FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N9010F is Assigned

N-Number Entered: 9010f Aircraft Description
Serial Number 190004 Status Valid
Manufacturer Name HUGHES Certificate Issue Date 05/10/2010
Model 369H Expiration Date 06/30/2027
Type Aircraft Rotorcraft Type Engine Turbo-shaft
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 53072501
MFR Year 1969 Mode S Code (Base 16 / Hex) AC7541
Type Registration Individual Fractional Owner NO
Registered Owner
Name CODY RICHARD A
Street 5921 WOODLEY RD
City MCLEAN State VIRGINIA
County FAIRFAX Zip Code 22101-3342
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 H3WE Type Certificate Holder MD HELICOPTERS INC (MDHI)
Engine Manufacturer AMA/EXPR Classification Standard
Engine Model UNKNOWN ENG Category Normal
A/W Date 10/13/1994 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
None
Fuel Modifications
Mod Code 28 Mod Date 20100130
STC# SH207WE, INSTALLATION OF RANGE EXTENSION FUEL TANK IN THE CARGO AREA..." ROBERTSON AVIATION LLC FAA FORM 8130-6, DATED 1/21/2010, FORM TRACKING NO. 012110-001, WORK ORDER NUMBER WO 367817 B. THIS ALTERATION IS THE UPGRADE FOR THE ROBERTSON AVIATION LLC AUX. FUEL SYSTEM TO THE CURRENT -BSC CONFIGURATION CONCERNING THE FILLER NECK ONLY WITH PARTS USAGE AS DEFINED IN PARAGRAPH 2 BELOW. 1. AUXILIARY FUEL TANK ASSEMBLY, P/N HA-075 WAS"...REFURBISHED, INSPECTED, AND LEAK TESTED IAW FACTORY PROCEDURES (ASSEMBLY AND TEST PROCEDURES HA010C FOR THE AND FOUND TO BE IN AN AIRWHORY CONDITION, IAW 14 CFR PART 43.3J." 2. THIS ASSEMBLY WAS INSTALLED IAW ROBERTSON AVIATION, FAA APPROVED MASTER DRAWING LIST MDL-HA-010, DATED JANUARY 1978 OR LATER APPROVED REVISION FOR THE " -BSC HAL010C LOW FILLER NECK". REMOVED ORIGINAL FUEL FILLER NECK (FIXED/RED), P/N HA-053 AND REPLACED WITH FILLER FLANGE, P/N HA010-118-1.3. NOTE: IAW ROBERTSON AVIATION INSTALLATION DRAWING, ENGINEERING DRA WING HA-075 NOTE 15, "WHEN TANK IS REMOVED INSTALL ITEM 018 & 019 ONTO ITEM 060 FOR THE -BSC FUEL AUX FUEL SYSTEM. (ITEM 018 = O-RING, P/N MS29513-042 (ALTN SAE/AS 29513: ITEM 019 = PLUG ASSMEBLY, P/N HA010-112-11; ITEM 060 = FILLER FLANGE, P/N HA010-118-1 THIS INSTALLATION DOES NOT CHANGE THE EXISTING WEIGHT AND BALANCE FOR THIS AIRCRAFT AND THE EQUIPMENT LIST IS UPDATED TO REFLECT THIS CHANGE.

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