AD 78-18-05

AD Final Rules - DRS_78-18-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
78-18-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Aerostar Model 600, 601 and 601P Airplanes
Subject:
Wing Tank Fuel Quantity Indicator
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
09/13/1978
Make:
Aerostar Aircraft Corporation
Model:
PA-60-600 (Aerostar 600) | PA-60-601 (Aerostar 601) | PA-60-601P (Aerostar 601P)
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 78-18-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3295

AD NUMBER:   78-18-05

SUBJECT HEADING:   Airworthiness Directives; Piper Aerostar Model 600, 601 and 601P Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective September 13, 1978.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
78-18-05 PIPER AEROSTAR: Amendment 39-3295. Applies to Piper Aerostar Model 600, 601 and 601P airplanes certificated in all categories, serial numbers 150 through 520.

Compliance required as indicated. To prevent reversed readings of left and right wing tank fuel quantity accomplish the following:

(a) Within 10 hours time in service after the effective date of this AD, unless already accomplished, with LH and RH wing tanks at least 50% depleted from tank capacity:

1) Read and record fuel quantity indication for LH and RH wing fuel tanks.

2) Add 10 gallons of fuel to one wing tank only.

3) Read and record fuel quantity for each wing tank.

4) Determine that the added fuel registers on the correct wing tank fuel quantity indicator selector position.

5) If the correct wing tank fuel quantity selector position registers the added fuel, the system is normal and no further action is required under this AD.

(b) If the appropriate wing tank fuel indicator position does not correctly register the added fuel the system may be improperly wired or the selector may be improperly indexed. In this event, prior to further flight:

Correct the fuel quantity indicating system malfunction. Refer to figure 1 for details of proper switch installation.

(c) Within 10 hours time in service after the effective date of this AD, on those airplanes with the fuel quantity indicating selector switch relabelled as an interim solution under (B)(2) of the original message of July 7, 1978, correct the fuel quantity indicating system as in (b) of this AD and revert to standard switch labelling.

(d) Special flight permits may be issued in accordance with FARs 21.197 and 21.199 to operate aircraft to a base for accomplishment of the repair required by paragraph (b) of this AD.

(e) Equivalent inspections and repairs may be used when approved by the Chief, Aircraft Engineering Division, FAA Western Region.

This amendment becomes effective September 13, 1978.




FOOTER: