N39122
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| WALTER DURAUR | Operator | on 1999-06-20 | 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.
17 reports on file, 1995-05-17 – 1999-02-23.
Part: INDICATOR — MALFUNCTIONED (FUEL QUANTITY)
FUEL QUANTITY INDICATOR HAS EXCESSIVE FRICTION ERROR.
Part: ACTUATOR — FAILED (DROOP BAY)
ACTUATOR WILL NOT ACTUATE.
Earlier reports · 1995–1998 · 15 reports
1998
Part: TRANSCEIVER — MALFUNCTIONED (COCKPIT)
TRANSCEIVER'S MODULATION DISTORTED AT 85 PERCENT MODULATION.
Part: ACTUATOR — STUCK (M/R)
ACTUATOR STUCK ON HIGH SIDE.
Part: DUAL INDICATOR — FAILED (COCKPIT)
DUAL INDICATOR LOADMETER IS INOPERATIVE.
Part: ALTIMETER — CORRODED (COCKPIT)
ALTIMETER CASE LEAKAGE AND CORROSION ON BARO KNOB.
Part: PROBE — LOOSE (TANK UNIT)
TANK UNIT HEAD IS LOOSE FROM TUBE.
1997
Part: GYRO — PRECESSES (COCKPIT DG)
DIR GYRO PRECESSES.
Part: TRANSPONDER — FAILED (COCKPIT)
TRANSPONDER NOT RECEIVED BY GROUND RADAR. PERFORMED PRELIMINARY INSPECTION. FOUND V101 TO HAVE LOW POWER OUT, ADJUSTED V101. NO HELP. REPLACED V101 P/N C2080A. REPAIRED. BENCH CHECK GOOD.
Part: NOZZLE VANES — CRACKED (NR 1)
YNGINE REMOVED DUE TO TURBINE 1750 HOUR INSPECTION. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED AND BOWED BEYOND SERVICEABLE LIMITS ON NR 1 NOZZLE VANES. INSTALLED A NEW NR 1 NOZZLE.
Part: NOZZLE — DEFECTIVE (1ST STG NR 2)
ENGINE REMOVED DUE TO 1750 HOUR INSPECTION. UPON INSPECTION OF TURBINE PARTS NOTED: EXCESSIVE RUNOUT BEYOND SERVICEABLE LIMITS ON #2 NOZZLE 1ST STAGE (.009) AND 2ND STAGE (.006) TIP PATHS. CRACKED BETWEEN DIAPHRAGM AND INNER BAND AS MARKED. INSTALLED A DALLAS AIRMOTIVE OVERHAULED #2 NOZZLE.
1996
Part: TRANSCEIVER — MALFUNCTION (COCKPIT ATC)
LOCK BROKEN. REPLACED BROKEN LOCKING MECHANISM. ALSO REPLACED DEFECTIVE DIODE CR202 THAT CAUSED WEAK SENSITIVITY. ADJUSTED PRESELECTOR FOR PROPER SENSITIVITY. UNIT BENCH CHECK GOOD.
Part: SKID TUBE — MIS MFG (SADDLE)
BOLT HOLE IN TOP OF AFT SKID TUBE SADDLE, WAS NOT LINED UP, WOULD NOT MATCH WITH CROSS TUBE MOUNT HOLE.
Part: BEARING — CRACKED (T/R BLADE)
BEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101.NOTE: SEE MMIR #6826 THROUGH #6835 FOR ADDITIONAL BEARINGS REPLACED.
Part: TRANSCEIVER — DEFECTIVE (COCKPIT)
TRANSCEIVER GOES OFF AND ON INTERMITTENTLY.
1995
Part: TRANSCEIVER — DEFECTIVE (COCKPIT ATC)
ATC UNABLE TO READ IDENT. FOUND EXTRA NUMBERS ON SCOPE WHEN DIALING IN NUMBERS. CLEANED CONTACTS ON ALL WAFER SWITCHES. REPAIRED. FOUND POWER OUT VERY LOW. REPLACED CAVITY OSCILLATOR V101. REPAIRED. FOUND UNABLE TO SWITCH FROM ON TO STANDBY MODE. CLEANED CONTACTS ON ALL WAFERS. REPAIRED. ADJUSTED PULSE WIDTH. BENCH CHECK GOOD.
Part: SUPPORT — REQ REPLACEMENT (SWASHPLATE)
REMOVED TO COMPLY WITH ASB 206-93-74 REV. B (REPLACEMENT OF -109 SUPPORT WITH -113 SUPPORT)