Other State of Design

2024-0002

ATA 72 – Engine – High-Pressure Turbine Inner Stationary Seal – Inspection

CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3, CFM56-5B1/P, CFM56-5B2, CFM56-5B2/2P, CFM56-5B2/3, CFM56-5B2/P, CFM56-5B3/2P, CFM56-5B3/2P1, CFM56-5B3/3, CFM56-5B3/3B1, CFM56-5B3/P, CFM56-5B3/P1, CFM56-5B4, CFM56-5B4/2P, CFM56-5B4/2P1, CFM56-5B4/3, CFM56-5B4/3B1, CFM56-5B4/P, CFM56-5B4/P1, CFM56-5B5, CFM56-5B5/3, CFM56-5B5/P, CFM56-5B6, CFM56-5B6/2P, CFM56-5B6/3, CFM56-5B6/P, CFM56-5B7, CFM56-5B7/3, CFM56-5B7/P, CFM56-5B8/3, CFM56-5B8/P, CFM56-5B9/2P, CFM56-5B9/3 and CFM56-5B9/P engines, all serial numbers (s/n); CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F, CFM56-5C2/F4, CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C2/P, CFM56-5C3/F, CFM56-5C3/F4, CFM56-5C3/G, CFM56-5C3/G4, CFM56-5C3/P, CFM56-5C4, CFM56-5C4/1, CFM56-5C4/P and CFM56-5C4/1P engines, all s/n; and CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3, CFM56-7B20E, CFM56-7B22, CFM56-7B22/2, CFM56-7B22/3, CFM56-7B22/3B1, CFM56-7B22/B1, CFM56-7B22E, CFM56-7B22E/B1, CFM56-7B24, CFM56-7B24/2, CFM56-7B24/3, CFM56-7B24/3B1, CFM56-7B24/B1, CFM56-7B24E, CFM56-7B24E/B1, CFM56-7B26, CFM56-7B26/2, CFM56-7B26/3, CFM56-7B26/3B1, CFM56-7B26/3B2, CFM56-7B26/3B2F, CFM56-7B26/3F, CFM56-7B26/B1, CFM56-7B26/B2, CFM56-7B26E, CFM56-7B26E/B1, CFM56-7B26E/B2, CFM56-7B26E/B2F, CFM56-7B26E/F, CFM56-7B27, CFM56-7B27/2, CFM56-7B27/3, CFM56-7B27/3B1, CFM56-7B27/3B1F, CFM56-7B27/3B3, CFM56-7B27/3F, CFM56-7B27/B1, CFM56-7B27/B3, CFM56-7B27A, CFM56-7B27A/3, CFM56-7B27AE, CFM56-7B27E, CFM56-7B27E/B1, CFM56-7B27E/B1F, CFM56-7B27E/B3 and CFM56-7B27E/F engines, all s/n.

EASA

ISR I-57-2021-12-4R1

Wings-Flaps-Fairing Seal Repair

GALP model G200 aircraft serial numbers 004 through 250 certificated in any category

CAA Israel

2023-0221

ATA 25 – Equipment / Furnishings – Mini-Suite Entry Door(s)/Emergency Passage Feature Mechanism – Inspection / Modification

Boeing 787-9 aeroplanes, if modified by EASA STC 10082968.

EASA

2023–25–02

Joint Aircraft System Component (JASC) Code 2701, Control Column Section.

This AD applies to Piper Aircraft, Inc. airplanes identified in paragraphs (c)(1) through (3) of this AD,certificated in any category. (1) Model PA–46–350P airplanes, serial numbers 4636811 through 4636814 inclusive and 4636816through 4636829 inclusive. (2) Model PA–46–500TP airplanes, serial numbers 4697692 through 4697700 inclusive. (3) Model PA–46–600TP airplanes, serial numbers 4698224 through 4698240 inclusive and 4698242through 4698274 inclusive.

FAA

2023-0215 [Correction: 13 December 2023]

ATA – Aircraft Flight Manual – Auto Flight System Control Panel ALT Outer Knob Use – Amendment ATA 22 – Auto Flight – Flight Control Unit – Modification

Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.

EASA

2023-0215

ATA – Aircraft Flight Manual – Auto Flight System Control Panel ALT Outer Knob Use – Amendment ATA 22 – Auto Flight – Flight Control Unit – Modification

Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.

EASA

2023–23–12

Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section; 7250, Turbine Section.

This AD applies to CFM International, S.A. (CFM) Model LEAP–1B21, LEAP–1B23, LEAP–1B25, LEAP–1B27, LEAP–1B28, LEAP–1B28B1, LEAP–1B28B2, LEAP–1B28B2C, LEAP–1B28B3, LEAP– 1B28BBJ1, and LEAP–1B28BBJ2 engines.

FAA

2023-0214

ATA 53 – Fuselage – Tail Rotor Drive Shaft / Rear Transmission Bearing Support – Inspections / Modification

EC 130 T2 helicopters, all serial numbers on which AH modification 074581 has been embodied in production.

EASA

2023-0213

ATA 25 – Equipment / Furnishings – Hook Damper – Modification

MBB-BK117 C-2, D-2, D-3 and D-3m helicopters, all variants, all serial numbers (s/n).

EASA

2023-0212

ATA 53 – Fuselage – Double Joggle Area at Frame 16 and Frame 20 – Inspection

Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A319-151N, A319-153N, A319-171N, A320-211, A320-212, A320-214, A320-216, A320-231, A320-232, A320-233, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N, A321-251NX, A321-252N, A321-252NX, A321-253N, A321-253NX, A321-271N, A321-271NX, A321-272N and A321-272NX aeroplanes, all manufacturer serial numbers (MSN), except aeroplanes in any of the configurations below: – Aeroplanes on which Airbus modification (mod) 160917 has been embodied in production; – A318 aeroplanes on which Airbus mod 39195 has been embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 has been embodied in service; – A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 have been embodied in production; – A319 aeroplanes on which Airbus mod 162338 has been embodied in production; – A320 aeroplanes on which Airbus mod 162339 has been embodied in production;- CEO aeroplanes on which Airbus SB A320-53-1378, SB A320-53-1379, SB A320-53-1380 and SB A320-53-1381 have been embodied in service; – NEO aeroplanes on which Airbus SB A320-53-1422, SB A320-53-1423, SB A320-53-1424, and SB A320-53-1425 have been embodied in service.

EASA

2023–21–10

Air Transport Association (ATA) of America Code: 55, Stabilizers.

This AD applies to ATR—GIE Avions de Transport Régional Model ATR42–500 and ATR72–212A airplanes, certificated in any category, as identified in ATR Service Bulletin ATR42–55–0020,dated March 2, 2023; or ATR Service Bulletin ATR72–55–1013, dated March 2, 2023; as applicable.

FAA

2023–23–14

Air Transport Association (ATA) of America Code 28, Fuel.

This AD applies to all The Boeing Company Model 747–100, 747–100B, 747–100B SUD, 747–200B, 747–200C, 747–200F, 747–300, 747–400, 747–400D, 747–400F, 747SR, 747SP, 747–8F, and 747–8 series airplanes, certificated inany category.

FAA