AD 98-24-19
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Embraer S.A. | EMB-145 | [Correction] Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 Series Airplanes |
| aircraft | Embraer S.A. | EMB-145ER | [Correction] Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 Series Airplanes |
| aircraft | Embraer S.A. | EMB-145LR | [Correction] Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 Series Airplanes |
| aircraft | Embraer S.A. | EMB-145MR | [Correction] Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 Series Airplanes |
Unsafe Condition
Increased flight idle thrust when the anti-icing system is active could result in landing overrun.
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Required Actions
Revise the Performance Section of the Airplane Flight Manual (AFM) to provide procedures to adjust landing distances with the anti-icing system active. Revise the Limitations Section of Supplement 6 of the AFM to prohibit certain approaches with the anti-icing system active.
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Compliance Time
Effective December 10, 1998
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Affected Aircraft
Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 series airplanes: EMB-145, EMB-145ER, EMB-145LR, EMB-145MR.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
AFM - Performance & Limitations Section
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - 982419.pdf Copy URL Document Versions Feedback DetailsAttachments/Public Comments AD Number: 98-24-19 Document Type: AD Final Rules Docket Number: 98-NM-317-AD Subject Heading: [Correction] Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-14...Show more Subject: AFM - Performance & Limitations Section Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/10/1998 Make: Embraer S.A. Model: EMB-145 | EMB-145ER | EMB-145LR | EMB-145MR Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 [63 FR 65050 No. 227 11/25/98] Comments: CORRECTION: [Federal Register: February 18, 1999 (Volume 64, Number 32); Page 7993-7994; www.access....Show more Automatic Zoom Actual Size Page Fit Page Width 50% 75% 100% 125% 150% 200% 300% 400% 125% of 8 1 [Federal Register: February 18, 1999 (Volume 64, Number 32)] [Rules and Regulations] [Page 7993-7994] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr18fe99-3] ––––––––––––––––––––––––––––––––––– DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 98-NM-317-AD; Amendment 39-10904; AD 98-24-19] RIN 2120-AA64 Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB- 145 Series Airplanes AGENCY: Federal Aviation Administration, DOT. ACTION: Final rule; correcting amendment. ––––––––––––––––––––––––––––––––––– SUMMARY: This document corrects information in an existing airworthiness directive (AD) that applies to certain Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 series airplanes. That AD currently requires revising the Performance Section of the Airplane Flight Manual (AFM) to provide the flightcrew with procedures to adjust landing distances for landings performed with the anti-icing system active. That AD also requires revising the Limitations Section of the AFM to prohibit certain types of approaches with the anti-icing system active. This document corrects a typographical error that resulted in reference to a supplement of the AFM that does not exist. This correction is necessary to ensure that the appropriate supplement of the AFM is revised. DATES: Effective December 10, 1998. The incorporation by reference of certain publications listed in the regulations was approved previously by the Director of the Federal Register as of December 10, 1998 (63 FR 65050, November 25, 1998). FOR FURTHER INFORMATION CONTACT: Thomas Peters, Aerospace Engineer, ACE-118A, FAA, Small Airplane Directorate, Atlanta Aircraft Certification Office, One Crown Center, 1895 Phoenix Boulevard, suite 450, Atlanta, Georgia 30349; telephone (770) 703-6063; fax (770) 703- 6097. SUPPLEMENTARY INFORMATION: On November 16, 1998, the Federal Aviation Administration (FAA) issued AD 98-24-19, amendment 39-10904 (63 FR 65050, November 25, 1998), which applies to certain Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB- 145 series airplanes. That AD requires revising the Performance Section of the Airplane Flight Manual (AFM) to provide the flightcrew with procedures to adjust landing distances for landings performed with the anti-icing system active. That AD also requires revising the Limitations Sections 2 of the AFM to prohibit certain types of approaches with the anti-icing system active. That AD was prompted by a report that increased (i.e., higher than normal) flight idle thrust may occur when the anti-icing system is active. The actions required by that AD are intended to ensure that the flightcrew is advised of appropriate landing field lengths when operating with the anti-icing system active, and that instrument approaches at certain flap settings are prohibited with the anti-icing system active. Increased flight idle thrust when the anti-icing system is active, if not corrected, could result in landing overrun. Need for the Correction As published, AD 98-24-19 contains a typographical error in paragraph (a)(2) of the AD. That paragraph specified a revision to the Limitations Section of Supplement 12 of the FAA-approved AFM; however, the correct supplement is Supplement 6. Supplement 12 of the AFM does not exist. The FAA has determined that a correction to AD 98-24-19 is necessary. The correction will ensure that the appropriate supplement of the AFM is revised. Correction of Publication This document corrects the error and revises the AD as an amendment to section 39.13 of the Federal Aviation Regulations (14 CFR 39.13). The AD is reprinted in its entirety for the convenience of affected operators. The effective date of the AD remains December 10, 1998. Since this action only corrects a typographical error, it has no adverse economic impact and imposes no additional burden on any person. Therefore, the FAA has determined that notice and public procedures are unnecessary. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Correction Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) by making the following correcting amendment: PART 39–AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Corrected] 2. Section 39.13 is amended by revising the following airworthiness directive (AD):
Document Text
Show stored source text (verify against official source)
AD Final Rules - 982419.pdf Copy URL Document Versions Feedback DetailsAttachments/Public Comments AD Number: 98-24-19 Document Type: AD Final Rules Docket Number: 98-NM-317-AD Subject Heading: [Correction] Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-14...Show more Subject: AFM - Performance & Limitations Section Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/10/1998 Make: Embraer S.A. Model: EMB-145 | EMB-145ER | EMB-145LR | EMB-145MR Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 [63 FR 65050 No. 227 11/25/98] Comments: CORRECTION: [Federal Register: February 18, 1999 (Volume 64, Number 32); Page 7993-7994; www.access....Show more Automatic Zoom Actual Size Page Fit Page Width 50% 75% 100% 125% 150% 200% 300% 400% 125% of 8 1 [Federal Register: February 18, 1999 (Volume 64, Number 32)] [Rules and Regulations] [Page 7993-7994] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr18fe99-3] ––––––––––––––––––––––––––––––––––– DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 98-NM-317-AD; Amendment 39-10904; AD 98-24-19] RIN 2120-AA64 Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB- 145 Series Airplanes AGENCY: Federal Aviation Administration, DOT. ACTION: Final rule; correcting amendment. ––––––––––––––––––––––––––––––––––– SUMMARY: This document corrects information in an existing airworthiness directive (AD) that applies to certain Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 series airplanes. That AD currently requires revising the Performance Section of the Airplane Flight Manual (AFM) to provide the flightcrew with procedures to adjust landing distances for landings performed with the anti-icing system active. That AD also requires revising the Limitations Section of the AFM to prohibit certain types of approaches with the anti-icing system active. This document corrects a typographical error that resulted in reference to a supplement of the AFM that does not exist. This correction is necessary to ensure that the appropriate supplement of the AFM is revised. DATES: Effective December 10, 1998. The incorporation by reference of certain publications listed in the regulations was approved previously by the Director of the Federal Register as of December 10, 1998 (63 FR 65050, November 25, 1998). FOR FURTHER INFORMATION CONTACT: Thomas Peters, Aerospace Engineer, ACE-118A, FAA, Small Airplane Directorate, Atlanta Aircraft Certification Office, One Crown Center, 1895 Phoenix Boulevard, suite 450, Atlanta, Georgia 30349; telephone (770) 703-6063; fax (770) 703- 6097. SUPPLEMENTARY INFORMATION: On November 16, 1998, the Federal Aviation Administration (FAA) issued AD 98-24-19, amendment 39-10904 (63 FR 65050, November 25, 1998), which applies to certain Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB- 145 series airplanes. That AD requires revising the Performance Section of the Airplane Flight Manual (AFM) to provide the flightcrew with procedures to adjust landing distances for landings performed with the anti-icing system active. That AD also requires revising the Limitations Sections 2 of the AFM to prohibit certain types of approaches with the anti-icing system active. That AD was prompted by a report that increased (i.e., higher than normal) flight idle thrust may occur when the anti-icing system is active. The actions required by that AD are intended to ensure that the flightcrew is advised of appropriate landing field lengths when operating with the anti-icing system active, and that instrument approaches at certain flap settings are prohibited with the anti-icing system active. Increased flight idle thrust when the anti-icing system is active, if not corrected, could result in landing overrun. Need for the Correction As published, AD 98-24-19 contains a typographical error in paragraph (a)(2) of the AD. That paragraph specified a revision to the Limitations Section of Supplement 12 of the FAA-approved AFM; however, the correct supplement is Supplement 6. Supplement 12 of the AFM does not exist. The FAA has determined that a correction to AD 98-24-19 is necessary. The correction will ensure that the appropriate supplement of the AFM is revised. Correction of Publication This document corrects the error and revises the AD as an amendment to section 39.13 of the Federal Aviation Regulations (14 CFR 39.13). The AD is reprinted in its entirety for the convenience of affected operators. The effective date of the AD remains December 10, 1998. Since this action only corrects a typographical error, it has no adverse economic impact and imposes no additional burden on any person. Therefore, the FAA has determined that notice and public procedures are unnecessary. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Correction Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) by making the following correcting amendment: PART 39–AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Corrected] 2. Section 39.13 is amended by revising the following airworthiness directive (AD):
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