לתפריט האתר לתוכן האתר

תפריט

  • לשפה האנגלית
  • פורטל עובדים
AD NumberSubjectEffective
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 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). 15/06/2010
05-10-05-05 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.  
01-10-01-07 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 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 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 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
31-07-01-12 Inspection and repair of Instrument Panel Wiring Harness for chafe condition. 28/02/2007
53-06-01-09 Visual inspection of the aircraft lower skin at STA 16595, for possible cracks
developed around drainage diverter rivets.
01/02/2006
28-05-06-08 Fuel standby feed pump plugs (3Q1 and 4Q1) electrical wiring, inspection
and repair.
15/07/2005
35-04-09-03 Replacement of Hydraflow oxygen system tubing by steel braided hoses. Immediately
72-03-05-09 Incorporation of new take-off performance tables in the Airplane
Flight Manual.
30/09/2003
27-04-02-06 Inspection and lubrication of Aileron Artificial Feel Spring Unit External
and Internal Sleeves.
15/07/2004
35-03-07-12R1 Oxygen-Pilot/Copilot oxygen mask stowage box-supply line inspection
and replacement.
05/09/2003
32-03-08-07 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 Oxygen-Pilot/Copilot oxygen mask stowage box-supply line replacement. 28/07/2003
57-02-10-15 Inspection of flap actuator fairing separation from the wing lowers skin. 10/11/2002
71-03-03-02 Replacement of forward engine mount yoke attachment bolts, nuts & washers. 22/03/2003
53-02-08-08 Inspection of damage occurred to forward engine cross spar
(STA 14783) P/N 4AS3177200-501.
15/09/2002
28-02-03-15 Inspection of evidence / accumulation of fuel in the service compartment. 26/03/2002
52-00-12-15 Potential jamming of the Main Entrance Door. Immediately
25-01-12-17R1 1. Disabling of the Baggage Compartment Heating Blankets System.
2. Return to Service.
01/08/2002
52-00-12-15R1 Potential jamming of the Main Entrance Door. Immediately
52-01-11-11 Main Entrance Door Interlock Mechanism Improvement. 08/04/2002
32-11-10-13 MLG Brake Assy. Wear Indicating Pin inspection and Modification. 31/10/2011

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