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EASA Regulations for Bell Textron Inc. (Bti) 212

25 airworthiness directives and regulations affecting Bell Textron Inc. (Bti) 212.

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New ADs and bulletins for Bell Textron Inc. (Bti) 212, summarized like the ones below, every Monday.

EASA AD 2015-0226R8

Equipment / Furnishings — Hoist — Test / Replacement

EASA Airworthiness Directive 2015-0226R8 is a regulatory document addressing the inspection, testing, and replacement requirements for Goodrich externally mounted rescue hoists installed on various helicopter models including Leonardo AW109SP, AB139, AW139, AB412; Bell Textron 212, 214, 412, 429, 430; Airbus Helicopters AS 365 N3, AS 332 L2, EC225 LP, MBB-BK117 C-2, EC135, EC635; MD Helicopters MD900; and Sikorsky S-61, S-76, and S-92A. The directive mandates load checks, cable replacements, and overload clutch replacements to ensure continued airworthiness and safety of hoist operations.

Airworthiness Directive

Airbus Helicopters SA 330
Airbus Helicopters AS 332
Airbus Helicopters EC 225
Airbus Helicopters SA
Airbus Helicopters AS 365
Airbus Helicopters EC 155
Airbus Helicopters EC135
Airbus Helicopters 635
Airbus Helicopters MBB-BK 117
Bell 429
Bell 430
Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412
Leonardo S.P.A. Helicopters A109
Leonardo S.P.A. Helicopters A119
Leonardo S.P.A. Helicopters AB139
Leonardo S.P.A. Helicopters AW139
Leonardo S.P.A. Helicopters AB212
Leonardo S.P.A. Helicopters AB412
Md Helicopters Inc (Mdhi) MD900
Mcdermott 214 Holdings, 214
Sikorsky S-61
Sikorsky S-76
Sikorsky S-92

EASA AD US-2024-20-07

Equipment / Furnishings - Emergency Float Kit Activation Handle - Repetitive Inspections / Replacement

The document titled 'Equipment / Furnishings - Emergency Float Kit Activation Handle - Repetitive Inspections / Replacement' is a regulatory directive addressing the maintenance requirements for the emergency float kit activation handle on certain aircraft. It mandates repetitive inspections and replacement procedures to ensure the proper functioning of this critical safety equipment. The directive applies to aircraft equipped with the specified emergency float kit activation handle assemblies.

Airworthiness Directive

Airbus Helicopters AS 350
Airbus Helicopters EC 130
Airbus Helicopters EC 120 B
Airbus Helicopters BO 105
Airbus Helicopters EC135
Airbus Helicopters 635
Airbus Helicopters MBB-BK 117
Bell 206
Bell 407
Bell Textron Inc. (Bti) 210
Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412
Leonardo S.P.A. Helicopters AB212
Leonardo S.P.A. Helicopters AB412
Md Helicopters Inc (Mdhi) 369
Md Helicopters Inc (Mdhi) 500N
Robinson R44 (Raven)
Robinson R66
Sikorsky S-76

EASA AD 2022-0047-CN

CANCELLED: Fuselage — Tailboom Attachment — Inspection / Replacement

EASA Airworthiness Directive Cancellation Notice 2022-0047-CN is an official cancellation of the previous EASA AD 2022-0047 concerning inspection and replacement of tailboom attachment components on Bell Textron Inc. 212 and 412 helicopters. The cancellation applies to specific serial numbers of these helicopter models and relates to tailboom attachment bolts and barrel nuts. This notice confirms that the FAA AD 2024-16-19 supersedes the requirements previously mandated by EASA AD 2022-0047.

Airworthiness Directive

Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412
Bell Textron Inc. 212
Bell Textron Inc. 412

EASA AD US-2024-16-19

Fuselage — Tailboom Attachment — Inspection / Replacement

The document titled 'Fuselage — Tailboom Attachment — Inspection / Replacement' is a regulatory directive concerning the inspection and replacement procedures for the tailboom attachment on certain aircraft fuselages. It addresses structural integrity issues related to the tailboom attachment point, which is critical for safe aircraft operation. The directive applies to specific aircraft models that utilize this fuselage-tailboom configuration, although no explicit aircraft or engine models are identified in the provided text.

Airworthiness Directive

Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412

EASA AD US-2024-19-17

Rotors Flight Control - Tension Torsion (TT) Straps - Removal / Installation Prohibition

The document titled 'Rotors Flight Control - Tension Torsion (TT) Straps - Removal / Installation Prohibition' is a regulatory directive addressing the handling of tension torsion straps in rotor flight control systems. It applies to specific rotorcraft models equipped with these components, prohibiting their removal or installation to ensure flight safety and structural integrity.

Safety Directive

Bell Textron Inc. (Bti) 204B
Bell Textron Inc. (Bti) 205
Bell Textron Inc. (Bti) 210
Bell Textron Inc. (Bti) 212

EASA AD US-2024-16-01

Fuselage - Tail Boom Attachment Cap Angle - Inspection

The Federal Aviation Administration's Airworthiness Directive 2024-16-01 is a final rule addressing Bell Textron Inc. helicopters, including Models 412, 412CF, 412EP, 212, 205A, 205A-1, and 205B. It mandates inspections of the tail boom attachment cap angle and adjacent structures for cracks to prevent potential failure and loss of helicopter control. This directive updates previous requirements and incorporates new inspection procedures and reporting obligations.

Airworthiness Directive

Bell Textron Inc. (Bti) 205
Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412
Bell Textron 412
Bell Textron 412CF
Bell Textron 412EP
Bell Textron 212
Bell Textron 205A1
Bell Textron 205B

EASA AD US-2022-20-14

Main Rotor Drive - Main Transmission Housing Assembly - Inspection

Airworthiness Directive 2022-20-14 is a final rule issued by the Federal Aviation Administration addressing Bell Textron Inc. helicopters including models 204B, 205A, 205A-1, 205B, 210, 212, 412, 412CF, 412EP, and various restricted category helicopters. This directive mandates repetitive inspections of the main transmission housing assembly for cracks, corrosion, and pitting due to reported cracks in the main transmission support case. The directive aims to ensure continued airworthiness and safety of these helicopter models by identifying and correcting potential structural issues.

Airworthiness Directive

Bell Textron Inc. (Bti) 204B
Bell Textron Inc. (Bti) 205
Bell Textron Inc. (Bti) 210
Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412
Bell 204B
Bell 205A1
Bell 205B
Bell 210
Bell 212
Bell 412
Bell 412CF
Bell 412EP

EASA AD US-2022-22-12

NOT ADOPTED - EASA DECISION ATTACHED

The document titled NOT ADOPTED - EASA DECISION ATTACHED is an official position from EASA regarding FAA Airworthiness Directive 2022-22-12. This FAA AD applies to certain helicopters modified by FAA STC SR01298NY, including Bell Textron Inc. type designs and Leonardo AB412 helicopters. EASA has determined that FAA AD 2022-22-12 is not eligible for adoption within the European Union because the FAA STC SR01298NY is not validated by EASA for all affected helicopter types, specifically Leonardo AB412 helicopters.

Agency Decision

Bell Textron Inc. (Bti) 204B
Bell Textron Inc. (Bti) 205
Bell Textron Inc. (Bti) 210
Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412
Leonardo S.P.A. Helicopters AB212
Leonardo S.P.A. Helicopters AB412
Mcdermott 214 Holdings, 214
Bell Textron Inc. Helicopter
Leonardo AB412

EASA AD CF-2022-46

Landing Gear — Forward Crosstube — New Airworthiness Limitation

The Canadian Airworthiness Directive CF-2022-46 addresses the landing gear forward crosstube on Bell Textron Inc. helicopters models 204B, 205A-1, 205B, 212, 214B, 214B-1, 412, 412 CF, and 412 EP modified with Dart Aerospace Ltd. forward crosstube part number D212-664-101/-101B. This directive introduces a new airworthiness limitation concerning the fatigue life of the forward crosstube to enhance safety. It mandates compliance with updated maintenance instructions to prevent structural failure during landing.

Airworthiness Directive

Bell Textron Inc. (Bti) 204B
Bell Textron Inc. (Bti) 205
Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412
Mcdermott 214 Holdings, 214
Bell Textron Inc. 204B
Bell Textron Inc. 205A-1
Bell Textron Inc. 205B
Bell Textron Inc. 212
Bell Textron Inc. 214B1
Bell Textron Inc. 412
Bell Textron Inc. 412 CF
Bell Textron Inc. 412 EP

EASA AD 2021-0163-CN

CANCELLED: Fuel / Oil — Check Valves — Inspection / Replacement

The document titled CANCELLED: Fuel / Oil — Check Valves — Inspection / Replacement concerns the BELL TEXTRON INC. (BTI) 212 and 412 helicopter models. It originally addressed inspection and replacement procedures for fuel and oil check valves on these aircraft. However, this document has been cancelled and is no longer in effect.

Airworthiness Directive

Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412
Bell Textron Inc. 212
Bell Textron Inc. 412

EASA AD US-2022-11-19

Fuel / Oil — Check Valves — Inspection / Replacement

Federal Register Volume 87, Number 105 (June 1, 2022) Final Rule titled "Fuel / Oil — Check Valves — Inspection / Replacement" is an FAA Airworthiness Directive (AD 2022-11-19) addressing Bell Textron Inc. Model 212, 412, 412CF, and 412EP helicopters. It targets engine oil check valve P/N 209-062-520-001 and fuel check valve P/N 209-062-607-001 manufactured by Circor Aerospace with specific markings and manufacturing dates. The directive mandates inspection and replacement procedures to mitigate risks associated with cracked check valves.

Airworthiness Directive

Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412
Bell Textron Inc. 212
Bell Textron Inc. 412
Bell Textron Inc. 412CF
Bell Textron Inc. 412EP

EASA AD US-2022-07-02

Fuselage - Tail Boom Spar Caps - Inspection / Removal

The Federal Register Volume 87, Number 64, Final Rule titled "Fuselage - Tail Boom Spar Caps - Inspection / Removal" is an airworthiness directive issued by the FAA for certain Bell Textron Inc. helicopters including Models 205A, 205A-1, 205B, 210, 212, 412, 412CF, and 412EP equipped with tailboom left hand fin spar cap part number 212-030-447-117. This directive addresses the detection and removal of cracked spar caps to ensure continued airworthiness and safety.

Airworthiness Directive

Bell Textron Inc. (Bti) 205
Bell Textron Inc. (Bti) 210
Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412
Bell Textron 205A1
Bell Textron 205B
Bell Textron 210
Bell Textron 212
Bell Textron 412
Bell Textron 412CF
Bell Textron 412EP

EASA AD US-2022-06-03

Main Rotor - Hub Strap Pins - Removal / Inspection

The Federal Aviation Administration's Airworthiness Directive 2022-06-03 addresses safety concerns for Bell Textron Inc. helicopters, specifically Models 204B, 205A, 205A-1, 205B, 210, and 212 equipped with main rotor hub strap pins part number 204-012-104-005 with serial number prefix "FNFS". This directive mandates removal and inspection of all affected pins, both outboard and inboard, to prevent potential main rotor blade detachment. It also requires removing the mating strap fitting if any deformation is found on the pins.

Airworthiness Directive

Bell Textron Inc. (Bti) 204B
Bell Textron Inc. (Bti) 205
Bell Textron Inc. (Bti) 210
Bell Textron Inc. (Bti) 212
Bell 204B
Bell 205A1
Bell 205B
Bell 210
Bell 212

EASA AD 2022-0036

Fuselage – Tailboom Attachment – Inspection / Replacement

EASA Airworthiness Directive 2022-0036 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Bell Textron Inc. 212 and 412 helicopter models. It addresses the inspection and replacement of tailboom attachment bolts and barrel nuts to prevent potential failure due to cracking, corrosion, fatigue, and low torque. The directive mandates specific inspections, replacements, and torque checks to ensure continued airworthiness.

Airworthiness DirectiveSuperseded

Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412
Bell Textron Inc. 212
Bell Textron Inc. 412

EASA AD US-2022-02-02

Superseded by FAA AD 2022-06-03

FAA Airworthiness Directive 2022-02-02 is a final rule addressing unsafe conditions in Bell Textron Inc. Model 204B, 205A, 205A-1, 205B, 210, and 212 helicopters. It targets defective main rotor hub strap pins, part number 204-012-104-005 with serial number prefix "FNFS", which have been linked to a fatal accident due to pin failure causing rotor detachment.

Airworthiness Directive

Bell Textron Inc. (Bti) 204B
Bell Textron Inc. (Bti) 205
Bell Textron Inc. (Bti) 210
Bell Textron Inc. (Bti) 212
Bell Textron Inc. 204B
Bell Textron Inc. 205A1
Bell Textron Inc. 205B
Bell Textron Inc. 210
Bell Textron Inc. 212

EASA AD US-2021-15-51

Superseded by FAA AD 2022-02-02

FAA Airworthiness Directive 2021-15-51 is a final rule addressing unsafe conditions in certain Bell Textron Inc. Model 204B, 205A, 205A-1, 205B, and 212 helicopters. It targets main rotor hub strap pins, part number 204-012-104-005 with serial number prefix "FNFS", which have been found to shear off during flight, causing detachment of the main rotor blade and head. This directive follows a fatal accident and mandates removal of these pins from service to ensure flight safety.

Airworthiness Directive

Bell Textron Inc. (Bti) 204B
Bell Textron Inc. (Bti) 205
Bell Textron Inc. (Bti) 212
Bell Textron Inc. 204B
Bell Textron Inc. 205A1
Bell Textron Inc. 205B
Bell Textron Inc. 212

EASA AD 2021-0148

Equipment & Furnishings — Emergency Flotation System — Rotorcraft Flight Manual (Supplement)

EASA Airworthiness Directive 2021-0148 is an update addressing the Emergency Flotation System (EFS) information in the Rotorcraft Flight Manual (Supplement) for Sikorsky S-76 and S-92A helicopters, Bell Helicopter Textron 212, 214B, 214ST, 412 series, and Bell Helicopter Textron Canada 222, 230, and 430 helicopters equipped with EFS. It mandates amendments to the Limitations Section of the flight manuals to include demonstrated sea state conditions for ditching performance of the EFS. This directive applies to helicopters with EFS installed as optional kits or via Supplemental Type Certificates.

Airworthiness Directive

Bell 222
Bell 230
Bell 430
Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 214ST
Bell Textron Inc. (Bti) 412
Mcdermott 214 Holdings, 214
Sikorsky S-76
Sikorsky S-92
Sikorsky S-92A
Bell Helicopter Textron 212
Bell Helicopter Textron 214B
Bell Helicopter Textron 214ST
Bell Helicopter Textron 412
Bell Helicopter Textron Canada 222
Bell Helicopter Textron Canada 230
Bell Helicopter Textron Canada 430

EASA AD US-2020-19-08

Main Rotor - Main Rotor Hub Tension-torsion Strap Assembly - Life Limit / Removal

Federal Register Volume 85, Number 180 (September 16, 2020) is a final rule airworthiness directive issued by the FAA addressing Bell Textron Inc. Model 204B, 205A-1, and 212 helicopters. It focuses on the main rotor hub tension-torsion strap assembly part number 204-012-112-005 due to corrosion issues. The directive mandates reducing the life limit of this TT strap assembly and prohibits its installation on any helicopter.

Airworthiness Directive

Bell Textron Inc. (Bti) 204B
Bell Textron Inc. (Bti) 205
Bell Textron Inc. (Bti) 212
Bell 204B
Bell 205A-1
Bell 212

EASA AD US-2020-16-10

Seat Belt Shoulder Harness - Inspection / Modification

Airworthiness Directive 2020-16-10 is a final rule issued by the FAA addressing certain Bell Textron Inc. helicopters, including Models 204B, 205A, 205A-1, 205B, 212, 214B, 214B-1, 412, 412CF, and 412EP. The directive focuses on the removal and inspection of specific shoulder harness seat belt comfort clips with part numbers D7LZ-6560286-A, D7LZ-6560286-B, and 504636-401. It aims to prevent interference with the seat belt inertia reel that could compromise occupant safety during emergency landings.

Airworthiness Directive

Bell Textron Inc. (Bti) 204B
Bell Textron Inc. (Bti) 205
Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412
Mcdermott 214 Holdings, 214
Bell Textron Inc. 204B
Bell Textron Inc. 205A1
Bell Textron Inc. 205B
Bell Textron Inc. 212
Bell Textron Inc. 214B1
Bell Textron Inc. 412
Bell Textron Inc. 412CF
Bell Textron Inc. 412EP

EASA AD US-2020-12-10

Tail Rotor Blades - Inspection / Repair / Replacement

Airworthiness Directive 2020-12-10 is a final rule issued by the FAA addressing Bell Textron Inc. helicopters, specifically models 205A, 205A-1, 205B, 212, 412, 412CF, and 412EP equipped with tail rotor blades part number 212-010-750. The directive focuses on inspecting these tail rotor blades for corrosion and pitting to prevent potential cracks and loss of control. It updates previous requirements by excluding certain newer tail rotor blades from inspection applicability.

Airworthiness Directive

Bell Textron Inc. (Bti) 205
Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412
Bell 205A1
Bell 205B
Bell 212
Bell 412
Bell 412CF
Bell 412EP