AD 2007-03-05 Airworthiness Directives; Gulfstream Aerospace LP Model Gulfstream 100 Airplanes, and Model Astra SPX and 1125 Westwind Astra Airplanes

Models named: Gulfstream 100, Astra SPX, 1125 Westwind Astra. Read the applicability below — it usually turns on serial or part numbers too.

This AD applies to Gulfstream Model Gulfstream 100 airplanes; and Model Astra SPX and 1125 Westwind Astra airplanes; certificated in any category; all serial numbers. Reason (d) The unsafe condition is incomplete closure of the main entry door, which may result in the door opening in flight, causing damage to wing, fuselage, engine, and/or tail, and possible damage to the airplane. The mandatory continuing airworthiness information (MCAI) requires amending the airplane flight manuals to include additional procedures for verifying complete closure and locking of the main entry door.

Unless already done, do the following actions. Within 10 days after the effective date of this AD, amend section IV, Normal Procedures, of the following Gulfstream airplane flight manuals (AFMs): Model 1125 Astra, 25W-1001-1; Model Astra SPX, SPX-1001-1; and Model G100, G100-1001-1; as applicable; to include the following statement. Insertion of copies of this AD at the appropriate places of the AFMs is acceptable. “1. BEFORE ENGINE START: (PRE and POST Mod 20052/Gulfstream Service Bulletin 100-31-284): CABIN DOOR—CLOSED (Physically verify door latch handle pin is fully engaged in the handle lock). 2. BEFORE TAXIING: Change the CABIN DOOR procedure as follows (POST Mod 20052/Gulfstream Service Bulletin 100-31-284): Check CABIN DOOR light—OUT. 3. BEFORE TAKE-OFF: Insert between the POSITION lights switch and the THRUST LEVERS procedures: (PRE Mod 20052/Gulfstream Service Bulletin 100-31-284): Check CABIN DOOR light—OUT (50% N1 may be required). (POST Mod 20052/Gulfstream Service Bulletin 100-31-284): Check CABIN DOOR light—OUT; CABIN DOOR SEAL light—OUT (50% N1 may be required).” Note 1: Mod 20052 is equivalent to Gulfstream Service Bulletin 100-31-284, dated August 17, 2006. Note 2: This AD may be accomplished by a holder of a Private Pilot's License. FAA AD Differences Note 3: This AD differs from the MCAI and/or service information as follows: We revised the order in which the AFM procedures for verifying closure and locking of the main entry door appear in the MCAI. We also removed one procedure under “BEFORE TAXIING” for verifying the cabin door seal light is out (Post Mod 20052/Post Gulfstream Service Bulletin 100-31-284) and for verifying the cabin door light is out (Pre Mod 20052/Pre Gulfstream Service Bulletin 100-31-284). Other FAA AD Provisions (f) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, Attn: Mike Borfitz, Aerospace Engineer, 1601 Lind Avenue, SW., Renton, Washington 98057-3356, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Before using any AMOC approved in accordance with § 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (g) Refer to MCAI Israeli Airworthiness Directive 52-06-11-08, dated November 28, 2006, for related information. Material Incorporated by Reference (h) None. Issued in Renton, Washington, on January 23, 2007. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-1397 Filed 1-30-07; 8:45 am] BILLING CODE 4910-13-P

Unless already done, do the following actions. Within 10 days after the effective date of this AD, amend section IV, Normal Procedures, of the following Gulfstream airplane flight manuals (AFMs): Model 1125 Astra, 25W-1001-1; Model Astra SPX, SPX-1001-1; and Model G100, G100-1001-1; as applicable; to include the following statement. Insertion of copies of this AD at the appropriate places of the AFMs is acceptable. “1. BEFORE ENGINE START: (PRE and POST Mod 20052/Gulfstream Service Bulletin 100-31-284): CABIN DOOR—CLOSED (Physically verify door latch handle pin is fully engaged in the handle lock). 2. BEFORE TAXIING: Change the CABIN DOOR procedure as follows (POST Mod 20052/Gulfstream Service Bulletin 100-31-284): Check CABIN DOOR light—OUT. 3. BEFORE TAKE-OFF: Insert between the POSITION lights switch and the THRUST LEVERS procedures: (PRE Mod 20052/Gulfstream Service Bulletin 100-31-284): Check CABIN DOOR light—OUT (50% N1 may be required). (POST Mod 20052/Gulfstream Service Bulletin 100-31-284): Check CABIN DOOR light—OUT; CABIN DOOR SEAL light—OUT (50% N1 may be required).” Note 1: Mod 20052 is equivalent to Gulfstream Service Bulletin 100-31-284, dated August 17, 2006. Note 2: This AD may be accomplished by a holder of a Private Pilot's License. FAA AD Differences Note 3: This AD differs from the MCAI and/or service information as follows: We revised the order in which the AFM procedures for verifying closure and locking of the main entry door appear in the MCAI. We also removed one procedure under “BEFORE TAXIING” for verifying the cabin door seal light is out (Post Mod 20052/Post Gulfstream Service Bulletin 100-31-284) and for verifying the cabin door light is out (Pre Mod 20052/Pre Gulfstream Service Bulletin 100-31-284). Other FAA AD Provisions (f) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, Attn: Mike Borfitz, Aerospace Engineer, 1601 Lind Avenue, SW., Renton, Washington 98057-3356, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Before using any AMOC approved in accordance with § 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (g) Refer to MCAI Israeli Airworthiness Directive 52-06-11-08, dated November 28, 2006, for related information. Material Incorporated by Reference (h) None. Issued in Renton, Washington, on January 23, 2007. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-1397 Filed 1-30-07; 8:45 am] BILLING CODE 4910-13-P