# Service difficulty reports: Douglas DC-8-63F

A list on [Douglas DC-8-63F](https://openairdocs.org/model/douglas-dc-8-63f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 38 · 1,883 reports

- [SDR U2RA464AML5501](https://openairdocs.org/sdr/U2RA464AML5501.md): Bulb · burned out · Mar 31, 2011 · N865F · Doug DC863F · Emergency Lighting
  > EMERGENCY EXIT DISARM LIGHT INOP.
- [SDR U2RA464M85463](https://openairdocs.org/sdr/U2RA464M85463.md): Access Panel · cracked · Mar 4, 2011 · N865F · Doug DC863F · Nacelle/Pylon, Plate/Skin
  > NR 4 PYLON UPPER L/E CAP FAIRING HINGE IS CRACKED 2 PLACES ON OTBD SIDE.
- [SDR U2RA464OSC18858](https://openairdocs.org/sdr/U2RA464OSC18858.md): Skin · cracked · Aug 26, 2010 · N865F · Doug DC863F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT FS 8.000 AIR CONDITIONING CONDENSER EXHAUST DOOR CUTOUT UPPER AFT CORNER CRACK LENGTH APPROX 2".
- [SDR U2RA464OSC18837](https://openairdocs.org/sdr/U2RA464OSC18837.md): Longeron · cracked · Aug 25, 2010 · N865F · Doug DC863F · Fuselage Main, Longeron/Stringer
  > LONGERON 35RIS CRACKED FROM STA 1343-1348 (5").
- [SDR U2RA464OSC18449](https://openairdocs.org/sdr/U2RA464OSC18449.md): Attach Fitting · cracked · Aug 20, 2010 · N865F · Doug DC863F · Fuselage Main, Attach Fittings
  > FUSELAGE FRAME TO CUSP FITTING CRACKED APPROX 5" AT STA 717.75.
- [SDR U2RA464OSC18836](https://openairdocs.org/sdr/U2RA464OSC18836.md): Longeron · cracked · Aug 19, 2010 · N865F · Doug DC863F · Fuselage Main, Longeron/Stringer
  > LONGERON 34R IS CRACKED FROM STA 1343-1349.
- [SDR U2RA865FLP3376](https://openairdocs.org/sdr/U2RA865FLP3376.md): Skin · cracked · Sep 19, 2009 · N865F · Doug DC863F · Fuselage Main, Plate/Skin
  > FOUND 2 EACH CRACKS IN FUSELAGE SKIN APPROX AT STA 1760 LT SIDE MID POINT VERTICALLY. ONE CRACK APPROX 2 INCHES LONG BETWEEN L13L AND L14L AND ONE CRACK APPROX 1 INCH LONG BETWEEN L14L AND L15L. CRACKS WILL BE REPAIRED IAW DWG 53-09405-1.
- [SDR U2RA865FLP3371](https://openairdocs.org/sdr/U2RA865FLP3371.md): Skin · damaged · Sep 13, 2009 · N865F · Doug DC863F · Fuselage Main, Plate/Skin
  > FUSELAGE DAMAGED BY FORKLIFT BETWEEN LONGERON 26 AND 27 AT STA 370. REPAIRED IAW DWG 53-09382-1.
- [SDR 22AA20090505](https://openairdocs.org/sdr/22AA20090505.md): Spar · cracked · May 9, 2009 · N784AL · Doug DC863F · Wing Spar
  > ON PRE FLIGHT FOUND FUEL LEAK BY LEFT WING ROOT FORWARD OF WHEEL WELL. UPON FURTHER INVESTIGATION THE LEFT REAR SPAR WAS FOUND CRACKED.
- [SDR 22AA20081203](https://openairdocs.org/sdr/22AA20081203.md): Bleed Valve · stuck · Dec 31, 2008 · N784AL · Doug DC863F · Compressor Bleed Valve
  > LOG PAGE NR 128276. NR 1 ENGINE WOULD NOT ACCELERATE TO TAKE-OFF POWER; REJECTED TAKE OFF AT 80 KTS. - RETURNED TO GATE. FOUND NR 1 COMPRESSOR BLEED VALVE STUCK IN OPEN POSITION. R&R NR 1 ENGINE COMP. BLEED CONTROL VALVE IAW DC-8 M/M 75-30-3; OPS CHECK NOR
- [SDR 22AA20081102](https://openairdocs.org/sdr/22AA20081102.md): Control Cable · broken · Dec 1, 2008 · N784AL · Doug DC863F · Stabilizer Control System
  > ON DESCENT LONG TRIM SUITCASE HANDLE, RIGHT SUITCASE HANDLE JAMMED. FOUND BROKEN CABLE RUNNING NR 49B. REMOVED AND REPLACED 1/16 CONTROL CABLE RUNNING NR 49B IN ACCORDING WITH DC-8 MAINTENANCE MANUAL 27-40-01. RIGGING AND OPERATION CHECKED, FOUND NORMAL IN
- [SDR 22AA20081002](https://openairdocs.org/sdr/22AA20081002.md): Cylinder · malfunctioned · Oct 15, 2008 · N784AL · Doug DC863F · Trailing Edge Flap Actuator
  > ON APPROACH INTO MROC THE FLAPS WOULD NOT EXTEND BEHOND 23 DEGREES. FOUND OUTBOARD FLAP LOCKOUT CYLINDER RETRACTED; SERVICE FLAP LOCKOUT CYLINDERS IAW MM 27-51-10. OPERATIONAL CHECK FOUND NORMAL IAW MM 27-50-00.
- [SDR ARWA20080802](https://openairdocs.org/sdr/ARWA20080802.md): Unknown · sparks · Aug 14, 2008 · N784AL · Doug DC863F · Landing Gear System
  > AIR TURNBACK REPORTED SPARKS COMING FROM RT MAIN GEAR. DECLARED EMERGENCY AND RETURNED TO MIA. (S)
- [SDR ARWA20080707](https://openairdocs.org/sdr/ARWA20080707.md): Fuel Control · malfunctioned · Jul 31, 2008 · N661AV · Doug DC863F · Fuel Control/Turbine Engines
  > ENG NR 1 FAILED TO ACCELERATE BEYOND GROUND IDLE. REMOVED AND REPLACED FUEL CONTROL UNIT AT NR 1 ENG IAW DC8 MM 73-20-1. PERFORMED ENG RUN UP IAW DC8 MM 77-00. FOUND NORMAL. (S)
- [SDR ARWA20080705](https://openairdocs.org/sdr/ARWA20080705.md): Gyro · malfunctioned · Jul 24, 2008 · N661AV · Doug DC863F · Directional Gyro and Indicating System
  > NR 2 COMPASS PROCESSES 10 DEGREES. REMOVED AND REPLACED NR 2 DIRECTIONAL GYRO IN ACCORDANCE WITH DC8 M/M 34-21-1; OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH DC8 M/M 34-21-0. (A)
- [SDR 865FLP2936](https://openairdocs.org/sdr/865FLP2936.md): Compressor · stalled · Mar 28, 2008 · N865F · Doug DC863F · Turbine Engine Compressor Section
  > NR 1 ENGINE COMPRESSOR STALLED AT 1000 FT AND WAS SECURED. ENGINE WAS RELIT PRIOR TO LANDING. ENGINE POWER ASSURANCE RUN ON GROUND DETECTED NO DISCREPANCIES.
- [SDR ARWA20080304](https://openairdocs.org/sdr/ARWA20080304.md): Compass · inoperative · Mar 23, 2008 · N661AV · Doug DC863F · Directional Gyro and Indicating System
  > FIRST OFFICER'S COMPASS INOPERATIVE. REMOVED AND REPLACED DIRECTIONAL GYRO NR 2 (DG-2) IN ACCORDANCE WITH M/M 34-21-1 AND RADIO DIRECTION INDICATOR NR 2 (RDI NR 2) IN ACCORDANCE WITH 31-00. COMPASS GROUND TEST NORMAL IN ACCORDANCE WITH M/M 34-21-0; 34-54-0 A
- [SDR ARWA20080201](https://openairdocs.org/sdr/ARWA20080201.md): Limit Switch · malfunctioned · Feb 3, 2008 · N784AL · Doug DC863F · Trailing Flap Position Indicating System
  > DURING TAKEOFF ROLL, TAKEOFF WARNING HORN CAME ON. REMOVED AND REPLACED SI-278 FLAP UPLIMIT SWITCH IN ACCORDANCE WITH M/N 27-52-1 AND SI-177 AND 176 SPOILERS SWITCH IN ACCORDANCE WITH 27-63-1, SYSTEM GROUND TEST NORMAL.
- [SDR IXXA08SMN020S](https://openairdocs.org/sdr/IXXA08SMN020S.md): Skin · misrepaired · Jan 19, 2008 · N41CX · Doug DC863F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD FLAP LOWER SURFACE HAS IMPROPER REPAIR AT STATION XW 59.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL.
- [SDR ARWA20071205](https://openairdocs.org/sdr/ARWA20071205.md): Snap Ring · loose · Dec 18, 2007 · N784AL · Doug DC863F · Cabin Pressure Control System
  > DURING CLIMB-OUT, UNABLE TO CONTROL THE CABIN PRESSURIZATION, NEITHER WITH AUTO OR MANUAL (WITH 4 T.C. ON). FOUND NR 2 TC DISFUSER SNAP RING LOOSE. REINSTALLED SNAP RING AT NR 2 TC IN ACCORDANCE WITH DC-8 M/M 21-10-6. PRESSURIZATION CHECK FOUND NORMAL IN AC
- [SDR N921RM81664](https://openairdocs.org/sdr/N921RM81664.md): Skin · cracked · Oct 26, 2007 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > "D" PIT DOOR DAMAGED FORWARD UPPER SKIN AT CORNER. APPROX.375 INCH CRACK RADIATED FROM EDGE OF FUSELAGE SKIN IN DOOR RADIUS AND TERMINATED AT FIRST FASTENER.
- [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 ABXA070265](https://openairdocs.org/sdr/ABXA070265.md): Hinge Pin · sheared · Aug 2, 2007 · N812AX · Doug DC863F · Cargo/Baggage Doors
  > DURING MAINTENANCE ON WO 600267980, UPPER FORWARD CARGO DOOR FORWARD HINGE PIN WAS SHEARED. REMOVED AND REPLACED FORWARD HINGE PIN IAW DC8 AMM 20-10-0.
- [SDR ARWA20070703](https://openairdocs.org/sdr/ARWA20070703.md): Bleed Valve · malfunctioned · Jul 10, 2007 · N661AV · Doug DC863F · Compressor Bleed Valve
  > ABORTED TAKE-OFF AT 118 KTS, UNABLE TO MAINTAIN TAKEOFF POWER WITHOUT EXCEEDING NR 3 ENGINE EGT LIMIT. REMOVED NR 3 ENGINE SURGE VALVE IN ACCORDANCE WITH M/M 75-30-3. INSTALLED NEW COMPRESSOR BLEED VALVE AND CONTROL IN ACCORDANCE WITH M/M 75-30-3. OPERATION
- [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 ARWA20070607](https://openairdocs.org/sdr/ARWA20070607.md): Control Unit · unknown · Jun 17, 2007 · N661AV · Doug DC863F · Brake Anti-Skid Section
  > L/F I/B ANTI-SKID LIGHT ILLUMINATED. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT IN ACCORDANCE WITH M/M 32-43-1; CHECK GOOD IN ACCORDANCE WITH M/M 32-43-0.
- [SDR ARWA20070611](https://openairdocs.org/sdr/ARWA20070611.md): Access Door · cracked · Jun 15, 2007 · N661AV · Doug DC863F · Wing, Plate/Skin
  > DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; RT WING UPPER SURFACE MAIN FUEL TANK ACC DOOR NR 505C WT OUT WITH 02 CRACKS. REPAIR ACC DOOR NR 505C OF RT WING UPPER SURFACE MAIN FUEL TANK IN ACCORDANCE WITH DRAWING NR AIPSAC - N661AV-02/07, DATED 01-12
- [SDR ARWA20070610](https://openairdocs.org/sdr/ARWA20070610.md): Access Door · cracked · Jun 15, 2007 · N661AV · Doug DC863F · Wing, Plate/Skin
  > DURING "C" CHECK INSPECTIONS, THE FOLLOWING WAS FOUND; RT WING UPPER SURFACE MAIN FUEL TANK ACCESS DOOR NR 505E CUT OUT WITH CRACK. REPAIRED RT WING UPPER SURFACE MAIN FUEL TANK ACC DOOR NR 505E CUT OUT IN ACCORDANCE WITH DRAWING NR AIPSAC-N661AV-02/07 RD, SH
- [SDR ARWA20070609](https://openairdocs.org/sdr/ARWA20070609.md): Skin · corroded · Jun 15, 2007 · N661AV · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR STATION 260 L-21L SKIN WITH CORROSION. REPAIRED FUSELAGE EXTERIOR SKIN ATW FS 200 AND FS 350 AND BETWEEN L-18L AND L-24L IN ACCORDANCE WITH DRAWING NR AIPSAC-N661AV-01/06, REVISION 0, SHE
- [SDR ARWA20070608](https://openairdocs.org/sdr/ARWA20070608.md): Skin · dented · Jun 15, 2007 · N661AV · Doug DC863F · Horizontal Stabilizer, Plate/Skin
  > DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND LT HORIZONTAL STABILIZER XH 285.00 L/E LOWER SURFACE WITH DENT. REPAIRED L/E PLATING OF LT HORIZONTAL STABILIZER BETWEEN XFS 263 AND XH 285 IN ACCORDANCE WITH AIPSAC DRAWING NR AIPSAC-N661AVE-03/07, SHEET 1
- [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 ABXA070184](https://openairdocs.org/sdr/ABXA070184.md): Battery · discharged · Jun 12, 2007 · N816AX · Doug DC863F · Emergency Lighting
  > EMERGENCY EXIT LIGHT BATTERY PACK DEAD UNABLE TO CHANGE. REMOVED AND REPLACED EMERGENCY LIGHT PACK ASSEMBLY IAW DC8 AMM 33-50-01.
- [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 N865F1480010](https://openairdocs.org/sdr/N865F1480010.md): Panel · corroded · Apr 30, 2007 · N865F · Doug DC863F · Fuselage Floor Panel
  > COCKPIT SUBFLOOR PRESSURE PANEL EXISTING REPAIR WITH CORROSION STA -17.00 LBL 50".
- [SDR N865F1479009](https://openairdocs.org/sdr/N865F1479009.md): Stringer · corroded · Apr 30, 2007 · N865F · Doug DC863F · Fuselage Main, Longeron/Stringer
  > COCKPIT SUB FLOOR STRINGER DOUBLER WITH CORROSION AT STA -117.00 CPCP 455R 0552.
- [SDR ABXA070149](https://openairdocs.org/sdr/ABXA070149.md): Transmitter · defective · Apr 30, 2007 · N826AX · Doug DC863F · Engine Oil Pressure
  > DURING CRUISE NR 2 ENGINE OIL PRESSURE WENT TO OFF SCALE LOW MOMENTARILY AND RECOVERED. FIFTEEN MINUTES LATER, AGAIN OFF SCALE LOW AND STAYED. SECURED NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE PRESSURE TRANSMITTER IAW DC8 MM 70-32-01-2. RAN ENGINE, NO
- [SDR ABXA070107](https://openairdocs.org/sdr/ABXA070107.md): Transmitter · defective · Apr 17, 2007 · N826AX · Doug DC863F · Engine Oil Pressure
  > AT TOP OF CLIMB, NR 1 ENGINE OIL PRESSURE STARTED DROPPING OFF INTO CAUTIONARY RANGE. RAN ABNORMAL CHECK LIST, REDUCED POWER TO IDLE. OIL PRESSURE DROPPED BELOW RED LINE, SECURED ENGINE AND RETURNED FOR LANDING. REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER
- [SDR N865F1134011](https://openairdocs.org/sdr/N865F1134011.md): Unknown · corroded · Mar 26, 2007 · N865F · Doug DC863F · Fuselage Structure (General)
  > FOUND COCKPIT SUBFLOOR WITH CORROSION AT STA.-67.00 L21L CPCP455L 0552.
- [SDR N865R1125006](https://openairdocs.org/sdr/N865R1125006.md): Unknown · corroded · Mar 26, 2007 · N865F · Doug DC863F · Fuselage Miscellaneous Structure
  > COCKPIT SUBFLOOR INNER AREA WITH CORROSION AT STA 67 L-21R CPCP 455R 0552.
- [SDR N865R1124005](https://openairdocs.org/sdr/N865R1124005.md): Angle · corroded · Mar 26, 2007 · N865F · Doug DC863F · Fuselage Miscellaneous Structure
  > COCKPIT SUBFLOOR ANGLE WITH CORROSION AT STA 32.000 L-21R CPCP455R 0552.
- [SDR N865R1076007](https://openairdocs.org/sdr/N865R1076007.md): Access Door · corroded · Mar 23, 2007 · N865F · Doug DC863F · Wing, Plate/Skin
  > LT WING XFS 836 OUTBD L/E INNER LOWER SECTION ACCESS DOOR NR 517B JAMB WITH CORROSION CPCP 107L 0552.
- [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 N865F753008](https://openairdocs.org/sdr/N865F753008.md): Skin · corroded · Mar 19, 2007 · N865F · Doug DC863F · Rudder, Plate/Skin
  > RUDDER ZR 168.656 LT EXTERNAL SKIN WITH CORROSION CPCP 6820 0551.
- [SDR N865R623002](https://openairdocs.org/sdr/N865R623002.md): Bulkhead · cracked · Mar 15, 2007 · N865F · Doug DC863F · Fuselage Main, Bulkhead
  > AFT FLAT PRESSURE BULKHEAD WEB STA 1766 L11L CRACK CPCP 5730 0551.
- [SDR ABXA070072](https://openairdocs.org/sdr/ABXA070072.md): Wire · damaged · Mar 15, 2007 · N816AX · Doug DC863F · Light System Wiring
  > DURING SERVICE CHECK FOUND ELECTRICAL ODOR COMING FROM OVERHEAD LIGHT. FOUND ONE FLUORESCENT LIGHT RECEPTACLE CORRODED AT TERMINAL ENDS AND SHORTING. CLEANED RECEPTACLE AND REPLACED BOTH TERMINAL ENDS ON WIRES COMING TO RECEPTACLE. REPLACED LAMP AND OPS CHE
- [SDR N865F624003](https://openairdocs.org/sdr/N865F624003.md): Bulkhead · cracked · Mar 13, 2007 · N865F · Doug DC863F · Fuselage Main, Bulkhead
  > AFT FLAT PRESSURE BULKHEAD WEB STA 1766 L-11R-12R CRACK CPCP 5730 0551.
- [SDR ABXA070069](https://openairdocs.org/sdr/ABXA070069.md): Wire · chafed · Mar 13, 2007 · N816AX · Doug DC863F · Navigation System Wiring
  > ACRID ODOR OF ELECTRICAL SMOKE BY ALL 3 CREW MEMBERS, SOURCE NOT IDENTIFIED. ODOR COMES AND GOES. FOUND LOAD CALCULATOR WIRES CHAFING ON PANEL. ROUTED PANEL AREA OUT AND REPAIRED WIRES IAW DC8 MM CHAPTER 20. NO OTHER DEFECTS NOTED AT THIS TIME.

Next page: https://openairdocs.org/model/douglas-dc-8-63f/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 aircraft_model_key = 'DC863F'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/douglas-dc-8-63f/reports

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