N330KW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Evergreen Helicopters International, Inc. | Operator | on 2007-02-28 | Operator named in NTSB report |
Accident & incident history
Operated by Evergreen Helicopters International, Inc. (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
10 reports on file, 2016-06-18 – 2018-10-05.
Part: REINFORCEMENT — CRACKED (ZONE 200) · airframe 816 hrs · 10,098 cycles
CRACKS WERE DISCOVERED IN THE MGB ATTACH REINFORCEMENT AT FRAME 3855. THE MAXIMUM CRACK LENGTH IS APPROXIMATELY 3.0 INCHES IN THE VERTICAL LEG OF THE FITTING. REF SRM TABLE 11, FIGURE 17, ITEM 18 P/N 330A-22-9701-22. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRENTLY IN WORK. ONCE THE REPAIR IS COMPLETED, SUPPLEMENTAL INFORMATION MAY BE ADDED TO THIS SDR. SUPPLEMENTAL INFORMATION- REPAIR ACCOMPLISHED IAW EO2018043 REV B, AQRD EO-930736 REV IR, SAS-932736 REV A, AND FAA FORM 8110-3 D/N 932736 DATED 14JAN2019.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 816 hrs · 10,098 cycles
WHILE PERFORMING A P2 INSPECTION, CORROSION WAS DISCOVERED ON THE FLOORBEAM END CAP IN TWO LOCATIONS AT FRAME 5295. THE CORROSION REMOVAL RESULTED IN A MAXIMUM MATERIAL LOSS IN THE PRIMARY STRUCTURE OF 0.035 INCHES IN DEPTH. TECHNICAL DATA PACKAGE PR2018023 WAS CREATED TO PROVIDE GUIDANCE FOR REPAIR OF THE PRIMARY STRUCTURE USING AQRD ERO-931486 AS APPROVED REPAIR DATA. ONCE THE REPAIR IS COMPLETED, SUPPLEMENTAL INFORMATION MAY BE ADDED TO THIS SDR. SUPPLEMENTAL INFORMATION - FLOORBEAM REPAIR ACCOMPLISHED IAW AIRLIFT TDP PROJECT PR2018032 REV B,ERO-931486A,AND FAA 8110-3 NUMBER 931486A ON FILE WITH AIR CARRIER. THIS INFORMATION WILL COMPLETE THIS SDR.
Part: BRACKET — CORRODED (M/R BLADE) · corrosion level 3 · airframe 9,687 hrs · 10,930 cycles
DURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.
Part: BRACKET — CORRODED (M/R BLADE) · corrosion level 3 · airframe 9,687 hrs · 10,930 cycles
DURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.
Part: BRACKET — CORRODED (M/R BLADE) · corrosion level 3 · airframe 9,687 hrs · 10,930 cycles
DURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.
Part: BRACKET — CORRODED (M/R BLADE) · corrosion level 3 · airframe 9,687 hrs · 10,930 cycles
DURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 9,687 hrs · 10,930 cycles
DURING AN AGING INSPECTION, AREAS OF CORROSION WERE FOUND ON THE LT DECK ANGLE.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,687 hrs · 10,930 cycles
DURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE MAIN FRAME OF STRUCTURE AT JACK SUPPORT.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,687 hrs · 10,930 cycles
DURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE UPPER ANGLE FORWARD AND REAR.
Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,687 hrs · 10,930 cycles
DURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE UPPER ANGLE BRACKET.