Published 1999-02-19 · Federal Register document 99-4017
Airworthiness Directives; Allison Engine Company Model AE 3007A and AE 3007A1/1 Turbofan Engines; Correction
Publication summary
This document makes a correction to Airworthiness Directive (AD) 99-03-03 applicable to Allison Engine Company Model AE 3007A turbofan engines that was published in the Federal Register on January 29, 1999 (64 FR 4525). A full authority digital electronic control (FADEC) assembly part number (P/N) in the compliance section is incorrect. This document corrects that P/N. In all other respects, the original document remains the same.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:22:57.343810+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_1999-e9a7378e7e7d30d5
- Source row
- results[82]
- Raw source SHA-256
- e9a7378e7e7d30d51578560dc0677c56bb1fef0a9323224e2a0afe1544919217
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 99-03-03
- Effective date printed in this edition
- Unknown
This correction is a separate source edition; it is not counted as a new adopted rule.
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.
Find all recorded historical references to AD 99-03-03 · 0 printed reference observations in this pinned collection.
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: beba4cf7626b1b3986daf0fa0104c1124db2452d26a172eab9399d56bfcd0a2e. Source manifest: 4a3af6df20b9969f8495ff65a15a3b26ceb8fd318eba6316a9673cb2ddd50249.
Official source · 1999-02-19
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 64, Number 33 (Friday, February 19, 1999)]
[Rules and Regulations]
[Page 8233]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 99-4017]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 98-ANE-14; Amendment 39-11017; AD 99-03-03]
RIN 2120-AA64
Airworthiness Directives; Allison Engine Company Model AE 3007A
and AE 3007A1/1 Turbofan Engines; Correction
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: This document makes a correction to Airworthiness Directive
(AD) 99-03-03 applicable to Allison Engine Company Model AE 3007A
turbofan engines that was published in the Federal Register on January
29, 1999 (64 FR 4525). A full authority digital electronic control
(FADEC) assembly part number (P/N) in the compliance section is
incorrect. This document corrects that P/N. In all other respects, the
original document remains the same.
EFFECTIVE DATE: February 19, 1999.
FOR FURTHER INFORMATION CONTACT: Kyri Zaroyiannis, Aerospace Engineer,
Chicago Aircraft Certification Office, FAA, Small Airplane Directorate,
2300 East Devon Avenue, Des Plaines, IL 60018; telephone (847) 294-
7836, fax (847) 294-7834.
SUPPLEMENTARY INFORMATION: A final rule airworthiness directive
applicable to Allison Engine Company Model AE 3007A and AE 3007A1/1
turbofan engines, was published in the Federal Register on January 29,
1999 (64 FR 4525). The following correction is needed:
Sec. 39.13 [Corrected]
On page 4526, in the third column, in the Compliance Section, in
paragraph (c), in the sixth line, ``2306867'' is corrected to read
``23068670''.
Issued in Burlington, MA, on February 8, 1999.
David A. Downey,
Assistant Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 99-4017 Filed 2-18-99; 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 2026-10-09T04:52:56.048534+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 94e82d1bf556942a076c23659612ab0637f990dea2f8cb57904d5d6d8109dba1
- Text SHA-256
- beba4cf7626b1b3986daf0fa0104c1124db2452d26a172eab9399d56bfcd0a2e
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.