Airworthiness directive · Withdrawal of AD 99-05-13 · Beech B17B, B17L, B17R (Army UC-43H) and 107 more

Effective
July 5, 2000
Issued
July 5, 2000
Supersedes
AD99-05-13
Models
B17B, B17L, B17R (Army UC-43H), C17B (Army UC-43G), C17L (Army UC-43J), C17R (Army UC-43E) and 104 more
Registered aircraft
13,521 matched by model
Product
Aircraft · Small airplane
Amendment
39-11061
Docket
98-CE-61-AD

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 May 30, 2024.

On this page

Summary

This amendment withdraws Airworthiness Directive (AD) 99-05-13, which currently applies to Raytheon Aircraft Company (Raytheon) Beech 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55, 56, 58, 58P, 58TC, 60, 65, 70, 76, 77, 80, 88, and 95 series airplanes. AD 99-05-13 requires installing a placard on the fuel tank selector to warn of the no-flow condition that exists between the fuel tank detents. Since the issuance of AD 99-05-13, the Federal Aviation Administration (FAA) has re-evaluated all information related to this subject, and determined that the subject matter in this AD is an operational issue and does not address an unsafe condition. Accordingly, this action withdraws AD 99-05-13.

The airworthiness directive

99-05-13 RAYTHEON AIRCRAFT COMPANY (Formerly Beech): Amendment 39-11061 Docket No. 98-CE-61-AD.

Applicability: Models 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55, 56, 58, 58P, 58TC, 60, 65, 70, 76, 77, 80, 88, and 95 Series Airplanes.

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

Supplementary information

Discussion

Has FAA taken any action to this point? Reports of engine stoppage on Raytheon Beech 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55, 56, 58, 58P, 58TC, 60, 65, 70, 76, 77, 80, 88, and 95 series airplanes caused FAA to issue AD 99-05-13, Amendment 39-11061 (64 FR 10560, March 5, 1999). AD 99-05-13 currently requires installing a placard on the fuel tank selector to warn of the no-flow condition that exists between the fuel tank detents.

After issuing AD 99-05-13, we re-evaluated all information related to the subject matter of this AD and determined that:

- the positioning of the fuel selector is an operational issue and not an unsafe condition under part 39 of the Federal Aviation Regulations (14 CFR part 39) and should be handled by other methods;

- normal operating and procedural information such as this should be handled through regular revisions to the Airplane Flight Manual (AFM) or Pilot s Operating Handbook (POH); and

- issuing an AD to require a placard that conveys normal operating information reduces the pilots sensitivity to true emergency information that should be conveyed by placards.

Consequently, FAA issued a proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to withdraw AD 99-05-13. This proposal published in the Federal Register as a notice of proposed rulemaking (NPRM) on March 30, 2000 (65 FR 16845).

Was the public invited to comment? The FAA invited interested persons to participate in the making of this amendment. The following describes each comment and presents FAA's response.

Comment Issue No. 1: AD is Valid if an Unsafe Condition Exists What is the Commenter's Concern? One commenter states that FAA is withdrawing this AD because it is an operational issue and should be handled by other methods. The commenter believes that the AD is valid because FAA has the authority to issue an AD on any issue as long as an unsafe condition exists.

What is FAA s Response to the Concern? We concur that we have the authority and responsibility to act on an unsafe condition, regardless of the factors that create the unsafe condition. We were in error in including information in the NPRM specifying that an operational procedure cannot be the subject of an AD. However, we determined that the fuel selector valve, when functioning properly and used properly, does not create an unsafe condition. The FAA determined that the procedures to operate the fuel selector valve are readily available and that our authority is not to issue AD's against aircraft where the operators do not operate the equipment correctly. Utilizing positive detent to assure that the fuel valve is fully open to the tank selected is considered a standard design practice in the aircraft industry.

We are not changing the AD action as a result of this comment.

Comment Issue No. 2: AD is Needed for Airplanes Without an AFM/POH What is the Commenter's Concern? One commenter states that many airplanes currently affected by AD 99-05-13 are not required to have a POH, and Civil Aviation Regulations (CAR) part 3 allows a manufacturer to use placards instead of an AFM. The commenter believes that, for these reasons, the AD is valid.

What is FAA s Response to the Concern? We concur that many aircraft do not require a POH and were certificated under CAR part 3 where the use of placards is acceptable over an AFM. However, airplanes in this situation usually only have placards installed that contain safety information when an unusual design, operating, or handling characteristic is prevalent.

The FAA has the authority to issue an AD to require operational placards. However, as discussed above, utilizing a positive detent to assure that the fuel valve is fully open to the tank selected is considered a standard design practice in the aircraft industry.

We are not changing the AD action as a result of this comment.Comment Issue No. 3: Placards Are Necessary to Convey Safe Operation What is the Commenter's Concern? One commenter states that the AD is valid because placards are necessary to convey safe operation for airplanes certificated under the Civil Aviation Regulations and part 23 of the Federal Aviation Regulations (14 CFR part 23). The commenter also states that placards should not be limited to only emergency information.

What is FAA s Response to the Concern? We concur that placards are not just limited to emergency information. All required placards should convey information for safe operation. However, both CAR 3.777/3.777-1 and 14 CFR 23.1541 state that placards should convey safe operation information if the aircraft has unusual design, operation, or handling characteristics. As discussed previously, utilizing a positive detent to assure that the fuel valve is fully open to the tank selected is considered a standard design practice in the aircraft industry.

We arenot changing the AD action as a result of this comment.

Comment Issue No. 4: FAA has Changed the Definition of Unsafe Condition What is the Commenter's Concern? One commenter states that, by withdrawing AD 99-05-13, FAA will have changed the historical definition of an unsafe condition. We infer that the commenter wants to maintain the effectiveness of AD 99-05-13.

What is FAA s Response to the Concern? We do not concur that we have altered the definition of an unsafe condition. Determination of an unsafe condition is based on each individual situation. Factors that are considered include the design, operation, or handling characteristics of the type design airplanes. As discussed above, utilizing a positive detent to assure that the fuel valve is fully open to the tank selected is considered a standard design practice in the aircraft industry.

We are not changing the AD action as a result of this comment.

Comment Issue No. 5: Numerous Occurrences Justify the Current AD What is the Commenter's Concern? One commenter states that placing a warning placard specifying the safe operation of the fuel selector as AD 99-05-13 requires supports the 49 occurrences from the records of the National Transportation Safety Board (NTSB). We infer that the commenter wants to maintain the effectiveness of AD 99-05-13.

What is FAA s Response to the Concern? We do not concur with the commenter's assessment. We have reviewed 37 reports of the above-referenced 49 occurrences (commenter only provided 37). Approximately half of the occurrences listed the cause as fuel starvation in combination with the fuel selector not positioned in the detent. The most prevalent cause was failure to follow checklist procedures. In no instance was the pilot's lack of knowledge or understanding of the positioning of the fuel selector listed as the cause of the occurrence.

In addition, NTSB has not recommended that FAA issue an AD on this subject. Therefore, weconclude that the commenter believes NTSB supports the placard requirement, when in fact, NTSB has made no recommendation supporting it. Again, utilizing a positive detent to assure that the fuel valve is fully open to the tank selected is considered a standard design practice in the aircraft industry.

We are not changing the AD action as a result of this comment.

The FAA's Determination What is FAA's final determination on this issue? Based on the above information, FAA has determined that there is no need for AD 99-05-13 and that it should be withdrawn.

This action withdraws AD 99-05-13. Withdrawal of AD 99-05-13 will not preclude us from issuing another notice in the future, nor will it commit us to any course of action in the future.

Regulatory Impact Since this action only withdraws an AD, it is not an AD and, therefore, is not covered under Executive Order 12866, the Regulatory Flexibility Act, or DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979).

List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Safety.

The Withdrawal Accordingly, FAA withdraws AD 99-05-13, Amendment 39-11061 (64 FR 10560, March 5, 1999).

Affected TCDS · 22

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

See all 22 data sheets

Registered aircraft · 13,521

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
  • Beech12,973 aircraft
  • Raytheon530 aircraft
  • Beech-Parks5 aircraft
  • Beech-Nogle4 aircraft
  • Beech/Bond2 aircraft
  • Other makers77 aircraft
By year built
19242016
Registered aircraft by year built: 11,673 aircraft
19241
19281
19343
19352
19366
193711
193810
193911
19404
19412
19425
194332
194438
19459
194625
194715
194885
194947
1950108
195189
1952122
1953149
1954142
1955243
1956226
1957259
1958196
1959263
1960248
1961245
1962235
1963251
1964430
1965338
1966436
1967360
1968343
1969265
1970205
1971148
1972227
1973361
1974398
1975404
1976439
1977478
1978525
1979563
1980424
1981355
1982195
1983115
1984126
198586
198661
1987102
1988121
198996
1990119
1991122
199272
199385
199490
199556
199644
199772
199866
199967
200067
200163
200230
20038
200418
20058
20071
20161

1,848 with no year recorded

By model

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Aircraft

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