N1258B
Registered owner: SOUTHERN AIRWAYS PACIFIC LLC, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Multi-Aero Inc. (MUIA) | 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.
6 reports on file, 2002-11-14 – 2024-03-29.
Part: MASTER CYLINDER — DEFECTIVE (BRAKES) · airframe 21,790 hrs · 19,111 cycles
LEFT HAND BRAKE INEFFECTIVE. MAINTENANCE REPLACED LEFT HAND MASTER CYLINDER. PERFORMED HIGH SPEED TAXI. OPS CHECKED GOOD
Part: CALIPER — LEAKING (MLG BRAKES) · airframe 21,763 hrs · 19,087 cycles
BRAKE SYSTEM MALFUNCTIONING. RIGHT WHEEL BRAKE APPEARED TO BE STUCK. MAINTENANCE REMOVED RIGHT BRAKE CALIPERS AND PADS. CLEANED, INSPECTED AND REINSTALLED ASSEMBLY. REPLACED LEFT BRAKE CALIPER AND BRAKE DUE TO SLIGHT LEAK. OPS CHECKED GOOD
Part: CONTROL UNIT — SHORTED (ANNUNCIATOR) · airframe 19,639 hrs · 16,940 cycles
SMELL OF SMOKE/ODOR IN COCKPIT AND STANDBY POWER ON ANNUNCIATOR ILLUMINATED
Part: BRAKE SYS — CONTAMINATED (MLG) · airframe 12,995 hrs · 11,618 cycles
CREW REPORTED LOSS OF BRAKING DURING TAXI INTO THE GATE. AIRCRAFT WAS TOWED TO THE GATE. HAD CONTRACT MAINTENANCE PERFORM VISUAL INSPECTION OF SYSTEM WITH NO LEAKAGE OR OBVIOUS DEFECTS. CONTRACT MAINTENANCE PERFORMED BLEEDING OF BRAKE SYSTEM AND PERFORMED OPERATIONAL CHECK WITH CREW WITH SATISFACTORY RESULTS. NO REPORTED ISSUES WITH BRAKES REPORTED PRIOR TO OR SINCE THIS INCIDENT.
Part: WIRE HARNESS — DAMAGED (PROPELLER) · airframe 8,513 hrs · 8,065 cycles
PROPELLER DE-ICE SYS TO BE OPERATING AT 10 AMPS WITH SWITCH SHORTED & CAUSING FUMES. OPERATED SYS & FOUND TO BE RUNNING AT 10 AMPS. PERFORMED TROUBLESHOOTING PROCEDURE IAW 208 MM. REPLACED PROP DE-ICE BRUSHES WITH NEW UNITS, FOUND ONE PROP DE-ICE HARNESS TO BE OPEN. REPLACED ALL THREE DE-ICE HARNESS LEADS WITH NEW UNITS. SYS FUNCTIONS NORMALLY WITH NO DIFFICULTIES. REPLACED PROP DE-ICE SWITCH AS A PRECAUTIONARY MEASURE. SYS OPERATIONS CHECKED GOOD.
Part: WIRE HARNESS — CHAFED (DIRECTIONAL GYRO) · airframe 20 hrs
OPERATOR NOTED NR 2 DIRECTIONAL GYRO CIRCUIT BREAKER POPPING. MAINTENANCE DETERMINED A WIRE BUNDLE ROUTED AROUND THE DATA TRANSFER UNIT (DTU) WAS CHAFING AGAINST THE OUTBOARD CONNECTOR PLUG ON THE DTU. ONE WIRE IN THE BUNDLE WAS FOUND SHORTED AGAINST THE CONNECTOR PLUG. THE WIRE WAS REPAIRED BY INSTALLING AN ENVIRONMENTAL SPLICE IN THE DAMAGED AREA. SPIRAL WRAP WAS INSTALLED AROUND THE WIRE BUNDLE AND THE WIRE BUNDLE WAS RELOCATED AS MUCH AS POSSIBLE TO PREVENT A RECURRENCE OF THE PROBLEM. FUNCTION TEST REVEALED NO FURTHER DEFECTS.