STC SA796WE

Supplemental type certificate · Boeing Company

Holder
Boeing Company · United States
Status
Current · Reissued
Status date
September 7, 2010
Applied
June 5, 1964
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21
Data sheet
TCDS4A10

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Wing flap attachments modification. S/Ns 44903, 44904. 45143 thru 45149, 45151 thru 45154, 45356, 45358, 45360, 45482 thru 45490

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

1'lnitc() ~tlltC5 (g£ ~mcrirll ~cpnrtmcnt of 'illrnnsportntion - JIfcOHnl J\btntion J\omtntstrntion ~uppl£m£ntal ijJ1JP£C1I£rtifirat£ The Boeing Company 4000 Lakewood Boulevard Long Beach, California 90808 CI",,'.I~J d-/...!~ Ck//1Y'fiVt ~ (ypl" df,J~/b ft/'~~a;..//'Vff7/VN/I/C.I //Jrd ~ h/be«b.lU'/tJ ///d c/'/b/k-/iwtJ ~/'~/' 0'..) ,ybl"c~dk"w'/bm.N.{) ~ tZVt/'wd/bI"JJ/'f'j7-UVI"//bI"/MJ 1'/-7;//.1 4b /y-a,7ff;;',iI'.Au'./6WHh...!H'/tJ'.

4AIO Boeing DC-7 (Serial Nos, 44903, 44904, 45143 thru 45149,45151 thru 45154, 45356, 45358, 45360, 45482 thru 45490 !!fJI"JC"rUUWr/~bI" 9~I"J~/b 1ff/h/1Y'~' Modification of wing flap attachments per Douglas Aircraft Company Drawing No. 5779438, Change "A".

Aircraft structural limits are: take-off 123,800 lbs; landing 100,000 lbs.; zero fuel weight 94,500 lbs., Serial Nos. as listed above. Airplane Flight Manual Supplement dated September 25, 1964, to Douglas Aircraft Company AFM No. SM-18268 is required.

::i5i-/ldo-...!U'/tJ1'//1//6"Wtdt:?U'/lJ' Data not suitable for reproduction of installation in other aircraft; therefore, it is satisfactory only for Serial Nos. listed above. No additional modifications of this type are to be approved solely by reference to this Supplemental Type Certificate or the data submitted therefor.

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JrL,ybl"/Kb'fd/wN,,.{;,d N' tZ.If'/'''/bt/t-tZ.luwa;{;;-p,iJ ,.,.a,,/'//'iJl" ",,)hA!~a! &~ ,AoY/iubiJ.lnzlf'/' r/'.I/£'.!]?;cknzt .A,wkw .A~tUbiJv//...!HJ-a September 25, 1964 Douglas Aircraft Co., Inc.

!!fJr/...!t'n~UN./,' Reissued to McDonnell Douglas Corporation August 25, 1967; Reissued to The Boeing Company September 7, 2010 91",-«O'/'Hy?cka!, .5iJ'yavrdHvb r/?~...r6&/u/t.0,t-.O'...!N' r=\\ ~g~ '-~ . ~ ~tu~ Supervisor, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office (Title) ~ny a{teratwn of tfiis certificate is punislia6fe ~y a jim of 7Wt e>i!eerfi1lf]$1,000, or improonment7Wt' e>i!eed'ing3 years, ilr both.

FAA Form H10-2 (10-68) Page 1 of 2 'T1iiscertificate may 6e transjerredin accordancewitli '1)1'1(21.47,

TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number _ to (:Nameof transferee) _ {:4.tft:fressof transfer) _ (:Num6eratuf street) (City, State, aTUfZip coae) from (:Nameof grantor)(Print or type) _ (:4.cfcfressofgrantor) (:Num6eraTUfstreet) (City, State, atuf Zip coae) Extent of Authority (if licensing agreement): _ Date ofTransfer: _ Signature of grantor (In inRJ: _ Page 2 of 2

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
The Boeing CompanyDC-74A10