Emergency PZZ a důležité dokumenty k zachování letové způsobilosti letadel pro letadla zapsaná v Leteckém rejstříku ČR vydané v roce 2020
| Úřad vydávající PZZ/PZZ Issuing authority/AD | Účinnost od Effective date | Výrobce/Typ/Model Manufacturer/Type/Model | Předmět Subject |
 FAA2020-24-02 | 20.11.2020 | The Boeing Company letadla 737-8 a 737-9 (737 MAX) | AD 2020-24-02 supersedes AD 2018-23-51, which required revising certificate limitations and operating procedures of the Airplane Flight Manual (AFM) to provide the flightcrew with runaway horizontal stabilizer trim procedures to follow under certain conditions. This AD requires installing new flight control computer (FCC) software, revising the existing AFM to incorporate new and revised flightcrew procedures, installing new MAX display system (MDS) software, changing the horizontal stabilizer trim wire routing installations, completing an angle of attack (AOA) sensor system test, and performing an operational readiness flight, for more details see relevant AD. |
 EASA2020-0224R1-E | 18.11.2020 | Airbus Helicopters vrtulníky – AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS350 B2, AS 350 D a AS 355 E, AS 355 F, AS 355 F1, AS 355 F2, AS 355 N všech výrobních čísel | ATA 64 – Tail Rotor – Tail Rotor Blades – Inspection / Replacement / Modification |
| EASA 2020-0201R1-E | 02.10.2020 | GE Aviation Czech s.r.o. M601D, M601D-1, M601D-11, M601D-11NZ, M601E, M601E-11, M601E-11A, M601E-11AS, M601E-11S, M601E-21, M601F, M601F-22, M601F-32, M601FS, M601T, H75-200, H80-100, H80-200 and H85-200 engines, all serial numbers | ATA 73 – Engine Fuel & Control – Fuel Control Unit – Replacement |
| FAA 2020-18-51-E | ihned | Sandia attitude indicator | |
| EASA 2014-0076R2-E | ihned | Airbus Helicopters AS 350 B, BA, BB, B1, B2, B3 and D helicopters, and AS 355 E, F, F1, F2, N and NP helicopters, all serial numbers, if an affected part, as defined in this AD, is installed, except helicopters on which Airbus Helicopters modification (MOD) 073232 has been embodied in production, or AH AS350 Service Bulletin (SB) No. 53.00.58 and AS355 SB No. 53.00.34, as applicable, have been embodied in service | |
| FAA 2020-16-51-E | ihned | The Boeing Company letadla Model 737-300, -400, -500, -600, -700, -700C, -800, -900 a -900ER | Inspections of the engine bleed 5th stage check valves – This Emergency AD provides information continued operational safety activities related to the engine bleed 5th stage check valves |
| EASA 2020-0143 | 09.07.2020 | GE Aviation Czech s.r.o. (dříve Walter Engines a.s.) | Motory H80-200 v kombinaci s vrtulemi Avia Propeller AV-725, které jsou instalovány na letadlech Aircraft Industries (AI) L 410 UVP-E20 a L 410 UVP-E20 CARGO, a motory H85-200 (konfigurace BC04) v kombinaci s vrtulemi Avia Propeller AV-725, které jsou instalovány na letadlech AI L 410 NG |
| EASA 2020-0068-E | 25.03.2020 | BLANIK AIRCRAFT CZ s.r.o. L 23 Super-Blaník sailplanes, all serial numbers | Requires visual inspection before next flight of Rudder control cable attachment screws and hinge bolts for cracks |
| FAA 2020-03-16 | 09.03.2020 | Textron Aviation Inc. (Type Certificate previously held by Cessna Aircraft Company) M210 series | Requires visual and eddy current inspections of the carry-thru spar lower cap. This AD was prompted by the in-flight break-up of Model T210M due to fatigue cracking that initiated at a corrosion pit |
| EASA 2020-0001 | 22.1.2020 | CEAPR letadla DR 400/100, DR 400/120, DR 400/120 A, DR 400/120 D, DR 400/140, DR 400/140 B, DR 400/160, DR 400/160 D, DR 400/180, DR 400/180 R, DR 400/180 S a DR 400 NGL | ATA 75 – Air – Air Intake Duct – Modification / Inspection |
| FAA 2019-25-55-E | ihned | The Boeing Company letadla 737-300, -400, -700 | Modified to a Bedek Division Special Freighter (BDSF) by supplemental type certificate (STC) ST01566LA, ST01961SE, or ST02556SE, with a 9G rigid barrier |
| EASA 2019-0239R1-E | 25.12.2019 | XtremeAir GmbH letadla XA41, XA42 | ATA 71 – Power Plant – Engine Mount – Inspection ATA 11 – Placards & Markings – Aerobatics Manoeuvres Prohibited – Installation ATA – Aircraft Flight Manual – Section Limitations – Amendment |
Důležité dokumenty k zachování letové způsobilosti letadel
| Úřad/Přímý odkaz Issuing authority/Link | Účinnost od Effective date | Výrobce/Typ/Model Manufacturer/Type/Model | Předmět Subject |
| EASA CI 2020-12 | ihned | Certification Information on the transfer of Supplemental Type Certificates due to change of Company registration for Air Ambulance Technology GmbH | |
| EASA SIB 2020-05 | ihned | Aircraft Maintenance Programme under Part-ML | |
 Transport CanadaCASA 2019-08 | ihned | Aircraft parts distributed by Sofly Aviation Services, Inc. | Suspected unapproved parts alert |
| EASA SIB 2020-03 | ihned | Data Link Exemptions and Flight Plans | |
| FAA CAN-2020-03 | ihned | CFM International, S.A. motory LEAP–1B21, LEAP –1B23, LEAP –1B25, LEAP –1B27, LEAP –1B28, LEAP –1B28B1, LEAP –1B28B2, LEAP –1B28B2C, LEAP –1B28B3, LEAP –1B28BBJ1 a LEAP-1B28BBJ2 instalované na letadlech Boeing 737-8 a -9 (MAX) | FAA’s ongoing activities related to multiple in-flight shutdown (IFSD) events |
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