AD 69-12-01

Airworthiness directive · Air Induction Hose · Piper PA-28R-180 and PA-28R-200

Effective
June 10, 1969
Published
June 6, 1969
Issued
May 27, 1969
Models
PA-28R-180, PA-28R-200
Data sheet
TCDS2A13
Registered aircraft
1,759 matched by model
Product
Aircraft · Small airplane
Amendment
39-773

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

69-12-01 PIPER: Amdt. 39-773 applies to PA-28R-180 series airplanes, Serial Numbers 28-30004 through 28-31092 and to PA-28R-200 series airplanes, Serial Numbers 28-35000 through 28-35237, 28-35239 through 28-35251 and 38-35253 through 28-35256.

Compliance required as indicated.

To prevent the possibility of restricting air flow through the engine air induction system, accomplish the following:

(a) Within the next 10 hours' time in service after the effective date of this airworthiness directive, unless already accomplished, remove air induction inlet hose Piper Part Number 63633-43 and inspect for deterioration, broken or frayed cord wrapping, evidence of hose partially collapsed, indication of reinforcement wire slippage or evidence of wire not being bonded properly to the hose interior wall, especially in the vicinity of the Koroseal ties or clamps.

(b) If the hose shows any deterioration, as noted in (a), remove it from service. Install an airworthy hose, Piper P/N 63633-43, or Aero-Duct SCAT 3-1/4 O.D. hose, or MIL-H- 8796B Type 1 Class 3 hose, 22-1/2 long, making sure that the wire reinforcing coils extend over the pilot tubes at each end and under the clamps. Piper Kit 760 328 may be installed in lieu of duct replacement. (See Item (d) below).

(c) Repeat the inspections of item (a) above at intervals not to exceed 10 hours' time in service. These inspections need not be continued after installation of Piper Kit 760 328.

(d) Within the next 50 hours' time in service after the effective date of this AD, unless already accomplished, install a new Piper air induction hose installation Kit No. 760 328 in accordance with the instructions included with the kit.

(e) The inspection or kit installation time intervals (other than for the initial inspection) may be adjusted by an FAA inspector up to a maximum of 5 hours to coincide with aircraft annual or 100-hour scheduled inspections.

Other means of compliance with the requirements of this directive may be utilized, if approved by the Chief, Engineering and Manufacturing Branch, FAA, Southern Region.

(Piper Service Bulletin No. 297 covers this same subject.)

This amendment becomes effective 10 June 1969.

Affected TCDS · 1

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

Registered aircraft · 1,759

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
  • Piper1,759 aircraft
By year built
19671976
Registered aircraft by year built: 1,526 aircraft
1967144
1968260
1969216
197060
197195
1972179
1973187
1974105
1975162
1976118

233 with no year recorded

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Aircraft

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