FAA REGISTRY
N-Number Inquiry Results
Serial Number | 920067 | Status | Valid |
Manufacturer Name | SIKORSKY | Certificate Issue Date | 07/25/2019 |
Model | S-92A | Expiration Date | 07/31/2029 |
Type Aircraft | Rotorcraft | Type Engine | Turbo-shaft |
Pending Number Change | None | Dealer | No |
Date Change Authorized | None | Mode S Code (base 8 / Oct) | 51327024 |
MFR Year | 2007 | Mode S Code (Base 16 / Hex) | A5AE14 |
Type Registration | Corporation | Fractional Owner | NO |
Name | TVPX AIRCRAFT SOLUTIONS INC TRUSTEE | ||
Street | 39 E EAGLE RIDGE DR STE 201 | ||
City | NORTH SALT LAKE | State | UTAH |
County | DUCHESNE | Zip Code | 84054-2533 |
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 | 09/24/2007 | 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/ |
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Certificate Number | T195673 | Issue Date | 07/25/2019 | Expiration Date | 08/24/2019 |
Mod Code | 28 | Mod Date | 20091226 |
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: 2 EA SIDE FACING UTILITY SEAT P/N:MBCS12410 ( 15 LBS EACH ARM 350 AND 370). FUEL MANAGEMENT CONTROL PANEL P/N: 06092A10W010-1 ( 1 LBS ARM 170). 2. INSTALLED THE FOLLOWING EQUIPMENT: MFG AERAZUR TYPE P/N: 508617-1 DESCRIPTION IAFS COMPLETION KIT STATION/LOCATION 357.4/CABIN COMPARTMENT 3. ALL IAFS CIRCUIT BREAKERS ARE LOCATED IN THE ACFT MANUFACTURER'S SUPPLIED PANELS AND ARE APPROPRIATELY LABELED IAW THIS STC AND S92A-AMM-31-10-06, 07 AND 08. 4. ALL WORK ACCOPLISHED IN ACCORDANCE WITH: A.C.43.13-1B CHAPTER 10 SECTION 1-2 WEIGHT AND BALANCE CONSIDERATIONS CHAPTER 11 SECTION 3-6 ELECTRICAL LOADING AND PROTECTION. CHAPTER 11 SECTION 8-17 WIRE ROUTING, MARKING AND CONNECTING.A.C.43-13-2A CHAPTER 1 PARA 1-12 STRUCTURAL MOUNTING DATA. CHAPTER 2 PARA 21-28 EQUIPMENT PHYSICAL MOUNTING TECHNIQUES. 5. EQUIPMENT LIST UPDATED TO REFLECT INSTALLATION OF THIS SYSTEM. 6. WEIGHT AND BALLANCE AMENDED AS REQUIRED. 7. COMPASS SYSTEM VERIFIED AND CORRECTED AS REQUIRED. 8. ELECTRICAL LOAD ANALYSIS APPROVED ON FAA FORM 8110-3 DATED 12/10/2009 BY DERT-710113-SW. 9. THE MANUFACTURER'S INSTRUCTIONS FOR CONTINUED (ICA) ARE ATTACHED IN THE FOLLOWING DOCUMENT: AERAZUR ICAS- S-92 IAFS ISSUES 1 PROVISION KIT. 10. FAA APPROVED ROTOCRAFT FLIGTH MANUAL SUPPLEMENT, VL-S92AUXFUEL-001, REV IR, DATED 12/07/2009, FOR SIKORSKY MODEL S-92A PART 1 AERAZUR-ZODIAC GROPU INTERNAL AUXILIARY FUEL SYSTEM IS REQUIRED FOR THIS INSTALLATION AND IS INSTALLED IN THE ROTOCRAFT FLIGHT MANUAL. FAA APPROVAL: 12/11/2009. 11. TESTING AND TROUBLESHOOTING INSTRUCTIONS ARE ATTACHED IN THE FOLLOWING DOCUMENTS: (A) AERAZUR |
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