N227HA
Registered owner: WILMINGTON TRUST CO TRUSTEE, 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
EPSU BAT (15WL) FAIL. GROUNDED - YES. REMOVED AND REPLACED EPSU BATTERY (15WL) IAW AMM 33-51-38. BITE TEST OK. OK FOR SBC..
ETOPS - DURING T/C 321-724000-W2-1 FOUND ENG 2 LOWER IGNITER DAMAGED. REMOVED AND REPLACED IGNITER PER AMM 74-21-00. OPS TEST GOOD, OK TO CONTINUE.
SMOKE LAVATORY SMOKE LAV D. FA REPORTED ALL CLEAR. PERFORMED OPERATIONAL CHECK OF THE LAV SMOKE DETECTION PER AMM 26-17-00-710-001-A. OPS CHECK GOOD. NO FAULTS NOTED. A/C OK TO CONTINUE
POSSIBLE BIRD STRIKE DESCENDING BETWEEN 6-5000 FEET. REMOVED & REPLACED RADOME PER AMM 53-15-11. OK FOR SERVICE.
ETOPS - WHILE PERFORMING E1128-321-73-019 FOUND AS11 TUBE B-NUT CROSS THREADED ON #2 ENGINE BURNER PRESSURE (PB) SENSOR. REMOVED & REPLACED AS11 TUBE PER AMM 73-21-23.
ETOPS - ECAM APU AUTO SHUTDOWN ON START ATTEMPT 3 UNSUCCESSFUL START ATTEMPTS. REMOVED AND REPLACED IGNITION UNIT PER A321 AMM 49-41-38 ECB TEST OK OPS CHECK NORMAL A/C OK FOR SERVICE
ETOPS - ECAM AIR ENG 2 BLEED FAULT ON REVERSE THRUST SELECTION ON LANDING. FOUND FAN AIR VALVE ACTUATOR ROD BOLT BROKEN, REPLACED BOLT IN REFERENCE TO AMM 36-11-54-400-802-A, ACCOMPLISHED ENG RUN CHECK PER AMM 71-00-00-860-823-A, NO DEFECTS NOTED ON GROUND, ALERTS EXTINGUISHED, OK TO CONTINUE
ETOPS - AIR ENG 2 ABNORM PR ON THRUST LVR ADVANCE ON TO W/ RTO SYSTEM RESET SUCCESSFUL. FOUND PRESSURE REGULATING VALVE (PRV) FAULTING. REMOVED AND REPLACED PRV PER AMM 36-11-52-000-802-A/400-802-A. OPS AND LEAK CHECK GOOD. OK FOR SVC.
DIV - AIR ENG 2 BLEED FAULT DURING CLIMB. ACCOMPLISHED GVI OF #2 ENG BLEED VALVES. FOUND FAV ACTUATRO ROD BROKEN. REMOVED FAV PER AMM 36-11-54. INSTALLED FAN AIR VALVE ON ENG 2 PER AMM 36-11-54. OPS/BITE/LEAK CHECK GOOD.
ETOPS - DURING VISUAL INSPECTION OF THE THRUST REVERSERS FIRE SEAL AND VAPOR BARRIER SEALS T/C: 321-783200-W3-1, FOUND 2 FIRE SEALS DAMAGED. REMOVED AND REPLACED BOTH FIRE SEALS PER IPC: 78-32-05-75 ITEM NUMBER 240, 350. OK TO CONTINUE SERVICE.
ETOPS - DURING TAXI IN, APU BLEED SELECTED ON TO CONFIRM PACKS 10 MINS AFTER SELECTING ON, OBSERVED AN INTENSE BURING ASPHALT/CHEMICAL ODOR IDENTICAL TO PREVIOUS TEST FLIGHTS. REMOVED #2 RT OZONE FILTER IAW AMM 21-51-41 TO FOM FOUND CONTAMINATED. INSTALLED #2 OZONE FILTER IAW AMM 21-51-41. OPS & LEAK CHKD OK. REMOVED #1 LT OZONE FILTER IAW AMM 21-51-41 TO FOM FOUND CONTAMINATED. INSTALLED #1 LT OZONE FILTER IAW AMM 21-51-41. OPS/LEAK CHKD GOOD. REPLACED RECIRC FILTERS IAW AMM 21-21-41. SECURITY CHKD GOOD. OK FOR SCV. INSP IP CHK VALVE IAW AMM 36-11-41-200-801-A. NO CONTAMINATION, DUCTING GOOD. REINSTALLED DUCTING & IP CHK VALVE. LEAK CHK FAILED. FOUND LEAK AT PRV FWD CLAMP. TIGHTENED #1 ENG PRV CLAMP. RAN ENGINE BLEED 10 MIN. LEAK CHKD OK. ALL OPS & LEAK CHKD GOOD. NO DEFECTS.
ATB - AFTER TAKEOFF PRIOR TO THRUST REDUCTION, BURNING ELECTRICAL AND CHEMICAL SMELL OBSERVED IN THE COCKPIT. TAKEOFF THRUST WAS TOGA. PERFORMED DECONTAINATION OF THE BLEED AIR DUCTS LEVEL C AMM 36-10-00-615-806-A. NO BURNING SMELL WHEN PACKS 1 AND 2 ON AND OFF. CLEARED MIC SHEET. PLACARD REMOVED OK FOR SERVICE
LAV E SMOKE DETECTOR INOP. REMOVED AND REPLACED SMOKE DETECTOR AT LAV E PER AMM 26-17-15-400-807-A.OPS CHECK GOOD OK FOR SERVICE.
ETOPS-ON ARRIVAL DESENDING THRU 12,000 ECAM GEN 2 FAULT. COMPLETE ECAM ACTIONS GEN 2 FAULT STILL ILLUMINATED. STARTED APU. REMOVED AND REPLACED RH IDG IAW AMM 24-21-51-400-803-A UP TO AND INCLUDING STAEP 4. A. (15) (H). 12570/25041, 03/08/24.. NEED TO CONTINUE. ACCOMPLISHED AMM 24/21-51-400-803-A STEP 4B THRU 4F. 13113 3/8/24.. NEED TO CONTINUE AT STEP 4G. REFER TO LOG 1000005/1 FOR OPS CK OF IDG #2 GEN CHG FOR STEP 4G ON. VERIFICATION FLIGHT FOR #2 IDG COMPLETED SATISFACTORY
ETOPS - #1 ENGINE EDP SUCTION LINE FOUND TO HAVE PUNCTURE/LEAKING. REMOVED AND REPLACED #1 ENGINE EDP SUCTION LINE PER AMM 29-11-51-400. LEAK CHECKED, OPS CHECKED. NO DEFECTS NOTED. OK FOR SERVICE.
ETOPS - ENG 1 N1 AND N2 VIB DISPLAY LOST FOR 30 MIN IN FLT, CAME BACK. (SEEMED TO CORRESPOND WITH ENG I OIL SENSOR FAULT ECAM, WHICH IS MEL'D) REMOVED PHMU PER AMM 77-31-01-000-801-AAND INSTALLED PER AMM 77-31-0-400-801-A. RAN EEC OPERATION TEST PER TASK 7 3-21-00-710-807-A. NO FAULTS NOTED ON EV! GROUND SCAN AND SYSTEM TEST. EEC1 CHAN A AND CHAN B, NO FAULTS NOTED. TEST OK. OK FOR SERVICE.
ETOPS - AFTER BOTH ENG STARTS (2&1) GOT ECAM: ENG 2 EIU FAULT. DID QRH RESET PROCEDURE ECAM CLRD. OPS NORM. ACCOMPLISHED BITE TEST OF EIU 1 & 2 PER AMM 73-25-34. NO FAULTS FOUND. OK TO CONTINUE SERVICE. REMOVED AND REPLACED (6KS) SWITCH PER AWM 73-25-34 AS PRECAUTION.
ETOPS - RECIEVED FAULT MESSAGE EIU2-008-ENGINE START FAULT. REMOVED AND REPLACED EIU-2 PER AMM 73-25-34 OPS AND SECURITY CHECK GOOD OK FOR SERVICE
AFTER TOUCHDOWN, LOSS OF BRAKES WITH AUTOBRAKES ON LOW. PERFORM TSM 32-42-00-810-919-A, NO FAULTS PRESENT. PERFORM AMM TASK 32-42-00-710-001-A, ALL RESULTS AS INDICATED IN REFERENCE. OK TO CONTINUE SERVICE.
LAV SMOKE WARNING IN FLIGHT. PERFORMED LAVATORY SMOKE TEST IAW TSM 26-17-00-810-804-A. TEST PASSED, OPS CHECK GOOD. NO DEFECTS NOTED. A/C OK TO CONTINUE.
ETOPS - APU WILL NOT START // REMOVED AND REPLACED EXCITER-IGNITION PER AMM 49-41-38 OPS TEST OK. OK FOR SERVICE
ETOPS - ENG 2 FIRE LOOP B FAULT DISPLAYED NUMEROUS TIMES DURING CRUISE // PERFORMED TSM 26-12-00-810-806-A. MEASURE OHMS 1472 OHMS, VISUAL INSP TERMINAL BLOCK 2WD-D (450VT2). NO DEFECTS NOTED. REMOVED AND REPLACED FIRE LOOP B AT PYLON & REMOVED AND REPLACED FIRE LOOP A AT PYLON OPS CHK GOOD IAW 26-12-16
ETOPS - ENG 2 FIRE LOOP B FAULT CAME ON FOR 30 SECONDS. T/S PER A321 TSM 26-12-00-810-806-A. PERFORMED OP TEST ENG FIRE & OVERHEAT DET & SAME ALL TEST OK. PERFORMED GVI OF ENG 2 FIRE DET SYS IAW ESPM CH 20 & ENG 2. NEED HARNESS FIN 4166KS (DL304822). REMOVED AND REPLACED WIRE HARNESS FIN 4166KS PN 636W5709-505 S/N P770774 PER A321 AMM 26-12-63-000-801. OPS CHECK GOOD.
ETOPS-ANTI-ICE ENGINE 2 VALVE CLOSED. ECAM AND OVERHEAD AMBER FAULT. FAULT DID NOT CLEAR. REMOVED AND REPLACED ENGINE 2 UPPER ANTI-ICE VALVE, PER AMM 30-21-51. OPERATIONS CHECK GOOD. SECURITY AND CONDITION CHECK OK. MESSAGE CLEARED, NO FAULTS NOTED. A/C OK FOR SERVICE.
ETOPS SIGNIFICANT SYSTEM - BTB - ECAM: ENG 2 FADEC SYS FAULT FOLLOWED BY ENG 2 MINOR FAULT OIL CHIP DETECTED. // INSTALLED NEW PHMU ON #2 ENG, CONDITION SAME. RE-INSTALLED ORIGINAL PHMU PER AMM 77-31-01. REMOVED AND REPLACED #2 EEC PER AMM 73-21-01. LAND TEST PASSED PER 22-97-00. CHECKED #2 CHIP DETECTORS, NO METAL FOUND. RAN #2 ENG, NO FAULTS, OK FOR SVC.
AT 1250Z A GARBAGE TYPE ODOR STARTED IN THE CABIN AND INCREASED FOR THE NEXT TEN MINUTES. ONE PASSENGER FELT ILL, AT FIRST, THE SMELL WAS IN CABIN. IT LATER DISAPPEARED. NOTED BY MX. OK TO CONTINUE.