This N-number isn't registered right now. Below is its last known registration, canceled May 12, 2017.
Safety record in brief:1 NTSB accident (Feb 2007)3 ADs may apply28 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
an in-flight encounter with clear air turbulence, which resulted in a serious injury to a deadheading crewmember.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for LAX07CA077)
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 |
|---|---|---|---|
| 2014-14-02 | Pratt & Whitney Canada Corp. Turboprop Engines | Aug 15, 2014 | Engine (PW121)Only with: PW120, PW121, PW121A engines with Post SB21610 configuration; PW124B, PW127, PW127E, PW127F engines with Post SB21607 and/or Post SB21705 configuration; PW127G and PW127M engines unconditionally. |
| 2012-26-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Feb 15, 2013 | Engine (PW121)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. |
| 2003-21-03 | Pratt & Whitney Canada Models PW118, PW120, PW120A, and PW121 Turboprop Engines | Nov 20, 2003 | Engine (PW121) |
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.
LEFT MAIN GEAR DOOR APPEARED TO RE-OPEN AFTER NORMAL RETRACTION. WOULD NOT CLOSE AFTER CYCLE. R & R LG SELECTOR VLV IAW D8 AMM 32-30-41. FUNCTIONAL CHECKED GOOD NO LEAKS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.ON TOUCHDOWN, THE NR 1 HYD ISOLATION VALVE CAUTION LIGHT ILLUMINATED, LOST NR 1 HYD QTY AND ASSOCIATED BRAKES. TAXIIED IN USING REVERSE AND THE PARKING BRAKE. REPLACED RT INBD SPOILER ACTUATOR.
From FAA Service Difficulty Reports; matched by N-number and serial number.THE AUTOPILOT DISPLAY WENT BLACK (ID-802) AND COULD SMELL BURNING WIRE. R & R NR 1 ID-802 ADVISORY DISPLAY.
From FAA Service Difficulty Reports; matched by N-number and serial number.STRONG CHEMICAL ODOR IN COCKPIT AFTER TAKEOFF. FOUND PINHOLE LEAK IN NOSE GEAR HYD LINE. REPAIRED THE LINE AND CYCLED 8 TIMES WITH NO DEFECTS OR LEAKS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.STRONG CHEMICAL ODOR ON FLIGHT DECK AND IN CABIN AFTER TAKEOFF WITH BLEED AIR ON FOR AN APPROX 4 MINUTE DURATION. MX PERSONNEL REMOVED, CLEANED, AND REINSTALLED CONDENSOR/MIXER. MX PERFORMED AN ENGINE RUN AFTER CLEANING AND NOTED NO FURTHER ODOR.
From FAA Service Difficulty Reports; matched by N-number and serial number.SMOKE LIGHT ILLUMINATED INTERMITTENTLY ON CLIMBOUT. CLEANED AND RESEATED CONNECTORS IN THE BAG BAY - CONNECTOR DESIGNATOR 2612-P2 & 2612-P4
From FAA Service Difficulty Reports; matched by N-number and serial number.FLIGHT 51395 SMOKE MASTER WARNING ANNUNCIATOR ILLUMINATED INTERMITTENTLY IN FLIGHT FOR APPROX 5 SECOND INTERVALS EACH TIME, THEN EXTINGUISHED. CREW RETURNED TO BASE AS A PRECAUTIONARY MEASURE. UPON INSP, MX FOUND A PIN PUSHED OUT OF THE BAGGAGE SMOKE DETECTOR CONNECTOR. THE SMOKE DETECTOR WIRING…
From FAA Service Difficulty Reports; matched by N-number and serial number.NO RT BRAKES DURING LANDING ROLLOUT. REPLACED DAMAGED CONTROL CABLE (SEPARATED STRANDS).
From FAA Service Difficulty Reports; matched by N-number and serial number.(PIREP) HYDRAULIC FLUID LEAKING FROM LEFT WING. (MX) REMOVED AND REPLACED LT OUTBOARD SPOILER ACTUATOR IAW DHC-8 MM 27-14-05 PG 201-203. UPON INSPECTION IT IS NOTED THAT THE ACTUATOR HOUSING CRACKED AND FAILED AT THE PISTON END CAP. THE END CAP SEPARATED FROM THE ACTUATOR UNIT.
From FAA Service Difficulty Reports; matched by N-number and serial number.(PIREP) ON CLIMBOUT AT 3000FT, THE NR 2 ENGINE OIL PRESSURE LIGHT ILLUMINATED AND ZERO OIL PRESSURE ON THE GAUGE. SHUT THE ENGINE DOWN PER CHECKLIST AND LANDED WITHOUT INCIDENT. (MX) REMOVED AND REPLACED NR 2 ENGINE IAW RORM AIA M-105. OPS AND LEAK CHECK IAW DHC-8 MM 71-00-00 PG 529-532.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 28 reports.