Grumman American AA5A Cheetah

Number of Active Aircraft: 542 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1260 lbs
Max Weight 2200 lbs
Useful Load: 940 lbs
Engine Name LYC O-320-E2G
Engine Number 1
Horsepower 150 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 12650 ft
Max Fuel 51 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 128 kts
GPH (75% BHP): 9
MPG (75% BHP) 14.2
Range (75% BHP): 633 nm
Fuel Cost Per Seat Mile 0.11 $
Fuel Cost Per Hour 54 $
MPG per 1000 lbs of Payload 13.37
F-T (Speed^2/FuelBurn) 18.2 HP
F-T Payload 17.1 kts
MPH To HP: 8.5 kts
T/O Roll - T/O over 50 FT OBST 880 ft / 1600 ft

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
SA00058WI-D Installation of Bendix/King KAP100/KAP 150/KFC 150 automatic flight control systems with optional KAS297B altitude/vertical speed selector. Reissued 2/28/2000
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
SA00079SE Installation of low oil pressure warning in conjunction with ADC (Oberg) oil filter. Amended 11/10/1994
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00136WI Operation of airplane on unleaded or leaded automotive gasoline 91 minimum antiknock index (RON+MON)/2 Issued 8/12/1994
SA00161BO (2 OF 3 Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005 0:00
SA00187AT Installation of carbon steel brake discs P/N AA-20. Reissued 11/14/1994
SA00206BO Installation of alternate air induction system.  Reissued 9/26/2007
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00238SE Installation of Aviation Development Corporation s sump mounted chip detector Issued 10/31/1995
SA00243BO (1 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
SA00243BO (3 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 (2 OF 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
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 ( PAGE3) 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 0:00
SA00380LA Limited to installation on serial number AA5-0037 ONLY. Issued 6/12/1997
SA00393SE Installation of the G/S 2500 and G/S2500R Aircraft Security Alarm System. Issued 12/6/1996
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00457WI Replacement of a new oil cooler. Issued 7/22/1996
SA00478CH (PAGE 3) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00780SE (PAGE 3) 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
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
SA00958CH Install split nose bowl. Issued 10/16/1998
SA01085LA (PAGE 2) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01240SE (1 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
SA01250WI Installation of Concorde Sealed Lead-acid (VRSLA) battery Reissued 7/30/2012
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
SA01284AT Installation of Composite Spinner Bulkhead. Amended 10/13/2000
SA01354CH Install BRC Aviation tailcone part number BRC 5103011-1 -2 BRC 5103012 -2. Issued 6/29/2001
SA01406CH Install BRC Aviation main landing gear faring part numbers BRC 5701050-3 -4. Issued 1/10/2002
SA01410CH Install BRC Aviation dorsal fin part number BRC 5302040-1. Issued 6/28/2001
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01473SE (3 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 2) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01516AT Installation of Vision Micro Systems Inc. VM1000/EC100 digital/analog engine instrumentation and caution advisory system. Amended 10/24/2008
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
SA01658NY Installation of MT-Propeller MTV-18-B/180-17 3-blade electrically controlled propeller. Issued 4/11/2003
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 (3 OF 5) Installation of an antenna Amended 2/15/2007
SA01800SE (PG 2) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01852AT Replace metal propeller spinner bulkhead with composite bulkhead. Amended 10/13/2000
SA01860NY (2 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01861SE (PAGE 2)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01933LA-D Page 2 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
SA01944CH (1 OF 2) Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index per ASTM Specification D-439 or D-4818 of any volatility class A through E or 82UL AVGAS per ASTM D-6227. Issued 3/5/2004
SA01988SE (PAGE 4) 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
SA02018SE-D (PAGE 2) Provisions installation of Garmin GPS/XM Antennas in accordance with FAA Approved Model List (AML) SA02018SE-D dated January 4 2011 or later FAA approved revision and FAA Approved GPS/XM Antenna STC Master Drawing List Document No.: 005-00638-01 Revision 1 Issued 1/4/2011 0:00
SA02019SE-D Page 2 Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/19/2012
SA02033AT (PAGE 1) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. Amended 7/25/2008
SA02033AT (PAGE 5) 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 0:00
SA02057AT Installation of a composite nose bowl. Amended 3/27/2001
SA02119SE Page 2 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02153LA-D (Page 2) 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
SA02212AK (PG 4) Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Amended 5/4/2011
SA02217AK (1 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
SA02251LA Installation of fiberglass cowling and improved engine baffles.  Reissued 8/6/2012
SA02268CH (PAGE 5) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02268CH (PAGE 6) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02283SE Page 2 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02448AT Replace exhaust system with a tuned exhaust system. Issued 1/8/2002
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02547AT (PG 2) Installation of a Voice Alert System. Amended 8/28/2007 0:00
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 3) 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
SA08528SW-D Installation of a Century Flight System Model AK1051 consisting of a Century 2110/2150/2151 autopilot. Issued 7/3/1998
SA09369AC-D Installation of S-TEC System 20/30 single and two-axis automatic flight guidance systems Model ST-822-20/30. Issued 6/19/1998
SA09370AC-D Installation of S-TEC System 30 ALT altitude hold system Model ST-823. Issued 6/19/1998
SA09386AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-840-20/30. Issued 9/17/1998
SA09390AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-841. Issued 9/17/1998
SA09990SC Installation of Sensenich Propeller 74DM7S10-1-57B and 74DM7S10-1.5-61B. Issued 5/16/2002
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
SA1018NW Installation of a Lycoming O-320-E2A engine (with a controllable pitch propeller crankshaft P/N 75010) and a McCauley 1C172/BTM7356 propeller Issued 9/12/1980
SA10344SC Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot.  Issued 10/12/2004
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1133SO Installation of an adjustable trim tab on left aileron. Amended 1/24/1991
SA1169NW Installation of a Lycoming O-360-A4K engine and a Sensenich76EM8S10-0-63 propeller. Reissued 4/29/1991
SA1186NW Installation of a Lycoming O-360-A4K engine a McCauley 1A170FFA/7563 or a Sensenich76EM8S10-0-60 thru -65 propeller and associated systems. Amended 4/29/1991
SA1195NW Installation of Sensenich 76EM8S10-0-60 through -65 propellers on a Lycoming O-360-A4K engine Reissued 6/14/1991
SA1299NW Installation of a McCauley propeller on Lycoming O-320-E2G engine. Reissued 4/29/1991
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1472SW Mitchell automatic flight system AK373 consisting of Century I autopilot with optional omni tracker. Reissued 7/10/1984
SA1486SW Mitchell automatic flight system AK374 consisting of Century IIB autopilot with optional radio coupler. Reissued 7/10/1984
SA1498NM Repair of the wing rear spar Issued 4/23/1982
SA1512WE (2 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007 0:00
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1600NM ONE-ONLY STC S/N AA5A-0342: Installation of Sensenich or McCauley propellers and engine cooling baffles Issued 4/2/1982
SA1735GL Installation of Master Nag warning system. Amended 3/21/1994
SA1745SO Installation of Appalachian Access. stainless steel brake rotors P/N 75-20. Reissued 2/6/1995
SA1767NM Alteration of the oil cooler and air induction system. Reissued 4/29/1991
SA191NE Replace original brake discs with discs modified in accordance with Roland Longarzo procedure. Reissued 10/4/1984
SA1965CE Operation on unleaded and/or leaded automotive gasoline. Amended 11/27/1985
SA2125NM Installation of Lycoming 0-360-A4M engine and Sensenich76EM8S10-0-60 propeller. Reissued 4/29/1991
SA2141NM Installation of Sensenich 76EM8S10-0-63 Propeller Model and a Gulfstream American Spinner Service Kit #143 Issued 8/23/1983
SA2190NM Page 2 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2268SO Installation of an instrument panel overlay and glove box door. Issued 3/7/1988
SA2275SO Installation of a glare shield assembly. Issued 3/7/1988
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 3) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2593NM Installation of Hoskins Model CFS-1000A -1001A FT-100 or FT-101 fuel flow indicating system. Reissued 1/30/1998
SA2601NM Installation of AVCO Lycoming IO360-A1B6 engine McCauley propeller Model 2D34C215/90DJA-14 Stewart Warner 486 oil cooler Bendix RSA-5Ad1 fuel pump and Wing Tip Landing Light Installation.  Amended 12/3/1987
SA2619NM Replace carburetor air induction system with a Beechcraft Airbox (P/M 169-910049-59) on Lycoming O-360-A4K engine with a Sensenich 76EM8S10-0-63 propeller installed per STC SA1195NW with Grumman Spinner Assembly SK142-K Issued 7/2/1984
SA2620NM Modify engine baggles and relocate oil cooler to above and behind the left hand rear cylinder on Lycoming O-360-A4K engine with Sensenich76EM8S10-0-63 propeller. Reissued 4/29/1991
SA2683NM Installation of Precise Flight Inc. stand-by vacuum system (SVS) Amended 3/10/2005
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
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA3031SW-D Mitchell automatic flight system AK514 consisting of Century I autopilot with omni tracking system. Reissued 6/21/1984
SA3032SW-D Mitchell automatic flight system AK515 consisting of Century IIB autopilot with optional radio coupler. Reissued 6/21/1984
SA308EA (1 OF 2) Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Marvel-Schebler MA-2 MA-3 MA-4 MA-4-5 MA-6 and HA-6 series carburetors. (Normal Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.) Amended 11/20/1978
SA3301WE Installation of Model EGT-1 exhaust gas temperature monitoring system. Issued 11/23/1976
SA3308NM Installation of Lycoming O-360-A4K engine Issued 2/4/1986
SA3309WE Modification of primary control system by addition of rudder- aileron interconnect and installation of Pathfinder autopilot systems and/or pitch trim systems. Reissued 9/30/1998
SA330NE Replace original brake discs w/William C. Roberts stainless steel discs P/N 201-120-SS. (M20M s/n 27-0001 thru 27-0116) Reissued 6/18/2002
SA3326NM Install Sensenich Propeller model76EM8S10-0 (60-inch to 63-inch pitch inclusive) and Gulfstream Aerospace spinner assembly Kit P/N SK143-2. Issued 2/7/1986
SA3344NM Relocation of oil cooler. Issued 4/3/1986
SA3531NM Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) Reissued 9/8/2010
SA3564SW Modification of torque tube assembly. Amended 12/15/1989
SA3760NM Installation of single piece frameless windshield. Reissued 6/25/2001
SA3841NM Installation of a Lycoming O-360-F1A6 engine and a McCauley B2D34C propeller Issued 6/11/1987
SA4005NM (PG 1) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4005NM (PG 5) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4165NM Installation of a Lycoming O-540-E4A5 engine and a Hartzell Model HC-C2YK-8477-8R propeller Issued 1/25/1988
SA4172NM Installation of Aviation Development oil filter. Amended 5/22/2009
SA4325NM Installation of modification to engine cowl nose bowl which splits the nose bowl horizontally allowing it to be removed without prop removal Issued 5/20/1988
SA4708NM Installation of bolts to strengthen the nose gear torque tube assembly. Issued 2/28/1989
SA4721NM Installation of SynCon alarm system. Amended 5/8/1990
SA4740NM Installation of a landing light in the left wing tip or in both wing tips. Reissued 4/9/2012
SA4849SW Install fuel flow transducer in fuel line and install fuel flowmeter/totalizer in aircraft Amended 10/26/1984
SA4966NM Installation of a Lycoming IO-540-D4A5 engine and a Hartzell HC-C2YK-8477-7 propeller. Issued 9/4/1990
SA4968NM Installation of a Lycoming O-320-E2D engine equipped with a Sensenich 4DM6-0-58 propeller reduced to 73-inch diameter using a Lycoming propeller spacer P/N E18776 modified with 5/8 bushings threaded to accept 3/8 bolts. Issued 8/14/1990
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
SA5156NM (PG 3) Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 7/29/2010 0:00
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA5372SW-D Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-278. Reissued 10/10/1986
SA5376SW-D Installation of S-TEC System 60 pitch stabilization system Model ST-279. Issued 2/15/1985
SA5386SW-D Installation of 40/50 single and two axis automatic flight guidance systems. Reissued 5/12/1989
SA5387SW-D Installation of S-TEC System 60 single axis automatic flight guidance system model ST-277. Issued 3/25/1985
SA540NE Installation of an aft baggage compartment auxiliary 18 gallon fuel tank and transfer system to the right wing tank. Issued 10/14/1987
SA5452NM Installation of a Lycoming IO-360-C1C6 engine and Hartzell HC-C2YK-1BF/F7666A-2 propeller. Reissued 5/24/2004
SA563CH Authorizes installation of engines equipped w/Unison Limited Authority Spark Advance Regulator (LASAR) ignition system w/Cylinder Head Temp. (CHT) monitoring capability on airframes. engines. Reissued 2/10/2009
SA5656NM Installation of burglar alarm system. Reissued 7/21/1993
SA5656NM (PAGE 1) Installation of burglar alarm system. Reissued 7/21/1993
SA5775NM Replacement of rudder tip with Aviation Red Lexan tip with flashing anticollision light located inside. Issued 10/2/1992
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
SA5934NM Installation of cockpit sunvisor. Reissued 3/24/2003
SA593CH (1 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009
SA6016NM Installation of an electronic digital engine tachometer Horizon Model P-1000 P/N P100050-( ). Amended 1/14/2002
SA6089SW-D Installation of S-TEC System 65 two axis automatic flight guidance system Model ST-381. Issued 10/10/1986
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
SA66NW Installation of Van s Aircraft model BA-4 fiberglass wheel fairings. Amended 9/23/1994
SA683NE Installation of Lycoming Model O-320-E2G engine that has been converted to high compression IAW STC SE682NE amended 10/27/89. Amended 11/1/1989
SA693CE Replace existing engine induction air filter with AC Spark Plug filter. Reissued 6/20/2000
SA69NW Installation of Matney s engine charge air-air filter assembly. (AA-1B AA-1 AA-1A 1969 AND ON) (AA-5 1972 1973 AND 1974 ONLY) Amended 10/8/1974
SA71GL Installation of air filters Reissued 6/20/2000
SA7205SW-D Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-456. Reissued 9/27/1990
SA7211SW-D Installation of S-TEC System 60 single axis automatic flight guidance system model ST-277. Reissued 10/15/1990
SA7212SW-D Installation of S-TEC system 60 pitch stabilization system. Reissued 10/19/1990
SA7213SW-D Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-458-40/50. Reissued 9/28/1990
SA7974SW Installation of wheel pant fairings. Amended 1/10/2006
SA800EA (PAGE 1) 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
SA8031SW Installation of Zeftronics alternator controller unit P/N R15100 or R15V00. Amended 1/6/1994
SA8505SW-D Installation of a Century Automatic Flight System Model AK1022 consisting of a Century 2010/2050/2051 autopilot. Issued 9/20/1995
SA863SO Installation of portable hand control Reissued 7/7/2013
SA867GL Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index. Surrendered 3/5/2004
SE683NE Installation of Lycoming Model O-320-E2G engine that has been converted to high compression. Reissued 8/7/1998
ST00811CH Installation of Mitchell Aircraft Products gauge cluster. Issued 1/30/1998
ST01085LA (PAGE 2) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
ST02547AT (2 OF 2) Installation of a voice alert system. Amended 5/13/2003
AirFrame
Fusulage Construction
Airframe Material
Number of Doors
Wing
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
--Aileron
Aileron Type
Aileron Trim
Aileron Control System
--Flap
Flap Type
Wing Flap Actuation
Empennage
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
Retractable
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Cabin
Instrument Panel
Flight Control
Number of Seats
Heating
Window Defrost
Cooling
Profiles
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Engine
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Geared
Cooled
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller
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
Limitations
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)