Cessna 210/T210/P210
WeekendCessna 210 TrainingCessna P210 Training
Cessna T210 Training
Flight Level Aviation is pleased to
offer periodic Cessna 210 Weekends conducted in a group format
designed to take you beyond just the normal procedures found in your
Cessna POH. The group format includes individual flight
instruction but also allows you to meet and discuss Cessna
210/T210/P210 operation with other owners.
The two day group program is
taught periodically and consists of time in Flight Level
Aviation's full motion flight simulator as well flight training in
your own Cessna 210/T210/P210.
Flight training will be conducted
out of KWAY. If weather conditions are not VFR (KWAY does not have
an instrument approach as of yet),
KMGW
can be used as an alternate location for arrival and flight
training. KMGW is just a 30 minute drive from KWAY (Flight Level
Aviation will provide transportation to and from KMGW if that
becomes necessary).
The flight training will be conducted by Dr. Richard Kaplan,
owner of Flight Level Aviation. Dr. Kaplan is a NAFI Master CFI,
certificated instrument flight instructor (CFII), aviation medical
examiner, and aviation safety counselor. An experienced
simulator instructor will also be available
The course will be conducted over a Saturday-Sunday period with 4
pilots and 2 instructors. The pilots will train in pairs,
alternating between airplane instruction with Richard and simulator
instruction with a second instructor. Time not spent flying
the simulator or airplane will be spent observing the other student.
Additionally Richard will include ground time in a group setting
reviewing the Cessna 210/T210/P210 accident history, operational
procedures, maintenance considerations, and other topics of interest
to pilots.
Training will be conducted 8AM to
5PM Saturday and Sunday in pairs as above. The group will also go
out to dinner at a local restaurant Saturday evening, followed by an
evening roundtable discussion lead by Richard covering pertinent but
difficult or controversial topics relevant to the 210/T210/P210
(i.e. lean of peak operation, maintenance decisions, major upgrade
considerations, gear-up/gear-down timing). If weather does not permit sufficient
airplane time, then additional ground and simulator time will be
provided by Richard.
This two-day program must be
scheduled in advance. Send an e-mail to
rkaplan@flyimc.com if you
have any questions about this new program or would like to set up a
training schedule.
The cost of this unique program is $595 per pilot and includes
simulator, ground and flight training.
If your own airplane is not available for this weekend, you may
drive or fly on the airlines and then rent Flight Level Aviation's
Cessna P210N for $125/hour wet (dual instruction only) in addition
to the $595 weekend course fee.
The program price does not include food, lodging, car rental or
parking/landing fees. Two to four students will be accommodated
during this two-day program.
About Richard Kaplan CFII/MCFI/AME/ASC
Flight
Level Aviation, Inc. was founded by Richard S. Kaplan, an
FAA-certificated pilot for over 12 years who is also an
instrument flight instructor and FAA Aviation Safety
Counselor. Richard retains a very active
role in managing all operations of Flight Level Aviation,
and he personally instructs Flight Level Aviation's advanced
single-engine IFR students and P210/T210/210-specific
training. In addition to extensive experience in the
Cessna 210/T210/P210 series, Richard has experience flying
the Mooney M20C, various Bonanza models, and most Cessna and
Piper single-engine aircraft. Richard also holds a
B.S. Degree in Engineering Science.
Richard frequently flies
Flight Level Aviation’s Cessna P210 on practical
cross-country flight, like many single-engine instrument
pilots. You will have the ability to learn about
single-pilot single-engine piston instrument flight
first-hand from an experienced peer who regularly flies
practical missions in this aircraft type.
Richard has a history of over a decade of accident-free
practical cross-country instrument flight with his family.
This makes Richard particularly qualified to offer Cessna
210/T210/P210-specific training and single-engine recurrent
IFR training so that single-engine IFR pilots can learn from
an instructor who regularly flies mission profiles similar
to theirs.
Richard is also an aviation
medical examiner and conducts flight physicals as part of
his medical practice (Uniontown Medical Rehab PC); his
extensive experience in both aviation and medicine is
particularly helpful in teaching pressurized Cessna P210
pilots about the medical and aviation factors related to
single-engine pressurized aircraft operation.
More than anything else,
you will no doubt recognize Richard’s high level of
enthusiasm for single-engine general aviation IFR flight and
the energy with which he approaches flight instruction. Many
of Richard’s students have become long-term friends and
email pen-pals (see
Student Feedback) – If you email an aviation question to
Richard at night, you might even get a reply back the same
night at 1AM!
As of August 2003, Richard is proud to have been designated
as a
Master CFI by the National Association of Flight
Instructors.
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Cessna 210/T210/P210
Training Checklist
Cessna 210/T21/P210
training programs include use of a 210-specific
training checklist developed and continually modified
by Richard to cover important type-specific areas of
training in this airplane. This checklist will include
the following:
- Lowered risk of
water contamination of fuel with non-recessed fuel
caps
- Importance of
fueling aircraft “to the brim” in proper ground
attitude when planning cross-country flight
- Emergency
procedures for vapor lock (fuel pump on, switch
tanks)
- Caution against
use of fuel pump routinely for takeoff or cruise
- Full throttle
activates high setting of fuel pump (important if
engine failure occurs on takeoff)
- Operation of
interlock mechanism on pilot door (? Lock vs .
Unlock safety lock)
- Procedures if
emergency exit opens in flight (expect buffeting,
opening openable window may reduce this)
-
Preflight/Pre-purchase to include check of
horizontal stabilizer noseribs and implications for
ground handling (powered tug recommended)
- Location of
hydraulic fluid reservoir (check each 25 hours)
- Location of 5 fuel
sumps during preflight
- Preflight
inspection of propeller spinner (slightly loose/low)
and propeller blades (no looseness permitted)
- Emphasize proper
leaning and cylinder/TIT temperature monitoring
procedures
- Limiting factor
for summer climbs = Cylinder head temps
- Limiting factor
for leaning = TIT temperature
- Altered power
settings for intercooler-equipped aircraft
- Emergency gear
extension procedure
- Emergency descent
procedure for decompression at high altitude
- High altitude
physiology factors, esp. re: exponentially increased
risks above 18,000 feet
-
Inspection/Replacement of oxygen generator
- Flight planning
for climb/descent distances for high altitude flight
- ATC factors for
high-altitude flight (ATC often unfamiliar with
relatively low P210 climb/descent rates for a
flight-level-flown aircraft)
- Physiology of
moving pressurization controls in-flight
- Pressurization
system = Electric+Pneumatic+Mechnical and
implications for emergency operations
- Implications of
cabin pressurization differential in marginally high
range (aircraft has reverted to backup outflow
system)
- Location of
pressurization bulkhead
- Locations which
can block pressurization outflow valves
- Go-Around
procedure (timing of gear up?, not specified in POH)
- Switching fuel
tanks consistently enroute (50 lb. max imbalance for
factory autopilot) -- by time or fuel flow?
- *** Electric Trim
= Most Dangerous part of aircraft ***à Runaway trim
can be unrecoverable if undetected, Extreme control
forces can occur by attempting to manually control
pitch when autopilot is engaged, Need to memorize
location of electric trim circuit breaker
- Maximum altitude
loss during autopilot malfunction à Implications for
autopilot-coupled approaches
- Need for autopilot
disengage check as part of pre-flight/runup
- Need to memorize
location of gear motor circuit breaker in event pump
stays on after takeoff
- Procedures to
verify gear-down (visually, gear-down light/switch
bulbs, audible warning/retard throttle) (Recommend
add-on mirror to verify nosegear is down)
- Procedures for
landing gear-up if necessary
- Potential high
sink-rate on final with no power vs. long rollout if
final flown with power on
- Cessna Pilots
Association vs. Lycoming recommendations/Aircraft
placard for leaning procedures (operate lean of peak
vs. rich of peak?, GAMIjectors?)
- Implications of
operating prop heat if ammeter does not respond
appropriately (potential asymmetric prop icing)
- Competing theories
of de-ice boot operation/timing
- De-Ice vs.
Known-Ice, icing procedures in POH
- Warning signs of
induction icing
- Cowl flap
operation (keep open in summer esp. if digital
engine probe not available?)
- “Critical vacuum
pump” for dual-vacuum pump aircraft with boots
- *** Accident
History à Dual vacuum pumps and/or dual
vacuum/electric attitude indicators seem essential
- Max Takeoff Weight
vs. Max Landing Weight
- Critical circuit
breakers – Gear motor, electric trim, autopilot
- Methods to
deactivate autopilot (intentionally and
unintentionally)
- Never manually
overpower autopilot in pitch!
- Note and observe
altitude guideline for maximum altitude loss if
autopilot malfunctions
- Autopilot
preflight techniques (multiple axis)
- Max gear operating
speed
- Max gear-down
speed = Never exceed speeds (facilitates emergency
descent esp. after depressurization)
- Max speed for 10
degrees flaps, full flaps
- Max takeoff power
= 5 minutes
- Caution against
overboosting turbocharger, esp. in winter
- Hot starting
procedure
- Presence/Use of
manual fuel primer (and importance to check as part
of preflight inspection)
- Timing of gear-up
decision and related safety factors
- Cabin altitude
light illumination implications
- Use of alternate
static source
- Location of
tie-down rings
- Location of fuel
vents (check during preflight)
- Potential for
filliform corrosion on original foam-filled trim tab
- Use of rudder trim
in takeoff vs. cruise and implications for fuel
spray from fuel vents
- Ice light
location/use
- Availability of
CPA Cessna 210 Systems/Procedures Course
- Check for
operation of avionics fan during preflight (No-Go
Item)
- Operation of cabin
ventilation fan for passenger comfort
- Use of rudder trim
essential for proper autopilot navigation
- Heater/Defroster
interlock to prevent damage to windshield
- ** Caution against
ground operation with significant power esp. in
vicinity of stones; marginal soft-field abilities of
this aircraft
- Location of Squat
Switch
- Nose strut
inflation technique (Nitrogen)
- Proper Intercooler
operation (altered power settings, caution operating
unintentionally at too high a power setting) (See
article)
- Intercooled
aircraft typically set for takeoff fuel flow above
redline (for adequate fuel flow at higher altitudes)
- Typical target TIT
<1500, CHT < 400, Oil temp < 200
- Competing theories
of boot operation timing (See article)
- *** Importance of
replacing original factory fuel caps to minimize
water entry in tanks
- *** Pre-flight
inspection to check for damaged noseribs on
horizontal stabilizer
- Caution high power
or taxiing over stones/gravel/soft fields during
ground operations
- Continental
TopCare program for engine trend monitoring
- Importance of
engine baffling/oil cooler to engine life
- Alternate points
of view re: leaning engine on ground
- Turbocharger
theory and critical altitude check procedure
- Consider 2
weight/balance lists (with 6th seat installed vs.
removed)
- Location of
autopilot computer (often under rear seats)
- How to identify
turbocharger failure on engine runup
- Failure modes with
double alternator failure (i.e. master switch
solenoid) --> Suggest Battery-powered backup GPS
- Varied trim
settings based upon aircraft loadings
- Oil filler cap gasket as a
critical preflight item
- Need to carry high-altitude
enroute charts for flight at and above FL180
- Potential altitude-related
failure mode of fuel controller
- Need to include fuel flow in scan
on takeoff run (186 lbs./hr), implications on engine
operation and pilot reactions to low vs. high fuel
flow
- Failure modes with dual vacuum
pump, including need to inspect/replace vacuum
manifold periodically
- Potential sources pressurization
leaks, including common (emergency door or windows)
and uncommon (gear boots leading to pressurization
leak only when gear up)
- Do not be alarmed at
pressurization "whistles"
- Limitations/Comparisons of Cessna
Standby Generator vs. B&C Alternator vs.
TurboAlternator
- Operating
considerations/limitations for Speed Brake and/or
STOL equipped airplanes
- Operating
considerations/limitations for airplanes with
wing-tip and/or baggage compartment fuel tanks
- Emergency gear procedures with
vs. without gear doors, i.e. turning off master
switch can open solenoid
- Pilot and Maintenance procedures
to address temperature-depenent variance in fuel
flow on takeoff
- Identification/implications on
boot operations of weak but operative primary vacuum
pump
- Implications of asymmetric prop
icing with partial prop heat failure
- Operation of 2 door interlocks
both inside and outside cabin
- Operational cautions vs.
usefulness operating with pressurization set to sea
level in winter
- Door mechanism operation to seal
fully when plane is left in rain
- Minimum airspeed for operation in
icing conditions
- Landing procedures after
encountering icing conditions
- Minimum airspeed in icing
condition climb
- Hot start procedures
- Operating procedures at high
density altitude airports
- Pros/cons of leaning for taxi
- Turbocharger cooldown procedures
- Flight profiles to avoid shock
cooling
- Comparative risk of decompression
in a single-engine piston airplane vs. multi-engine
turboprop/jet
- Consider 20-minute emergency
oxygen system for flight above Fl190 in P210
- Consider carrying Afrin onboard
for depressurization medical incidents
- High altitude engine performance
including "bootstrapping"
- Recent P210 inflight breakup an
potential causes/preventive techniques
- Potential engine failure from
loss of upper air deck hose and corrective action
(boost pump on)
- Seasonal variations in engine
operating procedures
- Varying thoughts on takeoff fuel
flow, i.e. redline vs. over redline
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