FAA REGISTRY
N-Number Inquiry Results
Serial Number | 920089 | Status | Valid |
Manufacturer Name | SIKORSKY | Certificate Issue Date | 06/04/2019 |
Model | S-92A | Expiration Date | 06/30/2029 |
Type Aircraft | Rotorcraft | Type Engine | Turbo-shaft |
Pending Number Change | None | Dealer | No |
Date Change Authorized | None | Mode S Code (base 8 / Oct) | 53355653 |
MFR Year | 2008 | Mode S Code (Base 16 / Hex) | ADDBAB |
Type Registration | Corporation | Fractional Owner | NO |
Name | BANK OF UTAH TRUSTEE | ||
Street | 50 S 200 E STE 110 | ||
City | SALT LAKE CITY | State | UTAH |
County | SALT LAKE | Zip Code | 84111-1617 |
Country | UNITED STATES |
Type Certificate Data Sheet | R00024BO | Type Certificate Holder | SIKORSKY AIRCRAFT CORP |
Engine Manufacturer | GE | Classification | Standard |
Engine Model | CT7-8A | Category | Transport |
A/W Date | 08/14/2008 | 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/ |
None |
Certificate Number | T257413 | Issue Date | 06/05/2025 | Expiration Date | 07/05/2025 |
Mod Code | 28 | Mod Date | 20110714 |
INSTALLED AERAZUR-ZODIAC INTERNAL AUXILIARY FUEL SYSTEM (IAFS) COMPLETION KIT IAW EASA STC NO. EASA.R.S.01263 REV 2. 1. EQUIPMENT REMOVED FOR THIS INSTALLATION: 2EA SIDE FACING UTILITY SEAT P/N: MBCS12410 (15 LBS EACH ARM 350 AND 370). FUEL MANAGEMENT CONTROL PANELP/N: 06092A10W010-1 (1 LBS RM 170). 2. INSTALLED THE FOLLOWING EQUIPMENT: AERAZUR P/N: 508617-1 IAFS COMPLETION KIT 357.4/CABIN COMPARTMENT. 3. ALL IAFS CIRCUIT BREAKERS ARE LOCATED IN THE AIRCRAFT MANUFACTURER'S SUPPLIED PANELS AND ARE APPROPRIATELY LABELED IAW THIS STC AND S92A-AMM-31-10-06, 07 AND 08.ALL WORK ACCOMPLISHED IN ACCORDANCE WITH A.C.43.13.1B CHAPTER 10 SECTION 1-2, CHAPTER 11 SECTION 3-6, CHAPTER 11 SECTION 8-17, A.C.43-13-2A CHAPTER 1 PARA 1-12CHAPTER 2 PARA 21-28. EQUIPMENT LIST UPDATED TO REFLECT INSTALLATION OF THIS SYSTEM. WEIGHT AND BALANCE AMENDED AS REQUIRED. COMPASS SYSTEMVERIFIED AND CORRECTED AS REQUIRED. ELECTRICAL LOAD ANALYSIS APPROVED ON FAA FORM 8110-3 DATED 12/10/2009 BY DERT710113-SW. THE MANUFACTURERINSTUCTIONS FOR CONTINUED (ICA) ARE ATTACHED IN THE FOLLOWING DOCUMENTAERAZUR ICAS-S-92 IAFS ISSUES 1 PROVISION KIT. FAA APPROVED ROTORCRAFTFLIGHT MANUAL SUPPLEMENT, VL-S92AUXFUEL-001, REV 1R DATED 12/07/2009, FOR SIKORSKY MODEL S-92A PART 1 AERAZUR-ZODIAC GROUP INTERNAL AUXILIARY FUEL SYSTEM IS REQUIRED FOR THIS INSTALLATION AND IS INSTALLED IN THE ROTORCRAFT FLIGHT MANUAL. FAA APPROVAL: 12/11/2009. TESTING AND TROUBLESHOOTING INSTRUCTIONS ARE ATTACHED IN THE FOLLOWINGDOCUMENTS: AERAZUR DOC NO. 060S432,REV 15, GROUND FUNTIONAL TEST PROCEDURE 508687-1/508688-1 FOR S92 FUEL SYS. AERAZUR MAINTENANCE MANUAL SUPPLEMENT NO S92 AMM-S 28-10-00, ISSUE 5; SECTION 28-00-00 FOR |