Gulfstream V airworthiness directives FAA ADs that may apply, with the official text
- In effect
- 30
- Recurring
- 6
- Superseded or removed5
- Latest2023-02-02
Gulfstream V: price, specs and every tail number · Look up ADs by N-number · AD burden by model, ranked
IN EFFECT
30 V ADs in effect, newest first
Informational only. These are FAA airworthiness directives whose published applicability names this make and model. Whether an AD applies to a particular aircraft depends on its serial number, installed engines, propellers, parts and modifications, and some ADs listed here will not apply. This list is not the official AD record and not a compliance determination: confirm applicability and compliance against the FAA’s Dynamic Regulatory System and the aircraft’s records with a certificated mechanic or inspector. Covers ADs published in the Federal Register since 1995, through Oct 1, 2026; older ADs, and engine, propeller and appliance ADs that do not name the aircraft, are not included.
- AD 2023-02-02 One-time
Gulfstream Aerospace Corporation Airplanes
This AD was prompted by the omission of a life limit in the airworthiness limitations section (ALS) for a certain main landing gear (MLG) trunnion pin.
Applicability, as the AD words it
This AD applies to Gulfstream Aerospace Corporation Model GV and GV-SP airplanes, all serial numbers, certificated in any category.
- AD 2022-16-04 One-time
Gulfstream Aerospace Corporation Airplanes
The FAA is issuing this AD to detect and correct bond line corrosion, which if not addressed, could result in compromise of the structural integrity of the horizontal stabilizer and lead to loss of control of the airplane.
Applicability, as the AD words it
This AD applies to Gulfstream Aerospace Corporation Model GV and GV-SP airplanes, all serial numbers, certificated in any category.
- AD 2021-26-02 One-time
Gulfstream Aerospace Corporation Airplanes
This AD was prompted by the omission of a life limit in the airworthiness limitations section (ALS) for a certain main landing gear (MLG) trunnion pin.
Applicability, as the AD words it
This AD applies to Gulfstream Aerospace Corporation Model GV and GV-SP airplanes, all serial numbers, certificated in any category.
- AD 2021-06-04 One-time
Gulfstream Aerospace Corporation Airplanes
This AD was prompted by a report that current inspection procedures of floor beam support links, which can fail due to corrosion, are inadequate.
Applicability, as the AD words it
This AD applies to Gulfstream Aerospace Corporation Model GV airplanes, all serial numbers, certificated in any category.
- AD 2017-20-08 One-time
Gulfstream Aerospace Corporation Airplanes
This AD was prompted by a report indicating that the type design sealant (Aerospace Material Specification (AMS) 3374), as applied to the auxiliary power unit (APU) enclosure (firewall), does not meet the requirement in 14 CFR 25.1191(b)(1) for a firewall to be fireproof, and failed a certification test and a company test.
Applicability, as the AD words it
This AD applies to the Gulfstream Aerospace Corporation airplanes, certificated in any category, identified in paragraphs (c)(1) through (c)(5) of this AD. (1) Model G-IV airplanes, having serial numbers (S/Ns) 1000 and subsequent. (2) Model GIV-X airplanes, having S/Ns 4001 and subsequent. (3) Model GV airplanes, having S/Ns 501 and subsequent. (4) Model GV-SP airplanes, having S/Ns 5001 and subsequent. (5) Model GVI airplanes, having S/Ns 6001 and subsequent.
- AD 2017-08-01 One-time
Gulfstream Aerospace Corporation Airplanes
This AD was prompted by reports of two independent types of failure of the fuel boost pump with overheat damage found on the internal components and external housing on one of the failure types, and fuel leakage on the other.
Applicability, as the AD words it
This AD applies to all Gulfstream Aerospace Corporation Model GV and GV-SP airplanes, certificated in any category.
- AD 2016-22-04 One-time
Gulfstream Aerospace Corporation Airplanes
This AD was prompted by a new revision to the Airworthiness Limitations Section (ALS) of the Aircraft Maintenance Manual (AMM), Chapter 05-10-10, based on fatigue and damage tolerance testing, and updated analysis.
Applicability, as the AD words it
This AD applies to Gulfstream Aerospace Corporation Model GV airplanes, certificated in any category, serial numbers 501 through 693 inclusive and serial number 699; and Model GV-SP airplanes, certificated in any category, serial numbers 5001 through 5433 inclusive.
- AD 2016-18-11 One-time
Gulfstream Aerospace Corporation Airplanes
This AD was prompted by a report that the right main landing gear (MLG) failed to extend due to fatigue cracking of the end cap fitting.
Applicability, as the AD words it
This AD applies to the Gulfstream Aerospace Corporation airplanes, certificated in any category, identified in paragraphs (c)(1) through (c)(7) of this AD. (1) All Model G-1159 airplanes. (2) All Model G-1159A airplanes. (3) All Model G-1159B airplanes. (4) All Model G-IV airplanes. (5) All Model GV airplanes. (6) Model GIV-X airplanes, serial numbers 4001 through 4350 inclusive. (7) Model GV-SP airplanes, serial numbers 5001 through 5542 inclusive.
- AD 2012-13-12 One-time
Gulfstream Aerospace Corporation Airplanes
This AD was prompted by reports of failure to inspect or document the paint thickness on flight controls (ailerons, rudder, elevator), potentially having a negative impact on the flutter characteristics of the airplane.
Applicability, as the AD words it
This AD applies to the airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category. (1) Gulfstream Aerospace Corporation Model G-IV airplanes, serial numbers 1265, 1286, 1298, 1301, 1347, 1372, 1378, 1380, 1423, 1458, and 1497. (2) Gulfstream Aerospace Corporation Model GIV-X airplanes, serial numbers 4064, 4151, 4192, 4194, 4199, and 4214. (3) Gulfstream Aerospace Corporation Model GV airplanes, serial numbers 612, 630, and 691. (4) Gulfstream Aerospace Corporation Model GV-SP airplanes, serial numbers 5038, 5079, 5223, 5227, 5237, 5240, 5245, 5246, 5252, 5258, 5261, 5265, 5267, 5283, 5290, 5293, 5294, 5302, 5307, 5311, 5318, and 5320.
- AD 2011-24-02 One-time
Gulfstream Aerospace Corporation Model GV and GV-SP Airplanes
This AD was prompted by notification from the airplane manufacturer that the third fire extinguisher bottle is mounted in a small-fragment impact zone.
Applicability, as the AD words it
This AD applies to the Gulfstream Aerospace Corporation airplanes, certificated in any category, identified in paragraphs (c)(1) and (c)(2) of this AD. (1) Model GV airplanes having serial numbers (S/Ns) 501 and subsequent. (2) Model GV-SP airplanes having S/Ns 5001 through 5308 inclusive.
- AD 2011-22-01 One-time Engine
Rolls-Royce Deutschland Ltd & Co KG (RRD) BR700-710 Series Turbofan Engines
We are issuing this AD to prevent failure of high-energy, life- limited parts, uncontained engine failure, and damage to the airplane.
Applicability, as the AD words it
This AD applies to all Rolls-Royce Deutschland BR700-710A1- 10 and BR700-710A2-20 turbofan engines, all BR700-710C4-11 model engines that have hardware configuration standard 710C4-11 engraved on the engine data plate (Service Bulletin SB-BR700-72-101466 standard not incorporated), and all BR700-710C4-11 model engines that have hardware configuration standard 710C4-11/10 engraved on the engine data plate (Service Bulletin SB-BR700-72-101466 standard incorporated). These engines are installed on, but not limited to, Bombardier BD-700-1A10 and BD-700-1A11 airplanes and Gulfstream GV (G500) and GV-SP (G550) airplanes.
- AD 2010-25-05 One-time Engine
Rolls-Royce Deutschland Ltd & Co KG Models BR700-710A1-10; BR700-710A2-20; and BR700-710C4-11 Turbofan Engines
We are issuing this AD to prevent failure of the HPT stage 1 and stage 2 discs, uncontained engine failure, and damage to the airplane.
Applicability, as the AD words it
This AD applies to Rolls-Royce Deutschland Ltd & Co KG models BR700-710A1-10, BR700-710A2-20, and BR700-710C4-11 turbofan engines with any of the high-pressure turbine (HPT) stage 1 and stage 2 discs installed as listed by part number (P/N) in Table 1 and Table 2 of this AD. These engines are installed on, but not limited to, Gulfstream model G-V and GV-SP airplanes, and Bombardier model BD-700-1A10 and BD-700-1A11 airplanes. Table 1--Declared Safe Cyclic Life of Affected HPT Stage 1 Discs Declared safe HPT stage 1 disc P/N Engine model cyclic life (flight cycles) BRR21215: BR700-710A1-10: 6,075 BRR21215: BR700-710A2-20: 5,950 BRR22005: BR700-710A1-10: 6,200 BRR22005: BR700-710A2-20: 6,200 BRR22006: BR700-710A1-10: 6,200 BRR22006: BR700-710A2-20: 6,200 BRR22007: BR700-710A1-10: 6,200 BRR22007: BR700-710A2-20: 6,200 BRR22358: BR700-710A1-10: 6,200 BRR22358: BR700-710A2-20: 6,200 BRR23864: BR700-710A1-10: 6,200 BRR23864: BR700-710A2-20: 6,200 BRR23884: BR700-710A1-10: 6,200 BRR23884: BR700-710A2-20: 6,200 BRR23885: BR700-710A1-10: 6,200 BRR23885: BR700-710A2-20: 6,200 BRR23952: BR700-710A1-10: 6,200 BRR23952: BR700-710A2-20: 6,200 BRR23952: BR700-710C4-11 6,200 (Service Bulletin (SB) No. SB-BR700-72- 101466 not incorporated). BRR23952: BR700-710C4-11 (SB No. 3,800 SB-BR700-72-101466 incorporated). BRR23953: BR700-710A1-10: 6,200 BRR23953: BR700-710A2-20: 6,200 BRR23953: BR700-710C4-11 (SB No. 6,200 SB-BR700-72-101466 not incorporated). BRR23953: BR700-710C4-11 (SB No. 3,800 SB-BR700-72-101466 incorporated). BRR23954: BR700-710A1-10: 6,200 BRR23954: BR700-710A2-20: 6,200 Table 2--Declared Safe Cyclic Life of Affected HPT Stage 2 Discs Declared safe HPT stage 2 disc P/N Engine model cyclic life (flight cycles) BRR18291: BR700-710A1-10: 9,300 BRR21214: BR700-710A1-10: 9,600 BRR21214: BR700-710A2-20: 9,600 BRR22008: BR700-710A1-10: 10,500 BRR22008: BR700-710A2-20: 10,500 BRR22008: BR700-710C4-11 (SB No. 10,500 SB-BR700-72-101466 not incorporated). BRR22008: BR700-710C4-11 (SB No. 3,700 SB-BR700-72-101466 incorporated). BRR22009: BR700-710A1-10: 10,500 BRR22009: BR700-710A2-20: 10,500 BRR22009: BR700-710C4-11 (SB No. 10,500 SB-BR700-72-101466 not incorporated). BRR22009: BR700-710C4-11 (SB No. 3,700 SB-BR700-72-101466 incorporated). BRR22010: BR700-710A1-10: 10,500 BRR22010: BR700-710A2-20: 10,500 BRR22359: BR700-710A1-10: 10,500 BRR22359: BR700-710A2-20: 10,500
- AD 2009-08-01 One-time
Honeywell Flight Management Systems (FMSs) Equipped With Honeywell NZ-2000 Navigation Computers and Honeywell IC-800 or IC-800E Integrated Avionics Computers; as Installed on Various Transport Category Airplanes
We are issuing this AD to prevent a shift in the FMS computed position, which could result in uncommanded deviations from the intended flight path of the airplane and, if those deviations are undetected by the flight crew, compromised terrain/traffic avoidance.
Applicability, as the AD words it
This AD applies to all Honeywell NZ-2000 navigation computers and Honeywell IC-800 or IC-800E integrated avionics computers; as installed on transport category airplanes, certificated in any category, including but not limited to the airplanes identified in Table 1 of this AD. Table 1--Known Affected Airplanes Manufacturer Model Bombardier, Inc: CL-600-2B16 (CL-601-3A, CL-601- 3R, and CL-604) airplanes. Dassault Aviation: Mystere-Falcon 900 airplanes. Gulfstream Aerospace Corporation: G-1159A and GV airplanes, and G- IV series airplanes. Lockheed: 382G series airplanes. Hawker Beechcraft (formerly Raytheon BAe.125 Series 800A (including Aircraft Company). C-29A and U-125) airplanes. Hawker 800XP and 1000 airplanes.
- AD 2007-12-25 Recurring
Gulfstream Model GIV-X, GV, and GV-SP Series Airplanes
We are issuing this AD to prevent leakage from failed water drain/ supply valves allowing the build-up of ice on the airplane, which could separate and strike the airplane structure aft of the failed valves; become ingested by a propulsion engine; or become a hazard to persons or property on the ground.
Applicability, as the AD words it
This AD applies to Gulfstream Model GIV-X, GV, and GV-SP series airplanes, certificated in any category; as identified in the alert customer bulletins specified in Table 1 of this AD. Table 1.--Gulfstream Alert Customer Bulletins Airplane model Alert Customer Bulletin Date GIV-X: G350 Number 5: April 11, 2007. G450 Number 5: April 11, 2007. GV: GV Number 26: April 11, 2007. GV-SP: G500 Number 7: April 11, 2007. G550 Number 7: April 11, 2007.
- AD 2006-18-13 One-time
Gulfstream Model GV and GV-SP Series Airplanes
We are issuing this AD to prevent the loss of the hardover prevention system (HOPS) in the roll axis due to a short circuit in the wiring harness, which could result in reduced controllability of the airplane.
Applicability, as the AD words it
This AD applies to the following Gulfstream Aerospace Corporation airplanes, certificated in any category: Table 1.--Applicability Model Serial Nos. GV series airplanes: 674 through 693 inclusive. GV-SP series airplanes: 5001 through 5072 inclusive.
- AD 2006-18-08 One-time
Goodyear Aviation Tires, Part Number 217K22-1, Installed on Various Transport Category Airplanes, Including But Not Limited to Bombardier Model BD-700-1A10 and BD-700-1A11 Airplanes; and Gulfstream Model G-1159, G-1159A, G-1159B, G-IV, GIV-X, GV, and GV-SP Series Airplanes
We are issuing this AD to prevent tread separation from a nosewheel tire during takeoff or landing, which could result in compromised nosewheel steering or ingestion of separated tread by an engine, and consequent reduced controllability of the airplane on the runway or in the air.
Applicability, as the AD words it
This AD applies to Goodyear aviation tires, part number 217K22-1, identified in Goodyear Aviation Service Bulletin SB-2005- 32-004, Revision 5, dated December 22, 2005; installed on various transport category airplanes, certificated in any category, including but not limited to Bombardier Model BD-700-1A10 and BD- 700-1A11 airplanes, and Gulfstream Model G-1159, G-1159A, G-1159B, G-IV, G-IV-X, G-V, and G-V-SP series airplanes.
- AD 2006-11-03 Recurring
Gulfstream Model GV and GV-SP Series Airplanes
We are issuing this AD to prevent broken damper shafts, which could result in locking of an aileron or elevator actuator (hard-over condition), which would activate the hard-over protection system (HOPS), resulting in increased pilot workload and consequent reduced controllability of the airplane.
Applicability, as the AD words it
This AD applies to all Gulfstream Model GV series airplanes, and Model GV-SP series airplanes having serial numbers (S/Ns) 5001 through 5052 inclusive; certificated in any category.
- AD 2005-21-05 Recurring Engine
Rolls-Royce Deutschland Ltd & Co KG (Formerly Rolls-Royce Deutschland GmbH, formerly BMW Rolls-Royce GmbH) Models BR700-710A1-10 and BR700-710A2-20 Turbofan Engines
Applicability, as the AD words it
This AD applies to Rolls-Royce Deutschland Ltd & Co KG (RRD) (formerly Rolls-Royce Deutschland GmbH, formerly BMW Rolls-Royce GmbH) models BR700-710A1-10 and BR700-710A2-20 turbofan engines. These engines are installed on, but not limited to, Bombardier Inc. BD-700-1A10, BD-700-1A11, and Gulfstream Aerospace Corp. G-V series airplanes.
- AD 2005-16-14 One-time
Gulfstream Model G-IV, GIV-X, GV, and GV-SP Series Airplanes
The FAA is issuing this AD to prevent short-circuiting of the floor heater pad system, which could result in a fire in the airplane cabin.
Applicability, as the AD words it
This AD applies to the airplanes identified in Table 1 of this AD, certificated in any category. Table 1.--Applicability Gulfstream model/series Serial Nos. G-IV: All. GIV-X: 4001 through 4023 inclusive. GV: All. GV-SP: 5001 through 5075 inclusive.
- AD 2004-22-16 One-time
Gulfstream Model GV and GV-SP Series Airplanes
This AD was prompted by reports of insufficient clearance between certain wiring harnesses and the crew oxygen bottle on several in-production and in-service airplanes.
Applicability, as the AD words it
This AD applies to Gulfstream Model GV series airplanes, serial numbers (S/N) 550 through 693 inclusive and 699; and Model GV-SP series airplanes, S/N 5001 through 5051 inclusive; certificated in any category.
- AD 2004-02-01 One-time
Gulfstream Model G-V Series Airplanes
To prevent uncommanded unlocking of the landing gear, which could result in collapse of the landing gear.
Applicability, as the AD words it
Model G-V series airplanes, certificated in any category; equipped with a landing gear selector dump valve (LGSDV) having part number 1159SCH512-7, -9, or -19.
- AD 2003-18-11 One-time
Gulfstream Model G-V Series Airplanes
To prevent separation of the balance weights of the aileron, which could result in jamming of the pilot's aileron control system, subsequent loss of aileron control and consequent reduced controllability of the airplane.
Applicability, as the AD words it
Model G-V series airplanes, serial numbers 501 through 667 inclusive, and serial number 699; certificated in any category.
- AD 2002-21-03 One-time
Gulfstream Model G-V Series Airplanes
To prevent the circuit breaker wiring from becoming pinched or damaged, causing arcing between the wire and attaching bracket, which could result in smoke and/or fire in the pilot's circuit breaker panel.
Applicability, as the AD words it
Model G-V series airplanes; having serial numbers 501 through 686 inclusive, and 699; certificated in any category.
- AD 2001-21-06 One-time
Gulfstream Model G-V Series Airplanes
To prevent fire extinguishing agent from being discharged into the wrong location, which could result in failure to extinguish an in-flight fire on an affected engine and jeopardize operation of the opposite engine.
Applicability, as the AD words it
Model G-V series airplanes, serial numbers 501 through 652 inclusive; certificated in any category.
- AD 2001-14-16 Recurring
Gulfstream Model G-V Series Airplanes
To prevent loss of nose wheel steering control, without a corresponding alert message annunciation, due to the effects of moisture intrusion into the rotary variable displacement transducer (RVDT) inside the steering actuator, which could result in the airplane departing the runway if an over steering condition were to occur during landing.
Applicability, as the AD words it
Model G-V series airplanes, serial numbers 501 and subsequent, certificated in any category.
- AD 2001-08-13 One-time
Gulfstream Model G-1159, G-1159A, G-1159B, G-IV, and G-V Series Airplanes
Applicability, as the AD words it
Model G-1159, G-1159A, G-1159B, G-IV, and G-V series airplanes, as specified in the Gulfstream Alert Customer Bulletins listed in the following table; certificated in any category: Table--Gulfstream Airplane Models and Alert Customer Bulletin's (ACB) Model ACB No. Dated G-1159 and G-1159A (G-II/IIB) 27 March 20, 2001. series airplanes. G-1159B (G-III) series airplanes. 13 March 20, 2001. G-IV series airplanes: 27 March 20, 2001. G-V series airplanes: 12 March 20, 2001.
- AD 2001-01-01 One-time Engine
BMW Rolls-Royce GmbH Models BR700-710A1-10 and BR700-710A2-20 Turbofan Engines.
Applicability, as the AD words it
This airworthiness directive (AD) applies to BMW Rolls-Royce (RR) GmbH models BR700-710A1-10 and BR700-710A2-20 turbofan engines with oil filter differential pressure switch part number (P/N) 21SN04-419 or P/N 21SN04-431 installed. These engines are installed on, but not limited to Bombardier Inc. BD-700 and Gulfstream Aerospace Corp. G-V series airplanes.
- AD 98-24-03 Recurring Engine
BMW Rolls-Royce GmbH Models BR700- 710A1-10 and BR700-710A2-20 Turbofan Engines
To prevent engine compressor and combustion core fairing (also referred to as the engine core fairing) detachment which could result in damage to the engine bypass duct, engine failure and damage to the aircraft.
Applicability, as the AD words it
BMW Rolls-Royce GmbH (BRR) Model BR700-710A1-10 and BR700-710A2-20 turbofan engines installed on, but not limited to, Gulfstream Aerospace G-V and Bombardier BD-700-1A10 series airplanes.
- AD 98-18-15 One-time
Gulfstream Model G-V Series Airplanes
To prevent chafing of a wiring harness against the crew oxygen bottle, which could result in electrical shorting and possible fire in the underfloor structure of the airplane.
Applicability, as the AD words it
Model G-V series airplanes, serial numbers 501 through 549 inclusive, certificated in any category.
- AD 98-09-01 Recurring
Gulfstream Model GV Series Airplanes
To prevent the incorrect operation of the elevator Hardover Prevention System (HOPS), which could result in loss of control of the airplane.
Applicability, as the AD words it
Model GV series airplanes, serial numbers 501 and 504 through 540 inclusive, certificated in any category.
5 superseded or removed ADs
- AD 2013-22-19 Superseded by AD 2017-08-01
Gulfstream Aerospace Corporation Airplanes
This AD was prompted by reports of two independent types of failure of the fuel boost pump with overheat damage found on the internal components and external housing on one of the failure types, and fuel leakage on the other.
Applicability, as the AD words it
This AD applies to all Gulfstream Aerospace Corporation Model GV and GV-SP airplanes, certificated in any category.
- AD 2009-17-01 Superseded by AD 2017-20-08
Gulfstream Model G-IV, GIV-X, and GV-SP Series Airplanes and Model GV Airplanes
Applicability, as the AD words it
This AD applies to the Gulfstream airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category. (1) Model G-IV series airplanes, having serial numbers (S/Ns) 1000 and subsequent. (2) Model GIV-X series airplanes, having S/Ns 4001 through 4146 inclusive, and S/Ns 4148 through 4150 inclusive. (3) Model GV airplanes, having S/Ns 501 and subsequent. (4) Model GV-SP series airplanes, having S/Ns 5001 through 5204 inclusive, S/Ns 5206 through 5217 inclusive, and S/N 5219.
- AD 2007-07-12 Superseded by AD 2009-08-01
Honeywell Flight Management Systems (FMSs) Served by Honeywell NZ-2000 Navigation Computers Approved Under Technical Standard Order (TSO) TSO-C115a, and IC-800 Integrated Avionics Computers Approved Under TSOs C9c, C52a, and C115a; as Installed on Various Transport Category Airplanes
We are issuing this AD to prevent a shift in the FMS computed position, which could result in uncommanded deviations from the intended flight path of the airplane and, if those deviations are undetected by the flight crew, compromised terrain/traffic avoidance.
Applicability, as the AD words it
This AD applies to all Honeywell NZ-2000 navigation computers approved under Technical Standard Order (TSO) TSO-C115a, and IC-800 integrated avionics computers approved under TSOs C9c, C52a, and C115a; as installed on transport category airplanes, certificated in any category, including but not limited to the airplanes identified in Table 1 of this AD. Table 1.--Known Affected Airplanes Manufacturer Model Bombardier, Inc: CL-600-2B16 (CL-601-3A, CL-601- 3R, and CL-604) airplanes. Dassault Aviation: Mystere-Falcon 900 airplanes. Gulfstream Aerospace Corporation: G-1159A, G-IV, and GV airplanes. Lockheed: 382G series airplanes. Raytheon Aircraft Company: BAe.125 Series 800A (including C-29A and U-125) airplanes. Hawker 800XP and 1000 airplanes.
- AD 2003-07-11 Superseded by AD 2005-21-05 Engine
Rolls-Royce Deutschland Ltd & Co KG Models BR700-710A1-10 and BR700-710A2-20 Turbofan Engines
To detect cracks in the fan disc that could result in an uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
This airworthiness directive (AD) is applicable to Rolls-Royce Deutschland Ltd & Co KG (RRD) (formerly Rolls-Royce Deutschland GmbH, formerly BMW Rolls-Royce GmbH) models BR700-710A1- 10 turbofan engines with fan disc part numbers (P/Ns) BRR18803, BRR19248, or BRR20791 installed, and BR700-710A2-20 turbofan engines with fan discs P/Ns BRR19248 or BRR20791 installed. These engines are installed on, but not limited to Bombardier Inc. BD-700-1A10, and Gulfstream Aerospace Corp. G-V series airplanes.
Federal Register Official PDF Correction (May 20, 2004)Correction (May 9, 2003)Correction (Apr 23, 2003)
- AD 2001-05-06 Superseded by AD 2003-07-11 Engine
BMW Rolls-Royce GmbH Models BR700-710A1-10 and BR700-710A2-20 Turbofan Engines
To detect cracks in the fan disk, that could result in an uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
BMW Rolls-Royce (RR) GmbH models BR700-710A1-10 with fan disks part numbers (P/N's) BRR18803, BRR19248, or BRR20791 installed, and BR700-710A2-20 turbofan engines with fan disks P/N's BRR19248 or BRR20791 installed. These engines are installed on but not limited to Bombardier Inc. BD-700-1A10, and Gulfstream Aerospace Corp. G-V series airplanes.
Radar reads the aircraft’s logbooks and ties each AD to the entries that show how and when it was complied with, with recurring ADs due by date and hours.
QUESTIONS
V AD questions
Source: FAA final rules under 14 CFR part 39, from the Federal Register. The FAA’s Dynamic Regulatory System holds the official list.
How many airworthiness directives apply to the V?
35 FAA ADs published since 1995 name the Gulfstream V's type certificate model (G-V) in their applicability. 30 are still in effect as far as the Federal Register shows; the others were superseded by a later AD or removed. How many apply to one aircraft depends on its serial number, equipment and modifications.
Which V ADs are recurring?
6 of the ADs in effect require actions that repeat, such as inspections at set intervals, until a terminating action is done. They are marked Recurring above. One-time ADs are complied with once, but the compliance record stays with the aircraft.
What is the latest V airworthiness directive?
AD 2023-02-02, effective Feb 28, 2023: Gulfstream Aerospace Corporation Airplanes. The list is refreshed from the Federal Register every weekday.
How do I know whether an AD applies to my V?
Read the AD's applicability paragraph, shown with each AD on this page, against the aircraft's serial number and its installed engines, propellers, parts and modifications. A certificated mechanic or inspector makes the determination and records the method of compliance in the maintenance records. The FAA's Dynamic Regulatory System holds the official list of ADs.
Why are engine and propeller ADs missing?
This page lists ADs whose applicability names the Gulfstream V airframe, plus appliance ADs that list it among the aircraft they can be installed on. Engine and propeller ADs name the engine or propeller model rather than the aircraft, so check them by the installed engine and propeller models.
Every AD on your V, tied to the logbook entry that closed it.
Radar reads every logbook page, typed or handwritten, and builds one searchable record per tail: times, inspections, ADs and components, each tied to the page it came from.