This N-number isn't registered right now. Below is its last known registration, canceled May 15, 2002.
Safety record in brief:1 NTSB accident (substantial damage, Apr 2000)No ADs since 1998 matched25 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.
The failure of the clamp that secured the high-pressure bleed air duct to the high-pressure relief valve. Factors were the resulting excessive pressurization of the engine nacelle, and the subsequent separation of the engine cowling.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DEN00FA078)
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.
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SPLICE FITTING IN THE AFT ACCESSORY COMPT AT STA 1340 AND 1360 AND L29R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SPLICE FITTING IN THE FWD LWR CARGO COMPT BETWEEN STA''S 600 AND 620 AND L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A MAINTENANCE VISIT FOUND A TEAR TO THE STRAP BETWEEN STRINGERS AT STA 902 STRINGER 9-10 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW PD 08-53-049.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A MAINTENANCE VISIT FOUND A TEAR TO THE STRAP BETWEEN STRINGERS AT STA 902 AND 9 - 10 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW PD08-53-049.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LONGERON 9L AT FS 935, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 1D AND 51-1-24.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A MAINTENANCE VISIT FOUND A TEMP REPAIR ON FUSELAGE AT STA 879 TO 946 AND L5L TO L11L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW EA PD08-53-047.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A MAINTENANCE VISIT FOUND A CRACK TO THE END FITTING ON THE LONGERON AT FS 902 AND L10L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, EA PD08-53-048 AND DWG 3645859.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A MAINTENANCE VISIT FOUND DAMAGE TO THE NR 2 ENGINE PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LONGERON AT FS 935 AND L9L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 1D, 51-1-24 AND 51-1-8 FIG 10.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A MAINTENANCE VISIT FOUND A TEMP REPAIR ON FUSELAGE AT STA 879 TO 946 AND L5L TO L11L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EA PD08-53-047.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 25 reports.