# N918SJ: 2007 Israel Aircraft Industries GULFSTREAM 200

- Status: Valid registration
- Airframe: [Israel Aircraft Industries GULFSTREAM 200](https://openairdocs.org/model/israel-aircraft-industries-gulfstream-200) (registry code 4500308, 19 seats)
- Engine: [Pratt & Whitney Canada PW306A](https://openairdocs.org/engine/pratt-whitney-canada-pw306a) (registry code 52165)
- Data sheets: [TCDS A53NM](https://openairdocs.org/tcds/A53NM) (Gulfstream Aerospace LP), [TCDS E35NE](https://openairdocs.org/tcds/E35NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 177
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 18, 2010
- Certificate issued: July 29, 2020
- Expires: July 31, 2027
- Mode S code: ACB5FC
- Registered owner: [Nonstop Capital LLC](https://openairdocs.org/faa-owner/NONSTOP%20CAPITAL%20LLC)
- Location: [Newport Beach, CA](https://openairdocs.org/faa-place/CA/Newport%20Beach)
- Owner type: LLC
- Owner's area on the map: 33.6346° N, 117.8749° W: Placed by OpenAirDocs at the center of ZIP code 92660, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=918SJ
- Page: https://openairdocs.org/aircraft/N918SJ

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 19 in force

### Matched by airframe (Israel Aircraft Industries GULFSTREAM 200)

- [AD 2026-16-09](https://openairdocs.org/ad/2026-16-09): Time Limits/Maintenance Checks · Gulfstream Aerospace LP Gulfstream 200 and Galaxy. Effective Sep 18, 2026
- [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 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2023-06-09](https://openairdocs.org/ad/2023-06-09): Wings · Gulfstream Aerospace LP Galaxy and Gulfstream 200. Effective May 18, 2023
- [AD 2011-23-07](https://openairdocs.org/ad/2011-23-07): Flight controls · Gulfstream Aerospace LP Galaxy, Gulfstream 200 and Gulfstream G150. Effective Dec 15, 2011
- [AD 2011-20-04](https://openairdocs.org/ad/2011-20-04): Standard Practices/Structures · Gulfstream Aerospace LP Galaxy and Gulfstream 200. Effective Nov 7, 2011
- [AD 2010-20-04](https://openairdocs.org/ad/2010-20-04): Flight controls · Gulfstream Aerospace LP Galaxy and Gulfstream 200. Effective Oct 28, 2010
- [AD 2008-16-10](https://openairdocs.org/ad/2008-16-10): Hydraulic tubes · Gulfstream Aerospace LP Galaxy and Gulfstream 200. Effective Dec 26, 2008
- [AD 2007-17-16](https://openairdocs.org/ad/2007-17-16): Poppet covers · Gulfstream Aerospace LP Galaxy and Gulfstream 200. Effective Oct 2, 2007
- [AD 2007-07-13](https://openairdocs.org/ad/2007-07-13): Avionics and electrical wire harnesse · Gulfstream Aerospace LP Galaxy and Gulfstream 200. Effective Apr 20, 2007
- [AD 2007-07-11](https://openairdocs.org/ad/2007-07-11): Right Fuel Standby Pump Connector 4Q1 · Gulfstream Aerospace LP Gulfstream 200. Effective Apr 18, 2007
- [AD 2006-10-18](https://openairdocs.org/ad/2006-10-18): Airplane flight manual (AFM) · Gulfstream Aerospace LP Galaxy and Gulfstream 200. Effective Jul 5, 2006
- [AD 2005-16-13](https://openairdocs.org/ad/2005-16-13): Fuel standby feed pumps · Gulfstream Aerospace LP Galaxy and Gulfstream 200. Effective Aug 30, 2005
- [AD 2004-16-03](https://openairdocs.org/ad/2004-16-03): Wing flap actuators · Gulfstream Aerospace LP Galaxy and Gulfstream 200. Effective Sep 14, 2004
- [AD 2004-09-24](https://openairdocs.org/ad/2004-09-24): Internal and external spring sleeves · Gulfstream Aerospace LP Galaxy and Gulfstream 200. Effective May 24, 2004
- [AD 2002-23-01](https://openairdocs.org/ad/2002-23-01): Forward engine cross spar assembly · Gulfstream Aerospace LP Galaxy and Gulfstream 200. Effective Nov 29, 2002
- [AD 2002-10-09](https://openairdocs.org/ad/2002-10-09): Fuel Accumulation Inside Aft Service Compartment · Gulfstream Aerospace LP Galaxy and Gulfstream 200. Effective Jun 6, 2002
- [AD 2002-07-02](https://openairdocs.org/ad/2002-07-02): Main Landing Gear (MLG) Actuators · Gulfstream Aerospace LP Galaxy and Gulfstream 200. Effective Apr 18, 2002

### Matched by engine (Pratt & Whitney Canada PW306A)

- [AD 2001-03-02](https://openairdocs.org/ad/2001-03-02): Compressor Rotor 2nd, 3rd and 4th Stage Drum Assembly · Pratt & Whitney Canada PW306A and PW306B. Effective Feb 21, 2001

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N918SJ.

## FAA accident and incident reports

None matched to N918SJ.

## Reports on N918SJ not matched to an aircraft (2)

They name N918SJ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19940923043189I](https://openairdocs.org/incident/19940923043189I), Sep 23, 1994: Lkheed 382G (N918SJ), Charleston, SC, Minor damage. During touch and go landing NR2 engine lost power. Aircraft veered off runway. Hit marker. Throttle cable broke.
- [Incident 19881003059689I](https://openairdocs.org/incident/19881003059689I), Oct 3, 1988: Lkheed 382B (N918SJ), Pacific Ocean, HI. Advised ATC that they had an omega navigational equipment problem. ATC located aircraft 105 miles south of course.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N918SJ not matched to an aircraft (13)

They name N918SJ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR SRAA971105](https://openairdocs.org/sdr/SRAA971105), Sep 16, 1997: SKIN. DAMAGED. WHILE ON THE GROUND, AIRCRAFT WAS STRUCK BY A FORKLIFT. INSPECTED AIRCRAFT AND FOUND BOTTOM SKIN OF LEFT WING HAD GOUGING AND SCRAPES. PERFORMED INTERIM REPAIR 
- [SDR SRAA970907](https://openairdocs.org/sdr/SRAA970907), Sep 13, 1997: VALVE. INOPERATIVE. DURING FLIGHT, AIRCRAFT WOULD NOT PRESSURIZE, NOTICED BLEED AIR LEAK IN RIGHT WHEEL WELL. DUMPED 3,000 LBS OF FUEL AND LANDED WITHOUT INCIDENT AT DEPARTURE STAT
- [SDR SRAA970802](https://openairdocs.org/sdr/SRAA970802), Aug 1, 1997: VALVE. MALFUNCTIONED. DURING FLIGHT APPROX 50 MILES FROM DESTINATION, NR 4 ENGINE DROPPED TO 97 PERCENT, THEN PROP LOW OIL LIGHT CAME ON. SHUT DOWN NR 4 ENGINE AS PRECAUTIONARY AND L
- [SDR SRAA970420](https://openairdocs.org/sdr/SRAA970420), Apr 26, 1997: VALVE HOUSING. BEARING FAILED. SHUTDOWN OF NR 4 ENGINE DUE TO SUSPECTED DECOUPLE APPROX 30 MIN. AFTER TAKEOFF FROM LCK. RETURNED TO LCK AND LANDED WITHOUT INCIDENT. FOUND NO DECOUPLE CONDITIO
- [SDR SRAA970112](https://openairdocs.org/sdr/SRAA970112), Jan 15, 1997: TEMP CTR VALVE. INOPERATIVE. CARGO COMPARTMENT OVERHEAT ILLUMINATED ON TAXI. FOUND TEMPERATURE CONTROL VALVE INOPERABLE. REPLACED VALVE AND OPERATIONAL CHECK GOOD PER IAW MM CH 21.
- [SDR SRAA961012](https://openairdocs.org/sdr/SRAA961012), Oct 15, 1996: TRACK. CRACKED. DURING WALK AROUND INSPECTION, FOUND ON RIGHT WING O/B FLAP VERTICAL BEAM I/B TRACK CRACKED FROM LOWER WING SURFACE AND TRAVELS UPWARD APPROX 50 PERCENT OF VERT
- [SDR SRAA961002](https://openairdocs.org/sdr/SRAA961002), Oct 2, 1996: FITTINGS. CRACKED. ON PRE-FLIGHT INSPECTION AT HOW, FOUND AIRCRAFT FUSELAGE FITTINGS AT STA 780 AND 830 CRACKED. ADDITIONAL INSPECTION FOUND TOTAL OF THREE CARGO COMPARTMENT SUPPO
- [SDR SRAA960909](https://openairdocs.org/sdr/SRAA960909), Sep 11, 1996: GASKETS. LEAKING. DURING CRUISE INTO PHL. FLT 9010, NR 2 NACELLE OVERHEAT LIGHT CAME ON, SHUT DOWN ENGINE AND LANDED WITHOUT INCIDENT AT PHL. FOUND SCOOP ANTI-ICE LINE ON LEFT HA
- [SDR SRAA960907](https://openairdocs.org/sdr/SRAA960907), Sep 11, 1996: DUCT SEAL. FAILED. DURING FLIGHT, NR 2 NACELLE OVERHEAT LIGHT CAME ON APPROXIMATELY FIVE MINUTES AFTER LEVELED OFF. SHUTDOWN ENGINE AND ACCOMPLISHED AIR TURNBACK TO CHS, AIRCRAFT 
- [SDR SRAA960811](https://openairdocs.org/sdr/SRAA960811), Aug 23, 1996: CONTROLLER. DEFECTIVE. DURING FLIGHT, AIRCRAFT WOULD NOT PRESSURIZE OVER 4 AT 14,000 FT IN AUTO OR MANUAL. ACCOMPLISHED AIR TURNBACK TO LCK AND LANDED WITHOUT INCIDENT. FOUND PRESSURE
- [SDR SRAA69602](https://openairdocs.org/sdr/SRAA69602), Jun 8, 1996: VALVE HSG. BAD BEARING. ON CLIMB-OUT FROM AVB TO AAB - NR 1 ENGINE RPM FLUCTUATED FROM 105 PERCENT TO 95 PERCENT IN LESS THAN ONE SECOND, NO LOW OIL LIGHT AND MECHANICAL GOVERNING HAD 
- [SDR SRAA99514](https://openairdocs.org/sdr/SRAA99514), Sep 25, 1995: WIRE. CHAFED. ON PRE-FLIGHT, FOUND NR 2 ENGINE FIRE WARNING WILL NOT TEST. INSPECTED FIRE LOOP ALL SECURED, TROUBLESHOT SYSTEM AND FOUND CHAFED WIRE AT FIRE WARNING CONTROL U
- [SDR SRAA99503](https://openairdocs.org/sdr/SRAA99503), Sep 2, 1995: BOW BEAM. CRACKED. POST FLIGHT INSPECTION, FOUND RIGHT WHEEL WELL AT FUSELAGE STATION 537, HAD BAD BOW IN SKIN AREA. FOUND RIGHT BOW BEAM AT FUSELAGE STATION 537, WATER LEVEL 170 

## STCs that may be installed (OpenAirDocs) (155, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Israel Aircraft Industries GULFSTREAM 200)

- [STC ST12526IB](https://openairdocs.org/stc/ST12526IB): Radiant Type III RIPS Installation. Sky Service F.B.O. Inc
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST04753NY](https://openairdocs.org/stc/ST04753NY): Installation of Galileo HDX with GOGO Avance Platforms. Trimec Aviation
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [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 ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing 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 ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine
- [STC ST02586AK](https://openairdocs.org/stc/ST02586AK): Approval of the Thomas Global Systems TFD-4000/4100 Active Matrix Liquid Crystal Display. ADS-B Technologies
- [STC ST01833WI](https://openairdocs.org/stc/ST01833WI): Modification of a Rockwell Collins Global Positioning System (GPS) installation. Rockwell Collins Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST00204IB](https://openairdocs.org/stc/ST00204IB): Installation of Structural Provisions for a Swift Broadband Antenna. STC Twenty One Limited
- [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 ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST01108DE](https://openairdocs.org/stc/ST01108DE): Installation of Curtiss Wright GSD1000 Digital Flight Data Acquisition Unit. Peregrine
- [STC ST04223NY](https://openairdocs.org/stc/ST04223NY): Installation of Gogo Business Aviation AVANCE L3 System. Trimec Aviation
- [STC ST01985WI](https://openairdocs.org/stc/ST01985WI): Installation of the Garmin GI-275 I Electronic Standby Instrument (ESI). Peregrine
- [STC ST04345AT-D](https://openairdocs.org/stc/ST04345AT-D): Replace existing Flight Data Recorder with an Universal FDR-25. Gulfstream Aerospace Corporation
- [STC ST04186NY](https://openairdocs.org/stc/ST04186NY): Installation of the Prolink/Universal UNS1-Fw FMS, CVR, Unilink and Latitude DL-150 Iridium Transceiver to include LPV, FANS-1A, ATN-81. Chicago Jet Group LLC
- [STC ST04198NY](https://openairdocs.org/stc/ST04198NY): Installation of Becker Avionics DVCS6500 Digital Voice Communication System. Aerospace Design & Compliance LLC
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST01951WI](https://openairdocs.org/stc/ST01951WI): Installation of Gogo Business Aviation AVANCE L5 Broadband System. Duncan Aviation Inc
- [STC ST04331AT-D](https://openairdocs.org/stc/ST04331AT-D): Installation of a Dual Universal Avionics System. Gulfstream Aerospace Corporation
- [STC ST04366NY](https://openairdocs.org/stc/ST04366NY): Installation of Rockwell Collins TDR94D Transponder Upgrade - ADS-B Out. Mid Canada Mod Center
- [STC ST00912DE](https://openairdocs.org/stc/ST00912DE): Installation of Future Air Navigation System (FANS) 1/A+, Remote Oceanic Controller Pilot Data Link Communications (CPDLC), Automatic Dependent Surveillance - Contract (ADS-C), and CPDLC Departure Clearance (CPDLC-DCL). Gulfstream Aerospace Corporation
- [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 ST04294NY](https://openairdocs.org/stc/ST04294NY): Replacement of certain Goodrich pneumatic de-icer boots. BE Aerospace Inc. DBA SMR Technologies Inc
- [STC ST04013NY](https://openairdocs.org/stc/ST04013NY): Installation of the Collins TDR-94D-502 Transponder. Trimec Aviation
- [STC ST04168NY](https://openairdocs.org/stc/ST04168NY): Installation of ADS-B OUT on RC Pro Line 4 (G-200). 328 Support Services GmbH
- [STC ST01650WI](https://openairdocs.org/stc/ST01650WI): Activation of the Wireless Fidelity (WiFi) capabilities of previously installed router(s) and Aircraft Transmitting Portable Electronic Devices (T-PEDs) Tolerance Testing. MSP Aero LLC
- [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 ST03964NY](https://openairdocs.org/stc/ST03964NY): Installation of a Gogo Biz 4G (L5 AVANCE ) System. Gogo Business Aviation LLC
- [STC ST03966NY](https://openairdocs.org/stc/ST03966NY): Certification of Transmitting Portable Electronic Devices (T-PED) and Interference Path Loss (IPL) Measurement. Trimec Aviation
- [STC ST04261AT](https://openairdocs.org/stc/ST04261AT): Replacement of the inner aluminum barrel of the engine inlet cowl, with an inlet barrel of carbon graphite sandwich construction. Quiet Technology Aerospace
- [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 ST01419LA](https://openairdocs.org/stc/ST01419LA): Installation of thermal/acoustic insulation kit. Luminary Air Group LLC
- [STC ST03813NY](https://openairdocs.org/stc/ST03813NY): Installation of Dual UASC UNS-1Ew FMS with FANS-1/A + Data Link Option. Sky Service F.B.O. Inc
- [STC ST03305CH](https://openairdocs.org/stc/ST03305CH): Install Air Ambulance conversion. Paul/ Lanna Egan LLC
- [STC ST10349SC](https://openairdocs.org/stc/ST10349SC): Installation of MSA manually operated window shades. Aero Shade Technologies, Inc
- [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 ST04035AT-D](https://openairdocs.org/stc/ST04035AT-D): Installation of Micro Quick Access Recorder (-QAR). Gulfstream Aerospace Corporation
- [STC ST00800DE](https://openairdocs.org/stc/ST00800DE): Modification of a TCAS II system installation to Change 7.1. West Star Aviation Inc
- [STC ST04021AT-D](https://openairdocs.org/stc/ST04021AT-D): Installation of an Automatic Dependent Surveillance Broadcast Out (ADS-B) System. Gulfstream Aerospace Corporation
- [STC ST04023AT-D](https://openairdocs.org/stc/ST04023AT-D): Installation of an APU Access Door Modification. Gulfstream Aerospace Corporation
- [STC ST01431WI-D](https://openairdocs.org/stc/ST01431WI-D): Modification of a Rockwell Collins, Inc. Data Base Unit (DBU) installation. Rockwell Collins Inc
- [STC ST04208AT-D](https://openairdocs.org/stc/ST04208AT-D): Installation of Rockwell Collins Flight Management System. Gulfstream Aerospace Corporation
- [STC ST01433WI-D](https://openairdocs.org/stc/ST01433WI-D): Modification of a Collins GPS-4000 or GPS-4000A. Rockwell Collins Inc
- [STC ST01635WI-D](https://openairdocs.org/stc/ST01635WI-D): Modification of Rockwell Collins, Inc. VHF-4000 and VHF-4000E installations. Rockwell Collins Inc
- [STC ST02362LA](https://openairdocs.org/stc/ST02362LA): This modification reduces the passenger configuration to (9) passengers by removing one seat, in accordance with Master Document List SA3-1-02 revision A dated August 16, 2011 The Airplane Flight Manual Supplement, document number SA3-08-02, revision Original, dated August 9, 2011, or later FAA approved revision, is required with this installation. Strong Aero Engineering

All 155: https://openairdocs.org/aircraft/N918SJ/stcs.md

## Related

- Other Israel Aircraft Industries GULFSTREAM 200 aircraft: https://openairdocs.org/model/israel-aircraft-industries-gulfstream-200/aircraft.md
- The Pratt & Whitney Canada PW306A engine: https://openairdocs.org/engine/pratt-whitney-canada-pw306a.md

---
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.