# N997CF: 1972 Mcdonnell Douglas DC-8-62F, registration cancelled 2004-03-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 18, 2004 - Exported to: Brazil - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-8-62F](https://openairdocs.org/model/mcdonnell-douglas-dc-8-62f) (registry code 302197D) - Engine: [Pratt & Whitney JT3D-3&3B](https://openairdocs.org/engine/pratt-whitney-jt3d-3-3b) (registry code 52039) - Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs) - Serial number: 46154 - Year built: 1972 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 7, 1984 - Certificate issued: June 26, 2002 - Last registry action: June 26, 2002 - Mode S code: ADECDC - Owner when cancelled: [Skytrade International Enterprises Inc](https://openairdocs.org/faa-owner/SKYTRADE%20INTERNATIONAL%20ENTERPRISES%20INC) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Non-citizen corporation - Owner's area on the map: 25.8166° N, 80.3105° W: Placed by OpenAirDocs at the center of ZIP code 33166, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N997CF - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=997CF - Page: https://openairdocs.org/deregistered/N997CF-2004-03-18 From the FAA registry file of October 28, 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-8-62F: https://openairdocs.org/model/mcdonnell-douglas-dc-8-62f.md ## Service difficulty reports (124, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR RRXA010033](https://openairdocs.org/sdr/RRXA010033), Apr 10, 2001: INDICATOR. FAULTY. ON TAKEOFF ROLL NR 1 ENG EGT TEMP WENT TO 575 DEGREES AND WAS CLIMBING OUTSIDE TEMP 22 EPR 1.88 N1 & FF WERE EVEN ACFT SPEED WAS 70 KNOTS. PERFORMED EGT INDICAT - [SDR RRXA010015](https://openairdocs.org/sdr/RRXA010015), Mar 2, 2001: HYDRAULIC LINE. RUPTURED. ON TAXI IN A/C LOST ALL HYD FLUID. FOUND FLEX LINE ON STOW PUMP RUPTURED. REMOVED AND REPLACED FLEX LINE. LEAK AND OP CK''S GOOD. A/C RETURNED TO SERVICE. - [SDR RRXA001094](https://openairdocs.org/sdr/RRXA001094), Dec 16, 2000: O-RING. DAMAGED. RADAR SPOKE IS FUZZY AND TILT POINTS TO THE GROUND AT ALL TIMES. REPLACED DAMAGED O-RING ON BACK OF RADAR RT WAVE GUIDE. PERFORMED FUNCTIONAL TEST PER DC-8 MM 3 - [SDR RRXA000285](https://openairdocs.org/sdr/RRXA000285), May 1, 2000: FRAME. CRACKED. REPAIR CRACK ON FRAME AT STA 340 BETWEEN L20L AND L21L AND CRACKED WEB PN5772787-13. FABRICATED AND INSTALLED REPAIR ITEM PER EWA SKETCH 04-30-2000-001. BOEING - [SDR RRXA000198](https://openairdocs.org/sdr/RRXA000198), Mar 31, 2000: PIN. BROKEN. AFTER TAKE OFF FROM DEN UPON GEAR RETRACTION A LOUD NOISE WAS HEARD AND THE LEFT MAIN GEAR REMAINED DOWN. PER VERIFIED ALT GEAR DOOR LIGHT ON AND SPOILER PRESS - [SDR RRXA000182](https://openairdocs.org/sdr/RRXA000182), Feb 2, 2000: ENGINE. LEAKING. DURING CLIMBOUT, NOTED NR 1 ENGINE LOW OIL PRESS LIGHT ILLUMINATED. NR 1 OIL PRESS 20 PSI AND DROPPING, OIL TEMP DECREASING, NR 1 OIL QUANTITY 1.5 GAL AND DECRE - [SDR RRXA991469](https://openairdocs.org/sdr/RRXA991469), Sep 16, 1999: SKIN. CORRODED. DURING LINE INSPECTION FOUND 6 EACH POPPED FASTENERS ON EXTERNAL SKIN AT STA 270 AND LONGERON 21 RIGHT. INSPECTED ENTERNAL AREA AND FOUND DOUBLER WITH CORROSION - [SDR RRXA99804](https://openairdocs.org/sdr/RRXA99804), May 19, 1999: PACKING. MISSING. HYDRAULIC OIL LOW LIGHT CAME ON HYDRAULIC QUANTITY DECREASING, RESERVOIR LOW PRESSURE LIGHT ON. EMERGENCY PROCEDURE INITIATED. EMERGENCY DECLARED. FOUND HYD LIN - [SDR RRXA99897](https://openairdocs.org/sdr/RRXA99897), May 15, 1999: ACTUATOR. FAILED. ON TEST OF FUEL DUMP SYSTEM, WHEN DUMP SWITCH WAS PLACED TO DRAIN THE CHUTES WOULD NOT MOVE TO DRAIN. TRIED MANUAL DRAIN, NO HELP. FUEL CONTINUED TO DUMP TO STA - [SDR RRXA991186](https://openairdocs.org/sdr/RRXA991186), Apr 18, 1999: FITTING. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD CARGO COMP C-2 DOOR CUT-OUT BETWEEN STA 500 AND STA 560, BL 34 RIGHT AT FITTINGS. DAMAGE EXCEEDED LIMI - [SDR RRXA991176](https://openairdocs.org/sdr/RRXA991176), Apr 6, 1999: ANGLE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ATTACH ANGLE, RT W/W AT STA 879, BL 0, WL 16 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, - [SDR RRXA991225](https://openairdocs.org/sdr/RRXA991225), Apr 5, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSEALAGE, LT CABIN FLOOR BETWEEN STA 680 AND STA 700 AT BL 54 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DA - [SDR RRXA991226](https://openairdocs.org/sdr/RRXA991226), Apr 1, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSEALAGE, CABIN FLOOR PLANK AT STA 1460 AND BL 6 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATE - [SDR RRXA991224](https://openairdocs.org/sdr/RRXA991224), Apr 1, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1500 AND STA 1520 AT BL 36 LEF. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991237](https://openairdocs.org/sdr/RRXA991237), Mar 29, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1160 AND STA 1270 AT BL 54 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOV - [SDR RRXA991236](https://openairdocs.org/sdr/RRXA991236), Mar 29, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1000 AND STA 1160 AT BL 54 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOV - [SDR RRXA991235](https://openairdocs.org/sdr/RRXA991235), Mar 29, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1460 AND STA 1500 AT BL 26 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOV - [SDR RRXA991234](https://openairdocs.org/sdr/RRXA991234), Mar 29, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1270 AND STA 1300 AT BL 54 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOV - [SDR RRXA991233](https://openairdocs.org/sdr/RRXA991233), Mar 29, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PANEL BETWEEN STA 1360 AND STA 1420 AT BL 22 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMO - [SDR RRXA991232](https://openairdocs.org/sdr/RRXA991232), Mar 29, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1360 AND STA 1440 AT BL 12 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOV - [SDR RRXA991231](https://openairdocs.org/sdr/RRXA991231), Mar 29, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 580 AND STA 700 AT BL 28 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVE - [SDR RRXA991230](https://openairdocs.org/sdr/RRXA991230), Mar 29, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 760 AND STA 800 AT BL 32 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991229](https://openairdocs.org/sdr/RRXA991229), Mar 29, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 600 AND STA 740 AT BL 6 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991228](https://openairdocs.org/sdr/RRXA991228), Mar 29, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 420 AND STA 520 AT BL 12 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991227](https://openairdocs.org/sdr/RRXA991227), Mar 29, 1999: FFLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSEALAGE, CABIN FLOOR PLANK BETWEEN STA 580 AND STA 700 AT BL 36 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVE - [SDR RRXA991242](https://openairdocs.org/sdr/RRXA991242), Mar 25, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE,CABIN FLOOR PLANK BETWEEN STA 1240 AND STA 1280 AT BL 12 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. /////C - [SDR RRXA991241](https://openairdocs.org/sdr/RRXA991241), Mar 25, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK AT STA 1220 AND BL 18 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREA - [SDR RRXA991240](https://openairdocs.org/sdr/RRXA991240), Mar 25, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1120 AND 1140 AT BL 12 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991239](https://openairdocs.org/sdr/RRXA991239), Mar 25, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1040 AND STA 1060 AT BL 32 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVE - [SDR RRXA991238](https://openairdocs.org/sdr/RRXA991238), Mar 25, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1100 AND STA 1120 AT BL 32 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOV - [SDR RRXA991251](https://openairdocs.org/sdr/RRXA991251), Mar 24, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 700 AND STA 822 AT BL 49 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991250](https://openairdocs.org/sdr/RRXA991250), Mar 24, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 460 AND STA 540 AT BL 12 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991249](https://openairdocs.org/sdr/RRXA991249), Mar 24, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PANEL BETWEEN STA 900 AND STA 920 AT BL 54 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991248](https://openairdocs.org/sdr/RRXA991248), Mar 24, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PANEL AT STA 700 BL 36 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AR - [SDR RRXA991247](https://openairdocs.org/sdr/RRXA991247), Mar 24, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PANEL BETWEEN STA 1460 AND STA 1480 AT BL 12 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVE - [SDR RRXA991246](https://openairdocs.org/sdr/RRXA991246), Mar 24, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1460 AND STA 1480 AT BL 12 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVE - [SDR RRXA991245](https://openairdocs.org/sdr/RRXA991245), Mar 24, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 1400, BL 12 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED A - [SDR RRXA991244](https://openairdocs.org/sdr/RRXA991244), Mar 24, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PANEL AT STA 880, BL 38 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AR - [SDR RRXA991243](https://openairdocs.org/sdr/RRXA991243), Mar 24, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 717 AND STA 759 AT BL 36 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991189](https://openairdocs.org/sdr/RRXA991189), Mar 24, 1999: WEB. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, WEB, CABIN RT TOP OF LOWER CARGO DOOR BETWEEN STA 480 AND STA 520 AT BL 53 RIGHT. DAMAGE EXCEEDED LIMITS I - [SDR RRXA991255](https://openairdocs.org/sdr/RRXA991255), Mar 22, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 600 AND STA 620 AT BL 8 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991254](https://openairdocs.org/sdr/RRXA991254), Mar 22, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PANEL BETWEEN STA 660 AND STA 680 AT BL 20 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991253](https://openairdocs.org/sdr/RRXA991253), Mar 22, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 840, BL 4 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED ARE - [SDR RRXA991252](https://openairdocs.org/sdr/RRXA991252), Mar 22, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 800, BL 54 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AR - [SDR RRXA991256](https://openairdocs.org/sdr/RRXA991256), Mar 21, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 580 AND STA 879 AT BL 13 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED - [SDR RRXA991257](https://openairdocs.org/sdr/RRXA991257), Mar 18, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN INT UNDER FLOOR PLANK TOP W/W AT STA 980, BL 24 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED D - [SDR RRXA991258](https://openairdocs.org/sdr/RRXA991258), Mar 15, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOORBEAM AT STA 580, BL 45 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED ARE - [SDR RRXA991185](https://openairdocs.org/sdr/RRXA991185), Mar 15, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE,FUSELAGE SKIN BETWEEN STA 1118 AND STA 1165 BETWEEN LONGERONS 32 RIGHT AND LONGERON 34 RIGHT. DAMAGE EXCEED - [SDR RRXA991184](https://openairdocs.org/sdr/RRXA991184), Mar 15, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CENTER TANK AFT TOP SKIN PANEL AT STA 857, BL 46 RIGHT, 2 FORWARD OF REAR SPAR. DAMAGE EXCEEDED LIMITS IAW - [SDR RRXA991183](https://openairdocs.org/sdr/RRXA991183), Mar 15, 1999: FLOORBEAM. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN TOP OF W/W UNDER FLOOR BETWEEN STA 902 AND STA 920 AT BL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REM All 124: https://openairdocs.org/deregistered/N997CF-2004-03-18/reports.md ## FAA accident and incident reports (1) 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 19980925040329I](https://openairdocs.org/incident/19980925040329I), Sep 25, 1998: Doug DC862F (N997CF), Newark, NJ. (-5)Upon landing ewr eww 342 given clearance to intercept taxing papa and hold short of taxiway whiskey. Coa 135 was cleared for take-off 22R. Eww 342 entered… --- 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.