N424RA
Registered owner: DABBLE AVIATION LLC, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
6 reports on file, 2001-08-01 – 2021-11-11.
Part: SPAR CAP — CRACKED (ZONE 600) · airframe 32,603 hrs · 59,607 cycles
CRACK FOUND WHILE PERFORMING SID INSPECTIONS VIA X-RAY ON R/H WING BOTTOM FWD WING SPAR STRUCTURE CLOSE TO THE WING ROOT.
Part: SKIN — CRACKED (ZONE 500) · airframe 32,487 hrs · 59,419 cycles
THE TRAILING EDGE OF THE L/H INBOARD FLAP COVE SKIN WAS FOUND TO BE CRACKED ALONG THE RIVET LINE. AFTER DAMAGED MATERIAL WAS REMOVED, THE HOLE WAS ABOUT 8.5"X2.5" THIS AREA WAS FLUSH PATCHED PER CASA 212 SRM.
Part: SKIN — DENTED (ZONE 300) · airframe 32,487 hrs · 59,419 cycles
DENT FOUND IN THE LOWER SKIN OF THE R/H HORIZONTAL STABILIZER. UPON REMOVAL OF ALL THE DAMAGED MATERIAL, THE HOLE WAS 0.65" IN DIAMETER. REPAIRED BY APPLYING A FLUSH PATCH PER CASA 212 SRM.
Part: FRAME SPLICE — CHAFED (ZONE 100) · airframe 32,487 hrs · 59,419 cycles
AIRCRAFT WAS FOUND TO HAVE CHAFE DAMAGE TO THE R/H CARGO DOOR FRAME BEAM NEAR LOWER SPLICE OF CENTER BEAM SEGMENT. BLENDED CHAFED AREAS, REMOVED FACTORY SPLICE AND FABRICATED A NEW SPLICE TO ENCOMPASS CHAFE DAMAGE. ALL WORK CARRIED OUT IAW CASA SRM APPX II B-4 & B14.
Part: TRANSMITTER — INOPERATIVE (FUEL FLOW) · airframe 2,245 hrs · 1,674 cycles
TROUBLESHOT INOPERATIVE LT ENGINE FUEL FLOW INDICATION. FOUND ROTATING ELEMENT OF INLINE FUEL FLOW TRANSMITTER LOOSE AND SHIFTED FWD. REMOVED FUEL LINE FROM TRANSMITTER OUTLET AND FOUND ROTATING ELEMENT SNAP RING INSIDE FUEL LINE. REMOVED SNAP RING AND CLEARED FUEL LINE. REMOVED FUEL FLOW TRANSMITTER PN 1/2-2-81-306, SN 511086 AND INSTALLED AN OVERHAULED EXCHANGE UNIT. GROUND OPS CHECKED. NO DEFECTS NOTED.
Part: BOLT — BACKED OUT (ENGINE CONTROL)
AN5-4A BOLT IN BOTTOM PIVOT POINT ROD ATTACHMENT BACKED OUT CAUSING LOSS OF ENGINE CONTROL. AN936B516 LOCK WASHER WAS PRESENT.