# N1808E: 1969 Douglas DC-8-62, registration cancelled 2017-03-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 10, 2017
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Douglas DC-8-62](https://openairdocs.org/model/douglas-dc-8-62) (registry code 3021970)
- Engine: [Pratt & Whitney JT3D series](https://openairdocs.org/engine/pratt-whitney-jt3d-series) (registry code 52035)
- Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs)
- Serial number: 46105
- Year built: 1969
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 9, 1996
- Certificate issued: April 20, 1999
- Last registry action: April 15, 2008
- Mode S code: A14421
- Owner when cancelled: [Agro Air Associates Inc](https://openairdocs.org/faa-owner/AGRO%20AIR%20ASSOCIATES%20INC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Corporation
- Owner's area on the map: 25.7743° N, 80.1937° W: Placed by OpenAirDocs: center of Miami, FL, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N1808E
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1808E
- Page: https://openairdocs.org/deregistered/N1808E-2017-03-10

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 Douglas DC-8-62: https://openairdocs.org/model/douglas-dc-8-62.md

## Service difficulty reports (161, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ARWA20020207](https://openairdocs.org/sdr/ARWA20020207), Feb 26, 2002: COMPRESSOR. STALLED. UPON COMMENCING T/O ROLL NR 2 ENGINE COMPRESSOR STALLED SPEED NIL WIND CALM. AIRCRAFT RETURNED TO THE RAMP. PERFORMED VISUAL INSPECTION OF NR 2 ENGINE IN ACCORD
- [SDR ARWA20020105](https://openairdocs.org/sdr/ARWA20020105), Jan 5, 2002: VALVE. LOG PAGE 108167. DISCREPANCY:ON ATART UP WHEN # 2 ENGINE THROTTLE IS ADVANCED ENGINE SURGES AND VIBRATES. WHEN REVERSE IS SELECTED TR TRANSLATES AND BUCKET DEPL
- [SDR ARWA20011116](https://openairdocs.org/sdr/ARWA20011116), Nov 20, 2001: STRAP. CRACKED. DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND: NR 4 PYLON ACCESS DOOR 409 RT WITH TEMPORARY REPAIR, AFTER EVALUATION, FOUND CRACK ON OUTBOARD UPPER STRAP A
- [SDR ARWA20011107](https://openairdocs.org/sdr/ARWA20011107), Nov 20, 2001: FITTING. CRACKED. DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: AFT CARGO COMPT STA 980 BULKHEAD LT STIFFENER WITH 1.5 INCH CRACK, NEAR MAIN CARGO DOOR COMPARTMENT FLOOR. REMOV
- [SDR ARWA20011115](https://openairdocs.org/sdr/ARWA20011115), Nov 20, 2001: STRINGER. N/R 1080 - DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND: RH WING # 3 MAIN FUEL TANK INTERIOR BETWEEN STA. XRS 74 & SRS 107, STIFFENER 69 WITH 1.500" CRA
- [SDR ARWA20011114](https://openairdocs.org/sdr/ARWA20011114), Nov 20, 2001: FLOORBEAM. CRACKED. DURING "C" CHECK INSPECTION, STA 1120, X=10 RT SIDE, FLOORBEAM WEB WITH CORROSION. ACCOMPLISHED HFEC INSPECTION IAW DC-8 NDT MANUAL CHAPTER 06, FOUND CRACK OF 0
- [SDR ARWA20011113](https://openairdocs.org/sdr/ARWA20011113), Nov 20, 2001: SKIN PANEL. N/R 1076 - DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND: RH INBOARD FLAP LOWER SKIN WITH CRACK OF 0.500" BETWEEN STA. XW 92 & XW 104 FAIRING AREA.CORREC
- [SDR ARWA20011112](https://openairdocs.org/sdr/ARWA20011112), Nov 20, 2001: PLATE. N/R 1068 - DURING "C" CHECK, THE FOLLOWING WAS FOUND: LH WING I/B FLAP LOWER SKIN WITH DENT AT STA. XW L7.CORRECTIVE ACTION: FOUND DENT OUT OF LIMITS IAW DC8 SR
- [SDR ARWA20011111](https://openairdocs.org/sdr/ARWA20011111), Nov 20, 2001: NOZZLE. CRACKED. DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: NR 4 ENGINE EXHAUST NOZZLE SPLITTER WITH CRACK AT 2 O'CLOCK. REMOVED SPLITTER; FABRICATED NEW SPLITTER IAW DC8 S
- [SDR ARWA20011110](https://openairdocs.org/sdr/ARWA20011110), Nov 20, 2001: FITTING. N/R 440 - DURING "C" CHECK INSPECTION, FOUND THE FOLLOWING: RH WING # 4 ALT. TANK INTERIOR STA. XRS 408.00 STRINGER # 58 END FITTING WITH CRACK.CORRECTIVE ACTIO
- [SDR ARWA20011108](https://openairdocs.org/sdr/ARWA20011108), Nov 20, 2001: PLATE. N/R 412 - DURING "C" CHECK INSPECTION, FOUND THE FOLLOWING: RH HORIZONTAL STABILIZER TIE STA. XE 77.000 AND 92.000 UPPER SKIN WITH INNER CORROSION.CORRECTIVE AC
- [SDR ARWA20011106](https://openairdocs.org/sdr/ARWA20011106), Nov 20, 2001: SKIN. CORRODED. DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: RT HORIZONTAL STABILIZER T/E BETWEEN STA 175.000 & STA 190.000 UPPER SKIN WITH INNER CORROSION. REMOVED CORROSIO
- [SDR ARWA20011105](https://openairdocs.org/sdr/ARWA20011105), Nov 20, 2001: PLATE. N/R 192 - DURING "C" CHECK INSPECTION, FOUND THE FOLLOWING: LH ELEVATOR LWR SKIN WITH CORRUGATION & OIL CANNING IN SEVERAL POINTS, BETWEEN STA. XE 28.343 AND XE
- [SDR ARWA0010603](https://openairdocs.org/sdr/ARWA0010603), Jun 8, 2001: LINK ROD. DEFECTIVE. AFTER TAKEOFF OUT OF KMIA AND RAISED THE LANDING GEAR EXPERIENCED HEAVY NOSE VIBRATION. RECYCLED LANDING GEAR, BUT DID NOT HELP. DECLARED EMERGENCY AND LANDED O
- [SDR ARWA0010310](https://openairdocs.org/sdr/ARWA0010310), Mar 30, 2001: GUIDE. LOOSE. RADAR WILL NOT PAINT WEATHER. AIRCRAFT DIVERTED TO MIAMI AND LANDED WITHOUT INCIDENT. TIGHTENED WAVE GUIDE; OPS CHECK NORMAL IAW MM 34-41-0.
- [SDR ARWA0010303](https://openairdocs.org/sdr/ARWA0010303), Mar 6, 2001: TIRE. SEPARATED. AFTER TAKEOFF FROM KATL ATC ADVISED FLIGHT 509 THAT A TIRE WAS LEFT ON THE RUNWAY, FLIGHT CREW REPORTED THE INCIDENT TO MIAMI MX AND CONTINUE TO TJSJ. EMERGENCY
- [SDR ARWA0010103](https://openairdocs.org/sdr/ARWA0010103), Jan 28, 2001: BLEED VALVE. DIRTY. AT THE BEGINNING OF TAKEOFF ROLL NR 2 ENGINE HAD COMPRESSOR STALL. ENGINE PARAMETER WERE TAKEOFF, EPR WAS 1.88; DROPPED TO 1.75 N2 AND RECOVERED, FUEL FLOW DMI 
- [SDR ARWA0010102](https://openairdocs.org/sdr/ARWA0010102), Jan 25, 2001: BALLAST. SMOKE. DURING DESCENT, CO-PILOTS RADAR SCREEN HAD EVIDENCE OF SMOKE. TURNED OFF AND PULLED C/B. CHECKED WEATHER RADAR SYSTEM WIRING IAW W/D 34-10-0, FOUND NORMAL. GROU
- [SDR ARWA0001204](https://openairdocs.org/sdr/ARWA0001204), Dec 23, 2000: SWITCH. DEFECTIVE. AFTER TAKE OFF KATL, DOOR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. PERFORMED ABNORMAL PROCEDURE. UNABLE TO EXTINGUISH LIGHT; AIRCRAFT DIVERTED TO MI
- [SDR 99T64R297AR](https://openairdocs.org/sdr/99T64R297AR), Aug 14, 1999: SKIN. CORRODED. NR 0928 - PREVIOUS REPAIR SKIN CORRODED AND CORROSION EMANATING FROM UNDER REPAIR DOUBLER RIGHT WING UPPER SKIN STATION XW 50 STRINGER 11. REMOVED DOUBLERS. REM
- [SDR 99T64R348AR](https://openairdocs.org/sdr/99T64R348AR), Jul 15, 1999: DUCT. CHAFED. LEFT UPPER NOSE SECTION AC DUCT (HORSE SHOE) DUCT HAS HOLE CHAFFED IN IT. FABRICATED DOUBLER STRAP AND WELDED TO DUCT IAW BOEING MESSAGE M-7200-99-03383. (M)
- [SDR 99T64R344AR](https://openairdocs.org/sdr/99T64R344AR), Jul 15, 1999: SKIN. DENTED. RIGHT WING BOTTOM OUTBOARD OF RIGHT MLG PANEL DENTED IN TWO PLACES STATION XW90. NDT AREA, NO CRACKS NOTED, FILLED DENTS WIT HYSOL EA 934 NA, FABRICATED DOUBLER
- [SDR 99T64R358AR](https://openairdocs.org/sdr/99T64R358AR), Jul 9, 1999: TUBE. LOOSE. LEFT NOSE SCOOP ANTI-ICE TUBE T PULLED LOOSE FROM DUCT OUTBOARD OF VALVE. REINSTALLED T AND WELDED PER EO 99-061. (M)
- [SDR 99T64R357AR](https://openairdocs.org/sdr/99T64R357AR), Jul 9, 1999: TUBE. CHAFED. RIGHT NOSE CHIN SCOOP ANTI-ICE TUBE T PULLED LOOSE AND CHAFFED HALF THROUGH O/B OF VALVE. WELDED CHAFFED AREA, REINSTALLED T TUBE AND WELDED PER EO 99-061. (M)
- [SDR 99T64R334AR](https://openairdocs.org/sdr/99T64R334AR), Jul 8, 1999: TUBE. MISSING. FLT 2823 - CABIN SMOKE DETECTOR LINES AND END FITTINGS NOT INSTALLED. FABRICATED AND INSTALLED SMOKE DETECTOR TUBES AND FITTINGS IAW AS ELEVEN DWG AS 11045 WITH
- [SDR 99T64R350AR](https://openairdocs.org/sdr/99T64R350AR), Jul 7, 1999: SPAR. CRACKED. RIGHT WING LOWER FORWARD TANG OF FRONT SPAR OUTBOARD OF STATION XFS 515, 3 HOLES CRACKED. REMOVED NUT CHANNEL IAW DC-8 SRM 51-1-21. REAMED HOLES, EDDY CURRENT H
- [SDR 99T64R370AR](https://openairdocs.org/sdr/99T64R370AR), Jul 7, 1999: DUCT. WORN. NR 2 ENGINE STARTER SUPPLY DUCT BADLY WORN. WELDED DUCT IAW BOEING MESSAGE M7200-99-05-0359. (M)
- [SDR 99T64R343AR](https://openairdocs.org/sdr/99T64R343AR), Jul 7, 1999: GUIDE. BROKEN. RIGHT WING INBOARD LEADING EDGE OUTBOARD END HAS CABLE GUIDE (PHENOLIC BLOCK) BROKEN. APPLIED EPOXO 88 TWO PART EPOXY WITH AN ADDITIONAL 4 FASTENERS PER EO 99-0
- [SDR 99T64R386AR](https://openairdocs.org/sdr/99T64R386AR), Jul 7, 1999: FITTING. DAMAGED. NR 2579 - REMOVE FLAP CANOE FITTING AT STATION XF340, HOLE ELONGATED. REMOVED FLAP CANOE FITTING AT STATINO XF340 IAW DC-8 MM 27-51-12. REPLACED FLAP CANOE FITT
- [SDR T64R387AR](https://openairdocs.org/sdr/T64R387AR), Jul 5, 1999: COVER. PUNCTURED. ARROW AIR - NR 2073, LEFT HORIZ STABILIZER T/E OUTBOARD DAMPER WELL HOLE PUNCHED THROUGH. REMOVED DAMPER WELL COVER IAW DC-8 SRM 51-1-21, WELDED HOLE PER EO 99-
- [SDR 99T64R283AR](https://openairdocs.org/sdr/99T64R283AR), Jun 25, 1999: DUCT. CRACKED. NR 3050 - NR 3 TURBO COMPRESSOR OIL COOLING DUCT CRACKED. WELDED CRACK IAW BOEING MESSAGE M-7200-99-05081. ARROW AIR (M)
- [SDR 99T64R258AR](https://openairdocs.org/sdr/99T64R258AR), Jun 25, 1999: DUCT. CRACKED. NR 0161 - CSD OIL COOLER DUCT CRACKED AT FORWARD MOUNTING FLANGE ENG S/N 670982 NR 4 POSITION. WELDED CRACK IAW BOEING ENGINEERING MESSAGE M-7200-99-05081 WITH 
- [SDR 99T64R367AR](https://openairdocs.org/sdr/99T64R367AR), Jun 24, 1999: PANEL. CORRODED. RIGHT OUTBOARD INBOARD SLOT PANEL HAS CORROSION XS 442.185. REMOVED CORROSION AND BLENDED AREA IAW EO 99-061. (M)
- [SDR 99T64R243AR](https://openairdocs.org/sdr/99T64R243AR), Jun 17, 1999: ACCESS DOOR. CRACKED. NR 1066 - ACCESS DOOR STA 1380 BENT AND CRACKED (PLEXIGLASS CRACKED). FABRICATED NEW ACCESS DOOR PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-10-99. REF:
- [SDR 99T64R341AR](https://openairdocs.org/sdr/99T64R341AR), Jun 15, 1999: ANGLE. MISINSTALLED. MAIN CARGO DOOR UPPER JAM INSTALLATION Z ANGLE INCORRECTLY INSTALLED STATION 450. DOES NOT EFFECT THE INTEGRITY OF THE DOOR. NO CORRECTIVE MEASUREMENTS NECESSAR
- [SDR 99T64R241AR](https://openairdocs.org/sdr/99T64R241AR), Jun 15, 1999: FRAME. CRACKED. NR 0762 - 6 INCH CRACK IN NR 3 PYLON CAP FORMER (HORSE COLLAR) FORWARD SECTION STA YN161. FABRICATED REPLACMENT PART PER EO 99-061 WITH APPROVED FAA FORM 8110-3
- [SDR 99T64R383AR](https://openairdocs.org/sdr/99T64R383AR), Jun 9, 1999: SKIN. GOUGED. NR 0907 D-PIT DOOR CUTOUT - SKIN FORWARD LOWER EDGE GOUGED. CUT OUT DAMAGED AREA, FABRICATED FILLERS AND DOUBLERS, AND INSTALLED PER EO 99-048 AND 99-061 WITH A
- [SDR 99T64R252AR](https://openairdocs.org/sdr/99T64R252AR), Jun 9, 1999: SKIN. DAMAGED. NR 2392 - LEFT INBOARD FLAP WEDGE, DAMAGED SKIN LOWER STA XW 47. FABRICATED NEW LOWER SKIN LEFT INBOARD FLAP WEDGE PER EO 99-061 WITH APPROVED FAA FORM 8110-3 D
- [SDR 99T64R349AR](https://openairdocs.org/sdr/99T64R349AR), Jun 7, 1999: DUCT. CHAFED. HEAVY CHAF MARK NR 3 ENGINE STARTER DUCT 10 OCL POS. FABRICATED DOUBLERS AND WELDED ON DUCT IAW BOEING MESSAGE M-7200-99-04226. (M)
- [SDR 99T64R346AR](https://openairdocs.org/sdr/99T64R346AR), Jun 7, 1999: ANGLE. DAMAGED. CLEAN INSPECT REPAIR AS NECESSARY ALL SIDE RAIL SYSTEM. CUT OUT DAMAGED AREAS FABRICATED ANGLE TIERNAY AND INSTALLED PER AS 11040. (M)
- [SDR 99T64R337AR](https://openairdocs.org/sdr/99T64R337AR), Jun 7, 1999: BEAM. MISMANUFACTURED. MAIN CARGO DOOR JAM AFT JAM AFT BEAM INBOARD LEAG TO SHORT. FABRICATED DOUBLER SHIM/SPACER IAW EO DWG AS 11042. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLE
- [SDR 99T64R336AR](https://openairdocs.org/sdr/99T64R336AR), Jun 7, 1999: BEAM. SHORT. FLT 2851 - MAIN CARGO DOOR FORWARD JAMB - FORWARD BEAM INBOARD LEG TOO SHORT. FABRICATED DOUBLER SHIMS IAW EO DWG AS11042, TREATED AND PRIMED IAW DC-8 SRM 51-1-
- [SDR 99T64R265AR](https://openairdocs.org/sdr/99T64R265AR), Jun 7, 1999: SPAR. CORRODED. NR 2841 - LT WING REAR SPAR HAS 4 EACH AREAS OF CORROSION BETWEEN XRS 139-172. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED SPECIAL WASHERS AND DOUBLER, IN
- [SDR 99T64R345AR](https://openairdocs.org/sdr/99T64R345AR), Jun 4, 1999: SPAR. CORRODED. LT WING AFT SPAR HAS 7 EACH AREAS OF CORROSION AT XRS 190. REMOVED CORROSION, FABRICATED SPECIAL WASHERS AND DOUBLERS AND INSTALLED PER EO 99-061. (M)
- [SDR 99T64R368AR](https://openairdocs.org/sdr/99T64R368AR), Jun 3, 1999: DOOR. CORRODED. FORWARD RIGHT O/W EXIT DOOR CORROSION WINDOW FRAME INTERNAL STATION 730. REMOVED CORROSION FILLED WITH HYSOL EA 9309NA. FAIRED TO ORIGINAL THICKNESS. TREATED AN
- [SDR 99T64R260AR](https://openairdocs.org/sdr/99T64R260AR), Jun 3, 1999: WINDOW FRAME. CORRODED. NR 2633 - AFT LT OVER WING DOOR, WINDOW FRAME CORRODED STA 798 - STA 822.500. REMOVED CORROSION IAW DC-8 SRM 51-1-8. INSTALLED HYSOL 9309NA, FAIR TO ORIGINAL TH
- [SDR 99T64R251AR](https://openairdocs.org/sdr/99T64R251AR), Jun 3, 1999: WINDOW FRAME. CORRODED. NR 2286 - FORWARD LT O/W EXIT DOOR, CORROSION WINDOW FRAME INTERNAL. STA 717-742. REMOVED CORROSION IAW DC-8 SRM 51-1-8. INSTALLED HYSOL EA 9309NA TO FRAME, FAI
- [SDR 99T64R250AR](https://openairdocs.org/sdr/99T64R250AR), Jun 3, 1999: WINDOW FRAME. CORRODED. NR 2285 - AFT RIGHT O/W EXIT DOOR, CORROSION WINDOW FRAME INTERNAL. STA 798 - STA 822.500. REMOVED CORROSION IAW DC-8 SRM 51-1-8. INSTALLED HYSOL EA 9309NA TO F
- [SDR 99T64R269AR](https://openairdocs.org/sdr/99T64R269AR), Jun 2, 1999: FLOORBEAM. CORRODED. NR 2958 - CORROSION BLISTER AFT SIDE CABIN FLOORBEAM STA 1120 RBL 34 INCHES. REMOVE CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER AND INSTALLED PER EO 99-01
- [SDR 99T64R267AR](https://openairdocs.org/sdr/99T64R267AR), Jun 2, 1999: NUTPLATE. MISSING. NR 288 - TWO EACH, CHANNEL NUTPLATES AND SCREWS MISSING LT INBOARD L/E FUEL TANK XRS 64-XFS 14. INSTALLED NAS-1670-4 BLIND FASTENERS PER EO 99-061 WITH APPROVED

All 161: https://openairdocs.org/deregistered/N1808E-2017-03-10/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 19930714030709I](https://openairdocs.org/incident/19930714030709I), Jul 14, 1993: Doug DC862 (N1808E), Miami, FL. Aircraft blew NR3 and NR4 main tires while taxiing to gate. Found anti skid unit faulty.

## Other aircraft with N1808E

- [Cancelled 1965-05-27](https://openairdocs.org/deregistered/N1808E-1965-05-27): Aeronca 7AC, S/N 7AC-5375. Owner: [Usaf Nouasseur Aero Club](https://openairdocs.org/faa-owner/USAF%20NOUASSEUR%20AERO%20CLUB), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)

---
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.