# N832AL: 1969 Douglas DC-8-73, registration cancelled 2006-02-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 21, 2006 - Status when cancelled: Triennial form not returned - Airframe: [Douglas DC-8-73](https://openairdocs.org/model/douglas-dc-8-73) (registry code 302199C) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs) - Serial number: 46063 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 10, 1984 - Certificate issued: December 27, 1999 - Last registry action: December 20, 2005 - Mode S code: AB5FD3 - Owner when cancelled: [Wilmington Trust Co Tr](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TR) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Corporation - Owner's area on the map: 25.7795° N, 80.2996° W: Placed by OpenAirDocs at the center of ZIP code 33126, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N832AL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=832AL - Page: https://openairdocs.org/deregistered/N832AL-2006-02-21 From the FAA registry file of November 3, 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 Douglas DC-8-73: https://openairdocs.org/model/douglas-dc-8-73.md ## Service difficulty reports (30) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR RRXA001081](https://openairdocs.org/sdr/RRXA001081), Nov 10, 2000: SKIN. DAMAGED. 2 INCH HOLE IN BELLY OF ACFT AT 2 FT AFT OF AVIONICS COMPARTMENT. INSP HOLE AFTER REMOVAL OF FWD BUG BIN FWD CENTER PANEL. FOUND NO STRUCTURAL DAMAGE OTHER THAN - [SDR RRXA001054](https://openairdocs.org/sdr/RRXA001054), Sep 14, 2000: WIRE. MISINSTALLED. SMOKE IN COCKPIT WITH SPARKS COMING OUT OF BOTTOM OF BULKHEAD. UPON INSP FOUND QUESTIONABLE TERMINAL CONNECTIONS AND BROKEN WIRE ON LT WINDOW OVERHEAT MODIFICAT - [SDR RRXA000293](https://openairdocs.org/sdr/RRXA000293), Jan 31, 2000: SEAT TRACK. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO OBSERVERS AFT SEAT TRACK AT STA -12 TO STA . DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREA - [SDR RRXA000292](https://openairdocs.org/sdr/RRXA000292), Jan 29, 2000: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 28 LEFT BETWEEN STA 1050 TO STA 1160. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TR - [SDR RRXA000291](https://openairdocs.org/sdr/RRXA000291), Jan 28, 2000: SEAT TRACK. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 159 AND BL/L 48. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA I - [SDR RRXA000290](https://openairdocs.org/sdr/RRXA000290), Jan 28, 2000: SEAT TRACK. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CARGO SEAT TRACK AT STA 280 AND BL/L 55. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TRE - [SDR RRXA001036](https://openairdocs.org/sdr/RRXA001036), Jan 24, 2000: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, FLAP EXTERNAL SKIN BETWEEN XW 2 TO XW 64. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REM - [SDR RRXA000288](https://openairdocs.org/sdr/RRXA000288), Jan 20, 2000: FRAME. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO TORQUE BOX (FRAME) WEB AT STA 270 BETWEEN LONGERONS 33 RIGHT TO 34 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW D - [SDR RRXA001038](https://openairdocs.org/sdr/RRXA001038), Jan 18, 2000: VANE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, FLAP VANE BETWEEN XFS 383 TO XFS 386. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED - [SDR RRXA000289](https://openairdocs.org/sdr/RRXA000289), Jan 17, 2000: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, LEADING EDGE, EXTERNAL SKIN BETWEEN XFS 885 TO XFS 892. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM - [SDR RRXA001033](https://openairdocs.org/sdr/RRXA001033), Jan 16, 2000: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, LEADING EDGE LOWER SKIN BETWEEN XFS 347 TO XFS 379. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC- - [SDR RRXA001028](https://openairdocs.org/sdr/RRXA001028), Jan 13, 2000: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 34 LEFT BETWEEN STA 390 TO STA 410. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMA - [SDR RRXA001021](https://openairdocs.org/sdr/RRXA001021), Jan 13, 2000: SEAT TRACK. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 1590 AND BL48R TO WL 0. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, - [SDR RRXA000286](https://openairdocs.org/sdr/RRXA000286), Jan 13, 2000: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, LEADING EDGE, EXTERNAL SKIN AT XFS 710. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE - [SDR RRXA001027](https://openairdocs.org/sdr/RRXA001027), Jan 12, 2000: FRAME. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1040 AND LONGERON 35 RIGHT. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, - [SDR RRXA001035](https://openairdocs.org/sdr/RRXA001035), Jan 10, 2000: VANE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, FLAP VANE AT XFS 225 TO XFS 322. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMA - [SDR RRXA001030](https://openairdocs.org/sdr/RRXA001030), Jan 10, 2000: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 30 RIGHT BETWEEN STA 370 TO STA 410. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAM - [SDR RRXA001025](https://openairdocs.org/sdr/RRXA001025), Jan 8, 2000: FITTING. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT FITTING AT STA 960 TO STA 980 AND BL44R. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOV - [SDR RRXA001039](https://openairdocs.org/sdr/RRXA001039), Jan 4, 2000: CLIP. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WHEEL WELL ATTACHMENT CLIP AT STA 902, BL59R AND WL 12. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 - [SDR RRXA001026](https://openairdocs.org/sdr/RRXA001026), Jan 4, 2000: FITTING. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 1480 TO STA 1490 AND LONGERON 33 RIGHT. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. RE - [SDR RRXA001022](https://openairdocs.org/sdr/RRXA001022), Jan 4, 2000: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 21 RIGHT AT STA 1190. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AR - [SDR RRXA001037](https://openairdocs.org/sdr/RRXA001037), Jan 3, 2000: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, OUTBOARD SLOT VANE BETWEEN XFS 430 TO XFS 440. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM - [SDR RRXA001034](https://openairdocs.org/sdr/RRXA001034), Jan 3, 2000: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, UPPER SKIN AT XFS 390 AND STRINGER 11. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVE - [SDR RRXA001032](https://openairdocs.org/sdr/RRXA001032), Jan 3, 2000: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, OUTBOARD SLOT VANE BETWEEN XFS 430 TO XFS 440. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM - [SDR RRXA001024](https://openairdocs.org/sdr/RRXA001024), Jan 3, 2000: FITTING. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT FITTING AT STA 1020 AND LONGERON 21 LEFT. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMO - [SDR RRXA001023](https://openairdocs.org/sdr/RRXA001023), Jan 3, 2000: FITTING. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT FITTING AT STA 1040 AND LONGERON 21 LEFT. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMO - [SDR RRXA001031](https://openairdocs.org/sdr/RRXA001031), Jan 2, 2000: ATTACH ANGLE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM ATTACHMENT ANGLE AT STA 260, BL 65R AND WL-1. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. R - [SDR RRXA001029](https://openairdocs.org/sdr/RRXA001029), Jan 2, 2000: SPLICE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 33 LEFT SPLICE, BETWEEN STA 380 TO STA 440. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMO - [SDR RRXA000287](https://openairdocs.org/sdr/RRXA000287), Dec 30, 1999: SEAT TRACK. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FE'S FORWARD SEAT TRACK. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SR - [SDR RRXA99005](https://openairdocs.org/sdr/RRXA99005), Jan 15, 1999: SWITCH. FAILED. ON GEAR EXTENSION RIGHT MAIN GEAR LIGHTS WOULD NOT COME ON. SWAPPED BULBS FROM LEFT WITH NO HELP. REMOVED AND REPLACED RIGHT MAIN GEAR DOWNLOCK SWITCH, OPS CHEC ## 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 20000914037689I](https://openairdocs.org/incident/20000914037689I), Sep 14, 2000: Doug DC873 (N832AL), Middletown, PA. (-23) The aircraft was inbound for philadelphia airport when the flight crew noticed a flash of light and sparks from the rear cockpit. The cockpit filled with… ## Other aircraft with N832AL - [Registered now](https://openairdocs.org/aircraft/N832AL): Zipline International P2 ZIP, S/N 18736P22589 --- 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.