FAA REGISTRY
N-Number Inquiry Results
Serial Number | AC-767B | Status | Valid |
Manufacturer Name | FAIRCHILD | Certificate Issue Date | 04/18/2019 |
Model | SA227-AC | Expiration Date | 04/30/2029 |
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) | 50771174 |
MFR Year | 1990 | Mode S Code (Base 16 / Hex) | A3F27C |
Type Registration | LLC | Fractional Owner | NO |
Name | NEW MOUNTAIN AVIATION LLC | ||
Street | 8001 INTERPORT BLVD STE 310 | ||
City | ENGLEWOOD | State | COLORADO |
County | ARAPAHOE | Zip Code | 80112-2902 |
Country | UNITED STATES |
Type Certificate Data Sheet | None | Type Certificate Holder | None |
Engine Manufacturer | AIRESEARCH | Classification | Standard |
Engine Model | TPE331 SERIES | Category | Normal |
A/W Date | 03/18/2003 | 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 |
None |
Mod Code | 28 | Mod Date | 19901130 |
INSTALLED A TEMPORARY FERRY FUEL TRANSFER SYSTEM PER VKV-FAIRCHILD SA227 SERIES PREVIOUSLY APPROVED DATA. SAM ON FILE AT THIS ACTIVITY. CABIN TNAKS COMPLY WITH MIL-E-1605K, MIL-E-15997A, AND QQR-556 SPECIFICATIONS. AC 43.13-1A METHODS AND TECHNIQUES ADHERED TO. CABIN FUEL TRANSFERS BY GRAVITY AND CABIN PRESSURE TO RH WING TANK SUMP WITHVKV-FAIRCHILD SA227 TEE ASSEMBLY. SYSTEM PRESSURE TESTED. SYSTEM TRANSFER PERFORMED. RAT OF FLOW EXCEEDS POWERPLANT(S) BURN RATE. SYSTEM TO BE FLIGHT TESTED AND RESULTS ENTERED INTO AIRCRAFT RECORDS. W&B LOADINS SHOWN ON 337. LOWER RH WING FUEL LEVEL FOR REFILL. SELECT CABIN TRANSFER SV ON. MONITOR RATE OF REFILL. DO NOT FILL ABOVE 3/4 FULL. REPEAT ABOVE STEPS AS NEEDED. ENSURE CABIN TRANSFER SV IS OFF. WHEN NOT TRANSFERRING CABIN FUEL TO RH WING. | |||
Mod Code | 28 | Mod Date | 20130220 |
MODIFIED AIRCRAFT BY INSTALLATION OF ONE SHROUDED 100 US GALLON (670 LBS) AUXILIARY FUEL TANK LOCATED IN THE CABIN A FUSELAGE STATION F.S. 306.7 IN ACCORDANCE WITH WORLDWIDE AIRCRAFT SERVICES INC. ENGINEERING ORDER NUMBER E.O. 227-28-04, REV. IR, AND SUBSTANTIATED BYFAA FORM 8110-3'S DATED 2/8/2013 (STRUCTURAL, SYSTEM AND ELECTRICAL). INSERTED FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT, REPORT AF-227-3 (AS SUBSTANTIATED BY FAA FORM 8110-3 DATED FEBRUARY 16, 2013) DATED4/3/2013 INTO AIRPLANE FLIGHT MANUAL. INSTUCTIONS FOR CONTINUED AIRWORTHINES (ICA) ARE CONTAINED IN WORLDWIDE AIRCRAFT SERVICES, INC. DOCUMENT NUMBER WA227-ICA-04 REVISION IR DATED 2/7/2013. AIRCRAFT WEIGHED AFTER MODIFICATION AND EQUIPMENT LIST UPDATED AS APPLICABLE. |