# N486EV: 1974 Boeing 747-212B, registration cancelled 2018-01-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 8, 2018
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 747-212B](https://openairdocs.org/model/boeing-747-212b) (registry code 1384886)
- Engine: [Pratt & Whitney JT9D series](https://openairdocs.org/engine/pratt-whitney-jt9d-series) (registry code 52054)
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE) (OpenAirDocs)
- Serial number: 20888
- Year built: 1974
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 21, 1983
- Certificate issued: June 9, 2001
- Last registry action: October 13, 2011
- Mode S code: A5FF5B
- Owner when cancelled: [Evergreen International Airlines Inc](https://openairdocs.org/faa-owner/EVERGREEN%20INTERNATIONAL%20AIRLINES%20INC)
- Location: [Mcminnville, OR](https://openairdocs.org/faa-place/OR/Mcminnville)
- Owner type: Corporation
- Owner's area on the map: 45.2117° N, 123.2817° W: Placed by OpenAirDocs at the center of ZIP code 97128, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N486EV
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=486EV
- Page: https://openairdocs.org/deregistered/N486EV-2018-01-08

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 Boeing 747-212B: https://openairdocs.org/model/boeing-747-212b.md

## Service difficulty reports (234, newest 50)

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

- [SDR EIAA20121108093](https://openairdocs.org/sdr/EIAA20121108093), Nov 8, 2012: LIGHT. INOPERATIVE. EMERGENCY LIGHT M/D BS 390 LEFT INOP. REPLACED M/D EMERGENCY LIGHT ASSY M415 BS 390 LEFT PER AMM 33-51-07 PG 201, OPS CHECK GOOD.
- [SDR EIAA20120923067](https://openairdocs.org/sdr/EIAA20120923067), Sep 23, 2012: STRIKER. MISSING. SIDE CARGO DOOR WARNING LIGHT ILLUMINATED WITH P4 CAUTION LIGHT. MX PRESSURIZED A/C TO GROUND LIMIT AND UNABLE TO DUPLICATE FAULT. IN PROGRESS CHECKING INTEGRIT
- [SDR EIAA20111219259](https://openairdocs.org/sdr/EIAA20111219259), Dec 19, 2011: ENGINE. MALFUNCTIONED. NR 4 ENGINE FIRE INDICATION. CREW REPORTED NR 4 ENGINE FIRE INDICATION AND BOTH FIRE BOTTLES DISCHARGED. PASSING THRU FL310 HEAD MUFFLED THUD FROM RIGHT SIDE, N
- [SDR EIAA20111012238](https://openairdocs.org/sdr/EIAA20111012238), Oct 12, 2011: CADC. FAILED. FIRST OFFICER SAT GAGE, ALTIMETER, MACH IND, FLIGHT DIRECTOR & AIRSPEED INOPERATIVE WITH ALTITUDE ALERT LIGHT ON. AUTO PILOT B INOPERATIVE, TRANSPONDER NR 2 ATC
- [SDR EIAA2011233](https://openairdocs.org/sdr/EIAA2011233), Oct 2, 2011: WARNING SWITCH. OUT OF ADJUST. SIDE CARGO DOOR OPEN LIGHT ILLUMINATED AT FL 310-8.2 DIFF PRESS, NO LOSS OF PRESSURIZATION DURING DEPRESSURIZATION AT FL 310. LIGHT EXTINGUISH AT APP 6.2 DIFF P
- [SDR EIAA2011232](https://openairdocs.org/sdr/EIAA2011232), Oct 2, 2011: WARNING SWITCH. DIRTY. AFTER LANDING - DURING TAXI TO PARKING, L5 DOOR OPEN LIGHT ILLUMINATED. CLEANED L5 DOOR WARNING SWITCH & PERFORMED ADJ/TEST PER AMM 52-71-00 SATISFACTORY. PERFO
- [SDR EIAA2011231](https://openairdocs.org/sdr/EIAA2011231), Oct 2, 2011: WARNING SWITCH. MALFUNCTIONED. SIDE CARGO DOOR OPEN LIGHT ILLUMINATED AT FL 290, COMPLETED QRH PROCEDURE AND DEPRESSURIZED AIRCRAFT. LIGHT EXTINGUISHED AT APP 5.8 DIFF. PRESSURE FL 255 CABIN 
- [SDR EIAA2011220](https://openairdocs.org/sdr/EIAA2011220), Aug 24, 2011: BATTERY PACK. DISCHARGED. THREE EACH EMERGRENCY EXIT LIGHT FAILED TO LIGHT UP IN MAIN DECK. THREE EACH EMERGENCY LIGHT BATTERY PACKS IN MAIN DECK REMOVED AND REPLACED. OPS CHECK CARRIED 
- [SDR EIAA2011219](https://openairdocs.org/sdr/EIAA2011219), Aug 24, 2011: STRAP. CRACKED. HFEC OPEN HOLE INSP ON BS 2213 BELOW S16L FOUND STRAP CRACKED. CRACKED STRAP REMOVED. NEW STRAP AND WEB FABRICATED PER BOEING DRAWINGS 65B61849 AND 65B05000 RES
- [SDR EIAA2011218](https://openairdocs.org/sdr/EIAA2011218), Aug 24, 2011: STRINGER. CRACKED. NR 2 PYLON (INTERIOR), PANEL CUTOUT NR 463CL AT NAC STA 180.0, I/B SRTINGER FOUND CRACKED. CRACKED STRINGER REMOVED AND REPLACED PER SRM 51-30-02.
- [SDR EIAA2011217](https://openairdocs.org/sdr/EIAA2011217), Aug 24, 2011: FRAME. CRACKED. FRAME AT BS 260 FWD S31A-R FOUND CRACKED. MAIN FRAME WEB AT BS 260 BETWEEN S27R AND S39R REMOVED. NEW WEB FABRICATED PER BOEING DRAWING 65B07934 AND INSTALLED P
- [SDR EIAA2011216](https://openairdocs.org/sdr/EIAA2011216), Aug 24, 2011: FLOORBEAM. DAMAGED. MAIN DECK, BS 500 TO 520, LBL 70, UPPER DECK FLOORBEAM WEB FOUND PUNCTURED AND DENTED BY LONG SCREW. CRACKED CHORD REMOVED AND REPLACED PER SRM 51-10-02.
- [SDR EIAA2011215](https://openairdocs.org/sdr/EIAA2011215), Aug 24, 2011: FLOORBEAM. CRACKED. MAIN DECK, BS 380 TO 400, RBL 10, UPPER DECK FLOORBEAM WEB UPPER CHORD FOUND CRACKED. CRACKED CHORD REMOVED AND REPLACED PER SRM 51-10-02.
- [SDR EIAA2011214](https://openairdocs.org/sdr/EIAA2011214), Aug 24, 2011: FRAME. DAMAGED. MAIN DECK RT FRAME RIVET HOLE ELONGATED AT BS 2231 AT WL 195. REPAIRED IN ACCORDANCE WITH EN 059-11 APPROVED BY BOEING ODAS.
- [SDR EIAA2011213](https://openairdocs.org/sdr/EIAA2011213), Aug 24, 2011: FRAME. CRACKED. MAIN DECK FRAME INNER CHORD CRACKED AT BS 2231 BETWEEN S16R & S18R. REPAIRED PER B747 SRM 53-10-04, FIGURE 140.
- [SDR EIAA2011212](https://openairdocs.org/sdr/EIAA2011212), Aug 24, 2011: FRAME. DAMAGED. FRAME FOUND DAMAGED WITH DRILL HOLES AT BS 180 BETWEEN S19R & S24R. DAMAGED FRAME REMOVED AND NEW FRAME INSTALLED PER SASCO EN 068-11 APPROVED BY BOEING ODAS.
- [SDR EIAA2011211](https://openairdocs.org/sdr/EIAA2011211), Aug 24, 2011: FRAME. DAMAGED. FRAME FOUND DAMAGED WITH DRILL HOLES AT BS 180 BETWEEN S19L & S24L. DAMAGED FRAME REMOVED AND NEW FRAME INSTALLED PER SASCO EN 068-11 APPROVED BY BOEING ODAS.
- [SDR EIAA2011210](https://openairdocs.org/sdr/EIAA2011210), Aug 24, 2011: FRAME. DAMAGED. FRAME FOUND DAMAGED WITH DRILL HOLES AT BS 220 BETWEEN S22R & S23R. DAMAGED FRAME REMOVED AND NEW FRAME INSTALLED PER EN 068-11 APPROVED BY BOEING ODAS.
- [SDR EIAA2011209](https://openairdocs.org/sdr/EIAA2011209), Aug 24, 2011: FRAME. DAMAGED. FRAME FOUND DAMAGED WITH DRILL HOLES AT BS 220 BETWEEN S19L & S24L. DAMAGED FRAME REMOVED AND NEW FRAME INSTALLED PER EN 068-11 APPROVED BY BOEING ODAS.
- [SDR EIAA2011208](https://openairdocs.org/sdr/EIAA2011208), Aug 24, 2011: SKIN. CHAFED. NR 2 PYLON LOWER SPAR WEB (EXTERIOR) SY NAC STA 180 TO 250 FOUND LT & RT PLATES CHAFED ADJ TO ENGINE THRUST UPPER LINK. REPAIRED PER B747 SRM 54-30-03 FIGURE 23
- [SDR EIAA2011207](https://openairdocs.org/sdr/EIAA2011207), Aug 24, 2011: CAP. CRACKED. NR 4 PYLON STA 280 LOWER END CAP ASSY FOUND CRACKED. CRACKED LOWER END CAP ASSY REMOVED. NEW END CAP FABRICATED PER BOEING DRAWING 69B90354 AND ISTALLED PER B74
- [SDR EIAA2011206](https://openairdocs.org/sdr/EIAA2011206), Aug 24, 2011: STRINGER. CRACKED. REMOVE AND REPLACE REPAIR ON S37R BETWEEN BS 421 & 430. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED PER B747 SRM 53-10-03 FIGURE 3.
- [SDR EIAA2011205](https://openairdocs.org/sdr/EIAA2011205), Aug 24, 2011: BEAR STRAP. CORRODED. L5 DOOR CUTOUT BEAR STRAP AT STA 2284 BETWEEN S24L & S25L FOUND CORRODED. REPAIRED IN ACCORDANCE WITH EN 044-11 APPROVED BY BOEING ODAS.
- [SDR EIAA2011204](https://openairdocs.org/sdr/EIAA2011204), Aug 24, 2011: STRINGER. CRACKED. REMOVE AND REPLACE REPAIR ON S38L BETWEEN BS 480 TO 500. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED PER B747 SRM 53-10-03 FIGURE 3.
- [SDR EIAA2011203](https://openairdocs.org/sdr/EIAA2011203), Aug 24, 2011: STRINGER. CRACKED. REMOVE AND REPLACE REPAIR ON S37L BETWEEN BS 460 & 480. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED PER B747 SRM 53-10-03 FIGURE 3.
- [SDR EIAA2011199](https://openairdocs.org/sdr/EIAA2011199), Aug 24, 2011: SKIN. CRACKED. HFEC INSPECTION FOUND APPROX 1 INCH CRACK THROUGH STOP DRILLED HOLE ON L1 DOOR SKIN UPPER HINGE CUTOUT RADIUS. REPAIRED IN ACCORDANCE WITH EN 048-11 APPROVED BY
- [SDR EIAA2011163](https://openairdocs.org/sdr/EIAA2011163), Aug 24, 2011: CHANNEL. DAMAGED. CHANNEL ON MAIN DECK FRAM AT BS 2020 BETWEEN S20R AND S22R DAMAGED. DAMAGED CHANNEL REMOVED. NEW CHANNEL FABRICATED AND INSTALLED PER B747 SRM 51-30-02.
- [SDR EIAA2011159](https://openairdocs.org/sdr/EIAA2011159), Aug 24, 2011: FRAME. DAMAGED. MAIN DECK FRAME DAMAGED DUE TO DRILL HOLE AT BS 1200 BETWEEN STRINGER 17R AND 21R. FRAME REPAIRED PER B747 SRM 51-4-04, FIGURE 3.
- [SDR EIAA2011202](https://openairdocs.org/sdr/EIAA2011202), Aug 23, 2011: STRINGER. CRACKED. STRINGER CRACKED AT BS 220 S0. CRACKED STRINGER REMOVED AND REPLACED WITH NEW STRINGER PER B747 SRM 51-30-02.
- [SDR EIAA2011201](https://openairdocs.org/sdr/EIAA2011201), Aug 23, 2011: SPLICE. CRACKED. ZEE SPLICE FOUND CRACKED AT BS 220 S4L. NEW ZEE SPLICE FABRICATED PER BOEING DRAWING 65B07618 AND INSTALLED PER SRM 51-30-02.
- [SDR EIAA2011183](https://openairdocs.org/sdr/EIAA2011183), Aug 21, 2011: SUPPORT BEAM. CRACKED. RT WING REAR SPAR CAVITY SPOILER SUPPORT BEAM UPPER CHORD AT WBL 235.2 FOUND CRACKED. CRACKED CHORD TRIMMED. HFEC INSP TO VERIFY CHORD IS CRACK FREE. FABRICATED
- [SDR EIAA2011179](https://openairdocs.org/sdr/EIAA2011179), Aug 21, 2011: SKIN. PUNCTURED. EMP - FUSELAGE LT AT APPROX BS 2670 ADJACENT TO VERT STAB SEAL RETAINER SKIN HAS A PUNCTURE. REPAIRED PER B747 SRM 53-30-03 FIGURE 2.
- [SDR EIAA2011178](https://openairdocs.org/sdr/EIAA2011178), Aug 20, 2011: BEAR STRAP. CRACKED. HFEC INSPECTION FOUND CRACKS AT BEARSTRAP AT L3 DOOR CUTOUT EDGE AFT UPPER CORNER. REPAIRED PER B747 SRM 53-30-03 AND EN 065-11.
- [SDR EIAA2011175](https://openairdocs.org/sdr/EIAA2011175), Aug 20, 2011: SPAR. CRACKED. DURING HFEC OPEN HOLE INSPECTION ON NR 3 PYLON FRONT SPAR CHORD FOUND 2 EA HOLE CRACKED. NR 3 PYLON FRONT SPAR CHORD REPAIRED PER BOEING SB 747-54A2158 AND SASC
- [SDR EIAA2011174](https://openairdocs.org/sdr/EIAA2011174), Aug 20, 2011: BULKHEAD. CRACKED. DURING HFEC OPEN HOLE INSPECTION FOUND CRACK AT LT BS 2598 BULKHEAD INNER CHORD. REPAIRED PER SASCO EN 047-11 APPROVED BY BOEING ODAR.
- [SDR EIAA2011172](https://openairdocs.org/sdr/EIAA2011172), Aug 20, 2011: BULKHEAD. CRACKED. DURING HFEC OPEN HOLE INSPECTION FOUND CARCK AT RT BS 2598 BULKHEAD INNER CHORD. REPAIRED PER EN 052-11 APPROVED BY BOEING ODAR.
- [SDR EIAA2011171](https://openairdocs.org/sdr/EIAA2011171), Aug 20, 2011: SPAR. CRACKED. DURING HFEC OPEN HOLE INSPECTION ON NR 2 PYLON FRONT SPAR CHORD FOUND 2 HOLE CRACKS. NR 2 PYLON FRONT SPAR CHORD REPAIRED PER BOEING SB 747-54A2158 AND EN 041-1
- [SDR EIAA2011166](https://openairdocs.org/sdr/EIAA2011166), Aug 19, 2011: DOUBLER. CRACKED. HFEC INSPECTION FOUND CRACK ON WEB DOUBLER ON L1 DOOR CUTOUT FRAME ST STA 488 FWD SIDE OF DOUBLER AT LWR EDGE OF DOOR STOP NR 1. DAMAGED FRAME REMOVED. NEW WEB 
- [SDR EIAA2011164](https://openairdocs.org/sdr/EIAA2011164), Aug 19, 2011: FLOORBEAM. CRACKED. UPPER DECK FLOORBEAM WEB AT BS 330 RBL 60 FOUND CRACKED. DAMAGED WEB REMOVED. FLOORBEAM UPPER CHORD TRIMMED OUT PER SRM 51-10-01 AND REPAIRED CARRIED OUT PER BO
- [SDR EIAA2011162](https://openairdocs.org/sdr/EIAA2011162), Aug 19, 2011: STRAP. CRACKED. OPEN HOLE HFEC INSP FOUND STRAP CRACKED AT UPPER DECK FLOORBEAM BS 340 LT COMMON TO CRES STRAPS INSTALLED ON UPPER CHORD VERTICAL FLANGE AREA. DAMAGED STRAP REM
- [SDR EIAA2011161](https://openairdocs.org/sdr/EIAA2011161), Aug 19, 2011: SHEAR TIE. CRACKED. MAIN DECK SHEAR TIE CRACKED AT BS 1180 AROUND LT S23 AREA. REPLACE CRACKED SHEAR TIE PER B747 SRM 51-30-02.
- [SDR EIAA2011160](https://openairdocs.org/sdr/EIAA2011160), Aug 19, 2011: FLOORBEAM. DAMAGED. FWD CARGO COMPARTMENT FLOORBEAM WEB AT BS 720 AT LBL 12 HAS A 1 INCH HOLE. FLOORBEAM WEB REPAIRED BER B747 SRM 53-10-04, FIG 70.
- [SDR EIAA2011157](https://openairdocs.org/sdr/EIAA2011157), Aug 16, 2011: SKIN. CRACKED. HFEC OPEN HOLE INSPECTION FOUND CRACK ON FUSELAGE SKIN AT BS 980 S38R. FUSELAGE SKIN REPAIRED FOR B747 SRM 53-30-03, FIGURE 60 WITH MINOR DEVIATIONS APPROVED BY
- [SDR EIAA2011145](https://openairdocs.org/sdr/EIAA2011145), Aug 12, 2011: DOUBLER. CRACKED. R1 MED FWD FRAME UNDER UPPER HINGE CUTOUT DOUBLER CRACKED. CRACKED DOUBLER REMOVED AND REPAIR CARRIED OUT PER B747 SRM 52-10-02, FIG 13.
- [SDR EIAA2011144](https://openairdocs.org/sdr/EIAA2011144), Aug 12, 2011: DOUBLER. CORRODED. RT BLG WW NEAR STA 1460 O/B FRAME, CEILING SKIN FOUND CORRODED. CORROSION REMOVED AND AREA BLENDED. AREA CLEANED & INSPECTED TO ENSURE COMPLETE CORROSION REMOVA
- [SDR EIAA2011140](https://openairdocs.org/sdr/EIAA2011140), Aug 12, 2011: STRINGER. DAMAGED. IN MAIN EQUIPMENT CENTER (MEC) STRINGER 36L FOUND DEFORMED AND RIVIT HOLE CRACKED AT BS 420. EXISTING REPAIR REMOVED, NEW CHORD FABRICATED PER DRAWING 65B09014,
- [SDR EIAA2011138](https://openairdocs.org/sdr/EIAA2011138), Aug 12, 2011: FRAME. CORRODED. LEFT BLG WW OVERWING LONGERON AT STA 1438, FRAME STRUCTURE HAS CORROSION. EXISTING REPAIR REMOVED, NEW CHORD FABRICATED PER DRAWING 65B09014, FOI CARRIED OUT OE
- [SDR EIAA2011137](https://openairdocs.org/sdr/EIAA2011137), Aug 12, 2011: STRINGER. CRACKED. OPEN HOLE HFEC INSPECTION FOUND 2 EACH CRACKS AT FASTENER HOLES ON STRINGER 38R AT BS 980. EXISTING REPAIR REMOVED, NEW CHORD FABRICATED PER DRAWING 65B09014, F
- [SDR EIAA2011135](https://openairdocs.org/sdr/EIAA2011135), Aug 12, 2011: STRINGER. DENTED. IN MAIN EQUIPMENT CENTER (MEC) STRINGER 38L BETWEEN BD 380 TO 400 FOUND DENTED. EXISTING REPAIR REMOVED, NEW CHORD FABRICATED PER DRAWING 65B09014, FOI CARRIED 
- [SDR EIAA2011126](https://openairdocs.org/sdr/EIAA2011126), Aug 11, 2011: FRAME. DEFORMED. MID FRAME DEFORMED & CHAFED AT BS 1849 AROUND RT S11 AREA. DEFORMED FRAME AT BS 1840 AT S-11R REPAIRED PER BOEING 747 SRM 51-40-03 FIG 2, DETAIL III.

All 234: https://openairdocs.org/deregistered/N486EV-2018-01-08/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CEN09LA114](https://openairdocs.org/ntsb/CEN09LA114), Dec 23, 2008: Boeing 747-212B (N486EV), Rockford, IL, substantial damage. Probable cause: The ground crew's failure to maintain clearance from the light pole while directing the airplane to parking.

## FAA accident and incident reports (2)

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 20111219028969I](https://openairdocs.org/incident/20111219028969I), Dec 19, 2011: Boeing 747-212B (N486EV), Minor damage. During climb crew reported a muffled thud and an illuminated #4 engine fire light. Crew accomplished emergency procedures checklist and returned to the airport.
- [Accident 20081223854799A](https://openairdocs.org/incident/20081223854799A), Dec 23, 2008: Boeing 747212B (N486EV), Chicago/Rockfo, IL, Substantial damage. (-23) As the aircraft was being marshalled into position the marshaller brought the Boeing 747 on the incorrect lead in line which was intended for Boeing 757…

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