N901BC
Registered owner: AVIATION INVENTORY RESOURCES INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| IBC AIRWAYS, Inc. (OZCA) | Certificate holder | — | Matched by certificate designator |
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.
6 reports on file, 1997-09-30 – 2023-02-07.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,225 hrs · 55,187 cycles
DURING CRUISE, HYD PUMP TURNED ON & NO MAIN ACCUM PRESS INCREASED. RETURNED TO MIA. FOLLOWED QRH. HYD CWP LIGHT ILLUM. R/R MAIN HYD RES. PERFORMED AIR BLEED SYS AT HYD SYS IAW 29-00-00 OPS & LEAK CHECK SAT. TAXI OUT, HYD PUMP MULTIPLE TIMES PER MINUTE: PRESSURE IN MAIN RES DECREASE FASTER THAN NORMAL. HYD FLUID QTY DID NOT CHANGE. R/R HYD PUMP IAW 29-00-00 OPS & LEAK CHECK SAT. PRESS IN MAIN RES DECREASE FASTER THAN NORMAL, EMERG RES DECREASED. R/R MAIN & EMER ACCUM IAW 29-00-00 OPS & LEAK CHECK SAT. MAIN ACCUM DROPPING PRESS BELOW 2000 PSI PUMP CYCLE 6-8 TIMES DURING TAXI FROM RAMP - RWY. INSPECTED HYD SYS, FOUND HAND PUMP SELECT VALVE OUT OF POSTION. OPS CHECKED ON MAIN ACCUM IAW FAULT ISOLATION 29-10-00-01 PAGE 7 OF MM 29-20-15-04.
Part: CLAMP — CRACKED · airframe 46,181 hrs · 54,535 cycles
DURING TO/O ROLL @ V1, PLANE DISPLAYED HIGH TEMP + LOW PROP OIL PRESSURE IN #2 ENG PROP RPM DROPPED, ENGINE SHUTDOWN. COMPLIED W/QRH, RETURNED TO LAND AT MYNN. ON INVESTIGATION FOUND THAT THE HP BLEED LINE V-BAND CLAMP FAILED P/N 12J63-125 AT THE RETAINER SEGMENT WHICH CAUSED THE HP BLEED LINE TO OPEN UP AND ALLOW BLEED AIR LOSS TO CAUSE THE SHUTDOWN OF THE ENGINE.
Part: PROPELLER — LOW PRESSURE (NR 1) · airframe 45,567 hrs · 54,195 cycles
DURING CRUISE FLIGHT AT 13000, WE HAD PROP OIL PRESSURE LOW ON #1 ENGINE. PROCEEDED ACCORDING TO QRH PG E3-6
Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 45,377 hrs · 54,049 cycles
RIGHT TAIL PIPE HOT WARNING IN FLIGHT. INSPECTED RT ENG. FOUND LOOSE CLAMP ON LOW PRESS BLEED LINE. TORQUED CLAMP IAW MM. PERFORMED OPERATIONAL CHECK OF SYS. OPERATIONAL CHECKED SATISFACTORY IAW MM. COMPLIED WITH PARAGRAPH C OF AIRWORTHINESS DIRECTIVE 2006-18-12.
Part: SWITCH — FAILED (MLG)
REF: FLIGHT LOG PG 1341. LEFT GEAR LIGHT DID NOT SHOW DOWN AND LOCK AND WOULD NOT RETRACT EITHER. TROUBLESHOT SYSTEM AND FOUND DIRTY CONTACT ON LEFT GEAR DOWNLOCK MICROSWITCH. CLEANED MICROSWITCH, RETRACTED GEAR SEVERAL TIMES, AND CHECKED EMERGENCY MANUAL EXTENSION. ALL SYSTEMS FOUND TO BE WORKING CORRECTLY PER CE MM, SECTION 4-1.
Part: SKIN — CRACKED (WING NACELLE)
MID-WAY BETWEEN FORWARD AND AFT SPAR UNDER NACELLE SKIN INBOARD OF NACELLE AUXILIARY FUEL TANK FOUND CRACKS IN WING SKIN. WOULD NOT HAVE BEEN FOUND UNLESS SKIN OVER WING LOCKER AND AUXILIARY FUEL TANK WAS REMOVED FOR REPAIR. NO ACCESS.