27-10-11-03 |
One-time detailed inspection of the aileron & elevator servo actuator centering spring rods to verify the rods integrity. |
06/12/2010 |
57-10-06-18
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This Airworthiness Directive, issued by the Civil Aviation Authority in accordance with the Israeli Air Navigation Regulations applies to an aircraft for which our records list you as the registered owner. It affects aviation safety and requires your immediate attention. No person may operate an aircraft to which an Airworthiness Directive applies, except in accordance with that Directive. |
15/08/2010 |
05-10-05-05 R1 |
G200 Aircraft Maintenance Manual (AMM), introduction of safe life limits to the Airworthiness Limitation Section (ALS).
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15/06/2010 |
05-10-05-05
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This Airworthiness Directive, issued by the Civil Aviation Authority in accordance with the Israeli Aviation Regulations, applies to an aircraft for which our records list you as the records list you as the registered owner. It affects aviation safety and your immediate attention. No person may operate an aircraft to ehich an Airworthiness Directive applies, except in accordance with that Directive. |
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01-10-01-07
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This AD mandates a new limitation in the G200 AFM, pertaining to operation of the Air Brakes. The new limitation prohibits deployment of the Air Brakes above 360 KIAS/0.79 Mi, and this is incorporated in Rev. 14 to the AFM. |
15/01/2010 |
01-10-01-07R1
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This AD mandates a new limitation in the G200 AFM, pertaining to operation of the Air Brakes. The new limitation prohibits deployment of the Air Brakes above 360 KIAS/0.79 Mi, and this is incorporated in Rev. 14 to the AFM. |
20/01/2010 |
29-07-01-11
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Visual inspection of hydraulic lines and attaching blocks for damage and wear. Replacement of existing blocks made of Teflon to new blocks made of Nylon 6/6. The blocks are installed in the R.H. aft fuselage equipment bay. |
11/06/2007 |
21-07-01-01
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Recall and replacement of defective Pressurization Safety Valves P/N 103842-3 in accordance with Honeywell Service Bulletin No. 103842-21-4126 as adopted by Gulfstream SB 200-21-308. |
06/03/2007 |
28-07-02-03
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Right Fuel Standby Pump Connector (4Q1) electrical wiring, inspection and repair. |
28/02/2007 |
31-07-01-12
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Inspection and repair of Instrument Panel Wiring Harness for chafe condition. |
28/02/2007 |
53-06-01-09
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Visual inspection of the aircraft lower skin at STA 16595, for possible cracks developed around drainage diverter rivets. |
01/02/2006
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28-05-06-08
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Fuel standby feed pump plugs (3Q1 and 4Q1) electrical wiring, inspection and repair. |
15/07/2005 |
35-04-09-03
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Replacement of Hydraflow oxygen system tubing by steel braided hoses. |
Immediately |
72-03-05-09
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Incorporation of new take-off performance tables in the Airplane Flight Manual. |
30/09/2003 |
27-04-02-06
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Inspection and lubrication of Aileron Artificial Feel Spring Unit External and Internal Sleeves. |
15/03/2004 |
35-03-07-12R1
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Oxygen-Pilot/Copilot oxygen mask stowage box-supply line inspection and replacement. |
05/09/2003 |
32-03-08-07
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Landing Gear – Main Landing Gear (MLG) – Retorque of MLG Bearing Retaining Nut after compliance of SB 200-32-076. |
27/08/2003 |
35-03-07-12
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Oxygen-Pilot/Copilot oxygen mask stowage box-supply line replacement. |
28/07/2003 |
57-02-10-15
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Inspection of flap actuator fairing separation from the wing lowers skin. |
10/11/2002 |
71-03-03-02
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Replacement of forward engine mount yoke attachment bolts, nuts & washers. |
22/03/2003 |
53-02-08-08
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Inspection of damage occurred to forward engine cross spar (STA 14783) P/N 4AS3177200-501 |
15/09/2002 |
28-02-03-15
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Inspection of evidence / accumulation of fuel in the service compartment. |
26/03/2002 |
32-11-10-13
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MLG Brake Assy. Wear Indicating Pin inspection and Modification. |
31/10/2011 |