PMA Supplement Test and Computations
MAULE M-7-260C · Parts Catalog
Overview
This document is a parts catalog for the Maule M-7-260C, detailing approved replacement parts and their eligibility for various aircraft models. It includes information on auxiliary fuel pumps and their specifications, as well as the approval basis for these parts.
- Includes approved replacement parts for Maule M-7-260C.
- Lists auxiliary fuel pumps with 14 Volt and 28 Volt specifications.
- Approval basis is per 14 CFR 21.303.
- Contains eligibility information for multiple aircraft models.
- Document is FAA-approved.
- Includes minor and major design change processes.
- Instructions for continued airworthiness are referenced.
- Supplemental ICA may be required for differences in replacement articles.
Document
Source
Originally published by mcfarlaneaviation.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Parts Catalog
- Year ·
- 2022
- File size ·
- 1.5 MB
- Publisher ·
- mcfarlaneaviation.com
- Language ·
- en
What is the PMA Supplement Test and Computations?
The PMA Supplement Test and Computations is a parts catalog for the MAULE M-7-260C, dated 2022.
Where does the PMA Supplement Test and Computations come from?
This copy of the PMA Supplement Test and Computations was originally published by mcfarlaneaviation.com and is hosted on Sprinkle as a free, searchable reference copy.
What year was the PMA Supplement Test and Computations published?
The PMA Supplement Test and Computations — the MAULE M-7-260C parts catalog on file — is dated 2022.
Most owners only have the POH. Here's the essential set for the MAULE M-7-260C.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Approved Replacement Parts
Lists various auxiliary fuel pumps with their article numbers and approved replacements.
Approval Basis
Details the approval basis for the parts as per 14 CFR 21.303.
Make/TCH Eligibility
Specifies the manufacturers and their respective aircraft models eligible for the parts.
General Notes
Outlines the process for design changes and instructions for continued airworthiness.
FAA Certification
Confirms the document is managed by the FAA's Central Certification Branch.
Full document text
FEDERAL AVIATION ADMINISTRATION – PARTS MANUFACTURER APPROVAL McFarlane Aviation, LLC 696 E. 1700 Rd PMA No. PQ3732CE Supplement No. Baldwin City, KS 66006 Date Page 1 of 10 Article Name Article Number Approved Replacement for Article Number Approval Basis and Approved Design Data Make/TCH Eligibility Model/Series Eligibility Aux. Fuel Pump 14 Volt 1184-00- 3CJ 1184-00-1, 1184-00-3 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Maule Aerospace Technology, Inc. M-4-180C, M-4-180V, M-4-220, M-5-180C, M-5-200, M-5-235C, M-6-180, M-6-235, M-7-235, M-7-235A, M-7-235B, M-7-235C, M-7-260, M-7-260C, MT-7-235, MT-7-260, MX-7-180, MX-7-180A, MX-7-180AC , MX-7-180B, MX-7-180C, MX-7-235, MXT-7-160, MXT-7-180, MXT-7-180A , M-8-235 Aux. Fuel Pump 28 Volt 1296-00- 1NVCJ 1296-00- 1NV, 1296- 00-1 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Textron Aviation Inc. F33A, F33C, V35, V35A, V35B, 36, A36 Page 2 of 10 Article Name Article Number Approved Replacement for Article Number Approval Basis and Approved Design Data Make/TCH Eligibility Model/Series Eligibility Aux. Fuel Pump 14 Volt 1471-00- 3CJ 1471-00-1, 1471-00-3 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Maule Aerospace Technology, Inc. M-4-220, M-5-180C, M-5-200, M-5-210TC, M-5-235C, M-6-180, M-6-235, M-7-235, M-7-235A, M-7-235B, M-7-235C, M-7-260, M-7-260C, M-7-420A, M-7-420AC, MT-7-235, MT-7-260, MX-7-180, MX-7-180A, MX-7-180AC , MX-7-180B, MX-7-180C, MX-7-235, MXT-7-160, MXT-7-180, MXT-7-180A , M-8-235, M-9-235 Aux. Fuel Pump 14 Volt 4140-00- 7NVCJ 4140-00-7, 4140-00-7NV Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Textron Aviation Inc. 35-C35, E33, F33 Page 3 of 10 Article Name Article Number Approved Replacement for Article Number Approval Basis and Approved Design Data Make/TCH Eligibility Model/Series Eligibility Aux. Fuel Pump 28 Volt 4140-00- 15CJ 4140-00-15, C291504- 0201 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Textron Aviation Inc. 172, 182, 182R, 188, 188A, 188B, 206, 207, 207A, 210, 210L, 210M, 210N, 310, 320, 337, 337A, 337B, 337C, 337D, 337E, 337F, 337G, 337H, 340, 340A, 401, 401A, 401B, 402, 402A, 402B, 411, 411A, 414, 421, 421A, 421B, A185F, A188, A188A, A188B, F337E, F337F, F337G, F337H, FR172K, FT337E, FT337F, FT337GP, FT337HP, P210N, P337H, R172E, R172F, R172G , R172K, R182, T207, T207A, T210L, T210M, T210N, T337B, T337C, T337D, Page 4 of 10 Article Name Article Number Approved Replacement for Article Number Approval Basis and Approved Design Data Make/TCH Eligibility Model/Series Eligibility Aux. Fuel Pump 28 Volt 1296-00- 1NVCJ 1296-00- 1NV, 1296- 00-1 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Textron Aviation Inc. T337E, T337F, T337G, T337H, TR182, TU206G, U206G Aux. Fuel Pump 14 Volt 4140-00- 17CJ 4140-00-17, C291504- 0101 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Textron Aviation Inc. 172, 177RG, 182, 182R, 185A, 185B, 185C, 185D, 185E, 188, 188A, 188B, 206, 207, 207A, 210, 210-5 (205), 210D, 210E, 210F, 210G, 210H, 210J, 210K, A185E, A185F, A188, A188A, A188B, F177RG, FR172E, FR172F, FR172G, FR172H, FR172J, FR172K, P206, P206A, P206B, P206C, P206D, P206E, R172H, R172K, T207, T207A, T210F, T210G, T210H, T210J, T210K, Page 5 of 10 Article Name Article Number Approved Replacement for Article Number Approval Basis and Approved Design Data Make/TCH Eligibility Model/Series Eligibility Aux. Fuel Pump 14 Volt 4140-00- 17CJ 4140-00-17, C291504- 0101 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Textron Aviation Inc. TP206A, TP206B, TP206C, TP206D, TP206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G Aux. Fuel Pump 14 Volt 4140-00- 17NCJ 4140-00-17N Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Sierra Hotel Aero, Inc. Navion H Aux. Fuel Pump 14 Volt 4140-00- 19ACJ 4140-00-19A, 610153-501 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Mooney Aircraft Corporation M20E, M20F, M20J, M20K Aux. Fuel Pump 14 Volt 4140-00- 19ACJ 4140-00-19A Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Revo, Incorporate d LA-4-200 Aux. Fuel Pump 14 Volt 4140-00- 21ACJ 4140-00-21A, 610153-000, 610153 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Mooney Aircraft Corporation M20C, M20D, M20E, M20G Page 6 of 10 Article Name Article Number Approved Replacement for Article Number Approval Basis and Approved Design Data Make/TCH Eligibility Model/Series Eligibility Aux. Fuel Pump 14 Volt 4140-00- 39NVCJ 4140-00- 39NV, 4140-00-39 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Textron Aviation Inc. S35, V35, V35A, V35B, 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33A, E33C, 36, A36, F33A, F33C, G33 Aux. Fuel Pump 14 Volt 4140-00- 57CJ 4140-00-57 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Maule Aerospace Technology, Inc. M-4-220C, M-5-220C Aux. Fuel Pump 28 Volt 4140-00- 153CJ 4140-00-153 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Textron Aviation Inc. 310L, 310N, 310P, T310P, 310Q, T310Q, 310R, T310R, 320E, 340, 340A, 401, 401A, 401B, 402, 402A, 402B, 411, 411A, 414, 421, 421A, 421B Aux. Fuel Pump 14 Volt 4140-00- 218CJ 4140-00-218 Test and Computations per 14 CFR 21.303
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DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Piper Aircraft, Inc. PA-24-250, PA-24-260 Page 7 of 10 Article Name Article Number Approved Replacement for Article Number Approval Basis and Approved Design Data Make/TCH Eligibility Model/Series Eligibility Aux. Aux. Fuel Pump 28 Volt 4140-00- 400CJ 4140-00-400 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Maule Aerospace Technology, Inc. M-4-220, M-5-180C, M-5-200, M-5-220, M-5-220TC, M-5-235C, M-6-180, M-6-235, M-7-235, M-7-235A, M-7-235B, M-7-235C, M-7-260, M-7-260C, MT-7-235, MT-7-260, MX-7-180, MX-7-180A, MX-7-180B, MX-7-180C, MX-7-180AC , MX-7-235, MXT-7-160, MXT-7-180, MXT-7-180A , M-8-235 Page 8 of 10 Article Name Article Number Approved Replacement for Article Number Approval Basis and Approved Design Data Make/TCH Eligibility Model/Series Eligibility Aux. Fuel Pump 28 Volt 4140-00- 401CJ 4140-00-401 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Maule Aerospace Technology M-4-220, M-4-180V, M-5-180C, M-5-200, M-5-220C, M-5-235C, M-6-180, M-6-235, M-7-235, M-7-235A, M-7-235B, M-7-235C, M-7-260, M-7-260C, MT-7-235, MT-7-260, MX-7-160, MX-7-160C, MX-7-180, MX-7-180A, MX-7-180B, MX-7-180C, MX-7-180AC , MX-7-235, MXT-7-160, MXT-7-180, M-8-235, M-9-235 Aux. Fuel Pump 28 Volt 4150-00- 1NVCJ 96-380020-1, 4150-00-1 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revisions Textron Aviation Inc. 95-A55, 95-B55, 95-B55A, 95-B55B (Navy T-42), 95-C55, D55, D55A, E55, E55A Aux. Fuel Pump 14 Volt 4258-00- 15NVCJ 4258-00- 15NV, 4258-00-15 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revisions Textron Aviation Inc. 36, A36 Page 9 of 10 Article Name Article Number Approved Replacement for Article Number Approval Basis and Approved Design Data Make/TCH Eligibility Model/Series Eligibility Aux. Fuel Pump 28 Volt 4404-00- 7NVCJ 4404-00-7NV Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Textron Aviation Inc. 95-B55, P35, E55, E55A, 58, 58A, G58, 95-B55, 95-B55A Aux. Fuel Pump 28 Volt 4613-00- 3NVCJ 4613-00-3, 4613-00-3NV Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Textron Aviation Inc. 36, A36, G36 Aux. Fuel Pump 28 Volt 4613-00- 5NVCJ 4613-00-5, 4613-00-5NV Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Textron Aviation Inc. 36, A36, G36 Aux. Fuel Pump 28 Volt 5100-00- 4CJ 5100-00-1, 5100-00-3, 5100-00-4 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Textron Aviation Inc. 172, 172R, 172S, 182S Aux. Fuel Pump 28 Volt 5100-00- 9CJ 5100-00-9 Test and Computations per 14 CFR 21.303 DWG No: 1384 Rev: C Date: 9/24/2024 or later FAA-approved revision Diamond Aircraft Industries Inc DA40, DA40F, DA42 --------------------End of Listing-------------------- GENERAL NOTES: Provide minor design changes in a manner as determined by the cognizant FAA certification branch. Process major design changes to drawings and specifications in the same manner as that for an original FAA PMA. The FAA accepted the instructions for continued airworthiness (ICA) approach for the above articles with their designs. These ICA may refer to those of the respective articles from the holders of type certificates. Otherwise, provide supplemental ICA for differences in the replacement articles. Make referral statements or supplemental ICA readily available per 14 CFR 21.50. FEDERAL AVIATION ADMINISTRATION – PARTS MANUFACTURER APPROVAL McFarlane Aviation, LLC 696 E. 1700 Rd PMA No. PQ3732CE Supplement No. Baldwin City, KS 66006 Date Page 10 of 10 Article Name Article Number Approved Replacement for Article Number Approval Basis and Approved Design Data Make/TCH Eligibility Model/Series Eligibility Paul Nguyen Manager, Central Certification Branch Compliance and Airworthiness Division Aircraft Certification Service Neal Rice Manager, Wichita Certificate Management Section Central Certificate Management Branch System Oversight Division Aircraft Certification Service