737NG飞机翼梢小翼STC
Number ST00830SE This certificate, issued to: Aviation Partners Boeing 2811 South 102nd Street, Suite 200 Seattle, WA 98168 certifies that the change in the type design for the following product with the limitations and conditions therefore as specified hereon meets the airworthiness requirements of Part 25 of the Federal Aviation Regulations. Original Product¾Type Certificate Number: A16WE Make: Boeing Model: 737-700, 737-700C, 737-800, 737-900 Description of the Type Design Change: Installation of winglets, wing structural reinforcement and related system changes on Boeing Model 737-700, 737-700C, 737-800, and 737-900 series airplanes. Fabrication and installation of parts must be accomplished in accordance with the FAA-approved Aviation Partners Boeing Master Drawing Lists as listed in the following attached Approved Model List (AML) documents (revision levels as stated or later FAA-approved revisions): Model | Description | Approved Model List (AML) document # | 737-700 | Winglet or Partial Wing Retrofit Installation | AP37.7-AML0830, Rev. IR, dated October 10, 2007, or later FAA-approved revision. | 737-700C | Winglet or Partial Wing Retrofit Installation | AP37.7C-AML0830, Rev. A, dated March 18, 2010, or later FAA-approved revision. | 737-800 | Winglet or Partial Wing Retrofit Installation | AP37.8-AML0830, Rev IR, dated October 10, 2007, or later FAA-approved revision. | 737-900 | Winglet or Partial Wing Retrofit Installation | AP37.9-AML0830, Rev. IR, dated October 10, 2007, or later FAA-approved revision. |
Limitations and Conditions: The limitations and conditions of Type Certificate A16WE apply except as outlined on Pages 3 through 4 of this STC. A copy of this certificate must be included in the permanent records of each airplane modified in accordance with this STC. Approval of this change in type design applies to the Boeing Model 737-700, 737-700C, 737- 800, and 737-900 series airplanes that are otherwise unmodified (unless identified as a previously determined compatible STC). This approval should not be extended to other airplanes of these models unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of the airplane. (Limitations and Conditions continued on Page 3 of 4) This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of application: | January 14, 1998 | Date reissued: December 23, 2009 | Date of issuance: | September 5, 2000 | Date amended: 12/7/2000; 3/23/2001; 7/6/2001; |
8/27/2001; 12/12/2001; 1/31/2002; 2/19/2004; 5/7/2004; 7/30/2004; 10/10/2006; 10/10/2007; 3/19/2010 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2(10-68) This certificate may be transferred in accordance with FAR 21.47.
s&j'd Um o/t"If'e mætJ .toF (SignaJu) Actina Manaaer. Seattle Aircraft Certification Office (Title) A ny alteration of this certificate is punishable bya fine of not e ceeding $1000or imprisonmenf not exceeding 3 y or both FAA FORM 8110-2(10-68) This certifica te may be trans9rred in accordance with FAR 21.47
Limitations and Conditions (continued): Airspeed Limits: | See Type Certificate Data Sheet A16WE. | C.G. Range: | See Type Certificate Data Sheet A16WE. | Maximum Weights: | See Type Certificate Data Sheet A16WE. | Eligible S / N’s: | Refer to the applicable Aviation Partners Boeing Approved Model List (AML) document referenced above for the applicable Eligible Airplane Serial Number document. | Operational Requirements: | This engineering approval of a changed type certificate limitation does not permit a change in operating rule applicability to the operator of the changed aircraft. An applicant for an operating rule applicability change must obtain any change in operating rule applicability through consultation with their responsible certificate management office (CMO). Airplane operation must be in accordance with the applicable Aviation Partners Boeing Airplane Flight Manual (AFM) Supplement, Configuration Deviation List (CDL) Supplement, and Weight and Balance Manual Supplement listed in the applicable Approved Model List (AML) document referenced above. |
This modification may not be installed after August 30, 2010 unless (1) previously approved electrical wiring interconnection system (EWIS) instructions for continued airworthiness (ICA) have been evaluated and determined to be adequate for this installation by the FAA, or (2) revised EWIS ICA have been approved by the FAA Oversigned Office (Refer to § 26.11) The 737-700C with PATS Auxiliary Fuel Tank installations are life limited to 60 months, 5000 cycles or 7000 hours after the blended winglets retrofit kit installation, whichever comes first. PAGE 3 of 4
Certification Basis: Refer to the applicable Aviation Partners Boeing Approved Model List (AML) document referenced above Equivalent Safety Findings: | Refer to the applicable Aviation Partners Boeing Approved Model List (AML) document referenced above. | Exemptions: | See Type Certificate Data Sheet A16WE | Certification Maintenance Requirements and Airworthiness Limitations: | Airplane maintenance must be in accordance with the applicable Aviation Partners Boeing Maintenance Planning Document (MPD) Supplement Certification Maintenance Requirements and Airworthiness Limitations documents listed in the applicable Approved Model List (AML) document referenced above. | Required Equipment: | See Type Certificate Data Sheet A16WE | Service Information: | Refer to the applicable Aviation Partners Boeing Approved Model List (AML) document referenced above for the applicable Structural Repair Manual Supplement, Airplane Maintenance Manual Supplement, Maintenance Planning Data Document, and Fault Isolation Manual Supplement documents. | Previously Determined Compatible SupplementalType Certificates (STC) | Refer to the applicable Aviation Partners Boeing Approved Model List (AML) document referenced above for notes identifying certain STC’s that have already been determined to be compatible with this STC. |
If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. - END - PAGE 4 of 4 | 
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