N316FR
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.
17 reports on file, 2020-03-26 – 2023-09-15.
Part: COMPUTER — INOPERATIVE (ZONE 100) · airframe 19,887 hrs · 8,635 cycles
THE AC WAS GROUNDED DUE TO AN SDR REPORTABLE EVENT. DEFECT FOR VENT SKIN VALVE FAULT. PER TSM 21-26-00-810-844-0-A, REMOVED AND REPLACED AEVC IAW AMM 21-26-34-000-001-A. OPS CHECK GOOD. NO FAULTS ON ECAM AT THIS TIME. AC OK FOR SERVICE. ORIGINAL SUBMISSION DATE 09/19/2023
Part: BATTERY — FAILED (ZONE 200) · airframe 18,690 hrs · 8,113 cycles
DISCREPANCY: REFERENCE LOG PAGE LP264465 ITEM #1, AIRCRAFT WAS NOT GROUNDED AND WAS AN OVERNIGHT LINE MX CHECK. EPSU TEST FAULT. CORRECTIVE ACTION: REMOVED AND REPLACED 10WL EPSU BATTERY PER AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS TEST GOOD PER AMM 33-51-00-710-001 TEST PASS.//END//
Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,266 hrs · 7,905 cycles
DISCREPANCY: REFERENCE NR 5001226088-0020 UPON REMOVAL FOR ACCESS ON INSPECTION FOUND 261LG PANEL CORRODED AND REQUIRES REPLACEMENT. CORRECTIVE ACTION: REPAIRED 261LG PANEL AS PER EA# N2-53R-37571 REV. ORIG REV DATE. N/A TASK SUBJECT TO RII. THE EMBODIED REPAIR IS CATEGORY C MAJOR REPAIR AND MUST BE MADE PERMANENT WITHIN 3 MONTHS OF DEFERRAL DATE APRIL 5, 2023. DROP-DEAD DATE WILL BE JULY 5, 2023 AS PER EA #N2-53R-37571 REV. ORIG REV DATA N/A //END//
Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,266 hrs · 7,905 cycles
DISCREPANCY: REFERENCE NR 5001226012-0010 CORROSION ON BEAM Y-254 BETWEEN FR12-FR24 AT FR15 MEASUREMENTS REWORK #1L-31.31MM W=22.56MM D=1.08MM REWORK#2 L-21MM W=2.96MM D=100% OF MATERIAL LOSS AREA FOUND OUT OFF LIMITS NO ALLOWABLE LIMITS IN SRM. CORRECTIVE ACTION: THE PERFORMED REPAIR BY REPLACEMENT ON RAIL AT -Y254 MAJOR AND PERMANENT REPAIR CATEGORY "A" WITH NO REPEAT INSPECTION REQUIRED AS PER AIRBUS RDAF REF. & ISSUE: 81200953/003/2023#A AND LTPR EO-A32F-53-21610-01-FINAL AND FRONTIER EA#N2-53R-37566. TASK SUBJECT TO RII. //END//
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,266 hrs · 7,905 cycles
DISCREPANCY: REFERENCE NR 5001225819-0010 FOUND CORROSION ON SEAT TRACK Y1292 AT FR16-17 MEASUREMENTS L-50MM W=20MM D=0.88MM AREA FOUND OUT OFF LIMITS AS PER SRM TASK 53-11-14-283-007 REV. 35 CORRECTIVE ACTION: REPLACED SEAT TRACK Y1292 AT FR16-17 AS PER SRM 51-72-11-911-01 REV. 35//END//
Part: DOOR SEAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,266 hrs · 7,905 cycles
DISCREPANCY: REFERENCE NR: 5001225799-0010 CORRODED ANCHOR NUT HOLE ON LH AFT PASSENGER DOOR SILL AT FRAME 68. CORRECTIVE ACTION: PERFORMED REPAIR PER A320 NEO SRM 53-41-14-300-001 REV. 35//END//
Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,266 hrs · 7,905 cycles
DISCREPANCY: REFERENCE NR 5001225807-0010 FOUND CORROSION ON BEAM Y-1162.5 FR 68-69 MEASUREMENTS: L=109MM W= 80.6MM D=0.43MM AREA FOUND OUT OF LIMITS AS PER SRM TASK 53-41-14-283-009 REV. 35. CORRECTIVE ACTION: REPLACED BEAM Y-1162.5 FR 68-69 AS PER SRM 51-72-11-911-01 REV. 35. /END/
Part: FMU — DEFECTIVE (NR 2 ENGINE) · airframe 17,780 hrs · 7,697 cycles
ENGINE 2 STALL ECAM. STALL WAS HEARD AND FELTED, 14,000 FEET 340 KNOTS, ECAM WANT AWAY IMMEDIATELY AND ENGINE PARAMETERS NORMAL. REMOVED & REPLACED ENG #2 FMU PER STEP 4.B.(5).(A). OPS CHECK AND LEAK CHECK GOOD.//END//
Earlier reports · 2020–2022 · 9 reports
2022
Part: LIGHT — UNKNOWN (CABIN) · airframe 16,992 hrs · 7,372 cycles
FLOOR LEVEL EMERGENCY EXIT LIGHTS AT AT THE FWD & AFT DOOR EXIT DID NOT ILLUMINATE. PERFORMED OPS TEST OF EMERGENCY LIGHTING, OPS TEST GOOD. REF AMM 33-51-16-860-056-A.
Part: UNKNOWN — ODOR (CABIN) · airframe 16,873 hrs · 7,319 cycles
FA'S REPORT AN UNUSUAL ODOR IN THE MID-AFT AIRCRAFT. PERFORMED INSPECTION OF CABIN FOR EVIDENSE OF ODOR OR SMOKE OR FUME. POST BORESCOPE INSPECTION OF THE NR 2 ENGINE. NO ODOR OR DEFECTS NOTED AT THIS TIME. TSM 71-00-00-810-892-A. ORIGINAL SUBMISSION DATE: 10/10/2022
Part: UNKNOWN — ODOR (CABIN) · airframe 16,832 hrs · 7,302 cycles
APPEARED TO BE FUME EVENT ON DOWN WIND SIDE LANDING PERFORMED INSPECTION CABIM FOR ODOR, SMOKE OR FUME. NO SMOKE OR FUME NOTED AT THIS TOME IAW TSM 05-50-00-810-831-A AC OK FOR SERVICE - LP295768#3 ENGINE#1 RUN - PERFORMED ENGINE#1 IDLE RUN NO DEFECTS NOTED ALL PAREMETERS NORMAL NO FUME IAW 05-50-00-810-831-A; #1 ENGINE#2 RUN REQUIRED - PERFORMED ENGINE IDLE RUN NO DEFECTS NOTED ALL PAREMETERS NORMAL NO FUME EVENT DONE IAW TSM 05-50-00-810-831-A
Part: PITOT TUBE — DIRTY · airframe 16,679 hrs · 7,226 cycles
RTO FOR STANDBY AIRSPEED INDICATOR 20 KTS LESS THAN PF PRIMARY AIRSPEED INDICATOR. PERFORMED CLEANING OF PITOT PROBES IAW 34-10-00-170-004-A AND BITE TEST IF ISIS AMM 34-22-25-740-001A OCF REQUIRED.//END//
2021
Part: FITTING — CRACKED (ZONE 500) · airframe 12,747 hrs · 5,408 cycles
LP156984 ITEM 1, DISCREPANCY: GREEN HYDRAULIC SYSTEM LO PRESSURE. AIR TURN BACK TO DENVER. CORRECTIVE ACTION: FOUND PRESSURE FITTING LEAKING IN #1 ENGINE PYLON. REPLACED FITTING AND HYD LINE, DUE TO BOTH NEEDING TO BE REPLACED AS A SET PER THE IPC (POST MOD). NO LEAKS NOTED DURING LEAK CHECK. TW USED F9TAB1361C CAL DUE 11/2021. REF AMM 29-11-49-000-813-A, 29-11-49-400-813-A AND IPC FIG 29-11-86-51B ITEMS 230A AND 240.
2020
Part: BATTERY PACK — NO TEST (DOOR SLIDE) · airframe 11,241 hrs · 4,737 cycles
DEFECT: EPSU TEST FAILURE. CORRECTIVE ACTION: REMOVED AND REPLACED EPSU BATTERY FOR UNIT (10WL) AND UNIT (13WL). EPSU TEST STILL FAILS. SYSTEM REQUIRES FURTHER TROUBLESHOOTING, REFERENCE AMM 33-51-38. REMOVED AND REPLACED R2 DOOR SLIDE, OPERATIONS CHECK GOOD. T/W F9TAB5827C DUE 9/21. AMM 25-62-44-400-803-A.
Part: SLIDE — NO TEST (L1 DOOR) · airframe 10,465 hrs · 4,395 cycles
DISCREPANCY: L1 DOOR SLIDE FAILED EPSU TEST. DURING OVERNIGHT MAINTENANCE. CORRECTIVE ACTION: REPLACED L1 DOOR SLIDE, REF AMM 25-62-44-000-012-A AND 25-62-44-400-007-A. OPS CHECKS GOOD AT THIS TIME.
Part: FITTING — BUCKLED (HYD SYSTEM) · airframe 9,829 hrs · 4,152 cycles
HYD GREEN RSVR LO LEVEL FOLLOWED BY GREEN PUMP LO PRESSURE, GREEN SYSTEM LO PRESS, PERFORMED QRH PROCEDURES. DECLARED EMERGENCY, NO FURTHER DEFECTS NOTED. UNDER LANDING WEIGHT. - ALSO GRAVITY GEAR EXTENSION PERFORMED W/NO DEFECTS NOTED, ALL 3 GREEN IND. MAINTAINED STEERING TO THE GATE. REPLACED FITTING, LEAK CHECKED, SERVICED & BLED GREEN SYSTEM. RESET MANUAL EXTENSION SYSTEM AND PERFORMED GENERAL VISUAL INSPECTION OF GEAR AND DOORS W/NO DEFECTS NOTED. AMM 20-21-12, 12-12-29, 29-00-00-870-003, 32-00-00-860-003-A
Part: EPSU — FAILED (CABIN) · airframe 9,555 hrs · 3,992 cycles
DISCREPANCY: LP1241800 ITEM 1: DURING OVERNIGHT MAINTENANCE, EPSU SYS TEST FAILED DUE TO EPSU 11WL FAULT. CORRECTIVE ACTION: REMOVED AND REPLACED EPSU 11WL, DUE TO FAULTING PERFORMED EPSU SYS TEST, TEST PASSED. REF AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A. AIRCRAFT RETURNED TO SERVICE BY 0630 HAD A 2054 SCHEDULED DEPARTURE TIME.