# STC SA8184NM-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Learjet Inc., United States
- Description: Reduced Max Take-off Weight to 75,000 LB, Reduced Max Landing Weight to 68,000 LB
- Applied: April 24, 2000
- Status date: December 23, 2015
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 43
- Data sheets: [TCDS T00003NY](https://openairdocs.org/tcds/T00003NY)
- Certificate PDF: https://openairdocs.org/files/sha256/8e/1e/8e1ecea22bef3a1f88da8fd2f6fec8ba9d3dcc5039d0bf16d09f31e74a882e4a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CB2FF03CA9F4E60C862583240045AB60.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA8184NM-D

## ADs that name it (0)

None.

## Approved models (1)

- Bombardier Inc. BD-700-1A10 ([TCDS T00003NY](https://openairdocs.org/tcds/T00003NY))

## 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.

SA8184NM-D

Learjet Inc.

One Learjet Way Wichita, Kansas 67209 25*

. *Certification basis is set forth in Type Certificate Data Sheet T00003NY

T00003NY Bombardier Aerospace BD-700-1A10 Reduced Max Take-off Weight to 75,000 LB, Reduced Max Landing Weight to 68,000 LB in accordance with Master Drawing List BAS67010002, revision C dated March 1, 2001 or later FAA approved revision. FAA approved Airplane Flight Manual Supplement BAS67040002 revision “A” dated March 1, 2001 or later FAA approved revision is required with this installation.

1) The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. 2) The approval of this modification applies to the above noted airplane model series only. 3) A copy of this STC must be included in the permanent records of the modified aircraft. 4) 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. 5) An aircraft maintenance record entry is required in accordance with CFR 14 Part 43.9 when the aircraft is operating in accordance with the weight restrictions of this STC.

April 24, 2000

March 2, 2001

December 23, 2015

Original signed by Keith Johnston

(Signature) Keith Johnston ODA administrator ODA-501508-CE, Learjet Inc.

Wichita, Kansas (Title)

NOTE:

**DO NOT DELETE THIS PAGE.**

**DO NOT ADD ANY DATA TO THIS PAGE.**

**THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.**

(STC No.)

## Every issue (2)

- December 23, 2015: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/8e/1e/8e1ecea22bef3a1f88da8fd2f6fec8ba9d3dcc5039d0bf16d09f31e74a882e4a)
- March 2, 2001: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/b8/f4/b8f462df0fc9e8f20dd783258e567e8f16e57c28a69ea7f3d8d71e3080800bd6)

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