# N470EV: 1974 Boeing 747-273C, 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 747-273C](https://openairdocs.org/model/boeing-747-273c) (registry code 1384896)
- Engine: [Pratt & Whitney JT9D-7J](https://openairdocs.org/engine/pratt-whitney-jt9d-7j) (registry code 51546)
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE), [TCDS E20EA](https://openairdocs.org/tcds/E20EA) (OpenAirDocs)
- Serial number: 20653
- Year built: 1974
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 28, 2006
- Certificate issued: August 15, 2003
- Last registry action: March 6, 2012
- Mode S code: A5C192
- 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/N470EV
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=470EV
- Page: https://openairdocs.org/deregistered/N470EV-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 747-273C: https://openairdocs.org/model/boeing-747-273c.md

## Service difficulty reports (264, newest 50)

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

- [SDR EIAA20120115002](https://openairdocs.org/sdr/EIAA20120115002), Jan 15, 2012: LUG. LOOSE. CAPTAINS MAP LIGHT SWITCH GETS VERY HOT AND PUTS OUT AN ACRID ODOR. FOUND BOTH TERM LUG LOOSE AND SECURED TERM LUGS. OP'S CHECKED OK PER 33-15-00/501.
- [SDR EIAA20111215261](https://openairdocs.org/sdr/EIAA20111215261), Dec 15, 2011: PRESSURE SWITCH. LOOSE. NR 3 OIL QUANTITY INDICATOR DROPPED TO ZERO AT 7000, OIL PRESSURE FLUCTUATED +/- 10 PSI. ENGINE SHUTDOWN. PERFORMED ENGINE WINDMILLING INSPECTION IAW MM 72-00-0
- [SDR EIAA20111215260](https://openairdocs.org/sdr/EIAA20111215260), Dec 15, 2011: DETECTION SYS. MALFUNCTIONED. APU FIRE LOOP "B" GIVES FIRE INDICATION. APU FIRE HANDLE LIGHT ON. RESEQUENCED FIRE HANDLE WITH C/B PERFORMED WI CHECK FROM CARD FILE J5 AND J3 TO APU FIRE LOOP
- [SDR EIAA20111121255](https://openairdocs.org/sdr/EIAA20111121255), Nov 21, 2011: LIGHT. FAILED. STAIRWAY DOME EMERGENCY LIGHT GOES OUT AFTER 10 SECONDS. REMOVED AND REPLACED LIGHT ASSY. PER MM 33-51-07 PG 201.
- [SDR EIAA20111116251](https://openairdocs.org/sdr/EIAA20111116251), Nov 16, 2011: LIGHT. DEFECTIVE. POSSIBLE DEFECTIVE EMERGENCY LIGHT - SCHEDULED B CHECK ITEM CHANGE.
- [SDR EIAA20111111250](https://openairdocs.org/sdr/EIAA20111111250), Nov 11, 2011: FITTING. LEAKING. ENGINE OIL PRESSURE LIGHT - SLOW LOSS OF OIL. FOUND EVIDENCE OF LEAKAGE AT THE ANGLE GEARBOX RIGHT SIDE FITTINGS, REPLACED WITH NEW SEAL PACKINGS PER MM 70-10-0
- [SDR EIAA2011241](https://openairdocs.org/sdr/EIAA2011241), Oct 19, 2011: ACTUATOR. CONTAMINATED. (SECOND FLIGHT) AFTER GEAR UP, MOVING GEAR LEVER TO OFF RESULTED IN GEAR LEVER LATCH IN VIEW. F/E ANNUNCIATOR PANEL SHOWED RIGHT WING TILT LIGHT ILLUMINATED WIT
- [SDR EIAA2011240](https://openairdocs.org/sdr/EIAA2011240), Oct 19, 2011: ACTUATOR. MALFUNCTIONED. AFTER GEAR UP, MOVING GEAR LEVER TO OFF RESULTED IN GEAR LEVER LATCH IN VIEW. F/E ANNUNCIATOR PANEL SHOWED RIGHT WING TILT LIGHT ILLUMINATED WITH BOTH PRIMARY A
- [SDR EIAA2011080](https://openairdocs.org/sdr/EIAA2011080), Jul 6, 2011: SPINNER. MALFUNCTIONED. NR 2 ENGINE EXPERIENCED SURGE STALL WITH INSTANTANEOUS EGT EVENT AND SHUTDOWN, WITH VIOLENT VIBRATION PRIOR TO EVENT. CREW REPORTED VISIBLE DEBRIS IN AREA OF NR
- [SDR EIAA2011071](https://openairdocs.org/sdr/EIAA2011071), Jun 28, 2011: PIN. DAMAGED. L5 DOOR EMERGENCY LIGHT INOP. REPAIR PIN ON CONNECTOR PER B747 WDM 33-51-01 AND AMM 33-51-07 PG 201, OP'S CHECK GOOD.
- [SDR EIAA2011070](https://openairdocs.org/sdr/EIAA2011070), Jun 28, 2011: LIGHT. INOPERATIVE. BS 2190L EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER AMM B747 33-51-07 PG 201 OP'S CHECK GOOD.
- [SDR EIAA2011069](https://openairdocs.org/sdr/EIAA2011069), Jun 28, 2011: LIGHT. INOPERATIVE. R5 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER AMM B747 33-51-07 PG 201, OP'S CHECK GOOD.
- [SDR EIAA2011020](https://openairdocs.org/sdr/EIAA2011020), Mar 2, 2011: LINE. LOOSE. NR 2 ENGINE SURGED PASSING FL140 EGT AT 750 EPR AT 1.3 HAD SURGE THEN HUNG, NO THROTTLE RESPONSE. SHUT DOWN ENGINE WAITED 5 MIN, THEN RE-STARTED, AFTER 10 MIN A
- [SDR EIAA2010050](https://openairdocs.org/sdr/EIAA2010050), Aug 22, 2010: BATTERY PACK. DISCHARGED. WITH EMERGENCY LIGHTS IN ON POSITION CREW SERVICE DOOR EMERGENCY LIGHTS DID COME ON, LEFT FWD DOOR OVERHEAD EMERGENCY LIGHTS CAME ON THEN WENT OUT. BOTH ITEMS D
- [SDR EIAA2010051](https://openairdocs.org/sdr/EIAA2010051), Aug 20, 2010: DOUBLER. CRACKED. NR 3 PYLON INBOARD SIDE NAC STA 252 APPROX 22 INCHES ABOVE SKIRT REPAIR DOUBLER HAS CRACK. REMOVED DAMAGE, NDT AREA FABBED REPAIR AND INSTALLED PER ECRA 470-54-
- [SDR EIAA2010047](https://openairdocs.org/sdr/EIAA2010047), Aug 19, 2010: SKIN. BENT. BS 426 STR. 37R HAS A STR. FLANGE TO SKIN BENT. REMOVED DAMAGED AND FABRICATED REPAIR IAW SRM 51-40-3, PG 1-6.
- [SDR EIAA2010046](https://openairdocs.org/sdr/EIAA2010046), Jul 29, 2010: SKIN. DENTED. EXTERNAL SKIN DENT AT BS 380-400 STRINGER 34R TO 35R. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER PER B747 SRM 53-30-03 PAGE 73.
- [SDR EIAA200900132](https://openairdocs.org/sdr/EIAA200900132), Nov 27, 2009: ENGINE. MALFUNCTIONED. NR 3 ENGINE SURGE/STALL AT MAX TAKEOFF POWER. EGT EXCEEDANCE 1088 DEG CELSIUS. REMOVED AND REPLACED NR 3 ENGINE PER WORKCARDS F7201, F7204, F7207, F7209. OPS & 
- [SDR EIAA20090057](https://openairdocs.org/sdr/EIAA20090057), May 11, 2009: ACM. LEAKING. DURING HIGH POWER SETTING (1.45 AND ABOVE) A SWEET SMELL OF OIL ENTERS AIRCRAFT. SIGNS OF OIL LEAK AT NR 1 PACK ACM AND DUCTING, DEACTIVATED NR 1 PACK, DEFERRED
- [SDR EIAA20090056](https://openairdocs.org/sdr/EIAA20090056), Apr 27, 2009: DOOR. DENTED. REPAIR DENT IN NOSE DOOR BS 190 STR 39. REMOVED DAMAGED STRINGER, RE-CONTOURED SKIN, FABBED AND INSTALLED NEW STRINGER PER B747 SRM 53-10-03 PG 8-10H AND 51-10-
- [SDR EIAA2008102800072](https://openairdocs.org/sdr/EIAA2008102800072), Oct 27, 2008: FLOOR SUPPORT. CRACKED. BULK CARGO STA 2025 LBL25 FLOOR SUPPORT ANGLE CRACKED. FLOOR SUPPORT REMOVED. NEW SUPPORT FABRICATED. HEAT TREATED, ALODINED AND PRIMED, AREA NDTD. NO CRACKS FO
- [SDR EIAA2008102800071](https://openairdocs.org/sdr/EIAA2008102800071), Oct 27, 2008: SEAT TRACK. CRACKED. AFT CARGO LT AFT FIXED STOP TIE-DOWN TRACK CRACKED STA 1900 LBL44, SEAT TRACK REMOVED. NEW SEAT TRACK FABRICATED ALODINED AND PRIMED. INSTALLED NEW SEAT TRACK P
- [SDR EIAA2008102800070](https://openairdocs.org/sdr/EIAA2008102800070), Oct 27, 2008: FLOOR SUPPORT. CRACKED. BULK CARGO STA 2100, BL 0 FLOOR SUPPORT FOUND CRACKED. REMOVE FLOOR SUPPORT NDTD AREA, NO CRACKS NOTED. FABRICATED NEW FLOOR SUPPORT PER BOEING DRAWING 65B06261
- [SDR EIAA2008102800068](https://openairdocs.org/sdr/EIAA2008102800068), Oct 27, 2008: SKIN. CRACKED. BULK CARGO STA 2160 STRINGER 46R SKIN ADJ AREA CRACKED. REMOVED FASTENERS, CUT SKIN FABRICATED REPAIR AND NEW SHEAR TIE, HEAT TREATED, ALODINED AND PRIMED, INST
- [SDR EIAA2008102800065](https://openairdocs.org/sdr/EIAA2008102800065), Oct 27, 2008: BATTERY PACK. NO TEST. UPPER DECK EMERGENCY LIGHT TEST FOUND DOOR EXIT SIGN INOP. REPLACED BATTERY PACK ASSY AND OPS CHECK NORMAL PER 33-51-00.
- [SDR EIAA2008102800064](https://openairdocs.org/sdr/EIAA2008102800064), Oct 27, 2008: FLOOR SUPPORT. CRACKED. BULK CARGO STA 2000 RBL 50 FLOOR SUPPORT CRACKED. REMOVED FASTENERS AT CRACKED FLOOR SUPPORT, STA 1990 TO STA 2010 RBL 50, AS PER SRM 51-30-02. REMOVED DAMAGE, 
- [SDR EIAA2008102800063](https://openairdocs.org/sdr/EIAA2008102800063), Oct 27, 2008: WEB. CRACKED. L-2 DOOR LOWER HINGE FWD CUT OUT WEB FOUND CRACKED. L-2 DOOR LOWER HINGE FWD CUT OUT WEB REPAIRED PER EA 52-0061.
- [SDR EIAA2008102800062](https://openairdocs.org/sdr/EIAA2008102800062), Oct 27, 2008: FLOORBEAM. CRACKED. MAIN DECK STA 228 UPPER CHORD AT BL L11 TO R33 FOUND CRACKED, MAIN DECK BS 228 FLOORBEAM UPPER CHORD AT LBL11 TO RBL33. REPAIRED AS PER TAECO EA 53-0062.
- [SDR EIAA2008102800061](https://openairdocs.org/sdr/EIAA2008102800061), Oct 27, 2008: SEAT TRACK. CRACKED. MAIN DECK STATION 520, RBL11, WL 200 SEAT TRACK FOUND CRACKED. SEAT TRACK REMOVED AS PER SRM 51-30-02 CRACKED SEAT TRACK TRIMMED OUT AS PER SRM 51-10-01 NDT CHE
- [SDR EIA2007208](https://openairdocs.org/sdr/EIA2007208), Dec 8, 2007: LIGHT. INOPERATIVE. FOUND UPPER DECK AFT EMERGENCY LIGHT INOP. REPLACED AFT EMERGENCY LIGHT ASSY PER B747 MM 33-51-02, SYSTEM OPS CHECKED PER 33-51-00.
- [SDR EIA2007210](https://openairdocs.org/sdr/EIA2007210), Dec 7, 2007: BATTERY PACK. DISCHARGED. UPPER DECK EMERGENCY LIGHT OVER DOOR SLIDE DOES NOT TEST. REPLACED BATTERY PACK PER B747 MM 33-51-04, OPS CHECKED NORMAL.
- [SDR EIA2007198](https://openairdocs.org/sdr/EIA2007198), Nov 6, 2007: WEB. CRACKED. NOSE WHEEL WELL HAS CRACK BS 270 WL 160 NWW WEB LT SIDE. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR PER B747 SRM 53-10-01 FIG 116 AND FIG 120.
- [SDR EIA2007193](https://openairdocs.org/sdr/EIA2007193), Nov 1, 2007: LIGHT. INOPERATIVE. SOLDERBURG LIGHT ASSY AT R-5 DOOR INOP. REMOVED AND REPLACED WITH SERVICEABLE UNIT PER BOEING 747 MM 33-51-07. TESTED GOOD PER BOEING 747 MM 33-51-07 PAGE 202.
- [SDR EIA2007150](https://openairdocs.org/sdr/EIA2007150), Aug 6, 2007: LIGHT. INOPERATIVE. L1 DOOR EMERGENCY SILL LIGHTS INOP (2).
- [SDR EIA2007118](https://openairdocs.org/sdr/EIA2007118), May 29, 2007: TIRE. FAILED. ON TAKEOFF, TOWER REPORTED SMOKE FROM NOSEGEAR RETURNED TO JFK. ON WALKAROUND, FOUND DAMAGE ON RT NLG TIRE (RECAP CAME OFF). ALL NOSE TIRES REPLACED IAW.
- [SDR EIA2007101](https://openairdocs.org/sdr/EIA2007101), May 14, 2007: BATTERY PACK. DISCHARGED. UPPER DECK EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECKED GOOD PER B747 MM 33-51-00 PAGE 501.
- [SDR EIA2007060](https://openairdocs.org/sdr/EIA2007060), Mar 13, 2007: SMOKE DETECTOR. NO TEST. NR 6 LOWER DECK SMOKE DETECTOR WILL NOT TEST. REPLACED DETECTOR WHEN RELAMPING DID NOT HELP. TESTED GOOD PER MM 26-16-00.
- [SDR EIA2007055](https://openairdocs.org/sdr/EIA2007055), Mar 13, 2007: SMOKE DETECTOR. INOPERATIVE. MAIN CARGO DECK SMOKE DETECTOR ZONE 5, ONE DETECTOR INOP.
- [SDR EIAA2007032](https://openairdocs.org/sdr/EIAA2007032), Mar 3, 2007: METERING VALVE. DEFECTIVE. WHEN APPLYING PARKING BRAKE, PRESSURE DROPS FROM 3000 TO 1000 ON APPROX 50 SEC, T/S IN PROGRESS WITH SHUTTLE VALVE AND BREAK MODULE. REMOVED AND REPLACED PARKIN
- [SDR EIA2007009](https://openairdocs.org/sdr/EIA2007009), Feb 5, 2007: LAMP. INOPERATIVE. NR 6 SMOKE DETECTOR OF AFT CARGO COMPARTMENT WILL NOT TEST. RELAMPED PER MM 26-14-00, SYS TESTS OK.
- [SDR EIA2007012](https://openairdocs.org/sdr/EIA2007012), Dec 29, 2006: BATTERY. INOPERATIVE. UPPER DECK CREW EXIT DOOR SILL LIGHTS WILL NOT TEST, LP 295539. REPLACED UPPER DECK LIGHT BATTERY CARTRIDGE IAW MM 33-51-00, OPS CHK GOOD.
- [SDR EIA2006380](https://openairdocs.org/sdr/EIA2006380), Nov 26, 2006: SKIN. DENTED. ON POST - FLIGHT INSPECTION, FOUND DENT ON FUSELAGE AFT OF L1 DOOR AT STA 510, STR 23. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW B747 SRM 53-30-03, 
- [SDR EIA2006197](https://openairdocs.org/sdr/EIA2006197), Aug 17, 2006: SKIN. GOUGED. LOWER SKIN OF LEFT WING STA 1241 OUTBOARD OF BUTTERFLY FITTING, SKIN GOUGED IN 4 AREAS. FABRICATED AND INSTALLED REPAIR PER B747 SRM 57-30-01 AND ECRA 470-292-2
- [SDR EIA2006195](https://openairdocs.org/sdr/EIA2006195), Aug 17, 2006: SKIN. CORRODED. SKIN CORRODED AND CRACKED BETWEEN BS 830 - 850 AT STR 50R. REPLACED DAMAGED SKIN AT BS 740 TO 850 AND STR 44L AND 44R PER ECRA 470-53-284-2.
- [SDR EIA2006196](https://openairdocs.org/sdr/EIA2006196), Aug 11, 2006: SKIN. CRACKED. SKIN CRACK ABOVE ROW OF FASTENERS ON STR 6L AT BS 630. REPAIRED CRACKED SKIN PER B747 SRM 53-30-03; REPAIRED STRINGER 6L BETWEEN BS 630-647 PER B747 SRM 53-10-0
- [SDR EIA2006194](https://openairdocs.org/sdr/EIA2006194), Jul 29, 2006: SPAR. CORRODED. LEFT WING LEADING EDGE SPAR WEB AT LOWER CHORD ILES 1071 HAS CORROSION. REMOVED CORROSION PER B747 SRM 51-10-01 & 57-10-01. FABRICATED AND INSTALLED REPAIR PER 
- [SDR EIA2006186](https://openairdocs.org/sdr/EIA2006186), Jul 21, 2006: STRINGER. DAMAGED. STR 46R, BS 825 HAS ELONGATED HOLES.
- [SDR EIA2006193](https://openairdocs.org/sdr/EIA2006193), Jul 20, 2006: SPAR. CORRODED. RT FRONT SPAR WEB CORRODED AT THE LOWER CHORD INTERFACE, INBOARD OF NR 4 PYLON IN 5 LOCATIONS; ILES 1027, 1037, 1059, 1066 & 1092. REMOVED CORROSION PER B747 SR
- [SDR EIA2006192](https://openairdocs.org/sdr/EIA2006192), Jul 20, 2006: SKIN PANEL. CORRODED. CENTER TANK LOWER SKIN ABOVE NR 3 HEAT EXCHANGER HAS EXFOLIATION CORROSION. REMOVED CORROSION AND FABRICATED REPAIR PER ECRA 470-57-291-2.
- [SDR EIA2006191](https://openairdocs.org/sdr/EIA2006191), Jul 20, 2006: STRINGER. ELONGATED. STR 45R HAS ELONGATED HOLES. REMOVED DAMAGED SECTION AND REPAIRED PER B747 SRM 53-10-03.

All 264: https://openairdocs.org/deregistered/N470EV-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 LAX01IA073](https://openairdocs.org/ntsb/LAX01IA073), Jan 6, 2001: Boeing 747-200F (N470EV), Honolulu, HI, incident, no damage. Probable cause: the failure of the lighting dimmer switch or circuit components for undetermined reasons, which resulted in smoke in the cockpit.
- [NTSB LAX96IA199](https://openairdocs.org/ntsb/LAX96IA199), May 19, 1996: Boeing 747-273C (N470EV), Los Angeles, CA, incident, minor damage. Probable cause: the operator's failure to adopt a manufacturer's stipulated ultrasonic inspection procedure, which led to the in-flight separation of the wing panel.

## FAA accident and incident reports (3)

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 20020512012419I](https://openairdocs.org/incident/20020512012419I), May 12, 2002: Boeing 747273C (N470EV), Fairfield, CA, Minor damage. (-23) Maintenance personnel on post flight inspection noted damage to l/h inboard aileron and l/h mid flap. Damage due to disconnected torque tube between #3 &…
- [Incident 20010104000889I](https://openairdocs.org/incident/20010104000889I), Jan 4, 2001: Boeing 747273C (N470EV), Honolulu, HI, Minor damage. (-23) Approx. 45 minutes after departure from hnl enroute ppg, the crew of eiaa 7550 detected smoke coming from the cener console. They declared an emergency…
- [Incident 19991211038899I](https://openairdocs.org/incident/19991211038899I), Dec 11, 1999: Boeing 747273C (N470EV), Toledo, OH, Minor damage. Pilot saw and struck bird at aircraft rotation. #4 engine shut down because of vibration. Pilot dumped fuel as aircraft circled airport at 5,000 feet. Aircraft…

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