N917R
Registered owner: PADACA GLOBAL LLC, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| North American Air Charter, Inc. (YNOA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
8 reports on file, 2000-02-03 – 2014-10-07.
Part: BUSHING — MIGRATED (TE FLAP) · airframe 7,372 hrs · 2,515 cycles
THE FWD INBD FLAP SPIGOT BUSHING HAS MIGRATED OUT OF THE, GM141-1152-1, RIB. THIS HAS CAUSED AN ELONGATION THAT MEASURES .013 IN ONE DIRECTION. WE HAVE FOUND 2 FLAPS THAT HAVE HAD THIS FAILURE. IN ADDITION TO THIS UNIT WE HAVE ALSO FOUND AND REPAIRED THE SAME PROBLEM ON BD 700-1A11, SERIAL 9358, FLAP PN GM148-1001-34, SN 00349. WE HAVE NOW SEEN THIS IN BOTH THE LT AND RT FWD INBD FLAPS. WE HAVE DETERMINED THIS IS A SIGNIFICANT SAFETY ISSUE ON A MAJOR FLIGHT CONTROL AND CONSIDER THIS A SERIOUS PROBLEM. THE REPAIRS HAVE BEEN ACCOMPLISHED WITH THE ASSISTANCE OF AN FAA DER AND SRPSA.
Part: TUBE — CRACKED (HYD SYSTEM)
ON AUGUST 2, 2006, AC WAS PREPARING TO DEPART AIRPORT. FOLLOWING A SUCCESSFUL NR 1 ENG START, PILOTS NOTICED NR 1 HYD SYSTEM QUANITY DROPPING RAPIDLY A FEW MINUTES AFTER START. PILOTS IMMEDIATELY SHUTDOWN BOTH ENGINES TO INVESTIGATE THE PROBLEM. UPON INSPECTION BY CREW AND MAINT, FOUND CRACKED HYDRAULIC PRESSURE LINE. (K)
Part: WINDSHIELD — CRACKED (COCKPIT)
AC WAS ENROUTE, ON A 91 LEG, PILOTS NOTICED THE RT WINDSHIELD OUTER LAYER CRACKED. THE AC DIVERTED AND LANDED WITH NO PROBLEM. MFG SERVICE CENTER REPLACED THE WINDSHIELD AND AIRCRAFT IS RETURNED TO SERVICE.
Part: PULLEY BRACKET — CORRODED (PAX DOOR)
PULLEY BRACKET FOUND CORRODED.
Part: PULLEY BRACKET — CORRODED (ELEVATOR)
ELEVATOR PULLEY BRACKET FOUND CORRODED.
Part: SUPPORT FITTING — CRACKED (FUSELAGE)
FRAME STRUT SUPPORT FOUND CRACKED AT FUSELAGE STATION 738, LONGERON 17. FRAME STRUT SUPPORT REPLACED. (M)
Part: SUPPORT FITTING — CRACKED (FUSELAGE)
FRAME STRUT SUPPORT FOUND CRACKED AT FUSELAGE STATION 370, LONGERON 17. FRAME STRUT SUPPORT REPLACED. (M)
Part: SUPPORT FITTING — CRACKED (FUSELAGE)
FRAME STRUT SUPPORT FOUND CRACKED AT FUSELAGE STATION 370, LONGERON 17. FRAME STRUT SUPPORT REPLACED. (M)