N284DH
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, 2017-08-09 – 2020-08-26.
Part: UNKNOWN — ODOR (CABIN) · airframe 86,247 hrs · 19,324 cycles
FOUL OIL SMELL COMING FROM GASPER VENTS. PERFORMED ENGINE 1 DUE RUN AND B767 AMM 21-00-21 A/C SYSTEM OIL SMOKE/FUME INSPECTION OF A/C PNEUMATIC SYSTEM DUCTS - NO OIL CONTAMINATION FOUND AT THIS TIME. OPERATIONS NORMAL.
Part: LIGHT — FAILED (CABIN) · airframe 85,474 hrs · 19,064 cycles
EMERGENCY LIGHTS FAIL TO ILLUMINATE
Part: FITTING — CORRODED (DOOR) · corrosion level 2 · airframe 85,474 hrs · 19,064 cycles
#2 MDCD LATCH PIN FITTING HAS EVIDENCE OF CORROSION ON INNER BORE
Part: FITTING — CORRODED (DOOR) · corrosion level 2 · airframe 85,474 hrs · 19,064 cycles
#1 MDCD LATCH PIN FITTING HAS EVIDENCE OF CORROSION ON INNER BORE
Part: FITTING — CORRODED (DOOR) · corrosion level 2 · airframe 85,474 hrs · 19,064 cycles
#11 MDCD LATCH PIN FITTING HAS EVIDENCE OF CORROSION ON INNER BORE
Part: SKIN — DENTED (NR 2 COWLING) · airframe 85,474 hrs · 19,064 cycles
#2 ENG INLET COWL LIP SKIN DENTED AT APPROX 5 OCLOCK POSITION
Part: PIN — MISSING (BRAKE SYS) · airframe 82,604 hrs · 17,469 cycles
ON GEAR UP, AN EICAS DISAGREE, RAN QRH TO THREE GREEN NO OTHER MESSAGES, AND LANDED. INSPECTED THE GEAR ASSEMBLY. FOUND THE NR 2 BRAKE ROD ASSEMBLY BROKEN IN HALF AND MISSING FORWARD PORTION AND BRAKE PIN ASSEMBLY. BRAKE ROTATION WITH HARD LINE BROKEN. REMOVED AND REPLACED BRAKE ROD ASSEMBLY IAW AMM 32-11-20, AND 32-41-06. INSTALLED A NEW BRAKE ROD PIN IAW AMM 32-11-20. REMOVED AND REPLACED THE NR 2 BRAKE HOSE ASSEMBLY IAW AMM 32-41-16. OPS CHECKED GOOD, LEAK CHECKED GOOD.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,753 hrs · 16,909 cycles
STATION 1285 FRAME INNER CHORD ADJACENT TO STRINGER 20L FOUND CORROSION ON PREVIOUS BLEND.