# N709AA: 2001 Gulfstream Aerospace G-V

- Status: Valid registration
- Airframe: [Gulfstream Aerospace G-V](https://openairdocs.org/model/gulfstream-aerospace-g-v) (registry code 3980116, 20 seats)
- Engine: [BMW Rolls BR-700 series](https://openairdocs.org/engine/bmw-rolls-br-700-series) (registry code 09500)
- Data sheets: [TCDS A12EA](https://openairdocs.org/tcds/A12EA) (Gulfstream Aerospace Corporation) (OpenAirDocs)
- Serial number: 635
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 23, 2001
- Certificate issued: November 2, 2010
- Expires: November 30, 2029
- Mode S code: A975FE
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=709AA
- Page: https://openairdocs.org/aircraft/N709AA

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. The registry lists only the engine series, so ADs for every BMW Rolls BR-700 model are included.

## ADs that may apply (OpenAirDocs): 52 in force

### Matched by airframe (Gulfstream Aerospace G-V)

- [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 2023-02-02](https://openairdocs.org/ad/2023-02-02): Landing Gear System · Gulfstream Aerospace GV and GV-SP. Effective Feb 28, 2023
- [AD 2022-16-04](https://openairdocs.org/ad/2022-16-04): Horizontal Stabilizer Structure · Gulfstream Aerospace GV and GV-SP. Effective Sep 7, 2022
- [AD 2021-26-02](https://openairdocs.org/ad/2021-26-02): Landing Gear System · Gulfstream Aerospace GV and GV-SP. Effective Jan 14, 2022
- [AD 2021-06-04](https://openairdocs.org/ad/2021-06-04): Fuselage Structure · Gulfstream Aerospace GV. Effective May 4, 2021
- [AD 2017-20-08](https://openairdocs.org/ad/2017-20-08): Airborne Auxiliary Power and Fuselage · Gulfstream Aerospace G-IV, GIV-X, GV and 2 more. Effective Nov 6, 2017
- [AD 2017-08-01](https://openairdocs.org/ad/2017-08-01): Fuel · Gulfstream Aerospace GV and GV-SP. Effective May 17, 2017
- [AD 2016-22-04](https://openairdocs.org/ad/2016-22-04): Landing Gear; Fuselage; Nacelles/Pylons; Wings · Gulfstream Aerospace GV and GV-SP. Effective Dec 27, 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 2012-13-12](https://openairdocs.org/ad/2012-13-12): Flight controls · Gulfstream Aerospace G-IV, GIV-X, GV and 1 more. Effective Aug 1, 2012
- [AD 2011-24-02](https://openairdocs.org/ad/2011-24-02): Fire bottle, fixed · Gulfstream Aerospace GV and GV-SP. Effective Jan 3, 2012
- [AD 2009-08-01](https://openairdocs.org/ad/2009-08-01): Honeywell FMSs · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R), CL-600-2B16 (CL-604) and 11 more. Effective May 14, 2009
- [AD 2007-12-25](https://openairdocs.org/ad/2007-12-25): Forward water drain/supply valves · Gulfstream Aerospace GIV-X, GV and GV-SP. Effective Jul 5, 2007
- [AD 2006-18-13](https://openairdocs.org/ad/2006-18-13): Hardover prevention system (HOPS) in the roll axis due to a short circuit in the wiring harness · Gulfstream Aerospace GV and GV-SP. Effective Oct 13, 2006
- [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 2006-11-03](https://openairdocs.org/ad/2006-11-03): Left and right aileron and elevator actuators · Gulfstream Aerospace GV and GV-SP. Effective Jun 29, 2006
- [AD 2005-16-14](https://openairdocs.org/ad/2005-16-14): Floor heater pad system · Gulfstream Aerospace G-IV, GIV-X, GV and 1 more. Effective Aug 30, 2005
- [AD 2004-22-16](https://openairdocs.org/ad/2004-22-16): Crew oxygen bottle/supports · Gulfstream Aerospace GV and GV-SP. Effective Nov 19, 2004
- [AD 2004-02-01](https://openairdocs.org/ad/2004-02-01): Landing gear selector dump valve (LGSDV) · Gulfstream Aerospace GV. Effective Feb 6, 2004
- [AD 2003-18-11](https://openairdocs.org/ad/2003-18-11): Left and right ailerons · Gulfstream Aerospace GV. Effective Sep 26, 2003
- [AD 2002-21-03](https://openairdocs.org/ad/2002-21-03): Pilot's overhead circuit breaker panel · Gulfstream Aerospace GV. Effective Oct 21, 2002
- [AD 2001-21-06](https://openairdocs.org/ad/2001-21-06): Fire Extinguisher Bottles · Gulfstream Aerospace GV. Effective Nov 6, 2001
- [AD 2001-14-16](https://openairdocs.org/ad/2001-14-16): Nose Wheel Steering Actuator · Gulfstream Aerospace GV. Effective Aug 21, 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 98-18-15](https://openairdocs.org/ad/98-18-15): Wiring Harness Clearance · Gulfstream Aerospace GV. Effective Sep 18, 1998
- [AD 98-09-01](https://openairdocs.org/ad/98-09-01): Elevator Hardover Prevention Sys. (HOPS) · Gulfstream Aerospace GV. Effective May 5, 1998

### Matched by engine (BMW Rolls BR-700 series)

- [AD 2026-21-04](https://openairdocs.org/ad/2026-21-04): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Nov 23, 2026
- [AD 2025-06-03](https://openairdocs.org/ad/2025-06-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 23, 2025
- [AD 2023-17-11](https://openairdocs.org/ad/2023-17-11): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Sep 20, 2023
- [AD 2022-26-02](https://openairdocs.org/ad/2022-26-02): Accessory Gearboxes · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20, BR700-710C4-11 and 1 more. Effective Jan 27, 2023
- [AD 2021-21-12](https://openairdocs.org/ad/2021-21-12): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A2-20. Effective Dec 13, 2021
- [AD 2021-14-03](https://openairdocs.org/ad/2021-14-03): Turbine Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 19, 2021
- [AD 2021-12-07](https://openairdocs.org/ad/2021-12-07): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 12, 2021
- [AD 2018-18-14](https://openairdocs.org/ad/2018-18-14): Engine Controls · Rolls-Royce Deutschland BR700-710A2-20 and BR700-710C4-11. Effective Oct 12, 2018
- [AD 2016-13-12](https://openairdocs.org/ad/2016-13-12): Pawl carrier pivot pins · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 5, 2016
- [AD 2014-12-03](https://openairdocs.org/ad/2014-12-03): Fuel metering units (FMUs) · Rolls-Royce Deutschland BR700-725A1-12. Effective Jul 17, 2014
- [AD 2014-08-05](https://openairdocs.org/ad/2014-08-05): Low-pressure compressor (LPC) case ice impact panels · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 23, 2014
- [AD 2014-07-02](https://openairdocs.org/ad/2014-07-02): High-pressure (HP) compressor stages 1 to 6 rotor disc assemblies · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 8, 2014
- [AD 2013-12-03](https://openairdocs.org/ad/2013-12-03): Fuel pump tube · Rolls-Royce Deutschland BR700-725A1-12. Effective Jun 14, 2013
- [AD 2013-03-17](https://openairdocs.org/ad/2013-03-17): High-pressure turbine (HPT) stage 1 and stage 2 discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Mar 21, 2013
- [AD 2012-14-01](https://openairdocs.org/ad/2012-14-01): LP compressor booster rotor · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Oct 19, 2012
- [AD 2009-07-01 R1](https://openairdocs.org/ad/2009-07-01-R1): High-pressure (HP) turbine stage 1 discs, and HP turbine stage 2 discs · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 6, 2012
- [AD 2011-22-01](https://openairdocs.org/ad/2011-22-01): Touch-and-go and overshoot on life cycle counting · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Nov 23, 2011
- [AD 2010-25-05](https://openairdocs.org/ad/2010-25-05): Turbine Discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 13, 2011
- [AD 2009-21-04](https://openairdocs.org/ad/2009-21-04): Engine Failure · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Dec 3, 2009
- [AD 2009-04-13](https://openairdocs.org/ad/2009-04-13): Low pressure (LP) compressor (fan) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Mar 26, 2009
- [AD 2005-21-05](https://openairdocs.org/ad/2005-21-05): Fan discs and fan blades · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Nov 25, 2005
- [AD 2005-16-12](https://openairdocs.org/ad/2005-16-12): Independent Overspeed Protection (IOP) unit. · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 26, 2005
- [AD 2000-25-51](https://openairdocs.org/ad/2000-25-51): High Pressure Turbine Disks · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Feb 20, 2001
- [AD 2001-01-01](https://openairdocs.org/ad/2001-01-01): Oil Filter · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Jan 31, 2001
- [AD 98-24-03 R1](https://openairdocs.org/ad/98-24-03-R1): Combustion Core Fairings · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Dec 27, 1999

### Historical (superseded or no longer in force)

- [AD 2013-22-19](https://openairdocs.org/ad/2013-22-19) (historical): Fuel boost pump · Gulfstream Aerospace GV and GV-SP. Effective Jan 7, 2014
- [AD 2009-17-01](https://openairdocs.org/ad/2009-17-01) (historical): Airborne Auxiliary Power · Gulfstream Aerospace G-IV, GIV-X, GV and 1 more. Effective Aug 26, 2009
- [AD 2022-24-06](https://openairdocs.org/ad/2022-24-06) (historical): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 6, 2023
- [AD 2013-05-13](https://openairdocs.org/ad/2013-05-13) (historical): Fuel pump splined couplings · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 24, 2013
- [AD 2012-26-14](https://openairdocs.org/ad/2012-26-14) (historical): High-pressure (HP) compressor stages 1 to 6 rotor disc assembly · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Jan 10, 2013
- [AD 2009-07-01](https://openairdocs.org/ad/2009-07-01) (historical): High Pressure (HP) Turbine · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Apr 27, 2009
- [AD 2003-07-11](https://openairdocs.org/ad/2003-07-11) (historical): Fan discs · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Apr 28, 2003
- [AD 2001-05-06](https://openairdocs.org/ad/2001-05-06) (historical): Fan Disk · BMW Rolls-Royce BR700-710A1-10 and BR700-710A2-20. Effective Mar 29, 2001

## Information bulletins (advisory) (4 in force)

- [SAIB CE-19-20](https://openairdocs.org/saib/CE-19-20): Flight Compartment Windows. Issued Dec 5, 2019
- [SAIB NM-15-02](https://openairdocs.org/saib/NM-15-02): Cabin Equipment/Furnishings. Issued Nov 6, 2014
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NM-07-55](https://openairdocs.org/saib/NM-07-55): Air Conditioning  Pack Inlet Valve Operation. Issued Sep 24, 2007

## NTSB investigations

None matched to N709AA.

## FAA accident and incident reports

None matched to N709AA.

## Service difficulty reports (1)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 2022F00336](https://openairdocs.org/sdr/2022F00336), Sep 9, 2022: PMA. SWOLLEN. ENGINE FAILURE ON CLIMB PASSING FL270 THE RIGHT ENGINE FAILED. R CONT IGN WAS SELECTED IN ORDER TO ATTEMPT AN AUTOMATIC RELIGHT. NO RELIGHT. ENGINE WIND MILLING

## Service difficulty reports on N709AA not matched to an aircraft (41)

They name N709AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DHL2002752001](https://openairdocs.org/sdr/DHL2002752001), May 17, 2002: METERING VALVE. FAILED. DURING MAX POWER ASSURANCE RUN, PARKING BRAKE FAILS TO SECURE A/C EPR IS 1.4 AND ABOVE. MLG BRAKES SAME AT POWER SETTING 1.6 AND ABOVE. PERFORMED PARKING T/S+RI
- [SDR AALA20010101](https://openairdocs.org/sdr/AALA20010101), Jan 22, 2001: CONTACTOR. DIRTY. MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONTACT AT AFT AIRSTAIR. SYSTEM GROUND CHECKE
- [SDR AALA20001465](https://openairdocs.org/sdr/AALA20001465), Sep 7, 2000: LIGHT. INOPERATIVE. DFW DURING OVERNIGHT MAINTENANCE AFT AIRSTAIRS EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AFT AIR STAIRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED N
- [SDR AALA20001466](https://openairdocs.org/sdr/AALA20001466), Sep 7, 2000: LIGHT. INOPERATIVE. DFW DURING OVERNIGHT MAINTENANCE AFT CARGO EXTERNAL EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AFT AIR CARGO EXTERNAL EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GRO
- [SDR AALA20001444](https://openairdocs.org/sdr/AALA20001444), Sep 3, 2000: CONTACTOR. LOOSE. MIA DURING OVERNIGHT MAINTENANCE AFT STAIRWAY OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONTACTS. SYSTEM GROUND CHECKED NORMAL OPE
- [SDR AALA20000721](https://openairdocs.org/sdr/AALA20000721), Apr 26, 2000: SKIN. CORRODED. TUL - CORROSION ON LOWER SKIN CENTER SECTION TANK. INSTALLED REPAIR PER SRM 57-30-3 FIG 7 AND FIG 8. (X)
- [SDR AALA20000719](https://openairdocs.org/sdr/AALA20000719), Apr 25, 2000: BEAM. CORRODED. TUL - CORROSION ON UPPER LEFT OUTBOARD TE BEAM AT NR 7 ELEVATOR HINGE AREA. REMOVED CORROSION, INSTALLED DOUBLER PER ESO 11697 DAED 4-25-00. (X)
- [SDR AALA20000720](https://openairdocs.org/sdr/AALA20000720), Apr 20, 2000: SKIN. SCRATCHED. TUL - DEEP SCRATCH IN SKIN STA 412, STR 24R. INSTALLED REPAIR AT STA 412, STR 24R IAW SRM 53-30-3. (X)
- [SDR AALA20000575](https://openairdocs.org/sdr/AALA20000575), Apr 1, 2000: LIGHT. INOPERATIVE. DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS UNDER EXIT MARKER ADJACENT TO AFT SERVICE DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR P
- [SDR AALA991388](https://openairdocs.org/sdr/AALA991388), Sep 13, 1999: LIGHT. INOPERATIVE. RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHT AT VENTRAL STAIRS INOPERATIVE. CLEANED AND ADJUSTED ELECTRICAL CONTACTS OF BATTERY/CHARGER TO 
- [SDR AALA991076](https://openairdocs.org/sdr/AALA991076), Jul 22, 1999: LIGHT. DEFECTIVE. LGA - FLT 1886 - DURING LANDING AT LGA COCKPIT EMERGENCY EXIT LIGHTS ILLUMINATED AND REMAINED ILLUMINATED WITH SWITCH TURNED OFF. REPLACED COCKPIT EMERGENCY EXI
- [SDR AALA991015](https://openairdocs.org/sdr/AALA991015), Jul 6, 1999: SPLICE. CORRODED. TUL - FOUND CORROSION ON STRINGER SPLICE AT BS 480. REMOVED CORRODED STRINGER SPLICE AND INSTALLED REPAIR SPLICE PE SRM 53-10-3. (M)
- [SDR AALA991016](https://openairdocs.org/sdr/AALA991016), Jul 2, 1999: FRAME. CORRODED. TUL - FOUND CORROSION ON SHEAR TIE STATION 700 BETWEEN STRINGER 27R AND 28R. INSTALLED DOUBLER ON SHEAR TIE STATION 700 BETWEEN STRINGER 27 AND 28R PER SRM 53-1
- [SDR AALA980099](https://openairdocs.org/sdr/AALA980099), Jan 12, 1998: TRANSFORMER. DEFECTIVE. ORD - FLT 1391 - AFTER TAKEOFF, COCKPIT CREW NOTED A LIGHT, BUT DEFINITE ELECTRICAL BURNING SMELL BEHIND FLIGHT ENGINEER'S PANEL. CREW PULLED RADIO PRIMARY CURC
- [SDR 98ZZZX327](https://openairdocs.org/sdr/98ZZZX327), Jan 12, 1998: BREAKER. SMOKE. ORD - AFTER TAKEOFF, SMOKE AND FUMES FROM BEHIND F/E. PULLED RADIO PRIMARY CIRCUIT BREAKER AND SMOKE AND FUMES WENT AWAY. REF: PREVIOUS WRITE-UP 07. REPLACED PA
- [SDR AALA972182](https://openairdocs.org/sdr/AALA972182), Nov 17, 1997: WIRE. LOOSE. MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT MID CABIN WOULD NOT TEST. SECURED WIRING, SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA972178](https://openairdocs.org/sdr/AALA972178), Nov 16, 1997: CONNECTOR. LOOSE. MIA - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING AT MID CABIN INOPERATIVE. SECURED SEGMENT OF EMERGENCY EXIT FLOOR PATH LIGHTING AT MID CA
- [SDR AALA971308](https://openairdocs.org/sdr/AALA971308), Jul 21, 1997: SKIN. CORRODED. TUL - CORROSION ON FUSELAGE SKIN INSIDE AFT CARGO ADJACENT TO OUTBOARD FLANGE OF STR 29R, STA 990 - STA 996. REPAIRED PER SRM 53-10-3, FIG 3 AND SRM 53-30-3, FI
- [SDR AALA971307](https://openairdocs.org/sdr/AALA971307), Jul 21, 1997: STRINGER. CRACKED. TUL - CRACK IN OUTBOARD FLANGE RADIUS IN STR 29R, STA 990 TO STA 995. INSTALLED STR 29R REPAIR PER SRM 53-10-3, FIG 1. INSTALLED SKIN REPAIR DOUBLER AND TRIPLER
- [SDR AALA971306](https://openairdocs.org/sdr/AALA971306), Jul 21, 1997: SKIN. CRACKED. TUL - FORWARD ENTRY DOOR UPPER HINGE CUT-OUT CRACKED. VERIFIED WITH HFEC (MARKED) EXTERNAL. ROUTED OUT CRACK AND INSTALLED DOUBLER AND FILLERS IAW SB 727-53-019
- [SDR AALA971305](https://openairdocs.org/sdr/AALA971305), Jul 21, 1997: ANGLE. CRACKED. TUL - NR 5 LEADING EDGE INBOARD ATTACH ANGLE CRACKED LOWER LEG. INSTALLED NEW ACTUATOR MOUNT INBOARD NR 5 SLAT. TST: 43,979 HOURS. CYCLES, 23,050. (X)
- [SDR AALA971309](https://openairdocs.org/sdr/AALA971309), Jul 1, 1997: SKIN. CRACKED. TUL - FIXED LEADING EDGE SKIN CRACKED 7 INCHES LONG AFT OF NR 5 SLAT OUTBOARD END. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PER SRM 57-30-4, PAGES 11A AND 11B
- [SDR AALA961862](https://openairdocs.org/sdr/AALA961862), Dec 24, 1996: HARNESS. DEFECTIVE. DFW - DURING OVERNIGHT MAINTENANCE, FOUND AFT CARGO EMERGENCY LIGHT INOPERATIVE. REPLACED AFT CARGO DOOR HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA961188](https://openairdocs.org/sdr/AALA961188), Aug 5, 1996: FLOOR BEAM. CORRODED. TUL - FOUND FLOOR BEAM CORRODED FROM INBOARD SEAT TRACK TO OUTBOARD CREASE ANGLE RIGHT STATION 380. CUT OUT CORRODED FLOOR BEAM UPPER FLANGE AND REPAIRED PER SR
- [SDR AALA961187](https://openairdocs.org/sdr/AALA961187), Aug 5, 1996: DOOR FRAME. CORRODED. TUL - FOUND FORWARD GALLEY FORWARD DOOR FRAME HAS CORROSION AT STRINGER 17R TO 'I' ABOVE 17R, STATION 376-377. CUT OUT CORROSION AREA, MADE AND INSTALLED FILLER
- [SDR AALA961186](https://openairdocs.org/sdr/AALA961186), Aug 5, 1996: SKIN. CORRODED. TUL - FOUND CORROSION ON SKIN AFT OF BUTTE AIR DOOR. REMOVED CORROSION. INSTALLED DOUBLER PER ESO 11697, DATED 6-28-96 AND SRM 53-30-3 FIG 2/3. (M)
- [SDR AALA961185](https://openairdocs.org/sdr/AALA961185), Aug 5, 1996: DOOR FRAME. CORRODED. TUL - FOUND GALLEY DOOR SUPPORT FRAME HAS CORROSION AT STA 372, STRINGER 17R TO 6 INCHES ABOVE 17R. FABRICATED AND INSTALLED FORMED ANGLE REPAIR PER SRM 51-40-3
- [SDR AALA961184](https://openairdocs.org/sdr/AALA961184), Aug 5, 1996: SKIN. CORRODED. TULE - FOUND CORROSION ON BELLY SKIN BETWEEN STRINGERS 28L-28R AND STATIONS 700-720 PLUS 10. REPLACED BELLY SKIN FROM STATION 680-720A AND STRINGER 28L - 28R PE
- [SDR AALA961183](https://openairdocs.org/sdr/AALA961183), Aug 5, 1996: FLOOR PNL. CORRODED. TUL - FOUND LEFT AFT LAVATORY FLOOR CORRODED THREE PLACES AND AROUND THE PUMP SHUTE TO THE ANGLE AT THE DITCHING PANELS. MADE STAINLESS STEEL WEB REPAIR, CAD-PL
- [SDR AALA961182](https://openairdocs.org/sdr/AALA961182), Aug 5, 1996: STRUCTURE. CORRODED. TUL - FOUND CORROSION LOWER FUSELAGE RIGHT INSIDE A/C BAY STATION 783.95 TO 804.5, 2 SMALL AREAS. REMOVED CORROSION BEYOND SRM LIMITS 57-30-1 BY ESO 11697, DATE
- [SDR AALA961181](https://openairdocs.org/sdr/AALA961181), Aug 5, 1996: SPLICE. CORRODED. TUL - FOUND CORROSION ON THE STRINGER 18 SPLICES PLATE RIGHT. REMOVED AND TREATED CORROSION, BLENDOUT BEYOND MM AND SRM LIMITS. REPAIRED PER BOEING MESSAGE AND 
- [SDR AALA961180](https://openairdocs.org/sdr/AALA961180), Aug 5, 1996: DRAG BRACE. CORRODED. TUL - FOUND DRAG BRACE BUSHING BORES CORRODED BEYOND ALLOWABLE LIMITS 2.730. REMOVED AND REPLACED DRAG BRACE PER DWG NR 6518413 AND SRM 53-43-1 PG 1. (M)
- [SDR AALA961179](https://openairdocs.org/sdr/AALA961179), Aug 5, 1996: TQ BOX WEB. CRACKED. TUL - FOUND 2 INCH CRACK IN RIGHT TORQUE BOX WEB BELOW AIR STAIR ACTUATOR. INSTALLED WEB REPAIR ON TORQUE BOX PER SB 727-53-0129 DATED 11-7-91 FIG 1-4. (M)
- [SDR AALA961178](https://openairdocs.org/sdr/AALA961178), Aug 5, 1996: STRINGER. CRACKED. TUL - FOUND VERT FIN INTERIOR, STRINGER 9L, CRACKED AT BOLT ATTACH POINT TO RIB NR 2. REPAIRED WITH DOUBLER PER ESO 11697, DATED 7-1-96. (M)
- [SDR AALA961177](https://openairdocs.org/sdr/AALA961177), Aug 5, 1996: SKIN. WORN. TUL - FOUND LEFT LEADING EDGE WING RUBBING FUSELAGE 2 SPOTS STATIONS 720D AND 720E, STRINGER 18L AND STRINGER 19. CUT OUT WORN SPOTS (2) ON FUSELAGE. INSTALLED 
- [SDR AALA961176](https://openairdocs.org/sdr/AALA961176), Aug 5, 1996: SKIN. CORRODED. TUL - FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE SKIN CORRODED, AT UPPER SKIN ABOVE OUTBOARD ELEVATOR FITTING. REMOVED CORROSION, TREATED AND INSTALLED EXTE
- [SDR AALA961175](https://openairdocs.org/sdr/AALA961175), Aug 5, 1996: ACT BRACKET. CORRODED. TUL - FOUND CORROSION VERTICAL BRACKET 11B NR 5 LSAT ACTUATOR BY NR 3 FUEL VALVE. REMOVED AND REPLACED BRACKET WITH NEW SERVICABLE BRACKET. (M)
- [SDR AALA961174](https://openairdocs.org/sdr/AALA961174), Aug 5, 1996: SPAR. CORRODED. TUL - FOUND CORROSION ON FORWARD WING SPAR AND LOWER CHORD ANGLE. CORROSION REMOVED INSTALLED DOUBLERS PER SRM 57-10-6 PG 2A-2C, 6, 7, AND 9. (M)
- [SDR AALA951869](https://openairdocs.org/sdr/AALA951869), Oct 28, 1995: SWITCH. DEFECTIVE. DFW - FLT 1039 - DURING APPROACH TO DFW WHEN LANDING GEAR EXTENDED, RT MLG DOOR LIGHT ON F/E PANEL DID NOT ILLUMINATE WHEN GEAR DOORS OPENED. ALL OTHER INDICATI
- [SDR AALA951868](https://openairdocs.org/sdr/AALA951868), Oct 28, 1995: EEL CONNECTOR. DEFECTIVE. RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 3EF TO 17DEF FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR
- [SDR AALA950196](https://openairdocs.org/sdr/AALA950196), Feb 2, 1995: SLIDE. DEFECTIVE. ORD - DURING SHOP VISIT, EMERGENCY EVACUATION SLIDE GIRT FOUND UNGLUED APPROXIMATELY 1.0 INCH AT MATING SURFACE. SLIDE INTRODUCED TO SHOP FOR REPAIR. (X)

## STCs that may be installed (OpenAirDocs) (328, 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 (Gulfstream Aerospace G-V)

- [STC ST11970AT](https://openairdocs.org/stc/ST11970AT): Installation of Honeywell MKV-A EGPWS System. Gulfstream Aerospace Corporation
- [STC ST04817NY](https://openairdocs.org/stc/ST04817NY): Replacement of OEM Standard 44 amp-hour batteries. ALOFT AeroArchitects
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [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 ST04572AT](https://openairdocs.org/stc/ST04572AT): Installation of SpaceX Starlink Aviation System. Gulfstream Aerospace Corporation
- [STC ST04099NY](https://openairdocs.org/stc/ST04099NY): Installation of Satcom Direct Plane Simple. Delta Engineering Corporation
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [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 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 ST04611CH](https://openairdocs.org/stc/ST04611CH): INSTALLATION OF A SPACE-X STARLINK AVIATION SYSTEM. Nextant Aerospace
- [STC ST04344AT-D](https://openairdocs.org/stc/ST04344AT-D): Installation of Satcom Direct Plane Simple KU System. Gulfstream Aerospace Corporation
- [STC ST04543AT](https://openairdocs.org/stc/ST04543AT): Honeywell RT-300 Radio Altimeter Bandpass Filter Installation (FAA AD 2023-10-02 Terminating Action). Gulfstream Aerospace Corporation
- [STC ST04273CH](https://openairdocs.org/stc/ST04273CH): Installation of a GOGO Avance L5 Integrated in-flight connectivity system. Pentastar Aviation LLC
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST01109DE](https://openairdocs.org/stc/ST01109DE): Installation of Gogo MB13 Antennas. Peregrine
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions 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 ST04348AT-D](https://openairdocs.org/stc/ST04348AT-D): Installation of Honeywell AIS-2000 High Definition (HD) Upgrade. Gulfstream Aerospace Corporation
- [STC ST00126IB](https://openairdocs.org/stc/ST00126IB): Replacement of Halon agent with alternate Halon-free Portable Fire Extinguisher agent. AMAC Aerospace Switzerland AG
- [STC ST00105IB](https://openairdocs.org/stc/ST00105IB): Introduction of Activation of Wireless Charging Systems for Portable Electronic Devices. AMAC AEROSPACE SWITZERLAND AG
- [STC ST01985WI](https://openairdocs.org/stc/ST01985WI): Installation of the Garmin GI-275 I Electronic Standby Instrument (ESI). Peregrine
- [STC ST04787NY](https://openairdocs.org/stc/ST04787NY): Installation of True Blue Power TFC4000 AC-to-AC Converter. Sterling Helicopter
- [STC ST01097DE](https://openairdocs.org/stc/ST01097DE): Installation to Replace Nickel Cadmium Original Equipment Batteries with Valve Regulated Lead-Acid Batteries. Concorde Battery Corporation
- [STC ST01987WI](https://openairdocs.org/stc/ST01987WI): Limitation of Maximum Passenger Capacity to Nine (9). Duncan Aviation Inc
- [STC ST04345AT-D](https://openairdocs.org/stc/ST04345AT-D): Replace existing Flight Data Recorder with an Universal FDR-25. Gulfstream Aerospace Corporation
- [STC ST04335AT-D](https://openairdocs.org/stc/ST04335AT-D): Installation of Honeywell Display Unit Software Upgrade with SXM Weather. Gulfstream Aerospace Corporation
- [STC ST00179MC](https://openairdocs.org/stc/ST00179MC): ARC-210 Safe Carriage Installation. Gulfstream Aerospace Corporation
- [STC ST04338AT-D](https://openairdocs.org/stc/ST04338AT-D): Installation of L3 Harris GH-3900.2 Secondary Flight Display. Gulfstream Aerospace Corporation
- [STC ST01159CH](https://openairdocs.org/stc/ST01159CH): Install air ambulance conversion. Spectrum Aeromed LLC dba Spectrum Aeromed
- [STC ST04352AT](https://openairdocs.org/stc/ST04352AT): Installation of a Talon Aerospace LED Replacement Navigation / Position Light. Aaxico Technical Services Inc
- [STC ST02469SE](https://openairdocs.org/stc/ST02469SE): Installation of a ViaSat VR-12C system. ALOFT AeroArchitects
- [STC ST04002AT](https://openairdocs.org/stc/ST04002AT): Installation of a Talon LED Replacement Wing and Tail Mounted Anti-Collision Lights. Aaxico Technical Services Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04339AT-D](https://openairdocs.org/stc/ST04339AT-D): Installation of Air Ionizer System. Gulfstream Aerospace Corporation
- [STC ST04480CH](https://openairdocs.org/stc/ST04480CH): Installation of a Collins KuSAT-2000 Tail-Mounted SATCOM system in accordance with Western Jet Aviation Master Data list 1469900 Revision (B), dated January 13, 2021 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST00412BO](https://openairdocs.org/stc/ST00412BO): Installation of Whelen non-required underwing wingtip flood lights. Whelen Aerospace Technologies
- [STC ST04329AT-D](https://openairdocs.org/stc/ST04329AT-D): Installation of a Ka Broadband High Speed Data System. Gulfstream Aerospace Corporation
- [STC ST00001MC-D](https://openairdocs.org/stc/ST00001MC-D): Installation of a Directional Infrared Countermeasures System. Gulfstream Aerospace Corporation
- [STC ST04333AT-D](https://openairdocs.org/stc/ST04333AT-D): Installation of Satcom Direct Gateway and WiFi Hub System. Gulfstream Aerospace Corporation
- [STC ST02932AT](https://openairdocs.org/stc/ST02932AT): Installation of an interior arrangement and exterior on model GV, serial numbers 683 and 689 ONLY. Fokker 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 ST04483NY](https://openairdocs.org/stc/ST04483NY): Installation of Astronics T-310 KU SATCOM HSD System. Gulfstream Aerospace Ltd
- [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 ST04432CH](https://openairdocs.org/stc/ST04432CH): Upgrade of a Honeywell LASEREF Inertial Reference System in accordance with Western Jet Aviation Master Data List 1037254, Revision (B), dated January 9, 2020 or later FAA approved revision. StandardAero Business Aviation Services LLC

All 328: https://openairdocs.org/aircraft/N709AA/stcs.md

## Related

- Other Gulfstream Aerospace G-V aircraft: https://openairdocs.org/model/gulfstream-aerospace-g-v/aircraft.md
- The BMW Rolls BR-700 series engine: https://openairdocs.org/engine/bmw-rolls-br-700-series.md

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