AD 78-09-02

Airworthiness directive · Emergency Float Kits · Bell Helicopter Textron 212

Effective
May 9, 1978
Model
212
Data sheet
TCDSH4SW
Registered aircraft
59 matched by model
Product
Aircraft · Rotorcraft
Amendment
39-3203

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

On this page

The airworthiness directive

78-09-02 BELL: Amendment 39-3203. Applies to Bell Model 212 helicopters, certificated in all categories, that are equipped with emergency float kits 212-706-021 or 212-706-042 and that are operated under conditions that require ditching capability or aircraft floatation devices.

Compliance required as indicated.

To permit opening of the passenger emergency exits in the event of a ditching and deployment of the emergency float bags, accomplish the following, unless already accomplished in accordance with data previously approved by the FAA (including STC No. SH2746SW issued April 4, 1978):

Prior to further flight, after the effective date of this AD, modify the forward and aft passenger emergency exit on each side of the helicopter in accordance with information and/or data approved by the Chief, Engineering and Manufacturing Branch, FAA, Southwest Region, except that the helicopter may be flown in accordance with FAR 21.197 to a base where the work may be performed.This amendment becomes effective May 9, 1978.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 59

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Bell54 aircraft
  • Bell Helicopter Textron5 aircraft
By year built
19711995
Registered aircraft by year built: 50 aircraft
19711
19722
19733
19744
19754
19762
19774
19782
19798
19808
19813
19824
19841
19911
19932
19951

9 with no year recorded

By model

Aircraft

See all 59 aircraft