# N993CF: Mcdonnell Douglas DC-8-62, registration cancelled 2009-08-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 31, 2009 - Status when cancelled: Triennial form not returned - Airframe: [Mcdonnell Douglas DC-8-62](https://openairdocs.org/model/mcdonnell-douglas-dc-8-62) (registry code 302197B) - Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs) - Serial number: 46028 - Type of aircraft: Fixed wing multi engine - Certificate issued: April 30, 2002 - Last registry action: July 15, 2008 - Mode S code: ADDE00 - Owner when cancelled: [Mk Airlines Inc](https://openairdocs.org/faa-owner/MK%20AIRLINES%20INC) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7376° N, 75.6671° W: Placed by OpenAirDocs at the center of ZIP code 19808, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N993CF - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=993CF - Page: https://openairdocs.org/deregistered/N993CF-2009-08-31 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Mcdonnell Douglas DC-8-62: https://openairdocs.org/model/mcdonnell-douglas-dc-8-62.md ## Service difficulty reports (69, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR RRXA001040](https://openairdocs.org/sdr/RRXA001040), Aug 2, 2000: CONTROL PANEL. FAILED. NR 1 TRANSPONDER SQUAKS 7777 NO MATTER WHAT THE INPUT (THE VARIOUS CODES) ON THE BOX IS, NR 2 TRANSPONDER INOP (NO SQUAK) FOR VARIOUS CODES. REMOVED AND REPLACE - [SDR RRXA991586](https://openairdocs.org/sdr/RRXA991586), Nov 24, 1999: VALVE. INOPERATIVE. DURING FLIGHT AT FL 26.0 MADE AN EMERGENCY DESCENT DUE TO LOSS OF CABIN PRESSURIZATION. REPLACED LEFT AND RIGHT PRESSURIZATION VALVES. PERFORMED PRESSURIZATION - [SDR RRXA991585](https://openairdocs.org/sdr/RRXA991585), Nov 19, 1999: CONTROLLER. MALFUNCTIONED. AT FL 260, AIRCRAFT EXPERIENCED A RAPID CLIMB IN CABIN PRESSURE CREW DESCENDED TO FL 120 AND LANDED IN (MKE). PRESSURIZED A/C TO 1.5 DPSI NO MAJOR LEAKS NOTED. - [SDR RRXA991377](https://openairdocs.org/sdr/RRXA991377), Aug 31, 1999: VALVE. MALFUNCTIONED. AFTER TAKEOFF, DURING RIGHT TURN AIRCRAFT HAD STUDDERING, TURNING OUT OF TURN SAME BUFFETING EFFECT IN AIRFRAME. DID NOT FEEL IN YOKE, NO VISIBLE ENGINE INDICAT - [SDR RRXA991541](https://openairdocs.org/sdr/RRXA991541), Jul 23, 1999: STRAP. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO CIRCUMFERENCIAL STRAP AT STA 1180, LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMA - [SDR RRXA991528](https://openairdocs.org/sdr/RRXA991528), Jul 22, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING SKIN AT STA XCW=69.5 AND STRINGER 9 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED - [SDR RRXA991563](https://openairdocs.org/sdr/RRXA991563), Jul 9, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO DOOR JAMB PAN SKIN BETWEEN STA 1240 AND STA 1280, AND BETWEEN LONGERONS 31 RIGHT AND LONGERON 33 RIGHT. - [SDR RRXA991561](https://openairdocs.org/sdr/RRXA991561), Jul 8, 1999: FITTING. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AT DOOR JAMB TORQUE BOX FITTING AT STA 490, BETWEEN LONGERONS 32 RIGHT AND LONGERON 33 RIGHT. DAMAGE EXCEE - [SDR RRXA991562](https://openairdocs.org/sdr/RRXA991562), Jul 7, 1999: FITTING. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO DOOR JAMB TORQUE BOW FITTING AT STA 500, BETWEEN LONGERONS 32 RIGHT AND LONGERON 33 RIGHT. DAMAGE EXCEE - [SDR RRXA991546](https://openairdocs.org/sdr/RRXA991546), Jul 2, 1999: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 36 AT STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SR - [SDR RRXA991545](https://openairdocs.org/sdr/RRXA991545), Jul 2, 1999: INTERCOSTAL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO INTERCOSTAL BETWEEN STA 1240 AND STA 1280, AT WL 4 RIGHT, AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS - [SDR RRXA991530](https://openairdocs.org/sdr/RRXA991530), Jun 19, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INNER SKIN BETWEEN STA 480 AND STA 580, AND BETWEEN LONGERONS 34 LEFT AND LONGERON 35 RIGHT. DAMAGE EXCEEDE - [SDR RRXA991542](https://openairdocs.org/sdr/RRXA991542), Jun 12, 1999: FRAME. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME AT STA 1200, BETWEEN LONGERONS 35 LEFT AND LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM - [SDR RRXA991559](https://openairdocs.org/sdr/RRXA991559), Jun 7, 1999: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 34 RIGHT, AT STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW - [SDR RRXA991558](https://openairdocs.org/sdr/RRXA991558), Jun 7, 1999: FRAME. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME AT STA 1250 AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA I - [SDR RRXA991557](https://openairdocs.org/sdr/RRXA991557), Jun 7, 1999: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 34 LEFT, BETWEEN STA 1240 AND STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, - [SDR RRXA991555](https://openairdocs.org/sdr/RRXA991555), Jun 7, 1999: SHEAR TIE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1240 AND LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREA - [SDR RRXA991554](https://openairdocs.org/sdr/RRXA991554), Jun 7, 1999: SHEAR TIE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1220, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. - [SDR RRXA991553](https://openairdocs.org/sdr/RRXA991553), Jun 7, 1999: FITTING. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 560, BETWEEN LONGERONS 33 LEFT AND 34 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991552](https://openairdocs.org/sdr/RRXA991552), Jun 7, 1999: SHEAR TIE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1220, BETWEEN LONGERONS 35 LEFT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. - [SDR RRXA991551](https://openairdocs.org/sdr/RRXA991551), Jun 7, 1999: SHEAR TIE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1200, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. - [SDR RRXA991550](https://openairdocs.org/sdr/RRXA991550), Jun 7, 1999: SHEAR TIE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1200, BETWEEN LONGERONS 35 LEFT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. - [SDR RRXA991547](https://openairdocs.org/sdr/RRXA991547), Jun 7, 1999: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 35 RIGHT AT STA 1280. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW D - [SDR RRXA991544](https://openairdocs.org/sdr/RRXA991544), Jun 7, 1999: SHEAR TIE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1235, BETWEEN LONGERONS 33 RIGHT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC- - [SDR RRXA991543](https://openairdocs.org/sdr/RRXA991543), Jun 7, 1999: SHEAR TIE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE BETWEEN STA 1220 AND STA 1240, AND BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDE - [SDR RRXA991538](https://openairdocs.org/sdr/RRXA991538), Jun 7, 1999: ANGLE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME ATTACHMENT ANGLE AT STA 580, BETWEEN LONGERONS 33 LEFT AND LONGERON 34 LEFT. DAMAGE EXCEEDED LIMI - [SDR RRXA991537](https://openairdocs.org/sdr/RRXA991537), Jun 7, 1999: FITTING. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 560, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. RE - [SDR RRXA991534](https://openairdocs.org/sdr/RRXA991534), Jun 7, 1999: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 34 RIGHT AT STA 580. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 - [SDR RRXA991532](https://openairdocs.org/sdr/RRXA991532), Jun 7, 1999: FITTING. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 540, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. RE - [SDR RRXA991531](https://openairdocs.org/sdr/RRXA991531), Jun 7, 1999: FITTING. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 500, LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AR - [SDR RRXA991529](https://openairdocs.org/sdr/RRXA991529), Jun 7, 1999: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION TO LONGERON 32 RIGHT, BETWEEN STA 460 TO STA 600. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA - [SDR RRXA991536](https://openairdocs.org/sdr/RRXA991536), Jun 6, 1999: ANGLE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO ATTACHMENT ANGLE AT STA 500, LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, T - [SDR RRXA991564](https://openairdocs.org/sdr/RRXA991564), Jun 1, 1999: FITTING. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 260 AND BL 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA - [SDR RRXA991560](https://openairdocs.org/sdr/RRXA991560), May 31, 1999: FRAME. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO NUMBER 2 LOWER CARGO DOOR JAMB FRAME WEB AT STA 461, BETWEEN LONGERONS 33 RIGHT AND 34 RIGHT. DAMAGE EX - [SDR RRXA991535](https://openairdocs.org/sdr/RRXA991535), May 31, 1999: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 30 RIGHT, SPLICE DOUBLER BETWEEN STA 600 AND STA 620. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REM - [SDR RRXA991549](https://openairdocs.org/sdr/RRXA991549), May 30, 1999: FRAME. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME STRAP AT STA 1180, BETWEEN LONGERONS 33 RIGHT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW D - [SDR RRXA991548](https://openairdocs.org/sdr/RRXA991548), May 27, 1999: FRAME. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME AT STA 1420, BETWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. R - [SDR RRXA991539](https://openairdocs.org/sdr/RRXA991539), May 27, 1999: FINGER DOUBLER. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FINGER DOUBLER AT STA 310 AND LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, - [SDR RRXA991556](https://openairdocs.org/sdr/RRXA991556), May 26, 1999: FRAME. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME AT STA 1240, BETWEEN LONGERONS 34 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REM - [SDR RRXA991540](https://openairdocs.org/sdr/RRXA991540), May 26, 1999: BRACKET. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO BRACKET AT STA 1165, BETWEEN LONGERONS 29 RIGHT AND LONGERON 30 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 - [SDR RRXA991527](https://openairdocs.org/sdr/RRXA991527), May 26, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING UPPER SKIN BETWEEN FRONT SPAR AND CENTER SPAR, BETWEEN STA XW=22.750 AND STA XW=107. DAMAGE EXCEEDED LIMI - [SDR RRXA991526](https://openairdocs.org/sdr/RRXA991526), May 26, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, UPPER SKIN SURFACE AT STA XRS=421 AND STRINGER 9. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, - [SDR RRXA991584](https://openairdocs.org/sdr/RRXA991584), May 25, 1999: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 24 RIGHT AT STA 920, BL 24 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATE - [SDR RRXA991583](https://openairdocs.org/sdr/RRXA991583), May 25, 1999: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 24 RIGHT AT STA 920, BL 64 RIGHT, AND WL 3 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991582](https://openairdocs.org/sdr/RRXA991582), May 25, 1999: SEAT TRACK. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 560 AND STA 660 AT BL 45 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. RE - [SDR RRXA991581](https://openairdocs.org/sdr/RRXA991581), May 25, 1999: SEAT TRACK. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 500 AND STA 560 AT BL 56 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. RE - [SDR RRXA991579](https://openairdocs.org/sdr/RRXA991579), May 25, 1999: SEAT TRACK. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 270 AND STA 340 AT BL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991571](https://openairdocs.org/sdr/RRXA991571), May 25, 1999: SEAT TRACK. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 580 AND STA 620 AT BL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991570](https://openairdocs.org/sdr/RRXA991570), May 25, 1999: SEAT TRACK. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 560 AND STA 660 AT BL 56 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. RE - [SDR RRXA991569](https://openairdocs.org/sdr/RRXA991569), May 25, 1999: SEAT TRACK. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 500 AND STA 560 AT BL 22 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. RE All 69: https://openairdocs.org/deregistered/N993CF-2009-08-31/reports.md ## FAA accident and incident reports (4) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19990417026069I](https://openairdocs.org/incident/19990417026069I), Apr 17, 1999: Doug DC862 (N993CF), Minneapolis, MN, Minor damage. While parking at gate, marshaler failed to observe instructions from wingwalkers for aircraft to stop. Pilot was on centerline and following marchallers… - [Incident 19980714025809I](https://openairdocs.org/incident/19980714025809I), Jul 14, 1998: Doug DC862 (N993CF), Newburgh, NY. After takeoff pilot experienced #4 engine warning. Discharged fire bottle and fire warning light extinguished. On landing roll out, fire warning indication… - [Incident 19960306007059I](https://openairdocs.org/incident/19960306007059I), Mar 6, 1996: Doug DC862 (N993CF), Peoria, IL. Narrative: on March 6, 1996, at approximately 2240 CST, emery worldwide airlines DC-8 aircraft, N993CF, was taxiing on taxiway a. the aircraft slid sideways… - [Incident 19910121003939I](https://openairdocs.org/incident/19910121003939I), Jan 21, 1991: Doug DC862 (N993CF), Dover, DE. Co-pilot became sick en route. Removed from co-pilots position. Transported to hospital at airport. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.