N336FR
Registered owner: UMB BANK NA 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.
7 reports on file, 2022-10-10 – 2024-04-12.
Part: DOOR SILL — CORRODED (LT DOOR) · corrosion level 2 · airframe 18,413 hrs · 8,209 cycles
AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFTER DVI CABIN FLOOR STRUCTURE FOUND CORROSION ON LH DOOR SILL ATTACHMENT HOLES, REPAIR IS REQUIRE AS PER A320N SRM 53-41-14-300-001 REV. 39. REPAIRED LH DOOR SILL ATTACHMENT HOLES AS PER A320N SRM 53-41-14-300-001 REV. 39.
Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,413 hrs · 8,209 cycles
REFERENCE LTPR NR 5001313278-0040 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFTER DVI CABIN FLOOR STRUCTURE FOUND CORROSION ON RH DOOR SILL ATTACHMENT HOLES, REPAIR IS REQUIRE AS PER A320N SRM 53-41-14-300-001 REV. 39. REPAIRED RH DOOR SILL ATTACHMENT HOLES AS PER A320N SRM 53-41-14-300-001 REV. 39 MX ACTION IS ACCEPTABLE.
Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 18,413 hrs · 8,209 cycles
REFERENCE LTPR NR 5001313278-0020 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFTER DVI CABIN FLOOR STRUCTURE AFT ENTRANCE; LH SHEAR PLATE FOUND CRACK & REQUIRE REPLACEMENT AS PER A320N SRM 51-72-11 REV. 39 REPLACED LH SHEAR PLATE AS PER SRM A320N 51-72-11 REV. 39 MX ACTION IS ACCEPTABLE.
Part: SEAT TRACK — CORRODED (FRMS 12-21) · corrosion level 2 · airframe 18,413 hrs · 8,209 cycles
DISCREPANCY: REFERENCE LTPR NR 5001313336-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFTER DVI CABIN FLOOOR STRUCTURE BTW FR12 & FR21 BEAM Y503.2 FOUND WITH HEAVY CORROSION & REPLACEMENT IS REQUIRED AS PER A320N SRM 51-72-11 REV. 39. CORRECTIVE ACTION: REPLACED FLOOR BEAM (TRACK) BETWEEN FR12 & FR16 ALONG Y503.2 AS PER A320N SRM 51-72-11 REV. 39. MX ACTION IS ACCEPTABLE.
Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 18,413 hrs · 8,209 cycles
AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING EPSU BATTERIES CAPACITY TEST 13WL FAILED. REPLACEMENT REQUIRED I.A.W. CMM 33-51-07 REV. 05. REPLACEMENT OF EPSU (13WL) BATTERY PERFORMED I.A.W. AMM 33-51-38-04 CONF 00 REF 97.
Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 18,413 hrs · 8,209 cycles
AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING EPSU BATTERIES CAPACITY TEST 11WL FAILED. REPLACEMENT REQUIRED I.A.W. CMM 33-51-07 REV. 05. REPLACEMENT OF EPSU (11WL) BATTERY PERFORMED I.A.W. AMM 33-51-38-04 CONF 00 REF 97.
Part: PUMP — LEAKING (FUEL SYSTEM) · airframe 13,086 hrs · 5,861 cycles
CLEAR FLUID LEAKING FROM UNDER #1 ENGINE. CORRECTIVE ACTION: REMOVED MAIN FUEL PUMP REF AMM 73-11-05-000-801A. INSTALLED NEW PUMP REF AMM 73-11-05-400-801A. LEAK CHECK GOOD AT THIS TIME.