# N482EV: 1973 Boeing 747-212B, registration cancelled 2018-02-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 7, 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: 20713
- Year built: 1973
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 21, 1983
- Certificate issued: August 21, 2003
- Last registry action: March 6, 2012
- Mode S code: A5F07F
- 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/N482EV
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=482EV
- Page: https://openairdocs.org/deregistered/N482EV-2018-02-07

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 (355, newest 50)

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

- [SDR EIAA20120813061](https://openairdocs.org/sdr/EIAA20120813061), Aug 12, 2012: SKIN. CORRODED. EXTERIOR SKIN AT BS 2360 APPROX STRINGER 6L FOUND SKIN BULGING. REMOVED DAMAGE FROM STRINGER 3 TO 8L IAW SRM 51-10-01. ACCOMPLISHED HFEC AND DVI OF CUT­ OUT LAW
- [SDR EIAA20120813060](https://openairdocs.org/sdr/EIAA20120813060), Aug 12, 2012: SKIN. CRACKED. SKIN CRACKED AT NR 1 PYLON FWD STRUT ACCESS PANEL NR 452AL. CRACK FOUND TO BE OUT OF LIMITS LAW SRM 54-30-01. REMOVED DAMAGE LAW SRM 51-10-01. PERFORMED HFEC OF
- [SDR EIAA20120813059](https://openairdocs.org/sdr/EIAA20120813059), Aug 12, 2012: STRUCTURE. CHAFED. NR 4 PYLON STRUT FORWARD ENGINE MOUNT BULKHEAD O/B CHORD CHAFED. PERFORMED BLEND OUT OF DAMAGE LAW B747 SRM 54-10-01. PERFORMED UT THICKNESS CHECK OF BLENDED AR
- [SDR EIAA20120813058](https://openairdocs.org/sdr/EIAA20120813058), Aug 12, 2012: STRUCTURE. CHAFED. NR 3 PYLON STRUT FORWARD ENGINE MOUNT BULKHEAD O/B CHORD CHAFED. PERFORMED BLEND OUT OF DAMAGE LAW B747 SRM 54-10-01. PERFORMED UT THICKNESS CHECK OF BLENDED AR
- [SDR EIAA20120822064](https://openairdocs.org/sdr/EIAA20120822064), Aug 10, 2012: SHIELD. DAMAGED. NR 4 PYLON 1/B FIRE SHIELD DAMAGED NAC STATION 235. BLENDED DAMAGE ON FIRE SHIELD IAW SRM 54-30-03 FIG 23 FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER O
- [SDR EIAA20120822063](https://openairdocs.org/sdr/EIAA20120822063), Aug 10, 2012: SKIN. DAMAGED. EXTERIOR SKIN AT APPROX BS 1620 BETWEEN STRINGERS 4L AND 5L FOUND DAMAGED. REMOVED DAMAGE IAW SRM 53-30-01, FOUND REMAINING MATERIAL AFTER BLENDING OUT OF LIMIT
- [SDR EIAA20120822062](https://openairdocs.org/sdr/EIAA20120822062), Aug 10, 2012: SKIN. DAMAGED. EXTERNAL FUSELAGE BELOW AND AFT OF L1 DOOR AT BS 490 DAMAGED. REMOVED DOUBLER IAW SRM 51-30-02. FABRICATED NEW DOUBLER IAW SRM 53-30-03 FIG 01. TREATED PRIMED I
- [SDR EIAA20120625052](https://openairdocs.org/sdr/EIAA20120625052), Jun 23, 2012: LIGHT. INOPERATIVE. AFT LEFT UPPER DECK EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT UPPER DECK EMERGENCY LIGHT ASSEMBLY PER AMM 33-51-01 PG 201. OP'S CHECKED GOOD.
- [SDR EIAA20120506041](https://openairdocs.org/sdr/EIAA20120506041), May 6, 2012: CONTROL PANEL. MALFUNCTIONED. APU "A" FIRE LOOP INTERMITTENT WITH BELL. TROUBLESHOT SYSTEM FOUND "A" LOOP LIGHT ASSY HAS MASTER DIM/TEST TERMINAL BROKEN ON LIGHT ASSY IT'S SELF. LIGHT NR 6 P
- [SDR EIAA20111224263](https://openairdocs.org/sdr/EIAA20111224263), Dec 24, 2011: FIRE DETECTOR. FALSE ACTIVATION. DURING DESCENT APU FIRE DET"A" LOOP LIGHT STARTED FLICKERING. SHOOK DOWN "A" LOOP AND WIRES. CAN NOT DUPUCIATE PROBLEM, CLEANED WIRE HARNESS REF AMM 20-10-04. O
- [SDR EIAA20111217262](https://openairdocs.org/sdr/EIAA20111217262), Dec 17, 2011: SWITCH. BURNED. ON DEPARTURE, DURING THE LAST SEGMENT, A PUNGENT ODOR WAS DETECTED FOLLOWED BY VISUAL SMOKE ROLLING AND EMITTING OUT OF OVERHEAD PANEL BETWEEN LANDING LIGHT SWI
- [SDR EIAA20111115252](https://openairdocs.org/sdr/EIAA20111115252), Nov 15, 2011: LIGHT. INOPERATIVE. EMERGENCY LIGHT IN STAIRWAY DOME INOPERATIVE. REMOVED, REPAIRED AND REINSTALLED LIGHT ASSY. PER MM 33-51-07 PG. 201 - 203
- [SDR EIAA20111115254](https://openairdocs.org/sdr/EIAA20111115254), Nov 15, 2011: FRAME. MISREPAIRED. AFT CARGO PIT FWD, CARGO DOOR JAMB BS 1810 STR. 39R FRAME REPAIRED INCORRECTLY. MAJOR REPAIR ACCOMPLISHED. REMOVED, REPAIR, FABRICATED NEW REPAIR AND INSTALLED 
- [SDR EIAA20111115253](https://openairdocs.org/sdr/EIAA20111115253), Nov 15, 2011: STRUCTURE. DAMAGED. DURING DOWN JACKING OF ACFT, BOARDING STAND IMPACTED AT BS 540 S23L. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER SR
- [SDR EIAA20111109249](https://openairdocs.org/sdr/EIAA20111109249), Nov 9, 2011: B-NUT. LOOSE. DUE TO NR 4 HYD SYSTEM LEVEL LOW PERFORMED ALT GEAR EXTENSION WING OPEN. FLUID LEVEL CAME UP SO GEAR WAS RECYCLED AND RE-EXTENDED NORMALLY WITHOUT FURTHER INCID
- [SDR EIAA20111017239](https://openairdocs.org/sdr/EIAA20111017239), Oct 17, 2011: OVEN. CONTAMINATED. DURING INSPECTION, OVEN FOUND WITH EXCESSIVE GREASE BUILD UP ON OVEN TRAYS & OVEN INNER LINING. CLEANED OVEN & PERFORMED OPS AS PER AMM 25-31-00
- [SDR EIAA2011238](https://openairdocs.org/sdr/EIAA2011238), Oct 17, 2011: OVEN. MALFUNCTIONED. OVEN WAS TURNED ON AND SMOKED. DEFERRED PER MEL 25-21-2. UNINSTALLED PLACARD. ACCOMPLISHED INSPECTION AS PER MM 05-51-50. PROCEDURES AS PER MM 21-00-01 NOT REQU
- [SDR EIAA2011237](https://openairdocs.org/sdr/EIAA2011237), Oct 8, 2011: FIRE WARNING. FALSE ACTIVATION. DURING DESCENT AT APPROX 10,000FT APU FIRE BELL SOUNDED BRIEFLY AND "A" LOOP LIGHT ILLUMINATED. CLEANED C/P FIRE DET SYS, PERFORMED OPS TEST PER MM 26-15-00. OP
- [SDR EIAA2011234](https://openairdocs.org/sdr/EIAA2011234), Oct 3, 2011: CIRCUIT CARD. NOT SEATED. APU FIRE LOOP A BEGAN TO FLICKER DURING DESCENT. RESEATED A5 CIRCUIT GOOD AS PER MM 26-11-03.
- [SDR EIAA2011221](https://openairdocs.org/sdr/EIAA2011221), Aug 25, 2011: SMOKE DETECTOR. FAULTY. MAIN DECK SMOKE DETECTOR 2 INTERMITTENTLY ILLUMINATES NO EVIDENCE OF SMOKE PRESENT. ITEM PLACED ON DMI 387 PER MEL 26-11 CAT C PLACARDS INSTALLED. SWAPPED SMOKE
- [SDR EIAA2011155](https://openairdocs.org/sdr/EIAA2011155), Aug 22, 2011: SMOKE DETECTOR. FALSE ACTIVATION. MAIN DECK SMOKE DETECTOR NR 2 COMES ON IN FLIGHT - NO SMOKE. TEST SMOKE DETECTOR IAW AMM 26-14-00. OPS OK NO DEFECTS NOTED.
- [SDR EIAA2011150](https://openairdocs.org/sdr/EIAA2011150), Aug 20, 2011: SMOKE DETECTOR. MALFUNCTIONED. NR 2 MAIN DECK CARGO SMOKE DETECTOR LIGHT CAME ON NUMEROUS TIMES IN FLIGHT, VISUAL CHECK NORMAL. REPLACED MAIN DECK 2B SMOKE DETECTOR PER MM 26-14-02. ON GROUND
- [SDR EIAA2011154](https://openairdocs.org/sdr/EIAA2011154), Aug 19, 2011: SMOKE DETECTOR. MALFUNCTIONED. NR 2 MAIN DECK SMOKE DETECTOR LIGHT INTERMITTENT ON AND OFF. PERIODIC CHECKS REVEALED NO SMOKE. RESEATED NR 2 MAIN SMOKE DET CP PER 26-14-01.
- [SDR EIAA2011100](https://openairdocs.org/sdr/EIAA2011100), Aug 7, 2011: HANDLE. OUT OF POSITION. AFTER GEAR RETRACTION, BOTH LEFT AND RIGHT GEAR DOORS STAYED OPEN WITH GEAR HANDLE UP ACCOMPANIED BY GEAR DOOR LIGHT ON FWD ANNUCIATOR. ON SYSTEM CHECKOUT AND I
- [SDR EIAA2011095](https://openairdocs.org/sdr/EIAA2011095), Jul 27, 2011: SMOKE DETECTOR. FAILED. THE 3A MAIN DECK SMOKE DETECTOR WILL NOT TEST. TRANSFERRED TO DMI 352 AS PER MEL 26-11-1 CAT C DUE AUGUST 6, 2011 PLACARD INSTALLED. R&R SMOKE DETECTOR PER AMM 
- [SDR EIAA2011078](https://openairdocs.org/sdr/EIAA2011078), Jul 4, 2011: CONNECTOR. DISCONNECTED. CREW REPORTED TO TECH CENTER THAT THE NR 3 RT LED GROUP WAS STUCK IN TRANSIT. LIGHTS ON FLIGHT ENGINEERS PANEL INDICATED GROUP IN TRANSIT WHILE ALL OTHERS INDIC
- [SDR EIAA2011074](https://openairdocs.org/sdr/EIAA2011074), Jun 30, 2011: SMOKE DETECTOR. FAULTY. NR 2 MAIN DECK SMOKE DETECTOR ILLUMINATED INTERMITTENTLY DURING FLIGHT. ITEM TRANSFERRED TO DMI 328 PER MEL 26-11 CAT C OPTION 1 PLACARDS INSTALLED. DMI 328 CLE
- [SDR EIAA2011073](https://openairdocs.org/sdr/EIAA2011073), Jun 30, 2011: SMOKE DETECTOR. FAULTY. ON TAXI IN NR 2 MAIN DECK CARGO SMOKE DETECTOR ILLUMINATED. REPLACED NR 2B AND NR 3A MAIN CARGO SMOKE DETECTORS PER B747 MM 26-14-01 OP'S CHECK GOOD PER B747 MM
- [SDR EIAA2011072](https://openairdocs.org/sdr/EIAA2011072), Jun 26, 2011: CONNECTOR. DIRTY. NR 2 MAIN DECK CARGO SMOKE DETECTOR LIGHT FLICKERED DURING FLIGHT. CLEANED CONNECTOR ON SMOKE DETECTOR BOX OP'S CHECK OK PER MM 26-10-00.
- [SDR EIAA2011061](https://openairdocs.org/sdr/EIAA2011061), Jun 20, 2011: SMOKE DETECTOR. MALFUNCTIONED. NR 5 MAIN DECK SMOKE DETECTOR ILLUMINATED AND REMAINED ON FOR APPROX 10 MINTUES COMPLIED WITH EMERGENCY PROCEDURES. PER TECH CENTER SWAPPED 5B AND 2B AND 5A AND
- [SDR EIAA2011060](https://openairdocs.org/sdr/EIAA2011060), Jun 20, 2011: SMOKE DETECTOR. MALFUNCTIONED. NR 5 MAIN DECK SMOKE DETECTOR ILLUMINATED. VISUAL CHECK OF CARGO COMPARTMENT NO SMOKE NOTED. TROUBLE SHOT AND OP'S CHECK NR 5 CARGO SMOKE DETECTOR PER AMM26-14-
- [SDR EIAA2011059](https://openairdocs.org/sdr/EIAA2011059), Jun 20, 2011: FITTING. LOOSE. EN ROUTE EDFH NR 5 MAIN DECK SMOKE DETECTOR ILLUMINATED. EMERGENCY PROCEDURES COMPLIED WITH. LANDED AT CYQX. CARGO AREA INSPECTED NO EVIDENCE OF SMOKE OR FIRE. 
- [SDR EIAA2011068](https://openairdocs.org/sdr/EIAA2011068), Jun 18, 2011: SMOKE DETECTOR. FALSE ACTIVATION. MAIN DECK CARGO FIRE ZONE 5 RED LIGHT ILLUMINATED-INTERMITTENT. ON GROUND PERFORMED MAIN DECK CARGO SMOKE DETECTOR SYS OP'S CHECK GOOD PER AMM 26-14-00
- [SDR EIAA2011067](https://openairdocs.org/sdr/EIAA2011067), Jun 17, 2011: SMOKE DETECTOR. FALSE ACTIVATION. MAIN DECK CARGO SMOKE DETECTOR POSITION 4 ILLUMINATED. CONFIRMED NO SMOKE ON ENTIRE MAIN DECK. ACCOMPLISHED MAIN CARGO SMOKE DETECTOR SYS OP'S CHECK PER AMM 26-
- [SDR EIAA2011058](https://openairdocs.org/sdr/EIAA2011058), Jun 17, 2011: FLOORBEAM. CORRODED. FWD CARGO FLOORBEAM BS 640 LBL HAS CORROSION UNDER NUT PLATE FWD SIDE OF T-CHORD. REMOVED CORROSION REPLACED T-CAP INSTALLED REPAIR ANGLES PER B747 SRM 51-40-04
- [SDR EIAA2011056](https://openairdocs.org/sdr/EIAA2011056), Jun 17, 2011: SKIN. CORRODED. FWD CARGO PIT SKIN HAS CORROSION BS 1000 STR 40 TO 42 LT. REMOVED CORROSION, FABBED AND INSTALLED REPAIR DOUBLER PER B747 SRM 53-30-03 PGS 27-30.
- [SDR EIAA2011055](https://openairdocs.org/sdr/EIAA2011055), Jun 17, 2011: SKIN. CRACKED. BS 2060 ONE ROW OF FASTENERS ABOVE STR 45R HAS SKIN CRACK 1.5 INCH LONG BETWEEN AND PAST 2 FASTENERS. REMOVED DAMAGE, FABBED REPAIR DOUBLER AND FILLER AND INSTA
- [SDR EIAA2011054](https://openairdocs.org/sdr/EIAA2011054), Jun 17, 2011: FLOORBEAM. DAMAGED. UPPER DECK FLOOR BS 600 LBL TO LBL 77 TOP CAP ON FLOORBEAM HAS 6 EA DOUBLE DRILLED HOLES. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER B747 SRM 53-10-0
- [SDR EIAA2011053](https://openairdocs.org/sdr/EIAA2011053), Jun 17, 2011: SKIN. CORRODED. FUSELAGE EXTERIOR SKIN BS 1000 STR 40L CORRODED. REMOVED CORROSION, NDT, FABBED AND INSTALLED REPAIR PER B747 SRM 53-30-03 FIG 12 AND 47.
- [SDR EIAA2011052](https://openairdocs.org/sdr/EIAA2011052), Jun 17, 2011: SKIN. CRACKED. R-1 DOOR SKIN BS 450 WL 259 HAS SKIN CRACKED AREA ABOVE UPPER HINGE DOUBLER REPAIR. REMOVED DAMAGED AREAS OF SKIN, FABBED REPAIR DOUBLER AND TRIPLER AND INSTALL
- [SDR EIAA2011051](https://openairdocs.org/sdr/EIAA2011051), Jun 17, 2011: FLOORBEAM. DAMAGED. FLOORBEAM UPPER CHORD INSERT DAMAGED AT BS 2220 BL 0. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-40-04 FIG 1.
- [SDR EIAA2011050](https://openairdocs.org/sdr/EIAA2011050), Jun 17, 2011: PANEL. CORRODED. NR 2 PYLON PANEL 462CL HAS CORROSION ON LOWER I/B SIDE OF PYLON IN EDGE RADIUS OF SPAR. REMOVED CORROSION AND REPAIRED PER ECRA 482-54-240-2.
- [SDR EIAA2011049](https://openairdocs.org/sdr/EIAA2011049), Jun 17, 2011: SKIN. CRACKED. R1 DOOR SKIN CRACK AT BS 480 WL 266. REMOVED DAMAGE FABBED AND INSTALLED REPAIR PER B747 SRM 52-10-02 FIG 9.
- [SDR EIAA2011048](https://openairdocs.org/sdr/EIAA2011048), Jun 17, 2011: SKIN. CRACKED. R1 DOOR SKIN CRACK AT BS 480 WL 210. REMOVED DAMAGE FABBED AND INSTALLED REPAIR PER B747 SRM 52-10-02 FIG 9.
- [SDR EIAA2011047](https://openairdocs.org/sdr/EIAA2011047), Jun 17, 2011: FRAME. PUNCTURED. FWD CARGO PIT BS 720 RBL 60 HAS PUNCTURE IN FRAME WEB. REMOVED DAMAGED SECTION OF WEB, SPLICED IN NEW SECTION OF WEB AT STA 720 RBL 44-49 PER B747 SRM 53-10-04 
- [SDR EIAA2011046](https://openairdocs.org/sdr/EIAA2011046), Jun 17, 2011: STRUCTURE. CORRODED. BS 1241 STR 14R AND 15R FWD SIDE HAS CORROSION. REMOVED CORROSION FABBED AND INSTALLED REPAIR PER SRM 53-30-03 FIG 47.
- [SDR EIAA2011066](https://openairdocs.org/sdr/EIAA2011066), Jun 16, 2011: SMOKE DETECTOR. FALSE ACTIVATION. MAIN DECK CARGO SMOKE DETECTOR NR 5 SENSOR LIGHT CAME ON DURING CRUISE. VISUAL CHECK OF CARGO COMPARTMENT NO SMOKE NOTED. TROUBLESHOOT AND OP'S CHECKED NR 5 CAR
- [SDR EIAA2011044](https://openairdocs.org/sdr/EIAA2011044), May 26, 2011: DOOR FRAME. DAMAGED. ELEVEN EACH DEFECTIVE HOLES AT STA 800 R2 DOOR FRAME. REAMED, CLEANED AND DEBURRED DISCREPENT HOLES PER B747 SRM 51-30-05 PG 6-9.
- [SDR EIAA2011043](https://openairdocs.org/sdr/EIAA2011043), May 23, 2011: FITTING. CORRODED. NR 4 PYLON BOTH UPPER AND LOWER DUAL SIDE BRACE FITTINGS HAVE CORROSION IN THE BEARING MOUNT RACES. REPLACED DSB FITTINGS BEARING RACES PER EO 747-54-1804-05.
- [SDR EIAA2011040](https://openairdocs.org/sdr/EIAA2011040), Apr 25, 2011: LIGHT. INOPERATIVE. EMERGENCY LIGHT UPPER DECK LEFT SIDE CENTER AISLE INOP. REPAIRED LIGHT PER MFG. OHM 33-50-02 REV P.

All 355: https://openairdocs.org/deregistered/N482EV-2018-02-07/reports.md

## NTSB investigations (2)

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 ENG11WA005](https://openairdocs.org/ntsb/ENG11WA005), Nov 28, 2010: Boeing 747 (N482EV), Chubu, Japan, Japan, incident, no damage
- [NTSB DCA98WA069](https://openairdocs.org/ntsb/DCA98WA069), Jul 20, 1998: Boeing 747 (N482EV), Amsterdam, Netherlands, incident, no damage

## 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 20101128053169I](https://openairdocs.org/incident/20101128053169I), Nov 28, 2010: Boeing 747-212B (N482EV), Minor damage. On 11/28/2010, flight EV-238 aircraft N482EV (20713), a Boeing 747-212B departed Nagoya, Japan (ngo). On climb at approximately 3500' the crew noticed N1 and…

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