N112AE
Registered owner: PETTY MICHAEL C, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SIMMONS AIRLINES | Operator | on 1995-07-05 | Operator named in NTSB report |
Accident & incident history
Operated by SIMMONS AIRLINES (per NTSB report)
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, 1995-02-24 – 1996-01-30.
Part: HUB — CRACKED (LT PROP)
LAW - DURING NDT HUB INSPECTION IN SHOP, PROPELLER (S/N DRG/1538/88) THE HUB (P/N 66714200 S/N 108603) INDICATED A CRACK IN THE MOUNTING FACE AREA OUTBOARD OF NR 9 BOLT INSERT. THE HUB WAS REMOVED FROM SERVICE. (M)
Part: FIRE CNTRL UNIT — MALFUNCTIONED (NR 2 ENGINE)
DFW - FLT 3633 - AFTER TAKEOFF, NR 2 ENGINE WARNING ACTIVATED. CREW RESPONDED BY PULLING THE T-HANDLE AND BLOWING A FIRE BOTTLE, THEY DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. THE FIRE LIGHT HAD EXTINGUISHED AND NO EMERGENCY EVACUATION WAS PERFORMED. MAINTENANCE INITIAL INSPECTION SHOWED NO SIGN OF FIRE. REPLACED FIRE BOTTLE AND SQUIBB AND FIRE CONTROL UNIT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE)
DFW - FLT 3511 - AFTER TAKEOFF, NR 2 ENGINE GIVES FALSE WARNINGS ON BOTH HANDLE AND CAPTAIN'S WARNING PANEL. AIRCRAFT TURNED BACK. MAINTENANCE INSPECTED AND REPLACED ENGINE FIRE LOOP. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY — DISCHARGED (BATT COMPT)
DFW - FLT 3946 - EMERGNECY POWER LIGHT ILLUMINATED. AIRCRAFT TURNED BACK TO DFW. REMOVED AND INSTALLED EMERGENCY BATTERY. OPERATIONS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
Part: ECU — MALFUNCTIONED (LT ENGINE)
MQB - FLT 3944 - AIR TURN BACK - AFTER SETTING CTOT, THE LEFT ENGINE CONTINUED TO CLIMB TO 120 PERCENT PLUS TORQUE. CREW DEPARTED AND RETURNED TO MQB. AN OVERTORQUE INSPECTION WAS PERFORMED ALONG WITH A GROUND RUN IN WHICH THE PROBLEM COULD NOT BE DUPLICATED. THE AIRCRAFT WAS FERRIED TO LAW FOR AN OVERWEIGHT LANDING INSPECTION. THE ECU AND TORQUE/HP SENSOR, SN SIM2A385, WERE REPLACED AS A PRECAUTION. AIRCRAFT RETURNED TO SERVICE. (X)
Part: CTOT PANEL — MALFUNCTIONED (NR 1 ENGINE)
LAW - FLT 3804 - ON TAKEOFF, POWER WAS MANUALLY SET AT APPROXIMATELY 85 PERCENT WHEN CTOT WAS ENGAGED FOR A MAX POWER TAKEOFF LEFT TQ 120 PLUS DEGREES, ABORTED TAKEOFF, RETURNED TO GATE. TORQUE NOT EXCEEDED 12 SEC TRANS IAW GE MM 72-00-00. REMOVED AND INSPECTED CTOT PANEL IAW 76-10-30. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: WHEEL — BROKEN (NR 1)
ORD - WHEEL ASSY WAS REMOVED FROM AIRCRAFT IN ORD AND SENT OT WHEEL SHOP. THE WHEEL ASSY HAS 13 INCHES OF INNER FLANGE BROKEN OFF OF WHEEL INNER ASSY. THE INNER WHEEL ASSY HAS BEEN REMOVED FROM SERVICE. (W)