Published 1998-04-22 · Federal Register document 98-10596
Airworthiness Directives; Pilatus Aircraft Ltd. Model PC-12 Airplanes
Publication summary
This action confirms the effective date of Airworthiness Directive (AD) 98-05-06, which applies to Pilatus Aircraft Ltd. (Pilatus) Model PC-12 airplanes. AD 98-05-06 requires inspecting the elevator for incorrect rivet lengths and installing new rivets if incorrect rivet lengths are found. This AD also requires inspecting the elevator to assure that an excessive gap (more than .004 inches or .1 millimeters (mm)) does not exist in the rivet shanks, and installing a shim between the rib and skin to fill any excessive gap. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified in this AD are intended to prevent fatigue damage to the elevator, which could result in structural failure and eventual loss of control of the airplane.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:22:53.985165+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_1998-f5c1cf5c93c99179
- Source row
- results[220]
- Raw source SHA-256
- f5c1cf5c93c99179023030016db80652e7593139090148c64a6fd533918aa991
Publication role unknown
Recorded publication clauses
- AD identifier printed in this edition
- Unknown
- Effective date printed in this edition
- Unknown
No adopted-clause structure was recorded for this source edition. Read the complete text; no applicability conclusion has been inferred.
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: b2afc776933f106c470d30961079af611f20c231ec72a1afe3cac84adae2d840. Source manifest: f0235d9cfffad9c42ecaf6c49c9260fe22ae5159f413de7d93c0afa6a458f96e.
Official source · 1998-04-22
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 63, Number 77 (Wednesday, April 22, 1998)]
[Rules and Regulations]
[Pages 19798-19799]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-10596]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 97-CE-98-AD; Amendment 39-10367; AD 98-05-06]
RIN 2120-AA64
Airworthiness Directives; Pilatus Aircraft Ltd. Model PC-12
Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Direct final rule; confirmation of effective date.
-----------------------------------------------------------------------
SUMMARY: This action confirms the effective date of Airworthiness
Directive (AD) 98-05-06, which applies to Pilatus Aircraft Ltd.
(Pilatus) Model PC-12 airplanes. AD 98-05-06 requires inspecting the
elevator for incorrect rivet lengths and installing new rivets if
incorrect rivet lengths are found. This AD also requires inspecting the
elevator to assure that an excessive gap (more than .004 inches or .1
millimeters (mm)) does not exist in the rivet shanks, and installing a
shim between the rib and skin to fill any excessive gap. This AD is the
result of mandatory continuing airworthiness information (MCAI) issued
by the airworthiness authority for Switzerland. The actions specified
in this AD are intended to prevent fatigue damage to the elevator,
which could result in structural failure and eventual loss of control
of the airplane.
EFFECTIVE DATE: May 29, 1998.
FOR FURTHER INFORMATION CONTACT: Mr. Roman T. Gabrys, Aerospace
Engineer, Small Airplane Directorate, Airplane Certification Service,
FAA, 1201 Walnut, suite 900, Kansas City, Missouri 64106; telephone:
(816) 426-6932; facsimile: (816) 426-2169.
SUPPLEMENTARY INFORMATION: The FAA published this direct final rule
with request for comments in the Federal Register on March 3, 1998 (63
FR 10299). The FAA uses the direct final rulemaking procedure for a
non-controversial rule where the FAA anticipates that there will be no
adverse public comment. This direct final rule advised the public that
no adverse comments were anticipated, and that unless a written adverse
comment, or a written notice of intent to submit such an adverse
comment, was received within the comment period, the regulation would
become effective on May 29, 1998. No adverse comments were received,
and thus this notice confirms that this final rule will become
effective on that date.
[[Page 19799]]
Issued in Kansas City, Missouri, on April 14, 1998.
Michael Gallagher,
Manager, Small Airplane Directorate, Aircraft Certfication Service.
[FR Doc. 98-10596 Filed 4-21-98; 8:45 am]
BILLING CODE 4910-13-U
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T05:03:28.414840+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 7a7a8923b556e7249d3c49582da094db4755659e9a5853ca1bf71b93066da9bf
- Text SHA-256
- b2afc776933f106c470d30961079af611f20c231ec72a1afe3cac84adae2d840
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.