# Service difficulty reports: N345JW, cancelled Jan 18, 2018

A list on [N345JW, cancelled Jan 18, 2018](https://openairdocs.org/deregistered/N345JW-2018-01-18.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 · 118 reports

- [SDR ARWA20041204](https://openairdocs.org/sdr/ARWA20041204.md): Drive Link · broken · Dec 28, 2004 · N345JW · Doug DC863 · Trailing Edge Flap Control System
  > DURING SERVICE CHECK, FOUND LEFT WING INBOARD FLAP DRIVE LINK BROKEN. REMOVED AND REPLACED LEFT WING INBOARD FLAP DRIVE LINK IN ACCORDANCE WITH DC8-MM 27-51-4. OPERATIONAL CHECK NORMAL IAW DC8-MM 27-51-4.
- [SDR ARWA20041101](https://openairdocs.org/sdr/ARWA20041101.md): O-Ring · damaged · Nov 5, 2004 · N345JW · Doug DC863 · Hydraulic Pump (Electric/Engine), Main
  > LOSS OF HYDRAULIC PRESSURE EN ROUTE HYDRAULIC QUANTITY NORMAL. FOUND O-RING DAMAGED AT NR 3 ENGINE HYDRAULIC DRIVEN PUMP PRESSURE PORT. REMOVED AND REPLACED O-RING AS REQUIRED IN ACCORDANCE WITH DC-8 M/M 22-60-0. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH
- [SDR ARWA20040902](https://openairdocs.org/sdr/ARWA20040902.md): Bleed Valve · defective · Sep 27, 2004 · N345JW · Doug DC863 · Compressor Bleed Valve
  > DURING LINE UP FOR TAKE-OFF, NR 4 ENGINE FAIL TO ACCELERATE. FOUND DEFECTIVE SURGE BLEED VALVE. REMOVED AND REPLACED NR 4 SURGE BLEED VALVE IAW MM 75-30-3 AND SYSTEM OPERATIONAL CHECK NORMAL ON ENGINE RUN-UP IAW MM 71-00 ALL PARAMETERS NORMAL.
- [SDR ARWA20040604](https://openairdocs.org/sdr/ARWA20040604.md): Hydraulic System · contaminated · Jun 25, 2004 · N345JW · Doug DC863 · Hydraulic System, Main
  > PRIOR TO TOP OF DESCEND BOTH HYDRAULIC PUMPS OUTPUT PRESSURE ZERO. AILERON AND RUDDER REVERSION LIGHTS ON. COMPLETED EMERGENCY ABNORMAL HYDRAULIC CHECKLIST. CHECKED A/C FOR HYDRAULIC LEAK, NO LEAKS NOTED. INSPECTED MAIN HYDRAULIC CASE DRAIN FILTERS FOR CON
- [SDR ARWA20040503](https://openairdocs.org/sdr/ARWA20040503.md): Seal Depressor · damaged · May 11, 2004 · N345JW · Doug DC863 · Aircraft Structures
  > ON CLIMB PRESSURIZATION LEAK HAPPENED AT FL 280. UNABLE TO MAINTAIN CABIN PRESSURE 10,000 FT. REMOVED AND REPLACED LOWER SEAL DEPRESSOR IAW AERONAUTICAL ENGINEERS DRAWING AE2412 & DC8 SRM 51-3-0 PAGE 1, 2 & 3. PERFORMED CABIN PRESSURIZATION OPS CHECK IAW NA
- [SDR ARWA20040504](https://openairdocs.org/sdr/ARWA20040504.md): Actuator · inoperative · May 11, 2004 · N345JW · Doug DC863 · Fuel Dump System
  > DUMP CHUTE WILL NOT RETRACT ELECTRICALLY. REMOVE AND REPLACED AC MOTOR ACTUATOR IAW DC8 MM 28-30-2. OPERATIONAL CHECK ACCOMPLISHED FOUND OK IAW DC8 MM 28-30-2.
- [SDR ARWA20030808](https://openairdocs.org/sdr/ARWA20030808.md): Retainer · damaged · Aug 23, 2003 · N345JW · Doug DC863 · Cargo/Baggage Doors
  > MALFUNCTION OF PRESSURIZATION SYSTEM; CABIN CLIMB AT 2000 FT, A MIN UNABLE TO CONTROL. ADJUSTED SEAL RETAINER ON MAIN CARGO DOOR AT FORWARD LOWER AREA IAW MM 52-30-8. OPERATIONAL CHECK SYSTEM NORMAL IAW NASI FLOW CONTROL SYSTEM STC ST466CH.
- [SDR ARWA20030703](https://openairdocs.org/sdr/ARWA20030703.md): Line · broken · Jul 8, 2003 · N345JW · Doug DC863 · Cabin Pressure Sensor
  > ON CLIMB OUT HEARD LOUD NOISE AND CABIN CLIMBED, UNABLE TO MAINTAIN CABIN PRESSURE. ENTERED ON DMI NR 17926 IAW MEL 21-65 CAT "C" PLACARD INSTALLED. FOUND VENTURI SENSING LINE BROKEN. REMOVED AND REPLACED SENSING LINE IAW STC ST466CH; PERFORMED OPERATIONA
- [SDR ARWA20030503](https://openairdocs.org/sdr/ARWA20030503.md): Indicator · failed · May 13, 2003 · N345JW · Doug DC863 · Attitude Gyro and Indicating System
  > CAPTAIN'S ATTITUDE INDICATOR FAILED, TAKE OFF ABORTED. REMOVED & REPLACED NR 1 VG OPS CK GOOD IAW DC8 MM 34-25-0, REMOVED AND REPLACED NR 1 INSTRUMENT AMPLIFIER RACK AND NR 1 HORIZON INDICATOR OPS CHECKED GOOD IAW DC8 MM 34-5-0.
- [SDR ARWA20030304](https://openairdocs.org/sdr/ARWA20030304.md): Splice · cracked · Mar 12, 2003 · N345JW · Doug DC863 · Cargo/Baggage Doors
  > DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; MAIN CARGO DOORS JAMMED, AFT SECTION INTERIOR STA. 280 BETWEEN L-20 AND L-21 WITH 5 INCH CRACK. C/A: REPLACED SIDE BEAM SECTION FROM PRODUCTION SPLICE TO L-21L P/N AE2450-12 IAW SRM 51-1-21.
- [SDR ARWA20030309](https://openairdocs.org/sdr/ARWA20030309.md): Panel · damaged · Mar 12, 2003 · N345JW · Doug DC863 · Wing, Rib/Bulkhead
  > DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; LT W/W STA 902 STRAP PANEL AND SPLICE FITTING AFT FLANGE BOTH SIDE WITH OUT OF LIMITS CHECK IAW SB 53-61. REPLACED TRAPEZOLDAL FITTING P/N 5750092-505 IAW DC8 REPLACEMENT GUIDE AND DC-8-63 INSTALLATION DRA
- [SDR ARWA20030308](https://openairdocs.org/sdr/ARWA20030308.md): Spar Cap · cracked · Mar 12, 2003 · N345JW · Doug DC863 · Wing Spar
  > DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; LT WING STA. XRS 22.000 - STA.XRS 74.000 REAR SPAR UPPER CAP FLANGE WITH 8.00 INCH CRACK.
- [SDR ARWA20030307](https://openairdocs.org/sdr/ARWA20030307.md): Frame · cracked · Mar 12, 2003 · N345JW · Doug DC863 · Fuselage Main, Frame
  > DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; MAIN CARGO COMPARTMENT STA. 1280 BETWEEN L-20R AND L-21R FRAME WITH 0.5 INCH CRACK.
- [SDR ARWA20030306](https://openairdocs.org/sdr/ARWA20030306.md): Frame · cracked · Mar 12, 2003 · N345JW · Doug DC863 · Fuselage Main, Frame
  > DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; MAIN CARGO COMPARTMENT STA 980 BETWEEN L-18 AND L-19 FRAME WITH 1.5 INCH CRACK.
- [SDR ARWA20030305](https://openairdocs.org/sdr/ARWA20030305.md): Web · cracked · Mar 12, 2003 · N345JW · Doug DC863 · Fuselage Miscellaneous Structure
  > "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; MAIN CARGO COMPARTMENT STA. 1180 - STA. 1190 LT CUSP WITH 2 INCH CRACK.
- [SDR ARWA20030303](https://openairdocs.org/sdr/ARWA20030303.md): Door Frame · cracked · Mar 12, 2003 · N345JW · Doug DC863 · Fuselage Main, Structure
  > DURING "C" CHECK THE FOLLOWING WAS FOUND; MAIN CARGO DOOR JAMMED AT AFT SECTION INTERIOR STA 270 BETWEEN L-20L TO L-21L WITH 5 INCH CRACK. REPLACED SIDE BEAN SECTION FROM PRODUCTION SPLICE TO L-21L P/N AE2450-11 IAW DC8 SRM 51-1-21.
- [SDR ARWA20030110](https://openairdocs.org/sdr/ARWA20030110.md): Hose · leaking · Jan 30, 2003 · N345JW · Doug DC863 · Hydraulic System, Main
  > AFTER LANDING, LOST HYDRAULIC PRESSURE. T/S HYDRAULIC LEAK TO THE RT BOGIE TRIM CYLINDER HYDRAULIC FLEX LINE. REMOVED AND REPLACED BOGIE TRIM HYDRAULIC HOSE ASSEMBLY IAW MM 20-12-0; SERVICED MAIN HYDRAULIC RESERVOIR SYSTEM IAW MM 12-30-1, BLED HYDRAULIC SYSTE
- [SDR ARWA20021109](https://openairdocs.org/sdr/ARWA20021109.md): Hydraulic Line · leaking · Nov 20, 2002 · N345JW · Doug DC863 · Hydraulic System, Main
  > LOSS OF HYDRAULIC FLUID ON LANDING. REMOVED AND REPLACED PRESSURE HYDRAULIC LINE ON REVERSER PUMP. LEAK CHECK NORMAL IAW MM 29-10-0.
- [SDR ARWA20021006](https://openairdocs.org/sdr/ARWA20021006.md): Valve · frozen · Oct 16, 2002 · N345JW · Doug DC863 · Landing Gear Brake System
  > ON PUSH BACK (SAP), BRAKES DID NOT RELEASE. UNABLE TO MOVE AIRCRAFT UNDER NORMAL POWER. RETURNED TO BLOCK. AFTER TROUBLESHOOTING AND SYSTEM TEST FOUND BAD DUAL PWR.BRAKE VALVE. REPLACED VALVE. REPLACED AS PRECAUTIONARY MEANS BOTH THE LT MLG SHUTTLE VALVE,
- [SDR ARWA20021005](https://openairdocs.org/sdr/ARWA20021005.md): Connector · failed · Oct 10, 2002 · N345JW · Doug DC863 · Landing Gear Position and Warning
  > OUT OF MIA DURING CLIMB OUT, GEAR NOT LATCHED LIGHT ILLUMINATED AFTER UPLATCH CHECK. PERFORMED CHECKLIST, LIGHT STAYED ON. RETURNED TO MIA. TROUBLESHOOT RETRACT SYSTEM AND FOUND CONNECTOR TO UPLATCH SWITCH BAD. REMOVED AND REPLACED CONNECTOR, RECONNECT UP
- [SDR ARWA20020703](https://openairdocs.org/sdr/ARWA20020703.md): Brake Assy · fire · Jul 5, 2002 · N345JW · Doug DC863 · Brake
  > NR 1 MAIN BRAKE FIRE EXTINGUISHED WITH CO2 SMALL FIRE 15 SECOND DURATION A/C BRAKES WERE SLIGHTLY USED ON LANDING ROLL. REMOVED AND REPLACED NR 1 BRAKE ASSY IAW MM 32-42-1, ALSO REMOVED AND REPLACED NR 1 MAIN WHEEL ASSY IAW MM 32-40-1. ACCOMPLISHED VISUAL IN
- [SDR ARWA20020508](https://openairdocs.org/sdr/ARWA20020508.md): Engine · malfunctioned · May 25, 2002 · N345JW · Doug DC863F · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF, CLIMBING THROUGH 12 THOUSAND OIL QUANTITY CAME DOWN TO 2 GALLONS, FOLLOWED BY OIL PRESSURE LIGHT. PERFORMED ABNORMAL CHECK LIST NR 4 ENGINE OFF (SHUTDOWN). CAME BACK TO SAN SALVADOR WITHOUT ANY MORE ABNORMALITIES. PREPARED NR 4 ENGINE FOR FER
- [SDR ARWA20020204](https://openairdocs.org/sdr/ARWA20020204.md): Transponder · Feb 12, 2002 · N345JW · Doug DC863 · ATC Transponder System
  > LOG PAGE 108434. DISCREPANCY: BOTH TRANSPONDERS MODE "C" ALTTITUDE REPORTING INOPERATIVE, C/B's RESET, NO HELP. AIRCRAFT RETURNED TO KMIA AND LANDED OVERWEIGHT UNEVENTFULL. CORRECTIVE ACTION: REMOVED AND REPLACED BOTH #1 &#2 ATC TRANSPONDERS IAW MM 34-53-0 ACC
- [SDR ARWA20020102](https://openairdocs.org/sdr/ARWA20020102.md): Cylinder · inoperative · Jan 3, 2002 · N345JW · Doug DC863 · Landing Gear Retraction/Extension System
  > UPON DEPARTURE FROM MIA, BOTH DOOR NOT LATCHED AND GEAR NOT LATCHED ILLUMINATED AFTER GEAR RETRACTION ALL CHECKLIST COMPLIED WITH. FOUND LEFT BOGIE TRIM CYLINDER INOP. REMOVED AND REPLACED LT BOGIE TRIM CYLINDER. OPS CHECK NORMAL IAW 32-33-1.
- [SDR ARWA20011123](https://openairdocs.org/sdr/ARWA20011123.md): Wheel · broken · Nov 30, 2001 · N345JW · Doug DC863 · Wheel/Ski/Float
  > AFTER LANDING IN SDQ NR 3 WHEEL INBOARD BROKE AND NR 3 TIRE EXITED THE WHEEL. NR 3 TIRE AND HUB CAUSED DAMAGE TO LT MLG DOOR AND NR 1 ENGINE COWLING, NR 1 OSCILLANTING RING, LT GEAR DOOR BRACKET. REMOVED AND REPLACED NR 3 AND NR 4 MAIN WHEEL ASSY IAW MM 32-4
- [SDR ARWA0010810](https://openairdocs.org/sdr/ARWA0010810.md): Wire · damaged · Aug 22, 2001 · N345JW · Doug DC863 · Weather Radar System
  > NR 1 WEATHER RADAR INOP AFTER TAKEOFF. AIRCRAFT RETURN TO KMIA AND LANDED WITHOUT INCIDENT. REPAIRED COAXIAL WIRE ON RADAR INDICATOR CONNECTOR IAW MM 20-50-1, OPERATIONAL CHECK NORMAL IAW MM 34-41-0.
- [SDR ARWAA0010718](https://openairdocs.org/sdr/ARWAA0010718.md): Pin · broken · Jul 22, 2001 · N345JW · Doug DC863 · Landing Gear Actuator
  > ON DEPARTURE TAKEOFF OUT OF MIAMI, GEAR NOT LATCHED LIGHT ILLUMINATES WITH GEAR IN UP POSITION. ABNORMAL CHECKLIST PERFORMED. LANDED WITHOUT INCIDENT. OVERWEIGHT LANDING WEIGHT INSPECTION COMPLETED. UPON INSPECTION OF THE AIRCRAFT, THE RIGHT HAND MAIN GEAR
- [SDR ARWA0010606](https://openairdocs.org/sdr/ARWA0010606.md): Transformer · malfunctioned · Jun 22, 2001 · N345JW · Doug DC863 · Flight Compartment Lighting
  > TAXI OUT SMOKE CAME OUT OF ELECTRICAL PANEL. AIRCRAFT RETURN TO BLOCKS WITHOUT INCIDENT. LOCATED THE SOURCE, GLARE INSTRUMENT WHITE LIGHTS BALLAST TRANSFORMER. DEACTIVATED GLARESHIELD AND INSTRUMENT WHITE LIGHTS AND ENTERED ON DMI 15265 AS PER MEL 33-1 CAT
- [SDR ARWA0010406](https://openairdocs.org/sdr/ARWA0010406.md): Bleed Valve · Apr 26, 2001 · N345JW · Doug DC863 · Compressor Bleed Control
  > Log Page 54673. Discrepancy: Take Off roll was aborted at 65 Knots due to compressor stall on #3 engine. Corrective Action: Performed test of compressor bleed valve IAW MM 75-30-3 found normal. Checked on engine run up IAW MM 71-00 found normal operation no co
- [SDR ARWA74100](https://openairdocs.org/sdr/ARWA74100.md): Compressor · stalled · Apr 26, 2001 · N345JW · Doug DC863 · Turbine Engine Compressor Section
  > TAKEOFF ROLL WAS ABORTED AT 65 KNOTS DUE TO COMPRESSOR STALL ON NR 3 ENGINE. PERFORMED TEST OF COMPRESSOR BLEED VALVE IAW MM 75-30-3, FOUND NORMAL. CHECKED ON ENGINE RUN UP IAW MM 71-00, FOUND NORMAL OPERATION NO COMPRESSOR STALL NOTED.
- [SDR ARWA0010304](https://openairdocs.org/sdr/ARWA0010304.md): Hydraulic Line · leaking · Mar 13, 2001 · N345JW · Doug DC863 · Hydraulic System, Auxiliary
  > IN TOP OF CLIMB LOSS OF HYDRAULIC FLUID AND PRESSURE DOWN TO THE STAND-PIPE SLOWLY. FOLLOWED EMERGENCY CHECK LIST. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED PRESSURE LINE TO AUXILIARY PUMP OPERATIONAL CHECK IAW MM 29-0-3 OPS NORMAL, NO LEAKS NO
- [SDR ARWA990901](https://openairdocs.org/sdr/ARWA990901.md): Duct · rupture · Aug 30, 1999 · N345JW · Doug DC863 · Air Distribution System
  > SJU - FLT 501 - UNABLE TO CONTROL CABIN. NOISE COMING FROM UNDERNEATH COCKPIT FLOOR. EMERGENCY DESCENT PERFORMED. LANDED WITHOUT INCIDENT. REPLACED DISTRIBUTION DUCT. LEAK CHECKED OK PER MM 21-50-0. (M)
- [SDR ARWA990705](https://openairdocs.org/sdr/ARWA990705.md): Proximity Card · malfunctioned · Jul 27, 1999 · N345JW · Doug DC863 · Landing Gear Position and Warning
  > MIA - FLT 9038 - DURING GEAR RETRACTION, GOT DOOR NOT LATCHED LIGHT. FOLLOWED DOOR NOT LATCHED LIGHT CHECKLIST. DID NOT SOLVE PROBLEM. RETURNED TO MIAMI. RERACKED PROXIMITY CARD J-12 AND J-13. INDICATION OF GEAR DOOR WARNING. OPS CHECKED NORMAL IAW 32-10
- [SDR ARWA980904](https://openairdocs.org/sdr/ARWA980904.md): Boost Pump · failed · Sep 10, 1998 · N345JW · Doug DC863 · Fuel Boost Pump
  > NR 4 ALT BOOST PUMP POPS C/B IN FLIGHT. REMOVED AND REPLACED NR 4 ALT FUEL BOOST PUMP, OPS CHECKED NORMAL IAW MM 28-22-0.
- [SDR ARWA9807133](https://openairdocs.org/sdr/ARWA9807133.md): Gear Box · leaking · Jul 30, 1998 · N345JW · Doug DC863 · Turbine Engine Reduction Gear
  > BLD - FLT 505 - AFTER TAKEOFF OF BDL CREW PHONE LOST OIL QTY NR 2 ENGINE SHUT DOWN A/C DIVERTED TO MIAMI. AFTER LANDING, NR 2 ENGINE WAS OIL SERVICE, MOTORIZED. FOUND GEAR BOX LEAKING. ENGINE WILL BE REPLACED. (M)
- [SDR ARWA980799](https://openairdocs.org/sdr/ARWA980799.md): Controls · worn · Jul 16, 1998 · N345JW · Doug DC863 · Aileron Control System
  > LEFT AILERON VERY STIFF IN RIGHT TURN WHILE TROUBLESHOOTING AILERONS PROBLEMS. FOUND LT CABLE ROD END BEARING WORN, CRANK CRACKED AND SPOILER MIXER ROD END BEARING WORN. REMOVED AND REPLACED LATERAL SPOILER LT CONTROL CABLE IAW MM 20-17-0. REPLACED ACTUATOR
- [SDR ARWA980796](https://openairdocs.org/sdr/ARWA980796.md): Gcu · failed · Jul 10, 1998 · N345JW · Doug DC863 · AC Generation System
  > SJU - FLT 508 - PREFERENTIAL SYSTEM INOP ON PUSH BACK. REMOVED AND REPLACED NR 3 GENERATOR GCU. OPS CHECKED NORMAL IAW MM 24-20-0. (M)
- [SDR ARWA980703](https://openairdocs.org/sdr/ARWA980703.md): Switch · out of adjust · Jul 6, 1998 · N345JW · Doug DC863 · Door Warning System
  > LCK - FLT 507 - BELLY DOOR ILLUMINATED, ABORTED TAKEOFF AND RETURNED TO BLOCKS. AFTER BELLY DOOR WAS CYCLED AND LIGHT EXTINGUISHED. SECOND TAKEOFF WAS UNEVENTFUL. BRAKE TEMPS OK, ABORTED LESS THAN 60 KNOTS. TROUBLESHOT AND FOUND 'C' BELLY DOOR LIMIT SWITCH
- [SDR ARWA980736](https://openairdocs.org/sdr/ARWA980736.md): Skin · corroded · Jun 9, 1998 · N345JW · Doug DC863 · Fuselage Main, Plate/Skin
  > TAILCONE, SEVERAL SPOTS OF LEVEL 1 CORROSION ON SKIN, RT SIDE, FS 1890 TO 1995. REMOVED CORROSION FOUND TO BE BEYOND LIMITS IAW DC-8 SRM 53-2-20. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-0, 51-1-4. TREATED, PRIMED AND INSTALLED REPAI
- [SDR ARWA980735](https://openairdocs.org/sdr/ARWA980735.md): Skin · corroded · Jun 9, 1998 · N345JW · Doug DC863 · Rudder, Plate/Skin
  > VERTICAL STABILIZER LEVEL II CORROSION IN RUDDER SKIN RIGHT SIDE ZR 110.750. SMOOTHED AND BLENDED OUT CORROSION AREA FABRICATED REPAIR PARTS IAW EO NR CF-345JW 14/98. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-20D, 51-1-21 8
- [SDR ARWA980733](https://openairdocs.org/sdr/ARWA980733.md): Shim · corroded · Jun 9, 1998 · N345JW · Doug DC863 · Fuselage Main, Plate/Skin
  > LT MLG W/W LEVEL 1 CORROSION IN FWD LT UPPER ANGLE SHIM FUS STA 857.000. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC-8 SRM 53-2-0. REMOVED CORRODED SHIM CLEANED SURROUNDING AREA WITHIN LIMITS IAW DC-8 SRM 53-2-0. FABRICATED NEW SHIM IAW DC-8 SRM 51-1
- [SDR ARWA980732](https://openairdocs.org/sdr/ARWA980732.md): Doubler · corroded · Jun 9, 1998 · N345JW · Doug DC863 · Fuselage Miscellaneous Structure
  > EXTERIOR FUSELAGE LEVEL II CORROSION IN DOUBLER FUS STA 1660-1680 AND L-33R. REMOVED IMPROPER REPAIR FABRICATED REPAIR PARTS IAW EO CF N345JW. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-20D, 51-1-21, 8110-3 FORM ISSUED DATED
- [SDR ARWA980731](https://openairdocs.org/sdr/ARWA980731.md): Skin · damaged · Jun 9, 1998 · N345JW · Doug DC863 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE TEMPORARY REPAIR AT FS 1220 BETWEEN L-27L AND L-28L. REMOVED TEMPORARY REPAIR. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-1, 53-4-1, 51-1-4. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21, 51-1-20D REF SEE C
- [SDR ARWA980730](https://openairdocs.org/sdr/ARWA980730.md): Skin · damaged · Jun 9, 1998 · N345JW · Doug DC863 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE TEMPORARY REPAIR AT FS 1200 BETWEEN L-27L, SNF L-28L. REMOVED TEMPORARY REPAIR FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-1, 53-4-1, 51-1-4. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11,51-1-21, 51-1-20D REF SEE CF
- [SDR ARWA980729](https://openairdocs.org/sdr/ARWA980729.md): Skin · damaged · Jun 9, 1998 · N345JW · Doug DC863 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE TEMPORARY REPAIR AT FS 1160 BETWEEN L27L AND L 28L. REMOVED TEMPORARY REPAIR FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-1, 53-4-1, 51-1-4. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21, 51-1-20D REF SEE CF W
- [SDR ARWA980728](https://openairdocs.org/sdr/ARWA980728.md): Skin · damaged · Jun 9, 1998 · N345JW · Doug DC863 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE TEMPORARY REPAIR AT FS 55.000 BETWEEN L- 33L AND L-34L. REMOVED TEMPORARY REPAIR FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-1, 53-3-3, 51-1-4. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-2, 51-1-20D REF WORK
- [SDR ARWA980727](https://openairdocs.org/sdr/ARWA980727.md): Skin · damaged · Jun 9, 1998 · N345JW · Doug DC863 · Service Doors
  > TEMPORARY REPAIR IN RT SERVICE DOOR AFT LOWER CORNER. REMOVED TEMPORARY REPAIR. FABRICATED REPAIR PARTS IAW EO NR CF N345JW 3/98 REV 1 ACTION NR 355211 FILE 98-04-02-004 DRAWING 01763. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11,
- [SDR ARWA980726](https://openairdocs.org/sdr/ARWA980726.md): Frame · damaged · Jun 9, 1998 · N345JW · Doug DC863 · Fuselage Miscellaneous Structure
  > IMPROPER REPAIR IN LT AFT DOOR FRAME AFT LWR PART. REMOVED IMPROPER REPAIR. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-0, 53-4-1, 51-1-4. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21, 51-1-20D. REF SEE CF WORK ORDER 020663
- [SDR ARWA980725](https://openairdocs.org/sdr/ARWA980725.md): Skin · damaged · Jun 9, 1998 · N345JW · Doug DC863 · Service Doors
  > TEMPORARY REPAIR IN LT AFT DOOR FWD LWR CORNER. REMOVED TEMPORARY REPAIR FABRICATED REPAIR PARTS IAW EO NR CF-N345JW 4/98 REV 2 ACTION NR 365790 FILE 98-04-10-008, 98-04-01-0071, DRAWING 01780. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 CF WORK ORDER
- [SDR ARWA980724](https://openairdocs.org/sdr/ARWA980724.md): Skin · damaged · Jun 9, 1998 · N345JW · Doug DC863 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE TEMPORARY REPAIR AT FS 1723, BETWEEN L-30R AND L-32R. REMOVED TEMPORARY REPAIR. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-1, 53-5-3, 51-1-4. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21, 51-1-20D. REF S

Next page: https://openairdocs.org/deregistered/N345JW-2018-01-18/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 = 'N345JW' AND deregistration_id = 'N345JW-2018-01-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N345JW-2018-01-18/reports

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