# Gulfstream Aerospace 695A - Type: Aircraft model (FAA registry) - Registry code: 3970600 - Manufacturer (registry): GULFSTREAM AEROSPACE - Model: 695A - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 11 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS 2A4](https://openairdocs.org/tcds/2A4) (OpenAirDocs) - Holder: Twin Commander Aircraft LLC - Registered aircraft: 2 - Page: https://openairdocs.org/model/gulfstream-aerospace-695a Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008 - [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 2003-07-03](https://openairdocs.org/ad/2003-07-03): Wing and fuselage structure · Twin Commander 690D, 695A and 695B. Effective May 16, 2003 - [AD 2000-02-30](https://openairdocs.org/ad/2000-02-30): Airframe Pneumatic Deicing Boots · Twin Commander 680, 680-E, 680-F and 15 more. Effective Mar 24, 2000 - [AD 98-08-25 R1](https://openairdocs.org/ad/98-08-25-R1): Nose Landing Gear (NLG) Drag Link Bolt · Twin Commander 500-S, 500-U, 680-F and 9 more. Effective Jan 5, 1999 - [AD 98-20-34](https://openairdocs.org/ad/98-20-34): Airplane Flight Manuals--Severe Icing Conditions · Twin Commander 500, 500-A, 500-B and 24 more. Effective Nov 3, 1998 - [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998 - [AD 98-07-17](https://openairdocs.org/ad/98-07-17): Flap System · Twin Commander 500, 500-A, 500-B and 27 more. Effective May 29, 1998 - [AD 98-08-19](https://openairdocs.org/ad/98-08-19): Wing to Fuselage Attachment Brackets and Straps · Twin Commander 500, 500-A, 500-B and 27 more. Effective May 18, 1998 - [AD 95-19-18](https://openairdocs.org/ad/95-19-18): Turbulent Air Penetration and Maneuvering Speeds · Twin Commander 680-T, 680-V, 680-W and 9 more. Effective Oct 25, 1995 - [AD 95-13-02](https://openairdocs.org/ad/95-13-02): Twin Commander 685, 690, 690A and 5 more. Effective Jul 22, 1995 - [AD 87-24-07 R1](https://openairdocs.org/ad/87-24-07-R1): POH/AFM Revision - Icing · Twin Commander 690, 690A, 690B and 5 more. Effective Feb 9, 1988 - [AD 84-19-05](https://openairdocs.org/ad/84-19-05): Engine Mount Systems · Twin Commander 690, 690A, 690B and 4 more. Effective Oct 8, 1984 - [AD 79-07-02](https://openairdocs.org/ad/79-07-02): Batteries · Aircraft Parts & Development A, A-2, A-3 and 149 more. Effective Apr 3, 1979 Historical (superseded or no longer in force): - [AD 98-08-25](https://openairdocs.org/ad/98-08-25) (historical): Nose Landing Gear (NLG) Drag Link Bolt · Twin Commander 500-S, 500-U, 680-F and 9 more. Effective May 18, 1998 - [AD 96-12-08](https://openairdocs.org/ad/96-12-08) (historical): Nose Landing Gear (NLG) Drag Link Bolt · Twin Commander 500-S, 500-U, 680-F and 8 more. Effective Jun 27, 1996 - [AD 94-04-17](https://openairdocs.org/ad/94-04-17) (historical): Flap System Cable · Twin Commander 500, 500-A, 500-B and 27 more. Effective Apr 15, 1994 ## Information bulletins (advisory) (1) - [SAIB 2023-14](https://openairdocs.org/saib/2023-14): Landing Gear Retract/Extend System. Issued Nov 14, 2023 ## Registered aircraft (2) - [N695MM](https://openairdocs.org/aircraft/N695MM): [M8 Aviation LLC](https://openairdocs.org/faa-owner/M8%20AVIATION%20LLC), [Raleigh, NC](https://openairdocs.org/faa-place/NC/Raleigh), built 1982, S/N 96050 - [N95AB](https://openairdocs.org/aircraft/N95AB): [Ridgeaire Inc](https://openairdocs.org/faa-owner/RIDGEAIRE%20INC), [Jacksonville, TX](https://openairdocs.org/faa-place/TX/Jacksonville), S/N 96012 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20070712016939I](https://openairdocs.org/incident/20070712016939I), Jul 12, 2007: Gulstm 695A (N695GG), Lexington, KY, No damage. (-23) While operating at FL320 the pilot of N695GG noticed fumes coming from the aircraft environmental system. A similar problem had occurred in this aircraft… ## Service difficulty reports (37) As reported by operators and repair stations, by the model named in the report. - [SDR CA110430001](https://openairdocs.org/sdr/CA110430001), Apr 30, 2011: ISOLATOR. CORRODED. (CAN) DURING SCHEDULED 3600 HOUR REPLACEMENT OF ENGINE ISOLATORS, ISOLATOR WAS FOUND CORRODED ONCE REMOVED FROM THE AIRCRAFT. THE MOUNTING DESIGN OF THE ISOLATO - [SDR CA090922004](https://openairdocs.org/sdr/CA090922004), Sep 21, 2009: LINE. OBSTRUCTED. (CAN) THE TUBE THAT SUPPLIES PRESSURIZED AIR FROM AIRFRAME SYSTEMS TO INFLATE THE ENTRANCE DOOR SEAL BECOMES KINKED. (SEE ATTACHMENT)THE TUBE COMES FROM UNDER T - [SDR CA071022005](https://openairdocs.org/sdr/CA071022005), Oct 18, 2007: BOLT. CRACKED. (CAN) DURING DISASSEMBLY OF NOSE LANDING GEAR FOR ITS 5 YEAR INSPECTION/OVERHAUL, BOLT P/N 750076-1 OF THE NOSE LANDING GEAR DRAG BRACE-NOSE LANDING GEAR STRUT - [SDR CA070918007](https://openairdocs.org/sdr/CA070918007), Sep 17, 2007: BULKHEAD. CRACKED. (CAN) DURING WINTER MAINTENANCE, REAR NACELLE BULKHEAD FOUND CRACKED IN THE RADIUS. BULKHEAD TO BE REPLACED. (TC NR 20070918007) - [SDR 2006FA0000572](https://openairdocs.org/sdr/2006FA0000572), May 19, 2006: BOLT. SHEARED. DURING LANDING GEAR EXTENSION ON APPROACH, (GEAR IN TRANSIT) LIGHT REMAINED ON, NLG DID NOT INDICATE DOWN AND LOCKED. INITIAL FLY BYS INDICATED NLG TO BE ONLY P - [SDR 2006FA0000069](https://openairdocs.org/sdr/2006FA0000069), Jan 11, 2006: ANGLE. MISLOCATED. JOGGLE IN PART NEEDS TO BE RELOCATED .2500 INCH FURTHER FROM NEAR END OF ANGLE IN ORDER TO HAVE SUFFICIENT ED TO FASTENER. (K) - [SDR 2006FA0000068](https://openairdocs.org/sdr/2006FA0000068), Jan 11, 2006: ANGLE. MISLOCATED. JOGGLE IN PRAT NEEDS TO BE RELOCATED .2500 INCH FURTHER FROM NEAR END OF ANGLE IN ORDER TO HAVE SUFFICIENT ED TO FASTENER. (K) - [SDR 2006FA0000067](https://openairdocs.org/sdr/2006FA0000067), Jan 11, 2006: ANGLE. MISLOCATED. JOGGLE IN PART NEEDS TO BE RELOCATED .2500 INCH FURTHER FROM NEAR END OF ANGLE IN ORDER TO HAVE SUFFICIENT ED TO FASTENER. (K) - [SDR 2006FA0000066](https://openairdocs.org/sdr/2006FA0000066), Jan 11, 2006: ANGLE. MISLOCATED. JOGGLE IN PART NEEDS TO BE RELOCATED .2500 INCH FURTHER FROM NEAR END OF ANGLE IN ORDER TO HAVE SUFFICIENT ED TO FASTENER. (K) - [SDR 2004FA0000551](https://openairdocs.org/sdr/2004FA0000551), Jun 6, 2004: STATOR. DAMAGED. DURING ENGINE START THE OPERATOR OBSERVED SMOKE EXITING THE ENGINE EXHAUST DUCT. THE OPERATOR SHUT THE ENGINE DOWN. VISUAL INSPECTION REVEALED OIL AND IMPACT DA - [SDR FTU2003F00011](https://openairdocs.org/sdr/FTU2003F00011), Apr 24, 2003: COLLAR. LOOSE. DURING A NORMAL PERIODIC INSPECTION, BOTH LEFT AND RIGHT ELEVATORS WERE FOUND LOOSE. CLOSER INSPECTION REVEALED WORKING RIVETS WHICH HOLD COLLARS (PN 440000-246 - [SDR FTU2003F00010](https://openairdocs.org/sdr/FTU2003F00010), Apr 24, 2003: ARM. CRACKED. DURING A NORMAL PERIODIC INSPECTION, WHILE INSPECTING UNDER THE BAGGAGE COMPARTMENT FLOOR, THE ELEVATOR BOB WEIGHTS ARE BOLTED TO CRACKS WERE FOUND AROUND THE B - [SDR FTU2003F00009](https://openairdocs.org/sdr/FTU2003F00009), Apr 24, 2003: PIN. SCORED. DURING A NORMAL PERIODIC INSPECTION IT WAS DISCOVERED THAT THE TAPERED PINS WHICH RETAIN THE MLG HOUSING SUPPORT PINS HAD INCORRECT HARDWARE (PLAIN WASHERS UNDE - [SDR FTU2003F00003](https://openairdocs.org/sdr/FTU2003F00003), Feb 14, 2003: REGULATOR. FAILED. HYDRAULIC REGULATOR WAS INSTALLED IN THIS AIRCRAFT AS A OVERHAULED, EXCHANGED. THIS UNIT FAILED DURING TAKEOFF, WHICH PREVENTED HYDRAULIC PRESSURE TO BUILD UP T - [SDR MV5R055M](https://openairdocs.org/sdr/MV5R055M), Oct 24, 2002: SERVO. SEIZED. AILERON PRIMARY AUTO PILOT SERVO SEIZED. FLIGHT CREW APPLIED SUFFICIENT FORCE IN AN ATTEMPT TO FREE AILERON MOVEMENT. CAUSING AILERON CONTROL CABLE TO BECOME DI - [SDR MV52002F00006](https://openairdocs.org/sdr/MV52002F00006), Sep 19, 2002: MOUNT. CRACKED. OIL JET UTILIZED TO LUBRICATE THE BULL GEAR LOCATED WITHIN THE GEARBOX WAS CRACKED AT THE MOUNTING BASE. THIS CONDITION COULD CAUSE A REDUCED AMOUNT OF OIL FOR - [SDR MV52002F00004](https://openairdocs.org/sdr/MV52002F00004), Apr 25, 2002: RIB. CRACKED. RIGHT HORIZONTAL STABILIZER RIB CRACKED RIB LOCATED AT LEADING EDGE. - [SDR MV52002F00002](https://openairdocs.org/sdr/MV52002F00002), Apr 25, 2002: RIB. CRACKED. RIGHT HORIZONTAL STABILIZER RIB CRACKED. RIB LOCATED AT LEADING EDGE. - [SDR MB5R055N](https://openairdocs.org/sdr/MB5R055N), Apr 16, 2001: ANGLE. CRACKED. RIGHT MAIN LANDING GEAR OUTBOARD GEAR MOUNT SIDE BRACE TO WING ATTACHMENT ANGLE CRACKED. CRACK LOCATED AT THE AFT PORTION OF THE ANGLE EXTENDING ONE INCH FORWAR - [SDR MV5R055N1](https://openairdocs.org/sdr/MV5R055N1), Apr 6, 2001: BLOCK. SEPARATED. NOSE GEAR SEARING ATTACHMENT BLOCK PIN HAD SEPERATED FROM THE BLOCK. THE ROLL PIN THAT SECURES THE PIN TO THE BLOCK HAD SHEARED, INSPECTION OF THE ROLL PIN INDI - [SDR CA000830044](https://openairdocs.org/sdr/CA000830044), Aug 8, 2000: ACCUMULATOR. FAILED. (CAN) 1.A/C JUST COMPLETED ROUTINE 100 HR PERIODIC INSP. 2. HYDRAULIC ACCUMULATOR REGULATOR ASSY REPL, DUE TO LEAKING ACCUMULATOR (INTERNAL). IT WOULD NOT STORE - [SDR 20000609SH017](https://openairdocs.org/sdr/20000609SH017), May 15, 2000: BEARING SUPPORT. LACK OF LUBE. RUDDER PEDAL BEARINGS FAILED DUE TO LACK OF LUBRICATION. NO WAY TO LUBE WITHOUT COMPLETE DISASSEMBLY. BEARINGS CUT HALF WAY THROUGH RUDDER PEDAL TUBES, TUBES AR - [SDR 99ZZZX1571](https://openairdocs.org/sdr/99ZZZX1571), Apr 5, 1999: CONTROL CABLE. FRAYED. DURING INSPECTION, FOUND RIGHT RUDDER BALANCE CABLE FRAYED AT LOWER PULLEY. TT: APPROX 1,900 HOURS. INSTALLED NEW CABLE ASSY, RIGHT. - [SDR 98ZZZX4215](https://openairdocs.org/sdr/98ZZZX4215), Nov 4, 1998: WINDSHIELD. SHATTERED. LEFT WINDSHIELD OUTER LAYER SHATTERED AT ALTITUDE. WINDSHIELD HEAT OPERATED NORMALLY PRIOR TO INCIDENT. 500 HOURS ON WINDSHIELD. - [SDR 97ZZZX4010](https://openairdocs.org/sdr/97ZZZX4010), Sep 2, 1997: CONTROL CABLE. FRAYED. WHILE PERFORMING SB 226, THE LEFT AILERON CABLE WAS FOUND SEVERELY FRAYED AT WS 142.0. THE CABLE WAS PROPERLY ROUTED AND RUBBING ON THE FAIRLEAD AS IT WAS INTEN - [SDR CA971010012](https://openairdocs.org/sdr/CA971010012), Jul 8, 1997: CONTROL CABLE. BROKEN. (CAN) 75 PERCENT OF RT INBOARD FLAP CABLE STRANDS BROKEN. REPLACED. - [SDR 97ZZZX3339](https://openairdocs.org/sdr/97ZZZX3339), Jul 1, 1997: SKIN. CORRODED. ACFT RETURNED FOR FUSELAGE INSP AND FINAL REPAIRS OF THE RT WING. DURING INSP, CORROSION FND IN THE LT WING IN SAME AREA, WS 39, BOTTOM SIDE, FWD OF THE MAIN SP - [SDR 97ZZZX3338](https://openairdocs.org/sdr/97ZZZX3338), Jul 1, 1997: SKIN. CORRODED. ACFT RETURNED FOR FUSELAGE INSP AND FINAL REPAIRS OF THE RT WING. DURING INSP, CORROSION FND IN THE LT WING IN SAME AREA, WS 39, BOTTOM SIDE, FWD OF THE MAIN SP - [SDR 97ZZZX2087](https://openairdocs.org/sdr/97ZZZX2087), Apr 18, 1997: CONTROL CABLE. FRAYED. DURING A 100-HOUR INSPECTION, RUST WAS FOUND ON RIGHT HAND AILERON CABLE AS IT PASSED THROUGH A PULLEY AT FS 217. AFTER CLEANING RUST OFF, NOTED CABLE WAS BROKE - [SDR 97ZZZX1483](https://openairdocs.org/sdr/97ZZZX1483), Mar 1, 1997: FLAP. MISINSTALLED. WHILE AIRCRAFT WAS UNDERGOING MAINTENANCE, THE INBOARD LEFT FLAP WAS REMOVED. UPON INSTALLATION OF THE FLAP THE ATTACH BOLT MISSED THE ROD END THAT WAS COMING F - [SDR 96ZZZX4831](https://openairdocs.org/sdr/96ZZZX4831), Sep 4, 1996: STARTER. WRONG PART. DURING INSPECTION, NOTED ONE OF THE STARTER/GENERATORS HAD A DATA TAG ISSUED BY AIRCRAFT PARTS CORPORATION AND IDENTIFIED WITH P/N 300.S.G.119Q, NOT THE LEAR SI - [SDR 96ZZZX4129](https://openairdocs.org/sdr/96ZZZX4129), Aug 2, 1996: ARM ASSY. CRACKED. FOUND NLG ARM ASSY CRACKED FROM BOTH BOLT HOLES AND ALONG TUBE PORTION. TWO CRACKS FROM BOLT HOLES OUTBOARD AND ONE CRACK FROM OUTER EDGE .75 INCH INBOARD ON PA - [SDR 96ZZZX2236](https://openairdocs.org/sdr/96ZZZX2236), Apr 1, 1996: ANGLE. CRACKED. DURING A 100-HOUR INSPECTION, THE RT MLG INBOARD TRUSS ATTACH ANGLE WAS FOUND TO HAVE A 0.9 INCH RADIUS CRACK 1.0 INCH FROM AFT END. THIS CRACK WAS STOP DRILLED - [SDR 96ZZZX2235](https://openairdocs.org/sdr/96ZZZX2235), Apr 1, 1996: FIREWALL. CRACKED. THE LT AND RT ENGINE FIREWALLS FOUND TO HAVE CRACKS IN THE ALUMINUM PORTION OF FIREWALL AT THE AFT ENGINE MOUNT UPPER ATTACH FASTENERS DURING OTHER MAINTENANCE - [SDR 96ZZZX2229](https://openairdocs.org/sdr/96ZZZX2229), Apr 1, 1996: TRUSS SUPPORT. DAMAGED. AFTER RIGHT AFT LOWER NACELLE REMOVED TO FACILITATE MAINTENANCE, DISCOVERED THAT DURING A PREVIOUS LANDING GEAR REMOVAL, THE LEFT AND RIGHT OUTBOARD MLG TRUSS S - [SDR CA960502057](https://openairdocs.org/sdr/CA960502057), Mar 28, 1996: WINDSHIELD. CRACKED. (CAN) LEFT HAND WINDSHIELD FOUND CRACKED. - [SDR 96ZZZX25](https://openairdocs.org/sdr/96ZZZX25), Dec 14, 1995: REGULATOR. DIAPHRAGM BLOWN. DURING THE COURSE OF A 100-HOUR INSPECTION, FOUND THE BLEED AIR REGULATOR TO HAVE A BLOWN DIAPHRAGM. THIS IS THE REGULATOR LOCATED IN AFT BAGGAGE AREA THAT REDU ## STCs that may be installed (OpenAirDocs) (117, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc - [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc - [STC SA11300DS](https://openairdocs.org/stc/SA11300DS): Upgrade previously installed Collins Aerospace Radar Altimeter. BHE & Associates Ltd - [STC SA8408SW](https://openairdocs.org/stc/SA8408SW): Replace the o-ring seals in the landing gear lower strut seal. Metrea Special Aerospace ISR Inc - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc - [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc - [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc - [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc - [STC SA01586SE](https://openairdocs.org/stc/SA01586SE): Group Reduced Vertical Separation Minimum (RVSM). AeroMech Incorporated - [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics - [STC SA497GL](https://openairdocs.org/stc/SA497GL): Install Aircraft Wheel and Brake conversion kit 199-80 (MIL-H-5606 system). Kaman Corporation Aircraft Wheel and Brake LLC - [STC SA1458GL](https://openairdocs.org/stc/SA1458GL): Installation of a Cleveland nose wheel. Kaman Corporation Aircraft Wheel and Brake LLC - [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc - [STC SA02254AK](https://openairdocs.org/stc/SA02254AK): Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen". Genesys Aerosystems Inc - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King) - [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC - [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC - [STC SA02075SE](https://openairdocs.org/stc/SA02075SE): Installation of a Mid-Continent MD835( ) Lithium Ion Battery. Mid-Continent Instrument Co. Inc - [STC SA09763DS](https://openairdocs.org/stc/SA09763DS): Installation of an S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation - [STC SA04489NY](https://openairdocs.org/stc/SA04489NY): Installation of Astronics Max-Viz Enhanced Vision System. Air Spray (1967) Ltd - [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc - [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc - [STC SA4583SW](https://openairdocs.org/stc/SA4583SW): Installation of an electrically-driven Vapor Cycle, Freon or Refrigerant R-134a, Air Conditioning System. Air Comm Corporation - [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies - [STC SA00098SE](https://openairdocs.org/stc/SA00098SE): Installation of emergency medical stretcher, oxygen, and electrical systems. LifePort LLC - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA02153LA-D PAGE 2](https://openairdocs.org/stc/SA02153LA-D%20PAGE%202): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc - [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA00352BO PAGE 2](https://openairdocs.org/stc/SA00352BO%20PAGE%202): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA1177GL](https://openairdocs.org/stc/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. Paul/ Lanna Egan LLC - [STC SA00149BO](https://openairdocs.org/stc/SA00149BO): Installation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1. Aircraft Components Inc - [STC SA02547AT](https://openairdocs.org/stc/SA02547AT): Installation of a Voice Alert System. Aircraft Components Inc - [STC SA03658AT](https://openairdocs.org/stc/SA03658AT): Installation of a Voice Alert System to incorporate as primary annunciators for stall and gear warnings. Aircraft Components Inc - [STC SA02119SE PAGE 2](https://openairdocs.org/stc/SA02119SE%20PAGE%202): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc - [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics - [STC SA01229SE PAGE 2](https://openairdocs.org/stc/SA01229SE%20PAGE%202): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA02442AK PAGE 2](https://openairdocs.org/stc/SA02442AK%20PAGE%202): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC All 117: https://openairdocs.org/model/gulfstream-aerospace-695a/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Gulfstream AM Corp Comm Div 695A](https://openairdocs.org/model/gulfstream-am-corp-comm-div-695a): 17 registered aircraft, registry code 3970411 - [Rockwell International 695A](https://openairdocs.org/model/rockwell-international-695a): 0 registered aircraft, registry code 7630519 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.