# Service difficulty reports: N865F

A list on [N865F](https://openairdocs.org/aircraft/N865F.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 · 93 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 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 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 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 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 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 U2RA09900](https://openairdocs.org/sdr/U2RA09900.md): Downlock Switch · corroded · Nov 17, 2006 · N865F · Doug DC863F · Landing Gear Position and Warning
  > ON LANDING AT KYIP, RT MAIN GEAR DOWN AND SAFE GREEN LIGHT WOULD NOT ILLUMINATE. FLEW BY TOWER TO SEE IF LANDING GEAR WAS DOWN. EMERGENCY VEHICLES STANDING BYE ON LANDING. AFTER ENGINE SHUTDOWN LIGHT CAME ON. COMPLIED WITH MURRAY ABNORMAL CHECK LIST. REMO
- [SDR U2RA0990](https://openairdocs.org/sdr/U2RA0990.md): Downlock Switch · corroded · Nov 17, 2006 · N865F · Doug DC863F · Landing Gear Position and Warning
  > ON LANDING AT KYIP-RT MAIN GEAR DOWN AND SAFE GREEN LIGHT WOULD NOT ILLUMINATE. FLEW BY TOWER TO SEE IF LANDING GEAR WAS DOWN. EMERGENCY VEHICLES STANDING BYE ON LANDING. AFTER ENGINE SHUTDOWN LIGHT CAME ON, COMPLIED WITH MURRAY ABNORMAL CHECK LIST. REMOVE
- [SDR U2RA1013](https://openairdocs.org/sdr/U2RA1013.md): Frame · corroded · Feb 10, 2006 · N865F · Doug DC863F · Fuselage Main, Frame
  > DURING COCKPIT AREA CORROSION INSPECTION PER AD92-22-07 (CPCP 5), LEVEL 2 CORROSION WAS FOUND ON RT FRAME AT FS -67, L23R AND ADJACENT AREA. AFFECTED AREA IS IN PROCESS OF BEING REPAIRED.
- [SDR U2RA1013865](https://openairdocs.org/sdr/U2RA1013865.md): Frame · corroded · Feb 10, 2006 · N865F · Doug DC863F · Fuselage Main, Frame
  > DURING COCKPIT AREA CORROSION INSPECTION PER AD92-22-07 (CPCP 5), LEVEL 2 CORROSION WAS FOUND ON RT FRAME AT FS -67, L23R AND ADJACENT AREA. AFFECTED AREA IS IN PROCESS OF BEING REPAIRED.
- [SDR U2RA0809](https://openairdocs.org/sdr/U2RA0809.md): Transformer · broken · Nov 4, 2005 · N865F · Doug DC863F · Flight Compartment Lighting
  > PILOTS OVERHEAD PANEL LIGHTS INOP, GLOW FUSE ON FOLLOWED BY SMOKE.
- [SDR 0657](https://openairdocs.org/sdr/0657.md): Connector · dirty · Mar 5, 2005 · N865F · Doug DC863F · Landing Gear System Wiring
  > LEFT MAIN GEAR DOWN AND LOCK SAFE LIGHTS DID NOT COME ON. PERFORMED ABNORMAL CHECKLIST. AFTER LANDING LIGHT CAME ON.
- [SDR 0656](https://openairdocs.org/sdr/0656.md): Uplock · out of rig · Mar 5, 2005 · N865F · Doug DC863F · Landing Gear Position and Warning
  > AFTER MAIN LANDING GEAR RETRACTION GEAR HANDLE IN THE UP POSITION, DOOR NOT LATCH LIGHT REMAINS ON. POSITION GEAR HANDLE IN THE UP-LATCH CHECK POSITION, DOOR NOT LATCHED LIGHT, GEAR NOT LATCHED LIGHT AND ALTERNATE RIGHT HAND DOOR NOT LATCHED LIGHT REMAINS ON,
- [SDR 0378](https://openairdocs.org/sdr/0378.md): Frame · cracked · Feb 17, 2004 · N865F · Doug DC863F · Fuselage Main, Frame
  > DURING CPCP TASK NR 5570-0551 FORWARD LOWER CARGO COMPARTMENT FORWARD FRAME FITTING CRACKED AT FS299 BETWEEN LONGERON 32R AND 33R.
- [SDR 0377](https://openairdocs.org/sdr/0377.md): Doubler · cracked · Feb 17, 2004 · N865F · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING CPCP TASK 5570-0551 FORWARD LOWER CARGO COMPARTMENT INTERIOR SKIN DOUBLER CORRODED AND CRACKED AT FS270 LONGERON 31L AND IDENTIFIED AS LEVEL 2 CORROSION.
- [SDR 0375](https://openairdocs.org/sdr/0375.md): Frame · corroded · Feb 17, 2004 · N865F · Doug DC863F · Fuselage Main, Frame
  > DURING CPCP TASK 5570-0551 FORWARD LOWER CARGO COMPARTMENT CIRCUMFERENTIAL FRAME LOWER LEG CORRODED AT FS 80 BETWEEN LONGERON 36R AND 35R AND IDENTIFIED AS LEVEL 2 CORROSION.
- [SDR 0370](https://openairdocs.org/sdr/0370.md): Fitting · cracked · Feb 17, 2004 · N865F · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING CPCP TASK 5590-0551 AFT CARGO FS 1160 LONGERON 35R AND 34R FITTING CRACKED AND IDENTIFIED AS LEVEL 2 CORROSION.
- [SDR 0369](https://openairdocs.org/sdr/0369.md): Clip · cracked · Feb 17, 2004 · N865F · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING CPCP TASK 5690-0551 AFT CARGO FS 1210 LONGERON 33R CORRODED AND CRACKED 2 EACH FITTING CLIPS AND INDENTIFED AS LEVEL 2 CORROSION
- [SDR 0355](https://openairdocs.org/sdr/0355.md): Skin · corroded · Feb 17, 2004 · N865F · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING CPCP TASK 5600-0551 FOUND AFT ACCESSORY COMPARTMENT FS 1640 BETWEEN LONGERON 32R AND 33R. FASTENERS PULLING THROUGH FUSELAGE SKIN AND IDENTIFIED AS LEVEL 2 CORROSION.
- [SDR 0354](https://openairdocs.org/sdr/0354.md): Duct · delaminated · Feb 17, 2004 · N865F · Doug DC863F · Engine Cowling System
  > NR 2 ENGINE LT ENGINE COWL TRANSITION DUCT DELAMINATED ON INBOARD SIDE.
- [SDR 0479](https://openairdocs.org/sdr/0479.md): Fitting · cracked · Feb 17, 2004 · N865F · Doug DC863F · Wing Miscellaneous Structure
  > DURING FUEL TANK MAINTENANCE DETECTED LT WING NR 2 MAIN FUEL TANK CRACKED STRINGER END FITTING AT STA.XRS 78,S61.
- [SDR 0390](https://openairdocs.org/sdr/0390.md): Hinge Fitting · cracked · Feb 17, 2004 · N865F · Doug DC863F · Ailerons
  > VISUALLY DETECTED LT OB AILERON CENTER HINGE FITTING CRACKED.
- [SDR 0380](https://openairdocs.org/sdr/0380.md): Skin · cracked · Feb 17, 2004 · N865F · Doug DC863F · Nacelle/Pylon, Plate/Skin
  > VISUALLY DETECTED CRACK IN PREVIOUS DOUBLER LEFT WING LEADING EDGE AT NR 2 ENGINE PYLON CUTOUT.
- [SDR 0324](https://openairdocs.org/sdr/0324.md): Fitting · corroded · Feb 17, 2004 · N865F · Doug DC863F · Fuselage Main, Structure
  > EXTERNAL FUSELAGE SKIN HAS A BULGE AT FS 324 LONGERON 33R FOUND DURING C-CHECK. FOUND FORWARD LOWER BELLY CARGO (A-PIT) DOOR STRUCTURE FITTING CORRODED.
- [SDR 020104](https://openairdocs.org/sdr/020104.md): Fitting · corroded · Feb 17, 2004 · N865F · Doug DC863F · Fuselage Main, Structure
  > EXTERNAL FUSELAGE SKIN HAS A BULGE AT FS 315 LONGERON 33R FOUND DURING C-CHECK. FOUND FORWARD LOWER BELLY CARGO (A PIT) DOOR STRUCTURE FITTING CORRODED-TASK CARD #0323.
- [SDR 0471](https://openairdocs.org/sdr/0471.md): Longeron · corroded · Feb 14, 2004 · N865F · Doug DC863F · Fuselage Main, Longeron/Stringer
  > DURING CPCP TASK NR 5570-0551 FORWARD LOWER CARGO COMPARTMENT CORROSION ON LONGERON 30L AT FS 270 AND IDENTIFIED AS LEVEL 2 CORROSION.
- [SDR KO0R0323](https://openairdocs.org/sdr/KO0R0323.md): Fitting · corroded · Jan 15, 2004 · N865F · Doug DC863 · Fuselage Main, Attach Fittings
  > EXTERNAL FUSELAGE SKIN HAS A BULGE AT FS315, LONGERON NR 33R. FOUND DOOR STRUCTURE FITTING CORRODED (FS 315, LONGERON 33R). REMOVED AND REPLACED FITTING IAW DC8, SRM 53-2-0, FIG 2D. CORROSION REMOVED IAW DC SRM 51-1-8.
- [SDR U2RB010103](https://openairdocs.org/sdr/U2RB010103.md): Skin · cracked · Jan 3, 2003 · N865F · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING COMPLIANCE WITH A/D 2000-20-08 AND REMOVAL OF TEMPORARY EXTERNAL REPAIR AT LEFT FRONT PAX ENTRANCE DOOR UPPER FORWARD CORNER, VISUALLY DETECTED ONE ADDITIONAL FUSELAGE SKIN CRACK TERMINATING AT RIVET FASTENER 3 FASTENERS UP FROM PREVIOUS CRACK REPAIRED
- [SDR U2RB100102](https://openairdocs.org/sdr/U2RB100102.md): Skin · cracked · Oct 28, 2002 · N865F · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING B-4 CHECK, FOUND RIVET POPPED AT FUSELAGE STATION -12, LEFT LONGERON NR 30. INVESTGATION REVEALED STRESS CRACK IN FUSELAGE SKIN AT RIVET HEAD. REMOVED DAMAGE SKIN, CLEANED AND TREATED IAW DC8 SRM 51-1-8 AND REPAIRED IAW DC8 SRM 53-2-0 /51-1-21 AND REF
- [SDR U2RB070302](https://openairdocs.org/sdr/U2RB070302.md): Fitting · corroded · Jul 31, 2002 · N865F · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING COMPLIANCE OF BOEING S/B 53-61 R4 DURING DISASSEMBLY FOR REPLACEMENT OF CRACKED RT MLG SUPPORT FITTING DURING DISASSEMBLY FOUND RT LONGERON NR 24 FUSELAGE FRAME FITTING CORRODED.
- [SDR U2RB070202](https://openairdocs.org/sdr/U2RB070202.md): Support Fitting · cracked · Jul 30, 2002 · N865F · Doug DC863F · Fuselage, Landing Gear Attach Fittings
  > DURING COMPLIANCE WITH BOEING S/B DC8-53-61 R4, VISUALLY DETECTED LEFT HAND WHEEL WELL TRAPEZOID FITTING CRACKED AND EXTENDING FROM BOLT HOLE APPROXIMATELY 2.25 INCHES.
- [SDR U2RB070102](https://openairdocs.org/sdr/U2RB070102.md): Support Fitting · cracked · Jul 30, 2002 · N865F · Doug DC863F · Fuselage, Landing Gear Attach Fittings
  > DURING COMPLIANCE BOEING S/B DC8-53-061R4 VISUALLY DETECTED RT MLG SUPPORT FITTING CRACKED IN TWO PLACES. UPPER AREA.875 INCH AND AFT UPPER AREA CRACK EXTENDING UP AND OUT INTO SUPPORT FITTING FLANGE.
- [SDR U2RB040202](https://openairdocs.org/sdr/U2RB040202.md): Floorbeam · corroded · Apr 2, 2002 · N865F · Doug DC863F · Fuselage Main, Floor Beam
  > DURING CPCP 18 MONTH INSPECTION, AFT ACCESSORY COMPARTMENT INTERIOR. DETECTED LEVEL 2 CORROSION OF UPPER TEE OF FORWARD FLANGE OF FLOORBEAM 11.5 INCHES INBOARD OF RIGHT FUSELAGE CUSP LINE 1.75 INCHES LONG.
- [SDR U2RB050101](https://openairdocs.org/sdr/U2RB050101.md): Fitting · cracked · May 14, 2001 · N865F · Doug DC863F · Engine Thrust Reverser
  > ON POST FLIGHT INSPECTION WITH NR 4 ENGINE THRUST REVERSER (T/R) TRANSLATING RING EXTENDED FOUND LOWER AFT T/R TRACK SUPPORT FITTING MOUNTED ON BOTTOM CENTER LINE OF ENGINE EXHAUST NOZZLE OUTBOARD FLANGE CRACKED THROUGHOUT BOLT HOLE.
- [SDR U2RB030101](https://openairdocs.org/sdr/U2RB030101.md): Spar Cap · cracked · Mar 7, 2001 · N865F · Doug DC863F · Wing Spar
  > DURING COMPLIANCE OF MCDONNELL DOUGLAS DC-8 S/B 57-90 R5 (NPRM 99-NM-60-AD) DETECTED CRACK ATLOWER FORWARD SPAR AT ATTACH FASTENERS STA XFS 524. CRACK BEYOND S/B 57-90 R5 REPAIR LIMITS.
- [SDR RRXA98177](https://openairdocs.org/sdr/RRXA98177.md): Cowling · corroded · Apr 14, 1998 · N865F · Doug DC863F · Engine Cowling System
  > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO NR 1 ENGINE RIGHT SIDE FAN COWLING, ZEE CLOSE-OUT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-0448
- [SDR RRXA98166](https://openairdocs.org/sdr/RRXA98166.md): Cowling · corrosion · Apr 14, 1998 · N865F · Doug DC863F · Engine Cowling System
  > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO NR 4 ENGINE, RIGHT SIDE AFT FAN COWLING, ZEE CLOSE-OUT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO
- [SDR RRXA98153](https://openairdocs.org/sdr/RRXA98153.md): Cowl · worn · Apr 14, 1998 · N865F · Doug DC863F · Engine Cowling System
  > DURING A MAINTENANCE VISIT, FOUND NR 1 ENGINE FAN COWLING, ZEE CLOSE-OUT WORN. FABRICATED AND INSTALLED NEW ZEE CLOSE-OUT, (P/N 575716-503), IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04413.

Next page: https://openairdocs.org/aircraft/N865F/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 = 'N865F' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N865F/reports

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