# Service difficulty reports: N477EV, cancelled Jun 7, 2017

A list on [N477EV, cancelled Jun 7, 2017](https://openairdocs.org/deregistered/N477EV-2017-06-07.md).

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

Page 1 of 3 · 111 reports

- [SDR EIA2007154](https://openairdocs.org/sdr/EIA2007154.md): Engine · oil consumption · Aug 29, 2007 · N477EV · Boeing 747SR46 · Engine (Turbine/Turboprop)
  > 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 AND ENGINE REPLACED.
- [SDR EIA2007121](https://openairdocs.org/sdr/EIA2007121.md): Light · inoperative · Jun 4, 2007 · N477EV · Boeing 747SR46 · Emergency Lighting
  > 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 PER B747 MM 33-51-07.
- [SDR EIA2007120](https://openairdocs.org/sdr/EIA2007120.md): Light · burned out · Jun 4, 2007 · N477EV · Boeing 747SR46 · Emergency Lighting
  > 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 PER B747 MM 33-51-06.
- [SDR EIA2007047](https://openairdocs.org/sdr/EIA2007047.md): Skin · corroded · Feb 22, 2007 · N477EV · Boeing 747SR46 · Wing, Plate/Skin
  > 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.md): Skin · corroded · Feb 22, 2007 · N477EV · Boeing 747SR46 · Wing, Plate/Skin
  > 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. REMOVED CORROSION, FABBED AND INSTALLED REPAIR PER ECRA 477-57-116-2.
- [SDR EIA2007044](https://openairdocs.org/sdr/EIA2007044.md): Skin · corroded · Feb 22, 2007 · N477EV · Boeing 747SR46 · Wing, Plate/Skin
  > 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 477-57-117-2.
- [SDR EIA2007043](https://openairdocs.org/sdr/EIA2007043.md): Spar · corroded · Feb 22, 2007 · N477EV · Boeing 747SR46 · Wing Spar
  > 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 REPAIR PER ECRA 477-57-117-2.
- [SDR EIA2007042](https://openairdocs.org/sdr/EIA2007042.md): Structure · corroded · Feb 22, 2007 · N477EV · Boeing 747SR46 · Wing Miscellaneous Structure
  > 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 AREAS, FABBED AND INSTALLED REPAIR PER B747 SRM 57-30-01 PAGES 21-22.
- [SDR EIA2007041](https://openairdocs.org/sdr/EIA2007041.md): Spar · corroded · Feb 22, 2007 · N477EV · Boeing 747SR46 · Wing Spar
  > 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 AT FORWARD SIDE VERTICAL FLANGE FSSO 1261-1331 AND 1341 PER ECRA 477-57-118-2.
- [SDR EIA2007049](https://openairdocs.org/sdr/EIA2007049.md): Stringer · gouged · Feb 20, 2007 · N477EV · Boeing 747SR46 · Fuselage Main, Longeron/Stringer
  > 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.md): Spar · corroded · Feb 20, 2007 · N477EV · Boeing 747SR46 · Wing Spar
  > 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 477-57-113-2.
- [SDR EIA2007045](https://openairdocs.org/sdr/EIA2007045.md): Skin · cracked · Feb 20, 2007 · N477EV · Boeing 747SR46 · Fuselage Main, Plate/Skin
  > 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.md): Skin · corroded · Feb 8, 2007 · N477EV · Boeing 747SR46 · Wing, Plate/Skin
  > 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.md): Light · dirty · Oct 5, 2006 · N477EV · Boeing 747SR46 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOUT CREW SERVICE DOOR OPERATES INTERMITTENTLY. CLEANED AND RESEATED EMERGENCY LIGHT ASSEMBLY.
- [SDR EIAA2006185](https://openairdocs.org/sdr/EIAA2006185.md): Battery Pack · inoperative · Aug 23, 2006 · N477EV · Boeing 747SR46 · Emergency Lighting
  > CREW EMERGENCY THROUGH LIGHTS INOP. REPLACED BATTERY PACK PER MM 33-51-04, OPS CHECK GOOD.
- [SDR EIA2006223](https://openairdocs.org/sdr/EIA2006223.md): Sensor · malfunctioned · Aug 22, 2006 · N477EV · Boeing 747SR46 · Engine Temperature Indicating System
  > 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. ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT, ENGINE SHUTDOWN. PERFORMED EXTERNAL INSPECTION, EN
- [SDR EIAA2006184](https://openairdocs.org/sdr/EIAA2006184.md): Engine · stalled · Aug 22, 2006 · N477EV · Boeing 747SR46 · Engine (Turbine/Turboprop)
  > 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 RESPONSE OK AFTER INFLIGHT RESTART. REPLACED NR 4 ENGINE DUE TO METAL IN TAILPIPE.
- [SDR EIA2006183](https://openairdocs.org/sdr/EIA2006183.md): Battery Pack · discharged · Aug 10, 2006 · N477EV · Boeing 747SR46 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY POWER PACK DEAD FOR CREW SERVICE DOOR THRESHOLD LIGHTS.
- [SDR EIA2006218](https://openairdocs.org/sdr/EIA2006218.md): Battery Pack · inoperative · Aug 9, 2006 · N477EV · Boeing 747SR46 · Emergency Lighting
  > CREW EMERGENCY THRESHOLD LIGHT INOP. REPLACED BATTERY PACK PER MM 33-51-04, OPS CHECK GOOD.
- [SDR EIA2006078](https://openairdocs.org/sdr/EIA2006078.md): Floorbeam · cracked · May 3, 2006 · N477EV · Boeing 747SR46 · Fuselage Main, Floor Beam
  > 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.md): Skin · damaged · Apr 29, 2006 · N477EV · Boeing 747SR46 · Fuselage Main, Plate/Skin
  > 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.md): Skin · cracked · Apr 14, 2006 · N477EV · Boeing 747SR46 · Fuselage Main, Plate/Skin
  > 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 INSTALLED AND CORROSION BLENDED OUT PER SRM 51-10-01, BOEING SR1D1-181882088,SRM 53-30-03, ECRA 477-5
- [SDR EIA2006072](https://openairdocs.org/sdr/EIA2006072.md): Flap Track · damaged · Apr 7, 2006 · N477EV · Boeing 747SR46 · Trailing Edge Flaps
  > 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 PER DRWG 65B16774 ALL REWORK OTHERWISE CONFORMS TO DRWG 65B16774, 65B16768, SB 747-57-2262 REV 4 AND
- [SDR EIA2006069](https://openairdocs.org/sdr/EIA2006069.md): Skin · corroded · Apr 3, 2006 · N477EV · Boeing 747SR46 · Wing, Plate/Skin
  > 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, INSTALLED CHORD SECTION REPLACEMENT PER BOEING SR1D 1-177601899, SRM 51-10-02, SRM 57-30-01, AND SCPM 20-1
- [SDR EIA2006070](https://openairdocs.org/sdr/EIA2006070.md): Stringer · cracked · Mar 31, 2006 · N477EV · Boeing 747SR46 · Fuselage Main, Longeron/Stringer
  > 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, SPLICE INSTALLED PER SRM 51-10-03, BOEING SR1D1-177208480, ECRA 477-51-111-1.
- [SDR EIA2006071](https://openairdocs.org/sdr/EIA2006071.md): Frame · cracked · Mar 30, 2006 · N477EV · Boeing 747SR46 · Fuselage Main, Frame
  > 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 AND FILLERS PER SRM 51-10-02, BOEING SR1D1-181882088, SRM 53-10-04, ECRA 477-51-111-1.
- [SDR EIA2006073](https://openairdocs.org/sdr/EIA2006073.md): Frame · cracked · Mar 25, 2006 · N477EV · Boeing 747SR46 · Fuselage Main, Frame
  > 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, CONFORM TO DWG 65B10365 AND RESTORED FINISH PER AMM 51-21 HFEC INSPECTION C/W ON TRIM LINE TO ENSURE D
- [SDR EIA2006034](https://openairdocs.org/sdr/EIA2006034.md): Engine · leaking · Mar 16, 2006 · N477EV · Boeing 747SR46 · Turbine Engine Oil System
  > 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 PRESS DURING WINDMILL.
- [SDR EIA2006023](https://openairdocs.org/sdr/EIA2006023.md): Controller · malfunctioned · Feb 10, 2006 · N477EV · Boeing 747SR46 · Pneumatic Distribution System
  > PRESSURE RELIEF VALVE OPENS IN FLIGHT. UNABLE TO CONTROL OVER PRESSURE CONDITION RESULTING IN AN AIR TURN BACK. PRELIMINARY REVIEW ON GROUND REVEALED NO FINDINGS SO FAR. REPLACED AUTO PRESS CONTROLLER PER MM 21-31-02, OPS CHK OK, PITOT STATIC TEST C/W PER 3
- [SDR EIA2006024](https://openairdocs.org/sdr/EIA2006024.md): Light · inoperative · Jan 26, 2006 · N477EV · Boeing 747SR46 · Emergency Lighting
  > UPPER DECK LEFT HAND EMERGENCY LIGHT INOP. REPLACED LIGHT PER MM 33-51-07.
- [SDR EIA2006012](https://openairdocs.org/sdr/EIA2006012.md): Light · inoperative · Jan 26, 2006 · N477EV · Boeing 747SR46 · Emergency Lighting
  > 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.md): Light · malfunctioned · Jan 21, 2006 · N477EV · Boeing 747SR46 · Emergency Lighting
  > UPPER DECK EMERGENCY LIGHT ILLUMINATES MOMENTARILY THEN GOES OUT. DEFERRED DMI 657, REMAINS OPEN PENDING CORRECTIVE ACTION.
- [SDR EIA2006001](https://openairdocs.org/sdr/EIA2006001.md): Smoke Detector · inoperative · Jan 3, 2006 · N477EV · Boeing 747SR46 · Smoke Detection
  > LAV SMOKE DETECTOR FOUND INOPERATIVE ON INSPECTION. REPLACED BATTERY, SMOKE DETECTOR, OPERATIONAL CHECK GOOD.
- [SDR EIA23005257](https://openairdocs.org/sdr/EIA23005257.md): Skin · corroded · Dec 8, 2005 · N477EV · Boeing 747SR46 · Wing, Plate/Skin
  > 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 AND REPLACED A REPAIR SECTION OF CHORD FROM FSS 1260 TO THE PRODUCTION SPLICE AT FSS 1446.13. REPA
- [SDR EIA2005261](https://openairdocs.org/sdr/EIA2005261.md): Skin · damaged · Nov 29, 2005 · N477EV · Boeing 747SR46 · Leading Edge Devices
  > 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 LOWER SECTON AT WS 426 PER ECRA 477-57-107-2P, PART 1. AS APPROVED BY BACFAA FORM 8100-9, DATED NOV
- [SDR EIA2004149](https://openairdocs.org/sdr/EIA2004149.md): Battery Pack · inoperative · Dec 16, 2004 · N477EV · Boeing 747SR46 · Emergency Lighting
  > 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.md): Bulb · inoperative · Dec 3, 2004 · N477EV · Boeing 747SR46 · Emergency Lighting
  > 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.md): Floor Support · cracked · Sep 30, 2004 · N477EV · Boeing 747SR46 · Fuselage Miscellaneous Structure
  > 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 INSPECTION ECRA 477-53-105-1.
- [SDR AWXA200601495](https://openairdocs.org/sdr/AWXA200601495.md): Floor Support · cracked · Sep 30, 2004 · N477EV · Boeing 747SR46 · Fuselage Miscellaneous Structure
  > 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 INSPECTION ECRA 477-53-105-1.
- [SDR EIA2004125](https://openairdocs.org/sdr/EIA2004125.md): Stringer · cracked · Sep 30, 2004 · N477EV · Boeing 747SR46 · Fuselage Main, Longeron/Stringer
  > 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.md): Floor Support · cracked · Sep 30, 2004 · N477EV · Boeing 747SR46 · Fuselage Miscellaneous Structure
  > 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 INSPECTION ECRA 477-53-105-1.
- [SDR EIA2004112](https://openairdocs.org/sdr/EIA2004112.md): Frame · cracked · Sep 30, 2004 · N477EV · Boeing 747SR46 · Fuselage Main, Frame
  > 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 FRAME STRAP AND REVEAL PANEL ON RHS AND5. BOEING MESSAGE: I-OJHBI, I-P3MEM, AND I-P8ZPI. REPETITIVE
- [SDR EIA2004111](https://openairdocs.org/sdr/EIA2004111.md): Skin · corroded · Sep 30, 2004 · N477EV · Boeing 747SR46 · Fuselage Main, Plate/Skin
  > 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 OUT CORRODED OVERLAPPING SKIN. INTL REPAIR DOUBLER PER EN AND EA53-0825. BOEING MESSAGE I-PC15E,
- [SDR EIA2004119](https://openairdocs.org/sdr/EIA2004119.md): Skin · corroded · Sep 30, 2004 · N477EV · Boeing 747SR46 · Cargo/Baggage Doors
  > 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 OUTER DOUBLERS PER EN EA 52-0048. BOEING MESSAGE, 1-P48WC, 1-PBPA2, AND 1-P1QFU. TIME LIMITED REP
- [SDR EIA2004117](https://openairdocs.org/sdr/EIA2004117.md): Skin · cracked · Sep 30, 2004 · N477EV · Boeing 747SR46 · Landing Gear Doors
  > 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, AND INSTALLED REPAIR DOUBLER BONDED TO FILLER. INSTALLED THREE (3) ROWS OF BLIND RIVETS AROUND TH
- [SDR EIA2004124](https://openairdocs.org/sdr/EIA2004124.md): Frame · cracked · Sep 30, 2004 · N477EV · Boeing 747SR46 · Fuselage Main, Frame
  > 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.md): Skin · corroded · Sep 30, 2004 · N477EV · Boeing 747SR46 · Fuselage Main, Plate/Skin
  > 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, JUST O/B RBL 98.58 FLOORBEAM. INSPECTED AREA AND DETERMINED CORROSION AND CRACK FREE. SHOT PEENE
- [SDR EIA2004120](https://openairdocs.org/sdr/EIA2004120.md): Keelbeam · corroded · Sep 30, 2004 · N477EV · Boeing 747SR46 · Fuselage Main, Keel
  > 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 CORROSION FREE. SHOT PEENED AND REFINISHED PER EN EA 53-0827. BOEING MESSAGE 1-OJ18O, 1-OUNOI,
- [SDR EIA2004110](https://openairdocs.org/sdr/EIA2004110.md): Fairing · corroded · Sep 23, 2004 · N477EV · Boeing 747SR46 · Wing, Plate/Skin
  > 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 FREE. APPLIED FINISH PER BOEING MESSAGE NR I-OYSCJ, I-OW4AE, TEC-XMN-04-01388C. EN EA-57-0428, REPET
- [SDR EIA2004121](https://openairdocs.org/sdr/EIA2004121.md): Spar · cracked · Sep 22, 2004 · N477EV · Boeing 747SR46 · Nacelle/Pylon, Frame/Spar/Rib
  > 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.

Next page: https://openairdocs.org/deregistered/N477EV-2017-06-07/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N477EV' AND deregistration_id = 'N477EV-2017-06-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N477EV-2017-06-07/reports

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