Cessna 177 RG 72-78

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Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1768 lbs
Max Weight 2800 lbs
Useful Load: 1032 lbs
Engine Name Lycoming IO-360
Engine Number 1
Horsepower 200 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 17100 ft
Max Fuel 60 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 148 kts
GPH (75% BHP): 10.5
MPG (75% BHP) 14.1
Range (75% BHP): 744 nm
Fuel Cost Per Seat Mile 0.11 $
Fuel Cost Per Hour 63 $
MPG per 1000 lbs of Payload 14.55
F-T (Speed^2/FuelBurn) 20.9 HP
F-T Payload 21.6 kts
MPH To HP: 7.4 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1585 ft

SA00014WI Installation of stabilator tips. Issued 1/6/1993
SA00015WI Installation of wing tips. Issued 1/6/1993
SA00024NY Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Amended 10/3/2012
SA00048DE Installation of oil filtration system. Issued 8/26/1993
SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00068SE (PAGE 1) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010
SA00161BO (1 OF 3) Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005
SA00186AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00194AT Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface treatment P/N AA-40. Reissued 11/14/1994
SA00211AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/17/1994
SA00212AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/17/1994
SA00243BO (2 OF 5) Installation of Centurion Consulting Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100) or without roll steering (p/n 0025-5200). Amended 7/21/2011
SA00269BO (1OF 3) Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ) Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1 and Avidyne Mounting Tray P/N 700-00034-000. Reissued 4/9/2010
SA00272WI Replacement of hydraulic system pressure switch. Reissued 11/8/2007
SA00281BO Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ) Sensor Systems Inc. Antenna P/N S67-1575-109 or equivalent and optional Avidyne Mounting Tray P/N 700-00165-000 Amended 4/24/2012
SA00290BO (PAGE 1 ) Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX Reissued 7/1/2010
SA00317SE Installation of the Precise Flight Series 100 Speedbrake System Amended 11/7/2003
SA00382NY Installation of replacement windshields. Issued 12/7/1995
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00419NY Installation of cockpit utility light. Reissued 12/31/2002
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00680SE (3 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00709LA Installation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required. Reissued 5/14/2002
SA00749AT Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent) Amended 12/10/1997
SA00780SE (PAGE 2) Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No. SA00780SE dated February 1 2001 or later FAA approved revision. Amended 5/11/2010
SA00812CH Replace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies. Reissued 6/30/2006
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00895LA Installation of instrument panel. Reissued 5/14/2002
SA00897WI Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery. Issued 8/11/2000
SA00908NY Installation of Fiberglass stabilator tips. Issued 11/6/1998
SA00954SE (1 OF 2) Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711 Report 106P Revision B dated August 2 2001 or later FAA approved revision. Amended 8/11/2003
SA01033SE Installation of vortex generators on wings and tail surfaces in accordance with Drawing Package MA2162 Revision IR dated November 1 2001 and Installation Manual MA2163 Revision IR dated December 3 2001 or later FAA approved revisions. If more than five vortex generators are damaged or missing the aircraft is not airworthy. Issued 1/8/2002
SA01077SE (PAGE 1) Installation of fluoropolymer film. Reissued 8/20/2003
SA01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010 0:00
SA01105WI-D (1 OF 2) Installation of Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic Terrain and Weather Sensors. This STC also is approved for some single-engine aircraft. See SA01105WI-D (2 of 2). Amended 5/31/2007
SA01114CH Installation of P2 Incorporated 6600 Audio Advisory system Reissued 11/4/2013
SA01118WI Installation of the Concorde FLA or VRSLA RG series batteries in the Cessna Single Engine Airplanes listed on the attached FAA Approved Model List (AML) No. SA01118WI dated October 17 2001 Amended 11/30/2013
SA01120SE Installation of Door Steward. Amended 3/4/2010
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01158WI (1 OF 2) Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. Amended 3/29/2005
SA01164AT Installation of Composite Spinner. Amended 10/13/2000
SA01205WI-D (1 OF 2) Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors. );INSERT INTO stc_table VALUES (  Amended 11/20/2007
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01240SE (2 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
SA01280CH Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model s/n 67042 and up) (For Cessna 421C model s/n 1017 thru 1404) Issued 8/29/2000
SA01330LA (PAGE 1) Installation of alternate avionics support assembly. Reissued 10/6/2010
SA01386NY Installation of Fibre Glass Reinforced Plastic Nacelle Fairing Trade Name Exhaust Fairing . Reissued 10/9/2002
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01436SE (1 OF 2) Cockpit sunvisor retrofit kit. Issued 8/2/2004
SA01473SE (2 OF 5) Installation of a GTX 32 (mode C) GTX 33 (mode S) or GTX 33D (mode S with diversity) Remote Transponde Amended 5/21/2008
SA01487SE-D (Page 1) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01560WI-D Installation of the Honeywell KFD 840 Primary Flight Display System. );INSERT INTO stc_table VALUES ( REQUIRED DATA: AML No. 159-08325-0002 Revision - dated 12-1-2009. Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate. Amended 7/22/2010
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (1 OF 5) Installation of an antenna Amended 2/15/2007
SA01714WI (Page 1) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
SA01734SE (PG 4) Application of Stewart Systems synthetic fabric covering system to aircraft fuselage wings tail surfaces control surfaces and related parts. Amended 3/23/2011
SA01800SE (PG 1) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01834CH (1 OF 2) Installation of the High Intensity Discharge Light Assembly Kit. Amended 3/20/2009
SA01860NY (1 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01861SE (PAGE 1)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01933LA-D Page 1 Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation );INSERT INTO stc_table VALUES ( System Amended 4/1/2013
SA01933LA (2 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01988SE (PAGE 3) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02013CH Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). Amended 5/2/2011
SA02015SE-D Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Amended 2/5/2014
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
SA02033AT (PAGE 2) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) Amended 7/25/2008
SA02072AK Installation of hourmeter airspeed switch. Amended 11/14/1997
SA02110CH (PAGE 1) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02119SE Page 1 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02153LA-D (Page 1) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
SA02203AK (PAGE 3)  Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
SA02212AK (PG 1) Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems  Amended 5/4/2011
SA02217AK (2 OF 5) Installation of Garmin AT Model GDL90 UAT Data Link System in accordance with Garmin AT Inc. GDL 90 UAT Master Data List P/N 560-0278-01 Revision A dated November 12 2004 or later FAA approved revision.  Amended 12/1/2004 0:00
SA02265SE Installation of a camera housing Amended 11/1/2013
SA02268CH (PAGE 2) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02268CH (PAGE 3) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02276AK Installation of AMSAFE Aviation Inflatable Restraints Amended 3/12/2013
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02293AK (2 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
SA02408AK Installation of the LoPresti Speed Mods Cowlabunga Cowling System for Cessna 177RG aircraft Reissued 4/2/2013
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02446CH Installation of the Courtesy Light Kit. Issued 6/25/2007
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02547AT (PG 1) Installation of a Voice Alert System. Amended 8/28/2007
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 5) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02930NY Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3 G2 and G1 as primary Cylinder Head Temperature (CHT) Exhaust Gas Temperature (EGT) and Turbine Inlet Temperature (TIT) Instruments. Reissued 6/12/2012
SA02987CH Installation of the Electroair Electronic Ignition System Amended 7/23/2013
SA03148NY (PAGE 2 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA03623AT Installation of Power Flow Inc. (PFS) improved performance exhaust system. Issued 10/1/2008
SA09126AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-608 with Optional Autotrim System. Amended 4/30/2001
SA09296AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-741-20/30. Issued 11/7/1997
SA09300AC-D Installation of S-TEC System 20/30 single and two axis automatic flight guidance systems model ST-752-20/30. Issued 11/6/1997
SA09304AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-742. Issued 11/10/1997
SA09336AC-D Installation of S-TEC system 30 alt altitude hold system. Issued 1/30/1998
SA09387AC-D Installation of S-TEC Manual Electric Trim System Model ST-836. Issued 8/19/1998
SA09434AC-D Installation of S-TEC System 40X/50X Single and Two Axis Automatic Flight Guidance Systems Model ST-783-40X/50X. Issued 3/23/2000
SA09456AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-878. Amended 10/23/2001
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA10005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Reissued 12/29/2006
SA1005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Issued 7/23/2002
SA10126SC (1 OF 2) Installation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.  Amended 10/23/2003
SA10221SC Installation of a Chelton Aviation Corp. AP-3C autopilot in accordance with Master Drawing List No. MS-006-12 Rev. F dated February 3 2004 or later FAA approved revision. FAA approved Airplane Flight Manual MS-006-14 Rev. I. R. dated February 5 2004 or later FAA approved Revision is required. Issued 2/5/2004
SA10236SC (2 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA1049CE Installation of wing leading edge cuffs and vertical stabilizer vortex generators. Reissued 5/1/1977
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA10944SC Installation of a 210 HP Lycoming IO-390-A1A6 Engine Reissued 6/16/2009
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1309GL Installation of PAMCO Emergency Backup Pneumatic System. Amended 8/25/1988
SA1348CE Chrome-plated brake disc installation. Issued 8/18/1977
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1447GL Installation of on-board engine analyzer system. Amended 5/18/1992
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA1479SW Mitchell automatic flight system AK378 consisting of Century I auto- pilot with optional omni tracker. Reissued 7/10/1984
SA1510SW Mitchell automatic flight system AK379 consisting of Century IIB autopilot with optional radio coupler. Reissued 7/13/1984
SA1556GL Installation of Hartzell 3 bladed propeller model HC-C3YR-1RF/F7282 and associated spinner assembly no. A-2295-1 and mounting kit A-2476-7. Amended 1/6/1995
SA1557GL Installation of Hartzell 3 bladed propeller model HC-C3YR-1RF/F7282 and associated spinner assembly no. A-2295-1 and mounting kit A-2476-7. Reissued 12/29/1992
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1660NM Installation of a Descent Rate control (DRC) system (wing spoilers and speed brakes) including a pneumatic actuating system Issued 6/17/1982
SA1760SO Installation of Appalachian Access. stainless steel brake rotors P/N 75-15C. Reissued 2/6/1995
SA1778NM Installation of a descent rate control (DRC) system (wing spoilers and speed brakes) including pneumatic actuating system. Reissued 5/10/1984
SA1978SO Installation of Appalachian Accessories stainless steel brake discs P/N 75-40. Reissued 2/6/1995
SA1981SO Installation of Appalachian Accessories stainless steel brake discs P/N 75-40. Amended 1/14/1987
SA2-1178 Replacement of right front seat with stretcher. Amended 11/14/2001
SA2067NM Installation of BAS Inc. TSO Shoulder Harness and BAS Inc. Harness System Amended 7/11/2012
SA2162NM Installation of the Precise Flight stand-by vacuum system (SVS) Amended 11/7/2003
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2335CE Installation of fuel strainer quick drain provisions. Issued 12/14/1987
SA2344CE Installation of fuel strainer quick drain provisions. Issued 12/22/1987
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2381SO Installation of Appalachian Accessories P/N 75-92 Brake Rotors. (182 SERIES THRU 182A) Reissued 9/29/1995
SA2382SO Installation of Appalachian Accessories stainless steel brake discs. (182 SERIES THRU 182Q) Reissued 9/29/1995
SA2458CE Installation of fuel inlets and caps. (177RG S/N177RG0001 - 177RG1366) Reissued 5/3/2004
SA2557NM (1 OF 2) Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. Amended 2/22/2007
SA2586NM (PAGE 2) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2619WE Installation of Pathfinder Model P1-( ) autopilot system. Reissued 9/30/1998
SA2676NM Installation of external hinged-plate spoilers and dive brakes.  Issued 4/16/1985
SA2687NM (PAGE 1) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000
SA2693NM (PAGE 1) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009
SA2791CE Installation of wing mounted convex mirror for inspection of nose and main landing gear position. Issued 2/6/1992
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA2940NM Fabrication and installation of external hinged-plate spoilers and dive brakes. Issued 6/3/1985
SA3284NM Installation of ARNAV Systems FC-10 or FT-10 digital fuel flow indicating system. Issued 9/30/1986
SA3286SO Installationof engine cowling and firewall fasteners. (177 S/N 00001 THRU 02752) (177 RG S/N 0001 THRU 1366) Amended 8/29/2001
SA3296SW-D Mitchell automatic flight system AK758 consisting of Century I autopilot with optional omni tracking system. Reissued 3/29/1984
SA3297SW-D Mitchell automatic flight system AK759 consisting of Century IIB autopilot with optional radio coupler. Reissued 3/29/1984
SA3298SW-D Mitchell automatic flight system AK760 consisting of Century III autopilot with optional radio and glide slope couplers. Reissued 3/29/1984
SA3318NM Installation of a Venting fuel cap and restricting adapter assembly. Amended 6/23/1988
SA3387WE Installation of recognition lights on horizontal stabilizer. Reissued 2/28/1980
SA3420SW-D Mitchell automatic flight system AK921 consisting of Century III autopilot with optional radio coupler and glide slope coupler. Reissued 8/23/1983
SA3531NM Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) Reissued 9/8/2010
SA3860WE Installation of an air/oil separator. Reissued 9/28/2001
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA398NE Installation of Auto-Vac-2 manifold vacuum system per certain engine STC s. Amended 8/15/1990
SA4005NM (PG 2) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4024WE Installation of Silver Instruments Fueltron IG or IP or Fuelgard digital fuel flow and totalizer system. Reissued 4/29/1991
SA4030NM Installation of Lycoming IO-360-A1B6D or IO-360-A1B6 engine modified. Amended 6/22/1993
SA4081NM Installation of Avco Lycoming IO-360-A1B6 or IO-360-A1B6D engine equipped with FliteCraft Turbo turbocharger. Reissued 8/5/2002
SA4094NM Installation of Oilamatic engine preoiler. Amended 6/28/1991
SA4166NM Installation of Fairchild voltage regulator No. UA78 GUIC to replace the original voltage regulator in Cessna turn coordinator P/N 0661003-0506. Issued 1/25/1988
SA4302NM (PAGE 1) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA4359NM Installation of redesigned upper door hinge pin and retainer. Amended 5/17/1999
SA446GL Installation of Tull microwave landing system airborne equipment. (177RG S/N 177RG1267 AND SUBSEQUENT) Issued 9/17/1980
SA459NE Installation of a backup vacuum system similar to the Ray Ives auto-vac-2 system approved under STC SA398NE and SE414NE. Reissued 7/14/1987
SA4721NM Installation of SynCon alarm system. Amended 5/8/1990
SA475CH Installation of Inline Air Filter Kit P/N CV1J4-C Reissued 1/15/2013
SA477CH Installation of McCauley Propeller model B3D36C428/82NPA-6. Reissued 9/21/2005
SA4964NM Installation of a NSA sunvisor system for the pilot and copilot. Reissued 3/24/2003
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA5303SW-D Installation of S-TEC System 60 two axis automatic flight guidance system model ST-245 with optional automatic electric trim system. Reissued 10/22/1990
SA5318SW-D Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems model ST-243-40/50 Issued 5/10/1984
SA5334SW-D Installation of S-TEC System 60 two axis flight guidance system Model ST-241 with optional automatic electric trim system. Reissued 3/10/1989
SA5337SW-D Installation of S-TEC System 60 pitch stabilization system Model ST-242 with optional automatic electric trim system. Issued 9/5/1984
SA5340SW-D Installation of S-TEC System 60 pitch stabilization system Model ST-246 with optional automatic electric trim system. Issued 9/11/1984
SA5342SW-D Installation of S-TEC System 60 single axis automatic flight guidance system Model ST-244. Issued 10/2/1984
SA5344SW-D Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-247-40/50. Issued 10/3/1984
SA5347SW-D Installation of S-TEC System 60 single axis automatic flight guidance system Model ST-240. Issued 10/10/1984
SA5359SW-D Installation of S-TEC manual electric trim system Model ST-258. Issued 12/5/1984
SA5656NM Installation of burglar alarm system. Reissued 7/21/1993
SA5656NM (PAGE 1) Installation of burglar alarm system. Reissued 7/21/1993
SA5697NM Repair of upper hinge on the cabin door. Amended 8/4/2000
SA5701SW Installation of electrically driven vacuum pump as a standby auxiliary pump to the existing instrument. Reissued 4/6/2007
SA582NW Fabrication of replacement wire rope cable assemblies Issued 5/12/1978
SA5924NM Installation of RPM instrument. Amended 11/24/1997
SA5925NM Installation of oil pressure/temperature instrument. Amended 12/8/1997
SA5926NM Installation of manifold pressure instrument. Amended 8/15/1993
SA593CH (1 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009
SA6022NM Installation of an electronic digital engine tachometer Model P-1000. Issued 5/18/93. Reissued 1/14/2002
SA613GL Installation of a Shadin Co. fuel flow indicating system. Amended 1/10/1985
SA615EA (PAGE 1) Installation of Whelen Anti-Collision Strobe Light Systems Part Number 01-0770006-( ) 01-0770028-( ) 01-0770029-( ) 01-0770062-( ) 01-0770900-( ) and 01-0771055-( ) as replacement for originally installed anti-collision lights. Reissued 7/6/2010
SA71GL Installation of air filters Reissued 6/20/2000
SA8008SW Installation of Zeftronics alternator control units P/N s R25101 (27.7V systems) or R25102 (28.8V systems). Reissued 5/12/1998
SA800EA (PAGE 2) Installation of Aviation White Anti-Collision Strobe Lights. Whelen Models A429 A430 A434 A450 A408 (white) A408R/W or A47OR/W (red/white) A500 A625 or A650 and associated power supplies or Model SA strobe light system. Amended 7/6/2010
SA8018SW Installation of Zeftronics alternator controller unit P/N R15100 (Product configuration file ZOCPCF) or P/N R15V00 )Product configuration file (ZODPCF). Amended 1/6/1992
SA8031SW Installation of Zeftronics alternator controller unit P/N R15100 or R15V00. Amended 1/6/1994
SA8032SW Installation of Zeftronics over-voltage sensor unit P/N V11100 (Product configuration file ZOLPCF). Reissued 5/12/1998
SA838NE Installation of McCauley C3D36C415/82NGA-8 propeller. Issued 3/29/1991
SA8432SW Installation of V25101 overvoltage sensor. Reissued 5/12/1998
SA8922SW Installation of replacement Ultimate Engine Oil Filter for Textron Lycoming and Teledyne Continental engines. (411 S/N 000 THRU 0126 S/N 0127 AND UP) (T188C S/N 03474 AND UP) (206 S/N 05030 AND UP) (207 S/N 05227 AND UP) (T207 S/N 05227 AND UP) (P21 0 SERIES S/N 278 AND UP) (180 S/N 53087 AND UP) (210 S/N 63373 - 63375 AND UP) (B19 SPORT) Issued 7/21/1994
SA917EA Installation of Grimes aviation white anti-collision strobe light system two light or three light series 555 for wing tips and tail P/N 30-0555-( ). Reissued 6/4/2007
ST01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
ST01494LA (PG 1) Installation of the FiberLite Aircraft Lighting System in accordance with Master Document List listed on Aircraft Model List (AML) Number ST01494LA or later FAA approved revisions. No flight manual is required. Reissued 8/30/2011
ST01700NY (1 OF 2) Installation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator CHT-100 Cylnder Head Temperature INdicator FL-100 Dual Fuel Level Indicator FP-100 Fuel Pressure and Ammeter Indicator OL-100 Oil Pressure and Temperature Indicator and VA-100 Voltmeter and Ammeter Indicator. Issued 7/8/2003
ST02307CH Installation of Rudder Pedal Extensions. Amended 10/13/2006
ST02547AT (1 OF 2) Installation of a voice alert system. Amended 5/13/2003
Fusulage Construction
Airframe Material
Number of Doors
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
Aileron Type
Aileron Trim
Aileron Control System
Flap Type
Wing Flap Actuation
Empennage Type
Empennage Rib Material
Empennage Skin Material
Rudder Trim
Yaw Trim Actuator
Yaw Control System
Pitch Trim
Pitch Control System
Pitch Trim Actuator
Landing Gear
Landing Gear Type
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Instrument Panel
Flight Control
Number of Seats
Window Defrost
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller Manufacturer
Propeller Model
Number of Blades
Minimum Diameter
Maximum Diameter
Propeller Type
Propeller Governor
Fuel System
Fuel System Type
Approved Fuel Type 1
Approved Fuel Type 2
Approved Fuel Type 3
Fuel Capacity (G)
Tank Type 1 Location
Tank Type 1 Capacity (G)
Tank Type 2 Location
Tank Type 2 Capacity (G)
Usable Fuel (G)
Oil Capacity (Quarts)
Electrical System
Power Source
Power Storage
System Voltage
Alternator Amp
Battery Voltage
Battery Amp/Hour
Maximum T/O Weight (lbs)
Maximum LDG Weight (lbs)
Standard Empty Weight (lbs)
Useful Load (lbs) 0
Station 1 Baggage Location
Max Weight Station 1 (lbs)
Station 2 Baggage Location
Max Weight Station 2(lbs)
Station 3 Baggage Location
Max Weight Station 3(lbs)
Wing Loading (lbs/sq.ft)
Vne (KCAS)
Vno (KCAS)
Va(Max Gross) (KCAS)


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