# STC SA01380CH

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Storehouse LLC, United States
- Description: Installation of wing fuel tank quick valve drains.
- Applied: December 7, 2000
- Status date: April 30, 2014
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21, Part 23
- Data sheets: [TCDS 5A6](https://openairdocs.org/tcds/5A6), [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS A9CE](https://openairdocs.org/tcds/A9CE), [TCDS A4CE](https://openairdocs.org/tcds/A4CE), [TCDS A16CE](https://openairdocs.org/tcds/A16CE), [TCDS 3A21](https://openairdocs.org/tcds/3A21), [TCDS A42EU](https://openairdocs.org/tcds/A42EU)
- Certificate PDF: https://openairdocs.org/files/sha256/e5/87/e587d72f6c774315b5c121541e8d8631063b039cc991f74f76d519fb7706c1a4
- Approved model list and other attachments: [SA01380CH_AML .pdf](https://openairdocs.org/files/sha256/8a/94/8a94fd7f87332e592c2aecca4a391b15acb7350e685c88c67a4ce30588751169)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EB36FB9CEFB3A55B86257CCC004BE48C.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01380CH

## ADs that name it (0)

None.

## Approved models (87, first 50)

- Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180A ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180B ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180C ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180D ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180E ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180F ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180G ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180H ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180J ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180K ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182A ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182B ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182C ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182D ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182N ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182P ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182Q ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 185 ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185A ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185B ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185C ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185D ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 188 ([TCDS A9CE](https://openairdocs.org/tcds/A9CE))
- Cessna Aircraft Company 188A ([TCDS A9CE](https://openairdocs.org/tcds/A9CE))
- Cessna Aircraft Company 188B ([TCDS A9CE](https://openairdocs.org/tcds/A9CE))
- Cessna Aircraft Company 206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company 207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company 207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company 210 ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210-5 (205) ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210-5A (205A) ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210A ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210B ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210C ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210D ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210E ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210F ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company A185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company A185F ([TCDS 3A24](https://openairdocs.org/tcds/3A24))

All 87: https://openairdocs.org/stc/SA01380CH/models.md

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Installation of wing fuel cell drain valves in accordance with applicable installation instructions called out in Eagle Techn ologies Company Drawing List No. 70DLC, dated October 3, 2000 as listed on AML No. SA01380CH or later FAA approved revisions, or in accordance with Storehouse LLC applicable installation instructions 710C, 710CM, 720C, 720CM, 730C or 730CM, dated January 25, 2014 as listed on AML No. SA01380CH, or later FAA approved revisions.

1. Compatibility of this design change with previously approved modifications must be determined by the installer.

2. A copy of this Certificate and AML No. SA01380CH, dated January 25, 2001, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft.

3. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other p erson written evidence of that permission.

Storehouse LLC 914 Meta Lake Road Eagle River, WI 54521 * See Attached FAA Approved Model List (AML) No. SA01380CH for list of approved airplane models and applicable airworthiness regulations.

* * December 7, 2000

January 25, 2001

January 24, 2014; April 30, 2014

Original Signed By:

Christopher Richards

(Signature) Timothy P. Smyth Manager, Propulsion & Program Management Branch Chicago Aircraft Certification Office

(Title)

FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES

### SA01380CH_AML .pdf

FAA Approved Model List (AML) for STC # SA01380CH Page 1 of 2 Storehouse LLC Issue date: April 9, 2014

Fuel drain valve kits for Cessna Aircraft

Item Aircraft Make Aircraft Model Serial Number Applicability Original Type Certification basis Installation Instructions AFM Supplement AML Amendment Certificate # for alteration Revision # & Date Number & Date Date 1 Cessna Aircraft Company 180 604, 614, 30000 through 32661 5A6 CAR Part3 710C Rev. M 01/27/14 or None April 9, 2014 2 180A 32662 through 32999 710CM Rev. M 01/27/14 or 50001 through 50355 720C Rev. M 01/27/14 or 3 180B 50356 through 50661 720CM Rev. M 01/27/14 or 4 180C 624, 50662 through 50911 730C Rev. M 01/27/14 or 5 180D 18050912 through 18051063 730CM Rev. M 01/27/14 or 6 180E 18051064 through 18051183 later FAA approved revision 7 180F 18051184 through 18051312 8 180G 18051313 through 18051445 9 180H 18051446 through 18052284 10 180J 18052285 through 18052770 (except 18052490) 11 180K 18052771 through 18053000 18053168 through 18053203 (only aircraft with optional wing fuel cells installed)

12 Cessna Aircraft Company 182 613, 33000 through 33842 3A13 CAR Part3 710C Rev. M 01/27/14 or None April 9, 2014 13 182A 33843 through 34999 (except 34754) 710CM Rev. M 01/27/14 or 51001 through 51556 720C Rev. M 01/27/14 or 14 182B 34754, 51557 through 52358 (except 51623) 720CM Rev. M 01/27/14 or 15 182C 631, 52359 through 53007 730C Rev. M 01/27/14 or 16 182D 51623, 18253008 through 18253598 730CM Rev. M 01/27/14 or 17 182E 18253599 through 18254423 later FAA approved revision 18 182F 18254424 through 18255058 19 182G 18255059 through 18255844 20 182H 18255846 through 18256684 21 182J 18256685 through 18257625 22 182K 18255845, 18257626 through 18258505 (except 18257699) 23 182L 18258506 through 18259305 24 182M 18257699, 18259306 through 18260055 25 182N 18260056 through 18260825 26 182P 675, 18260826 through 18265175 (except 18263479) 27 182Q 18263479, 18265176 through 18266590 28 A182J A182-0001 through A182-0056 29 A182K A182-0057 through A182-0096 30 A182L A182-0097 through A182-0116 31 A182N A182-0117 through A182-0148 32 R182 R18200002 through R18200583 33 Cessna Aircraft Company F182P F18200001 through F18200025 A42EU FAR Part 21 & 23 710C Rev. M 01/27/14 or None. April 9, 2014 34 F182Q F18200026 through F18200169 710CM Rev. M 01/27/14 or 35 FR182 FR18200001 through FR18200070 720C Rev. M 01/27/14 or 720CM Rev. M 01/27/14 or 730C Rev. M 01/27/14 or 730CM Rev. M 01/27/14 or later FAA approved revision 36 Cessna Aircraft Company 188 / A188 188-0446 through 188-0572 * A9CE FAR Part 21 & 23 710C Rev. M 01/27/14 or None. April 9, 2014 37 188A / A188A 18800573 through 18800832 * 710CM Rev. M 01/27/14 or 38 188B 18800833 through 18802348 * 720C Rev. M 01/27/14 or 39 A188B 678T, 18800833 through 18803973 * 720CM Rev. M 01/27/14 or 40 T188C T18802839, T18803307T, T18803308T * 730C Rev. M 01/27/14 or T18803325T through T18803974T * 730CM Rev. M 01/27/14 or (* only aircraft with optional wing fuel cells installed) later FAA approved revision

FAA Approved Model List (AML) for STC # SA01380CH Page 2 of 2 Storehouse LLC Issue date: April 9, 2014 , Fuel drain valve kits for Cessna Aircraft

Item Aircraft Make Aircraft Model Serial Number Applicability Original Type Certification basis Installation Instructions AFM Supplement AML Amendment Certificate # for alteration Revision # & Date Number & Date Date 41 Cessna Aircraft Company 185 185-0001 through 185-0237 3A24 CAR Part3 710C Rev. M 01/27/14 or None April 9, 2014 42 185A 185-0238 through 185-0512 710CM Rev. M 01/27/14 or 43 185B 185-0513 through 185-0653 720C Rev. M 01/27/14 or 44 185C 185-0654 through 185-0776 720CM Rev. M 01/27/14 or 45 185D 185-0777 through 185-0967 730C Rev. M 01/27/14 or 46 185E 185-0968 through 185-1149 730CM Rev. M 01/27/14 or 47 A185E 185-0968 through 185-1599 later FAA approved revision 18501600 through 18502090 48 A185F 652, 18502091 through 18503683 (except 18502300) 18504139 through 18504448 (only aircraft with optional wing fuel cells installed) 49 Cessna Aircraft Company 206 206-0001 through 206-0275 A4CE CAR Part3 710C Rev. M 01/27/14 or None April 9, 2014 50 U206 U206-0276 through U206-0437 710CM Rev. M 01/27/14 or 51 U206A / TU206A U206-0438 through U206-0656 720C Rev. M 01/27/14 or 52 U206B / TU206B U206-0657 through U206-0914 720CM Rev. M 01/27/14 or 53 U206C / TU206C U206-0915 through U206-1234 730C Rev. M 01/27/14 or 54 U206D / TU206D U206-1235 through U206-1444 730CM Rev. M 01/27/14 or 55 U206E / TU206E U20601445 through U20601700 later FAA approved revision 56 U206F / TU206F U20601701 through U20603521 (except U20602589) 57 U206G / TU206G 676, U20603522 through U20604649 58 P206 P206-0002 through P206-0160 59 P206A / TP206A P206-0161 through P206-0306 60 P206B / TP206B P206-0307 through P206-0419 61 P206C / TP206C P206-0420 through P206-0519 62 P206D / TP206D P206-0520 through P206-0603 63 P206E / TP206E P206-0001, P20600604 through P20600647 64 Cessna Aircraft Company 207 / T207 20700001 through 20700362 A16CE FAR Part 23 710C Rev. M 01/27/14 or None April 9, 2014 65 207A / T207A 20700363 through 20700788 710CM Rev. M 01/27/14 or 720C Rev. M 01/27/14 or 720CM Rev. M 01/27/14 or 730C Rev. M 01/27/14 or 730CM Rev. M 01/27/14 or later FAA approved revision

66 Cessna Aircraft Company 210 618, 57001 through 57575 3A21 CAR Part3 710C Rev. M 01/27/14 or None April 9, 2014 67 210A 616, 21057576 through 21057840 710CM Rev. M 01/27/14 or 68 210B 21057841 through 21058085 720C Rev. M 01/27/14 or 69 210C 21058086 through 21058220 (except 21058140) 720CM Rev. M 01/27/14 or 70 210D 21058221 through 21058510 730C Rev. M 01/27/14 or 71 210E 21058511 through 21058715 730CM Rev. M 01/27/14 or 72 210F 21058716 through 21058818 later FAA approved revision 73 T210F T210-0001 through T210-0197 74 210-5 (205) 641, 205-0001 through 205-0480 75 210-5A (205A) 205-0481 through 205-0577

Original Signed By:

Mike Downs FAA APPROVED: ___________________________________________ Timothy P. Smyth Manager, Propulsion and Program Management Branch Chicago Aircraft Certification Office

## Every issue (2)

- April 30, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e5/87/e587d72f6c774315b5c121541e8d8631063b039cc991f74f76d519fb7706c1a4), [SA01380CH_AML .pdf](https://openairdocs.org/files/sha256/8a/94/8a94fd7f87332e592c2aecca4a391b15acb7350e685c88c67a4ce30588751169)
- January 27, 2014: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/23/77/23771d789290e97687d75843cfea4ce9a2c0fbed3a62ebe53881a426cccda673), [SA01380CH_AML .pdf](https://openairdocs.org/files/sha256/8a/94/8a94fd7f87332e592c2aecca4a391b15acb7350e685c88c67a4ce30588751169)

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