# Service difficulty reports: N489EV, cancelled Jan 8, 2018

A list on [N489EV, cancelled Jan 8, 2018](https://openairdocs.org/deregistered/N489EV-2018-01-08.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 2 · 72 reports

- [SDR EIAA20120404037](https://openairdocs.org/sdr/EIAA20120404037.md): Battery Pack · dirty · Apr 4, 2012 · N489EV · Boeing 747230B · Emergency Lighting
  > EMERGENCY EXIT SLIDE LIGHTS UPPER DECK LEFT DOOR SILL INOPERATIVE. REMOVED BATTERY CLEANED BATTERY PACK X631 CONTACTS AND RE-INSTALLED PER B747 MM 33-51-04 PG 204-205, OPS CHECK GOOD.
- [SDR EIAA20120404036](https://openairdocs.org/sdr/EIAA20120404036.md): Floorbeam · cracked · Apr 4, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > UPPER DECK FLOORBEAM VERTICAL WEB CRACKED AT UPPER AND LOWER END BS 420 RBL 80. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PER SRM 53-10-07 PG. 47-50A.
- [SDR EIAA20120403035](https://openairdocs.org/sdr/EIAA20120403035.md): Access Panel · gouged · Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Main Frame
  > NR 3 PYLON RT SIDE INSIDE ACCESS PANEL 473AR DEEP GOUGE JUST UNDER CUT OUT. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-020-2.
- [SDR EIAA20120403034](https://openairdocs.org/sdr/EIAA20120403034.md): Skin · damaged · Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON RT FRAMES STA 259 AND 234, RT SKIN BELOW LOUVER CUTOUT ARE HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.
- [SDR EIAA20120403033](https://openairdocs.org/sdr/EIAA20120403033.md): Skin · damaged · Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 4 PYLON RT BETWEEN FRAMES STA 248 AND 259, RT INTERNAL SKIN AT STIFFENER 2 TO 4 AND FRAMES HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.
- [SDR EIAA20120403032](https://openairdocs.org/sdr/EIAA20120403032.md): Skin · damaged · Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON RT BETWEEN FRAMES STA 259 AND 270, RT SKIN BETWEEN STIFFENERS 2 AND 3 HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.
- [SDR EIAA20120403031](https://openairdocs.org/sdr/EIAA20120403031.md): Skin · damaged · Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON RT BETWEEN FRAMES STA 234 AND 270, RT INTERNAL SKIN BETWEEN STIFFENERS 2 AND 4 HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.
- [SDR EIAA20120403030](https://openairdocs.org/sdr/EIAA20120403030.md): Skin · damaged · Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 3 PYLON RT BETWEEN FRAMES STA 234 AND 248, RT INTERNAL SKIN AT STIFFENER 3 AND STIFFENER HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.
- [SDR EIAA20120402029](https://openairdocs.org/sdr/EIAA20120402029.md): Battery · discharged · Apr 2, 2012 · N489EV · Boeing 747230B · Emergency Lighting
  > TWO EA UPPER DECK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERIES WITH SERVICEABLE.
- [SDR EIAA20120402028](https://openairdocs.org/sdr/EIAA20120402028.md): Skin · damaged · Apr 2, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 3 PYLON SKIN CAP DOUBLER MOST AFT I/B FASTENER HOLE HAS DEFECT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-023-2.
- [SDR EIAA20120330027](https://openairdocs.org/sdr/EIAA20120330027.md): Skin · damaged · Mar 30, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON SKIN CAP DOUBLER AFT I/B FASTENER HOLE HAS DEFECT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-024-2.
- [SDR EIAA20120330026](https://openairdocs.org/sdr/EIAA20120330026.md): Structure · cracked · Mar 30, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon Miscellaneous Structure
  > NR 4 PYLON O/B SIDE FWD ACCESS CUT OUT HAS CRACK IN UPPER FWD SIDE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-019-2
- [SDR EIAA20120327025](https://openairdocs.org/sdr/EIAA20120327025.md): Angle · damaged · Mar 27, 2012 · N489EV · Boeing 747230B · Fuselage Miscellaneous Structure
  > LT BS 800 FRAME STR 17L UPPER AFT HOLE IS MISMATCHED COMMON TO STRAP FRAME INNER CHORD AND DOOR STOP FITTING. REMOVED DAMAGE INNER CHORD ANGLE, FABBED AND INSTALLED REPAIR PER ECRA 489-53-021-2.
- [SDR EIAA20120327024](https://openairdocs.org/sdr/EIAA20120327024.md): Skin · cracked · Mar 27, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 4 PYLON I/B SIDE CRACK IN SKIN OF ACCESS CUT OUT, FWD UPPER CORNER NAC273. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-019-2.
- [SDR EIAA20120326022](https://openairdocs.org/sdr/EIAA20120326022.md): Floorbeam · damaged · Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > ELONGATED HOLE IN UPPER CHORD OF UPPER DECK FLOORBEAM BS 780 LBL 27. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-40-04 FIG 1.
- [SDR EIAA20120326020](https://openairdocs.org/sdr/EIAA20120326020.md): Strap · damaged · Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, Frame
  > RIGHT BS 800 FRAME STRAP AND STR 17R STRAP HAS 2 EACH HOLES WITH TOOL MARKS. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ERCA 489-53-021-2.
- [SDR EIAA20120326019](https://openairdocs.org/sdr/EIAA20120326019.md): Structure · damaged · Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Miscellaneous Structure
  > BS 2231 O/B CHORD ABOVE STR 19L HAS TOOL MARKS INSIDE HOLE AND HOLE ELONGATED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-53-022-2.
- [SDR EIAA20120326018](https://openairdocs.org/sdr/EIAA20120326018.md): Floorbeam · chafed · Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > LOWER CHORD OF UPPER DECK FLOORBEAM BS 560 LBL 87 IS CHAFED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-40-04 FIG 1.
- [SDR EIAA20120326017](https://openairdocs.org/sdr/EIAA20120326017.md): Floorbeam · chafed · Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > LOWER CHORD OF UPPER DECK FLOORBEAM BS 560 RBL 87.50 IS CHAFED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-40-04 FIG 1.
- [SDR EIAA20120326016](https://openairdocs.org/sdr/EIAA20120326016.md): Skin · chafed · Mar 26, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 4 PYLON CAP SKIN O/B SIDE NAC STA 258 HAS CHAFE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 54-31-03 FIG 2 SHEET 1-4 AND ENG DISPOSITION 17.
- [SDR EIAA20120326015](https://openairdocs.org/sdr/EIAA20120326015.md): Skin · chafed · Mar 26, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 4 PYLON CAP SKIN I/B SIDE NAC STA 258 HAS CHAFE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 54-31-03 FIG 2 SHEET 1-4 AND ENG DISPOSITION NR 16.
- [SDR EIAA20120326014](https://openairdocs.org/sdr/EIAA20120326014.md): Structure · damaged · Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Miscellaneous Structure
  > BS 2231 I/B CHORD BELOW STR 19L HAS DRILL START. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-53-022-2
- [SDR EIAA20120306012](https://openairdocs.org/sdr/EIAA20120306012.md): Skin · chafed · Mar 6, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 4 PLYON CAP SKIN I/B SIDE AT NAC 258 HAS CHAFING. REMOVED DAMAGED SECTION OF CAP SKIN, FABBED REPAIR PARTS AND INSTALLED PER EMC ENGINEERING DISPOSITION 3823 AND B747 SRM 54-31-03 PG 2 SHEET 1-4.
- [SDR EIAA20120201009](https://openairdocs.org/sdr/EIAA20120201009.md): Floorbeam · cracked · Feb 1, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > BS 360 FLOORBEAM LBL 54.50 FWD SIDE HAS CRACK. REMOVED DAMAGE FABBED AND INSTALLED REPAIR PER SB 747-53A2431 PART 3 FIG 9.
- [SDR EIAA20120131008](https://openairdocs.org/sdr/EIAA20120131008.md): Floorbeam · cracked · Jan 31, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > BS 340 FLOORBEAM LBL 13.25 AFT SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-747-1587-00 REV J SB 747-53A2431 REV 2 TABLE 1 FIG 9.
- [SDR EIAA20120131007](https://openairdocs.org/sdr/EIAA20120131007.md): Floorbeam · cracked · Jan 31, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > BS 360 FLOORBEAM LBL 13.12 AND 14.65 FWD SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-747-1587-00 REV J SB 747-53A2431 REV 2 PART 3 FIG 9.
- [SDR EIAA20120131006](https://openairdocs.org/sdr/EIAA20120131006.md): Floorbeam · cracked · Jan 31, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > BS 340 FLOORBEAM LBL 29.50 FWD SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-7471587-00 REV J, SB 747-53A2431 REV 2 TABLE 1 FIG 8.
- [SDR EIAA20120131005](https://openairdocs.org/sdr/EIAA20120131005.md): Floorbeam · cracked · Jan 31, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > BS 360 FLOORBEAM LBL 36.70 FWD SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-747-1587-00 REV J PART 3 FIG 9.
- [SDR EIAA20120126004](https://openairdocs.org/sdr/EIAA20120126004.md): Reveal · cracked · Jan 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, Structure
  > BS 2231 RT DOOR FRAME REVEAL HAS CRACK BETWEEN STR 16R AND 17R. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR DOUBLERS PER B747 SRM 53-10-04 FIG 91.
- [SDR EIAA20120101001](https://openairdocs.org/sdr/EIAA20120101001.md): Control Quadrant · lack of lube · Jan 1, 2012 · N489EV · Boeing 747230B · Power Lever
  > ON DESCENT THROUGH 8000 FT NR 2 THRUST LEVER SEIZED JUST FORWARD OF IDLE POSITION. CONFIRMED NR 2 THROTTLE SEIZED JUST FORWARD OF IDLE INSPECTED THROTTLE RUN FROM WING ROOT TO MEC NO OBVIOUS DEFECTS NOTED LUBRICATED QUADRANT AND INTERTOCK MECHANISM PER AMM 76
- [SDR EIAA2011235](https://openairdocs.org/sdr/EIAA2011235.md): Squib · no test · Oct 4, 2011 · N489EV · Boeing 747230B · Fire Bottle, Fixed
  > DURING PREFLIGHT FLIGHT, ENGINEER DISCOVERED FIRE BOTTLE SQUIB 3B WOULD NOT TEST. REMOVED AND REPLACED 3B FIRE BOTTLE SQUIB.
- [SDR EIAA2011229](https://openairdocs.org/sdr/EIAA2011229.md): Sign · unknown · Sep 19, 2011 · N489EV · Boeing 747230B · Emergency Lighting
  > EMERGENCY EXIT LIGHT LT CREW SERVICE DOOR WILL NOT STAY CLOSED. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER B747 MM 33-51-02 PG 301-302 AND B747 SWPM 20-30-00 PG 2-3.
- [SDR EIAA2011099](https://openairdocs.org/sdr/EIAA2011099.md): Battery Pack · discharged · Aug 3, 2011 · N489EV · Boeing 747230B · Emergency Lighting
  > AFT EMERGENCY LIGHT AFT UPPER DECK INOP. REMOVED AND REPLACED BATTERY PACK - OPS CHECK OK PER MM 33-51-00 PG 501.
- [SDR EIAA2011098](https://openairdocs.org/sdr/EIAA2011098.md): Light · defective · Aug 3, 2011 · N489EV · Boeing 747230B · Emergency Lighting
  > EMERGENCY LIGHT RIGHT UPPER DECK COCKPIT CLOSET IS ON AT ALL TIME WHEN A/C POWERS OFF. REMOVED AND REPLACED RIGHT UPPER DECK EMERGENCY LIGHT ASSY PER MM 33-51-00 PAGE 501.
- [SDR EIAA2011097](https://openairdocs.org/sdr/EIAA2011097.md): Warning System · false activation · Jul 31, 2011 · N489EV · Boeing 747230B · Fire Detection
  > NR 3 ENGINE A LOOP FIRE DETECTION SYSTEM FAULT LIGHT ILLUMINATED, GAUGE NEEDLE FLUCTUATING. XFRD TO DMI 182 AS PER MEL 26-1 CAT C DUE 8/11/11. INSTALLED PLACARD. RESEATED AND SHOOK DOWN LOOP SENSOR AND CHECKED FOR CHAFING WIRES. NO FAULT FOUND. OPS CHECK
- [SDR EIAA2011096](https://openairdocs.org/sdr/EIAA2011096.md): Circuit Card · defective · Jul 28, 2011 · N489EV · Boeing 747230B · Fire Detection
  > NR 3 ENGINE "A" LOOP FIRE DETECTION SYSTEM FAULT LIGHT ILLUMINATED. GAUGE FLUCTUATING. ITEM TRANSFERED TO DMI 181 PER MEL REF 26-1 CAT "C" DUE ON 8/7/11 PLACARDS INSTALLED. REPLACED NR 3 ENG "A" LOOP FIRE DETECT CARD IAW MM 26-10-00 PG 401 OPS CK OK IAW MM
- [SDR EIAA2011094](https://openairdocs.org/sdr/EIAA2011094.md): Circuit Card · malfunctioned · Jul 21, 2011 · N489EV · Boeing 747230B · Fire Detection
  > NR 3 ENGINE "A" FIRE DETECTOR FLUCTUATES BETWEEN 2 AND 5 UNITS - SELECTED "B" LOOP - "B" LOOP TESTS OK. TRANSFERED TO DMI 177 PER MEL 26-1 CAT C DUE 7-31-11 2359Z PLACARD INSTALLED. RE-RACKED NR 3 FIRE WARNING AND DETECTOR CARD PER AMM 26-10-00. OPS CHECK O
- [SDR EIAA2011042](https://openairdocs.org/sdr/EIAA2011042.md): Connector · unsecure · May 20, 2011 · N489EV · Boeing 747230B · Light System Wiring
  > FOUND EMERGENCY LIGHT ABOVE UPPER DECK STAIR WELL INOPERATIVE. RESEATED CONNECTOR ON POWER SUPPLY OP'S CHECK OK PER MM 33-51-00/501
- [SDR EIAA2011038](https://openairdocs.org/sdr/EIAA2011038.md): Battery Pack · discharged · Apr 22, 2011 · N489EV · Boeing 747230B · Emergency Lighting
  > CREW SERVICE DOOR EMERGENCY EXIT SIGNS DO NOT TURN ON. REPLACED EMERGENCY LIGHT BATTERY PACK IN CREW CLOSET UPPER SHELF WALL PER B747 MM 33-51-040 PG 204.
- [SDR EIAA2011037](https://openairdocs.org/sdr/EIAA2011037.md): Light · inoperative · Apr 22, 2011 · N489EV · Boeing 747230B · Emergency Lighting
  > EMERGENCY LIGHT AT STA 470L UPPER DECK INOP. REPLACED EMERGENCY LIGHT IN CEILING PER B747 MM 33-51-07 PG 201-207.
- [SDR EIAA2010065](https://openairdocs.org/sdr/EIAA2010065.md): Pin · damaged · Oct 5, 2010 · N489EV · Boeing 747230B · Light System Wiring
  > UPPER DECK CEILING AFT EMERGENCY LIGHT INOP. REPAIRED CONNECTOR PIN 7 (DM335) GOING TO EMERGENCY POWER SUPPLY OP'S. CHECKED NORMAL PER MM 33-51-00 PAGE 501 REF WDM 33-51-12 PG 16.
- [SDR EIAA2010043](https://openairdocs.org/sdr/EIAA2010043.md): Frame · damaged · Jun 30, 2010 · N489EV · Boeing 747230B · Fuselage Main, Frame
  > UPON REMOVAL OF FASTENERS FROM TENSION TIE AT STA 920 RT FOUND 5 HOLES IN FRAME PLUGGED. REMOVED DAMAGE, NDT AREA, REPAIRED TENSION TIE AT BS 920 RT PER B747 SRM 53-10-11 FIG 2 PG 17-35 AND FRAME SECTION FROM STR 6R - 12R PER B747 SRM 53-10-04 FIG 137 PG 897
- [SDR EIAA2010042](https://openairdocs.org/sdr/EIAA2010042.md): Frame · damaged · Jun 30, 2010 · N489EV · Boeing 747230B · Fuselage Main, Frame
  > UPON REMOVAL OF FASTENERS FROM TENSION TIE AT STA 920 RT FOUND 5 HOLES IN FRAME PLUGGED. REMOVED DAMAGE, NDT AREA, REPAIRED TENSION TIE AT BS 920 RT PER SRM 53-10-11 FIG 2 PG 17-35 AND FRAME SECTION FROM STR 6R - 12R PER SRM 53-10-04 FIG 137 PG 897-905.
- [SDR EIAA2010018](https://openairdocs.org/sdr/EIAA2010018.md): Relief Valve · defective · May 19, 2010 · N489EV · Boeing 747230B · Pneumatic Distribution System
  > NR 2 ENGINE FIRE WARNING INFLIGHT. A AND B LOOP NACELLE TEMP IN RED. PYLON VALVE WENT AUTOMATICALLY TO CLOSE, F/E SELECTED BLEED AIR TO OFF, FIRE BELL AND HANDLE LIGHT EXTINGUISHED. REMOVED AND REPLACED PRESSURE REL VALVE, OP'S CHECKED NORM PER MM 36-11-05.
- [SDR EIAA2010006](https://openairdocs.org/sdr/EIAA2010006.md): Wire · burned · Feb 16, 2010 · N489EV · Boeing 747230B · Air Conditioning System Wiring
  > AUTO PRESS CONTROL A/C CIRCUIT BREAKER TRIP, LEF OUT FLOW VALVE ON DMI. FOUND A LARGE BUNDLE OF WIRES SEVERELY DAMAGED (APPROXIMATELY 20-30) AT STA 2020-2040, ABOVE BULK CARGO BAY. REPAIRED WIRE BUNDLE TO LT OUTFLOW VALVE PER AMM 20 STANDARD WIRE PRACTICE, 3
- [SDR EIAA200900128](https://openairdocs.org/sdr/EIAA200900128.md): Indicator · defective · Nov 24, 2009 · N489EV · Boeing 747230B · Trailing Flap Position Indicating System
  > ON CLIMBOUT WHEN RETRACTING FLAPS, INBOARD FLAPS STOPPED AT 2 PERCENT. WHEN ALTERNATE RETRACT WAS ATTEMPTED LJ INBOARD FLAPS DID NOT MOVE AND RESULTED IN AN ASYMMETRIC LOCKOUT. FLAPS DISCREPANCY RECTIFIED WITH NEW INDICATOR.
- [SDR EIAA200900126](https://openairdocs.org/sdr/EIAA200900126.md): Pressure Switch · malfunctioned · Nov 3, 2009 · N489EV · Boeing 747230B · Engine Oil Pressure
  > DURING CRUISE APPROX 7 HOURS INTO FLIGHT NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED FLASHING. RETARDED NR 2 THRUST LEVER, LIGHT CONTINUED TO FLASH. ACCOMPLISHED INFLIGHT ENGINE FAILURE AND SHUTDOWN PROCEDURE. FILTER BYPASS LIGHT REMAINED ON STEADY AFTE
- [SDR EIAA20090055](https://openairdocs.org/sdr/EIAA20090055.md): Oil System · low pressure · Apr 20, 2009 · N489EV · Boeing 747230B · Engine Oil Indicating System
  > DURING CRUISE AT FL 310, NR 4 ENGINE OIL PRESSURE ILLUMINATED. CHECKED OIL QUANTITY GAUGE IT READ ZERO, AND OIL PRESSURE READ 10 PSI. SHUTDOWN ENGINE USING IN-FLIGHT FAILURE AN SHUT DOWN CHECKLIST. WINDMILL FOR 76 MIN, NOTIFY ATC AND DISPATCH, DUMPED FUEL A
- [SDR EIA2007206](https://openairdocs.org/sdr/EIA2007206.md): Slide · disconnected · Dec 4, 2007 · N489EV · Boeing 747230B · Escape Slide
  > RT EMERGENCY DOOR SLIDE PACK INFLATION BOTTLE DEPLOYMENT CABLE DETACHED. DEPLOYMENT CABLE RE-ATTACHED IAW 25-60-00.
- [SDR EIA2007205](https://openairdocs.org/sdr/EIA2007205.md): Skin · cracked · Dec 4, 2007 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NUMBER 2 PYLON PRECOOLER LOWER SKIN, TWO CRACKS FOUND AT AFT UPPER CORNER. REPAIR PER 54-50-35916. PERFORM DVI PER ECRA 489-54-010-1.

Next page: https://openairdocs.org/deregistered/N489EV-2018-01-08/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 = 'N489EV' AND deregistration_id = 'N489EV-2018-01-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N489EV-2018-01-08/reports

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