N339FR
Registered owner: BANK OF UTAH TRUSTEE, UT (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.
8 reports on file, 2019-08-26 – 2024-07-09.
Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 19,062 hrs · 8,445 cycles
REFERENCE LTPR NR 5001326227-0010_AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION OF THE AFT CABIN FLOOR STRUCTURE A CRACK WAS FOUND ON LH SHEAR PLATE BETWEEN FR 69 TO FR 70. REPLACEMENT IS REQIURED. PREFORM REPLACEMENT OF LH SHEAR PLATE IAW-SRM-51-72-11-REV 40 MX ACTION IS ACCEPTABLE.
Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 19,062 hrs · 8,445 cycles
REFERENCE LTPR NR __5001326226-0010__ AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION OF AFT CAB FLOOR STRUCTURE FOUND CRACK ON RH AFT SHEAR PLATE BETWEEN FR 69-70.REPLACEMENT REQIURED, PROFORMED REPLACE MENT OF RH SHEAR PLATE IAW-SRM-51-72-11-REV40.
Part: BATTERY — FAILED (ZONE 200) · airframe 19,062 hrs · 8,445 cycles
REFERENCE LTPR NR 5001326202-0020 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INCOMING CHECKS ON CAPACITY TEST FOUND EPSU BATTERIES 12 WL AND 13WL INOP REPLACEMENT REQUIRED IAW AMM 33-51-38-04 REV 98. REPLACED EPSU BATTERY AND POWER SUPPLY 12WL AND 13WL IAW AMM 33-51-38-04 CONF 00 REV. 98. MX ACTION IS ACCEPTABLE.
Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,062 hrs · 8,445 cycles
REFERENCE LTPR NR 5001326233-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORROSION ON RH AFT DOOR SILL BEAM NUT PLATE HOLE AT FRAME 68 REQUIRES REPAIR AS PER A320NEO SRM 53-41-14-300-001 REV. 40. REPAIRED RH AFT DOOR SILL BEAM NUT PLATE HOLE AT FRAME 68 AS PER A320NEO SRM 53-41-14-300-001 REV. 40.
Part: BEAM — CORRODED (LT AFT DOOR SILL) · corrosion level 2 · airframe 19,062 hrs · 8,445 cycles
REFERENCE LTPR NR 5001326235-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORROSION ON LH AFT DOOR SILL BEAM NUT PLATE HOLE AT FRAME 68 REQUIRES REPAIR AS PER A320NEO SRM 53-41-14-300-001 REV. 40. REPAIRED LH AFT DOOR SILL BEAM NUT PLATE HOLE AT FRAME 68 AS PER A320NEO SRM 53-41-14-300-001 REV. 40.
Part: BATTERY — FAILED (ZONE 200) · airframe 19,062 hrs · 8,445 cycles
REFERENCE LTPR NR 5001326202-0020 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INCOMING CHECKS ON CAPACITY TEST FOUND EPSU BATTERIES 12 WL AND 13WL INOP REPLACEMENT REQUIRED IAW AMM 33-51-38-04 REV 98. REPLACED EPSU BATTERY AND POWER SUPPLY 12WL AND 13WL IAW AMM 33-51-38-04 CONF 00 REV. 98. MX ACTION IS ACCEPTABLE.
Part: OIL SYSTEM — OVERSERVICED (NR 1 ENGINE) · airframe 8,742 hrs · 3,795 cycles
EXPERIENCED FUME EVENT DURING CRUISE. BURNING RUBBER SMELL IN FLIGHT DECK OCCURED 11 MINUTES INTO FLIGHT AND REMAINED UNTIL LANDING. CORRECTIVE ACTION: FOUND ENGINE 1 OIL OVERSERVICED TO 19 QT DRAINED DOWN OIL TO WITHIN SERVICEABLE LIMITS. PERFORMED TSM 05-50-00-810-831-A. INSPECTED RECENT MX ACTIONS AROUND ENGINE 1 FUEL NOZZLES. NO EVIDENCE OF LEAKS NOTED. NO OTHER DEFECTS NOTED AT THIS TIME, REF TSM 05-50-00-810-831-A.
Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 3,272 hrs · 1,392 cycles
R1 DOOR SLIDE DEPLOYED. REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE.