AD 72-17-01

Airworthiness directive · Induction Air Box Valve · Piper PA-34-200

Effective
April 26, 1973
Published
April 23, 1973
Issued
April 12, 1973
Model
PA-34-200
Data sheet
TCDSA7SO
Registered aircraft
172 matched by model
Product
Aircraft · Small airplane
Amendment
39-1625

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.

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The airworthiness directive

72-17-01 PIPER: Amendment 39-1500 as amended by Amendment 39-1625. Applies to PA-34-200 airplanes, Serial Nos. 34-E4 and 34-7250001 through 34-7350074.

Compliance required as indicated.

To prevent the possibility of a power loss due to the failure of the induction air box valve, accomplish the following:

(a) For those airplanes with 100 or more hours time in service on the effective date of this airworthiness directive unless already accomplished within the last 100 hours time in service comply with paragraph (c) within the next 10 hours time in service and thereafter at intervals not to exceed 100 hours time in service from the last inspection.

(b) For those airplanes with less than 100 hours time in service on the effective date of this airworthiness directive, unless already accomplished, comply with paragraph (c) upon the accumulation of 100 hours time in service or within the next 10 hours, whichever is later, and thereafter at intervals not to exceed 100 hours time in service from the last inspection.

(c) Remove the induction air box assembly from each engine and remove the valve assembly from the box assembly to permit a thorough visual inspection of the valve assembly. Inspect the valve assembly for any evidence of excessive wear or cracks in the areas where the shaft mates to the valve assembly.

(d) If valve assemblies are found to contain worn, loose, or cracked parts, replace the affected parts with serviceable parts of the same part numbers or incorporate Piper Kit Number 760 722V before further flight.

(e) Reassemble induction air boxes, install and rig in accordance with PA-34 service manual.

Piper Service Bulletin Number 358 dated August 2, 1972, pertains to this subject.

(f) The requirements of this AD do not apply when Piper Kit Number 760 722V is incorporated. Piper Service Bulletin No. 374 dated February 16, 1973, pertains to this subject.

Amendment 39-1500 was effective August 17, 1972, andwas effective upon receipt for all recipients of the air mail letter dated August 4, 1972, which contained this amendment.

This amendment 39-1625 becomes effective April 26, 1973.

Affected TCDS · 1

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

Registered aircraft · 172

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
  • Piper172 aircraft
By year built
19711980
Registered aircraft by year built: 138 aircraft
19717
197267
197341
197422
19801

34 with no year recorded

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