N308FR
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, 2018-10-15 – 2022-11-30.
Part: THRESHOLD — CORRODED (L2 DOOR) · corrosion level 2 · airframe 18,393 hrs · 8,034 cycles
L2 THRESHOLD HAS CORROSION AROUND FASTENER HOLE AND CORROSION ON ONE FASTENER HEAD. REPAIRED L2 DOOR SILL IAW A-320 NEO SRM 43-41-14-283-002 AND SRM 53-41-14-300-001 NO FURTHER ACTION REQUIRED. (REPAIR CATEGORY A)
Part: SHEAR WEB — CRACKED (ZONE 100) · airframe 18,393 hrs · 8,034 cycles
AFT WET AREA, LEFT SHEAR WEB CRACKED. REMOVED AND REPLACED LEFT SHEAR WEB AT AFT WET AREA IAW SRM 51-72-11-911-001. REMOVED AND REINSTALLED VOR ANTENNA CABLE SYSTEM #2 AT AFT WET AREA IAW ESPM 20-33-22-02.
Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,393 hrs · 8,034 cycles
R2 DOOR SILL AFT FASTENER HOLE CORRODED. REPAIRED R2 DOOR SILL IAW A-320 NEO SRM 43-41-14-283-002 AND SRM 53-41-14-300-001 NO FURTHER ACTION REQUIRED. (REPAIR CATEGORY A)
Part: SHEAR WEB — CRACKED (ZONE 100) · airframe 18,393 hrs · 8,034 cycles
AFT WET AREA, RIGHT SHEAR WEB CRACKED, LIGHT CORROSION ON LOWER SURFACE AND CORROSION AROUND FASTENER HOLE. REMOVED & REPLACED AFT R/H SHEA WEB IAW A320 SRM 51-72-11-911-001A.
Part: SEAT TRACK — CORRODED (FRMS 16-18) · corrosion level 2 · airframe 18,393 hrs · 8,034 cycles
FWD WET AREA, SEAT TRACK WAS CORRODED ON UPPER FLANGE FRAMES 16-18. REMOVED & REPLACED IAW SRM 51-74-00, 51-42-11, 51-44-11, ESPM 20-33-44-01.
Part: PIPE — LEAKING (HYD SYSTEM) · airframe 17,029 hrs · 7,393 cycles
DISCREPANCY: REFERENCE LP236656; LOSS OF GREEN HYDRAULIC PRESSURE AFTER TAKE OFF. PERFORMED LANDING GEAR GRAVITY DROP ENGINE #1 HYDRAULIC PUMP CAVEATTED DUE TO HYDRAULIC LEAK - REMOVED AND REPLACED HYDRAULIC PUMP IAW AMM 29-11-51-400-808-AC. LP236657 HYDRAULIC PIPE AT FORWARD SECTION OF THE #1 ENGINE PYLON WILL NOT BREAK TORQUE SUSPECTED CROSS THREADED P/N D290208380000 6" PIPE THAT ATTACHES TO THE A320NEO - LEAP - BYPASS VALVE FWD SECTION - REMOVED AND REPLACED ALONG WITH CONNECTION REPLACED PIPE AND CONNECTION REF AMM 29-11-49-400-813 - TFU A320NEO - HYDRAULIC PIPE DAMAGED AT FWD PYLON REF:29-11-00-018 REPORTED IN AC S/N 06642 TO 08025
Part: PIPE — LEAKING (ZONE 400) · airframe 17,029 hrs · 7,393 cycles
DISCREPANCY: REFERENCE LP236654 LOSS OF GREEN HYDRAULIC PRESSURE AFTER TAKE OFF. PERFORMED LANDING GEAR GRAVITY DROP ENGINE #1. REFERENCE LP236656 HYDRAULIC PUMP CAVEATTED DUE TO HYDRAULIC LEAK - CORRECTIVE ACTION: REFERENCE LP 236656 REMOVED AND REPLACED HYDRAULIC PUMP IAW AMM 29-11-51-400-808-AC. DISCREPANCY: REFERENCE LP236657 HYDRAULIC PIPE AT FORWARD SECTION OF THE #1 ENGINE PYLON WILL NOT BREAK TORQUE SUSPECTED CROSS THREADED P/N D290208380000 6" PIPE THAT ATTACHES TO THE A320NEO - LEAP - BYPASS VALVE FWD SECTION - CORRECTIVE ACTION: REFERENCE LP 236657 ITEMS 2 REMOVED AND REPLACED ALONG WITH CONNECTION REPLACED PIPE AND CONNECTION REF AMM 29-11-49-400-813 - TFU A320NEO - HYDRAULIC PIPE DAMAGED AT FWD PYLON REF:29-11-00-018 REPORTED IN AC S/N 06642 TO 08025*****SUPPLEMENTAL CORRECTION FOR THE DUPLICATE OF F3LA2022063000066. NEW UNIQUE CONTROL # IS F3LA2022063000067******
Part: FUEL LINE — LEAKING (ZONE 400) · airframe 5,716 hrs · 2,366 cycles
DISCREPANCY: REFERENCE LOG PAGE LP1133184 ITEM 1, FOUND EVIDENCE OF FUEL LEAK FROM DRAIN MAST NR 2 ENGINE. CORRECTIVE ACTION: REMOVED FUEL TUBE BETWEEN FUEL PUMP AND MAIN HEAT EXCHANGER REFERENCE 72-00-00-17A-530A-C. INSTALLED REFERENCE 72-00-00-17A-710AC. TWF9TAB1100C DUE 10-18 AND TWF9TAB2944C DUE 05-19 ENGINE NR 2.