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N169CA has Assigned/Multiple Records

N-Number Entered: 169ca Aircraft Description
Serial Number 8088 Status Valid
Manufacturer Name DORNIER Certificate Issue Date 07/16/2019
Model DO-228-202 Expiration Date 07/31/2029
Type Aircraft Fixed Wing Multi-Engine Type Engine Turbo-prop
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 50211520
MFR Year 1986 Mode S Code (Base 16 / Hex) A11350
Type Registration Government Fractional Owner NO
Registered Owner
Name ARIZONA STATE UNIVERSITY
Street 777 E UNIVERSITY
City TEMPE State ARIZONA
County MARICOPA Zip Code 85287-0001
Country UNITED STATES
Airworthiness INFORMATION PROVIDED HERE SHOULD NOT BE USED TO DETERMINE THE AIRWORTHINESS OF AN AIRCRAFT.
Refer to 14 CFR Parts 39, 43, 91, and FAA Order 8130.2 for airworthiness regulations and guidance.
Type Certificate Data Sheet None Type Certificate Holder None
Engine Manufacturer HONEYWELL Classification Standard
Engine Model TPE331-SER Category Normal
A/W Date 01/30/2015 Exception Code No
The information contained in this record should be the most current Airworthiness information available in the historical aircraft record. However, this data alone does not provide the basis for a determination regarding the
airworthiness of an aircraft or the current aircraft configuration. For specific information, you may request a copy of the aircraft record at https://aircraft.faa.gov/e.gov/ND/
Other Owner Names
None
Temporary Certificates
Certificate Number T195399 Issue Date 07/16/2019 Expiration Date 08/15/2019
Fuel Modifications
Mod Code 28 Mod Date 20151214
INSTALLED FERRY FUEL SYSTEM 91 POUNDS / STATION 295.7. INSTALLED PER (MOD A&HCC 1447 NZ DATA AS REFERENCE) DORNIER 228-202, REVISION (0), FEB, 15/09. POWER TO BE SUPPLIED TO FERRY PUMPS BY BUS 1, ESSENTIAL DC BUS. ALL WORK PERFORMED PER AC43.13/1B. TANK PLACARD - MAXIMUM 1534I/400 USG, COCKPIT PLACARD / FERRY SYSTEM INSTALLED, (A&HCC 1447).WEIGHT AND BALANCE AMENDED FOR THIS CONFIGURATION. SYSTEM HAS BEEN TESTED AND INSTALLED PER MODIFICATION A&HCC 1447 ISSUE 1 INSTALLATION MANUAL. DRAWINGS AND DOCUMENTS: A&HCC 1477 INSTALLATION OF FERRY FUEL SYSTEM DORNIER 228-202. A&HCC 1477A ASSEMBLY INTERNAL MANIFOLD DORNIER228-202, A&HCC 1477A1 ASSEMBLY INTERNAL MAINFOLD DORNIER 228-202, A&HCC 1477B ASSEMBLY FAIRING WING/FLAP DORNIER 228-202, A&HCC 1477C ASSEMBLY HOSE, WING TO FUSELAGE DORNIER 228-202, A&HCC 1477E ASSEMBLY ELECTRIC DORNIER 228-202. A LOG BOOK ENTRY HAS BEEN MADE. "THIS ALTERATION WILL NOT ADVERSELY AFFECT OTHER PREVOUSLY APPROVED MODIFCA TIONS, AND WILL INTRODUCE NO ADVERSE EFFECTS UPON THE AIRWORTHINESS OFTHE AIRPLANE". INSTRUCTIONS FOR CONTINUED AIRWORTHINESS WILL BE FOUND IN DOC A&HCC ICA 1447 DORNIER 228-202. OTHERWISE, THE SCOPE AND DETAILOF FAR 43 APPENDIX D WILL APPLY. MODIFICATION A&HCC 1477 INSTALLS A FERRY FUEL SYSTEM IN THE MAIN CABIN OF DORNIER 228-202, N169CA S/N 8088. THIS SYSTEM CONSISTS OF A BLADDER TANK IN THE CABIN WITH DUAL ELECTRIC PUMPS TO TRANSFER TO THE FUEL INTO THE STARBOARD WING TANK OFTHE AIRCRAFT. THE INSTALLATION FUCTIONS AS A "TOP UP" FERRY FUEL SYSTEM. INFORMATION IN THIS DOCUMENT SUPPLEMENTS OR SUPERSEDES INFORM ATION IN THE BASIC AIRCRAFT FLIGHT MANUAL. FOR LIMITATION, EMERGENCY PROCEDURES, NORMAL PROCEDURES AND PERFORMANCE INFORMATION NOT
Mod Code 28 Mod Date 20160303
INSTALLED FERRY FUEL SYSTEM 91 POUNDS / STATION 295.7. INSTALLED PER (MOD A&HCC 1447 NZ DATA AS REFERENCE) DORNIER 228-202, REVISION (0), FEB, 15/09. POWER TO BE SUPPLIED TO FERRY PUMPS BY BUS 1, ESSENTIAL DC BUS. ALL WORK PERFORMED PER AC43.13/1B. TANK PLACARD - MAXIMUM 1534I/400 USG, COCKPIT PLACARD / FERRY SYSTEM INSTALLED, (A&HCC 1447).WEIGHT AND BALANCE AMENDED FOR THIS CONFIGURATION. SYSTEM HAS BEEN TESTED AND INSTALLED PER MODIFICATION A&HCC 1447 ISSUE 1 INSTALLATION MANUAL. DRAWINGS AND DOCUMENTS: A&HCC 1477 INSTALLATION OF FERRY FUEL SYSTEM DORNIER 228-202. A&HCC 1477A ASSEMBLY INTERNAL MANIFOLD DORNIER228-202, A&HCC 1477A1 ASSEMBLY INTERNAL MAINFOLD DORNIER 228-202, A&HCC 1477B ASSEMBLY FAIRING WING/FLAP DORNIER 228-202, A&HCC 1477C ASSEMBLY HOSE, WING TO FUSELAGE DORNIER 228-202, A&HCC 1477E ASSEMBLY ELECTRIC DORNIER 228-202. A LOG BOOK ENTRY HAS BEEN MADE. "THIS ALTERATION WILL NOT ADVERSELY AFFECT OTHER PREVOUSLY APPROVED MODIFCA TIONS, AND WILL INTRODUCE NO ADVERSE EFFECTS UPON THE AIRWORTHINESS OFTHE AIRPLANE". INSTRUCTIONS FOR CONTINUED AIRWORTHINESS WILL BE FOUND IN DOC A&HCC ICA 1447 DORNIER 228-202. OTHERWISE, THE SCOPE AND DETAILOF FAR 43 APPENDIX D WILL APPLY. MODIFICATION A&HCC 1477 INSTALLS A FERRY FUEL SYSTEM IN THE MAIN CABIN OF DORNIER 228-202, N169CA S/N 8088. THIS SYSTEM CONSISTS OF A BLADDER TANK IN THE CABIN WITH DUAL ELECTRIC PUMPS TO TRANSFER TO THE FUEL INTO THE STARBOARD WING TANK OFTHE AIRCRAFT. THE INSTALLATION FUCTIONS AS A "TOP UP" FERRY FUEL SYSTEM. INFORMATION IN THIS DOCUMENT SUPPLEMENTS OR SUPERSEDES INFORM ATION IN THE BASIC AIRCRAFT FLIGHT MANUAL. FOR LIMITATION, EMERGENCY PROCEDURES, NORMAL PROCEDURES AND PERFORMANCE INFORMATION NOT
Mod Code 28 Mod Date 20170419
INSTALLED FERRY FUEL SYSTEM 91 POUNDS / STATION 295.7. INSTALLED PER (MOD A&HCC 1447 NZ DATA AS REFERENCE) DORNIER 228-202, REVISION (0), FEB, 15/09. POWER TO BE SUPPLIED TO FERRY PUMPS BY BUS 1, ESSENTIAL DC BUS. ALL WORK PERFORMED PER AC43.13/1B. TANK PLACARD - MAXIMUM 1534I/400 USG, COCKPIT PLACARD / FERRY SYSTEM INSTALLED, (A&HCC 1447).WEIGHT AND BALANCE AMENDED FOR THIS CONFIGURATION. SYSTEM HAS BEEN TESTED AND INSTALLED PER MODIFICATION A&HCC 1447 ISSUE 1 INSTALLATION MANUAL. DRAWINGS AND DOCUMENTS: A&HCC 1477 INSTALLATION OF FERRY FUEL SYSTEM DORNIER 228-202. A&HCC 1477A ASSEMBLY INTERNAL MANIFOLD DORNIER228-202, A&HCC 1477A1 ASSEMBLY INTERNAL MAINFOLD DORNIER 228-202, A&HCC 1477B ASSEMBLY FAIRING WING/FLAP DORNIER 228-202, A&HCC 1477C ASSEMBLY HOSE, WING TO FUSELAGE DORNIER 228-202, A&HCC 1477E ASSEMBLY ELECTRIC DORNIER 228-202. A LOG BOOK ENTRY HAS BEEN MADE. "THIS ALTERATION WILL NOT ADVERSELY AFFECT OTHER PREVOUSLY APPROVED MODIFCA TIONS, AND WILL INTRODUCE NO ADVERSE EFFECTS UPON THE AIRWORTHINESS OFTHE AIRPLANE". INSTRUCTIONS FOR CONTINUED AIRWORTHINESS WILL BE FOUND IN DOC A&HCC ICA 1447 DORNIER 228-202. OTHERWISE, THE SCOPE AND DETAILOF FAR 43 APPENDIX D WILL APPLY. MODIFICATION A&HCC 1477 INSTALLS A FERRY FUEL SYSTEM IN THE MAIN CABIN OF DORNIER 228-202, N169CA S/N 8088. THIS SYSTEM CONSISTS OF A BLADDER TANK IN THE CABIN WITH DUAL ELECTRIC PUMPS TO TRANSFER TO THE FUEL INTO THE STARBOARD WING TANK OFTHE AIRCRAFT. THE INSTALLATION FUCTIONS AS A "TOP UP" FERRY FUEL SYSTEM. INFORMATION IN THIS DOCUMENT SUPPLEMENTS OR SUPERSEDES INFORM ATION IN THE BASIC AIRCRAFT FLIGHT MANUAL. FOR LIMITATION, EMERGENCY PROCEDURES, NORMAL PROCEDURES AND PERFORMANCE INFORMATION NOT
Mod Code 28 Mod Date 20180206
INSTALLED FERRY FUEL SYSTEM 91 POUNDS / STATION 295.7. INSTALLED PER (MOD A&HCC 1447 NZ DATA AS REFERENCE) DORNIER 228-202, REVISION (0), FEB, 15/09. POWER TO BE SUPPLIED TO FERRY PUMPS BY BUS 1, ESSENTIAL DC BUS. ALL WORK PERFORMED PER AC43.13/1B. TANK PLACARD - MAXIMUM 1534I/400 USG, COCKPIT PLACARD / FERRY SYSTEM INSTALLED, (A&HCC 1447).WEIGHT AND BALANCE AMENDED FOR THIS CONFIGURATION. SYSTEM HAS BEEN TESTED AND INSTALLED PER MODIFICATION A&HCC 1447 ISSUE 1 INSTALLATION MANUAL. DRAWINGS AND DOCUMENTS: A&HCC 1477 INSTALLATION OF FERRY FUEL SYSTEM DORNIER 228-202. A&HCC 1477A ASSEMBLY INTERNAL MANIFOLD DORNIER228-202, A&HCC 1477A1 ASSEMBLY INTERNAL MAINFOLD DORNIER 228-202, A&HCC 1477B ASSEMBLY FAIRING WING/FLAP DORNIER 228-202, A&HCC 1477C ASSEMBLY HOSE, WING TO FUSELAGE DORNIER 228-202, A&HCC 1477E ASSEMBLY ELECTRIC DORNIER 228-202. A LOG BOOK ENTRY HAS BEEN MADE. "THIS ALTERATION WILL NOT ADVERSELY AFFECT OTHER PREVOUSLY APPROVED MODIFCA TIONS, AND WILL INTRODUCE NO ADVERSE EFFECTS UPON THE AIRWORTHINESS OFTHE AIRPLANE". INSTRUCTIONS FOR CONTINUED AIRWORTHINESS WILL BE FOUND IN DOC A&HCC ICA 1447 DORNIER 228-202. OTHERWISE, THE SCOPE AND DETAILOF FAR 43 APPENDIX D WILL APPLY. MODIFICATION A&HCC 1477 INSTALLS A FERRY FUEL SYSTEM IN THE MAIN CABIN OF DORNIER 228-202, N169CA S/N 8088. THIS SYSTEM CONSISTS OF A BLADDER TANK IN THE CABIN WITH DUAL ELECTRIC PUMPS TO TRANSFER TO THE FUEL INTO THE STARBOARD WING TANK OFTHE AIRCRAFT. THE INSTALLATION FUCTIONS AS A "TOP UP" FERRY FUEL SYSTEM. INFORMATION IN THIS DOCUMENT SUPPLEMENTS OR SUPERSEDES INFORM ATION IN THE BASIC AIRCRAFT FLIGHT MANUAL. FOR LIMITATION, EMERGENCY PROCEDURES, NORMAL PROCEDURES AND PERFORMANCE INFORMATION NOT

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