This N-number isn't registered right now. Below is its last known registration, canceled May 17, 2006.
Safety record in brief:1 NTSB incident (minor damage, Apr 1983)No ADs since 1998 matched99 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.
WHILE IN CURISE FLIGHT A TIRE ON THELEFT MAIN LANDING GEAR BLEW OUT. ON LANDING ROLL A FIRE ERUPTED IN THE AREA OF THE LEFT MAIN LANDING GEAR, WHICH WAS EXTINGUISHED BY AIRPORT CRASH RESCUE PERSONAL.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI83IA162)
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.
SPOILER PUMP INOP. FOUND SPOILER ACCUMULATOR BLADDER BLOWN AND SPOILER RESERVIOR EMPTY. REMOVED AND REPLACED SPOILER ACCUMULATOR AND SERVICED SPOILER RESERVOIR IAW MM 29-12-02. SPOILER PUMP OP CK GOOD IAW M/M 27-63-25.
From FAA Service Difficulty Reports; matched by N-number and serial number.AT ROTATION NOSE GEAR VIBRATION FELT AND METALLIC SOUND HEARD. REMOVED AND REPLACED LEFT AND RIGHT NOSE WHEEL ASSY IAW DC8 MM 32-41-10. OPS CHECKS GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.LOUD NOISE AND BUFFET FROM NOSE SECTION. RIGHT NOSE LANDING GEAR DOOR IN OPEN POSITION WHEN AIRCRAFT TAXIED IN. INSPECTED NOSE GEAR DOORS FOR CONDITION AND OPERATION NO DEFECTS NOTED. RE-SET POSITION, AIRCRAFT OK FOR FURTHER FLIGHT DC-8 M/M 32-20-00.
From FAA Service Difficulty Reports; matched by N-number and serial number.CAPTAINS GYRO AND FLIGHT DIRECTOR FLAGS IN VIEW WHEN A/C PITCHES UP OR DOWN 3 DEG AND HORIZON FREEZES IN POSITION. REMOVED AND REPLACED CAPT''S ADI, OPS CKS GOOD IAW UAL MM 41-20 -22.
From FAA Service Difficulty Reports; matched by N-number and serial number.PRECAUTIONARY SHUTDOWN NR 4 ENGINE, NO OIL QUANTITY OR PRESSURE. FOUND HAND CRANKING PAD COVER DAMAGED AND REPLACED COVER. SERVICED ENG, OIL AND LEAK CHECK NORMAL. INSPECTED CHIP DETECTORS AND OIL FILTERS, NO CONTAMINATION FOUND.
From FAA Service Difficulty Reports; matched by N-number and serial number.CLIMBING THRU 12,000 FEET NR 2 ENGINE FIRE WARNING SOUNDED. SECURED ENGINE PER EWW QRH. UPON INSPECTION OF ENGINE FOUND HIGH STAGE BLEED DUCT CRACKED AT FLEX COUPLING. REMOVED AND REPLACED HIGH STAGE BLEED DUCT IAW DC-8 M/M CH 36-11-61 AND FIRE WARNING CHECKS GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT CARGO COMPARTMENT AFT SIDE OF FRAME AT FS 1340 AND LONGERON 30L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-21 FIG 8C-2. (CORROSION…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FUSELAGE INT ON ATTACH ANGLE AT STA 857 TO 859 AND L11R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-8 FIG 1B. (CORROSION DAMAGE RECORDED IN…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SPAR CAP IN THE CABIN INT BELOW FLOOR LEVEL AT STA 857 AND RBL 48 THROUGH LBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED SPAR CAP IAW DC-8 SRM 53-2-5 AND 53-7-0 FIG…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FUSELAGE INT AT STA 857 TO 879 AND L12R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW ANGLE ASSY IAW DC-8 SRM 51-1-21D FIG 34 SHEETS 1 & 2.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 99 reports.