AD 87-11-01 R1

final rule

Airworthiness Directives; Bellanca Model 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes

AD Number
87-11-01 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

Applicability

TypeManufacturerModelDetails
aircraft Alexandria Aircraft, LLC 17-30 Airworthiness Directives; Bellanca Model 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes
aircraft Alexandria Aircraft, LLC 17-30A Airworthiness Directives; Bellanca Model 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes
aircraft Alexandria Aircraft, LLC 17-31 Airworthiness Directives; Bellanca Model 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes
aircraft Alexandria Aircraft, LLC 17-31A Airworthiness Directives; Bellanca Model 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes
aircraft Alexandria Aircraft, LLC 17-31ATC Airworthiness Directives; Bellanca Model 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes
aircraft Alexandria Aircraft, LLC 17-31TC Airworthiness Directives; Bellanca Model 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes

Unsafe Condition

Engine power loss due to either the accumulation of water or other contaminants in the fuel system or due to mismanagement of available fuel resources caused by lack of pilot familiarity with the airplane fuel system design and operating procedures.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect fuel filler caps and fuel filler well drains per Bellanca Service Letter No. B-105. Install specified AFM revisions and placards with minimum 1/10 inch height as outlined in the AD. Placards must state specific warnings and fuel tank capacities at designated locations.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within the next 30 days after the effective date of this AD or at the next annual inspection, whichever occurs later, and thereafter at each annual inspection for inspections. For AFM revisions and placards, within the next 30 days after the effective date.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Bellanca Models 17-30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC (all serial numbers) airplanes certificated in any category.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Fuel Caps & Drains

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_87-11-01_R.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
87-11-01 R1
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bellanca Model 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes
Subject:
Fuel Caps & Drains
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/28/1987
Make:
Alexandria Aircraft, LLC
Model:
17-30 | 17-30A | 17-31 | 17-31A | 17-31ATC | 17-31TC
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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 87-11-01 R1
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5684

AD NUMBER:   87-11-01 R1

SUBJECT HEADING:   Airworthiness Directives; Bellanca Model 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 28, 1987.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
87-11-01 R1 BELLANCA: Amendment 39-5624 as amended by Amendment 39-5684. Applies to Models 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC (all serial numbers) airplanes certificated in any category.

Compliance: Required as indicated, unless already accomplished.

To preclude engine power loss due to either the accumulation of water or other contaminants in the fuel system or due to mismanagement of available fuel resources caused by lack of pilot familiarity with the airplane fuel system design and operating procedures, accomplish the following:

(a) For all airplanes, within the next 30 days after the effective date of this AD or at the next annual inspection, whichever occurs later, and thereafter at each annual inspection, inspect the fuel filler caps and fuel filler well (scupper) drains in accordance with the instructions contained in Section II of Bellanca Service Letter No. B-105, dated February 2, 1987.

(b) For Bellanca Models and Serials identified in Table 1., within the next 30 days after the effective date of this AD, accomplish the following:

(1) Install the appropriate AFM revision, as specified in Table 1.

(2) Install permanent placards which state the following at the specified airplane locations:

(i) For Models 17-30 and 17-30A, on the instrument panel adjacent to the auxiliary fuel pump switch: "USE TO RESTORE FUEL PRESSURE AND RELEASE TO PREVENT ENGINE FLOODING."

(ii) On the instrument panel adjacent to the fuel quantity gauges: "FUEL GAUGES READ QUANTITY IN TANK SELECTED, MAIN FUEL TANK GAUGE INOPERATIVE WHEN AUXILIARY TANK SELECTED. FUEL REMAINING IN SELECTED TANK CANNOT BE USED SAFELY IN FLIGHT WHEN GAUGE READS ZERO."

(iii) On the console adjacent to the fuel selector valve (on airplanes with a 58 gallon capacity fuel system):

"LEFT TANK: 15.5 GALLONS
RIGHT TANK: 15.5 GALLONS
AUXILIARY TANK: 20 GALLONS
USE AUX. TANK IN LEVEL FLIGHT ONLY."

(3) Placards specified in (b)(2)(i), (b)(2)(ii), and (b)(2)(iii) may be fabricated and installed using letters with minimum 1/10 inch height.

NOTE: The AFM revisions specified above (and associated placards) are available at a nominal cost from Bellanca, Inc., P.O. Box 964, Alexandria, Minnesota 56308; Telephone (612) 762-1501. The placards are revised versions of existing placards. The existing placards may either be removed and discarded or overlaid by the corresponding revised placard. The placard specified in paragraph (2)(iii) deletes information which was contained in the placard being replaced. This information, however, is presented more clearly in the placard of paragraph (2)(ii) which is a new placard for the airplanes to which paragraph (2)(iii) applies.

(c) The requirements of paragraph (b) of this AD may be accomplished by the holder of a pilot certificate issued under Part 61 of the Federal Aviation Regulations (FAR) on any airplane owned or operated by him, provided the airplanes are not used in air taxi operations. The person accomplishing these actions must make the appropriate aircraft maintenance record entry as prescribed by FAR 91.173.

(d) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished.

(e) An equivalent means of compliance with this AD may be used if approved by the Manager, Chicago Aircraft Certification Office, FAA, 2300 East Devon Ave., Des Plaines, Illinois 60018; Telephone (312) 694-7357.

All persons affected by this directive may obtain copies of the document(s) referred to herein upon request to Bellanca, Inc., P.O. Box 964, Alexandria, Minnesota 56308; or may examine the document(s) referred to herein at FAA, Office of the Regional Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106.

Amendment 39-5624 became effective June 22, 1987.

This amendment, 39-5684, becomes effective on August 28, 1987.

Table 1.
Serial Numbers (may be AFM Revision Model prefixed with year of manufacture) to be installed.
17-30	30001 - 30262	Rev. 15, dtd. 2/2/87
-30A	30263 - 30514 (except 30498)	Rev. 6, dtd. 2/2/87
-31	32-1 - 32-14	Rev. 2, dtd. 2/2/87
-31A	32-15 - 32-102	Rev. 8, dtd. 2/2/87
-31TC	31001 - 31003	Rev. 2, dtd. 2/2/87
-31ATC	31004 - 31046	Rev. 8, dtd. 2/2/87


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_87-11-01_R.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
87-11-01 R1
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bellanca Model 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes
Subject:
Fuel Caps & Drains
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/28/1987
Make:
Alexandria Aircraft, LLC
Model:
17-30 | 17-30A | 17-31 | 17-31A | 17-31ATC | 17-31TC
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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 87-11-01 R1
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5684

AD NUMBER:   87-11-01 R1

SUBJECT HEADING:   Airworthiness Directives; Bellanca Model 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 28, 1987.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
87-11-01 R1 BELLANCA: Amendment 39-5624 as amended by Amendment 39-5684. Applies to Models 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC (all serial numbers) airplanes certificated in any category.

Compliance: Required as indicated, unless already accomplished.

To preclude engine power loss due to either the accumulation of water or other contaminants in the fuel system or due to mismanagement of available fuel resources caused by lack of pilot familiarity with the airplane fuel system design and operating procedures, accomplish the following:

(a) For all airplanes, within the next 30 days after the effective date of this AD or at the next annual inspection, whichever occurs later, and thereafter at each annual inspection, inspect the fuel filler caps and fuel filler well (scupper) drains in accordance with the instructions contained in Section II of Bellanca Service Letter No. B-105, dated February 2, 1987.

(b) For Bellanca Models and Serials identified in Table 1., within the next 30 days after the effective date of this AD, accomplish the following:

(1) Install the appropriate AFM revision, as specified in Table 1.

(2) Install permanent placards which state the following at the specified airplane locations:

(i) For Models 17-30 and 17-30A, on the instrument panel adjacent to the auxiliary fuel pump switch: "USE TO RESTORE FUEL PRESSURE AND RELEASE TO PREVENT ENGINE FLOODING."

(ii) On the instrument panel adjacent to the fuel quantity gauges: "FUEL GAUGES READ QUANTITY IN TANK SELECTED, MAIN FUEL TANK GAUGE INOPERATIVE WHEN AUXILIARY TANK SELECTED. FUEL REMAINING IN SELECTED TANK CANNOT BE USED SAFELY IN FLIGHT WHEN GAUGE READS ZERO."

(iii) On the console adjacent to the fuel selector valve (on airplanes with a 58 gallon capacity fuel system):

"LEFT TANK: 15.5 GALLONS
RIGHT TANK: 15.5 GALLONS
AUXILIARY TANK: 20 GALLONS
USE AUX. TANK IN LEVEL FLIGHT ONLY."

(3) Placards specified in (b)(2)(i), (b)(2)(ii), and (b)(2)(iii) may be fabricated and installed using letters with minimum 1/10 inch height.

NOTE: The AFM revisions specified above (and associated placards) are available at a nominal cost from Bellanca, Inc., P.O. Box 964, Alexandria, Minnesota 56308; Telephone (612) 762-1501. The placards are revised versions of existing placards. The existing placards may either be removed and discarded or overlaid by the corresponding revised placard. The placard specified in paragraph (2)(iii) deletes information which was contained in the placard being replaced. This information, however, is presented more clearly in the placard of paragraph (2)(ii) which is a new placard for the airplanes to which paragraph (2)(iii) applies.

(c) The requirements of paragraph (b) of this AD may be accomplished by the holder of a pilot certificate issued under Part 61 of the Federal Aviation Regulations (FAR) on any airplane owned or operated by him, provided the airplanes are not used in air taxi operations. The person accomplishing these actions must make the appropriate aircraft maintenance record entry as prescribed by FAR 91.173.

(d) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished.

(e) An equivalent means of compliance with this AD may be used if approved by the Manager, Chicago Aircraft Certification Office, FAA, 2300 East Devon Ave., Des Plaines, Illinois 60018; Telephone (312) 694-7357.

All persons affected by this directive may obtain copies of the document(s) referred to herein upon request to Bellanca, Inc., P.O. Box 964, Alexandria, Minnesota 56308; or may examine the document(s) referred to herein at FAA, Office of the Regional Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106.

Amendment 39-5624 became effective June 22, 1987.

This amendment, 39-5684, becomes effective on August 28, 1987.

Table 1.
Serial Numbers (may be AFM Revision Model prefixed with year of manufacture) to be installed.
17-30	30001 - 30262	Rev. 15, dtd. 2/2/87
-30A	30263 - 30514 (except 30498)	Rev. 6, dtd. 2/2/87
-31	32-1 - 32-14	Rev. 2, dtd. 2/2/87
-31A	32-15 - 32-102	Rev. 8, dtd. 2/2/87
-31TC	31001 - 31003	Rev. 2, dtd. 2/2/87
-31ATC	31004 - 31046	Rev. 8, dtd. 2/2/87


FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.