Rockwell Commander 112B

Number of Active Aircraft: 21 Active- Map


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Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1773 lbs
Max Weight 2800 lbs
Useful Load: 1027 lbs
Engine Name LYC IO-360-C1D6
Engine Number 1
Horsepower 200 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 15050 ft
Max Fuel 48 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 142 kts
GPH (75% BHP): 10.5
MPG (75% BHP) 13.5
Range (75% BHP): 551 nm
Fuel Cost Per Seat Mile 0.11 $
Fuel Cost Per Hour 63 $
MPG per 1000 lbs of Payload 13.89
F-T (Speed^2/FuelBurn) 19.2 HP
F-T Payload 19.7 kts
MPH To HP: 7.1 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1829 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
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
SA00165BO Installation of Avidyne Corporation Datalink Coupler part number 700-00015-000 per Avidyne Corporation Master Document List Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions. Issued 2/20/2003
SA00192AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00197AT Installation of Appalachian carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00236BO Installation of a Lycoming IO-580-B1A engine/Hartzell HC-C3YR-1RF/F7693F propeller. This approval is considered inadequate for duplication in other aircraft. Limited to Commander Model 114 serial no. 14405.  Issued 6/8/2006
SA00241BO Installation of a Lycoming IO-580-B1A engine/Hartzell HC-C3YR-1RF/F7693F or HC-M3YR-1RF/F7693F propeller. Issued 7/27/2006
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
SA00246BO Installation of a Lycoming IO-540-T4B5 engine. Issued 12/4/2006
SA00249WI-D Installation of Bendix/King KFC 200 Automatic Flight Control System. For serial numbers 20003 20008 and above Reissued 2/28/2000
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 (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
SA00291BO Installation of a Lycoming IO-390-A1A6 engine and MT-Propeller MTV-12-B/188-59b propeller. Issued 11/12/2009
SA00302BO Installation of a Lycoming IO-390-A1A6 engine and MT-Propeller MTV-12-B/188-59b propeller Issued 7/2/2010
SA00306BO Change the horizontal stabilizer angle of incidence in accordance with Aerodyme Installation Instructions AD1225-01 Revision 1 dated December 15 2010 or later FAA approved revision. Issued 1/3/2011
SA00326BO Installation of a Hartzell HC-C3YR-1RF/F7693F or HC-C3YR-1RF/F7693F-1 propeller  Issued 10/5/2012
SA00356DE Installation of modified Textron Lycoming engine equipped with turbo normalizing system. Reissued 4/12/2012
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
SA00499SE Installation of a Hartzell HC-E3YR-1RF/F7392 propeller and C-3535-1(P) spinner. Amended 2/2/2002
SA00556WI Installation of a functioning TKS ice protection system. Reissued 7/8/2008
SA00680SE (5 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00769CH Installation of Champion Limited Authority Spark Advance Regulator (LASARTM) ignition system with Cylinder Head Temperature (CHT) monitoring capability on airframes with FAA approved installations of Textron Lycoming model IO-540 AEIO-540 and HIO-540 engines. Reissued 2/10/2009
SA00780SE (PAGE 4) 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
SA00817WI-D Installation of Bendix/King KFC 225 Automatic flight Control System. Reissued 2/28/2000
SA00847WI Installation of a dual/single Garbin GNS 430 GPS/COM/NAV System. Issued 1/3/2000
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00865SE Installation of vortex generators on the wings horizontal tail surfaces and vertical fin. Issued 1/9/2001
SA00893WI Installation of a Garmin GNS 530 VHF COM/NAV/GPS system. Issued 7/28/2000
SA00929WI Installation of Garmin Model GTX 327 transponder. Issued 12/1/2000
SA00954SE (2 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
SA01026SE (PAGE 1) Improved fuel gascolator assembly. Amended 12/19/2012
SA01085LA (PAGE 2) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
SA01105WI-D (2 OF 2) Installation of Bendix/King KMD 550/850 Multi-Functional Display System with optional traffic terrain and weather sensors. This STC applies to both single-engine and small multi-engine aircraft (see 1 of 2 for small twin-engine). Amended 5/31/2007
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
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
SA01224AT Installation of wheel hub cabs with valve stem access door. Amended 4/17/1998
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01240SE (4 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
SA01435DE Installation of engines modified with a Firewall Forward Technologies LLC modified camshaft into aircraft listed on the AML per Firewall Forward Technologies LLC Installation Instructions FFT-INI-001-AFR Rev. - dated 02/06/03 or later FAA approved revision. This installation must be done concurrently with STC SE01436DE which installs the modified camshaft to the engine.  Reissued 5/25/2011
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01437SE The manufacture of a Commander Sunvisor System in accordance with Rosen Sunvisor Systems Drawing List No. 1430000-DL Revision D dated );INSERT INTO stc_table VALUES ( July 19 2004 or later Federal Aviation Administration (FAA) approved revision. The sunvisor system must be installed and maintained in accordance with Rosen Sunvisor Systems Installation and Continued Airworthiness Instructions Document 9050-0143-001 Revision C dated June 29 2004 or later FAA approved revision.  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
SA01647WI Installation of the Elevator Spar Outboard Hinge Bracket Assembly on the Commander 112 series and 114 series aircraft in accordance with Harrison Aero Drawing List DL-HA1050 Revision IR dated August 23 2011 or later FAA approved revisions. Issued 10/14/2011
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 (2 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 2) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
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
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 (2 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
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
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
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
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
SA02183LA Installation of Door Gas Springs in accordance with FAA approved Master Drawing List FIV-1000 Revision B Amended 8/3/2011
SA02203AK (PAGE 2)  Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
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
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
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
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
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 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 1) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02795AT Installation of a PXE7300SR In-Flight Entertainment System Issued 2/12/2004
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
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA09195AC-D Installation of S-TEC System 55 Two Axis Automatic flight guidance system Model ST-658 with Optional Autotrim System. Amended 5/23/2001
SA09258AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-713-20/30. Amended 11/16/1998
SA09259AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-714. Amended 10/12/1998
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA09632AC Installation of the hydraulically controlled variable pitch 3-blade MTV-9-B/190-18b propeller in accordance with installation instruction No. E-551-E dated July 19 2002 or later FAA approved revision. FAA approved Airplane Flight Manual Supplement E-842-E dated September 29 2004 or later approved revision is required. Issued 10/4/2004
SA09832SC Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-658. Issued 10/31/2000
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 (1 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA10442SC  Installation of Chelton Aviation Corporation (CAC) AP-3C autopilot. Issued 9/12/2005
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1229CE Installation of King KFC-200 2 axis(3 optional) flight control system with KCS 55/55A compass and a KI-255 (or -256) flight command indicator or a KG-258 attitude horizon gyro with a KC-292 mode controller or stand alone electric trim. Reissued 2/28/2000
SA1245SO Installation of an adjustable trim tab on the left aileron. Issued 6/29/1981
SA1389GL Installation of Pamco emergency backup pneumatic system. (114A S/N 14350 AND AFTER) Issued 6/23/1989
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1502SW Mitchell automatic flight system AK364 consisting of Century I autopilot with optional omni tracker. Reissued 7/10/1984
SA1503SW Mitchell automatic flight system AK 363 consisting of Century IIB autopilot with optional radio coupler. Reissued 7/10/1984
SA1504SW Mitchell automatic flight system AK362 consisting of Century III autopilot with optional command/ electric pitch trim optional radio and glide slope couplers. Reissued 7/10/1984
SA1505SW Mitchell command/electric pitch trim system. Reissued 7/10/1984
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
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1728SW Cabin air scoop. Amended 3/14/1983
SA2190NM Page 2 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2350NM Page 2 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA237GL Install edge landing lights. Reissued 9/12/2005
SA243NW Installation of Lycoming IO-540 engine with 3-bladed Hoffman 3-bladed Hartzell or 2-bladed Hartzell propeller. Amended 11/1/1998
SA2586NM (PAGE 3) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2677CE Installation of aileron and flap gap seals per Horton-STOL Craft Drawing List #15 with an approval date of August 18 1994 or later FAA approved revision. Amended 7/30/2003
SA2683NM Installation of Precise Flight Inc. stand-by vacuum system (SVS) Amended 3/10/2005
SA2687NM (PAGE 2) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000 0:00
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
SA2900WE Installation of Pathfinder autopilots. Reissued 9/30/1998
SA3000SO Installation of Appalachian stainless steel brake discs No. 75-15A. Reissued 9/29/1995
SA3001SO Installation of Appalachian Accessories stainless steel brake discs P/N 75-43. Reissued 9/29/1995
SA300CE Installation of Woodward propeller governors on single and twin engine aircraft. (PA-31-325 modified per Colemill STC SA 970SO) Amended 5/14/1992
SA3120SW-D Mitchell automatic flight system AK572 consisting of Century I autopilot with optional omni tracker. Reissued 6/5/1984
SA3121SW-D Mitchell automatic flight system AK473 consisting of Century IIB autopilot with optional radio coupler. Reissued 6/5/1984
SA3122SW-D Mitchell automatic flight system AK574 consisting of Century III autopilot with optional radio and glide slope. Reissued 6/5/1984
SA3123SW-D Mitchell command electric trim system model AK582. Reissued 6/5/1984
SA3155WE Installation of Pathfinder autopilot systems and/or pitch trim systems. Reissued 9/30/1998
SA3308WE Modification of aileron control system by addition of aileron centering spring and installation of Pathfinder autopilot system and/or pitch trim systems. Reissued 9/30/1998
SA3531NM Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) Reissued 9/8/2010
SA3727WE Installation of Model CFS-1000 -1001 FT-100 or FT-101 fuel flow indicating system. Reissued 1/30/1998
SA3778WE Installation of retractable landing lights in accordance with Metal Magic Inc. Rockwell Model 112 and 114 Wing Light Installation Procedures dated April 24 1978. Fred W. Jones FAA Approved Airplane Flight Manual Supplement dated November 8 1978 is required. Reissued 12/18/2003
SA3787WE Installation of Model CFS-1000 -1001 FT-100 or FT-101 fuel flow ndicating system. Reissued 1/30/1998
SA3862NM Page 2 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA3920WE Installation of Fueltron IG or IP or Fuelgard digital fuel flow and totalizer system. Reissued 4/29/1991
SA4005NM (PG 3) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4172NM Installation of Aviation Development oil filter. Amended 5/22/2009
SA4302NM (PAGE 2) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA4444NM Installation of McCauley B3D34C405/90DFA-13 propeller. Issued 7/9/1982
SA4479NM Installation of FC/FT-10 digital fuel flow indicating system. Issued 6/20/1988
SA4531NM Replace 100 watt landing light with a 250 watt lamp. Reissued 1/25/2006
SA5154SW-D S-TEC System 60 two axis automatic flight guidance system ST-143 with optional automatic electric trim system. Amended 7/21/2000
SA5155SW-D S-TEC yaw damper system ST-145. Amended 7/23/1987
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
SA5167SW-D S-TEC System 60 pitch stabilizer system ST-144 with optional autotrim system. Amended 9/8/2000
SA5187SW-D S-TEC System 60 single axis automatic flight. Issued 7/29/1983
SA5202NM Installation of Avco-Lycoming engine model IO-360-C1D6 modified. Amended 3/6/1998
SA5283SW-D S-TEC System 40/50 single and two axis automatic flight guidance system ST-217-40/50. Issued 3/9/1984
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
SA5757SW Installation of Alcor tru-flow/ fuel flow/totalizer system. Amended 9/30/2002
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 (2 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
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
SA7063NM Installation of acrylic window liners in accordance with FAA approved Drawing Lists. Drawing lists are listed on FAA approved Model List Number SA7063NM or later FAA approved revision. Reissued 10/17/2008
SA7155SW-D Installation of S-TEC System 65 two axis automatic flight guidance system Model ST-420. Amended 4/9/1996
SA71GL Installation of air filters Reissued 6/20/2000
SA771GL Install nose gear shimmey dampener P/N 1001 to replace Gerdes P/N A135-8. Amended 9/12/1997
SA7801SW-D Installation of S-TEC manual electric trim system. Issued 7/16/1991
SA7816SW-D Installation of S-TEC System 65 two axis automatic flight guidance system Model ST-481. Issued 6/25/1992
SA7817SW-D Installation of S-TEC yaw damper system Model ST-482. Amended 8/9/1995
SA7820SW-D Installation of System 40/50 single and two axis automatic flight guidance systems Model ST-494-40/50. Issued 6/26/1992
SA7822SW-D Installation of System 60 two axis automatic flight guidance system Model ST-496 with optional automatic electric trim system. Issued 7/20/1992
SA7823SW-D Installation of S-TEC manual electric trim system Model ST-497. Issued 7/21/1992
SA7855SW Installation of McCauley B3D32C419/82NHA-5 propeller. Reissued 3/3/2006
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
SA8384SW-D Installation of S-TEC System 55/55X Two Axis automatic flight guidance system Model ST-527 with optional automatic electric trim system. Amended 10/31/2001
SA8431SW Installation of R15VON alternator control unit. Amended 1/6/1994
SA8521SW-D Installation of a Century Automatic Flight System Model YK1044 consisting of a Century yaw damper. Issued 3/31/2000
SA8534SW-D Installation of a Century Automatic Flight System Model AK1056. Amended 3/13/2003
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
ST01085LA (PAGE 2) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
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 (2 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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