What it approves
Install a single ARINC 741 satellite communication system (SATCOM) provisions.
What the certificate saysPartly OCR
Some pages are OCR from the scanned FAA certificate. OCR can misread letters and numbers.
Bnlud Stam or B~~IP Certificate 1 SURRENDERED Bepartment of Ero~sportation -Tederal Boiation Bdminisa tion ?&~%eh,d(1, UNITED AIR LINES, INC.
~--d/i-&&d,.~LL1U&M~-aU~d.49~ 25 &&Feder a 1 Av i a t ion -,& Ref. T. C. Data Sheet A22WE for Special Conditions.
w.~z~-.~+e- . A22WE J%e. McDonnell Douglas DC10-10 Series ~~&~~@"d"8"d"8"d"8~~y~ Install and activate a single ARINC 741 Satellite Communication System (SATCOM). The installation consists of interconnect wiring, SATCOM antenna, circuit breakers and relays. This modification was accomplished in accordance with United Air Lines DAS 1WE amended approved master drawing list No. 5996 dated December 10, 1994 or later approved revisions. United Air Lines AFM Supplement to FAA approved Flight Manual MDC-31010 dated 12/8/94 or later approved revisions is required as part of this modification.
*n~~ind.d&-h- This approval does not extend to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage.
ab#&-hi-: September 15, 1994 %,b X~llA.
r/-- October 21, 1994 9ab .(~~NWIA~/ December 10, 1994 F. L. Mohr (S~"O,"'<) r Ilnited ~ir lines (T'll'h~~ 1 L~U Any allcrolion of this cerltjicafr ir plrnishoble by afine of no1 exceedfng El,OW, or fmprisonmenf no1 exceeding 3yeors, or both.
This rcrlr/icolr mq be lronrfmrrd in ocrordnnr< wrlh FZlR 21.47.
FU.Fu8llO-l(lO-b8,
United States of America Department of Transportation -Federal biation AdmiristriORRENDERED Certificate Supplemental Type Certificate 4.26.2029 Number: SA3941WE-D This certificate issued to: UNITED AIRLINES, INC.
Part 25 of the FAR Regulations. (SEE TC DATA SHEET A22WE) Original Product Type Certificate Number: A22WE Make: MCDONNELL-DOUGLAS Model: DC-10-10 Description of Type Design Change:
INSTALLATION OF A UHF RADIO TELEPHONE SYSTEM IN ACCORDANCE WITH UNITED AIRLINES, DAS-1WE, SEALED DRAWING LIST 3941 DATED JUNE 9, 1980 OR LATER SEALED REVISION.
Lirilalinsand fendilions: THE APPROVAL OF THIS CHANGE IN IYPE DESIGN APPLIES ONLY TO DC-10-10 AIRCRAFT. THIS APPROVAL DOES NOT EXTEND TO OTHER AIRCRAFT
OF THIS MODEL ON WHICH OTHER PREVIOUSLY APPROVED MODIFICATIONS ARE INCOR-
BETWEEN THIS CHANGE AND ANY OF THOSE OTHER PREVIOUSLY APPROVED MODIFICATIONS WILL INTRODUCE NO ADVERSE EFFECT UPON THE AIRWORTHINESS OF THAT AIRCRAFT.
THIS DETERMINATION SHOULD INCLUDE CONSIDERATION OF SIGNIFICANT CHANGES IN
NEIGHT DISTRIBUTION SUCH AS INCREASE IN THE FIXED DISPOSABLE WEIGHT IN THE
Date of Application: MAY 27, 1980 Jute missnes Date of Issuance: JUNE 9, 1980 I alcanended FEDERAL AVIATION By directin f the Sidministrater (Signature )
TO MINISTRATOE UNITED AIRLINES, DAS COORDINATOR DAS-1WE (Tille) 47 FAA FORM 8110-2 (10-68)
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate SURRENDERED on . Certificate 3069 Number: SA2790NM-D This certificate issued to: UNITED AIRIINES, INC.
Purt 25 of the Federal Aviation Regulations. ( see Type Certificate Data Sheet A22WE for Special Conditions ).
Original Product -Type bertificate Numben: A22WE Make: McDonnell-Douglas Model: DC10-30 Description of Type Design Change: Installation Of full provisions for a Collins Radio Traffic Alert and Collision Avoidance System (ICAS II) and a fully operational dual Collins Radio Mode S Transponder System, in accordance with United Airlines DAS 1 WE Approved Drawing List 2790 dated May 20, 1991 or later approved revisions.
United Airlines AFM Supplement to FAA Approved Flight Manual No. MDC-J5830 dated May 20, 1991, or later approved revisions, is required as part of this modification.
timilatinsandbindilions: This approval does not extend to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.
Date of Application: 5/1/91 Jule missued:
Date of Issuance: 5/20/91 Date Amended:
FEDERAL AVIATION slims the .. dminiatraler line R. M. Casterline ( Signature ) TAMINISTRAIO DAS Staff Coordinator United Airlines DAS 1 WE (Title)
47.
anmd %tarn of SIIKWJ Btpemtnt of '&reneportenon -federal Stmation Sldmo' treoon Certificate $5upplemental 'Qllpr Certifi a@ RRENDERED . ,/ 1 Jt/& SA2837WE-D , , , United Airlines, Inc.
d/!!.d=~& SCeyaituA, /+&y~~A~~J/,I.w~y~m(;c(urA d- Arn,i>Ll.n~ rr r,,/o.nA/;. t,,, ~~-od."/~c4d~d~.&.~iru~4,~.~~~~~~~ +:G J 25 ,J &;* Federal Aviation / ,&.A&,~.
(See T.C. Data Sheet A22WE for special conditions) . , A22WE J/ry~, McDonnell Douglas / DC-10-10 and DC-10-30 Installs new lavatory module/bustle assembly at Door 2 RH/LH, underfloor plumbing and related systems, modified main deck floor support structure, external service panel in accordance with United Airlines DAS-1-WE, Sealed Drawing list 2837 dated 12/9/77, or later sealed revision.
nr~d/orS~&A.d~d~d:
The approval of this change in type design applies basically to the McDonnell Douglas DC-10 airplane. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage.
I - ~dyC~calc nM/Ad+/++A/a mdid A rsC /!A Fr + ra/d,z//rr.,r,urn. ,r, rt/r/~rrr- L January 23, 1975 9,,4 w..u,,,J 9-4 May 1, 1975 9-4 ,,,,,,,, L,/ December 9, 1977 Aoril 18. 1984 R. M. Casterline DAS Coordinator, DAS-1-WE [ 'T,i!r 1 Any allnation ojthir ctrttjcntc is punishable by a fint ojno! rxcccdinp $/,OW, or tmprrsonmrnt no! rxcrtdtne 3vror.r. or both
Dcperrmcnt of Eramiportation -3Pedrral Bbiotion Bdminhtion @uppkmental PC ~f~tifiIa@ RRENDERED Certificate I on C i?&- jii? I *x& SA 3591 WE-D .%>L+A%ML* United Airlines, Inc.
.~~~~h~~~d,,&*2~k&~~~~~~-P-P~m.~rrh.~.~~Y~ 25 ./,&A Fed er a1 Avi at i o n 5, See T.C. Data Sheet A22WE.
@7+&a/t~%&-L~+d~,&~/- : A22W E McDonnell Douglas J&. DC-10-10 Western Airlines 9~+f2~~~>~9h~~/d2&?"~ :
Installs new lavatory module/bustle assembly at Door 2 RH/LH, underfloor plumbing and related systems, modified main deck floor support structure, external service panel in accordance with United Airlines DAS-1-WE, sealed drawing list 3591 dated 3/20/79.
Ad.&z~~.,~~~d~dt*i-nd.nd:
The approval of this change in type design applies basically to the McDonnell Douglas DC-10-10 airplane. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage.
.-%~~+-&,xmd,&~*ModmP~~ adA~~w-dMd~f"-f"-~~mdd/md/~erna~u~~A/dAdun.- mnr/~~~~~d~/w~/w~~nnl'~*rn?rn?~m~~rn~~c,~rh&~&~~~~~.&n~*~+-u/%p .Zl~~~Lir&>rn Ld~w,4:wdm&imA . January 2, 1979 ~?~Ih,H&dfeJ.
L??>&.{A~,~.-~ : March 20, 1979 . September 11, 1979 a' >7 L/~~~~.I/~L/LJ H . N . Tay 1 or (slsn~turci United Airlines DAS Coordinator , DAS-1-WE ,T.,,a, ( 1 ... "/
United States of America Department of Transportation Federal Aviation Administration tuatioSURRENDERED Certificate Supplemental me eerancate 6.26 22004 Number: SA2756NM -D This certificate issued to: UNITED AIR LINES, INC.
Purt 25 of the FEDERAL, AVIATION Regulations: SEE IXPE CERTIFICATE DATA SHEET AZZWE FOR SPECIAL CONDITIONS.
ната I troduct -Sype Tertificate umber A22WE Make: McDONNELL-DOUGLAS Model: DC-10-10 Description of Type Design Change: INSTALLATION OF WIRING PROVISIONS FOR A SINGLE TRAFFI LERT AND CÖLLISION AVOIDANCE SYSTEM (ICAS IL), THE PROVISIONS WILL INCLUDE INTER
CONNECT WIRING, CIRCUIT BREAKERS, MOUNTING TRAYS, ANTENNAE AND ANTENNA COAX CABLES, AND ICAS TYPE VERTICAL SPEED INDICATORS. IN ADDITION, A DUAL OPERATIONAL MODE S TRANSPONDER SYSTEM WILL BE INSTALLED. UNITED AIR LINES AFM SUPPLEMENT TO FAA APPROVED FLIGHT MANUAL MDC-J1010 DATED 7/27/90, OR LATER APPROVED REVISION, IS REQUIRED AS PART OF THIS INSTALLATION OF A DUAL OPERATIONAL MODE S TRANSPONDER SYSTEM.
THIS APPROVAL DOES NOT EXTEND TO OTHER AIRCRAFT OF THIS MODEL ON WHICH OTHER
PREVIOUSLY APPROVED MODIFICATIONS ARE INCORPORATED UNLESS IT IS DETERMINED BY THE
OTHER PREVIOUSLY APPROVED MODIFICATIONS WILL INTRODUCE NO ADVERSE EFFECT UPON THE AIRWORTHINESS OF THAT AIRCRAFT.
0 asterlie R. M. Gasterline (Signalure) YOMINISTRA DAS Staff Coordinator United Air Lines DAS 1 WE (Tille)
47.
United States of America Department of Transportation Federal Aviation Administration Certificate Supplemental Type CertificatesURRENDERED on 6.26.22009 Number SA 2755NM-D This certificate issued to: United AII LInes Purt 25 of the Federal Aviation Regulations: Ref. IC Data Sheet A22WE for Special Conditions Original Product - Type bertificate Numben: AZZWE Make: McDonnell-Douglas Model DC10-30 Series Description of Type Design Change: Replace First Class seats and increase Coach seating from 40 F/C + 245 Y/C to 38 F/C + 260 Y/C. Install new G-3 galley and F/C closet in Zone A. Install centerline stowbins in Zone B and C. Aircraft N1852U-54U and N18560-59U have a new mid-cabin lavatory installation. All zones have new aisle light covers and interior decor upgrade. This modification was accomplished in accordance with United Air Lines DAS IWE approved Master Drawing List 2775 dated January 14, 1991 or later approved revisions.
Timilations and bendilions This approval does not extend to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage.
M. Gay, DAS Coordinator, DAS-IWE (Title)
47.
Bniad 4tem of Smta a Certificate Btpamnent of rans sport at ion -federal 19oiation Sldminis 060 ~URRENDERED $5upplmmtal Egpe CSertific .
9L--w@d;dh UNITED AIR LINES, INC.
San Francisco International Airport San Francisco, California 94128 ~ad.+&~d~~&d.~p-mze&&.d 25 Federal Aviation Ref. T.C. Data Sheet A22WE for Special Conditions ~~&-~+f%+&~: A22WE a: WcDonnell Douglas : DC-10-10 Series g-43- 3+?& Install modified Plight Mode Annunciators to annunciate NAcnstead of Ig: and modified Horizontal Situation Indicators to annunicate GPS and associated wiring and relays. This installation vas accomplished in accordance vith United Air Lines DAS 1 WE approved amended Master Drawing List No. 5995, dated August 25, 1995, or later FAA approved revisions.
2f,n&&-d&dd.
This approval does not extend to other aircraft of this model on vhich other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship betveen this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage.
%&4m/r/L4;- August 31, 1994 %,4 c&,,.,/:
%&ythncu : October 21, 1994 9-6 A/ August 25, 1995, December 10, 1994 - H. Takeuchi (Signature] DAS Staff Coordinator United Air Lines DAS 1-WE
17.11. 1 , . .... , Any allnation of this crrtzjrolr ;s punishabit bp a /in< of not cxcrrdin~ 11,000, or imprisonmen1 no1 txcecdiq3~~ears, or both.
Thu crrl?firalr mo,, br lrnnrfirrrd in orrordonrc w~rh FAR 21.47.
United States of America Department of Transportation Federal Aviation Administration Certificate Supplemental Tupe CertifichtFURRENDERED 6. 26.2004 Number: SA5641N9-D This certificate issued to: UNITED AIR LINES Certifies that the change in the type design for the fillowing product with the linitations and conditions therefor as specified heven meets the airesshiness requirements f Puré 25 spilhe FEDERAL AVIATION Regulalions: Ref. IC Data Sheet AWE for Special Conditions Original Product -Type bertificale Number: ASWE Make: The Boeing Company Model: 727-200 Series Description of Type Design Change:
Installation of Collins DLM-700 series Aircraft Communications and Reporting System (ACARS) with dedicated Collins VHF-700 series VHF transceiver and a Bendix PT-45B printer in accordance with United Air Lines DAS IWE approved Master Drawing List dated September 25, 1992 or later approved revision.
This approval does not extend to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse affect upon the airworthiness of that aircraft.
Refer to AFM Supplement.
M. Vastulin he SIdministral R.M. Casterline (Signalure) TAMIN STRATO DAS Staff Coordinator United Air Lines DAS IWE (Title)
47.
FAA FORM B110-2 (10-68)
Certificate United States of America Department of Transportation Federal Aviation Administration RRENDERED Supplemental Type Certificate 6-26.2629 Number SA2775NM-D This certificate issued to: UNITED AIR LINES Part 25 of the Federal Aviation Regulations. Ref. IC Data Sheet AWE for Special Conditions.
Original Product - Type Bentificate Number:
Make The Boeing Company Model: 727-222 Series Description of Type Design Change: .
Installation of dual Mode S/ATCRBS transponders and full Traffic Alert and Collision Avoidance System (TCAS) provisions, in accordance with United Air Lines DAS 1WE approved Master Drawing List 2775, dated June 23, 1990, or later approved revision. United Air Lines AFM Supplement to FAA Approved Flight Manual D6-8728-222 dated 6/23/90, or later approved revision, is required as part of this installation.
finite operal de on fient one the fner pet of thie ate s This approval does not extend to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. The Mode S functions of the system are not approved for Traffic Alert and Collision Avoidance System (TCAS) rendered, suspended, revoked, or a termination date is thervise established by the Ildministrator of the Federal Aviation Administration Date of Application: 05/08/90 Date Reissued:
Date of Issuance: 06/23/90 Date Amended: 1/28/91, 9/6/90 FEDERAL AVIATION <-M.
R. M. Casterline(Signature) TMINISTATOE DAS Staff Coordinator
UNITED AIR LINES DAS IWE (Iitle)
United States of America Department of Transportation Federal Aviation Administration Certificate Supplemental Type Certificate SURRENDERED on 6. 26. 2009 Number SA2770NM-D This certificate issued to: United Airlines Part 25 sfithe Federal Aviation Regulations. See TC Data Sheet AWE Original Product Type Certificate Numben: АЗИЕ Make: Boeing Model: 727-222 Series Description of Type Design Change:
Installation of TCAS II and Mode 'S' Transponder provisions, consisting of system interwiring, antenna coaxial cables, antenna structure installations, ICAS directional antenna and transponder antenna, in accordance with United Airlines, DAS-1WE, approved drawing list 2770, gated February 9, 1990, or later approved revision.
This approval does not extend to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.
Date of Application: April 12, 1989 Date Reissued:
Date of Issuance: February 9, 1990 Date Amended:
FEDERAL AVIATION By Direction of the Administrator Anger M. Vaster ине (Signature)
TO MINISTRAIOS
INTED AIRLINES DATORDINATOR DAS-THE 47 FAA FORM 8110-2 (10-68)
United States of America Department of Transportation Federal Aviation Administration Supplemental CoDe Certinoat&RRENDERED Certificate on 6-26-2809 Number SA1130NW-D This certificate issued to: UNITED AIRLINES, INC.
Puri. 4.b of the CIVIL AIR Regulations. SPECIAL CONDITIONS: SEE TC DATA SHEET AWE Original Product - Type Certificale Numben АЗИЕ Make: Boeing Murted: 727-222 Description of Type Design Change:
Rework of weather radar system to install solid-state, color-display system in accordance with United Airlines, DAS-TWE, sealed drawing list 1130 dated November 7, 1981, or later sealed revision.
Limilalinsandhandilions: The approval of this change in type design applies only to 727-222 aircraft. This approval does not extend to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution such as increase in the fixed disposable weight in the fuselage.
Administrater f the Federal Aviation Administration Date of Application: October 16, 1981 Jule missued:
Date of Issuance: November 7, 1981 I ate une rated FEDERAL AVIATION By digestion of th KI. Casterlie ildministrah.r ( Signature )
CAINISTRAIO UNITED AIRLINES, DAS COORDINATOR DAS-TWE (Title)
47.
FAA Forn 8110-2 (10-68)
~n~tcd state5 of %mca Department of Transportation -fedtral gbiation Bdrmnieflan ,%+,&ica&d~, United Air Lines, Inc.
.&y/n/Ij,m..
dated December 1953 (See T.C. Data Sheet A~WE) /A- : A3WE -.HA& Boeing 727-222 .%~+xZZ#~&~?~n~~~kn~~; Installation of a McDonnell Douglas ~ros I1 Collision Avoidance System in accordance with FAA sealed UAL Report F-1555 and FAA approved UAL Airplane Flight Manual Supplement, dated 2 2 ,o-r, to Boeing Document D6-8728.1 or a later FAA approved revision.
X~n~fa/lij~,j-ud~~* The ARINC characteristic 587 Collision Avoidance System does not adversely affect any other aircraft system, but the use of the CAS has not been evaluated.
Therefore, flight operations must not be predicated on its use. This approval should not be extended to other specific airplanes of this model on which other previously approved modifications ase incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of the aircraft.
,~~d~~,aa~&rC,du~WA*a,I&~ui&u~~~~~~+~mn~~~~~)n)nun/~/~/~~m~~~u~- 9m44~/-h-~: 11 October 1971 ~A&mAdud:
7/Lumem: 22 NOV 1971 LZ>&,,w&.
9inlk2"??hF -1 (-2' --' ,- A,- A/, ~a<% ~c-~fl 'A, (Slgnolurr/y A i r-7.i c+ (Tllk)
Thls certrficatr may be trnmfiid in accorhnc< w~th FAR 21.47.
FMFou8110-2110-68)
btpoment of Eronsportoflon -f'tderal %iation 51dmmnu@i3FF-'"-- -- -- - Cert~f cote ,$3upplemen tal EJJ~ e @a ~~~~~~EJRREHDERED E oi-,J- - - $[p?
- -------- HA ST00552LA-D -~~+&ucd(o United Air Lines, Inc.
San Francisco International Airport San Francisco, California 94128 Ae+L~+t~44kd&~-4a~7 a.+%~ 25 && Federal Aviation .-&. (Ref. TC Data Sheet A22WE for Special Conditions) w,%&-r+ &..+&~d- : A22W a: McDonnell Douglas Corporation : DClO-10 -GL+.&"y!+9+*:
Modifies the aircraft to deactivate Global Positioning Systems (GPS), Satellite Communication System (SATCOM), Electronic Flight Indicators (EFI) and Electronic Resource System (ERS) including removal of respective components. The deactivation is in accordance with DAS 1 WE approved United Air Lines Master Document List 00552, dated November 22, 1998, or later FAA approved revision.
9-mmdgda:
The approval of this installation applies to the DC10-10 Series only. This approval does not extend to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. 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.
A' November 3, 1998 G~A d.
53~4' : November 22,1998 %A d:
Br& $/A# - . .
Sztnorurr) United Air Lines, DAS Fleet Engineering Coordinator, DAS 1 WE ( T,rtt, Anr vlfrrar,on oj ih,, rrrttfirorr rs pun,lhnb/r 6) a finr of not rlrrrdrnp 1/.Wf7. or ,mprrronmrnt not rrcrrd,n~ ? ,for,. or botr Thtr c,dfirarr ma? br frnnlfrrrrd in nrrorlnr< with FAR 21.17 IlArou8llO-2 ,lo-481
United States of America Department of Transportation Federal Aviation Administration - Supplemental Type CertificatERENDERED Certificate on 6-026. 2009 Number SAII22NW-D This certificate issued to: UNITED AIRLINES, INC.
Purt 4.B of the CIVIL AIR Pegulalions. SPECIAL CONDITIONS: SEE IC DATA SHEET 4A25.
Original Product - İype bentificate Nurnben: 4A25 Make: McDonnell-Douglas Mintel: DC8-61 Description of Type Design Change:
Rework of weather radar system to install solid-state, color-display system in accordance with United Airlines, DAS-WE, sealed drawing list 1122 dated July 1, 1981 or later sealed revision.
Limitations and Conditions: The approval of this change in type design applies only to DC-8-61 aircraft. This approval does not extend to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution such as increase in the fixed disposable weight in the tuselage
Date of Application: June 10, 1981 'Sule misaued Siate fiasuance: JUly 1, 1981 I ate unintel EDERAL AVIATION By Direction of the Administrator K.M. Casterline (Signature )
T MINISTRATO UNITED AIRLINES, DAS COORDINATOR DAS-TWE (Title)
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Cerificore SURRENDERED Number: SA1123NW-D on 6-26-2009 This certificate issued to: WITED AIRLINES, INC.
Purt 4.B of the CIVII AiX Regulalions. Special Conditions: See IC Data Sheet 4225.
Original Product - Type bentificate Number: 4725 Make: McDonnell-Douglas Model: DC-8-61 & DC-8-71 Description of Type Design Change:
Installation of an underwing fueling panel in accordance with United Airlines, DAS-1WE, sealed drawing list 1123 as amended and dated June 8, 1982 or later sealed drawing list.
Limilalins and funditions The approval of this change in type design applies only to DC-8-61 and DC-8-71 aircraft. This approval does not extend to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution such as increase in the fixed disposable weight in the fuselage.
Date of Application: Apri1 30, 1981 Sale missued Date of Issuance: . June 30, 1981 Jade unvented: May 14, 1982 FEDERAL AVIATION By Direction of the Administrator (Signature ) TOMINISTRKIO DAS-IWE United Airlines, DAS Coordinator (Title)
47.
federal Eluietion Elgent!
suppItmont8I QQpe @~rtlfi~~ - rtificate ENDEWED I z&~-/., dh United Air Lines, Inc .
San Francisco International Airport Maintenance Base San Francisco, California 94128 d&,A.&+~~n~d~~rll~/r-Jm/&~wi~~dd~JwL;mLM~r4mdumd:&~ Civil Air &~~-d~~~~&~m,-~~~~ua~ircrXX-rt~I/wdd.dd~~ner~~~~~ 4b J&-.
&yd?zINX~Ki- y@ ~?!A,.'~L~,,.&~ 4.425 &&&-: Douglas Aircraft Company, Inc .
DC-8-21, -31, -32, -33, -51, -52, -53, and E-8F-54 and E-SF-55 9i+it;~. J~M zdy :
Structural installation of a Dorne and Margolin DMC 33-2 Satcom VHF radio antenna in accordance with FAA sealed United Air Lines Report Nuuber F-1156 as revised April 25, 1967.
This is a structural installation only and does not include the operational evaluation of the antenna or system. Prior to operational approval of this radio antenna installation, an operational evaluation must be conducted by the FAA.
~~,~./~~,nn/JLPw~mv+uryAhnd~,ul,d~~ad~~PP~~~d/:~-ur~~~~-~~~dV11 MM,&&-/m&$m&-M I.-.db?z.n/a&,~.A,i8,~U&lIdw .&~~;u;llnnfm~% .PZmd ..dvia~m, .,$em-F %2&/fl~&m - March 31, 1967 %cCfl&..
a&&&--I: April 27, 1967 %b*.r"r"r"r"r"r"d:
FAA FORM 81 10-2 (1-661 0051-657-4000
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificaterificate SURRENDERED Number: SA1926WE on 6-26. 2009 This certificate issued to: United Air Lines, Inc. San Francisco International Airport San Francisco, California 94128 Part Ab sfithe CIVI I Air Fregulations:
Original Product - Typo-Certificate Number: 4A 25 Make: McDonnell Douglas Minted: DC-8-61 and DC-8-62 (Dual installation of the A.C. Electronics Carousel Description of Type Design Change: IV, INS units in the Mode1 DC-8-61 in accordance with Item 1 below and in the Model DC-8-62 in accordance with Items 2 or 3 below):
1. Sealed Appendix "C" of UAL Report #F-1366 and the UAL Supplement to the McDonnell Douglas Model DC-8-61, FAA Approved AFM DAC-33161 dated 27 May 1969.
2. Sealed Appendix "A" of UAL Report #F-1384 and the UAL Supplement to the McDonnell Douglas Model DC-8-62, FAA Approved AFM DAC-33162 dated 21 July 1969.
3. Sealed Appendix "A" of UAL Report #F-1384 modified by UAL's sealed COA 2-3498 ER #20 and the UAL Supplement to the McDonnell Douglas Model DC-8-62, FAA approved AFM DAC-33162 dated 16 JAN 1970 Limitations and Conditions: For cases 1 and 2 above the INS does not adversely aftect ON INS. Placards saying "INS NOT APPROVED FOR WAVIGATION" must be displayed below requirements prevent navigation solely being predicated the CDU head. This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Cerificore
SURRENDERED Number SA2709NM Loon_C 26-2009 This certificate issued to: UNITED AIRLINES, INC Purd 04. b of the CIVil Air Regulationa See Type Certificate Data Sheet 4A25 For Special Conditions Original Product - Type Certificate Number: 4A25 Make: McDonnell-Douglas Merted: DC-8-71 Description of Type Design Change: Installation of an Airfone, Inc. Air to Ground Passenger Telephone System. The installation was done according to UAL DAS-1WE sealed drawing list #2709 dated 5/09/86 or later revision.
Similalinsandtendilions: This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.
Date of Application: 9/03/85 Tute wissued:
Date of Issuance: 5/09/86 Date Amended:
EDERAL AVIATION By direch 11. Castaline Aldministrater (Signature ) TE MINISTRATION United Airlines DAS Coordinator DAS-WE R.M. Casterline (Title) 47 FAA FORM 8110-2 (10-68)
(Title ) United Airlines DAS Coordinator DAS-WE TOMNISTRAIOA R.M.Casterline (Signalure ) M. Pasterline Bydirecsion of the Adm AVIATION FEDERAL Date Amended: 4/30/87 Date of Issuance:
Date Reissued: Date of Application: 9/15/86 Federal Aviation Administration .
rendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the
change and any of those other previously approved modifications will introduce it is determined by the installer that the interrelationship between this model on which other previously approved modifications are incorporated unless Limitations and Conditions: This approval does not extend to other aircraft of this drawing list 2716, dated April 29, 1987, or later sealed revisions.
MODE-S transponder in accordance with UNITED AIRLINES, DAS-1WE, sealed Description of Type Design Change: Installation of an Bendix Model TRA-66A Model: DC-8-71 Make: McDonnell-Douglas Original Product - Type Certificate Number: 4825 Regulationi: See Type Certificate Data Sheet 4A25 for Special Conditions therefor as specified hereon meets the airvorthiness requirements of Part 04.b of the CIVIL AIR Certifies that the change in the type design for the following product with the limitations and condition's This certificate issued to: UNITED AIRLINES, INC.
Number: SA2716NN-D on 6-26-2009 Supplemental Type Certificate &RRENDERED Certificate Department of Transportation Federal Aviation Administration - United States of America
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Certificote SURRENDERED Number: SA2717NM-D on . 6-26-2001 This certificate issued to: UNITED AIRIINES, INC.
Pard 04. of the CiViI Air Regulutina. See Type Certificate Data Sheet 4A25 for Special Conditions.
Original Product - Type Certificate Number: 4A25 Make: McDonnell-Douglas Model: DC8-71 Description of Type Design Change: Installation of TCAS and Data Recording provisions, consisting of equipment mounting trays, antenna systems and cables, circuit breakers, and complete system interwiring, in accordance with United Airlines, DAS-1WE, sealed drawing list 2717, dated April 29, 1987 or later sealed revision.
Timilationsandteditions: This approval does not extend to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce effect upon the airworthiness of that aircraft.
Date of Application: 3/15/87 Date Reissued:
Date of Issuance: 4/30/87 Date Amended:
FEDERAL AVIATION Pay direction of the 2dm nistrator +.M. Castiline (Signature ) * MINISTRATO R.M.Casterline United Airlines DAS Coordinator DAS-WE
47.
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| McDonnell Douglas Corporation | DC-10-10 | A22WE |