Tillögur í öryggisátt Síða 8

Afgreiðsla

Afgreiðsla

Málið var aftur yfirfarið og telur Avians verklag í MANOP.S 330.3 TAKE OFF CLEARANCE fullnægjandi og telur ekki þörf á að breyta því enda er til staðar verklag í MANOP.S 330.3 TAKE OFF CLEARANCE og farið var yfir það m.t.t. Starfsemi Avians. Ekki hefur verið tekið upp start up time verklag á stýrðu flugvöllum Avians enda kemur fram í AMC11 ATS.TR.210(a)(3)(a) að það skuli gert "when necessary" og við mat reyndist ekki þörf á því. Varðandi það að halda ATFM brottfarartíma er eftirfarandi verklag til staðar:

o    MANOPS 330.3.10 / PANS-ATM 7.9.1 / GM6 ATS.TR.210(a)(3):

Departures shall normally be cleared in the order in which they are ready for take-off, except that deviations may be made from this order of priority to facilitate the maximum number of departures with the least average delay. Factors which should be considered in relation to the departure sequence include, inter alia: (N)

1. types of aircraft and their relative performance;
2. routes to be followed after take-off;
3. any specified minimum departure interval between take-offs;
4. need to apply wake turbulence separation minima;
5. aircraft which should be afforded priority; and (R)
6. aircraft subject to ATFM requirements.

o    MANOPS 330.3.10 Note / PANS-ATM 7.9.1 Note 2 / GM7 ATS.TR.210(a)(3):

For aircraft subject to ATFM requirements, it is the responsibility of the pilot and the operator to ensure that the aircraft is ready to taxi in time to meet any required departure time, bearing in mind that once a departure sequence is established on the taxiway system, it can be difficult, and sometimes impossible, to change the order.

• Sjá einnig PANS-ATM 6.3.3.2 b), reyna þó að fara eftir beiðnum operator ef það er mögulegt.

o    PANS-ATM 6.3.3.2 If departures are delayed, the delayed flights shall normally be cleared in an order based on their estimated time of departure, except that deviation from this order may be made to:

1. a) facilitate the maximum number of departures with the least average delay;
2. b) accommodate requests by an operator in respect of that operator’s flights to the extent practicable.

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Afgreiðsla

Norlandair hefur gefið út Safety Information letter 2025-2, De-/anti-icing Beechcraft King Air aircraft using Type II fluid, þar sem tekið er á efni tillögunnar.

Afgreiðsla

Norðurflug hefur innleitt tillöguna á eftirfarandi hátt:

• Hluti í handbók 8.1.2.2
• Hluti af OPC formi
• Hluti af þjálfun fyrir þyrlu skíðun þar sem einkum reynir á þetta og í kennsluefni er ítarlega farið yfir „whiteout“
• Hluti af áhættumati sem gert er vegna nýrrar reglugerðar Ferðamálastofu

Afgreiðsla

Precision Conversions has modified the structural design of the main cargo door to support the intended 45 knots maximum wind operation limit in compliance with FAA FAR and EASA CS, subchapters 25.301(a) and 25.303.

Afgreiðsla

The STC holder addressed through service bulletin (SB) PC-757-52-0018 a redesign of the cargo door, replacing the aluminum rods of the door with steel rods.

In addition, for both configurations, pre and post SB PC-757-52-0018, the following wind/gust limitations have been established and incorporated in the Aircraft Maintenance Manual and Operations Manual supplements:

- 45 knots up to the door canopy position, 0 (zero) knots beyond the door canopy position, for configuration pre SB PC-757-52-0018 (aluminum rods).

- 45 knots up to the door canopy position, 25 knots beyond the door canopy position, for configuration post SB PC-757-52-0018 (steel rods).

These design changes and wind/gust limitations were mandated by the FAA AD 2016-04-24, which has been adopted by EASA.

Afgreiðsla

FAA Safety Recommendation 14.055 was assigned to the FAA's Aircraft Certification Service, Transport Airplane Directorate on April 15, 2014, requiring Precision Conversions to modify the structural design of the main cargo door to support the intended 45 knots maximum wind operation limit in compliance with FAA FAR and EASA CS, subchapters 25.301(a) and 25.303.

The STC holder addressed through service bulletin (SB) PC-757-52-0018 a redesign of the cargo door, replacing the aluminum rods of the door with steel rods.

In addition, for both configurations, pre and post SB PC-757-52-0018, the following wind/gust limitations have been established and incorporated in the Aircraft Maintenance Manual and Operations Manual supplements:

- 45 knots up to the door canopy position, 0 (zero) knots beyond the door canopy position, for configuration pre SB PC-757-52-0018 (aluminum rods).

- 45 knots up to the door canopy position, 25 knots beyond the door canopy position, for configuration post SB PC-757-52-0018 (steel rods).

These design changes and wind/gust limitations were mandated by the FAA AD 2016-04-24.

Afgreiðsla

Moog has redesigned the Blocking and Thermal Relief Valve Housing with thicker material section and more radius in the area of the fracture surface. The redesigned Blocking and Thermal Relief Valve Housing is made from stainless steel instead of aluminum. This results in better fatigue performance of the Blocking and Thermal Relief Valve Housing. In addition the FAA has issued Safety Recommendation 15.115, a Boeing 757 airplane level safety issue, mandating evaluation of the spoiler actuator's blocking and thermal relief valve housing failure to determine appropriate corrective action.

Afgreiðsla

Boeing plans to release Boeing Alert Service Bulletin 757-SB-27A0154 on June 25 2016. In addition the FAA has issued Safety Recommendation 15.115, a Boeing 757 airplane level safety issue, mandating evaluation of the spoiler actuator's blocking and thermal relief valve housing failure to determine appropriate corrective action.