# Service difficulty reports: N441J, cancelled Jul 14, 2017

A list on [N441J, cancelled Jul 14, 2017](https://openairdocs.org/deregistered/N441J-2017-07-14.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 4 · 169 reports

- [SDR ARWA20070901](https://openairdocs.org/sdr/ARWA20070901.md): Engine · power loss · Sep 23, 2007 · N441J · Doug DC863F · Engine (Turbine/Turboprop)
  > ABORT TAKEOFF DUE TO NR 1 ENGINE UNABLE TO MAKE MAXIMUM TAKEOFF POWER EPR I-68 AT FIREWALL. ABORTED PRIOR REACHING 80 KNOTS. OPERATIONAL CHECKED NR 1 ENGINE AT ENGINE RUN-UP IN ACCORDANCE TO M/M 71-00; NOTED NR 1 EPR READING 0.1 LOW. ALL OTHER INDICATION NO
- [SDR ARWA20070802](https://openairdocs.org/sdr/ARWA20070802.md): Indicator · malfunctioned · Aug 18, 2007 · N441J · Doug DC863F · Engine EGT/TIT Indicating System
  > POWER REDUCTION REQUIRED ON NR 2 ENGINE AFTER TAKEOFF IN ORDER TO MAINTAIN EGT LIMIT. 09-04-07 REMOVED AND REPLACED NR 2 EGT INDICATOR IN ACCORDANCE WITH MM 77-20-1. REMOVED AND REPLACED FCU IN ACCORDANCE WITH DC-8 M/M 7320-1; ACCOMPLISHED ENGINE RUN-UP IN
- [SDR ARWA20070702](https://openairdocs.org/sdr/ARWA20070702.md): Brake Assy · damaged · Jul 5, 2007 · N441J · Doug DC863F · Landing Gear Brake System
  > WHILE TAXING TO RAMP, AFTER LANDING, BRAKES LOCKED UP. NR 5 BRAKE ASSEMBLY LOCKED UP ON TAXI WAY. REMOVED AND REPLACED NR 5 ANTI-SKID WHEEL SPEED TRANSDUCER IAW MM 32-43-2. NR 5 MAIN WHEEL ANTI-SKID TRANSDUCER DAMAGED. REMOVED AND REPLACED NR 5 BRAKE ASSEMBLY
- [SDR ARWA20070701](https://openairdocs.org/sdr/ARWA20070701.md): Brake Assy · locked · Jul 4, 2007 · N441J · Doug DC863F · Brake
  > AFTER LANDING, ON TAXI TO RAMP, BRAKES "LOCKED UP". REMOVED AND REPLACED BRAKE ASSEMBLY NR 2 IN ACCORDANCE WITH DC-8 M/M 32-42-1. OPERATIONAL CHECK FOR LEAKS OK.
- [SDR ARWA20070606](https://openairdocs.org/sdr/ARWA20070606.md): Transducer · inoperative · Jun 13, 2007 · N441J · Doug DC863F · Brake Anti-Skid Section
  > PRIOR TO TAKEOFF ANTI-SKID INOPERATIVE LIGHT REMAINED ILLUMINATED; RETURN TO BLOCK. REMOVED AND REPLACED NR 8 MAIN LANDING GEAR WHEEL SPEED TRANSDUCER IN ACCORDANCE WITH M/M 32-43-02; GROUND TEST NORMAL IN ACCORDANCE WITH M/M 32-43-00.
- [SDR ARWA20070604](https://openairdocs.org/sdr/ARWA20070604.md): Unknown · unknown · Jun 7, 2007 · N441J · Doug DC863F · Central Warning
  > BEFORE TAKEOFF ANTI-SKID INOPERATIVE LIGHT PLUS RAI (F/W) LIGHTS BOTH ILLUMINATED.
- [SDR ARWA20070602](https://openairdocs.org/sdr/ARWA20070602.md): Bypass Valve · broken · Jun 5, 2007 · N441J · Doug DC863F · Aileron Control System
  > AILERON MANUAL REVERSER LIGHT STAYS ON WHILE AILERON IS POWERED AND CONTROL CHECK UNSATISFACTORY. REMOVED AND REPLACED BROKEN BYPASS VALVE TURNBUCKLE AND ADJUSTED AILERON POWER TO MANUAL REVERSION MECHANISM IN ACCORDANCE WITH DC-8 M/M 27-11-8; OPERATIONAL CHE
- [SDR ARWA20070306](https://openairdocs.org/sdr/ARWA20070306.md): Hose · leaking · Mar 22, 2007 · N441J · Doug DC863F · Hydraulic System, Main
  > IN FLIGHT EN COUNTER A LOSS OF HYDRAULIC PRESSURE; PERFORMED EMERGENCY CHECKLIST. T/S AND FOUND RT MAIN LANDING GEAR BOGIE TRIM CYLINDER HYDRAULIC HOSE LEAKING; REMOVED AND REPLACED IN ACCORDANCE WITH DC8 M/M 32-33-1. SERVICE HYDRAULIC RESERVOIR IN ACCORDANC
- [SDR ARWA20060701](https://openairdocs.org/sdr/ARWA20060701.md): Skin · corroded · Jul 8, 2006 · N441J · Doug DC863F · Elevator, Plate/Skin
  > DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; LEFT ELEVATOR XE 195-313 T/E LOWER SKIN WITH CORROSION.
- [SDR ARWA20060702](https://openairdocs.org/sdr/ARWA20060702.md): Panel · corroded · Jul 8, 2006 · N441J · Doug DC863F · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; LT HORIZONTAL STABILIZER BETWEEN XE 312.500 AND XE 149.000 T/E UPPER PANELS WITH CORROSION.
- [SDR ARWA20060703](https://openairdocs.org/sdr/ARWA20060703.md): Skin · corroded · Jul 8, 2006 · N441J · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR STATION 25, L-33R SKIN WITH CORROSION.
- [SDR ARWA20060303](https://openairdocs.org/sdr/ARWA20060303.md): Pin · unknown · Mar 23, 2006 · N441J · Doug DC863F · Navigation System
  > FIRST OFFICER'S COURSE DEVIATION INDICATOR (CDI) DOES NOT CORRESPOND TO OMNI BEARING SELECTOR (OBS) IN FLIGHT. FIRST OFFICER'S HEADING "BUG" DOES NOT CORRESPOND TO SELECTED HEADING. REMOVED AND REPLACED PIN NR 1 AT PTO-117 IN ACCORDANCE WITH M/M 20-50-1 AND
- [SDR ARWA20051202](https://openairdocs.org/sdr/ARWA20051202.md): Actuator · leaking · Dec 20, 2005 · N441J · Doug DC863F · Rudder Actuator
  > LOG PAGE NR 116558. ON POST FLIGHT FOUND LEAKING BY EMPANAGE LOWER SIDE REAR STRIKE PAD REAR ACCESS PANEL. REMOVED AND REPLACED RUDDER PACK ACTUATOR IAW MM 27-21-6. LEAK CHECK AND OPERATIONAL CHECK IAW MM 27-20-0 FOUND NORMAL, NO LEAKS NOTICE.
- [SDR ARWA20051002](https://openairdocs.org/sdr/ARWA20051002.md): Line · leaking · Oct 8, 2005 · N441J · Doug DC863F · Hydraulic System, Main
  > LOST HYD FLUID FROM MAIN HYD RESERVOIR AFTER LANDING. UPON INSPECTION; FOUND FLEX LINE LEAKING ON RT MAIN GEAR TRUCK O/B HYD MANIFOLD NEXT TO BOGGIE TRIM ACTUATOR. REMOVED & REPLACED LINE WITH E EACH FLEX LINE FROM FAK. REPLACED DAMAGE LINE IN HYD SYSTEM ON
- [SDR ARWA20050803](https://openairdocs.org/sdr/ARWA20050803.md): Link Assy · vibration · Aug 17, 2005 · N441J · Doug DC863F · Nose/Tail Landing Gear
  > AFTER TAKEOFF AND GEAR RETRACTION, EXPERIENCED CONTINUOUS VIBRATION AND NOISE FROM NOSE WHEEL WELL AREA. RETURNED AND LANDED TO INVESTIGATE. REMOVED AND REPLACED RT NOSE DOOR LINK ASSEMBLY IAW MM. PERFORMED ADJUSTMENT TEST SYSTEM IAW M/M. TEST GOOD.
- [SDR ARWA20050507](https://openairdocs.org/sdr/ARWA20050507.md): Wire · open · May 28, 2005 · N441J · Doug DC863F · Electrical Power System Wiring
  > AFTER TAKEOFF, ZNS ON NR 2 GENERATOR WITH LEFT EMERGENCY BUS POWER FAIL LIGHT ON. PERFORMED ABNORMAL CHECKLIST TO NO AVAIL; PERFORMED FUEL DUMP AS PER CHECKLIST. TRANSFERRED TO DMI 19258 AS PER MEL 24-1 CAT-C (ON T/S FOUND NR 2 GENERATOR CAUSING FAIL ZNS).
- [SDR ARWA20050504](https://openairdocs.org/sdr/ARWA20050504.md): Generator · failed · May 7, 2005 · N441J · Doug DC863F · AC Generator-Alternator
  > DURING CLIMB-OUT, NR 2 GEN SYSTEM DEVELOPED A ZNS. AFTER PERFORMING ABNORMAL CHECK-LIST ONLY LT EMERGENCY BUSS WAS RESTORED. REMOVED AND REPLACED CSD AND AC GENERATOR IN ACCORDANCE WITH DC-8 M/M 24-10-1 AND 24-20-1. LEAKS CHECKED; NO LEAKS NOTED; GENERATOR
- [SDR ARWA20050404](https://openairdocs.org/sdr/ARWA20050404.md): Connector · dirty · Apr 28, 2005 · N441J · Doug DC863F · Flight Control System Wiring
  > DURING TAXI, ELEVATOR POSITION INDICATOR (EPI) FAILED DURING FLIGHT CONTROL CHECK. TRANSFERRED TO DMI NR 19171 AS PER MEL 27-9 CAT "C". CLEANED AND SECURED ELEVATOR EPI INDICATOR IN ACCORDANCE WITH M/M 31-10-30. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/
- [SDR ARWA20041203](https://openairdocs.org/sdr/ARWA20041203.md): Amplifier · malfunctioned · Dec 17, 2004 · N441J · Doug DC863F · Fire Detection
  > AFTER TAKEOFF NR 4 ENGINE FIRE WARNING ILLUMINATED INTERMITTENTLY, SHUT DOWN ENGINE AND RETURNED TO KMIA AFTER FUEL DUMPING. OVERWEIGHT LANDING IN KMIA, SMOOTH LANDING. REMOVED AND REPLACED AMPLIFIER (POSITION NR 4) IN ACCORDANCE WITH MM 26-10-4 AND REMOVED
- [SDR ARWA20041005](https://openairdocs.org/sdr/ARWA20041005.md): Fire Loop · shorted · Oct 24, 2004 · N441J · Doug DC863F · Fire Detection
  > ON CLIMBOUT THROUGH 15,000 FT MASTER FIRE WARNING SOUNDED WITH LIGHT INDICATION ON NR 4 ENGINE. PERFORMED EMERGENCY CHECKLIST (RETARDED POWER LEVER, FIRE SHUTOFF LEVER FORWARD, LIGHT CONTINUED ON, FIRE EXT AGENT, LIGHT WENT OUT). COMPLETED CHECKLIST, ALL OTH
- [SDR ARWA20040904](https://openairdocs.org/sdr/ARWA20040904.md): Pin · damaged · Sep 29, 2004 · N441J · Doug DC863F · Main Landing Gear
  > DURING UP-LATCH CHECK THE GEAR NOT LATCHED, LIGHT ILLUMINATED AND PERFORMED ABNORMAL CHECKLIST, THEN BOTH GEAR NOT LATCHED AND DOOR NOT LATCHED REMAINED ILLUMINATED. REMOVED RT GEAR ASSY SENT TO AAR LANDING GEAR; REPAIRED STUD ASS PART NR 5759145508 ON RT GEA
- [SDR ARWA20040804](https://openairdocs.org/sdr/ARWA20040804.md): Indicator · failed · Aug 22, 2004 · N441J · Doug DC863F · Rate of Climb Indicator
  > DURING TAXI, FIRST OFFICER'S VERTICAL SPEED INDICATOR (VSI) DISPLAY SHOWS REPEATER ANNUNCIATOR. FAILURE AND NO NEEDLE. REMOVED AND REPLACED TCAS/VSI AT FIRST OFFICER'S SIDE. CHECK SYSTEM ON GROUND OK IN ACCORDANCE WITH MM 34-12-0 AND 34-11-1.
- [SDR ARWA20040802](https://openairdocs.org/sdr/ARWA20040802.md): Indicator · inoperative · Aug 17, 2004 · N441J · Doug DC863F · Weather Radar System
  > WEATHER RADAR DOES NOT PAINT WEATHER NOR DOES IT WORK IN MAPPING MODE. TEST FUNCTION IS NORMAL; AIRCRAFT RETURNED. REMOVED AND REPLACED WHEATHER INDICATOR IN ACCORDANCE WITH MM 34-00; OPERATIONAL CHECK DUE; REMOVED AND REPLACED RADAR R/T IN ACCORDANCE WITH M
- [SDR ARWA20040801](https://openairdocs.org/sdr/ARWA20040801.md): Transceiver · failed · Aug 15, 2004 · N441J · Doug DC863F · Weather Radar System
  > CLIMBING WEATHER RADAR DOES NOT PAINT WEATHER; AIRCRAFT RETURNED. REMOVED AND REPLACED WEATHER RT AND ANTENNA IAW MM 34-41-0 AND 34-41-1 GROUND TEST NORMAL.
- [SDR ARWA20040703](https://openairdocs.org/sdr/ARWA20040703.md): Unknown · unknown · Jul 15, 2004 · N441J · Doug DC863F · Wing Structure
  > AFTER APP TAKEOFF POWER HEARD BANG ON LEFT HAND SIDE WING. INSPECTED LEFT HAND WING IN ACCORDANCE WITH MM 57-00; NO OBVIOUS DEFECTS NOTED. ALSO INSPECTED LEFT HAND MAIN LANDING GEAR AND DOORS IN ACCORDANCE WITH MM 32-10-0, NO OBVIOUS DEFECTS NOTED. PERFORME
- [SDR ARWA20040301](https://openairdocs.org/sdr/ARWA20040301.md): Fitting · cracked · Mar 17, 2004 · N441J · Doug DC863F · Fuselage, Landing Gear Attach Fittings
  > DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 3 PYLON STATION YN 300 APPROX. FOOT STOOL FITTING LEFT SIDE WITH CRACK. REMOVED AND REPLACED FOOT STOOL FITTING FROM NR 3 PYLON IN ACCORDANCE WITH BOEING MESSAGE INW-SCL-04-000084, DATED 22-MAR-04, DOUGLAS
- [SDR ARWA20040202](https://openairdocs.org/sdr/ARWA20040202.md): Web · corroded · Feb 2, 2004 · N441J · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE INTERIOR BETWEEN STA 1060.000 AND STA 1080.000 LT CUSP WITH CORROSION. ACCOMPLISHED REPAIR IN ACCORDANCE WITH BOEING ROD SKETCH 04-05-18-001. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR.
- [SDR ARWA20040201](https://openairdocs.org/sdr/ARWA20040201.md): Cargo Track · corroded · Feb 2, 2004 · N441J · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT LOWER CARGO COMPARTMENT BETWEEN STA 940.000 AND STA 1500.000, RBL 58.5 INCHES TRACK WR SECTION WITH CORROSION. REMOVED CORROSION IN ACCORDANCE WITH DC-8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IN ACCORDANCE
- [SDR ARWA20040104](https://openairdocs.org/sdr/ARWA20040104.md): Keelbeam · cracked · Jan 13, 2004 · N441J · Doug DC863F · Fuselage Main, Keel
  > DURING A C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; LT MAIN LANDING GEAR W/W STATION 920, KEELBEAM LT TEE EXTRUSION WITH 3 INCH CRACK. REPAIRED KEEL WEB STIFFENER AT STA 920 IN ACCORDANCE WITH BOEING MESSAGE INW-SCL-04-00005H, DATED 02 MARCH 04, DC8 SRM 51-2
- [SDR ARWA20031207](https://openairdocs.org/sdr/ARWA20031207.md): Bulkhead · corroded · Dec 19, 2003 · N441J · Doug DC863F · Fuselage Main, Bulkhead
  > NR 970. DURING (C) CHECK INSPECTION, NLG WW RT TUNNEL STATION 8.000 PRESSURE BULKHEAD FORWARD FACE. NOSE LANDING GEAR RT FITTING WITH CORROSION AT L-31.
- [SDR ARWA20031003](https://openairdocs.org/sdr/ARWA20031003.md): Warning Light · false activation · Oct 20, 2003 · N441J · Doug DC863F · Door Warning System
  > LANDING GEAR DOOR NOT LATCH LIGHT ILLUMINATED AFTER TAKEOFF; PERFORMED ABNORMAL CHECKLIST, LIGHT WENT OUT. CLEANED, INSPECTED & LUBRICATED LANDING GEARS AND DOORS IAW DC8 MM 12-81-1. ACCOMPLISHED GEARS SWING IAW DC8 MM 32-30-0. NO DEFECTS NOTED.
- [SDR ARWA20030914](https://openairdocs.org/sdr/ARWA20030914.md): Bleed Valve · stuck · Sep 21, 2003 · N441J · Doug DC863F · Compressor Bleed Valve
  > UNABLE TO OBTAIN MAX POWER INDICATION WITH NR 1 TROTTLE AT IT'S FULL FORWARD STOP POSITION. FOUND NR 1 ENGINE SURGE BLEED VALVE STUCK OPEN; REMOVED AND REPLACED NR 1 ENGINE SURGE BLEED VALVE IAW DC-8 MM 75-30-3; OPERATIONAL CHECK NORMAL IAW MM 71-00.
- [SDR ARWA20030901](https://openairdocs.org/sdr/ARWA20030901.md): Cylinder · broken · Sep 3, 2003 · N441J · Doug DC863F · Landing Gear Retraction/Extension System
  > AFTER TAKE-OFF, WHEN GEAR WAS RETRACTED; NOT LATCHED AND DOORS NOT LATCHED. LIGHT REMAINED ILLUMINATED. PERFORMED LANDING GEAR SYSTEM ABNORMAL CHECK LIST AND RETURNED TO MNMG. FOUND RT GEAR BOGIE TRIM CYLINDER BROKEN AT FORWARD ATTACH POINT; REMOVED AND RE
- [SDR ARWA20030807](https://openairdocs.org/sdr/ARWA20030807.md): Door Frame · cracked · Aug 21, 2003 · N441J · Doug DC863F · Fuselage Main, Structure
  > DURING ROUTINE INSPECTION THE FOLLOWING WAS FOUND; AFT SERVICE DOOR JAMB, AFT TOP CORNER WITH CRACK OF 1.125 INCH. REPAIRED THE AFT SERVICE DOOR JAMB AFT TOP CORNER IAW SRM 53-2-0 FIG 16, SHEETS 4, 5, 6, 7 & 8 TEMPORARY REVISION 53-156, DATED 12/20/02. (EA 10
- [SDR ARWA20030806](https://openairdocs.org/sdr/ARWA20030806.md): Door Frame · cracked · Aug 21, 2003 · N441J · Doug DC863F · Fuselage Main, Structure
  > DURING ROUTINE INSPECTION THE FOLLOWING WAS FOUND; AFT ENTRANCE DOOR JAMB AFT BOTTOM CORNER WITH CRACKS OF 0.625 & 0.437 INCH. REPAIRED THE AFT ENTRANCE DOOR JAMB AFT BOTTOM CORNER IAW SRM 53-2-0 FIG 18, SHEETS 1, 5, 6, 7 & 8, TEMPORARY REVISION 53-134 & TEMP
- [SDR ARWA20030801](https://openairdocs.org/sdr/ARWA20030801.md): Bleed Valve · inoperative · Aug 5, 2003 · N441J · Doug DC863F · Compressor Bleed Valve
  > COMPRESSOR STALL NR 2 ENGINE COMMENCING THE TAKE OFF ROLL. REJECTED TAKE OFF (RTO). REMOVED AND REPLACED NR 2 PRESSURE RATIO SURGE BLEED VALVE IAW MM 75-30-3. OPERATIONAL CHECK ON RUN UP IAW MM 71-0 FOUND NORMAL.
- [SDR ARWA20030602](https://openairdocs.org/sdr/ARWA20030602.md): Transmitter · inoperative · Jun 10, 2003 · N441J · Doug DC863F · Engine Oil Pressure
  > AFTER BRAKE RELEASE, WHILE SETTING MAX POWER, NUMBER ONE ENGINE OIL PRESSURE ROSE TO 60 PSI. REMOVED AND REPLACED PRESSURE TRANSMITTER IAW MM 79-32-1. ACCOMPLISHED ENGINE RUN UP IAW ARROW AIR J/C 72-000-30-02
- [SDR ARWA20030302](https://openairdocs.org/sdr/ARWA20030302.md): Wire · damaged · Mar 11, 2003 · N441J · Doug DC863F · Brake Anti-Skid Section
  > ON FINAL ANTI-SKID LIGHT STAYED ON WITH LFI INDICATION. CHECKED ANTI-SKID WIRING IAW W/D 32-3-0. FOUND BROKEN WIRE GOING TO LT IN-BOUND VALVE, REPAIRED WIRE IN ACCORDANCE WITH MM 20-50-1, OPERATIONAL CHECKED ANTI-SKID SYSTEM IAW MM 32-43-0. OPERATIONAL CHECK
- [SDR ARWA20030105](https://openairdocs.org/sdr/ARWA20030105.md): Line · leaking · Jan 25, 2003 · N441J · Doug DC863F · Engine Oil Distribution (Airframe Furnished)
  > NR 2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO FLUCTUATING OIL PRESSURE AND INTERMITTENT PRESSURE WARNING LIGHT AT 1555Z WINDMILLING OIL PRESSURE 15-25 PSI. INSPECTED NR 2 ENGINE, FOUND RIGID LINE BETWEEN MAIN OIL FILTER AND DIFFERENTIAL PRESSURE SWITCH DAMAGED (L
- [SDR ARWA20030101](https://openairdocs.org/sdr/ARWA20030101.md): Spar Cap · Jan 2, 2003 · N441J · Doug DC863F · Wing, Attach Fittings
  > LOG PAGE # 503179. DISCREPANCY: DURING 1A CHECK THE FOLLOWING WAS FOUND; ITEM # 128M: L/H WING AUXILIARY SPAR INBD. UPPER LOG WITH CRACK. GENERATED BY J/C # 51-020-04-06-1. CORRECTIVE ACTION: ACCOMPLISHED TEMPORARY REPAIR IN ACCORDANCE WITH BOEING MESSAGE I
- [SDR ARWA20021103](https://openairdocs.org/sdr/ARWA20021103.md): Gyro · failed · Nov 7, 2002 · N441J · Doug DC863 · Directional Gyro and Indicating System
  > FIRST OFFICER'S COMPASS FLAG IN VIEW; FIRST OFFICER'S HORIZONTAL INDICATOR (HSI) CAPTAIN'S RADIO MAGNETIC INDICATOR (RMI). REMOVED AND REPLACED NR 1 DIRECTIONAL GYRO IAW MM 34-21-1. ALSO REMOVED AND REPLACED CIRCUIT BREAKER 2 AMP IAW MM 20-50-1. PERFORMED O
- [SDR ARWA20021007](https://openairdocs.org/sdr/ARWA20021007.md): Cap · loose · Oct 28, 2002 · N441J · Doug DC863F · Engine Oil Quantity
  > NR 4 ENGINE OIL QUANTITY DROPPED TO ZERO. PRECAUTIONARY SHUT DOWN: N1 26 PERCENT, N2 35 PERCENT, OIL TEMP 90C. INSPECTED NR 4 ENGINE AND FOUND CSD SPLINE STAND PIPE CAP LOOSE, RE-TIGHTENED CAP IAW MM 79-20-6. SERVICED ENGINE OIL IAW 12-20-1 RAN ENGINE PER
- [SDR ARWA20021001](https://openairdocs.org/sdr/ARWA20021001.md): Fire Detector · malfunctioned · Oct 6, 2002 · N441J · Doug DC863F · Fire Detection
  > NR 4 ENGINE FIRE WARNING ILLUMINATED IN FLIGHT. OVERWEIGHT LANDING AT 277.0 LBS PERFORMED. REMOVED AND REPLACED NR 4 FIRE SENSOR ON BURNED SECTION OF THE ENGINE IAW MM 26-10-1. ALSO REWIRED FROM PL-1341 CONNECTOR TO PL- 1368, PL-1367 CONNECTOR AND REPLACE
- [SDR ARWA20020916](https://openairdocs.org/sdr/ARWA20020916.md): Line · leaking · Sep 30, 2002 · N441J · Doug DC863F · Engine Oil Distribution (Airframe Furnished)
  > CLIMB FL 270 NR 2 ENGINE OIL PRESSURE FLUCTUATED BELOW 35 PSI, OIL PRESS LIGHT CAME ON, OIL TEMPERATURE WENT UP. FOLLOWED ENGINE SHUT DOWN PROCEDURES. 15 PSI OIL PRESS FOR 30 MINUTES. AIRCRAFT LANDED OVERWEIGHT WITHOUT INCIDENT. INSPECTED NR 2 ENGINE FOR EVIDE
- [SDR ARWA20020904](https://openairdocs.org/sdr/ARWA20020904.md): Computer · malfunctioned · Sep 7, 2002 · N441J · Doug DC863F · Stabilizer Control System
  > DURING DESCEND PITCH TRIM COMPENSATOR FAILED IN EXTENDED POSITION, PERFORMED EMERGENCY CHECKLIST PHASE 1 AND 2 ITEMS; INITIATED A FLAP 50 LANDING AND DECLARED AN EMERGENCY IAW PHASE 2 EMERGENCY ABNORMAL CHECKLIST. REMOVED AND REPLACED PITCH COMPUTER IAW MM 27
- [SDR ARWA20020809](https://openairdocs.org/sdr/ARWA20020809.md): Oil System · lack of lube · Aug 28, 2002 · N441J · Doug DC863F · Turbine Engine Oil System
  > NR 3 ENGINE OIL QUANTITY INDICATING ZERO; WITH OIL PRESSURE FLUCTUATING AND LOW OIL PRESSURE, LIGHT ILLUMINATED. PERFORMED IN-FLIGHT ENGINE SHUTDOWN AT 1920Z. NOTE WINDMILLING OIL PRESSURE 20 PSI TURNED ON START LEVER AT 2020Z AS PER AFM. SERVICED NR 3 ENGI
- [SDR ARWA20020803](https://openairdocs.org/sdr/ARWA20020803.md): Engine · power loss · Aug 13, 2002 · N441J · Doug DC863F · Engine (Turbine/Turboprop)
  > AFTER BRAKE RELEASE, LOST PARTIAL POWER ON NR 4 ENGINE. ABORTED TAKEOFF AND RETURNED TO RAMP. REMOVED AND REPLACED NR 4 ENGINE, OPS CHECK AND LEAK CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.
- [SDR ARWA20020801](https://openairdocs.org/sdr/ARWA20020801.md): Hydraulic Line · blown · Aug 3, 2002 · N441J · Doug DC863F · Landing Gear Brake System
  > LOST ALL HYDRAULIC ON LANDING. CHECK HYDRAULIC QUANTITY AND TO BOC AT STANDARD PIPE. REPLACED BLOWN BRAKE HYDRAULIC LINE AT LT GEAR, SERVICED MAIN HYDRAULIC SYSTEM; RUN UP ENGINES AND CHECK HYDRAULIC PUMPS OFR OPS AND FOUND NORMAL. OPERATED ALL FLIGHT CONTR
- [SDR ARWA20020601](https://openairdocs.org/sdr/ARWA20020601.md): B-Nut · loose · Jun 14, 2002 · N441J · Doug DC863F · Compressor Bleed Control
  > ABORTED TAKEOFF DUE TO NR 4 ENGINE WOULD NOT GO TO MAX POWER. FOUND COMPRESSOR BLEED ACTUATOR TO CONTROL CLOSED TUBE B-NUT LOOSE; TIGHTENED B-NUT IAW MM 75-30-2; PERFORMED FLAG CHECK ENGINE RUN UP OPS CHECKED NORMAL IAW MM 75-30-3 AND 71-00 MAX TAKEOFF POWER
- [SDR ARWA20020310](https://openairdocs.org/sdr/ARWA20020310.md): Hydraulic Line · leaking · Mar 21, 2002 · N441J · Doug DC863F · Hydraulic System, Main
  > WHEN READY TO TAXI, HYDRAULIC QUANTITY GAUGE INDICATED LOSS OF FLUID, HYDRAULIC PRESSURE GAUGE INDICATED LOSS OF PRESS. ACCOMPLISHED APPROPRIATE CHECKLIST, RETURNED TO RAMP. REMOVED AND REPLACED HYDRAULIC PRESSURE LINE FROM NR 3 ENGINE HYDRAULIC PUMP, OPS CH

Next page: https://openairdocs.org/deregistered/N441J-2017-07-14/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 = 'N441J' AND deregistration_id = 'N441J-2017-07-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N441J-2017-07-14/reports

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