Aero Commander 680 FL Grand

Number of Active Aircraft: 28 Active- Map


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Fuel Cost ($):
General Stats:
Seat Capacity: 7
Empty Weight: 5600 lbs
Max Weight 8500 lbs
Useful Load: 2900 lbs
Engine Name LYC IGSO-540-B1A
Engine Number 2
Horsepower 380 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 26500 ft
Max Fuel 223 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 211 kts
GPH (75% BHP): 38
MPG (75% BHP) 5.6
Range (75% BHP): 1122 nm
Fuel Cost Per Seat Mile 0.15 $
Fuel Cost Per Hour 228 $
MPG per 1000 lbs of Payload 16.1
F-T (Speed^2/FuelBurn) 11.7 HP
F-T Payload 33.9 kts
MPH To HP: 5.6 kts
T/O Roll - T/O over 50 FT OBST 1560 ft / 1740 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
SA00026WI New nose wheel spacer. Issued 2/9/1993
SA00051WI New nose landing gear scissor fitting. Issued 3/26/1993
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
SA00070WI Installation of Aero Commander690 windshield. Issued 6/10/1993
SA00079NY Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Amended 10/31/2012
SA00098SE Installation of emergency medical stretcher oxygen and electrical systems. Reissued 10/24/2013
SA00105SE Modify Flap Pulleys. Reissued 6/17/1999
SA00111WI New main landing gear scissor fittings. Issued 10/28/1993
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
SA00189SE Reduction in maximum takeoff gross weight to 9 985 lbs. (695 S/N 95070) Issued 4/10/1995
SA00212AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/17/1994
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
SA00354AT Installation of Garrett TPE331-5-511 engines. Reissued 10/20/1999
SA00481DE Installation of an Aircraft Noise Control (ANC) System. Issued 9/25/2002
SA00534SE Replacement of certain BF Goodrich pneumatic deicer boots Reissued 5/4/2000
SA00596CH Installation of Elliott Aviation Sound Management system. Issued 12/20/1996
SA00674WI-D Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II system installation. Amended 7/23/2012
SA00681WI-D Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation  Reissued 1/25/2011
SA00729SE Installation of twin temperature indicating system with fuel flow in accordance with J.P. Instruments (JPI) Installation manual Report No. 760 Revision - dated 7/20/99 or later FAA approved revision. Amended 11/30/2005
SA00770SE Installation of two (2) Hartzel Model HC-B3Z20-2A/10151(B)-8(R) or two (2) HC-93Z20-2C/10151(B)-8(R) propellers on the above model aircraft per James Metzger Amended 6/24/2004
SA00775NY Install equipment rack. Issued 12/15/1997
SA00794CH Replace Twin Commander fuel cap assembly with Shaw Aero Devices Fuel Cap (P/N 416-50) and adapter (P/N 416-938). Amended 8/10/2009
SA00804SE Installation of an engine failure indicator system also referred to as a low Thrust Detector system.  Amended 7/16/2000
SA00812NY Installation of Technisonic Industries Limited TFM-138 A and B (does not include TFM-138 s/n 1540 and up TFM-138B s/n 1500 and up). Amended 9/12/2005
SA00823CH Installation of various de-icer wire harnesses. Reissued 10/10/2002
SA00849AT Installation of a Bendix/King EFIS. Amended 6/18/1999
SA00884NY Installation of an Aerosening Terrain Mapping Radar System. Reissued 1/27/1999
SA01005SE Installation of replacement door hinges and support hardware. Issued 10/3/2001
SA01073SE Increase maximum ramp weight to 11 050 lbs. Amended 3/25/2005
SA01078SE Installation of externally mounted fuel pump manufactured in accordance with Master Drawing List AEA105-90 Revision A dated April 5 2002 or later FAA approved revision and installed in accordance with Installation Instructions VT-AEA105-12 Revision IR dated April 5 2002 or later FAA approved revision. Maintain in accordance with Instructions for Continued Airworthiness AEA-105-13 Revision IR dated April 5 2002 or later FAA approved revision. Issued 4/17/2002
SA01085LA (PAGE 2) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
SA01102CH Installation of AlliedSignal Inc. TPE331-5-251K Model Engines. Issued 8/25/1999
SA01141WI-D Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94 Mode S Transponder System installation with CTL-92E control head. Amended 5/24/2006
SA01143NY Installation of an Aerosensing Terrain Mapping Radar antenna System. Limited to installation on serial number 96085 ONLY. Reissued 5/15/2006
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01170NY Installation of NPX138N-XXX FM Transceiver. Amended 1/17/2007
SA01229SE Page 2 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01289CH Installation of McCauley 4HFR34C665/L106FRA-2 model propeller E-7155 spinner and de-ice system. Reissued 7/19/2006
SA01306WI-D Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation. Amended 2/28/2007
SA01444AT Installation of an Enviro Systems AirConditioner. Amended 6/10/1999
SA01452CH Installation of an air ambulance conversion kit. Amended 3/27/2013
SA01473SE (4 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
SA01586SE Group aircraft approval for Reduced Vertical Separation Minimum (RVSM).  Amended 1/9/2009
SA01620SE Installation of emergency medical equipment. Reissued 1/19/2010
SA01626CH Installation of a Meggitt Avionics Engine Instrument Display System (EIDS). Reissued 7/9/2007
SA01627CH Installation of a Meggitt Avionics Electronic Flight Instrument System (EFIS). Reissued 7/9/2007
SA01660CH Remove Janitrol P/N C15C54 or Twin Commander P/N 88035-5 combustion heater and install C & D Associates Model CD35K heater kit 10 P/N 12043K10. Issued 6/24/2002
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
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 2) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
SA01762SE Fabrication and Installation of Fuel Quantity Indication System. Reissued 11/12/2009
SA01787AT Installation of Brake and Rudder pedal extension. Issued 1/15/1999
SA01788AT Installation of Windshield sunscreens for pilot and copilot. Issued 1/15/1999
SA01789AT Installation of pilot and copilot frameless vent windows. Issued 1/15/1999
SA01790AT Installation of Split Engine Bowl. Issued 1/15/1999
SA01791AT Installation of Tinted Passenger Windows. Issued 1/15/1999
SA01800SE (PG 4) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01820AT Installation of Exhaust Deflectors. Issued 2/19/1999
SA01828SE Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System Reissued 5/12/2011
SA01861SE (PAGE 3)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01861SE (PAGE 5)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01877SE Installation of SAGEM Multi-function Display Systems as Primary Flight Displays (PFD) Multi-function Displays (MFD) and Engine Monitoring System (EMS) Reissued 10/2/2012
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 (5 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01956AT-D Installation of replacement fuel cell assemblies Reissued 5/5/2009
SA01969SE Installation of a Mid-Continent MD302 Standby Attitude Module Issued 1/17/2014
SA01988SE (PAGE 4) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02005NY Installation of SMR Technologies pneumatic deicer models. Amended 2/3/2006
SA02013CH Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). Amended 5/2/2011
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 6) 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
SA02075SE Installation of a Mid-Continent MD835( ) Lithium Ion Battery Amended 2/28/2013
SA02110CH (PAGE 4) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02119CH Installation of C&D Associates Combustion Heater Kit 17 P/N CD14045K17 in accordance with C&D Associates heater Installation Instructions IN14045K17 Rev. none dated February 3 2005 or later FAA approved revision. Issued 3/10/2005
SA02119SE Page 2 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02120CH Installation of C&D Associates Combustion Heater Kit 18 P/N CD14046K18 in accordance with C&D Associates heater Installation Instructions IN14046K18 Rev. none dated February 3 2005 or later FAA approved revision. Issued 3/10/2005
SA02153LA-D (Page 2) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
SA02154AK (PAGE 2) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005 0:00
SA02203AK (PAGE 1) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
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 (3 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
SA02254AK Installation of Single Screen Amended 11/7/2011
SA02265SE Installation of a camera housing Amended 11/1/2013
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
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 3) Installation of a Voice Alert System. Amended 8/28/2007 0:00
SA02564CH Installation of a Bendix/King EFS-50 Electronic Flight Instrument System Issued 5/22/2008
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
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA03273AT Installation of an air conditioning and pressurization system Peter Schiff Aero Amended 2/19/2010
SA09013AC-D Installation of S-TEC System 65 two axis automatic flight guidance system Model ST-590. Amended 9/21/1999
SA09014AC-D Installation of S-TEC yaw damper system Model ST-591. Amended 5/7/1999
SA09046SC Installation of replacement wing fuel cell bladders P/N DF308-1 & -2. Reissued 7/31/2002
SA09047SC Installation of replacement wing fuel cell bladders. Reissued 7/31/2002
SA09048SC Installation of replacement wing fuel cell bladders. Reissued 7/31/2002
SA09163AC-D Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-634-40/50. Issued 8/16/1996
SA09247AC Replace the engine exhaust ejector assembly P/N 260042-55 LH &-56 RH with a heavier gauge ejector which has a modified fairing. Reissued 11/9/2009
SA09527AC-D Installation of DFCS 01284 (MAGIC 2100) Autopilot System Model ST-902. Reissued 1/9/2008
SA09548AC-D Installation of S-TEC/Chelton CA370S Air Data Attitude Heading Reference System (ADAHRS)  Issued 8/25/2008
SA09628AC-D Installation of S-TEC 01298 or 01304 Digital Flight Control System (DFCS) Amended 8/25/2008
SA09628AC-D 1. Installation of S-TEC 01298 or 01304 Digital Flight Control System (DFCS) in according with Master Data List 921128 Rev. 11 dated 3-16-11 or later FAA Approved revisions of the above data. Reissued 3/21/2011
SA1-142 Modified ARC A13-B antenna. Issued 
SA1-143 Installation of Chamberlain 2001X series radome kits. Reissued 7/6/2005
SA1-231 Bendix fuel flow indicating system. Issued 
SA1-249 Fuel flow indicating system. Issued 
SA1-300 Bendix fuel flow indicating system. Issued 
SA1-385 Installation of BFGoodrich lightweight reservoir type pneumatic de-icing system. Reissued 3/1/1996
SA1-442 ANC-3A computer and ANO-C2 or ANC-D2 controller with Lear L2C autopilot. Amended 
SA1-445 ARC Type A13-B VHF navigational antenna on vertical fin. Amended 
SA1-476 SP-3 autopilot EB2597034. Amended 
SA1-520 Electrothermal propeller deicing system. Reissued 3/1/1996
SA1-525 ARC A13-B antenna on vertical fin with rotating beacon. Amended 
SA1-552 Pesco 2 P-R400-BRD fuel pumps. Amended 1/1/1996
SA1-553 Lightweight reservoir type pneumatic deicing system. Reissued 3/1/1996
SA1-624 Oxygen system. Amended 1/1/1960
SA1-653 Electrothermal propeller deicing system. Reissued 3/1/1996
SA1-68 Dual Wilcox ADF radio loop antenna. Issued 1/1/1960
SA1-83 Camera in fuselage tail section. Issued 1/1/1960
SA1-93 RCA AVQ-50 radar equipment and AVQ-50 antenna mounting bracket. Issued 1/1/1961
SA1005CE Installation of AID battery temperature monitor and over- temperature warning system. Reissued 2/11/1993
SA1007NW Installation of a low thrust detector system. Reissued 3/6/1998
SA1009CE ONE ONLY STC SN # 11138: Installation of King Model KFC 300 Automatic Flight Control System (autopilot and flight director). Reissued 2/28/2000
SA1011CE Install Model KVN-395 vertical navigation computer for operation with Model KFC-300 automatic flight control system. Reissued 2/28/2000
SA1017EA Installation of vertical tail floodlights. (680-F INCLUDES PRESSURIZED VERSIONS) Amended 10/29/1984
SA10236SC (3 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA1024SO Installation 7of AiResearch TPE331-5-252K engines replacing AiResearch TPE331-5-251K engines. Reissued 7/8/1985
SA10284SC Installation of a right side Meggitt EFIS i.e. Primary Flight Display (PFD) Navigation Display (ND) and Air Data Attitude Heading Reference System (ADAHRS). Reissued 7/9/2007
SA102EA Pump type pneumatic deicing system. Reissued 3/1/1996
SA102GL Installation of baggage compartment. Reissued 1/4/1983
SA10392SC Installation of a dual Innovative Solutions & Support (IS&S) Altimeter System.  Reissued 3/31/2005
SA10439SC Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot.  Issued 8/4/2005
SA1059SO Replace existing nickel-cadmium batteries with Teledyne Gill BB638/T series lead-acid batteries. Reissued 4/29/1996
SA1064SW Wild RC-8 aerial survey camera. Issued 8/8/1969
SA1080CE Installation of Collins Radio Group AP-107 autopilot system. Issued 3/1/1975
SA1089SW Installation of 59 gallon wing auxiliary fuel tank according to Drawing List 60400 dated 10/5/69 revised 5/1/70. );INSERT INTO stc_table VALUES (  Reissued 4/16/2005
SA1094SW RD-8 RC-9 and RMK-A-15/23 camera. Issued 1/1/1960
SA1095SW Installation of Bendix ANA-12A. Issued 1/1/1961
SA1122SW Dual cameras and navigation sights. Issued 1/1/1961
SA1125SW Aerial survey camera and navigation. Issued 3/2/1970
SA1130CE Installation of Collins Radio Group electric trim system. Issued 4/1/1975
SA1135SW Modification of fuselage for installation of Bendix ANA-12 doppler antenna. Issued 3/30/1970
SA114CE Windshield anti-ice system. Issued 1/1/1960
SA1155WE Camera. Issued 1/1/1960
SA115EA Pump type pneumatic deicing system. Reissued 3/1/1996
SA1177GL Install Aero Medical Products Mfg. Inc. Air Ambulance Stretcher P/N 125 using Installation Kit P/N 800 in accordance with Installation and Operating Instructions Form EA 109K dated April 23 2001 or later FAA approved revisions. The Medical Oxygen System Kit P/N 807 is an FAA approved option. The Inverter/Pump Kit No. 812 may be installed in accordance with Inverter/Pump Installation Instructions EA Form 170 dated June 9 2001 or later FAA approved revisions. Amended 3/29/2004
SA1182SW Dual camera and navigation sight. Issued 8/19/1970
SA1184NW Installation of Hartzell HC-B3TN-5/T10178E-13Q );INSERT INTO stc_table VALUES ( propellers on AiResearch Model TPE-331-43 series engines. Amended 6/30/2005
SA1204CE Installation of two 50 gallon slipper type fuel tanks. (680FL SN 1349-29 only) Reissued 10/8/2010
SA1205NW Installation of a digital Electronics International exhaust gas temperature (E.G.T.) gauge (P/N ET-1). Amended 12/8/2006
SA120CE Windshield anti-ice system. Issued 1/1/1960
SA1261SW Camera installation. Reissued 7/24/2012
SA1262GL Install supplement air scoop over the air cycle machine inlet. Amended 3/25/1988
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
SA132EA Install electrothermal propeller deicing system. Reissued 3/1/1996
SA1332SW Modify fuselage for camera and navigation sight. Issued 6/24/1971
SA133CE Installation of windshield wiper. Reissued 1/31/1997
SA1358SW Dual or single camera installation and navigation sights. Issued 8/25/1971
SA1359GL Install winglet wingtips. Reissued 9/13/1999
SA135EA Installation of engine exhaust combustion monitor. Reissued 2/14/1972
SA137CE Lower window line in cabin area. Issued 1/1/1960
SA1381GL Replace standard wing tip assembly with winglet tip assembly. Reissued 9/13/1999
SA13WE M-4 autopilot. Amended 2/24/1967
SA1440SW Separation of hydraulic pump seal drain from engine drain manifold. Reissued 9/4/1992
SA1454WE Installation of Brittain Model B-4A flight control system. Issued 1/1/1960
SA1457SW Modification of pressurization and air conditioning system. Reissued 6/19/1986
SA1458GL Installation of a Cleveland nose wheel. Issued 3/15/1990
SA1464NM Installation of Hartzell HC-B3TN-5NL/LT propellers on TPE331-5-252K engines (installed per STC SA1024SO) and AiResearch TPE331-5-251K and TPE331-5-254K engines. Amended 1/14/2004
SA1475SW Installation of taxi lights. Reissued 6/26/2001
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1529SW Modification of hydraulic system and air conditioning pressurization system. Issued 7/25/1973
SA1530SW Modify existing 3000 psi hydraulic system to 1000 psi hydraulic system. Issued 12/23/1972
SA155CE Intallation of Honeywell H-14 adaptive autopilot. Issued 1/1/1960
SA155RM Installation of Singer SKK-1000 doppler navigation system SKQ-601 dead reckoning computer and Sperry C-12 compass system. Reissued 3/7/2002
SA1565GL Installation of flap gap wing fairings. Reissued 9/13/1999
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1580WE Installation of Brittain Model B-5 flight control system. Issued 1/1/1960
SA1584SW Single and dual camera installations navigation sight installations drop port installation and emergency exit and door optical glass installations for oblique cameras.  Reissued 6/15/2005
SA1589NM Installation of dual accessory power outlets.  Amended 6/18/1985
SA1606SW Installation of Microcom battery temperature indicator system and battery isolation system. Reissued 6/19/1986
SA1611NM Installation of Hartzell propellers on AiResearch engines Issued 4/16/1982
SA1613CE Installation of Avcon stretcher. Reissued 8/21/1990
SA1649SW Camera installation. Issued 5/1/1973
SA164EA Airborne profile recorder probe on nose of fuselage. Issued 1/1/1960
SA1675WE Installation of exhaust gas temperature monitoring systems EGT-2. Amended 8/28/1974
SA1685NM Installatino of EASY TAXI Brake System Amended 5/9/1984
SA1686WE Installation of Vibration Isolation Products (VIP) engine mount P/Ns VIP 50525-1 and VIP 50545-1 on various aircraft as shown on FAA Approved Model List (AML) No. SA1686WE. Amended 10/17/2002
SA1705SW Installation of freon air conditioning system. Reissued 6/26/2001
SA1730SW Installation of aileron trim tab. Reissued 9/4/1992
SA1782WE Installation of drooped ailerons drooped wing leading edge stall fence and rudder seal. Reissued 9/8/2005
SA179EA Installation of electrothermal propeller deicing system. Reissued 3/1/1996
SA17GL Installation of Bendix FCS-810 autopilot. Issued 4/12/1973
SA1815SW Installation of AiResearch TPE331-1-151 engine. Reissued 6/26/2001
SA1847WE Installation of Brittain Up-Command Signal Adapter Kit. Reissued 10/20/1972
SA1873SW Installation of Sperry SPZ-200/STARS IVC. Reissued 7/13/2012
SA1876SW Installation of Collins Radio AP-106 autopilot and manual electric trim. Reissued 4/24/2000
SA1926SW Fuel purge system. Reissued 9/4/1992
SA1962SW Installation of generator over- current protection. Reissued 9/4/1992
SA1977SW Modification of fuselage for installation of doppler antenna. Issued 5/6/1975
SA199SW Four auxiliary fuel cells in each outer wing panel between wing stations 127 and 163. Issued 1/1/1960
SA2-22 Install 2 each 3/8 O.D. lines from LH nacelle to RH firewall. Reissued 8/31/2000
SA2-26 Installed 3/8 O.D. line from RH propeller governor pad on RH engine to LH propeller pad on LH engine. Reissued 8/31/2000
SA2-67 Install Eclipse Pioneer fuel flow indicating system. Reissued 8/31/2000
SA2-75 Revised and installed new electrical components. Reissued 8/31/2000
SA2-884 Installation of Collins AP-102 autopilot. Reissued 4/24/2000
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA2221CE Install cargo restraint system. Issued 1/13/1987
SA2282SW Installation of auxiliary battery in aft cabin with rerouting of control system cables. Amended 9/4/1992
SA2304CE Install cargo restraint and cargo provisions. Amended 8/1/1989
SA2308CE Installation of single GIll G-24724-volt battery. Issued 12/9/1987
SA231CE Twin engine synchronizer. Reissued 4/30/2007
SA236CH Installation of Allied Signal Inc. (Garrett) TPE331-10T series engines (-512K -515K or -516K in the 690A and 690B -511K or -513K in the 690C and 690D) and related changes. Reissued 11/12/2009
SA2380NM Installation of two Hartzell Model HC-B3TN-5FL/LT10876S-2Q propellers on aircraft equipped with two AiResearch TPE-331-10-501K Turboprop engines. Amended 4/6/2005
SA240CE Installation of Woodward propeller unfeathering accumulator kit #213315. Issued 1/1/1960
SA2415SW Modifications: cargo and baggage door installations cockpit crew door revised air conditioning and oxygen systems. (See Limitations) Reissued 6/19/1986
SA2439SW Installation of 690B dorsal fin and tailcone assembly. Reissued 9/4/1992
SA2448SW Extension of baggage area to F.S. 308 encompassing re-routing of powerplant and aileron control cables in baggage compartment area. Issued 4/7/1977
SA250CE Installation of Woodward electronic propeller synchraphaser system. Reissued 4/30/2007
SA2557NM (1 OF 2) Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. Amended 2/22/2007
SA2569WE Installation of battery temperature monitor system. Reissued 3/24/1976
SA256WE Control wheel replacement. Issued 1/1/1960
SA2577WE Installation of flight FCS-105 flight control system. Amended 8/14/1978
SA2586NM (PAGE 3) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA258SW Camera and camera view finder opening in main cabin floor of 30-inch x 39-inch maximum dimension. Issued 6/5/1970
SA2606WE Installation of Lear AFC-70 autopilot. Amended 7/20/1973
SA260SW Installation of a Protective Device in the ground side of the Battery and External Power relays Reissued 11/12/2009
SA265EA Installation of Chamberlain radome kit #2001K-B for use with Bendix radar RDR-100 or RDR-110. Amended 3/11/1970
SA2691WE Installation of Lycoming IO-720-B1B or  Reissued 4/16/2008
SA26GL Installation of Bendix M-4C autopilot. Issued 7/2/1973
SA2704CE Installation of Phoenix P/N GC-1010-24-3B I DC generator control. Amended 3/26/1992
SA2705CE Installation of Phoenix voltage regulator. (690A 11100 thru 11226) Amended 10/10/1991
SA2725NM Installation of an emergency medical evacuation system. Reissued 12/2/1985
SA2727WE Installation of LearAvia electric pitch trim system. Issued 7/20/1973
SA274NW Replacement of the left forward side window (pilots compartment) with a plexiglas dome (0.250 in. thickness) Issued 4/5/1976
SA278GL Installation of Cleveland Kit No. 199-74. Reissued 10/28/1980
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA2891WE Installation of Lycoming IO-720-B1B turbocharged engine. Reissued 4/16/2008
SA2903SW Installation of wing flap gap seals. Amended 2/7/1995
SA290GL Install Cleveland conversion kit No. 199-74 on listed models which use MIL-H-5606 brake fluid (red oil) or kit No. 199-74A on listed models which use Skydrol brake fluid (nonpetroleum base). Reissued 10/28/1980
SA290SW Installation of RC-9 aerial survey camera. Reissued 7/13/2012
SA29SW Auxiliary outboard fuel tank. Amended 4/23/2002
SA2EU Cargo door modification Issued 1/1/1960
SA3-112 Oil separators in vacuum pump outlet lines. Issued 1/1/1960
SA3-118 Installation of A.R.C. type A-13B navigational antenna. Reissued 6/22/1983
SA3-120 Relocation of aircraft battery to hose station 8. Reissued 6/30/1983
SA3-145 AP-101 automatic pilot. Issued 1/1/1960
SA3-259 Collins glide slope VOR navigation and VHF communications antenna Aircraft Radio Corp. ADF antenna and Grimes rotating beacons. Issued 1/1/1960
SA3-301 Hand-operated hydraulic pump deactivated or removed and replaced with electric-driven equivalent. Issued 1/1/1960
SA3-32 AP-101 automatic pilot. Issued 1/1/1960
SA3-349 Bendix fuel flow indicator system. Issued 1/1/1960
SA3-350 AP-11 automatic pilot. Issued 1/1/1960
SA3-406 Installation of AVQ-50 radar. Reissued 5/27/1983
SA3-721 Cabin temperature control system with Janitrol S-25 heater. Issued 1/1/1960
SA321EA Install wheels P/N 301174 P/N s2-993 and/or 2-1107. Reissued 9/4/1974
SA3299SW-D Mitchell automatic flight system AK772 consisting of Century III autopilot with optional radio and glide slope couplers. Reissued 3/29/1984
SA3300SW-D Mitchell automatic flight system AK773 consisting of Century IV autopilot consisting of Century IV flight director autopilot with optional remote annunciator. Reissued 9/21/1983
SA3322WE Installation of cockpit overhead windows. Reissued 5/10/1989
SA3336NM Cockpit Sun Visor installation in accordance with FAA approved Rosen Drawing List Number RAC-00DL dated January 7 1986 or later FAA approved revision. Reissued 3/24/2003
SA337GL-D Installation of AiResearch TPE331-1-151-K engines. Amended 8/27/1980
SA3405WE Installation of fuselage fuel tank in accordance with MR. RPM Top Drawing 57031 Revision E dated May 16 1977 or later FAA approved revisions. Reissued 11/7/2008
SA3469WE Installation of AiResearch TPE 331-6-252M engines. Amended 2/27/1978
SA3477WE Replacement installation of tail cone assembly. Reissued 12/7/1988
SA3493WE Replacement installation of vertical tip assembly. Reissued 12/7/1988
SA3517WE Installation of cockpit overhead windows. Issued 12/23/1977
SA3765SW Structural provisions for camera and navigation sight. Reissued 6/5/2012
SA37CE C210403 governor. Issued 1/1/1960
SA3849WE Installation of Fueltron IIIG or IIIP digital fuel flow and totalizer system. Reissued 4/29/1991
SA3861NM Installation of two Hartzell HC-B3TN-5FL/LT10876ANSB-2Q propellers on the above Twin Commander airplanes equipped with two AiResearch Model TPE331-5-24K or two Model TPE331-10T-511K -112K -113K -515K -516K engines. Amended 6/17/1999
SA38CE B21043 governor. Issued 1/1/1960
SA391EA Turbine bleed type pneumatic deicer system. Issued 1/1/1960
SA395SW Four-place seating capacity. Issued 1/1/1960
SA396SW Automatic pilot AK118 lateral guidance radio coupler AK123 and pitch trim AD135. Issued 1/1/1960
SA39CE C210310 governor. Issued 1/1/1960
SA4-1234 Installation of electrical low fuel warning device to indicate last 25 gallons of useable fuel in main (center) tank. Reissued 3/10/2009
SA4-1382 L2-C autopilot. Issued 1/1/1960
SA4-1442 Installation of collins AF-102 Autopilot. Reissued 11/18/1999
SA4-1579 Aerofilter 30690B full flow lube oil filter with element 1A0286. Issued 1/1/1960
SA4-1655 Outer wing non-icing fuel tank vent fairings. Issued 1/1/1960
SA4-240 Electric hydraulic pump. Issued 8/6/2007
SA4-443 Fiberglas wing tips. Reissued 11/4/1970
SA4-447 Fiberglass wing tips. Reissued 11/4/1970
SA4-454 Installation of fiberglass vertical stabilizer cap in lieu of metal repositioning of rotating beacon mounting to leading edge reduction of length of the two spar extensions to facilitate VHF antenna installation inside stabilizer cap area. Reissued 11/4/1970
SA4-455 Hamilton Standard governors IM12-G5. Issued 1/1/1960
SA4-530 Radio rack aft of baggage compartment. Issued 1/1/1960
SA4-551 L-102B automatic pilot. Issued 1/1/1960
SA4-989 Aerofiter 30690B full flow lube oil filter with element 1A0286. Issued 1/1/1960
SA4005NM (PG 1) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA404CE Installation of Hoskins supplemental position light system which includes Model A wing tip lights and Model D or K(dual) tail light. Reissued 9/30/2011
SA405GL Installation of a Collins LRN 70 omega navigation system. Issued 5/13/1980
SA408SW Installation of an RC-8 aerial survey camera. Reissued 7/13/2012
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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