# STC SA1787SO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: MU-2 Modifications, Inc, United States
- Description: Installation of a crew emergency exit in place of pilot window.
- Applied: February 1, 1985
- Status date: July 3, 1985
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A2PC](https://openairdocs.org/tcds/A2PC), [TCDS A10SW](https://openairdocs.org/tcds/A10SW)
- Certificate PDF: https://openairdocs.org/files/sha256/d5/cf/d5cf9aefaefd5f4eedf852f560a1cb8e92866cfd0ce868055d78969cbbd90b52
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6A6CEAC2288BB29585256CC10083D080.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1787SO

## ADs that name it (0)

None.

## Approved models (17)

- Mitsubishi Heavy Industries Ltd. MU-2B ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-10 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-15 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-20 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-25 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-25 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-26 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-26 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-26A ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-30 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-35 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-35 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-36 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-36 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-36A ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-40 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-60 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))

## 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.

I / 1 States or Slmmta Bepartment of ^transportation - federal Stoiation administration Supplemental t4Jpe Certificate SA1787SO <- MU-2 Modifications, Inc.

Box 7184 Dallas, Texas 75209 Civil Air A2PC/A10SW Micsubishi ,^^/ MU-2B Series if- Ay/tf'-S'eJtati <>j/mrt</t.

Installation of a crew emergency exit in place of pilot window in accordance with General Air Services, Inc. Drawing No. MU2-001, Revision A, dated May 13, 1985, or later FAA approved revision.

_/>/„/«/««j atu/(J,.Hf/,-&•„j Installation of this STC requires deactivation of the pressurization control system in accordance with above drawing MU2-Q01.

Airplane Flight Manual Supplement (AFMS) dated June 7, 1985, is a required part of this STC for the Model MU-2B-35 and AFMS dated July 3, 1985, for all other MU-2B aircraft.

*j ftr/tfinitr iini//Sit jH/t/tff/inaufii/u tti/iirfi fj (iv*1 /tulfj ft-r-a/iA*i-iii4Afmt/.rtii,atil -t'fi f//rr/ti '.t/frttf, JftJ/if/if/n/.f tvA'f'f, t~t< *t /r*r/tHfut/ti'ti* <f&£r tA-<4flfrwt&&.tAfii/'ft£/if4/{-tt &t£ SYt/j/tt'rt4j/?ti/'-r */ //it' of / February I, 1985 ^^ ^,^«,^. July 3( '/'JJ*""'" June 7, 1985 ,'/i«4-«™««4./.- July 3_ 19g5 Gerald R. Mack t-^<i""i-"i Acting Manager, Atlanta Aircraft Certification Office ( J i''' ) Any uUrrutian uj'//in ifili/icule a {>uni<.luibte hi a jtnf uj not exceeding II ,001), or tmftriwumtnl not rxctfdiiifi 3 yean, at both.

'I ha iriii/i,,itr "nit he tiaasfrr'td in mrnniamt it'llh I-.\K i'1.17.

INSTRUCTIONS. The transfer endorsement below may be used 10 notify the appropriate FAA Regional Office of [he transfer of (hit Supplemental Type Certificate.

The FAA will reissue the certificate m the name of the transferee and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) f Mumbe' and llrret) (Ciif, Stall, a.

from (Name of grantor) (Print or type) (Address of grantor) (Number and strttt J I Cily, SlaU, ami ZJP mail Extent of Aulhority (if licensing agreement):

Signature of grantor (In ink):

**C FAA AC 69-5536**

## Every issue (1)

- July 3, 1985: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d5/cf/d5cf9aefaefd5f4eedf852f560a1cb8e92866cfd0ce868055d78969cbbd90b52)

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