N95GK
Registered owner: PDII LLC, NC (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| PDII LLC | Operator | on 2024-02-14 | Operator named in NTSB report |
Accident & incident history
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, 2006-11-18 – 2011-11-06.
Part: STARTER GEN — FAILED (LT ENGINE) · airframe 9,252 hrs · 8,728 cycles
AFTER FUEL STOP IN GRI LEFT ENGINE WOULD NOT SPOOL. CREW CONTACTED MX. MX CONTACTED LOCAL MX TO EVALUATE. LOCAL MX FOUND LEFT STARTER/GENERATOR FAILED. REPLACED STARTER/GENERATOR WITH OVERHAULED UNIT, OPS CHECK GOOD.
Part: STARTER GEN — FAILED (NR 1 ENGINE) · airframe 8,901 hrs · 8,401 cycles
WHEN PREPARING TO DEPART BZN NR 1 ENGINE WOULD NOT SPOOL. TROUBLESHOOTING BY MAINTENANCE FOUND STARTER/GENERATOR HAD FAILED. REPLACED STARTER/GENERATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD.
Part: WIRE — BROKEN (BLEED AIR SYS) · airframe 8,900 hrs · 8,400 cycles
(E81R) DURING DESCENT "A/C FAIL" ANNUNUNCIATOR LIGHT ILLUMINATED AND EMERGENCY PRESSURIZATION SYS ACTIVATED. DURING TROUBLESHOOTING FOUND WIRE E067-P0108B-22 WIRE BROKEN AT BLEED AIR OVERPRESSURE SWITCH CONNECTOR P0108. REPAIRED WIRING AT CONNECTOR AND REPLACED DIRTY WATER SEPARATOR ASSY. COALESCER. ENVIRONMENTAL SYS OPS OK ON GROUND RUN-UP.
Part: WIRE — BROKEN (ACM) · airframe 8,900 hrs · 8,399 cycles
ON DESCENT "AIR CONDITIONING FAIL" ANNUNCIATOR ILLUMINATED & EMERGENCY PRESSURIZATION ACTIVATED. PER ACFT CHECKLIST DESCENDED TO 10,000 FT & CLOSED BLEED AIR SOURCES. LANDING WAS UNEVENTFUL. TROUBLESHOT AND FOUND WIRE BROKEN IN AIR CYCLE TURBINE OVER PRESSURE SWITCH CONNECTOR. REPAIRED BROKEN WIRE. OPERATIONAL CHECK GOOD.
Part: O-RING — FAILED (NLG STRUT) · airframe 8,577 hrs · 8,087 cycles
ON CLIMBOUT FROM MKE CREW NOTICED RUMBLE FROM NOSE AREA FOLLOWED BY A NOSE GEAR UNSAFE INDICATION. CREW DETERMINED NOSE GEAR HAD RELEASED FROM UPLOCK AND EXTENDED. CREW EXTENDED LANDING GEAR AND RETURNED TO MKE. LANDING WAS UNEVENTFUL. STERLING MAINTENANCE COMPLETED GEAR SWING AND FOUND UPLOCK ROLLER ON NOSE LANDING GEAR WAS BARELY ENGAGING UPLOCK HOOK. MAINTENANCE DETERMINED NOSE GEAR STRUT WAS NOT EXTENDING FULLY. WHEN CHECKING STRUT SERVICING MAINTENANCE FOUND HYDRAULIC FLUID IN THE NITROGEN SERVICE SIDE OF STRUT. MAINTENANCE DETERMINED AN INTERNAL SEAL HAD FAILED IN STRUT. MAINTENANCE REMOVED LANDING GEAR AND SENT OUT FOR INSPECTION/SEAL REPLACEMENT. ALL INTERNAL SEALS WERE REPLACED AND NOSE GEAR WAS REINSTALLED. GEAR SWING AND OPS CHECKS WERE GOOD.
Part: CONTROL BOX — FAILED (TRHUST REVERSER) · airframe 8,433 hrs · 7,938 cycles
DURING PREFLIGHT CHECKLIST RUDDER BOOST WOULD NOT TEST. CREW RETURNED TO BLOCK. DETERMINED PROBLEM DUE TO DAU NOT RECEIVING THRUST REVERSER STOWED SIGNAL. FOUND THRUST REVERSER CONTROL BOX FAILED. REPLACED THRUST REVERSER CONTROL BOX.
Part: BRACKET — CRACKED (FUSELAGE)
DURING SCHEDULED AIRFRAME INSPECTION FOUND PN 45A33606-5 AND PN 45A33606-6 CABIN UNDER FLOOR REINFORCING BRACKETS AT CABIN DOOR ENTRANCEWAY CRACKED. SEE SRM 53-10-50-001, FIG 1, SHEET 2 OR 3, ITEMS 29 AND 30. SUSPECT CRACKED FROM FATIGUE, ALSO POSSIBLY FROM PREVIOUS ROUGH CABIN DOOR STEP ASSY HANDLING. AC TECHNICIANS/ INSPECTORS SHOULD INSPECT THIS AREA CAREFULLY DURING SCHEDULED INSPECTIONS ON HIGHER TIME AIRCRAFT, AND/OR AIRCRAFT WITH PREVIOUS HISTORY OPERATED BY CHARTER/AIR TAXI/ FRACTIONAL OPERATORS. (K)
Part: RELEASE CABLE — FRAYED (LT MLG)
DURING SCHEDULE (A) AND (B) INSPECTION FOUND LT MLG EMERGENCY UPLOCK RELEASE CABLE ASSY. SEVERLY FRAYED AND CABLE FUNCTION COMPROMISED AT UPLOCK ATTACH CLEVIS END. THIS SB 32-3200. SB 32-3200 IS A RECOMMENDED SB ONLY, COMPLIANCE RECOMMENDED WHEN CABLE ASSY REPLACEMENT REQUIRED. NO RECORD OF PREVIOUS COMPLIANCE ON THIS AIRCRAFT. (K)