This N-number isn't registered right now. Below is its last known registration, canceled Aug 22, 2019.
Safety record in brief:1 NTSB accident (substantial damage, Jan 2014)No ADs since 1998 matched130 service difficulty reports
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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.
Inattention by ground crew personnel which resulted in the airplane being substantially damaged.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA14CA051)
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.
No ADs published since 1998 matched this airframe or engine model.
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.
ON POST FLIGHT IN CAK FOUND RT ENGINE MANUAL START VALVE DOOR MISSING. INSTALLED PANEL 7808C ON NR 2 ENGINE LOWER COWL IAW DAC DWG 5938090 AND AMM 20-30.
From FAA Service Difficulty Reports; matched by N-number and serial number.CREW REPORTED SMOKE COMING FROM THE AFT LEFT LAV TRASH CAN. FIRE EXTINGUISHER USED AS A PRECAUTION. THERE WERE NO VISIBLE FLAMES NOTED. FOUND CHAFED WIRE BEHIND MIRROR. REPAIRED WIRE AND REPOSITIONED WIRE BUNDLE.
From FAA Service Difficulty Reports; matched by N-number and serial number.RIGHT ENGINE FIRE LOOP "A" ILLUMINATED IN FLIGHT. POSITIONED LOOP SWITCH TO POSITION "B" IAW CHECKLIST. NO FURTHER PROBLEMS. FOUND CONNECTOR P1-826 LOOSE AND MISSING CLAMP THAT SECURES W251A16. CLEANED & SECURED CONN AND INSTALLED CLAMP. OPS CHECK NORMAL AT THIS TIME.
From FAA Service Difficulty Reports; matched by N-number and serial number.LEFT THROTTLE WOULD NOT ADVANCE PAST 1.5 ON THROTTLE QUADRANT AT LEVEL OFF. INSPECTED THE PUSH - PULL CABLE, CROSSOVER SHAFT, LT THROTTLE CABLE AFT CARGO DOOR TO PYLON, LT THROTTLE CABLE IN FWD CARGO FWD BULKHEAD TO AFT BULKHEAD, ALSO INSPECTED THE CABLE PULLEY SYS FROM E/E TO THROTTLE HANDLE. NO…
From FAA Service Difficulty Reports; matched by N-number and serial number.NR 2 ENG NOSE COWL MISSING ANGLES ON FWD SIDE INTERNAL- NUMEROUS FASTENERS MISSING ON OTHER ANGLES. REPLACED NOSE COWL SN OFF 49812 SER ON DL 128 FTN ON 53TR4R PER AMM 71-10-03.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SERVICE CHECK, FOUND THE AFT STAIR CABIN DOOR BLOCKED UNABLE TO OPEN, DUE TO AFT JUMP SEAT NOT RETRACTING.FOUND AFT JUMP SEAT INERTIA REEL RETAINING BUNGEE CORD BROKEN. REPLACED BUNGEE IAW AMM 25-23-02. JUMPSEAT/DOOR OPERATE NORMALLY. OK FOR SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.TAILCONE RELEASE MECHANISM CAM TORQUE CHECK FAILED. REPLACED THE RELEASE MECHANISM CAM SUPPORT BRACKET IAW AMM 53-53-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.EMERGENCY LIGHTS AT SEAT 23DEF INOP. FOUND BROKEN WIRE AT SEAT TRACK. RE-SPLICED SAME PER WDM 33-51-14, AND AMM 20-50. CHECKS GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.CENTER CARGO COMPARTMENT, STA 693-STA 750, X-15 TO X-16, LOWER DOOR FRAME OTBD FACE HAS CORROSION AROUND RIV-NUTS. BLENDED AREAS AT CENTER CARGO COMPARTMENT, STA 693-STA 750, X15 TO X16 LOWER DOOR FRAME, BLEND AREA FWD WAS FOUND TO BE OUT OF LIMITS. ACCOMPLISHED A REPAIR AREA FWD IAW SRM VOL I…
From FAA Service Difficulty Reports; matched by N-number and serial number.FWD WET AREA RIGHT SIDE BS 256 RBL 22 - 44 FLOORBEAM CORRODED ON UPPER SURFACE. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 3. REMOVED AND REPLACED IAW SRM 51-30-05 VOL II.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 130 reports.