Beechcraft A23

Number of Active Aircraft: 152 Active- Map

Description:

Includes a slight increase in (5)HP and an additional 50 pounds of gross weight.



If you feel like you have a particular interest in this model of aircraft you are welcome to submit a brief history and description/points of interest that make this model unique.

Please send descriptions to audriesaircraftanalysis@gmail.com

Or

Have an Update?
Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1476 lbs
Max Weight 2450 lbs
Useful Load: 974 lbs
Engine Name Continental IO-346-A
Engine Number 1
Horsepower 180 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 12500 ft
Max Fuel 57 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 124 kts
GPH (75% BHP): 11.3
MPG (75% BHP) 11
Range (75% BHP): 542 nm
Fuel Cost Per Seat Mile 0.14 $
Fuel Cost Per Hour 67.8 $
MPG per 1000 lbs of Payload 10.69
F-T (Speed^2/FuelBurn) 13.6 HP
F-T Payload 13.2 kts
MPH To HP: 6.9 kts
T/O Roll - T/O over 50 FT OBST 1300 ft / 1956 ft

SA00002SE Installation of fiberglass reinforced plastic wing tips Issued 6/14/1993
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
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
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00161BO (3 OF 3 Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005 0:00
SA00197AT Installation of Appalachian carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00208AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00243BO (4 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
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 2) 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
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00478CH (PAGE 3) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00638WI Installation of Concorde Battery Corporation (vrsla) Valve Regulated Sealed Acid Battery. Amended 8/10/2012
SA00747SE Installation of a Lycoming IO-360-A1B engine and a McCauley B3D36C429-82NPA-6 propeller. Issued 10/21/1999
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
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
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
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
SA01114CH Installation of P2 Incorporated 6600 Audio Advisory system Reissued 11/4/2013
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 (2 OF 2) Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. Amended 3/29/2005 1:00
SA01229SE Page 2 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01240SE (3 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006
SA01269LA Installation of replacement wing tip fairing assembly. Issued 11/21/2001
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 2) Installation of alternate avionics support assembly. Reissued 10/6/2010 0:00
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01473SE (5 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
SA01555SE Installation of vortex generators on the wings and tail surfaces. Issued 5/25/2005
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
SA01690SE Installation of S-TEC Autotrim System Model ST-667. Issued 7/19/2006
SA01692SE (Page 2 of 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (5 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
SA01800SE (PG 4) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01860NY (1 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01861SE (PAGE 4)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01923LA Installation of the P-1000 Digital Electronic Tachometer. Issued 1/23/2007
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 (5 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01988SE (PAGE 2) 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 4) 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
SA02053SE Cockpit Sun Visor installation Issued 2/23/2010
SA02110CH (PAGE 3) 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
SA02168AK (PG 1) Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. Issued 3/23/2001
SA02217AK (5 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
SA02246LA Installation of a flap handle extension. Amended 11/16/2010
SA02268CH (PAGE 4) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02532AT Installation of subject Michelin tires on appropriate aircraft. For Michelin 5 6 8 and 10-inch rim diameter tires on General Aviation Aircraft. Issued 6/5/2002
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 6) 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 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA03231AT Installation of an improved performance exhaust system. Issued 4/24/2006
SA09235AC-D Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance system Model ST-667 with Optional Autotrim System. Amended 10/25/2001
SA09409AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic flight Guidance Systems Model ST-855-20/30. Issued 5/24/1999
SA09510AC-D Installation of S-TEC System 20/30 single and two-axis automatic flight guidance systems model ST-889-20/30. Issued 6/22/2001
SA09514AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-893. Issued 11/19/2001
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
SA10236SC (4 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA10682SC Installation of alternator and voltage regulator Reissued 11/16/2007
SA106GL Installation of Gerdes Products wheels and brakes. Issued 2/13/1976
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1147EA Installation of DeVore vertical tail floodlights on upper surface of horizontal stabilator. (23 S/N M-555 AND UP) Reissued 2/28/1980
SA1237GL Installation of a Shadin Co. fuel flow indicating system. Reissued 6/8/2006
SA1262WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA1276GL Installation of an auxiliary vacuum system. Reissued 4/21/1988
SA1290WE Installation of Quazar high- intensity supplemental exterior flashing lights. Amended 11/25/1969
SA1315WE Installation of Mixture Monitor (exhaust gas temperature probe gage and selector) in accordance with Delta Products Part Lists A-192 and A-193 or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9 1981 or later FAA approved revision and/or Drawing List MM-127 dated November 15 1981 or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29 1968 copy attached or later FAA approved revision. Reissued 4/15/2011
SA1346SW Installation of Mitchell automatic flight system model AK341consisting of Century I autopilot and optional Omni Tracker. Reissued 7/10/1984
SA1348SW Installation of Mitchell automatic flight system AK342 consisting of Century IIB autopilot with optional radio coupler. Reissued 7/10/1984
SA135EA Installation of engine exhaust combustion monitor. Reissued 2/14/1972
SA1376WE Installation of Brittain Industries BSA-3 stability augmentation system. Reissued 10/20/1972
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA1475WE Installation of Brittain Model B2C Flight Control System. Reissued 10/20/1972
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
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
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1680SO Installation of an adjustable nine-inch trim tab on the left aileron. Issued 9/20/1984
SA1701SW Mitchell command electric trim system Model AK454. Reissued 7/16/1984
SA1724WE Installation of Brittain Model B-5 flight control system. Reissued 10/20/1972
SA1735GL Installation of Master Nag warning system. Amended 3/21/1994
SA1952SO Installation of Appalachian Access. stainless steel brake discs P/N 75-43. Amended 1/14/1987
SA2054SO Installation of Appalachian Acces. stainless steel brake discs P/N 75-69. Amended 5/19/1992
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA2148WE Installation of Brittain Industries B-VII NAV-2B B2C and BSA-6 flight control systems. Reissued 10/20/1972
SA2160NM 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
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2557NM (1 OF 2) Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. Amended 2/22/2007
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
SA2940SW Addition of Hydro Seal Fluid Additive to landing gear shock struts. Reissued 8/8/1980
SA3001SO Installation of Appalachian Accessories stainless steel brake discs P/N 75-43. Reissued 9/29/1995
SA3016SW-D Mitchell automatic flight system AK499 cons. of Century IV autopilot or AK499FD consisting of a Century IV flight director autopilot with opt. remote annunciator. Reissued 8/1/1984
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
SA3106SW-D Installation of Mitchell automatic flight system Model AK544consisting of a Century III auto-pilot with optional radio coupler and glide slope coupler. Reissued 5/24/1984
SA3153SW-D Installation of Mitchell automatic flight system Model AK632 consisting of a Century IIB autopilot with optional radio coupler. Reissued 6/6/1984
SA3154SW-D Installation of Mitchell automatic flight system Model AK633consisting of a Century I autopilot with optional omni tracker. Reissued 6/6/1984
SA3156WE Installation of Pathfinder autopilot systems. Reissued 9/30/1998
SA3160SW-D Installation of Mitchell command electric trim system Model AK454. Reissued 6/6/1984
SA3204SO Installation of Appalacian Accessories stainless steel brake discs P/N 75-69. Reissued 9/29/1995
SA3214SW-D Mitchell automatic flight system AK342 consisting of Century IIB autopilot with optional radio coupler. Reissued 3/28/1984
SA3223SW-D Mitchell automatic flight system consisting of Century I autopilot and optional omni tracker. Reissued 3/28/1984
SA3291WE Installation of Pathfinder autopilot systems. Reissued 7/3/2002
SA3312SW-D Installation of Mitchell automatic flight system Model AK767 consisting of a Century I autopilot with optional omni tracking system. Reissued 8/15/1983
SA3313SW-D Mitchell automatic flight system AK768 consisting of Century IIB autopilot with optional radio coupler. Reissued 9/21/1983
SA3314SW-D Mitchell automatic flight system AK769 consisting of Century III autopilot with optional radio and glide slope couplers. Reissued 9/21/1983
SA3315SW-D Mitchell command electric trim AK770. Reissued 9/21/1983
SA3331SW-D Mitchell automatic flight system AK779 consisting of Century I autopilot with optional omni tracker. Reissued 9/21/1983
SA3332SW-D Mitchell automatic flight system AK780 consisting of Century IIB autopilot with optional radio couplers. Reissued 9/21/1983
SA334SW Installation of InterAv Alternator. Reissued 7/20/1981
SA3404SO Installation of Appalachian stainless steel brake disks. Issued 4/30/1992
SA3799WE Installation of flexible stainless steel oil cooler hoses. Issued 11/28/1978
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA4005NM (PG 4) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4015WE Installation of Hoskins model fuel flow indicating system. Reissued 1/30/1998
SA401SW Full flow oil filter. Issued 1/1/1960
SA4152NM Installation of a Lycoming engine model O360-A4K Issued 12/17/1987
SA4172NM Installation of Aviation Development oil filter. Amended 5/22/2009
SA423NW Conversion of a Lycoming O-320-E2C (150 HP @ 2700 rpm) to a O-320-D2A (160 HP @ 2700 rpm) with a Sensenich M74DM-0-58 propeller Issued 4/14/1977
SA4302NM (PAGE 1) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA437GL Installation of Tull microwave landing system airborne equipment. Issued 8/22/1980
SA449WE Pneumatic pitch assist PC-1 and optional installation altitude hold AH-1. Reissued 10/1/1973
SA450WE Autopilot and optional nav-coupler add-on BI-300 BI-301 or BI-304. Reissued 10/1/1973
SA4721NM Installation of SynCon alarm system. Amended 5/8/1990
SA4762NM Installation of fiberglass wing tips. Issued 8/31/1989
SA4762NM Installation of fiberglass wing tips. Amended 8/1/1991
SA484CH Installation of instrument light dimmer system. Issued 3/7/1996
SA488WE Full flow aerofilter 30409A with element 1A0235. Issued 1/1/1960
SA496CH Installation of McCauley propeller model B3D36C429/82NPA-6. Reissued 2/8/2008
SA5108SW-D Installation of S-TEC System 60two axis automatic flight guidance system Model ST-064 with optional automatic electric trim system. Amended 4/13/1998
SA5127SW-D S-TEC System 60 Two Axis Automatic Flight Guidance System ST-124 with Optional Autotrim system. Amended 1/5/1998
SA5128SW-D S-TEC System 60 single axis automatic flight guidance system ST-063. Amended 4/9/1998
SA5130SW-D S-TEC System 60 Single Axis Automatic Flight Guidance System ST-123. Amended 1/15/1998
SA5142SW-D S-TEC System 60 pitch stabilization system ST-122 with optional automatic electric trim system. Reissued 3/15/1985
SA5147SW-D S-TEC System 60 pitch stabilization system ST-125 with optional automatic electric trim system. Amended 11/28/1984
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
SA5246SW-D Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems Model ST-215-40/50. Amended 10/24/1997
SA5254SW-D S-TEC System 40/50 single and two axis automatic flight guidance system ST-214-40/50. Amended 4/13/1998
SA5581SW Installation of ALCOR true-flow/ totalizer system. Requires STC SE5583SW which can be installed on aircraft equipped with Teledyne Continental engines IO-360 L/TSIO-360 TSIO-360 TIO-360 TSIO-470 GTSIO-520 L/TSIO-520 TSIO-520 IO-520 and IO-470. The approved model numbers listed may not be inclusive. Amended 9/30/2002
SA560WE Flight control system B-4 including pitch assist PC-1 altitude hold AH-1 and navigational coupler NAV-1. Reissued 10/1/1973
SA562NE Installation of a Textron Lycoming O-320-D2B engine(150 h.p.) and a Sensenich model 74DM6-0-60 propeller. Issued 3/22/1988
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
SA589WE Full flow oil filter F-94056 and F-94056-12 with element E-3560 MEL 800. Reissued 10/5/1976
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 (4 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
SA597EA Installation of electronic voltage alarm Drawing No. 80106. Issued 1/1/1960
SA6078SW-D Installation of S-TEC system65 two axis automatic flight guidance system Model ST-371. Amended 4/17/1998
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
SA630WE Installation of oil filter assemblies. (NAVION A AND B with optional engine) Reissued 8/29/1974
SA662WE Hi-Lo sensitivity adaptor BI-400 and autopilot with NAV-1 navigation coupler and heading lock. Reissued 10/1/1973
SA664CE Installation of Hoskins MK1B Light System. Reissued 9/30/2011
SA693CE Replace existing engine induction air filter with AC Spark Plug filter. Reissued 6/20/2000
SA7152SW-D Installation of S-TEC manual electric trim system Model ST-410. Issued 5/29/1987
SA71GL Installation of air filters Reissued 6/20/2000
SA798EA Installation of Monitair exhaust gas combustion monitor kit. Reissued 2/14/1972
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
SA812WE BSA stability augmentation system. Reissued 10/1/1973
SA8431SW Installation of R15VON alternator control unit. Amended 1/6/1994
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
SA920NW Installation of a spar repair Issued 4/1/1980
ST00961LA Installation of MASS Systems fire extinguisher cartridges as replacements for Walter Kidde Aerospace fire extinguisher cartridges in fire extinguisher bottles installed in the airplane models noted on the FAA Approved Model List dated June 29 2000 or later FAA approved revisions. These fire extinguisher cartridges are in accordance with the MASS Systems Master Drawing List No. 30980-1 Slug Thrower Cartridges Master Drawing List Reissued 7/13/2011
ST01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
ST01085LA (PAGE 2) 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
ST02547AT (1 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)