N929PH
Registered owner: U S BANK NA, MN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| PHI Aviation, LLC (HEEA) | Certificate holder | — | Matched by certificate designator |
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.
7 reports on file, 2012-07-29 – 2025-05-25.
Part: SENSOR — INOPERATIVE (APU) · airframe 9,316 hrs
APU FAIL CAUTION LIGHT ILLUMINATED DURING BEFORE LANDING CHECKS.
Part: FIRE DETECTOR — FALSE ACTIVATION (NR 2 ENGINE) · airframe 8,089 hrs
DURING CRUISE FLIGHT ENGINE #2 FIRE LIGHT AND AUDIO WOULD COME ON MOMENTARILY AND THEN EXTINGUISH MULTIPLE TIMES. WE THEN RETURNED TO BASE.
Part: CONTROL UNIT — INOPERATIVE (NR 1 GENERATOR) · airframe 7,818 hrs
DURING CRUISE, #1 AC GENERATOR FAILED AND WOULD NOT RESET. THEN RETURNED TO BASE.
Part: FIRE DETECTOR — INOPERATIVE (APU) · airframe 7,453 hrs
APU FIRE DETECTOR INTERMITTENT IN FLIGHT.
Part: FIRE DETECTOR — INOPERATIVE (APU) · airframe 7,453 hrs
DURING CRUISE FLIGHT, THE APU FIRE AUDIO OCCURRED INTERMITTENTLY (EVERY 2-3 MINUTES) WITH THE APU - OFF (NOT RUNNING). NO SECONDARY OR INDICATIONS OF FIRE WERE PRESENT. CREW PERFORMED REQUIRED ACTIONS PER RFM INCLUDING CLEARING TURNS, AND ELECTED TO RTB TO HOUMA.
Part: FIRE WARNING — ACTIVATED (COCKPIT) · airframe 1,323 hrs
FIRE LIGHT ILLUMINATED FOR 2-3 SECONDS, THEN WENT OUT. REPEATED 3 TIMES. LIGHT WAS OUT APPROX 30 SECONDS BETWEEN REPETITIONS.
Part: FIRE DETECTOR — FALSE ACTIVATION (NR 2 NACELLE) · airframe 396 hrs
DURING CLIMB, FIRE LIGHT WITH AUDIO AND NR 2 ENGINE FIRE LIGHT CAME ON. ON BRINGING NR 2 ENGINE LEVEL TO IDLE FIRE WARNING LIGHT WENT OUT. LANDED AND PUT ENGINE TO FLY BEFORE LANDING, ON LANDING FIRE NR 2 ENGINE LIGHT CAME ON AGAIN. REMOVED NR 2 ENGINE OTBD FIRE DETECTOR AND WIRING HARNESS. INSTALLED PROTECTIVE SHRINK WRAP IAW ENGINEERING INSTRUCTION E92-702-55-991 DATED 7-2-12. REINSTALLED NR 2 ENGINE OTBD FIRE DETECTOR AND WIRING HARNESS. PERFORMED FUNCTION CHECK - CHECKED GOOD. OPS CHECK FLIGHT WAS SUCCESSFUL.