Cessna 182S 182T, T182T Skylane Systems & Procedures Course

%ase Price 1on-turEo 4,500 7urEo 7,500 *ross weight 110 lEs. raPp non-7urEo 112 lEs. 7urEo/ 100 lEs. 7aNeo൵ 7otal %uilt - 1827 - 26 71827 - 2 *6WDQGDUG(TXLSPHQW 2SWLRQVLQFOXGH7$:6%7HUUDLQ *DUPLQ 7$67UD൶F %HQGL[.LQJ .7$    $') .5 ,QW¶O RQO\  '0( .1  ,QW¶O RQO\  $UWH[ &1)UHTXHQF\(/7 H[FKDQJHLQW¶ORQO\ $LUFRQGLWLRQLQJ .HLWK EWXK(QJLQH'ULYHQ  2008 - 1827 71827 Serial 1uPEers 18282046 to 18282145 718208807 to 71820808 %ase Price 1on-turEo 67,000 7urEo 7,500 *ross weight 110 lEs. raPp non-7urEo 112 lEs. 7urEo/ 100 lEs. 7aNeo൵ 7otal %uilt 1827 -  71827 - 101 *6WDQGDUG(TXLSPHQW 2SWLRQVUHPDLQWKHVDPH FRORURSWLRQVIRUSDLQWVFKHPHV 200 - 1827 71827 Serial 1uPEers 18282146 to 18282204 7182080 to 718208 %ase Price 1on-turEo 84,500 7urEo 418,000 *ross weight 110 lEs. raPp non-7urEo 112 lEs. 7urEo/ 100 lEs. 7aNeo൵ 7otal %uilt 1827 - 58 71827 - 84 *6WDQGDUG(TXLSPHQW 2SWLRQVUHPDLQWKHVDPH $OOVHDWVLQFOXGH$PVDIHLQÀDWDEOHUHVWUDLQWV ©Cessna Pilots Association - April 27, 2022 5HVWDUW+LVWRU\SDJH 2010 - 1827 71827 Serial 1uPEers 18282205 to 18282276 718204 to 7182001 %ase Price 1827 0,00 71827 424,00 *ross weight 110 lEs. raPp non-7urEo 112 lEs. 7urEo/ 100 lEs. 7aNeo൵ 7otal %uilt 1827 - 71 71827 - 75 *6WDQGDUG(TXLSPHQW 2SWLRQV5HPDLQWKH6DPH $OO6HDWVLQFOXGH$PVDIH5HVWUDLQWV 2011 - 1827 71827 Serial 1uPEers 18282277 to 1828211 7182001 to 71820055 %ase Price 1827 8,100 71827 42,800 7otal %uilt 1827 - 4 71827 - 6 2012 - 1827 71827 Serial 1uPEers 1828212 to 1828258 71820056 to 71820068 %ase Price 1827 8,100 71827 44,500 7otal %uilt 1827 - 46 71827 - 12 201 1827 71827 Serial 1uPEers 182825 to 1828268 7182006 to 71820100 Cessna no longer o൵ered the 71827 aIter 201. It was dropped in Iavor oI the ³soon to coPe´ diesel -1827. As oI August, 2015 it appears that Cessna has dropped the -1827 proMect with no planes certi¿ed or delivered. 2015 1827 Serial 1uPEers 182826 to 18282418 %ase Price 450,000 7otal %uilt 4 2016 1827 Serial 1uPEers 1828241 - 18282467 %ase Price 470,000 7otal %uilt 48 2017 1827 Serial 1uPEers 1828001 to 1828027 %ase Price 470,000 7otal %uilt 26 2018 1827 Serial 1uPEers 182800 - 1828060 %ase Price 40,000 7otal %uilt 0 ©Cessna Pilots Association - April 27, 2022 5HVWDUW+LVWRU\SDJH 201 - 1827 Serial 1uPEers 1828062 through 182802 %ase Price 515,000 *ross weight 100 lEs 7otal Euilt - 0 2020- 1827 Serial 1uPEers 182804 - 1828120 *ross weight 100 lEs 7otal %uilt - 26 2021 - 1827 Serial nuPEers 1828121 - 182815 *ross weight 100 lEs 7otal %uilt - 2 Section Two 182S, 182T, T182T Skylane Airframe, Wings & Empennage Section Two FUSELAGE STATIONS WING STATIONS 209 & 230 BULKHEAD S Wing Reference Stations S2 2 CPA TECH NOTE #024 Jacking Details S2 3 SNL05-1 WING JACK PAD INSTALL CPA TECH NOTE #036 SNL 85-3R2 WINDSHIELD MAINTENANCE Windshield Installation S2 4 LOWER FORWARD DOORPOST AREA SB04-53-02R1 Lower Cowling Shock Mounts Fuselage Assembly S2 5 209 BULKHEAD 230 BULKHEAD CORROSION UNDER SOUND DEADENING PANELS SNL93-3 CABIN CORROSION SE73-38 CORROSION PREVENTION Legacy 182 Cabin Soundproofing S2 6 SEL-51-01 Use Of Corrosion Inhibiting Compounds LUBE DOOR AND WINDOW HINGES BROKEN SPRING TECH NOTE# 015 DOOR LOCKS Cabin Door S2 7 DOOR HINGE ARTICLE IN 8/04 CPA Mag SB02-52-01 PLASTIC DOOR HANDLES 182S Seat Belt/Shoulder Harness Installation S2 8 SB02-25-01 Shoulder Harness Guide Removal AD2007-05-10 SB04-25-01R2 SB04-25-02 SB04-25-04 SB07-25-01 SB07-25-02 AD2008-05-09 SB07-25-11 SB09-25-R01 Crew Seat Cylinder and Base Insp Seat Installation S2 9 Seat Rail S2 10 AMSAFE Inflatable Restraint System S2 11 SB05-25-01 Inflatable Seat Belt Check Installation SB05-25-02 Inflatable Seat Belt For All Seats SB10-25-01 Inflatable Seat Belt Connector Cover Wing Installation S2 12 WING ADJUST CAMS BROKEN DOOR STOP ALLOWS DOOR TO WEAR INTO STRUT ALT TAPE PART NUMBER 3M PROTECTIVE TAPE 8672 Wing Strut Installation S2 13 WEAR LIMITS ON STRUT CALLED OUT IN OCT 2006 CPA MAG ARTICLE Tail Cone Structure S2 14 230 BULKHEAD 209 BULKHEAD SB02-53-01 ADDS BALLAST WEIGHT TO 230 BULKHEAD 1-5 POUNDS CAN BE ADDED Tail Cone Structure S2 15 GLIDER TOW HOOK ATTACHES HERE NO PROBLEM WINCHING OFF THE TIEDOWN RING LUBE PIVOT POINTS CRACKS IN ATTACHMENT BOXES Nose Rib Security Horizontal Stabilizer Installation S2 16 LUBE Vertical Stabilizer Installation S2 17 QUESTIONS? S2 18 Section Three 182S, 182T, T182T Skylane Flight Controls Wing Flap Control System Flap Panels Pre-Select Flap Motor Follow Up Cable S3 2 Flap System Schematic S3 3 Wing Flap Control System Installation SB11-27-03 Flap Motor Housing Inspection Missing Nuts On Motor S3 4 Pre-Select Lever Flap Lever & Follow-up System Pre-Select Switches Follow Up Cable S3 5 Flap Lever & Follow-up System Aileron and Flap Cables Pass Through Cabin S3 6 Flap Installation Pre-Flight Inspection Items SB03-27-02 Bracket Attachment Screws Missing Buttons #11 S1093-1 Loose Attachment Hardware S3 7 Aileron Control System S3 8 Control Column SB00-27-02R1 Cable Quadrant Inspection SEB-27-01- R02 Glide Attach Screw S3 9 Aileron Control Surface Pre-Flight Inspection Items Hinges S3 10 Aileron Control Surface Pre-Flight Inspection Items Balance Weight Rivets S3 11 Pre-Flight Inspection items: #24 Actuator Rod Aileron bellcrank S3 12 SB00-27-01R1 Pulley Bracket Alignment Insp Elevator Control System S3 13 Elevator Trim Tab Pre-Flight Inspection Items: Security, Condition & Operation Differential Movement SSP03-27-01 Safety Wire Turnbuckles Elevator Bellcrank Installation SB00-55-01 Elevator Rivet Inspection SB04-27-01R1 Wrong Rivets Inside Elevator S3 14 Item B Trim Wheel Assembly Elevator Trim Tab Control System S3 15 F.S. 209 Bulkhead Actuator Elevator Trim Actuator Installation S3 16 Trim Tab Free Play Inspection S3 17 Rudder Pedal Installation Rudder Control Surface Rudder Control System S3 18 Bearing Blocks Rudder Pedal Installation Lube with LPS-1 S3 19 Rudder Trim Control Installation S3 20 Rudder Pedal Assembly Nose Strut - Steering Collar Rudder Trim Actuation Bungee Installation S3 21 11 Lube A, B & C with LPS-1 Rudder Installation Pre-Flight Inspection Items Security, Condition & Operation #11 Rudder Stop S3 22 Section Four 182S, 182T, T182T Skylane Landing Gear Nose Gear Installation S4 2 Strut Extension Axle Installation S4 3 Nose Gear Wheel and Tire Assembly S4 4 Cleveland Wheel 182S Nose Wheel Fairing 182T Nose Wheel Fairing S4 5 Castle Nut & Cotter Pin SEB03-4 FAIRING REPAIR KIT Nose Gear Shock Strut Assembly S4 6 Servicing the Nose Strut: SK172-1F Seal Kit MIL-H-5606 & Nitrogen HI-Pressure Air Valve “H” Evidence of External Hydraulic Fluid KEEP CLEAN Cracks in Steering Arm Assembly Nose Gear Shock Strut Assembly S4 7 SEB-32-02 Strut Tube Replacement Aluminum back to Steel-Orifice Piston Support 182S thru 182811997 182T thru T18208185 Use This Dampener As Original Equipment Shimmy Dampener S4 8 Torque Links S4 9 10 8 Hardware Spacers & Bushings Shim Accordingly Lubrication Torque Links S4 10 Max Nose Strut Extension 5 Inches Shims Added Turn Limits S4 11 16 Cracks in Steering Arm Assembly During Annual Insp: Attachment into Fuselage SB09-32-02 SEB-32-01 Brake line for Chafing Main Landing Gear Installation S4 12 Main Landing Gear Installation S4 13 USE 3M CHAFE TAPE p/n 8672 Strut Fairing Disc Linings > 3/32” = #40 drill bit Main Wheel Assembly S4 14 McCauley Wheel Shown 182T Use Cleveland Wheels 182S Main Landing Gear Fairing S4 15 182T Main Landing Gear Fairing S4 16 Nose Wheel Steering Brake Master Cylinder Installation S4 17 Left Bracket Bending and Cracking Brake Master Cylinders Servicing the Brake Reservoir: Vent Plug Mil-Spec 5606 ? Intermittent Braking? Brake Master Cylinder Assembly S4 18 Lock Spring 1/16” Cables Return Spring Operation Cracks at Notches In Rod Parking Brake Installation S4 19 Main Wheel Alignment Check S4 20 Section Five 182S, 182T, T182T Skylane Fuel Systems S5 2 Cessna Service information ICA-172-28-00001A dated 01/30/2009 Single Engine Restart Fuel Quantity Indication System ICA Supplement Revision This ICA contains a lot of nice to know information and details testing of the varies systems used on the new production models SSP08-28-01 Fuel Level Sensor Inspection dated 09/01/2008 Applies to 182T and T182T specific serial numbers but also has some nice to know information on the system. This service information is available from Cessna at their www.cessna/support .com web site. Article in the January 2012 CPA magazine details that web site. S5 3 182S Fuel System S5 4 182T & T182T Fuel System S5 5 182T, T182T G1000 Fuel System S5 6 182S Fuel System Installation SB02-28-01 R1 Hose Inspection- Bad Hoses SB11-28-02 Fuel Hose Inspection-Bad Hoses See Aft Line Drawing See Aft Line Drawing Fuel LEVEL SENSOR Fuel LEVEL SENSOR See Forward Fuel System Components Page 10 S5 7 182T&T182T Forward Fuel Line Installation SB02-28-01 R1 Hose Inspection- Bad Hoses SB11-28-02 Fuel Hose Inspection-Bad Hoses SEL-28-01 Suspect ½ inch Metal Fuel Lines 18282331-18282356, T18209078-T18209086 S5 8 182T & T182T Aft Fuel line Installation SB02-28-01 R1 Hose Inspection- Bad Hoses SB11-28-02 Fuel Hose Inspection-Bad Hoses SEL-28-01 Suspect ½ inch Metal Fuel Lines 18282331-18282356, T18209078-T18209086 S5 9 182T, T182T Forward Fuel System Components SEL-28-02 Belly Drain Fitting Inspection 18282350-18282360, T18209069-T18209086 SEL-28-01 Suspect ½ inch Metal Fuel Lines 18282331-18282356, T18209078-T18209086 S5 10 182S, 182T & T182T Fuel Drain Valve Installation S5 11 182S Electric Auxiliary Fuel Pump Overboard Drain Line S5 12 182S Fuel Selector Valve Installation S5 13 182T & T182T Fuel Selector Valve Installation Fuel Return Path Fuel Flow To Engine Path S5 14 Fuel Strainer Assembly INSPECT EVERY 100 HOUR/ ANNUAL INSPECTION S5 15 Wing Fuel Tank Vent Check Valve AIR ENTERS FAIRING AT GAP AT LOWER WING SKIN AIR EXITS HERE AND GENERATES VORTEX JUST FORWARD OF VENT TUBE Tech Note #003 Uneven Fuel Feed S5 16 Fuel Vent Location 182S 182T S5 17 182S & 182T Fuel Filler Cap GASKET p/n B100142-1 FRICTIONLES S WASHER p/n B100143 SEALPAK CO. SEALANT S5 18 Integral Fuel Bay Components S5 19 Classification of Fuel Leaks Section Six 182S, 182T, T182T Skylane Powerplant S6 2 Lycoming IO-540 used in 182S and 182T S6 3 Lycoming TIO-540 used in T182T TIO-540 AK1A O – OPPOSED ENGINE NOT A RADIAL ENGINE 540- CUBIC INCHES DISPLACEMENT T– TURBOCHARGED S6 4 BREAKDOWN OF ENGINE MODEL NUMBERS X-POWER SECTION AND RATING X- NOSE SECTION X-ACCESSORY SECTION X- COUNTERWEIGHT APPLICATION I– FUEL INJECTED IO-540 AB1A5 S6 5 SI1009AW TBO SUPERSEDED TO SI1009AY S6 6 SI1009AY CONDENSED 8 Pages Long Page 1 S6 7 SI1009AY CONDENSED Page 2 S6 8 SI1009AY CONDENSED Page 3 NOTES #2, #10, #11 S6 9 SI1009AY CONDENSED Page 4 NOTES #2, #10, #11 S6 10 SI1009AY CONDENSED Page 5 TBO EXTENSION NOTES #10, #11 S6 11 IO 540 Crankcase Assembly LYC SB 240 MANDATORY REPLACEMENT PARTS OIL PRESSURE RELIEF VALVE CAM FOLLOWERNow Roller Tappet S6 12 IO 540 Crankcase Assembly S6 13 Roller Tappets Roller Tappet SI1514A Roller Tappets “E” Suffix Added To Serial Number Camshaft Crankshaft AD 2002-20-51 S/S TO AD2002-23-06 S/S TO AD2004-05- 24 CHANGE CRANKSHAFT BOLT S6 14 Crankshaft & Camshaft AD2005-19-11 SEB05-3 AND LYCOMING SB566 NEW CRANKSHAFTS AFTER MARCH 1, 1999 CHECK CRANK S/N FOR COMPLIANCE AD2012-19-01 SS AD2006-20-09 LYC MSB569A REPLACE CRANKS MARCH 1,1997 TO JULY 11, 2005 12 YEAR COMPLIANCE S6 15 Crankshaft & Camshaft AD2004-10-14 S/S TO 2004-10-14 C1 DEFINITION OF PROP STRIKE LYC SB 533A PROP STRIKE AD2004-10-14 DEFINITION OF PROP STRIKE (1) Any incident, whether or not the engine is operating, that requires repair to the propeller other than minor dressing of the blades (2) Any incident during the engine operation in which the propeller impacts a solid object that causes a drop in revolutions per minute (RPM) and also requires structural repair of the propeller (incidents requiring only paint touch-up are not included). This is not restricted to propeller strikes against the ground. (3) A sudden RPM drop while impacting water, tall grass, or similar yielding medium, where propeller damage is not normally incurred. Camshaft Crankshaft S6 16 Crankshaft & Camshaft S6 17 Prop Governor Drive S6 18 182S, 182T, T182T IO- 540 Gear Train Diagram S6 19 Lubrication Schematic NORMAL OIL CONSUMPTION 1 QT IN 10-20 HRS. OIL PRESSURE MIN 20 PSI NORMAL 50-90 PSI MAX 115 PSI OIL PRESSURE ORIGINALLY TAKEN AT THIS POINT OIL PRESSURE NOW TAKEN AT THIS POINT S6 20 Oil Pressure Switch Replacement SB07-79-01 issued 1/29/2007 Replacement of oil pressure switch p/n 83278 every 3000 hours! SEL-05-03 issued 11/28/2012 Airworthiness Limitations added to Maintenance Manual –Chapter 4 Article In CPA Magazine Feb 2013 Numeric Gage Indication Warning Light Indication AD2013-11-11 Effective Date 08/01/2013Replacement Of Oil Pressure Switch Every 3000 Hours S6 21 Oil Level Gauge S6 22 IO-540 Accessory Housing Oil Pump #8 OIL TEMPERATURE CONTROL VALVE S6 23 IO-540 & TIO-540 Accessory Housing & Related Parts S6 24 Lycoming SI 1014M S6 25 SI 1014M page 2 S6 26 SI 1014M page 3 S6 27 Lycoming MSB 480E S6 28 MSB 480E page 2 Suction screen location S6 29 Oil Return S6 30 Inter-Cylinder Baffling S6 31 Cylinder Valve Train Lycoming SI1425A Valve Sticking Oil Pressure Should Be 80-90 PSI in Cruise- Normal Oil Temp Section Seven 182S, 182T, T182T Skylane Electrical Systems Electrical Schematic FLOODED CELL LEAD ACID BATT DOES NOT LIKE DEEP CYCLE 24V-28V THE SAME 15.5 AMP/HR REPLACE 2-4 YRS. DEPENDING ON A/C USAGE PROPER BATTERY MAINTENANCE CHECK FLUID LEVEL EVERY 4 MONTHS, SOONER IF BASED IN HOT CLIMATE Optional Prop Deice S7 2 Electrical Schematic BATTERY CONTACTOR HIGH CURRENT SWITCH GROUNDING CIRCUIT TO CLOSED POSITION. STARTER CONTACTOR INTERMITTMENT DUTY ALTERNATOR CONTACTOR S7 3 Electrical Schematic 60/95 AMPERE CURRENT LIMITED BY DESIGN MAJOR ADVANTAGE OF ALTERNATOR ABILITY TO PRODUCE RATED CURRENT AT LOWER ENGINE RPMs MAJOR DISADVANTAGE OF ALTERNATOR AC NOISE ON BUS S7 4 Electrical Schematic ALTERNATOR CONTROL UNIT VOLTAGE SETTING 28.0-28.5 OVERVOLTAGE SETTING 31.75±.0.5 ALTERNATOR FIELD BREAKER POPS WARNING ON 24.5 VOLTS G1000-BELOW 20 VOLTS SYSTEM SHUT DOWN S7 5 Electrical Schematic APU GPU Ground Service Contactor Must Close Master Switch G1000- BELOW 20 VOLTS SYSTEM SHUT DOWN S7 6 Electrical Schematic Master On Alternator Off Master On Alternator On S7 7 Electrical Schematic Power Junction Box J-BOX S7 8 SB00-24-01 Circuit Protection SB99-24-01 New ACU & Wiring 182S Power Junction Box Installation S/N 18280001 thru 18280675 S7 9 SB03-24-02 40A CB replaces 30A SB04-24-01 ACU Replacement AD2005-13-10 SB05-24-01 CB Replacement 182S Power Junction Box Starting with S/N 18280676 S7 10 182T Power Junction Box PUSH TO RESET AD2005-13-10 SB05-24-01 CB Replacement S7 11 Electrical Schematic PUSH TO RESET S7 12 182S, Electrical Schematic Only Allows Flow In One Direction With Arrow S7 13 182S, Electrical Schematic OVERVOLT AGE SETTING 31.75±.0.5 ALTERNAT OR FIELD BREAKER POPS S7 14 G1000-182T Electrical Schematic Only Allows Flow In One Direction With Arrow S7 15 G1000-182T Electrical Schematic OVERVOLTAGE SETTING 31.75±.0.5 ALTERNATOR FIELD BREAKER POPS S7 16 G1000-182T Electrical Schematic Standby Battery System BELOW 20 VOLTS SYSTEM SHUT DOWN S7 17 G1000- Standby Battery System Test Mode Master Off Preflight Check Operation LESS THAN ABOUT 20 VOLTS CONTROL CLOSES GREEN LIGHT ON SWITCH TO ARM MODE FOR ENGINE START S7 18 G1000-Standby Battery System Arm Mode Normal Flight Condition STANDBY BATTERY BEING CHARGED BY ALTERNATOR SYSTEM S7 19 G1000-Standby Battery Circuit Arm Mode Normal Flight Condition BELOW 20 VOLTS SYSTEM SHUT DOWN LESS THAN ABOUT 20 VOLTS CONTROL CLOSES S7 20 Alternator Installation SB03-24-01 Alternator Replacement due to excessive brush spring pressure, mfgd 5/2000 thru 12/2002. SB98-24-01 new alternator incorporating a new rotor designed to enhance alternator reliability. SB09-24-03 Alternator Ring Terminal Inspection/replacement S7 21 Detail A Stator Detail B Diodes Phase-1 Phase-2 Phase-3 Detail C Rotor Alternator Component Internal Relationship S7 22 One Winding One Winding Rectified Three Windings, Combined Output One Winding, Open Diode Combined Output, Shorted Diode Alternator Output S7 23 VR SET Alternator with Bad Diode S7 24 VR SET VOLTAGE SPIKE REGULATOR ON REGULATOR OFF Normal Alternator Output Tech Note #050 S7 25 182S, 182T, T182T Electrical Load Analysis -NOT G1000 S7 26 182T G1000 Electrical Load Analysis S7 27 182T G1000 Electrical Load Analysis S7 28 182T G1000 Electrical Load Analysis S7 29 182S, 182T,T182T Skylane Propeller Section Eight Dynamic Balancing of Propeller 1 3 4 2 Vibration Levels 0.4 IPS to 0.8 IPS ROUGH 0.2 IPS to 0.4 IPS MODERATELY ROUGH 0.1 IPS to 0.2 IPS FAIR 0.1 IPS and Below SMOOTH S8 2 Two-Blade Propeller and Spinner Installation SPINNER FITTED TO AFT BULKHEAD WITH .050 INCH HOLE MISALIGNMENT- SPINNER FORWARD OF REAR BULKHEAD- SHIMS ADDED TO CREATE THE .050 INCH HOLE MISALIGNMENT Spinner must be tight against the forward support S8 3 182S, 182T, T182T Three- Blade Propeller Installation SPINNER FITTED TO AFT BULKHEAD WITH .050 INCH HOLE MISALIGNMENT- SPINNER FORWARD OF REAR BULKHEAD- SHIMS ADDED TO CREATE THE .050 INCH HOLE MISALIGNMENT Spinner must be tight against the forward support S8 4 Field Inspection and Repair of Propeller Blades SNL93-9 S8 5 FACE OF BLADE PAINTED FLAT BLACK CAMBER SIDE LEADING EDGE TRAILIN G EDGE DRESSING PROP IS A&P FUNCTION!! Blade Repair S8 6 BLADE SHAKE- FOR AND AFT MOVEMENT BLADE TWIST- ROTATING MOVEMENT BLADE TRACKING 1/8 INCH MAX BLADE TWIST 1 DEGREE MAX DIFF BETWEEN BLADES Blade Preflight S8 7 Propeller Governor Control Installation S8 8 S8 9 Propeller Governor S8 10 Flyweight Force and Speeder Spring Force are Equal S8 11 Flyweight Force less Than Speeder Spring Force CLIMB Flyweight Force Greater Than Speeder Spring Force DESCENT S8 12 182S, 182T, T182T Skylane Powerplant Management Section Nine •AVOID STARTS •LEAN AGGRESSIVELY •THERMAL CYCLES •HIGH M/P & LOW RPM POWERPLANT MANAGEMENT S9 2 POWERPLANT MANAGEMENT COLD STARTS- LYC SI 1505 BELOW 10°F, CPA SAYS ANYTIME TEMPS ARE BELOW 40° F PRE-HEAT SYSTEMS, TANIS, REIFF, E-Z-HEAT, 100-WATT LIGHT BULBS TECH NOTE 032 DO NOT KEEP PRE-HEATER PLUGGED IN ALL THE TIME IF TEMPERATURE SWINGS FROM FREEZING TO ABOVE FREEZING DO NOT PULL PROP THRU IF NOT FLYING DO NOT RUN ENGINE FOR 20 MINUTES AND NOT FLY THE AIRPLANE ENGINE PRESERVATIVE OIL, AEROSHELL 2F AND PHILLIPS CORROSION PREVENTIVE OIL AVOID STARTS S9 3 POWERPLANT MANAGEMENT LEAN AGGRESSIVELY Lycoming Service Instruction SI1094D NO LEAN ABOVE 75% 75% LEAN TO 50 DEGREES RICH OF PEAK 65% LEAN TO PEAK REGARDLESS OF ALTITUDE MAX CHT 400°F- STOP BEFORE 500°F RED LINE CHTS 350°F TO 380°F IN CRUISE OT 180°F IN CRUISE ENGINE MONITORS LEAN FOR ALL GROUND TAXI OPERATIONS S9 4 Fuel Flow Relationship S9 5 POWERPLANT MANAGEMENT THERMAL CYCLES MINIMIZE HEAT UP AND COOL DOWN NO PART THROTTLE TAKEOFFS REDUCE POWER-- 2 INCHES 2 MINUTES USE COWL FLAPS TO CONTROL CHTS S9 6 POWERPLANT MANAGEMENT ANY POWER SETTING IN THE PERFORMANCE CHARTS IS AN APPROVED POWER SETTING ACCURACY OF TACHOMETER AND MANIFOLD PRESSURE GAUGE HIGH MP/LOW RPM S9 7 POWERPLANT MANAGEMENT HIGH MP/LOW RPM ANY POWER SETTING IN THE PERFORMANCE CHARTS IS AN APPROVED POWER SETTING ACCURACY OF TACHOMETER AND MANIFOLD PRESSURE GAUGE WHY OPERATE THE ENGINE OVERSQUARE? BECAUSE THE ENGINE LIKES IT!!!!! S9 8 182S Cruise Performance S9 9 182T Cruise Performance S9 10 T182T Cruise Performance S9 11 Friction Horsepower Loss S9 12 Brake Mean Effective Pressure S9 13 Ring Seating S9 14 FLY FREQUENTLY! And The Most Important S9 15 Tactical Data Analysis Identifying a problem before it identifies you Paul New Section Ten Cause and Effect S10 2 S10 3 A True 182T Story S10 4 Catastrophic cast aluminum failure An Inside Job S10 5 S10 6 Using Data in Real Time S10 7 • How/where to view and analyze data • What’s normal – establish baselines • Understand what the various engine parameters are • Distinguish indication issues from true failures • Find correlations between indications Data Acquisition S10 8 S10 9 Data Acquisition S10 10 Data Acquisition Savvy Analysis Free www.savvyanalysis.com free Savvy Analysis Pro www.savvyanalysis.com $129 Cirrus Reports www.cirrusreports.com free EGTrends www.egtrends.com $99 EZ Trends www.jpinstruments.com free S10 11 S10 12 Whether you own, rent or borrow the airplane you fly, in-flight problem solving is your job. Know Your Limitations S10 13 Max RPM? ___________ Max MAP? ___________ Max FF TIT max and normals CHT Max Oil Temp Red line Know Your Baselines S10 14 EGT at take off TIT normals in flight CHT in climb & cruise Oil pressure at 180 degrees Buss voltages S10 15 S10 16 Tires – just to make a point S10 17 Cylinder Arrangement - right side S10 18 EGT #1 EGT #3 EGT #5 TIT right CYL #5 CYL #3 CYL #1 Exhaust Transition Cylinder Arrangement - left side S10 19 CYL #6 CYL #4 CYL #2 EGT #2 TIT left EGT #4 EGT #6 CHT probe Ignition Configuration S10 20 Left Magneto Top #2 Top #4 Top #6 Bottom #5 Bottom #3 Bottom #1 Ignition Configuration S10 21 Right Magneto Bottom #2 Bottom #4 Bottom #6 Top #5 Top #3 Top #1 Magneto Impulse Coupling S10 22 S10 23 NEVER turn the propeller in it’s operating direction. Ignition System S10 24 • System Ops Check • RPM drop • EGT rise on one spark plug Ignition System S10 25 S10 26 Pre-ignition - broken ceramic and more. S10 27 Destructive Detonation sample S10 28 Destructive Detonation sample S10 29 Power up Fuel flow CHT excursion start EGT CHT EGT Excursion before CHT Oil Pressure vs Oil Temp S10 30 Oil Pressure vs Oil Temp S10 31 Typical oil pressure at 180 degrees F should be 55 p.s.i. Oil Pressure S10 32 Fuel Flow S10 33 Fuel Flow Transducer Location Fuel Nozzles – dirt simple S10 34 Naturally Aspirated Turbocharged Reference to Upper Deck pressure Reference to Ambient pressure High CHT S10 35 Take off #3 CHT is high but goes low in cruise. Note the EGT during the two extra leaning events. CHT is a good indicator of power. Lean Test S10 36 • www.gami.com for full procedure • Exposes fuel injector imbalance and condition (should be used to determine maintenance action) • Can help identify induction leaks • Establishes base line for certain maintenance events (injector cleaning) Lean Test - Detail S10 37 Lean Test S10 38 Up close view of Fuel Flow on each cylinder when it peaked. Your results may vary. :) S10 39 Don’t clean the fuel injector nozzles unless the data supports it. Minimize MIF Induction Leak Test S10 40 Amps vs Volts S10 41 Battery Alternator Exposed to the Elements Troubleshooting Exercise #1 S10 42 Troubleshooting Exercise #2 S10 43 Putting It Together S10 44 • Know your Baselines • Watch for Baselines in all flight situations • React to Changes based on actual data. • Corroborate data to confirm actual issue vs just indication anomaly • Save all flight data for possible review • Results: Safer flights, reduced stress and confident decision making. Section Eleven 182S, 182T, T182T Skylane Utilities Pitot Tube Static Ports & Sumps AD2008-10-2 AD2008-26-10 SB97-34-02R1 SB08-34-02R1 Alternate Static Port Blockage Pitot and Static Systems Installation S11 2 Pitot and Static Installation G1000 Installation S11 3 182S, 182T Vacuum System NOT G1000 2 Vacuum Pumps Inlet Filter Suction Gage 4.5- 5.5 in Hg Vacuum Pump Shrouds S11 4 182S, 182T Vacuum System NOT G1000 Check Date Code Replace Hoses Every 10 Years SB02-37-04 10 yr change Cessna SE82-8 Vacuum System Maintenance Replace Regulator Filter Every 100 hours or Annual Inspections B3-5-1 Filter Part Number Replace Every 500 hours S11 5 182S, 182T Vacuum System NOT G1000 SB99-37-01 Aluminum Elbows, To avoid collapsing of hoses on 182S SB00-37-01 Only 182S Mandatory Filter Replacement due to bad batch of D9-18-1 inlet filters. SB02-37-01 182T, T182T SB02-37-03 182S Reducer Fitting inspection and replacement S11 6 S11 7 System Installation182T G1000 Vacuum Vacuum Pump Inlet Filter Suction Gage Regulator Valve Replace Every 600 hours Replace Regulator Filter Every 100 hours or Annual Inspections B3-5-1 Filter Part Number Green Line 4.5 to 5.5 inches Min 4.5 at 1200 RPM Myth of Moving the Propeller Backwards . . . S11 8 Dry Air Vacuum Pump S11 9 SNL00-8 S11 10 SNL00-8 Cont. S11 11 182S & 182T Cabin Heat and Defrost Systems Airflow Path S11 12 T182T Exhaust Pipes & Transition Assembly S11 13 182S 182T Cabin Heating, Ventilation & Defrost Systems S11 14 182S, 182T Fresh Air System Installation SB99-21-01 182S Fresh Air Vent Replacement To keep water from entering cabin. CPA Tech Note# 013 O2 Bottle specs & testing S11 15 T182T Oxygen Systems T182T Bottles Now SP8162- 5 Year Test Cycle 15 Year Replacement S11 16 T182 Goodrich 2-Bladed Propeller De-Ice System 0 CPA Tech Notes Vendor List 600 17th St, Ste 2800S, Denver, CO 80202-5428 www.cessna.org © Copyright 2018, Cessna Pilots Association, Inc. Handouts Rev. 57 (08/08/2022) Tech Notes Available to CPA Members Numbered Tech Notes 001 Nose Wheel Shimmy 002 Owner Performed Maintenance and Excerpts from FAR Part 43 003 Uneven Fuel Feed 004 Excessive Oil Discharge “Blaylock Drawings” 005 Seat Latching System Inspection and AD 006 Good & Bad News About Landing Lights 007 TBO & Beyond 008 Six “Tools” That Tell Engine Health 009 Items Most Overlooked During Inspection 010 Hot Starts 011 Vapor Lock Problems in 210 Series from ‘64 thru ‘81 Model Years 012 Troubleshooting the Turbo-System 013 Inspecting & Retiring Oxygen Bottles 014 Rigging — The Key To Speed 015 Door Locks A-Batch 016 337 Skymaster Fuel System 017 The Traveling Tool Kit 018 Compass Swinging 019 Tips on Tip Tanks (Twins) 020 Cessna 150/152 Engine Upgrades 021 What is Wrong With Lycoming’s O-320-H2AD (172N) Engine? 022 Alignment Procedures for 182 Main Landing Gear 023 Voltmeter or Ammeter? Maybe a Smart Volt Meter 024 Single Engine Cessnas & Their Jack Pads 025 Stabilator Maintenance for Cardinals & RGs 026 Landing Gear Retraction System on Twins 027 Twin Cessna Electromechanical Gear Retraction System 028 Nose Gear Spring Guide 172RG, R/TR182, 210, 337 Landing Gear 029 Strobe Lights for Single Engine Cessnas 030 Child Seats 031 Obtaining Manuals for Cessna Aircraft 032 Preheaters 033 Installing Spin-On Oil Filter Kits on Lycoming Engines 034 Determining Operating Costs 035 Proper Engine Break-In Procedures 036 Windshield Installation 037 A Guide to Changing Cessna Fuel Bladders 038 When Metal Let Us Down 039 Published Service Ceiling 040 Mandatory Service Bulletins: Are They Really Mandatory? 041 AD 96-09-10 (Oil Pump Gears) Clari¿cation 042 Products to Clean Aircraft 043 Starting Sequence For Split Master/Alternator 043 ‡ Switch Models 044 Putting Compressions In Context Revisited 045 Converting Air Conditioning System 046 Aircraft Engine Cylinder Color Code Identi¿er 047 Replacing Missing Data Plates 048 Single Engine 95 AMP Alternator Installation Tips 049 Avionics Master Switch 050 Alternator & Voltage Regulator 051 Owner-Produced Aircraft Parts 052 Landing Gear Hydraulic Hose Information 053 Finding Placards 054 Brakes on Retractable Singles 055 Heat Exchanger (Knisley) 056 Koroseal Lacing 057 Vacuum Pump Cork Gaskets 058 Strut Gut Job 059 Trim Tab Actuator Rebuild 060 Dealing with Damage to Wing Lift Struts 061 Repairing Brake Cylinder Assemblies 062 Turbocharger Check Valves 063 The TR182 Throttle and Waste Gate Control Assembly 064 Contactors - Critical But Often Neglected 172-T01 PowerÀow Exhaust System In 172L 172-T02 172 Engine Upgrade 172-T03 172 High Oil Temperatures 180-T01 Engine Upgrade 182-T01 Lower Cowl Inspection on The 182 182-T02 Engine Upgrade 206-T01 Engine Upgrade 210-T01 Replacing Hydraulic Power Pack 210-T02 Smoking Rivets Can Be Detrimental to Your 210 337-T01 The Pressurized Skymaster 337-T02 Landing Gear Electro Hydraulic Powerpack 337-T04 Skymaster Alternator Drive Couplings Model Histories 150/152 History 185 History 172 History 205/206/207 History R172K History 210 History 172RG History P210 History 175 History 310 History 177 History 320 History 180 History 340 History 182 History 337 History R/TR 182 History Sources For... S-01 Powered Tow Bars S-02 AD Notes S-03 Fairings and Wing Tips S-04 Carburetor Temperature Gauges S-05 Shoulder Harnesses S-06 Cockpit Organizers S-07 Preheaters S-08 Standby & Dual Vacuum Kits S-09 STOL Kits & Vortex Generators S-10 Floats, Skis and Tundra Tires Other Available Tech Notes Recommended Paint Shops Salvage Yard List Numbered Tech Notes, Model Histories and Sources For... are available to read or download on the members-only side of CPA’s web site: www.cessna.org 182R and Earlier VENDOR CALL OUTS IN PRESENTATION Cessna Propeller Aircraft Customer Support 316/517-5800 Pre-1976 Parts/Service Manuals McCurtain Technologies 877/603-3578 www.mccurtaintg.com Window Latches Starter Adapters NIAGARA AIR PARTS 800/565-4268 www.niagaraairparts.com Oil Coolers PACIFIC OIL COOLER 800/866-7335 www.oilcoolers.com Oil Filter Adapter F&M ENTERPRISES 888/317-5222 www.fm-enterprises.com Airbox Repair and Reinforcement DYNAMIC PROPELLER 509-546-0430 Engine Heat Shields OREGON AIRCRAFT DESIGN 503/267-1486 www.oregonaircraftdesign.com For Replacement Flap Indicator VISUAL INSTRUMENTS 503/472-3350 www.visualinstruments.com Flap Motor and Transmission Repair Commercial Aircraft Products 316/942-7987 Flap Roller Kits, Cowl Flap Cables Rudder Pedal Repair MCFARLANE AVIATION, INC. 800/544-8594 www.mcfarlaneaviation.com  Fuel Gauge Repair INSTRUMENT REBUILD 360/683-6245 Stewart Warner Gauge Repair AIRPARTS OF LOCKHAVEN 800/443-3117 Wet Wing Sealants SEALPAK 316/942-6211 www.sealpackcoinc.com Voltage Regulators ZEFTRONICS 800/362-8985 www.zeftronics.com Monarch Fuel Caps HARTWIG FUEL CELLS 800/843-8033 or 204/668-3234 www.hartwig-fuelcell.com Air Oil Separators AIRWOLF FILTER CORP. 800/326-1534 or 440/632-5136 www.airwolf.com Air Oil Separator M-20 TURBOS, INC. 800/421-1316 or 561/995-9800 www.m-20turbos.com Vents SOROS 940/668-8470 www.ventube.com Vents Precise Flow 63257<¶6 800/776-7897 www.sportys.com     dŚĂŶŬLJŽƵĨŽƌĂƚƚĞŶĚŝŶŐĂŶĚƌĞŵĞŵďĞƌ ƚŚŝƐŝƐĂŶ&ƉƉƌŽǀĞĚŽƵƌƐĞ  tĞŚŽƉĞLJŽƵŚĂǀĞĞŶũŽLJĞĚĂŶĚůĞĂƌŶĞĚ ŵŽƌĞĂďŽƵƚLJŽƵƌϭϴϮ