N225NE
Registered owner: 2/25/94 LLC, MA (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.
21 reports on file, 2019-12-23 – 2026-03-30.
Part: FUEL CAP — LEAKING · airframe 102,458 hrs · 16,695 cycles
AFTER PASSING 10,000 FT., INFORMED FROM CABIN OF SLIGHT FUEL LEAK IN OVERWING FUEL CAP. RT WING LEAK INCREASED AT 310. DECLARED EMERGENCY, DUMPED 24.5K FUEL, RETURN TO PGUA.
Part: ANNUNCIATOR — INOPERATIVE (AUTOTHROTTLE) · airframe 102,322 hrs · 16,665 cycles
AT CRUISE AUTOTHROTTLE AND AUTOPILOT DISCONNECTED. AUTO THROTTLE WOULD NOT RE-ENGAGE. AUTOPILOT L AND C INOP. R AUTOPILOT WORKED. LEFT AND FO FLIGHT DIRECTORS INOP. CAPT HEADING BUG INOP. CAPT SPEED BUG INOP. CAPT ALTITUDE SEL INOP.
Earlier reports · 2019–2025 · 19 reports
2025
Part: REGULATOR — LEAKING (ZONE 200) · airframe 101,362 hrs · 16,435 cycles
AT 10,000 MSL, CREW O2 QTY DROPPED TO 70 PSI
2024
Part: SKIN — CORRODED (ZONE 100) · airframe 100,788 hrs · 16,314 cycles
CORROSION FOUND ON FUSELAGE SKIN AND STRINGER 36R BETWEEN STA 1175 - 1197+22 AFT CARGO
2022
Part: PSU — SPARKS (SEAT 14KJ) · airframe 99,871 hrs · 16,050 cycles
FLIGHT ATTENDANT STATED THAT SPARKS AND A BURNING ODOR HAD BEEN OBSERVED AT THE PSU AREA ABOVE SEAT 14 KJ. INSPECTED AND FOUND A 3 WIRE BUNDLE OF WHAT I ESTIMATE TO BE 22 TO 24 GAUGE WIRE. ONE WIRE IN THE BUNDLE HAD SHORTED BY CONTACT WITH A FASTENER HEAD ABOVE THE PLASTIC COVERING OF THE OXYGEN MASKS,
Part: WIRE HARNESS — BURNED (ZONE 100) · airframe 100,464 hrs · 16,192 cycles
DURING THE COMPLIANCE OF THE AD 2007-16-18 (F) AND S/B 767-25-0376 REV 2 WERE FOUND POWER DRIVE UNITS (PDU) WIRE BUNDLES BURNT IN THE FWD CARGO COMPARTMENT CARGO HANDLING SYSTEM.
Part: NONE — NONE · airframe 100,067 hrs · 16,093 cycles
DURING THE DAILY CHECK MAINTENNANCE FOUND BATTERY PACK INOP. MX REMOVED AND REPLACE THE POWER SUPPLY M730. OPS CHECK GOOD PER AMM 33-51-07. SEE LOG PAGE 37640.
Part: NONE — NONE · airframe 100,067 hrs · 16,093 cycles
EMERGENCY LIGHT INOP AT RIGHT SIDE. REMOVED AND REPLACED M730 POWER SUPPLY BATTERY PACK IAW 33-51-01. OPS CHECK GOOD.
2021
Part: NONE — NONE · airframe 99,721 hrs · 16,024 cycles
LEFT SIDE "L" WING SLIDE AFT DOOR SIDE (L396, L645, L397) EMERGENCY EXTERIOR LIGHT INOP. MX REPLACED THE BATTERY PACK TO M738 POWER SUPPLY MODULE IAW AMM 33-55-07-201. OPS CHECK NORMAL.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 99,520 hrs · 15,982 cycles
EMERGENCY LIGHTS INOP FOR GROUPS ZONE 3 CABIN, L4 R1 EXIT LIGHTS, LEFT EXTERIOR AFT, LEFT EXTERIOR FORWARD, 1L, 1R EXIT SIGNS, AND OVERVIEW EXIT SIGNS. MX MECHANIC R&R THE POWER SUPPLY BATTERY PACKS (M734, M1210,M738,M736, M1208 AND M1209) PER AMM 33-51-21. OPS CHECK GOOD.
Part: RELIEF VALVE — FAILED · airframe 99,375 hrs · 15,953 cycles
DEPARTED FROM SPJC WITH A CREW OF TWO (PILOTS) AND NO PASSENGERS UNDER DAY TIME FLIGHT CONDITIONS. THE FLIGHT CREW REPORTED DURING CLIMB TO FL 380 THEY ENCOUNTERED AN EICAS STATUS MESSAGE CABIN ALT AUTO 2 MESSAGE. THE FLIGHT CREW SELECTED AUTO 1. THEY CONTINUED THE FL 380, WITH FOUR MINUTES OF BEING AT FL 380 THEY WERE ALERTED TO EICAS MESSAGE: CABIN ALTITUDE, AS WELL AS CABIN ALT DISCREET LIGHT. THE FLIGHT CREW DONNED THEIR O2 MASK AND PERFORMED THE QRH PROCEDURES FOR THE INDICATED WARNING. THE FLIGHT CREW BEGAN AN EMERGENCY DESCENT FOR THE ALERT. ATC WAS NOTIFIED AND THE AIRCRAFT RETURNED TO SPJC TO AN UNEVENTFUL LANDING.
2020
Part: DISPLAY — INOPERATIVE (EICAS) · airframe 99,342 hrs · 15,942 cycles
UPPER EICAS DISPLAY IS INOP.
Part: MICROPHONE — STUCK (CAPTAIN'S) · airframe 99,342 hrs · 15,942 cycles
CAPTAIN'S HAND MIKE BECAME STUCK IN THE TRANSMITTING POSITION. HAND MIKE WAS UNPLUGGED TO RESOLVE THE IMMEDIATE ISSUE.
Part: VIEW PORT — INOPERATIVE (DOORS) · airframe 99,336 hrs · 15,938 cycles
L1 & R1 DOOR VIEW PORTS ARE INOPERATIVE.
Part: DIMMER — INOPERATIVE (FLOOD LIGHT) · airframe 99,336 hrs · 15,938 cycles
CAPTAIN'S FLOODLIGHT CONTROLLER IS INOPERATIVE.
Part: ANTENNA — INOPERATIVE (ZONE 100) · airframe 99,336 hrs · 15,938 cycles
LEFT COMM INOPERATIVE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,335 hrs · 15,937 cycles
NUMEROUS OVERHEAD PANEL INTEGRAL BACKLIGHTING AREAS ARE INPOPERATIVE.
Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 99,335 hrs · 15,937 cycles
LEFT HAND AFT EMERGENCY LIGHT BATTERY WILL NOT HOLD A CHARGE.
Part: MICROPHONE — INOPERATIVE (COCKPIT) · airframe 99,335 hrs · 15,937 cycles
FIRST OFFICER'S HAND MIC IS INOPERATIVE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,335 hrs · 15,937 cycles
LH MIDDLE EMERGENCY EXIT LIGHTS ARE INOPERATIVE.
2019
Part: INDICATOR — INOPERATIVE (FUEL QTY) · airframe 99,331 hrs · 15,934 cycles
FUEL QUANTITY SYSTEM DISPLAYED ON PREFLIGHT EICAS CHECK. TROUBLESHOT DOWN TO INDICATOR FAILURE, REMOVE AND REPLACE THE FUEL QUANTITY INDICATOR. THE OPERATIONAL CHECK WITH THE OEM MANUAL IS GOOD.