N723FR
Registered owner: ALC A321 8640 LLC, DE (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.
9 reports on file, 2019-09-09 – 2024-05-31.
Part: SHEAR PLATE — CRACKED (FRM 69) · airframe 15,584 hrs · 6,898 cycles
AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. AFT CABIN R/H LATERAL SHEER PLATE CRACKED AT FR 69. REMOVED AND REPLACED AFT CABIN L/H LATERAL SHEAR PLATE IAW A321 SRM 51-72-11-911-001. MX ACTION IS ACCEPTABLE.
Part: SHEAR PLATE — CRACKED (FRM 69) · airframe 15,584 hrs · 6,898 cycles
REFERENCE AIRBORNE/PEMCO N/R 15334.0295 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. AFT CABIN L/H LATERAL SHEER PLATE CRACKED AR FR 69. AFT CABIN L/H LATERAL SHEAR PLATE DAMAGED REMOVED AND REPLACED IAW A321 SRM 51-42-11. APPLIED TOP COAT IAW A321 SRM 51-23-11 AND APPLIED C.I.C IAW A321 SRM 51-23-12. ACCOMPLISHED OP TEST OF VOR #2 IAW A321 AMM 34-55-00-740-008-A. MX ACTION IS ACCEPTABLE. /END/
Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 15,510 hrs · 6,861 cycles
EPSU TEST FAILED, EPSU BATTERY 11WL FAULT. THIS FAILURE WAS DURING OVERNIGHT MAINTENANCE AND DID NOT CAUSE A FLIGHT DELAY. REPLACED BATTERY EPSU 11WL. EPSU TEST PASS. AMM 33-51-3R-400-002-A./END/
Part: CARRIAGE — STUCK (TE FLAP SYS) · airframe 10,473 hrs · 4,559 cycles
ECAM F/CTL FLAPS LOCKED, LESS THAN FLAPS ONE, QRH PROCEDURES APPLIED INCREASED APPROACH SPEED. EMERGENCY DECLARED. PERFORMED TSM 27-51-00-810-818-A STEP # 1 AND FOUND FLAP CARRIAGE REQUIRED LUBE LUBRICATED L/H AND R/H FLAP CARRIAGES IAW AMM 12-22-27-640-004-A. AC IS OK FOR SERVICE. PERFORMED TSM 27-51-00-810-818-A STEP #1 NO DEFECTS NOTED AT THIS TIME. REPLACED R/H INBOARD SEAL IAW AMM 57-55-11-960-801-A.
Part: CONTROL LEVER — INOPERATIVE (MLG) · airframe 6,459 hrs · 2,792 cycles
LGCIU 1 FAULT. LANDING GEAR WOULD NOT EXTEND, USED GRAVITY GEAR EXTENSION PER QRL. REMOVED AND INSTALLED LANDING GEAR NORMAL CONTROL LEVER. OPS CHECK GOOD. REF TSM 32-31-00-810-809-A AND AMM 32-31-11-400-001-A.
Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 4,792 hrs · 2,017 cycles
DISCREPANCY: EXIT LIGHT AT 4R DOES NOT ILLUMINATE. CORRECTIVE ACTION: FOUND EMERGENCY LIGHT NOT CONNECTED TO WIRING. RECONNECTED EXIT LIGHT 4R AND OPS CHECK GOOD REF AMM 25-23-49-400-010-A. AMM 33-51-00-710-804A
Part: TRIM SYSTEM — BINDING (STAB) · airframe 3,648 hrs · 1,554 cycles
STAB TRIM BINDING // PERFORMED OPERATIONAL TEST OF LOGISTICS ACTUATION ELAC 1&2 & SEC STANDBY POWER SUPPLY & ABILITY OF SEC 1&2 TO ACHIEVE PITCH CTL & ABILITY OF SIDE STICK PRIORITY FUNCTION, OPS CHECKS GOOD. A/C OK FOR SERVICE PER E/C 279000-05-1, WO# 394380 AMM 27-96-00-710-018-A.
Part: OXYGEN MASK — BROKEN (FIRST OFFICER'S) · airframe 2,945 hrs · 1,412 cycles
FIRST OFFICER`S OXYGEN MASK HAS A BROKEN CONNECTOR TO HOSE. SWAPPED THE FIRST OFFICER`S OXYGEN MASK WITH 4TH OBSERVER`S.
Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 2,651 hrs · 1,102 cycles
CAPTAINS O2 MASK MAIN HOSE CAME OFF DURING PREFLIGHT SYSTEM CHECK. SWAP PILOTS O2 MASK W/4TH OBSERVER MASK OP CHECKS NORMAL AIRCRAFT OK TO CONTINUE. 4TH OBSERVERS O2 MASK INOP. DEFERRED PER MEL 25-11-07A CT# 1154512 DUE DATE 07-07-2020.