AD 76-13-11 R1

Airworthiness directive · Aft Fuselage Longerons · K & L Soaring SGS 2-33, SGS 2-33A, SGU 2-22C and 3 more

Effective
May 25, 1988
Models
SGS 2-33, SGS 2-33A, SGU 2-22C, SGU 2-22CK, SGU 2-22E, SGU 2-22EK
Data sheets
TCDSG-18TCDSG2EA
Registered aircraft
282 matched by model
Product
Aircraft · Glider
Amendment
39-5924

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

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

Adoption of the amendment

76-13-11 R1 SCHWEIZER: Amendment 39-2659 as amended by Amendment 39-5924. Applies to SGS 2-33, SGS 2-33A, S/N's 1 thru 424, and SGU 2-22C, CK, E, EK, S/N's 98 thru 258.

To prevent failure of the forward and aft fuselage tubular longerons due to internal corrosion caused by trapped water accomplish the following:

Within the next 30 days or 25 hours in service, whichever occurs first, after the effective date of this Airworthiness Directive, unless already accomplished, perform the following or an approved equivalent inspection.

(a) In the forward keel tube drill a No. 41 hole just ahead of the tow release slot.

(b) In the aft longerons drill a No. 41 hole approximately one inch forward of the weld cluster at the tail skid in the lower longerons.

(c) If there is any water drainage inspect for corrosion using x-ray or an approved equivalent inspection.

(d) Repair corroded parts prior to further flight, in accordance with an approved repair or replace with an unused part of the same part number or an approved equivalent part.

(e) Subsequent to the inspections, the No. 41 holes must be sealed with either a drive screw or a self plugging blind rivet. Holes may be enlarged to .125 inches for installation of a blind rivet. A waterproof sealant must be applied when installing the screw or rivet.

(f) Upon request, an equivalent means of compliance with the requirements of this AD may be approved by the Manager, New York Aircraft Certification Office, New England Region, Federal Aviation Administration, 181 South Franklin Avenue, Room 202, Valley Stream, New York 11581.

(g) Upon submission of substantiating data, by an owner or operator through an FAA Airworthiness Inspector, the Manager, New York Aircraft Certification Office, may adjust the compliance time specified in this AD.

(Schweizer Service Bulletin No. 102-33-1.1, covers this subject and is considered an approved equivalent inspection).

Amendment 39-2659, became effective July 7, 1976.

This Amendment 39-5924 amends AD 76-13-11, Amendment 39-2659 (41 FR 27029; July 1, 1976).

This Amendment 39-5924 becomes effective on May 25, 1988.

Affected TCDS · 2

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

Registered aircraft · 282

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
  • Schweizer282 aircraft
By year built
19471981
Registered aircraft by year built: 238 aircraft
19471
19581
19591
19605
19612
19624
19638
19649
196510
19667
196729
196814
196911
197012
197111
197212
197318
197421
197510
197618
197710
197812
19796
19803
19813

44 with no year recorded

By model

Aircraft

See all 282 aircraft