# Service difficulty reports: N478CT, cancelled Aug 8, 2014

A list on [N478CT, cancelled Aug 8, 2014](https://openairdocs.org/deregistered/N478CT-2014-08-08.md).

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

- [SDR 22AA201000070](https://openairdocs.org/sdr/22AA201000070.md): Proximity Switch · inoperative · May 3, 2010 · N478CT · Doug DC1030F · Landing Gear Position and Warning
  > AFTER TAKEOFF WITH GEAR HANDLE UP ALL (4) RED UNSAFE LIGHTS REMAINED ILLUMINATED. COMPLETED APPROPIATED CHECK LIST, NO CHANGE IN THE LIGHTS INDICATION. NOTIFIED ATC, FLIGHT CONTROL AND MX CONTROL. RETURNED TO DEPARTURE. IAW TAFI 32-30-00, R & R PROXIMITY ELECT
- [SDR 22AA201000066](https://openairdocs.org/sdr/22AA201000066.md): Skin · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage Main, Plate/Skin
  > DURING "C" CHECK, LOWER FUSELAGE, ALONG LONGERON 44L, ALONG STA 1701 FUSELAGE SKIN FOUND CRACKED THROUGH. NON-ROUTINE NR 0425, CRACK AREA AT LONGERON 44L ALONG STATION 1701 FUSELAGE SKIN REPAIRED IAW SRM 53-20-00 FIGURE 6 VOLUME I REVISION 96.
- [SDR 22AA201000065](https://openairdocs.org/sdr/22AA201000065.md): Roller Tray · corroded · Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage Floor Panel
  > DURING "C" CHECK, CTR CARGO COMPARTMENT LT OTBD CARGO ROLLER TRAY FOUND CORRODED AFTER CARGO SIDE GUIDE RAIL REMOVED TO FACILITATE FOR STRUCTURE REPAIR AT STA 1697 TO STA 1781. NON-ROUTINE NR 0450, CTR CARGO COMPARTMENT LT OTBD CARGO ROLLER TRAY REPAIR CARRIE
- [SDR 22AA201000064](https://openairdocs.org/sdr/22AA201000064.md): Seat Track · corroded · Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage, Seat/Cargo Attach Fittings
  > DURING "C" CHECK, CABIN CORROSION FOUND ON INNER SURFACE OF SEAT TRACK AT STATION 1139 TO STATION 1156, X= 47.5. NON-ROUTINE NR 0314, SEAT TRACK FROM STATION 1129 TO STATION 1169, X= 47.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIGURE 1 VOLUME 1 REVISION 96.
- [SDR 22AA201000063](https://openairdocs.org/sdr/22AA201000063.md): Intercostal · corroded · Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage Miscellaneous Structure
  > DURING "C" CHECK, CTR CARGO COMPARTMENT BILGE, INTERCOASTAL FOUND CORRODED AFTER SIDE GUIDE RAIL, REMOVED TO FACILITATE FOR STRUCTURE REPAIR AT STA 1764, L42 TO L43L (REFER CNTRL NR 0425). NON-ROUTINE NR 0449, CTR CARGO COMPARTMENT BILGE, INTERCOASTAL REPAIR
- [SDR 22AA201000062](https://openairdocs.org/sdr/22AA201000062.md): Skin · corroded · Feb 24, 2010 · N478CT · Doug DC1030F · Wing, Center Box
  > DURING "C" CHECK, CABIN CORROSION FOUND ON CTR WING SECTION SURFACE AT STA 1156 TO STA 1221 X = 107.5 (RT). NON-ROUTINE 0220, CTR WING SECTION SURFACE AT STA 1156 TO STA 1221 X = 107.5 (RT) CORROSION REMOVED AND REPROTECTED IAW SRM 51-21-01 VOLUME II AT S 21 F
- [SDR 22AA201000061](https://openairdocs.org/sdr/22AA201000061.md): Rib · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/Rib
  > DURING "C" CHECK, NR 2 ENGINE RT CORE COWL AFT RIB LOWER SIDE FOUND WITH CRACK. NON-ROUTINE NR 0297, CRACK AREA AT NR 2 ENGINE RT CORE COWL AFT RIB LOWER SIDE AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000060](https://openairdocs.org/sdr/22AA201000060.md): Rib · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/Rib
  > DURING "C" CHECK, NR 2 ENGINE LT CORE COWL AFT RIB LOWER SIDE FOUND WITH CRACK. NON-ROUTINE NR 0296, CRACK AREA AT NR 2 ENGINE LT CORE COWL AFT RIB LOWER SIDE AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000059](https://openairdocs.org/sdr/22AA201000059.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 2 ENG RT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0202, CRACKED UPPER LONGERON AT NR 2 ENGINE RT CORE COWL AREA REPAIRED IAW 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FROM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000058](https://openairdocs.org/sdr/22AA201000058.md): Rib · worn · Feb 24, 2010 · N478CT · Doug DC1030 · Nacelle/Pylon, Frame/Spar/Rib
  > DURING "C" CHECK, NR 2 ENG RT CORE COWL AFT MOST RIB FOUND WITH WEAR MARK. NON-ROUTINE NR 0201, WORN AREA AT NR 2 ENGINE RT CORE COWL AFT MOST RIB AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000057](https://openairdocs.org/sdr/22AA201000057.md): Skin · worn · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Plate/Skin
  > DURING "C" CHECK, NR 2 ENG LT CORE COWL UPPER AFT RUB STRIP FOUND WORN TO COWLING SKIN. NON-ROUTINE NR 0198, WORN COWLING SKIN AREA AT NR 2 ENG LT CORE COWL UPPER AFT RUB STRIP AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED
- [SDR 22AA201000056](https://openairdocs.org/sdr/22AA201000056.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 2 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0197, CRACK AREA AT NR 2 ENGINE LT CORE COWL UPPER LONGERON AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000055](https://openairdocs.org/sdr/22AA201000055.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 2 ENGINE LT CORE COWL LOWER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0196, CRACK AREA AT NR 2 ENGINE LT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000054](https://openairdocs.org/sdr/22AA201000054.md): Rib · worn · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/Rib
  > DURING "C" CHECK, NR 2 ENGINE LT CORE COWL AFT MOST RIB FOUND WITH WEAR MARK. NON-ROUTINE NR 0195, WORN AREA AT NR 2 ENGINE LT CORE COWL AFT MOST RIB AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000053](https://openairdocs.org/sdr/22AA201000053.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 3 ENGINE RT CORE COWL LOWER LONGERON CRACKED AT APPROX AT MID AND AFT FRAME SECTION. NON-ROUTINE NR 0163, CRACK AREA AT MID AND AFT SECTION OF LOWER LONGERON AT NR 3 ENGINE RT CORE COWL AREA REPAIRED IAW EN 1018-10 WORK INSTRUCTIONS AND F
- [SDR 22AA201000052](https://openairdocs.org/sdr/22AA201000052.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 3 ENGINE LT CORE COWL LOWER LONGERON AFT SECTION FOUND CRACKED. NON-ROUTINE NR 0159, CRACK AREA AT NR 3 ENGINE LT CORE COWL LOWER LONGERON AFT SECTION REPAIRED IAW EN 1018-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2
- [SDR 22AA201000051](https://openairdocs.org/sdr/22AA201000051.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 1 ENG, RT CORE COWL LOWER LONGERON AND STRAP FOUND CRACKED. NON-ROUTINE NR 0125, CRACKED STRAP AND LOWER LONGERON AT NR 1 ENGINE RT CORE COWL AREA REPAIRED IAW EN 1016-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000050](https://openairdocs.org/sdr/22AA201000050.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 1 ENG LT CORE COWL LOWER LONGERON FOUND CRACKED. NON-ROUTINE NR 0124, CRACK AREA AT NR 1 ENGINE LT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1016-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000049](https://openairdocs.org/sdr/22AA201000049.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 1 ENGINE LT CORE COWL UPPER LONGERON FOUND CRACK. NON-ROUTINE NR 0123, CRACK AREA AT NR 1 ENG LT CORE COWL UPPER LONGERON AREA REPAIR IAW EN 1016-10 AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA200900032](https://openairdocs.org/sdr/22AA200900032.md): Control Box · failed · Dec 19, 2009 · N478CT · Doug DC1030F · Brake Anti-Skid Section
  > ANTI-SKID TESTED NORMAL ON BEFORE LANDING CHECKLIST UPON NORMAL LANDING (NO EMERGENCY DECLARED) AND AFTER EXITING RUNWAY TOWER REPORTED OBSERVING SPARKS FROM RT WING LANDING GEAR, EMERGENCY VEHICLES WERE OUT TO INSPECT, FOUND NO FIRE OR DAMAGE, CLEARED TO TAXI
- [SDR 22AA200900029](https://openairdocs.org/sdr/22AA200900029.md): Oil System · low · Oct 16, 2009 · N478CT · Doug DC1030 · Turbine Engine Oil System
  > ENG NR 3 ESN NR 455-780 IN FLIGHT SHUT DOWN DUE TO OIL / PRESS, QTY DROP & COMPRESSOR STALL AND CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 3 ENG. ON ENGINE RUN UP, OPS CHECKED NORMAL.
- [SDR 22AA20090404](https://openairdocs.org/sdr/22AA20090404.md): Slide · unwanted deploy · Apr 30, 2009 · N478CT · Doug DC1030F · Escape Slide
  > LOG PAGE NR 130754: L-1 DOOR INADVERTED OPENED (BY GROUND HANDLER) WHILE ARMED DEPLOYING SLIDE. ENTERED ON DMI NR 22611 IAW MEL 52-10-2, CATEGORY ''C''. REMOVED AND REPLACED L1 EVACUATION SLIDE/RAFT CONTAINER IN ACCORDING WITH DC-10 MAINTENANCE MANUAL 25-61-01
- [SDR 22AA20090102](https://openairdocs.org/sdr/22AA20090102.md): Manifold · cracked · Jan 6, 2009 · N478CT · Doug DC1030F · Engine Fuel Distribution
  > AT APPROXIMATELY 1740 Z. ENGINE NR 1 FAILED FUEL PRESSURE, APPROXIMATELY 50 PSI. ATTEMPTED TO START, CROSS FEED FAILED. DIVERT TO SKCL. REMOVED AND REPLACED LT, RT Y-FUEL MANIFOLD NR 1 ENGINE IN ACCORDING WITH MAINTENANCE MANUAL 73-11-01. NO LEAKS NOTED.
- [SDR ARWA20080501](https://openairdocs.org/sdr/ARWA20080501.md): Cowling · dented · May 16, 2008 · N478CT · Doug DC1030F · Engine Cowling System
  > NR 3 ENGINE NOSE COWL LIP HAS A DENT AT 5 O'CLOCK POSITION. TRANSFERRED TO CARRY-OVER ITEM NR 7584 IN ACCORDANCE WITH ARROW CARGO GMM 5-08-1 AND EO NR AS11722 FOR TRACKING OF DENT.
- [SDR ARWA20080403](https://openairdocs.org/sdr/ARWA20080403.md): Control Panel · damaged · Apr 7, 2008 · N478CT · Doug DC1030F · Auto Flight System
  > HEADING KNOB WORKING IN FAST MODE ONLY. ENTERED ON DMI NR 21598 AS PER MEL 22-1-(L) CAT "C". REMOVED AND REPLACED HDG GUIDANCE CONTROL PANEL IN ACCORDANCE WITH M/M 22-00-00. CHECK GOOD IN ACCORDANCE WITH M/M 22-00-00. CLEARED DMI NR 21598; PLACARD REMOVED.
- [SDR ARWA20080402](https://openairdocs.org/sdr/ARWA20080402.md): Adc · malfunctioned · Apr 7, 2008 · N478CT · Doug DC1030F · Air Data Computer
  > NR 1 AUTO PILOT PORPOSES IN CRUISE; TRANSFERRED TO DMI NR 21586 AS PER MEL NR 22-1-2(A) CAT "C". REMOVED AND REPLACED NR 1 AIR DATA COMPUTER IN ACCORDANCE WITH M/M 34-16-01. CHECK GOOD IN ACCORDANCE WITH MM 34-16-00 AND MM 22-10-00 CLEARED DMI NR 21586; PLAC
- [SDR ARWA20080305](https://openairdocs.org/sdr/ARWA20080305.md): Adc · intermittent · Mar 24, 2008 · N478CT · Doug DC1030F · Air Data Computer
  > CAPTAIN'S AIR DATA COMPUTER (ADC) CONTINUOUSLY FAILS IN FLIGHT. REMOVED AND REPLACED NR 1 CAPTAIN'S AIR DATA COMPUTER (CADC) IN ACCORDANCE WITH M/M 34-16-00. NO LEAKS NOTICED AT THIS TIME IN ACCORDANCE WITH M/M 34-11-00.
- [SDR ARWA20080204](https://openairdocs.org/sdr/ARWA20080204.md): Engine · stalled · Feb 23, 2008 · N478CT · Doug DC1030F · Engine (Turbine/Turboprop)
  > DURING ROTATION, NR 3 ENGINE SUFFERED COMPRESSOR STALL AND THE TOWER AND VICINITY AIRCRAFT NOTED FIRE COMING OUT OF ENGINE AFT END. REMOVED AND REPLACED NR 3 ENGINE IN ACCORDANCE WITH ARROW AIR WORK CARD 143R7101M AND DC-10 M/M 71-00-00. PERFORMED ENGINE RUN
- [SDR ARWA20080202](https://openairdocs.org/sdr/ARWA20080202.md): Connector · dirty · Feb 3, 2008 · N478CT · Doug DC1030F · Engine Starting System Wiring
  > UPON ADVANCING, THE POWER LEVERS FOR TAKEOFF, NR 3 START VALVE LIGHT ILLUMINATED, LIGHT EXTINGUISHED WHEN POWER LEVERS WERE RETARDED TO IDLE. CLEANED AND SECURED CONNECTOR AT NR 3 ENGINE STARTED VALVE, OPERATIONAL CHECK AT BLAST FENCE TAKEOFF POWER IAW MM 71-
- [SDR ARWA20071103](https://openairdocs.org/sdr/ARWA20071103.md): Wire · broken · Nov 7, 2007 · N478CT · Doug DC1030F · Landing Gear System Wiring
  > AFTER GEAR RETRACTION, NOSE GEAR RED LIGHTS REMAINED ILLUMINATED ON BOTH THE FORWARD AND F/E PANELS, CYCLED GEAR ONCE AS PER CHECK LIST, BUT NO HELP. PERFORMED ELECTRICAL TROUBLE SHOOTING, SYSTEM FOUND BROKEN WIRE AT NOSE GEAR PROXIMITY SENSOR; REPAIRED WIRIN
- [SDR ARWA20071101](https://openairdocs.org/sdr/ARWA20071101.md): Handle · stuck · Nov 1, 2007 · N478CT · Doug DC1030F · Landing Gear Selector
  > AFTER TAKEOFF GEAR HANDLE WILL NOT GO UP. ACCOMPLISHED EXPANDED CHECKLIST, NOT HELP. RETURN TO KMIA. ACCOMPLISHED FUEL DUMP PROCEDURE TO BRING A/C TO MAX LANDING WEIGHT. REMOVED AND REPLACED RUPTURED BOGIE TRIM LINE ON LT MAIN LANDING GEAR. BLEAD SYSTEM
- [SDR ARWA20071003](https://openairdocs.org/sdr/ARWA20071003.md): Engine · making metal · Oct 26, 2007 · N478CT · Doug DC1030F · Engine (Turbine/Turboprop)
  > AFTER DEPARTURE FROM SVVA, FELT VIBRATION IN COCKPIT, THEN SMOKE IN COCKPIT, NR 1 ENGINE OIL QUANTITY TO ZERO AND OIL PRESSURE BEGAN FLUCTUATING; SHUTDOWN ENGINE NR 1 AT 1758Z. TROUBLESHOOT NR 1 ENGINE PER TAFI 79-00-00; FOUND METAL CONTAMINATION ON SCAVAGE P
- [SDR ARWA20071001](https://openairdocs.org/sdr/ARWA20071001.md): Oil System · leaking · Oct 9, 2007 · N478CT · Doug DC1030F · Turbine Engine Oil System
  > NR 1 ENGINE OIL QUANTITY STEADY CAME DOWN TO 1 1/2 QUARTS OF OIL REMAINING AND PRESSURE BEGAN TO FLUCTUATE, SHUT DOWN FOR PRECAUTION AT 1321-Z. 10-19-07 FOUND NR 1 ENGINE WAS REMOVED AND REPLACED AS PER ARROW W/C 141R7101M AND DC10 MM 71-00-00. OPERAT
- [SDR ARWA20061201](https://openairdocs.org/sdr/ARWA20061201.md): Bleed Valve · malfunctioned · Dec 5, 2006 · N478CT · Doug DC1030F · Compressor Bleed Valve
  > NR 3 PNEUMATIC TEMPERATURE HIGH, LIGHT ON; TEMP AT RED LINE. FOUND NR 3 ENGINE FAN AIR VALVE STICKING CLOSED; REMOVED AND REPLACED NR 3 ENGINE FAN AIR VALVE IN ACCORDANCE WITH M/M 36-13-03; ALSO REMOVED AND REPLACED HIGH STAGE TEMPERATURE SENSOR IN ACCORDANCE
- [SDR ARWA20060802](https://openairdocs.org/sdr/ARWA20060802.md): Flap System · lack of lube · Aug 21, 2006 · N478CT · Doug DC1030F · Trailing Edge Flap Control System
  > WHEN SELECTING FLAP 15, THE FLAP DISAGREE LIGHT CAME ON AND HAD A SLIGHT ROLL TO THE RIGHT. PERFORMED ABNORMAL CHECK FOR NO FLAPS. LUBED LT & RT WING FLAP AND SLAT SYSTEM IAW MM 12-21-04. PERFORMED TEST FLAP MECHANICAL CONTROL AND TEST FLAP HYDRAULIC ACTUAT
- [SDR ARWA20060402](https://openairdocs.org/sdr/ARWA20060402.md): Compressor · dirty · Apr 28, 2006 · N478CT · Doug DC1030F · Turbine Engine Compressor Section
  > BETWEEN 50 AND 60 PERCENT N1 NR 3 ENGINE HEAVY VIBRATION. REMOVED, CLEANED, LUBRICATED AND RE-INSTALLED FIRST STAGE FAN ROTOR BLADES IN ACCORDANCE WITH DC-10 A/M/M PAGE 811, M/M 72-21-00; RAN NR 3 ENGINE AT IDLE P/P AND MAX. NO EVIDENCE OF VIBRATION AT ANY S
- [SDR ARWA20060205](https://openairdocs.org/sdr/ARWA20060205.md): Indicator · inoperative · Feb 27, 2006 · N478CT · Doug DC1030F · Airspeed/Mach Indicator
  > NO AIR SPEED ON FIRST OFFICER'S SIDE; TAKEOFF ABORTED AT 90 KTS. PERFORMED ADC BOX SELF TEST NO FLAG SHOWED TO AIR SPEED INDICATOR IN ACCORDANCE WITH DC-10 M/M 34-13-00; MAINTENANCE CONTROL ADVISED.
- [SDR ARWA20051001](https://openairdocs.org/sdr/ARWA20051001.md): Unknown · unknown · Oct 6, 2005 · N478CT · Doug DC1030F · Navigation System
  > AT TOP OF CLIMB; AIR TRAFFIC CONTROL (ATC) REPORTED AIRCRAFT OFF COURSE. COULD NOT CORRECT AND REQUESTED VECTORS BACK TO SJU. RESET POWER IN A/C, REPROGRAMMED I.N.S. 1-2-3, ALL CHECKED NORMAL. NO FAULTS FOUND IN ACCORDANCE WITH M/M 34-43-0.
- [SDR ARWA20050801](https://openairdocs.org/sdr/ARWA20050801.md): Wire Harness · burned · Aug 9, 2005 · N478CT · Doug DC1030F · Hydraulic Power System Wiring
  > NR 1 AUXILIARY PUMP POPS C/B. T/S FOUND WIRE BUNDLE IN RT WHEEL WELL BURNED AT STA. 1381 FORWARD BULKHEAD; REROUTED WIRE BUNDLE RT WHEEL WELL FORWARD BULKHEAD STATION 1381 IN ACCORDANCE WITH 20-50-02; AUXILIARY PUMP CHECKED NORMAL IN ACCORDANCE WITH M/M 29-21
- [SDR ARWA20050706](https://openairdocs.org/sdr/ARWA20050706.md): Windshield · cracked · Jul 31, 2005 · N478CT · Doug DC1030F · Flight Compartment Windows
  > AFTER LANDING CAPTAIN'S WINDSHIELD OUTSIDE CRACKED. REMOVED AND REPLACED CAPT WINDSHIELD IN ACCORDANCE WITH M/M 56-11-00; OPERATIONAL CHECK IN ACCORDANCE WITH M/M 30-41-00 AND M/M 30-42-00 FOUND NORMAL.
- [SDR ARWA20050607](https://openairdocs.org/sdr/ARWA20050607.md): Connector · unsecure · Jun 24, 2005 · N478CT · Doug DC1030F · Weather Radar System
  > WEATHER RADAR SYSTEM FAILED DURING FLIGHT (CLIMBOUT); UNABLE TO FIX; RETURNED TO KMIA. CLEANED AND RE-SECURED CONNECTORS AT ANTENNA RADOME; PERFORMED TEST RADAR SYSTEM IN ACCORDANCE WITH M/M 34-41-00; NO DUPLICATE FAIL AT THIS TIME.
- [SDR ARWA20050604](https://openairdocs.org/sdr/ARWA20050604.md): Pump · failed · Jun 10, 2005 · N478CT · Doug DC1030F · Turbine Engine Oil System
  > AFTER LANDING IN KMIA, NR 2 ENGINE OIL PRESSURE DROP DOWN TO 20 PSI; SHUTDOWN ENGINE NR 2. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER AND REMOVED AND REPLACED OIL PUMP IN ACCORDANCE WITH DC-10 M/M 9-20-04. OPERATIONAL CHECK NORMAL IN ACCORDANC
- [SDR ARWA20050506](https://openairdocs.org/sdr/ARWA20050506.md): Transmitter · malfunctioned · May 23, 2005 · N478CT · Doug DC1030F · Engine Oil Pressure
  > LOG PAGE NR 117738. DURING TAXI, ENGINE NR 1 OIL PRESSURE INDICATOR DROPPED TO (ZERO). ALL OTHER PARAMETERS NORMAL, RETURN TO BLOCK IAW AOM ALTERNATE PROCEDURES. REMOVED AND REPLACED ENGINE NR 1 OIL PRESSURE TRANSMITTER IAW MM 79-33-01. OPERATIONAL CHECK

## 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 = 'N478CT' AND deregistration_id = 'N478CT-2014-08-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N478CT-2014-08-08/reports

---
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