AD 98-20-38 R1
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 200 | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | 200C | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | 200CT | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | 200T | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | A100-1 (U-21J) | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | A200 (C-12A) | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | A200 (C-12C) | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | A200C (UC-12B) | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | A200CT (C-12D) | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | A200CT (C-12F) | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | A200CT (FWC-12D) | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | A200CT (RC-12D) | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | A200CT (RC-12G) | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | A200CT (RC-12H) | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | A200CT (RC-12K) | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | A200CT (RC-12P) | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | B200CT | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
| aircraft | Textron Aviation Inc. | B200T | Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes |
Unsafe Condition
Operating in severe icing conditions without specified AFM procedures could lead to hazardous flight control device malfunctions or crew inability to exit icing conditions.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise the FAA-approved Airplane Flight Manual to prohibit flight in severe icing conditions based on visual cues, limit or prohibit use of flight control devices in such conditions, and provide crew recognition cues and exit procedures. Remove Models B200 and B200C from applicability of AD 98-20-38 and clarify AD 96-09-13 applies to them.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
before further flight
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Affected Aircraft
Raytheon Aircraft Company Beech 200 series airplanes excluding Models B200 and B200C, affected by AD 96-09-13 for those models.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Airplane Flight Manual (AFM)
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - 98-20-38R1.pdf Copy URL Document Versions Feedback DetailsAttachments/Public Comments AD Number: 98-20-38 R1 Document Type: AD Final Rules Docket Number: FAA-2004-19078 Subject Heading: Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes Subject: Airplane Flight Manual (AFM) Status: Current Citation: Federal Register: January 19, 2005 (Volume 70, Number 12) Citation Publish Date: 01/19/2005 Effective Date: 02/18/2005 Make: Textron Aviation Inc. Model: 200 | 200C | 200CT | 200T | A100-1 (U-21J) | A200 (C-12A) | A200 (C-12C) | A200C (UC-12B) ...Show more Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: 98-20-38 Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Automatic Zoom Actual Size Page Fit Page Width 50% 75% 100% 125% 150% 200% 300% 400% 125% of 7 1 [Federal Register: January 19, 2005 (Volume 70, Number 12)] [Rules and Regulations] [Page 2934-2936] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr19ja05-2] ––––––––––––––––––––––––––––––––––– DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-19078; Directorate Identifier 98-CE-17-AD; Amendment 39-13946; AD 98-20-38 R1] RIN 2120-AA64 Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. ––––––––––––––––––––––––––––––––––– SUMMARY: The FAA adopts a new airworthiness directive (AD) to revise AD 98-20-38, which applies to all Beech 200 series airplanes. AD 98-20-38 requires you to revise the FAA-approved Airplane Flight Manual (AFM) to specify procedures that would prohibit flight in severe icing conditions (as determined by certain visual cues), limit or prohibit the use of various flight control devices while in severe icing conditions, and provide the flight crew with recognition cues for and procedures for exiting from severe icing conditions. Part of the applicability of AD 98-20-38 includes the Raytheon Models B200 and B200C airplanes. AD 96-09-13 already requires AFM revisions on this subject for these airplane models. Consequently, FAA is revising AD 98-20-38 to remove the Models B200 and B200C from the applicability and add clarification that AD 96-09-13 affects these airplanes. We are issuing this AD to minimize the potential hazards associated with operating these airplanes in severe icing conditions by providing more clearly defined procedures and limitations. DATES: This AD becomes effective on February 18, 2005. ADDRESSES: To view the AD docket, go to the Docket Management Facility; U.S. Department of Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401, Washington, DC 20590- 0001 or on the Internet at http://dms.dot.gov . The docket number is FAA-2004-19078; Directorate Identifier 98-CE-17-AD. FOR FURTHER INFORMATION CONTACT: Mr. Paul Pellicano, Aerospace Engineer (Icing Specialist), Atlanta Aircraft Certification Office, FAA, One Crown Center, 1895 Phoenix Boulevard, Suite 450, Atlanta, Georgia 30349; telephone: (770) 703-6064; facsimile: (770) 703-6097. 2 SUPPLEMENTARY INFORMATION: Discussion Has FAA taken any action to this point? A review of the requirements for certification of Raytheon Beech 200 series airplanes in icing conditions caused FAA to issue AD 98-20-38, Amendment 39-10806 (63 FR 51805, September 29, 1998). AD 98-20-38 requires you to revise the FAA-approved Airplane Flight Manual (AFM) to specify procedures that would prohibit flight in severe icing conditions (as determined by certain visual cues), limit or prohibit the use of various flight control devices while in severe icing conditions, and provide the flight crew with recognition cues for and procedures for exiting from severe icing conditions. What has happened since AD 98-20-38 to initiate this proposed action? Part of the applicability of AD 98-20-38 includes the Raytheon Models B200 and B200C airplanes. AD 96-09-13 already requires AFM revisions on this subject for these airplane models. The language is similar but is not the same and AD 96-09-13 reflects the preferred information. Consequently, FAA is revising AD 98- 20-38 to remove the Models B200 and B200C from the applicability and add clarification that AD 96-09-13 affects these airplanes. Has FAA taken any action to this point? We issued a proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an AD that would apply to Raytheon Beech 200 series airplanes. This proposal was published in the Federal Register as a notice of proposed rulemaking (NPRM) on October 22, 2004 (69 FR 62005). The NPRM proposed to revise AD 98-20- 38 to remove the Beech Models B200 and B200C from the applicability. The Beech Models B200 and B200C are still affected by the actions of AD 96-09-13. Comments Was the public invited to comment? We provided the public the opportunity to participate in developing this AD. We received no comments on the proposal or on the determination of the cost to the public. Conclusion What is FAA's final determination on this issue? We have carefully reviewed the available data and determined that air safety and the public interest require adopting the AD as proposed except for minor editorial corrections. We have determined that these minor corrections: Are consistent with the intent that was proposed in the NPRM for correcting the unsafe condition; and Do not add any additional burden upon the public than was already proposed in the NPRM. Changes to 14 CFR Part 39–Effect on the AD How does the revision to 14 CFR part 39 affect this AD? On July 10, 2002, the FAA published a new version of 14 CFR part 39 (67 FR 47997, July 22, 2002), which governs the FAA's AD system. This regulation now includes material that relates to altered products, special flight permits, and alternative methods of compliance. This material previously was included in each individual AD. Since this material is included in 14 CFR part 39, we will not include it in future AD actions. Costs of Compliance How many airplanes does this AD impact? We estimate that this AD affects 1,600 airplanes in the U.S. registry.
Document Text
Show stored source text (verify against official source)
AD Final Rules - 98-20-38R1.pdf Copy URL Document Versions Feedback DetailsAttachments/Public Comments AD Number: 98-20-38 R1 Document Type: AD Final Rules Docket Number: FAA-2004-19078 Subject Heading: Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes Subject: Airplane Flight Manual (AFM) Status: Current Citation: Federal Register: January 19, 2005 (Volume 70, Number 12) Citation Publish Date: 01/19/2005 Effective Date: 02/18/2005 Make: Textron Aviation Inc. Model: 200 | 200C | 200CT | 200T | A100-1 (U-21J) | A200 (C-12A) | A200 (C-12C) | A200C (UC-12B) ...Show more Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: 98-20-38 Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Automatic Zoom Actual Size Page Fit Page Width 50% 75% 100% 125% 150% 200% 300% 400% 125% of 7 1 [Federal Register: January 19, 2005 (Volume 70, Number 12)] [Rules and Regulations] [Page 2934-2936] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr19ja05-2] ––––––––––––––––––––––––––––––––––– DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-19078; Directorate Identifier 98-CE-17-AD; Amendment 39-13946; AD 98-20-38 R1] RIN 2120-AA64 Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200 Series Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. ––––––––––––––––––––––––––––––––––– SUMMARY: The FAA adopts a new airworthiness directive (AD) to revise AD 98-20-38, which applies to all Beech 200 series airplanes. AD 98-20-38 requires you to revise the FAA-approved Airplane Flight Manual (AFM) to specify procedures that would prohibit flight in severe icing conditions (as determined by certain visual cues), limit or prohibit the use of various flight control devices while in severe icing conditions, and provide the flight crew with recognition cues for and procedures for exiting from severe icing conditions. Part of the applicability of AD 98-20-38 includes the Raytheon Models B200 and B200C airplanes. AD 96-09-13 already requires AFM revisions on this subject for these airplane models. Consequently, FAA is revising AD 98-20-38 to remove the Models B200 and B200C from the applicability and add clarification that AD 96-09-13 affects these airplanes. We are issuing this AD to minimize the potential hazards associated with operating these airplanes in severe icing conditions by providing more clearly defined procedures and limitations. DATES: This AD becomes effective on February 18, 2005. ADDRESSES: To view the AD docket, go to the Docket Management Facility; U.S. Department of Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401, Washington, DC 20590- 0001 or on the Internet at http://dms.dot.gov . The docket number is FAA-2004-19078; Directorate Identifier 98-CE-17-AD. FOR FURTHER INFORMATION CONTACT: Mr. Paul Pellicano, Aerospace Engineer (Icing Specialist), Atlanta Aircraft Certification Office, FAA, One Crown Center, 1895 Phoenix Boulevard, Suite 450, Atlanta, Georgia 30349; telephone: (770) 703-6064; facsimile: (770) 703-6097. 2 SUPPLEMENTARY INFORMATION: Discussion Has FAA taken any action to this point? A review of the requirements for certification of Raytheon Beech 200 series airplanes in icing conditions caused FAA to issue AD 98-20-38, Amendment 39-10806 (63 FR 51805, September 29, 1998). AD 98-20-38 requires you to revise the FAA-approved Airplane Flight Manual (AFM) to specify procedures that would prohibit flight in severe icing conditions (as determined by certain visual cues), limit or prohibit the use of various flight control devices while in severe icing conditions, and provide the flight crew with recognition cues for and procedures for exiting from severe icing conditions. What has happened since AD 98-20-38 to initiate this proposed action? Part of the applicability of AD 98-20-38 includes the Raytheon Models B200 and B200C airplanes. AD 96-09-13 already requires AFM revisions on this subject for these airplane models. The language is similar but is not the same and AD 96-09-13 reflects the preferred information. Consequently, FAA is revising AD 98- 20-38 to remove the Models B200 and B200C from the applicability and add clarification that AD 96-09-13 affects these airplanes. Has FAA taken any action to this point? We issued a proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an AD that would apply to Raytheon Beech 200 series airplanes. This proposal was published in the Federal Register as a notice of proposed rulemaking (NPRM) on October 22, 2004 (69 FR 62005). The NPRM proposed to revise AD 98-20- 38 to remove the Beech Models B200 and B200C from the applicability. The Beech Models B200 and B200C are still affected by the actions of AD 96-09-13. Comments Was the public invited to comment? We provided the public the opportunity to participate in developing this AD. We received no comments on the proposal or on the determination of the cost to the public. Conclusion What is FAA's final determination on this issue? We have carefully reviewed the available data and determined that air safety and the public interest require adopting the AD as proposed except for minor editorial corrections. We have determined that these minor corrections: Are consistent with the intent that was proposed in the NPRM for correcting the unsafe condition; and Do not add any additional burden upon the public than was already proposed in the NPRM. Changes to 14 CFR Part 39–Effect on the AD How does the revision to 14 CFR part 39 affect this AD? On July 10, 2002, the FAA published a new version of 14 CFR part 39 (67 FR 47997, July 22, 2002), which governs the FAA's AD system. This regulation now includes material that relates to altered products, special flight permits, and alternative methods of compliance. This material previously was included in each individual AD. Since this material is included in 14 CFR part 39, we will not include it in future AD actions. Costs of Compliance How many airplanes does this AD impact? We estimate that this AD affects 1,600 airplanes in the U.S. registry.
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