This N-number isn't registered right now. Below is its last known registration, canceled Jul 26, 2023.
Safety record in brief:1 NTSB accident (Aug 2009)3 ADs may apply97 service difficulty reports
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Total time and engine hours aren't public. They appear here once the owner adds logbooks.
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An in-flight encounter with convective clouds resulting in moderate turbulence and serious injury to a flight attendant.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA09LA444)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2013-15-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Sep 17, 2013 | Engine (PW123)Serial numbers per Table 1 of the Appendix of P&WC Service Bulletin No. PW100-72-21823, Revision 3. Only with: First-stage power turbine blade P/N 3120973-01, 3120983-01, or 3054053-01 installed with a serial number listed in the referenced SB table. |
| 2012-26-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Feb 15, 2013 | Engine (PW123)Serial numbers per P&WC ASB No. PW100-72-A21813 Rev 3, PW100-72-A21802 Rev 4, and PW100-72-A21798 Rev 5. Only with: Engines with propeller shafts having serial numbers listed in the referenced P&WC ASBs. |
| 2004-20-01 | Pratt & Whitney Canada Models PW123, PW123B, PW123C, PW123D, PW123E, PW123AF, PW124B… | Nov 5, 2004 | Engine (PW123)Only with: Mechanical fuel controls (MFCs) P/Ns 3244841-21, 3244853-17, 3244855-15, 3244857-14, 3244858-23, 3244871-5, 3244873-4, and 3244874-4 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
TWO EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED THE BULBS.
From FAA Service Difficulty Reports; matched by N-number and serial number.CABIN PRESSURIZATION FAILED IN FLIGHT AT ALTITUDE, 14,300 FT. UNABLE TO REGAIN CONTROL IN AUTO AND MANUAL MODES, IAW CABIN PRESSURIZATION FAILURE CHECKLIST. REMOVED DEBRIS FROM 2 BELLY DRAINS AND FOUND 1 DRAIN BROKEN. R & R THE DRAIN VALVE IAW 20-06-03. OPS CHECKED GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.NR 1 PROPELLER HEATER MATS CAUGHT FIRE DURING TAXI. NR 1 ENGINE NOT RUNNING. NOTED NR 1 PROP HEAT SELECTED ON AND ADV LIGHTS CYCLING. R & R THE NR 2 AND 3 BLADES ON THE NR 1 PROPELLER. R & R THE NR 1 AND 3 BULKHEAD HEATER LEADS AND NR 1 BRUSH BLOCK AS A PRECAUTION IAW W/C 61-10-07, HSCMM 61-13-02…
From FAA Service Difficulty Reports; matched by N-number and serial number.EMERGENCY LIGHTS ILLUMINATE WHILE IN ARMED POSITION. R & R THE EMERGENCY LIGHT CONTROL BOX, OPS CHECKED GOOD, OK FOR SERVICE
From FAA Service Difficulty Reports; matched by N-number and serial number.WHEN SELECTING NOSE GEAR UP, NOSE GEAR RED LIGHT STAYED ON WITH AMBER DOOR LIGHTS. ACCOMPANIED BY A GRINDING NOISE IN NOSE GEAR WELL FOR ABOUT 45 SECONDS. R & R THE DRAG STRUT SENSOR IAW MM 32-20-16, OPS CHECKED GOOD. OPERATED GEAR SEVERAL TIMES, CHECKED GOOD. OK FOR SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.EMERGENCY EXIT LIGHT AT ROW 9 IS INOPERATIVE. R & R THE BULB.
From FAA Service Difficulty Reports; matched by N-number and serial number.ROLL SPOILER, OTBD HYD CAUTION LIGHT ILLUMINATED DURING CLIMB OUT. SELECTED NR 2 SPOILER, PUSH OFF CAUTION LIGHT REMAINED ILLUMINATED. R & R THE 2762-S14 AND ASSOCIATED WIRING. RIGGED AND OPS CHECKED IAW MM 27-14-07. OK FOR SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.REJECTED TAKE OFF AT 85 KNOTS DUE TO TAKEOFF WARNING HORN WITH AUTOFEATHER ARM LIGHT INTERMITTENT, YAW DAMPER FAILED, DADC INVALID, AND NR 2 ALTIMETER AND IVSI FLAGGED. FLYING ON NR 2 AFCS. R & R THE NR 2 DADC, OPS GOOD IAW AMM 34-12-01. PERFORMED W/C 31-50-03. OPS CHECKED GOOD. OK FOR SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.ROLL SPOILER OTBD HYD LIGHT ILLUMINATED IN FLIGHT. REMOVED RT LOW HYD PRESSURE SWITCH CONNECTOR AND SWITCH. INSTALLED NEW O-RING AND SWITCH, INSTALLED CONNECTOR AND SAFETIED IAW STD PRACTRICES. PERFORMED ROLL SPOILER CONTROL SYSTEM. OPS CHECKED GOOD IAW 27-14-00.
From FAA Service Difficulty Reports; matched by N-number and serial number.AT FLIGHT LEVEL 9000 FT, NR 1 TORQUE ROLLED BACK 25%. THEN WENT BACK TO NORMAL AND REPEATED. RETURN TO FIELD. REMOVED AND REPLACED THE NR 1 ECU IAW SRT MANUAL, OPS CHECKED GOOD. OK FOR SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 97 reports.