308
171
160
148
1678
1500
1295
364
330
298
168
159
148
1520
1400
1295
333
310
293
-5
1970
385
155
1970
377
158
1970
364
161
1907
343
158
1763
307
154
1598
155
78
1444
456
238
1700
425
164
1700
421
168
1700
420
171
1600
407
173
1500
379
171
1400
347
167
1348
317
162
1430
384
154
1385
376
158
1345
366
161
1323
341
157
1295
329
159
1288
310
156
1290
304
159
Rev: Original
06 Nov 2014
Air Serv Limited
WT
LBS
9000
Ldg Speed
V50
80
C-208B Payload Extender Landing Performance Chart (Distances in Meters)
20 C
25 C
30 C
35 C
40 C
Press
Alt Gd Roll 50 ft Gd Roll 50 ft Gd Roll 50 ft Gd Roll 50 ft Gd Roll 50 ft
0
604
806
616
817
629
828
636
838
644
848
1000
625
829
638
840
650
850
660
861
670
872
2000
647
852
659
862
671
872
683
884
696
896
3000
673
874
683
884
694
895
707
908
720
921
4000
699
896
708
907
717
917
731
932
744
946
5000
723
922
735
934
746
946
759
959
772
972
6000
748
948
761
961
775
974
787
986
799
998
7000
780
980
792
991
804
1002
818
1016
831
1030
8000
812
1011
822
1021
833
1031
848
1046
863
1061
WT
LBS
8500
Ldg Speed
V50
78
Rev: Original 06 Nov 2014
Page 26
20 C
25 C
35 C
Press
30 C
40 C
Alt Gd Roll 50 ft Gd Roll 50 ft Gd Roll 50 ft Gd Roll 50 ft Gd Roll 50 ft
0
567
769
578
779
589
789
598
799
607
809
1000
589
791
600
801
610
811
620
821
630
831
2000
610
813
621
823
632
833
642
843
653
854
3000
635
836
645
846
656
856
667
868
677
879
4000
659
859
670
870
680
880
691
892
702
904
5000
683
884
695
895
706
907
718
919
729
931
6000
708
909
720
921
732
933
744
945
757
957
7000
737
937
749
949
761
961
774
974
787
986
8000
766
965
778
977
790
989
804
1002
818
1016
8900
80
0
1000
2000
3000
4000
5000
6000
7000
8000
597
618
639
665
691
715
739
771
803
799
822
844
866
889
914
940
971
1002
608
630
652
676
701
727
753
783
814
810
832
854
877
900
926
953
983
1012
620
642
664
687
710
738
766
795
824
820
842
864
887
911
938
966
995
1023
628
652
676
699
723
751
779
809
839
830
853
876
900
924
951
978
1008
1037
636
662
687
712
736
763
791
822
854
840
864
888
913
938
964
990
1021
1052
8400
77
0
1000
2000
3000
4000
5000
6000
7000
8000
561
582
603
627
651
676
700
728
757
762
784
805
828
851
876
901
929
957
571
592
614
638
662
687
712
740
769
772
794
815
839
862
887
913
941
969
582
603
624
648
672
698
724
752
781
782
804
825
849
873
899
924
953
981
591
613
635
659
683
710
736
765
794
792
814
836
860
884
910
936
965
994
600
622
645
669
694
721
748
778
808
801
824
846
871
896
922
948
977
1006
8800
79
0
1000
2000
3000
4000
5000
6000
7000
8000
589
611
632
658
684
707
730
762
794
792
814
836
859
882
907
932
962
992
600
622
644
669
693
719
744
775
805
802
824
846
869
893
919
945
974
1004
611
634
657
679
702
730
758
787
816
812
834
856
880
904
931
958
987
1015
620
644
668
691
715
742
770
800
830
822
845
868
892
917
944
970
1000
1029
629
654
679
703
727
755
782
813
844
832
856
880
905
930
956
982
1012
1042
8300
77
0
1000
2000
3000
4000
5000
6000
7000
8000
554
575
596
619
643
668
692
720
748
755
777
798
821
844
868
893
921
948
564
585
606
630
654
679
704
732
760
765
787
808
831
854
879
905
932
960
574
596
617
641
665
690
715
744
772
775
796
818
841
865
890
916
944
972
583
605
627
651
675
701
727
756
785
784
806
828
852
876
902
928
956
985
593
615
637
661
686
713
740
769
798
794
816
839
863
888
914
940
969
997
8700
79
0
1000
2000
3000
4000
5000
6000
7000
8000
586
607
629
654
680
703
726
758
790
789
811
833
855
878
903
928
958
987
596
619
641
665
690
715
740
770
801
799
821
842
866
889
915
941
970
999
607
630
653
676
699
726
754
783
812
809
830
852
876
900
927
955
983
1011
616
640
664
687
711
738
766
796
825
818
841
864
889
913
940
967
995
1024
625
650
674
699
723
751
778
809
839
828
852
876
901
926
952
979
1008
1037
8200
76
0
1000
2000
3000
4000
5000
6000
7000
8000
547
568
588
612
635
660
684
711
738
748
770
791
814
836
861
885
912
939
557
578
599
622
646
671
695
723
751
758
779
800
824
847
872
897
924
951
567
588
610
633
657
682
707
735
763
768
789
810
834
857
882
908
936
963
576
598
619
643
667
693
719
747
776
777
799
821
844
868
894
920
948
976
585
607
629
654
678
704
731
760
788
786
809
831
855
880
906
932
960
988
8600
78
0
1000
2000
3000
4000
5000
6000
7000
8000
582
603
625
650
676
699
722
754
785
785
807
829
851
874
899
924
954
983
593
615
637
661
686
711
736
766
796
795
817
838
862
885
911
937
966
995
603
626
649
672
695
722
749
778
807
805
826
848
872
896
923
950
979
1007
613
636
659
683
707
734
762
791
821
814
837
860
884
909
936
962
991
1020
622
646
670
694
719
746
774
804
835
824
848
872
897
922
948
974
1004
1033
8100
76
0
1000
2000
3000
4000
5000
6000
7000
8000
541
561
581
604
627
652
676
703
729
741
762
783
806
829
853
877
904
931
550
571
592
615
638
663
687
714
741
751
772
793
816
839
864
889
916
943
560
581
602
625
649
673
698
726
754
761
782
803
826
849
874
900
927
955
569
590
612
636
659
685
710
738
766
770
791
813
837
860
886
912
939
967
578
600
621
646
670
696
722
751
779
779
801
823
847
871
897
924
951
979
Air Serv Limited
WT
LBS
8000
Ldg Speed
V50
75
C-208B Payload Extender Landing Performance Chart (Distances in Meters)
20 C
25 C
30 C
35 C
40 C
Press
Alt Gd Roll 50 ft Gd Roll 50 ft Gd Roll 50 ft Gd Roll 50 ft Gd Roll 50 ft
0
534
734
543
744
552
754
561
763
571
771
1000
554
755
564
765
574
775
583
784
592
793
2000
574
776
584
786
595
795
604
805
613
815
3000
596
799
607
809
618
818
628
829
638
839
4000
619
822
630
831
641
841
651
852
662
863
5000
644
846
654
856
665
866
677
878
688
889
6000
668
870
679
880
690
891
702
903
714
915
7000
694
896
706
907
717
919
729
931
741
943
8000
720
922
732
934
744
946
757
958
769
970
WT
LBS
7500
Ldg Speed
V50
73
Rev: Original 06 Nov 2014
Page 27
35 C
20 C
25 C
30 C
40 C
Press
Alt Gd Roll 50 ft Gd Roll 50 ft Gd Roll 50 ft Gd Roll 50 ft Gd Roll 50 ft
0
500
700
510
708
519
717
528
726
537
734
1000
520
719
529
728
539
738
548
746
557
755
2000
540
739
549
749
558
758
567
767
577
776
3000
560
759
570
770
580
780
589
789
598
799
4000
580
780
590
791
601
802
610
812
619
822
5000
603
803
613
814
624
825
634
835
644
846
6000
625
826
636
837
647
848
658
859
668
870
7000
650
851
661
862
673
874
684
885
696
896
8000
674
876
686
888
699
900
711
911
723
922
7900
75
0
1000
2000
3000
4000
5000
6000
7000
8000
527
547
567
589
611
636
660
685
711
727
748
768
791
813
837
861
887
913
536
557
577
600
622
646
670
697
723
737
758
778
801
823
848
872
898
925
546
567
588
610
633
657
681
708
735
747
767
788
811
833
858
883
910
937
555
576
597
620
643
668
693
720
748
755
776
798
821
844
869
894
921
948
564
585
606
630
654
679
705
732
760
764
786
807
831
855
880
906
933
960
7400
73
0
1000
2000
3000
4000
5000
6000
7000
8000
494
513
533
552
572
594
617
641
665
693
712
731
752
772
795
818
843
867
503
522
542
562
582
605
628
652
677
701
721
741
762
783
806
828
854
879
511
531
550
571
593
615
638
664
689
710
730
751
772
794
816
839
865
890
521
540
560
581
602
625
649
675
701
719
739
759
781
804
827
850
876
901
530
549
569
590
611
635
659
686
713
727
748
768
791
813
837
861
887
912
7800
74
0
1000
2000
3000
4000
5000
6000
7000
8000
521
540
560
582
603
627
651
676
702
720
741
761
783
805
829
852
878
904
530
550
570
592
614
638
662
688
714
730
750
771
793
815
839
863
889
916
539
560
580
603
625
649
672
699
726
739
760
781
803
826
850
874
901
928
548
569
589
612
635
659
684
711
738
748
769
790
813
836
861
885
912
939
557
578
599
622
645
670
696
723
751
757
778
799
823
846
872
897
924
951
7300
72
0
1000
2000
3000
4000
5000
6000
7000
8000
487
506
525
545
564
586
608
632
656
686
705
724
744
765
787
809
834
859
495
515
534
554
574
596
619
643
668
694
714
733
754
775
797
820
845
870
504
523
542
563
584
607
630
654
679
703
723
743
764
785
808
830
856
881
513
532
552
573
594
617
640
665
691
711
731
751
773
795
818
841
866
892
522
542
561
582
603
627
650
676
702
720
740
760
783
805
829
852
877
903
7700
74
0
1000
2000
3000
4000
5000
6000
7000
8000
514
534
553
575
596
619
643
668
693
714
734
754
775
797
820
843
869
894
523
543
563
585
606
630
653
679
705
723
743
763
785
807
831
854
880
906
532
553
573
595
617
640
664
690
717
732
753
773
795
818
841
865
892
918
541
562
582
604
627
651
675
702
729
741
761
782
805
828
852
877
903
930
550
571
591
614
636
661
686
714
741
749
770
792
815
838
863
888
914
941
7200
72
0
1000
2000
3000
4000
5000
6000
7000
8000
480
499
518
537
556
578
600
623
647
679
698
717
737
757
779
801
826
850
488
507
526
546
566
588
611
634
658
687
707
726
746
767
789
811
836
861
497
516
535
555
575
598
621
645
669
696
715
735
756
777
799
822
846
871
506
525
544
565
585
608
631
656
681
704
724
744
765
787
810
833
857
882
515
534
553
574
596
618
641
666
692
712
732
752
775
797
820
843
868
893
7600
73
0
1000
2000
3000
4000
5000
6000
7000
8000
507
527
547
567
588
611
634
659
683
707
726
746
767
788
812
835
860
885
516
536
556
577
598
621
645
670
696
715
736
756
778
799
822
846
871
897
525
546
566
587
609
632
655
682
708
724
745
766
788
810
833
856
883
909
535
555
575
597
618
642
666
693
720
733
754
775
797
820
844
868
894
920
544
564
584
606
628
653
677
705
732
742
763
784
807
830
854
879
905
931
7100
71
0
1000
2000
3000
4000
5000
6000
7000
8000
474
492
511
529
548
570
591
614
638
672
690
709
729
749
771
793
817
841
481
500
519
538
557
580
602
625
649
680
699
718
738
759
781
803
827
851
489
508
527
547
567
590
613
636
660
689
708
727
748
769
791
813
837
862
499
517
536
557
577
600
622
646
671
697
716
736
757
779
801
824
848
873
508
526
545
566
588
610
632
657
682
705
725
744
766
788
812
835
859
883
CONDITIONS:
Flaps 30°
Power Lever - BETA
Prop Lever - MAX
Max Braking
NOTES:
Dry, Grass Runway
Zero Wind
ASL Ground Roll and 50' Distance +30%
1 Short Field Landing Technique as specified in Section 4
2 Decrease distances 10% for each 11 knots headwind. For operations with tailwinds up to 10 knots, increase
distances by 10% for each 2 knots.
3 Ground roll figures include 40% penalty due to operation on dry, grass runway
4 For wet or slippery runways, multiple Landing Roll by 1.75 to calculate 115% distance requirement.
5 The total calculated ground roll lengths in this chart are increased 70% over Cessna performance fiugres from
POH Section 5.
Page 28
Intercept Procedures
Excerpt from Ugandan Civil Aviation (Rules of the Air and Air Traffic Control) Regulations 2006.
40. (1) When intercepted by a military or government aircraft, the PIC shall comply with, by interpreting and responding to visual signals as shown in Table 2. (2) The intercepting aircraft shall
interpret visual signals from an intercepted aircraft as shown in Table 3.
Table 2 - SIGNALS INITIATED BY INTERCEPTING AIRCRAFT
Meaning
INTERCEPTED
Aircraft Responds
Meaning
Series
INTERCEPTING Aircraft Signals
You have been intercepted
Follow me.
DAY or NIGHT - Rocking aircraft. Flashing
Navigational lights at irregular intervals and following.
Understood, will
comply.
1
DAY or NIGHT - Rocking aircraft and flashing navigational lights at irregular
intervals (and landing lights in the case of a helicopter) from a position slightly above
and ahead of, and normally to the left of, the intercepted aircraft (or to the right if the
intercepted aircraft is a helicopter) and, after acknowledgement, a slow level turn,
normally to the left, (or to the right in the case of a helicopter) on the desired
heading.
Note 1
Meteorological conditions or terrain may require the intercepting aircraft to reverse
the positions and direction of turn given above in Series 1.
Note 2
If the intercepted aircraft is not able to keep pace with the intercepting aircraft, the
latter is expected to fly a series of race-track patterns and to rock
the aircraft each time it passes the intercepted aircraft.
DAY or NIGHT - An abrupt break-away maneuver from the intercepted aircraft
consisting of a climbing turn of 90 degrees or more without crossing the line of flight
of the intercepted aircraft.
You may proceed.
DAY or NIGHT - Rocking the aircraft.
Understood, Will
comply.
DAY or NIGHT - Lowering landing gear (if fitted), showing steady landing lights and
overflying runway in use or, if the intercepted aircraft is a helicopter, overflying the
helicopter landing area. In the case of helicopters, the intercepting helicopter makes
a landing approach, coming to hover near to the landing area.
Land at This aerodrome.
DAY or NIGHT - Lowering landing gear (if fitted), showing
steady landing lights and following the intercepting aircraft
and, if, after overflying the runway in use or helicopter
landing area, landing is considered safe, proceeding to
land.
Understood, will
comply.
DAY or NIGHT - Raising landing gear (if fitted) and flashing landing lights while
passing over runway in use or helicopter landing area at a height exceeding 300 m
(1,000 ft) but not exceeding 600 m (2,000 ft) (in the case of a helicopter, at a height
exceeding 50 m (170 ft) but not exceeding 100 m (330 ft) above the aerodrome
level, and continuing to circle runway in use or helicopter landing area. If unable to
flash landing lights, flash any other lights available.
Aerodrome you have
designated is inadequate.
DAY or NIGHT - If it is desired that the intercepted
aircraft follow the intercepting aircraft to an alternate
aerodrome, the intercepting aircraft raises its landing gear
(if fitted) and uses he Series 1 signals prescribed for
intercepting aircraft. If it is decided to release the incepted
aircraft. The intercepting aircraft uses the Series 2 signals
prescribed for intercepting aircraft.
Understood, follow
DAY or NIGHT - Regular switching on and off of all available lights but in such a
manner as to be distinct from flashing lights.
Cannot comply
DAY or NIGHT - Use Series 2 signals prescribed for
intercepting aircraft.
Understood.
DAY or NIGHT - Irregular flashing of all available lights.
In distress
DAY or NIGHT - Use Series 2 signals prescribed for
intercepting aircraft.
Understood
2
3
Table 3 - SIGNALS INITIATED BY INTERCEPTED AIRCRAFT
4
5
6
Rev: Original
Date: 06-Nov-2014
C208B Quick Reference Handbook
C208B
Normal Checklist
Original
C208B
Normal Checklist
Original
Climb
Before Start
After Start
*External Inspection ......... Complete (C)
*Documents ....................... Checked (C)
*Cabin Ht FW Cutoff ......... Open (IN) (C)
*Fuel Firewall Cutoff ......... Open (IN) (C)
Annunciator Panel ................. Checked (C)
Flaps ................. Set___°,Indic,Verified (C)
Trims ........................................... 3 Set (C)
Avionics/TAWS/TCAS .................... Set (F)
Engine Instruments ................ Checked (F)
Trims ............................... Checked/Set (C)
Flaps ............................... Checked/Set (C)
Emergency Power Lever ......... Stowed (C)
PWR, PROP, FUEL Lever............. Set (C)
Bleed Air......................................... Off (C)
Radar ............................................. Off (C)
Inertial Separator ................... As Req’d (C)
Control Lock ......................... Removed (C)
Park Brake ..................................... Set (C)
Lights (FSB,NS,Position)................ Set (C)
Circuit Breakers..................... Checked (C)
Brakes ................................... Checked (B)
Flight Controls ........................ Checked (F)
Flight Instruments ........ Set/X-Checked (F)
Taxi/Recog Lights ..........................Off (C)
Altimeters ....................... 1013 Set L/R(C/F)
Before Take-Off
Cruise
*Autopilot ........................... Checked (C)
*Fuel Boost Pump ....... Norm/On/Off (C)
*Avionics Fan / Xtie ..... Checked/Off (C)
*Alt Static Source .................... Norm (C)
*Fire Extinguisher .............. Checked (C)
*Fire Warning ......................... Tested (C)
*Annunciator Panel Lights.... Tested (C)
*Annunciator Day/Night Switch ..Set (C)
*Standby Flaps ........................ Norm (C)
Seat, seat belt, shoulder harness .. SET(B)
Fuel Selectors ................................ On (C)
Passenger Briefing ............... Complete (C)
Chocks/ Tail Stand ............... Removed (C)
Beacon ........................................... On (C)
Battery Switch ............................... On (C)
Voltage ......................... >24V/Set Batt (C)
Door Light...................................... Off (C)
Fuel .................... Lbs Req’d. Lbs Indic (C)
Prop Area ................................... Clear (B)
Fuel Boost Pump ............................ On (C)
Taxi
Crew Briefing ..................... Complete (PF)
*Feather/Unfeather ............ Checked (C)
*Beta/Reverse .................... Checked (C)
*Over-speed Gov ............... Checked (C)
*Inertial Separator ............. Checked (C)
*Suction.............................. Checked (C)
*Standby Power ................. Checked (C)
*Voltmeter ...................Checked/Batt (C)
Entering the Active
Transponder .....................................Alt (F)
Strobes.......................................... .On (C)
Radar .................................... As Req’d (F)
Environmentals (Bleed/HEAT/FLTFANS/OFF)Set (F)
Stdby Power ....................................On (C)
Annunc Panel ................... As Indicated (C)
Fuel Condition Lever ............. High Idle (C)
Compass/Rwy Hdg .............. Checked (B)
Passengers ............................ Checked (F)
Transfer of Controls
Lights (when cleared for takeoff)........................................ On (C)
( * Denotes First-Flight Items)
Page 29
Inertial Separator .................. As Req’d (C)
Landing Lights ................... As Req’d (PM)
Power......................................... Set (PM)
Flaps ........................................... Up (PM)
Annunciator Panel ........... Considered (PM)
Engine Instruments .............. Checked (PM)
Environmentals ................... .As Req’d (PM)
Transition Altitude
After Landing
Flaps ......................................... Set (F)
Radar ......................................... Off (F)
Transponder (clear of active) ................ Standby (F)
Lights ......................................... Set (C)
Ignition Switch ....................... Norm (C)
Stdby Power .............................. Off (C)
Fuel Cond Lever ........................ Set (C)
Shut Down
Cruise Power ................................ Set (PF)
Engine Instruments .............. Checked (PM)
Fuel Selectors ...................... As Req’d (PM)
*Trend Monitor ........................Complete (PM)
Descent
Seat, seat belt, shoulder harness ............. Set(B)
Cabin Signs/FSB/NS...............................On
App & Landing Data .......... .Reviewed (PF)
Navaids ........................... Set/Tune/ID (PM)
Fuel Selectors ..................... As ReQ’d (PM)
Transition Level
Taxi/Recog Lights .........................On (C)
Altimeters ........................... ____Set L/R (B)
TAWS .................................. As Req’d (PM)
Power Lever ............................ Idle (C)
Park Brake ............................... Set (C)
Avionics ................................... Off (C)
Standby Power ........................ Off (C)
Fuel Boost Pump ..................... Off (C)
Lights ....................................... Off (C)
Environmentals ........................ Off (C)
ITT ....................................... Stable (C)
Prop Lever .......................... Feather (C)
Fuel Condition Lever .......... Cut Off (C)
Fuel Selectors........................... Off (C)
Battery Switch........................... Off (C)
Control Lock .......................... Install (C)
Post Flight Duties .............Assigned (C)
Before Landing
Brakes.................................... Checked (B)
Bleed Air .............................. As Req’d (PM)
Radar ................................... As Req’d (PM)
Fuel Selectors .................... Qty/Bal/On(PM)
Passengers .................. Seated/Secured (PM)
Ignition ....................................... On (PM)
Inertial Separator .............. As Req’d (PM)
Flaps .............. Set__° / Ind / Vref____ (PM)
Prop ...................................... Full Fwd (PM)
Landing Lights ................................On (C)
Revision: .............................. ...Original
Date Revised: ...........................6-Nov-2014
Page 30
DEPARTURE BRIEF
IFR ARRIVAL BRIEF
Runway
Departing RWY
Initial Turn (L/ R)
Initial Course
Initial Altitude
Emergency Landing Plan
Chart
Name
Approach Chart Number
Jeppesen Briefing Strip
Minimums Vis Requirements (If A Factor)
Missed Approach Initial Actions
Terrain
Relevant Terrain And Obstacles
Minimum Safe IFR Altitude
Weather –
Relevant Weather
Wind – Wind/ X Wind/ Tailwind
Terrain
Relevant MSA And Highest MSA
Relevant Terrain And Obstacles
Weather
Relevant Weather
Wind – Wind/ X Wind/ Tailwind
Operational
Type Of Takeoff (If Non Standard)
Weight Restrictions (If Applicable)
Any Other Non Standard Items
Operational
Notams
Chart Notes And Warnings
Lateral Management
Vertical Management
Speed Control Configuration
Braking, Use Of Beta/ Reverse
Diversion Plan, Holding Time
Non Standard Items
THREATS
VFR ARRIVAL BRIEF
Runway –
Expected, Inspection/
Joining Procedure
Terrain –
Relevant Terrain And Obstacles
Weather –
Relevant Weather
Wind – Wind/ X Wind/ Tailwind
Operational
Notams
Type Of Landing (If Non Standard)
Speed Control
Configuration
Braking/ Use Of Beta Reverse
Any Other Non Standard Items
(Key Points, Slope, Specific Rwy
Characteristics)
THREATS
Rev: Original
Date: 06-Nov-2014
THREATS
Setup
1. Gps/ Vnav Setup
2. Nav Radio Setup
3. PM Crosscheck
4. Briefing
C208B Quick Reference Handbook
Rev: Original
06-Nov-2014
Rev: Original
06-Nov-2014
Rev: Original
06-Nov-2014
Rev: Original
06-Nov-2014
Rev: Original
06-Nov-2014
Rev: Original
06-Nov-2014
Page
C208B ANNUNCIATOR PANEL
ENGINE
FIRE
Ground – 10C
Flight – 9A
VOLTAGE
LOW
13B
Rev: Original
12A
VACUUM
LOW
15C
DOOR
WARNING
14C/D
OIL PRESS
LOW
-------------------
N/A
Date: 06-Nov-2014
GENERATOR
OFF
13B
RESERVOIR
FUEL LOW
12C
BATTERY
OVERHEAT
13A
EMERGENCY
POWER LEVER
AUX FUEL
PUMP ON
FUEL PRESS
LOW
17D
STARTER
ENERGIZED
12B
17D
LEFT FUEL
LOW
RIGHT FUEL
LOW
12E
12E
BATTERY
HOT
CHIP
DETECTOR
STBY ELEC
PWR INOP
WINDSHIELD
ANTI-ICE
19A
17C
13C
20A
STBY ELEC
PWR ON
19C
-------------------
13B
IGNITION
ON
20A
FUEL
SELECT OFF
12D/12E
C208B Quick Reference Handbook
DE-ICE
PRESSURE
20A
37