PZZ AD | Účinnost od Effective date | Výrobce/Typ/Model Manufacturer/Type/Model | Předmět Subject | |
2007-0209R1-E | | 25.9.2015 | Airbus Helicopters – vrtulníky AS 355 E, AS 355 F, AS 355 F1, AS 355 F2, AS 355 N | Rotor Drive – Main Gearbox Lubrication Pump – Inspection / Replacement |
2015-0185-E | | 3.9.2015 | Czech Sport Aircraft a.s. – letadla PS-28 Cruiser | Landing Gear – Nose Landing Gear – Inspection / Replacement |
CF-2015-16R1-E | | 6.8.2015 | Bell Helicopter Textron Canada Limited (BHTC) – vrtulníky model 429 | Tail Rotor – Pitch Link Spherical Bearing Accelerated Wear |
2015-0143-E | | 17.7.2015 | Airbus Helicopters – vrtulníky AS 355 NP | Tail Rotor – Blades – Inspection |
2015-0122-E | | 26.6.2015 | Airbus Helicopters – vrtulníky AS 355 N, AS 355 NP | Rotorcraft Flight Manual – Engine „CHIP“ Warning Emergency Procedure – Amendment |
2015-0109-E | | 16.6.2015 | Czech Sport Aircraft a.s. – letadla PS-28 Cruiser | Landing Gear – Nose Landing Gear – Inspection / Replacement |
2015-10-51-E | | ihned | Avidyne Corporation (Avidyne) Integrated Flight Displays (IFDs) part number (P/N) 700-00083-( ) loaded with software release 9.3.1.0 or earlier release (referred to as Model R9 – 10 inch), P/N 700-00171-( ) loaded with software release 9.2.5.0 or earlier release (referred to as Model R9 – 12 inch), and P/N 700-00182-( ) loaded with software release 10.0.3.0 or earlier release (referred to as Model IFD540) | Incorporating an operational limitation into the Limitations Section of the airplane flight manual (AFM) or airplane flight manual supplement (AFMS) |
2015-0035-E | | 3.3.2015 | AgustaWestland S.p.A (dříve Agusta S.p.A.), AgustaWestland Philadelphia Corp. (dříve Agusta Aerospace Corp.) – Vrtulníky Modely A109, AW109, A119, AW119 | Tail Rotor – Pitch Control Link Assembly – Inspection / Replacement |