# N477EV: 1974 Boeing 747-SR-46, registration cancelled 2017-06-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 7, 2017
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 747-SR-46](https://openairdocs.org/model/boeing-747-sr-46) (registry code 1384816)
- Engine: [Pratt & Whitney JT9D series](https://openairdocs.org/engine/pratt-whitney-jt9d-series) (registry code 52054)
- Serial number: 20784
- Year built: 1974
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 21, 1991
- Certificate issued: July 30, 2003
- Last registry action: July 21, 2009
- Mode S code: A5DB93
- 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/N477EV
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=477EV
- Page: https://openairdocs.org/deregistered/N477EV-2017-06-07

From the FAA registry file of November 5, 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-SR-46: https://openairdocs.org/model/boeing-747-sr-46.md

## Service difficulty reports (111, newest 50)

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

- [SDR EIA2007154](https://openairdocs.org/sdr/EIA2007154), Aug 29, 2007: ENGINE. OIL CONSUMPTION. PASSING THROUGH FL 200, NR 4 OIL QTY WENT TO "0", OIL TEMP REDLINED, OIL PRESSURE 5 PSI. ENGINE SHUT-DOWN AND RETURNED TO SUU STATION. AIRCRAFT FERRIED TO MZJ A
- [SDR EIA2007121](https://openairdocs.org/sdr/EIA2007121), Jun 4, 2007: LIGHT. INOPERATIVE. EMERGENCY LIGHT IN THE UPPER DECK STAIR WELL LIGHT ASSY INOP. REMOVE AND REPLACE EMERGENCY LIGHT AT UPPER DECK STAIRWAY PER B747MM 33-51-07. OPS CHECKED GOOD PE
- [SDR EIA2007120](https://openairdocs.org/sdr/EIA2007120), Jun 4, 2007: LIGHT. BURNED OUT. SELF CONTAINED EMERGENCY EXIT LIGHT AT L-5 INOP. REMOVED AND REPLACED SELF CONTAINTED EMERGENCY LIGHT AT L-5 DOOR LOCATION PER B747 MM 33-51-06. OPS CKD GOOD PE
- [SDR EIA2007047](https://openairdocs.org/sdr/EIA2007047), Feb 22, 2007: SKIN. CORRODED. RIGHT WING LOWER SKIN CORRODED ON UPPER SURFACE AT FSSO 1290 AT OUTBOARD JACKPAD. REMOVED CORROSION, NDT AREA, FABBED AND INSTALLED REPAIR PER ECRA 477-57-114-2
- [SDR EIA2007046](https://openairdocs.org/sdr/EIA2007046), Feb 22, 2007: SKIN. CORRODED. RIGHT WING FSSO 1528-1530 HAS AREA OF PREVIOUS CORROSION REMOVAL WHICH WAS OUT OF LIMITS AT UPPER SURFACE OF LOWER SKIN, FORWARD OF FRONT SPAR LOWER CHORD. REMO
- [SDR EIA2007044](https://openairdocs.org/sdr/EIA2007044), Feb 22, 2007: SKIN. CORRODED. RIGHT WING LEADING EDGE LOWER SKIN UPPER SURFACE CORRODED AT OLES/FSSO 1476-1490. REMOVED CORROSION, NDT'D AREA, FABBED AN INSTALLED REPAIR PER ECRA 477-57-117-
- [SDR EIA2007043](https://openairdocs.org/sdr/EIA2007043), Feb 22, 2007: SPAR. CORRODED. RIGHT WING FRONT SPAR LOWER CHORD FORWARD SIDE HAS CORROSION ON VERTICAL FLANGE BETWEEN OLES/FSSO 1514-1521. REMOVED CORROSION, NDT'D AERA, FABBED AND INSTALLED
- [SDR EIA2007042](https://openairdocs.org/sdr/EIA2007042), Feb 22, 2007: STRUCTURE. CORRODED. RIGHT WING LEADING EDGE LOWER CHORD FORWARD FACE CORRODED AT OLES 1520, 1440 AND 1374 AND LOWER CHORD TO SKIN INTERFACE AT OLES 1405. REMOVED CORROSION, NDT ARE
- [SDR EIA2007041](https://openairdocs.org/sdr/EIA2007041), Feb 22, 2007: SPAR. CORRODED. RIGHT WING FRONT SPAR LOWER CHORD AT FSSO 1341 HAS CORROSION ON FORWARD SIDE OF THE VERTICAL FLANGE. REMOVED CORROSION, NDT'D AREA, FABBED AND INSTALLED REPAIRS
- [SDR EIA2007049](https://openairdocs.org/sdr/EIA2007049), Feb 20, 2007: STRINGER. GOUGED. RIGHT FUSELAGE STATION 370 STRINGER 8R GOUGED ON UPPER FLANGE. REMOVED AND REPLACED STRINGER PER B747 SRM 53-10-03 FIGURE 3 DETAIL IV ALTERNATIVE II 9-10H.
- [SDR EIA2007048](https://openairdocs.org/sdr/EIA2007048), Feb 20, 2007: SPAR. CORRODED. CORROSION ON FRONT SPAR WEB UNDER RIGHT WING JACK PAD FITTING AT WING STATION 1290. REMOVED CORROSION, NDT'D AREA, FABBED AND INSTALLED REPAIR PER ECRA 477-57-1
- [SDR EIA2007045](https://openairdocs.org/sdr/EIA2007045), Feb 20, 2007: SKIN. CRACKED. RIGHT UPPER FUSELAGE FLAT SIDE SKIN CRACKED AT STATION 370 STRINGER 8R. REMOVED DAMAGE, NDT'D AREA, FABBED AND INSTALLED REPAIR PER ECRA 477-53-115-2.
- [SDR EIA2007050](https://openairdocs.org/sdr/EIA2007050), Feb 8, 2007: SKIN. CORRODED. RIGHT WING LEADING EDGE SKIN CORRODED ON UPPER SURFACE AT FFSO 1405. REMOVED CORROSION, NDT'D AREA, FABBED AND INSTALLED REPAIR PER B747 57-30-03 PAGE 9-13.
- [SDR EIA2006238](https://openairdocs.org/sdr/EIA2006238), Oct 5, 2006: LIGHT. DIRTY. EMERGENCY EXIT LIGHT ABOUT CREW SERVICE DOOR OPERATES INTERMITTENTLY. CLEANED AND RESEATED EMERGENCY LIGHT ASSEMBLY.
- [SDR EIAA2006185](https://openairdocs.org/sdr/EIAA2006185), Aug 23, 2006: BATTERY PACK. INOPERATIVE. CREW EMERGENCY THROUGH LIGHTS INOP. REPLACED BATTERY PACK PER MM 33-51-04, OPS CHECK GOOD.
- [SDR EIA2006223](https://openairdocs.org/sdr/EIA2006223), Aug 22, 2006: SENSOR. MALFUNCTIONED. DURING DESCENT INTO EDF, FL90, FLIGHT CREW REPORTED FEELING RUMBLE IN AIRFRAME. FLIGHT CREW NOTICE NR 4 ENGINE INDICATED N1 & N2 WERE LOWER THAN OTHER ENGINES. 
- [SDR EIAA2006184](https://openairdocs.org/sdr/EIAA2006184), Aug 22, 2006: ENGINE. STALLED. NO THROTTLE RESPONSE ON NR 4 ENG DURING DESCENT AT APPROX 8000 FT. CREW REPORTED ACCOMPLISHED COMMANDED INFLIGHT SHUT DOWN OF NR 4 ENG THEN RESTART. THROTTLE RE
- [SDR EIA2006183](https://openairdocs.org/sdr/EIA2006183), Aug 10, 2006: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT BATTERY POWER PACK DEAD FOR CREW SERVICE DOOR THRESHOLD LIGHTS.
- [SDR EIA2006218](https://openairdocs.org/sdr/EIA2006218), Aug 9, 2006: BATTERY PACK. INOPERATIVE. CREW EMERGENCY THRESHOLD LIGHT INOP. REPLACED BATTERY PACK PER MM 33-51-04, OPS CHECK GOOD.
- [SDR EIA2006078](https://openairdocs.org/sdr/EIA2006078), May 3, 2006: FLOORBEAM. CRACKED. DURING CHECK LT AND RT BS 440 FLOORBEAM UPPER DECK BEAM FASTENER HOLE CRACKED. REPAIRED PER B747 SRM 53-10-07.
- [SDR EIA2006077](https://openairdocs.org/sdr/EIA2006077), Apr 29, 2006: SKIN. DAMAGED. DURING CHECK AN OPEN HOLE FOUND COMMON TO STRINGER 30R AND SKIN AT BS 958. COMPLIED WITH REPAIR AS CALLED OUT IN ECRA 477-53-072-2 PART 2.
- [SDR EIAA2006068](https://openairdocs.org/sdr/EIAA2006068), Apr 14, 2006: SKIN. CRACKED. DURING C CHECK AT TAECO, STRESS CORROSION CRACK AND CORROSION WERE FOUND ON RT FUSELAGE SKIN BETWEEN STA 2276 AND 2299. DAMAGE TRIMMED OUT AND REPAIR DOUBLER IN
- [SDR EIA2006072](https://openairdocs.org/sdr/EIA2006072), Apr 7, 2006: FLAP TRACK. DAMAGED. DURING C CHECK, DISCREPANCIES FOUND IN THE NR 5 FLAP TRACK FWD SUPPORT FITTING. INSTALLATION OF BUSHING AND BEARING PER S/B 747-57-22262 REV 4- STEEL FITTING PE
- [SDR EIA2006069](https://openairdocs.org/sdr/EIA2006069), Apr 3, 2006: SKIN. CORRODED. DURING C CHECK, CORROSION WAS FOUND ON WING CENTER SECTION NR 2 UPPER WING SURFACE AT STA 1140 RBL11 AND RBL74. DAMAGE TRIMMED OUT AND REPAIRED DOUBLER, INSTALL
- [SDR EIA2006070](https://openairdocs.org/sdr/EIA2006070), Mar 31, 2006: STRINGER. CRACKED. DURING C CHECK, CRACKS WERE FOUND ON STR 13L END AREA AT BS 744, CRACKS APPROX. 0.866 & 0.787 IN LENGTH. DAMAGE STRINGER CUT OUT BETWEEN BS 741.10 AND BS 750, S
- [SDR EIA2006071](https://openairdocs.org/sdr/EIA2006071), Mar 30, 2006: FRAME. CRACKED. DURING C CHECK, ONE FASTENER HOLE HAD CRACKS COMMON TO RHS STA 800 FRAME INNER CHORD ANGLE AND STRAP AT STA 16R. DAMAGE TRIMMED OUT AND INSTALLED REPAIR STRAPS 
- [SDR EIA2006073](https://openairdocs.org/sdr/EIA2006073), Mar 25, 2006: FRAME. CRACKED. DURING C CHECK, A 3.0 IN CRACK WAS FOUND ON INNER CHORD ANGLE AT STA 1265 AND WL170 INNER CHORD ANGLE SECTION REPAIRED PER SRM 51-40-04, SRM 51-10-07. ALSO, CON
- [SDR EIA2006034](https://openairdocs.org/sdr/EIA2006034), Mar 16, 2006: ENGINE. LEAKING. DURING FLIGHT, NR 3 ENGINE OIL QUANTITY LESS THAN 1/8 MARK, PRESSURE DROPPED TO 35PSI, WITH FLICKERING LOW OIL PRESS LIGHT, ENGINE SHUTDOWN, MAINTAIN 17 PSI OIL
- [SDR EIA2006023](https://openairdocs.org/sdr/EIA2006023), Feb 10, 2006: CONTROLLER. MALFUNCTIONED. PRESSURE RELIEF VALVE OPENS IN FLIGHT. UNABLE TO CONTROL OVER PRESSURE CONDITION RESULTING IN AN AIR TURN BACK. PRELIMINARY REVIEW ON GROUND REVEALED NO FINDING
- [SDR EIA2006024](https://openairdocs.org/sdr/EIA2006024), Jan 26, 2006: LIGHT. INOPERATIVE. UPPER DECK LEFT HAND EMERGENCY LIGHT INOP. REPLACED LIGHT PER MM 33-51-07.
- [SDR EIA2006012](https://openairdocs.org/sdr/EIA2006012), Jan 26, 2006: LIGHT. INOPERATIVE. LEFT FORWARD EMERGENCY CEILING LIGHT UPPER DECK INOP. REMOVED AND REPLACED EMERGENCY CEILING LIGHT PER MM 33-51-07. OPS CK GOOD.
- [SDR EAI2006010](https://openairdocs.org/sdr/EAI2006010), Jan 21, 2006: LIGHT. MALFUNCTIONED. UPPER DECK EMERGENCY LIGHT ILLUMINATES MOMENTARILY THEN GOES OUT. DEFERRED DMI 657, REMAINS OPEN PENDING CORRECTIVE ACTION.
- [SDR EIA2006001](https://openairdocs.org/sdr/EIA2006001), Jan 3, 2006: SMOKE DETECTOR. INOPERATIVE. LAV SMOKE DETECTOR FOUND INOPERATIVE ON INSPECTION. REPLACED BATTERY, SMOKE DETECTOR , OPERATIONAL CHECK GOOD.
- [SDR EIA23005257](https://openairdocs.org/sdr/EIA23005257), Dec 8, 2005: SKIN. CORRODED. DURING "B" CHECK INSPECTION, FOUND CORROSION ON LT WING LOWER SKIN, LOWER FRONT SPAR CHORD, AND FRONT SPAR WEB BETWEEN FSS 1250 AND 1510. REMOVED DAMAGED CHORD 
- [SDR EIA2005261](https://openairdocs.org/sdr/EIA2005261), Nov 29, 2005: SKIN. DAMAGED. LT WING LDG EDGE NR 2 KRUEGER FLAP IB HINGE ARE, IB FRAME WEB LOWER SECTION HAS 4 INCH CRACK AT APPROXIMATELY WS 426. REPAIRED NR 2 KRUEGER FLAP IB FRAME WEB LO
- [SDR EIA2004149](https://openairdocs.org/sdr/EIA2004149), Dec 16, 2004: BATTERY PACK. INOPERATIVE. U/D SILL LIGHT ON CREW EXIT DOOR INOP. REPLACED UPPER DECK BATTERY PACK ASSY IAW MM 33-51-04.
- [SDR EIA2004147](https://openairdocs.org/sdr/EIA2004147), Dec 3, 2004: BULB. INOPERATIVE. AFT EMERGENCY LIGHT BULB AT L1 DOOR MAIN CARGO DECK INOP. RELAMPED AFT EMERGENCY LIGHT BULB AT L1 DOOR MAIN CARGO DECK. GRN CHECKED NORMAL IAW MM 33-51-00.
- [SDR SIMA200629203](https://openairdocs.org/sdr/SIMA200629203), Sep 30, 2004: FLOOR SUPPORT. CRACKED. UPPER DECK, FLOOR SUPPORT UPPER CHORD OPEN HOLES CRACKED AT BS380, 400, 420, 520, 540, 600, 660, AND 720. REPAIR OPEN HOLES PER SB 747-53A2452. REPETITIVE INSPE
- [SDR AWXA200601495](https://openairdocs.org/sdr/AWXA200601495), Sep 30, 2004: FLOOR SUPPORT. CRACKED. UPPER DECK, FLOOR SUPPORT UPPER CHORD OPEN HOLES CRACKED AT BS380, 400, 420, 520, 540, 600, 660, AND 720. REPAIR OPEN HOLES PER SB 747-53A2452. REPETITIVE INSPE
- [SDR EIA2004125](https://openairdocs.org/sdr/EIA2004125), Sep 30, 2004: STRINGER. CRACKED. UPPER DECK STRINGER CRACKED AT BS 746, STR L3. REPAIRED STRINGER PER SRM 53-10-03, FIG 10.
- [SDR EIA2004113](https://openairdocs.org/sdr/EIA2004113), Sep 30, 2004: FLOOR SUPPORT. CRACKED. UPPER DECK, FLOOR SUPPORT UPPER CHORD OPEN HOLES CRACKED AT BS380, 400, 420, 520, 540, 600, 660, AND 720. REPAIR OPEN HOLES PER SB 747-53A2452. REPETITIVE INSPE
- [SDR EIA2004112](https://openairdocs.org/sdr/EIA2004112), Sep 30, 2004: FRAME. CRACKED. MULTIPLE DEFECTS (CRACKS) ON LT AND RT SIDE BS 2231 FRAME ASSY AT MED NR 5L/R FWD EDGE CUTOUT AREA. TRIM OUT DAMAGED PORTION, SPLICE REPLACEMENT SECTION OF FRAM
- [SDR EIA2004111](https://openairdocs.org/sdr/EIA2004111), Sep 30, 2004: SKIN. CORRODED. FUSELAGE SKIN BULGED AT SB/T STA 2180 TO STA 2200, STR 44R. CORRODED SKIN TRIMMED OUT. REMOVE AND DISCARD EXISTING DOUBLER OVERLAPPING STR 46R LAP JOINT. TRIM O
- [SDR EIA2004119](https://openairdocs.org/sdr/EIA2004119), Sep 30, 2004: SKIN. CORRODED. BULGE FROM CORROSION ON SKIN AT AFT LWR CORNER OF AFT CARGO DOOR. TRIM OUT CORROSION PER SRM 51-10-01. HFEC INSPECTED. REINFORCE ENTIRE DAMAGED AREA WITH TWO OU
- [SDR EIA2004117](https://openairdocs.org/sdr/EIA2004117), Sep 30, 2004: SKIN. CRACKED. RT BLG I/B STRUT DOOR FOUND CORROSION AND CRACK ON EXT FACE OF OUTER DOOR-SKIN AT AFT EDGE. TRIM CORROSION AND CRACK IN 0.040 OUTER SKIN AT BS 1483.7, RBL 55.6,
- [SDR EIA2004124](https://openairdocs.org/sdr/EIA2004124), Sep 30, 2004: FRAME. CRACKED. CRACK AT END OF MAIN DECK FRAME AT FASTENER HOLE, BS 340, S-16L. REPAIRED FRAME PER SRM 53-10-04, FIG 85.
- [SDR EIA2004118](https://openairdocs.org/sdr/EIA2004118), Sep 30, 2004: SKIN. CORRODED. FOUND CORROSION ON UPPER CENTER SKIN SECTION AT STA 1140, RBL 100, MAIN DECK. CORROSION BLENDED FROM SKIN PAD ON UPPER SURFACE OF UPPER SKIN PANEL NR 2 AT S-14,
- [SDR EIA2004120](https://openairdocs.org/sdr/EIA2004120), Sep 30, 2004: KEELBEAM. CORRODED. CORROSION CRACK, KEEL BEAM, RT LWR CHORD IB LEG AT STA 1313. TRIM 5.0 INCHES INBOARD LWR FLANGE OF VERTICAL AND HORIZONTAL LEGS. HFEC INSPECTED, FOUND CRACK AND
- [SDR EIA2004110](https://openairdocs.org/sdr/EIA2004110), Sep 23, 2004: FAIRING. CORRODED. LT WING LEADING EDGE WING ROOT ALUMINUM NOSE CAP (D-FAIRING) AT LALDG LIGHT LWR AREA FOUND CORROSION. CORROSION REMOVED, HFEC INSP TO INSURE CORROSION CRACK FRE
- [SDR EIA2004121](https://openairdocs.org/sdr/EIA2004121), Sep 22, 2004: SPAR. CRACKED. CRACK AT NAC STA 210, LOWER SPAR WEB, CENTER AREA, NR 1 PYLON. REPAIR LWR SPAR WEB PER SRM 54-10-03, FIG 2, SPAR WEB FABRICATED IAW SRM 54-10-03, FIG 2.

All 111: https://openairdocs.org/deregistered/N477EV-2017-06-07/reports.md

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