AD 74-19-01

Airworthiness directive · Outer Wing Spars · Piper PA-28-235, PA-32-260, PA-32-300 and 1 more

Effective
September 7, 1974
Published
September 6, 1974
Issued
August 28, 1974
Models
PA-28-235, PA-32-260, PA-32-300, PA-34-200
Registered aircraft
2,674 matched by model
Product
Aircraft · Small airplane
Amendment
39-1952

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 November 21, 2025.

On this page

The airworthiness directive

74-19-01 PIPER: Amendment 39-1952. Applies to Piper PA-28-235 airplanes, serial numbers 28-7410001 through 28-7410090, PA-32-260 airplanes serial numbers 32-7400001 through 32-7400047, PA-32-300 airplanes 32-7440001 through 32-7440147, and PA-34-200 airplanes serial numbers 34-7450001 through 34-7450205 certificated in all categories.

Compliance required within the next ten hours time in service after the effective date of this AD, unless already accomplished.

To detect improperly formed lightening holes in the outer wing spars, accomplish the following:

(a) PA-28-235 and PA-32 series airplanes

(1) Remove the inspection plate on bottom of wing which is located adjacent to the aileron bellcrank.

(2) Inspect both sides of left and right spar around the first lightening hole outboard of the fish mouth of the main spar splice for evidence of a die stamping mark approximately six by six inches square surrounding the lightening hole area.

(3) Inspect the lightening hole flange radius for cracks.

(b) PA-34 series airplanes

(1) Remove the inspection plate on bottom of wing which is located adjacent to the aileron bellcrank and aft of the outboard fuel tank.

(2) Inspect as in paragraph (a)(2) around first and second lightening holes outboard of the fish mouth at the main spar splice.

(3) Inspect the lightening flange radii for cracks.

(c) If square die stamping mark is evident on the aft side of spar only and there are no cracks in the lightening hole flange radii, no further action is required.

(d) If square die stamping mark is evident on forward side of spar and/or if there are cracks in the lightening hole flange, replace the outboard spar with a serviceable spar of the same part number or repair in a method approved by the Chief, Engineering and Manufacturing Branch, FAA Southern Region.

(e) Report positive findings from paragraph (d) to Chief, Engineering and Manufacturing Branch, FAA SouthernRegion within 10 days of inspection.

(Reporting approved by the Bureau of the Budget under BOB No. 04-R0174.)

This amendment becomes effective September 7, 1974.

Affected TCDS · 3

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

Registered aircraft · 2,674

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
  • Piper2,673 aircraft
  • Piper/Valdes-Ervin1 aircraft
By year built
19481980
Registered aircraft by year built: 2,296 aircraft
19481
196387
1964136
1965129
1966277
1967227
1968158
1969172
197048
197188
1972189
1973206
1974132
1975101
197661
197763
1978101
1979118
19802

378 with no year recorded

By model

Aircraft

See all 2,674 aircraft