# Grumman G1159B - Type: Aircraft model (FAA registry) - Registry code: 3953535 - Manufacturer (registry): GRUMMAN - Model: G1159B - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-jet - Seats: 122 - Weight class: 20,000 lb and over - Certification: Type certificated - Data sheet: [TCDS A12EA](https://openairdocs.org/tcds/A12EA) (OpenAirDocs) - Holder: Gulfstream Aerospace Corporation - Registered aircraft: 1 - Page: https://openairdocs.org/model/grumman-g1159b 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 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2023-08-03](https://openairdocs.org/ad/2023-08-03): Flight Controls · Gulfstream Aerospace G-1159A, G-1159B, G-IV and 1 more. Effective Jun 20, 2023 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2017-07-06](https://openairdocs.org/ad/2017-07-06): Flight Controls · Gulfstream Aerospace G-1159B. Effective May 15, 2017 - [AD 2016-20-06](https://openairdocs.org/ad/2016-20-06): Flight Controls · Gulfstream Aerospace G-1159, G-1159A, G-1159B and 1 more. Effective Oct 14, 2016 - [AD 2016-18-11](https://openairdocs.org/ad/2016-18-11): Landing Gear · Gulfstream Aerospace G-1159, G-1159A, G-1159B and 4 more. Effective Sep 23, 2016 - [AD 2012-11-06](https://openairdocs.org/ad/2012-11-06): Wings, Fuselage · Gulfstream Aerospace G-1159, G-1159A and G-1159B. Effective May 29, 2012 - [AD 2006-18-08](https://openairdocs.org/ad/2006-18-08): Nosewheel tires · Bombardier BD-700-1A10, BD-700-1A11, Aviation Tires and 7 more. Effective Oct 11, 2006 - [AD 2004-21-03](https://openairdocs.org/ad/2004-21-03): Left and right aileron · Gulfstream Aerospace G-1159, G-1159A, G-1159B and 1 more. Effective Nov 2, 2004 - [AD 2001-22-14](https://openairdocs.org/ad/2001-22-14): Fire Extinguishing System Bottle Cartridges · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 105 more. Effective Dec 10, 2001 - [AD 2001-18-05](https://openairdocs.org/ad/2001-18-05): Flight Eagle Tires · Boeing 720 Series, 720B Series, 111 and 6 more. Effective Sep 24, 2001 - [AD 2001-08-13](https://openairdocs.org/ad/2001-08-13): Door Control Valves of the Landing Gear · Gulfstream Aerospace G-1159, G-1159A, G-1159B and 2 more. Effective May 10, 2001 - [AD 96-25-12](https://openairdocs.org/ad/96-25-12): Auxiliary Power Units · BAE Systems HS 748 Series 2A, HS 748 Series 2B, 707-100 Long Body and 74 more. Effective Jan 13, 1997 - [AD 94-14-03](https://openairdocs.org/ad/94-14-03): Water Heaters and Coffee Makers · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 130 more. Effective Aug 1, 1994 - [AD 94-01-04](https://openairdocs.org/ad/94-01-04): Traffic Alert and Collision Avoidance System · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 136 more. Effective Feb 4, 1994 - [AD 93-23-01](https://openairdocs.org/ad/93-23-01): Water Heaters and Coffee Makers · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 126 more. Effective Dec 7, 1993 - [AD 93-10-04](https://openairdocs.org/ad/93-10-04): Engine Fire Extinguisher System · Gulfstream Aerospace G-1159, G-1159A, G-1159B and 1 more. Effective Jul 1, 1993 - [AD 93-01-18](https://openairdocs.org/ad/93-01-18): Buttock Line Structural Degradation · Gulfstream Aerospace G-1159, G-1159A and G-1159B. Effective Mar 10, 1993 - [AD 91-10-05](https://openairdocs.org/ad/91-10-05): Oxygen Mask Presentation Units · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 14 more. Effective Jun 3, 1991 - [AD 90-02-05](https://openairdocs.org/ad/90-02-05): Takeoff Warning System · Gulfstream Aerospace G-1159, G-1159A, G-1159B and 1 more. Effective Feb 13, 1990 - [AD 82-11-02](https://openairdocs.org/ad/82-11-02): Elevator and/or Trim Tab · Gulfstream Aerospace G-1159 and G-1159B. Effective May 31, 1982 - [AD 80-05-02](https://openairdocs.org/ad/80-05-02): Safety Belt Assemblies · Gulfstream Aerospace G-1159, G-1159A, G-1159B and 17 more. Effective Feb 27, 1980 - [AD 74-11-03](https://openairdocs.org/ad/74-11-03): Auxiliary Power Units · Airesearch Auxiliary Power Units, F.28 Mark 0070, F.28 Mark 0100 and 13 more. Effective May 20, 1974 Historical (superseded or no longer in force): - [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996 ## Information bulletins (advisory) (3) - [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010 - [SAIB NM-07-39R1](https://openairdocs.org/saib/NM-07-39R1): Powerplant System: Forward bearing fitting attach bolts. Issued Oct 10, 2008 - [SAIB NM-07-39](https://openairdocs.org/saib/NM-07-39) (historical): Forward bearing fitting attach bolts. Issued Jun 28, 2007 ## Registered aircraft (1) - [N148V](https://openairdocs.org/aircraft/N148V): [Eastern Pine Enterprises LLC](https://openairdocs.org/faa-owner/EASTERN%20PINE%20ENTERPRISES%20LLC), [Charlotte, NC](https://openairdocs.org/faa-place/NC/Charlotte), S/N 54 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (34) As reported by operators and repair stations, by the model named in the report. - [SDR N382006F00004](https://openairdocs.org/sdr/N382006F00004), Dec 8, 2006: DOWNLOCK SWITCH. DAMAGED. GEAR LIGHT NOSE GEAR FAILED TO ILLUMINATE WITH GEAR EXTENSION UNTIL 150 KTS. PINNED LANDING GEAR , ISSUED SPECIAL FLIGHT PERMIT FOR AC RETURN. JACKED AC AND INS - [SDR N382005F00004](https://openairdocs.org/sdr/N382005F00004), Jul 19, 2005: STARTER. MELTED. LT ENGINE WILL NOT START; NO START VALVE OR IGNITION LIGHT WHEN STARTER BUTTON PRESSED. A REPLACEMENT STARTER WAS INSTALLED AND THE AIRCRAFT WAS FLOWN BACK TO I - [SDR 2005FA0000967](https://openairdocs.org/sdr/2005FA0000967), Jun 9, 2005: ATTACH FITTING. CORRODED. IAW MM TO COMPLY WITH THE 24 MONTH NDT REQUIREMENTS UNDER THE ULTRASONIC PART OF THE INSPECTION CORROSION WAS FOUND ON BOTH THE LT AND RT WING ATTACHMENT FITTIN - [SDR 2005FA0000489](https://openairdocs.org/sdr/2005FA0000489), Dec 15, 2004: RIVET. LOOSE. UPON X-RAY INSPECTION OF AIRCRAFT FOR A 4000 LANDING INSPECTION, FOUND SEVERAL WORKING RIVETS AROUND CABIN WINDOWS AS INDICATED. LT NR 3 WINDOW; ONE (1) WORKING - [SDR 2005FA0000105](https://openairdocs.org/sdr/2005FA0000105), Dec 12, 2004: PROBE. BROKEN. NR 2 STICK SHAKER AND PUSHER ACTIVATED IN FLIGHT. ENROUTE, CREW ENCOUNTERED ABOVE MENTIONED ISSUE. CREW DIVERTED, DECLARED AN EMERGENCY. LANDING WAS UNEVENTFUL. - [SDR N382005F00000](https://openairdocs.org/sdr/N382005F00000), Dec 9, 2004: DOOR FRAME. CRACKED. DURING AC 4000 LANDING INSPECTION, FOUND APPROX 1INCH CRACK AT THE UPPER FORWARD RADIUS OF DOOR FRAME. STOP DRILLED CRACK AND REPAIRED WITH AN OVERLAY DOUBLER I - [SDR 2005FA0000003](https://openairdocs.org/sdr/2005FA0000003), Dec 9, 2004: DOOR FRAME. CRACKED. DURING AIRCRAFT 4000 LANDING INSPECTION, FOUND APPROX A 1 INCH CRACK AT THE UPPER FORWARD RADIUS OF DOOR FRAME. STOP DRILLED CRACK AND REPAIRED WITH AN OVERLAY - [SDR N3B2004F00000](https://openairdocs.org/sdr/N3B2004F00000), Jul 16, 2004: TIRE. BLOWN. LT MAIN GEAR TIRE BLEW OUT ON TAKEOFF. DAMAGE TO LT WING, LT GEAR HARNESS, BRAKE LINES, AND A DENT IN THE LT LOWER ENGINE COWL. - [SDR JGV2004F00001](https://openairdocs.org/sdr/JGV2004F00001), Jan 29, 2004: PITOT LINE. BROKEN. ORIGINAL PITOT/STATIC TUBING AND PLASTIC FITTINGS BRITTLE AND EASILY BROKEN. MOVING TUBING OR EVEN WIRE BUNDLES TOUCHING TUBING CAUSES LEAKS. THIS IS DUE TO ITS - [SDR CA030507005](https://openairdocs.org/sdr/CA030507005), Apr 3, 2003: BOLT. BROKEN. (CAN) ENGINE IS AT RRC FOR REPAIR DUE TO HIGH VIBRATION ON WING. VIBRATION ON THE REAR PICK UP WAS CONFIRMED ON A TEST BED RUN AT RRC. DURING THE STRIP OF THE T - [SDR N382003F00000](https://openairdocs.org/sdr/N382003F00000), Feb 24, 2003: ACTUATOR. CRACKED. LEAKING ACTUATOR OR LINE CAUSED EXCESSIVE LESS OF COMBINED HYDRAULIC FLUID. FOUND THE END CAP CRACKED APPROXIMATELY .3333 OF THE CAP CIRCUMFERENCE. - [SDR O2G2003F00003](https://openairdocs.org/sdr/O2G2003F00003), Dec 25, 2002: HARNESS. INTERMITTENT. RT WING HEAVY CONDITION CAUSED BY FUEL IMBALANCE. ON CLIMB OUT, FUEL MIGRATED TO WING TIPS MAKING IMBALANCE SEEM MORE THAN IT WAS. BOTH FUEL TANKS OPENED, INSPE - [SDR 2002FA0000964](https://openairdocs.org/sdr/2002FA0000964), Aug 9, 2002: FITTING. SCORED. COMBINED HYDRAULIC SYSTEM INDICATED LOW QUANITY PRESSURE 330PSI TEE FITTING SCORED ON HYD LINE. - [SDR BTV2001F00000](https://openairdocs.org/sdr/BTV2001F00000), May 29, 2001: BRACKET. FRACTURED. DURING A ROUTINE SCHEDULED INSPECTION, A MECHANIC NOTED THE RUDDER GUST LOCK HOOK SUPPORTING STRUCTURE WAS FRACTURED. FURTHER INVESTIGATION FOUND THREE PIECES T - [SDR MQGR20013601](https://openairdocs.org/sdr/MQGR20013601), Apr 12, 2001: ATTACH FITTING. CORRODED. DURING RECOMMENDED INSPECTION OF WINGLET ATTACH HARDWARE FOR CORROSION, FOUND CORROSION IN THE WINGLET TO WING ATTACHMENT FITTING. IT APPEARS THIS CORROSION IS - [SDR 20010205CW019](https://openairdocs.org/sdr/20010205CW019), Jan 16, 2001: BEARING. BROKEN. NOTICED INBOARD ROLLER BEARING ON LEFT FLAP TRACK, B, WAS MISSING THE OUTER CASING AND BEARING...ONLY STUD REMAINED, CAUSE IS UNKNOWN. RECOMMEND THAT ROLLER BEA - [SDR 20001227SH015](https://openairdocs.org/sdr/20001227SH015), Nov 20, 2000: BEAM. CORRODED. LEFT WING REAR BEAM HAD CORROSION UNDERNEATH AILERON. (X) - [SDR 20000907SH009](https://openairdocs.org/sdr/20000907SH009), Sep 7, 2000: FLANGE. FAILED. FLANGE ON INBOARD SIDE OF HEAT EXCHANGER FAILED AND DUCT BECAME DISCONNECTED. HEAT EXCHANGER IS BEING SENT TO GULFSTREAM FOR ENGINEERING ANALYSIS. (X) - [SDR 2000ZZZX380](https://openairdocs.org/sdr/2000ZZZX380), Dec 6, 1999: RIVET. MISSING. DURING AN EXTERNAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER, FOUND TWO RIVET HEADS FROM LOWER RT SKIN TO BE MISSING. REMAINING RIVET STEMS/SHANKS FOUND, A - [SDR 99ZZZX4623](https://openairdocs.org/sdr/99ZZZX4623), Nov 24, 1999: PLANK. CORRODED. DURING NDT OF WING CLOTHESPIN FITTINGS, FOUND CORROSION ON TOP OF UPPER AFT WING PLANK. CORROSION MAY BE DUE TO HARSH AREA THAT IT IS SUBJECTED TO. - [SDR 98ZZZM772](https://openairdocs.org/sdr/98ZZZM772), Mar 30, 1998: TRANSDUCER. MALFUNCTIONED. LOST CABIN PRESSURIZATION CONTROL AT 37,000 FT, WENT TO MANUAL AND COULD NOT CONTROL. MADE EMERGENCY DESCENT TO 10,000 FT. REPLACED PRESSURIZATION SYSTEM TRANSD - [SDR 98ZZZX1631](https://openairdocs.org/sdr/98ZZZX1631), Feb 15, 1998: SEAL. TORN. 'LOST PRESSURIZATION AT FL 390. COULD NOT CONTROL CABIN. MADE EMERGENCY DESCENT AND RETURNED TO PONTIAC'. REPLACED CABIN DOOR SEAL AND DOOR SEAL CHECK VALVE. GR - [SDR 98ZZZX798](https://openairdocs.org/sdr/98ZZZX798), Jan 29, 1998: BOLTS. CORRODED. REMOVED LEFT WING WINGLET ATTACHMENT BOLTS AND SLEEVES TO REMOVE WINGLET FOR ACCESS. FOUND ALL SIX BOLTS EXCESSIVELY CORRODED. THERE IS NO REQUIRED INSPECTION I - [SDR 98ZZZX797](https://openairdocs.org/sdr/98ZZZX797), Jan 29, 1998: BOLTS. CORRODED. REMOVED LEFT WING WINGLET ATTACHMENT BOLTS AND SLEEVES TO REMOVE WINGLET FOR ACCESS. FOUND ALL SIX BOLTS EXCESSIVELY CORRODED. THERE IS NO REQUIRED INSPECTION I - [SDR 98ZZZX796](https://openairdocs.org/sdr/98ZZZX796), Jan 29, 1998: BOLTS. CORRODED. REMOVED LEFT WING WINGLET ATTACHMENT BOLTS AND SLEEVES TO REMOVE WINGLET FOR ACCESS. FOUND ALL SIX BOLTS EXCESSIVELY CORRODED. THERE IS NO REQUIRED INSPECTION I - [SDR 98ZZZM728](https://openairdocs.org/sdr/98ZZZM728), Jan 21, 1998: ACTUATOR. BINDING. FLAPS WOULD NOT DEPLOY IN FLIGHT, NORMAL OR EMERGENCY, UPON APPROACH TO TEB. RETURNED TO PTK AND LANDED. REPLACED LEFT WING INBOARD FLAP ACTUATOR P/N 1159SCC211 - [SDR 98ZZZX325](https://openairdocs.org/sdr/98ZZZX325), Aug 4, 1997: IGNITER. FAILED. IGNITER UNIT OVERHAULED 11 MONTHS, 138 HOURS, 66 CYCLES AGO. FAILED OPS INSPECTION WITH DISCHARGE ONLY EVERY 5-6 SECONDS. SHOULD BE APPROXIMATELY 1 SECOND. - [SDR 98ZZZX319](https://openairdocs.org/sdr/98ZZZX319), Jun 25, 1997: GENERATOR. WORN. BLACK SOOT ON COWLING. CHECKED GENERATOR BRUSHES AND FOUND UNDER ONE-QUARTER LIFE REMAINING. - [SDR 96ZZZX5073](https://openairdocs.org/sdr/96ZZZX5073), Sep 20, 1996: ALTERNATOR. FAILED. LEFT AC GENERATOR SUSPECT FAILED. DROPPED OFF LINE IN-FLIGHT. TVI FROM .5 TO 2.0 IPS. NOTED DEBRIS AROUND MOUNTING FLANGE UPON INSPECTION. REPLACED ALTERNATOR. - [SDR EW7A379W](https://openairdocs.org/sdr/EW7A379W), Aug 8, 1996: WINDSHIELD. CRACKED. PILOT NOTICED INTERIM WINDOW HEATING WIRES GLOWING AND OVERHEATING. APPROXIMATELY 10 SECONDS AFTER TURNING HEAT OFF, THE OUTER GLASS PANE CRACKED FROM SHOCK COO - [SDR 96ZZZM670](https://openairdocs.org/sdr/96ZZZM670), Mar 10, 1996: SKIN. DEBONDED. RIGHT LOWER AFT PYLON SKIN DELAMINATED BEYOND MANUFACTURE'S ACCEPTABLE LIMITS. - [SDR 96ZZZM671](https://openairdocs.org/sdr/96ZZZM671), Mar 3, 1996: DOUBLER. CORRODED. ON FS 580 PRESSURE BULKHEAD COMM SCAN INSPECTION, CORROSION WAS DETECTED BETWEEN THE SKIN AND LONGERON NR 24 ON THE RIGHT SIDE OF AIRFRAME AT LOCATION NR 59 BET - [SDR 96ZZZX803](https://openairdocs.org/sdr/96ZZZX803), Jan 22, 1996: BULB. BURNING END. AEROSPACE LIGHTING AD'S HAVE BEEN ISSUED, BUT THIS HAS NOT CORRECTED THE PROBLEM. FLUORESCENT BULB ENDS ARE STILL BURNING OFF. SUBMITTER SUGGESTS POSSIBLE CABIN - [SDR 97ZZZX3069](https://openairdocs.org/sdr/97ZZZX3069), Jan 11, 1996: FITTING. CORRODED. DURING PROCESS OF REMOVING RT THRUST STRUT FOR NDT, DISCOVERED SEVERE INTERGRANULAR CORROSION AT AFT/UPPER THRUST STRUT/FUSELAGE ATTACH FITITNG, PN 1159BM20518- ## STCs that may be installed (OpenAirDocs) (317, 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 ST01305WI-D](https://openairdocs.org/stc/ST01305WI-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 in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc - [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center - [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc - [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc - [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc - [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc - [STC ST11216DS](https://openairdocs.org/stc/ST11216DS): Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft. BHE & Associates Ltd - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc - [STC ST219CH](https://openairdocs.org/stc/ST219CH): Installation of BFGoodrich TCAS-791 traffic alert and collision avoidance system (TCAS I). Acron Aviation Inc - [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc - [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC - [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC - [STC ST02004WI](https://openairdocs.org/stc/ST02004WI): Installation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI). Peregrine - [STC ST04281AT](https://openairdocs.org/stc/ST04281AT): Installation for the Upgrade of the NZ-2000 FMS computer for software version NZ6. Chippewa Aerospace Inc - [STC SA2697CE](https://openairdocs.org/stc/SA2697CE): Installation of MK V ground proximity warning system. Honeywell International Inc - [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc - [STC ST01270WI-D](https://openairdocs.org/stc/ST01270WI-D): Installation of Honeywell MK V and MK VII EGPWS Runway Awareness and Advisory System (RAAS). This approval is limited to specifically idenitfied aircraft. Duncan Aviation Inc - [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS - [STC ST00790DE](https://openairdocs.org/stc/ST00790DE): Installation of BendixKing CAS 67B Traffic Alert and Collision Avoidance System (TCAS) II Version 7.1. Peregrine - [STC ST04368CH](https://openairdocs.org/stc/ST04368CH): Installation of a dual Universal Avionics Systems Corporation AHS-525 Attitude and Heading Reference System (AHRS) in accordance with Pentastar Aviation Master Data List, Document No. A-16738-001, Rev. A, dated December 19, 2018, or later FAA approved revision. Pentastar Aviation LLC - [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC ST00347BO](https://openairdocs.org/stc/ST00347BO): Modification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1. Pro Star Aviation, LLC - [STC ST00373BO](https://openairdocs.org/stc/ST00373BO): Installation of Rockwell Collins TDR-94D Transponders with ADS-B Out. Pro Star Aviation, LLC - [STC ST00135BO](https://openairdocs.org/stc/ST00135BO): Modification of Honeywell TCAS II system installation with R/T 910 and software Version 6.4a to R/T 910 with Change 7.0 software; or TCAS 2000 system with R/T 950, 951 and software Version 6.4a to R/T 950, 951 with Change 7.0 software. Pro Star Aviation, LLC - [STC ST00208BO](https://openairdocs.org/stc/ST00208BO): Installation of dual Innovative Solutions and Support Air Data Display Units and a single Skylight Avionics ADC-600 Air Data Converter in accordance with Pro Star Aviation Master Document List, Document Number 0704-MDL-01, dated July 2, 2004, or later FAA-approved revision. Pro Star Aviation, LLC - [STC ST03262CH](https://openairdocs.org/stc/ST03262CH): Installation of a Data Link Communication System supporting Air Traffic Services (ATS) utilizing SATCOM with a compliant Communications Management Unit. Chicago Jet Group LLC - [STC SA5636SW](https://openairdocs.org/stc/SA5636SW): Installation of dual long range LTN-72R/NTN211 navigation systems. Associated Air Center, Inc. - c/o CT Corporation System - [STC ST11071SC](https://openairdocs.org/stc/ST11071SC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc - [STC ST00117AT](https://openairdocs.org/stc/ST00117AT): Installation of a replacement coalescer filter Greentree Aerotech, Inc. (GAI) P/N 21D10-3. Purolator Facet, Inc - [STC ST00118AT](https://openairdocs.org/stc/ST00118AT): Installation of a replacement coalescer filter, Greentree Aerotech, Inc., (GAI) P/N 21D10-2. Purolator Facet, Inc - [STC ST02632LA](https://openairdocs.org/stc/ST02632LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out and optionally install ACSS NXG-900 GPS as a position source for ADS-B Out. Aviation Communications and Surveillance Systems - [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC ST02609LA](https://openairdocs.org/stc/ST02609LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS - [STC SA1519GL](https://openairdocs.org/stc/SA1519GL): Install Egan Aviation air ambulance stretcher. Paul/ Lanna Egan LLC - [STC ST03305CH](https://openairdocs.org/stc/ST03305CH): Install Air Ambulance conversion. Paul/ Lanna Egan LLC - [STC SA3743SW](https://openairdocs.org/stc/SA3743SW): Installation of decorative window reveal with integral window shade. Aero Shade Technologies, Inc - [STC ST10072SC](https://openairdocs.org/stc/ST10072SC): Installation of manual and electrical powered window shade assemblies. Aero Shade Technologies, Inc - [STC ST10083SC](https://openairdocs.org/stc/ST10083SC): Installation of Manual Window Shades. Aero Shade Technologies, Inc - [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC - [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc - [STC ST03138CH](https://openairdocs.org/stc/ST03138CH): Installation of Electronic Flight Bag (EFB Class 2) provisions for the use of Tablet PC s. Pentastar Aviation LLC - [STC ST04238AT](https://openairdocs.org/stc/ST04238AT): Upgrade of Honeywell Traffic Collision Avoidance Systems II (TCAS II) Processor Software from TCAS II Version 7.0 to TCAS II Version 7.1. Aviation Partners Group Inc - [STC ST00789CH](https://openairdocs.org/stc/ST00789CH): Installation of a Fairchild F1000 Flight Data Recorder. StandardAero Business Aviation Services, LLC - [STC ST02524LA](https://openairdocs.org/stc/ST02524LA): Installation of TCAS version 7.0. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC ST01461LA-D](https://openairdocs.org/stc/ST01461LA-D): Installation of Hawker P/N 9750W0538 24-volt amp-hour sealed lead acid battery. Securaplane Technologies - [STC ST00757DE](https://openairdocs.org/stc/ST00757DE): Reduced Maximum Gross Take-off Weight (MGTOW) and Reduced Maximum Ramp Weight (MRW). Trolltune Corporation - [STC ST01567LA](https://openairdocs.org/stc/ST01567LA): Installation of a pylon-mounted ejector system (without the thrust reversers installed) to show compliance with the Stage 3 requirements of 14 CFR part 36 through amendment 24. STC ACQUISITION LLC - [STC ST03958AT](https://openairdocs.org/stc/ST03958AT): The installation and activation of the EMS Satellite Communication System with Cabin Wireless Local Area Network (WLAN). Banyan Air Service All 317: https://openairdocs.org/model/grumman-g1159b/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Gulfstream Aerospace G1159B](https://openairdocs.org/model/gulfstream-aerospace-g1159b): 10 registered aircraft, registry code 3980110 --- 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.