# Service difficulty reports: Douglas DC-8-73

A list on [Douglas DC-8-73](https://openairdocs.org/model/douglas-dc-8-73.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 17 · 821 reports

- [SDR DHLA201000018](https://openairdocs.org/sdr/DHLA201000018.md): Battery Pack · inoperative · Jun 8, 2010 · N873SJ · Doug DC873 · Emergency Lighting
  > EMERGENCY EXIT LIGHT DISARM LIGHT INOP. R & R EMERGENCY BATTERY PACK ASSY IAW MM 33-50-0. OPS CK NORMAL. ACFT WAS GROUNDED.
- [SDR DHLA201000016](https://openairdocs.org/sdr/DHLA201000016.md): Skin · damaged · May 2, 2010 · N805DH · Doug DC873 · Trailing Edge Flaps
  > ACCOMPLISHED PERMANENT MAJOR REPAIR AT WING STA XFS 392.5, IAW EVA 857-00329 REV 1 AND DWG NR D85700329-001-D REV "A" APPROVED BY 8110-3 SIGNED DERT-510080-CE DTD 5-7-10. TRAX W/O 9269, N/R 005717 FOR DETAILS. ACFT WAS GROUNDED.
- [SDR IXXA100025O](https://openairdocs.org/sdr/IXXA100025O.md): Uplock · malfunctioned · Mar 31, 2010 · N603AL · Doug DC873 · Landing Gear Position and Warning
  > DURING CLIMB OUT, DOOR NOT LATCH LIGHT ILLUMINATED, THE CREW CYCLED THE GEAR AND DOOR NOT LATCH LIGHT CAME ON AGAIN. WHEN GEAR HANDLE IS PLACED IN UPLATCH CHECK POSITION, THE GEAR HANDLE IN UP POSITION THE LIGHT WENT OUT AND STAYED OUT REMAINDER OF FLIGHT. THE
- [SDR 2010FA0000325](https://openairdocs.org/sdr/2010FA0000325.md): Frame · worn · Mar 26, 2010 · N802DH · Doug DC873 · Engine Thrust Reverser
  > (SPUY) DURING ROUTINE C-CHECK INSPECTION, NR 3 ENG LT T/R FIXED STRUCTURE FRAME WORN, STA YN 203.000 AT 7 O`CLOCK POS.
- [SDR 2010FA0000324](https://openairdocs.org/sdr/2010FA0000324.md): Frame · worn · Mar 26, 2010 · N802DH · Doug DC873 · Engine Thrust Reverser
  > (SPUY) DURING ROUTINE C-CHECK INSPECTION, NR 2 ENGINE. T/R FIXED STRUCTURE FRAME WORN, STA YN 203.000 AT 5 O`CLOCK POSITION RT.
- [SDR 2010FA0000316](https://openairdocs.org/sdr/2010FA0000316.md): Unknown · unknown · Mar 26, 2010 · N802DH · Doug DC873 · Standard Practices/Structures
  > (SPUY) DURING ROUTINE C-CHECK INSPECTION, R & R EXISTING REPAIR LOCATED FS 1180.000- 1200.000, L36 WITH A REPAIR IAW APPROVED DATA (SRM) LIST ANY AND ALL REINSPECTIONS ON THE NON-ROUTINE.
- [SDR 2010FA0000312](https://openairdocs.org/sdr/2010FA0000312.md): Skin · corroded · Mar 26, 2010 · N802DH · Doug DC873 · Vertical Stabilizer, Plate/Skin
  > (SPUY) DURING ROUTINE C-CHECK INSPECTION, VERT STAB - CORROSION BETWEEN SKIN AND BEADED DOUBLER (STA ZR 153.000 - 281.963).
- [SDR DHLA201000040](https://openairdocs.org/sdr/DHLA201000040.md): Frame · corroded · Mar 18, 2010 · N802DH · Doug DC873 · Fuselage Main, Frame
  > AFT CARGO BAY FRAME CAP SHOWS MISDRILLED HOLES & CORROSION DAMAGE BS 1180.000 L32L-32R. PERFORMED MAJOR REPAIR IAW FORM 8110-3, DATED 04-23-10, EVA D853-00325, REV 01, DATED 04-15-10. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2
- [SDR DHLA201000008](https://openairdocs.org/sdr/DHLA201000008.md): Pump · low pressure · Mar 18, 2010 · N803DH · Doug DC873 · Engine Fuel Pump
  > NR 3 ENGINE AT FLT LEVEL 330 STARTED TO VIBRATE THEN DROPPED TO 70 PERCENT N1. MOVING THRUST LEVER HAD NO EFFECT. AFTER APPROX 1 MINUTE OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESS INDICATES 3 PSI. ENG SHUTDOWN PROCEDURE ACCOMPLISHED. T/S IAW MM 71-00-00 NO
- [SDR 2010FA0000230](https://openairdocs.org/sdr/2010FA0000230.md): Cable · broken · Mar 16, 2010 · N802DH · Doug DC873 · Aileron Control System
  > RT AILERON BUS CABLE PN 3763151-501 BROKEN JUST OTBD OF THE RT INBD AILERON. FOUND LT AILERON WAS INOPERATIVE; THEREFORE PLACING HIGH TENSION ON THE BUS CABLE. WE ARE QUARANTINING THE ACTUATOR AND CABLE ASSY UNTIL FURTHER INVESTIGATION.
- [SDR DHLA201000045](https://openairdocs.org/sdr/DHLA201000045.md): Skin · corroded · Mar 10, 2010 · N802DH · Doug DC873 · Vertical Stabilizer, Plate/Skin
  > VERT STAB-CORROSION BETWEEN SKIN AND BEADED DOUBLER STA ZR 253.000-281-963. RESOLUTION PERFORMED MAJOR REPAIR IAW SRM 55-5-1, FIG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-20. FOUND OUT OF LIMITS IAW SRM 55-2-0 FIG 6. REMOVED PLATING BEADED DOUBLER IAW SRM 55
- [SDR DHLA201000044](https://openairdocs.org/sdr/DHLA201000044.md): Support Fitting · cracked · Mar 8, 2010 · N802DH · Doug DC873 · Wing, Control Surface Attach Fittings
  > LT OTBD FLAP HINGE SUPPORT FITTING CRACKED 1" STA 339.000. PERFORMED MAJOR REPAIR IAW SB 27-249 DATED 05-29-74 REV IR JULY 15-93, DWG NR 5894377. REMOVED OTBD FLAP HINGE SUPPORT FITTING IAW SRM 57-1-0, PG 1, SRM 51-1-21, SRM 51-1-20D SRM 51-3-0. CLEANED, TREA
- [SDR DHLA201000043](https://openairdocs.org/sdr/DHLA201000043.md): Pin · cracked · Mar 7, 2010 · N802DH · Doug DC873 · Cargo/Baggage Doors
  > CARGO DOOR FITTING LATCH PIN CRACKED 1". RESOLUTION: PERFORMED MAJOR REPAIR IAW SRM 52-1-0, PG 1. REMOVED FITTING ASSY CORNER IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ASSY CORNER IAW SR
- [SDR DHLA201000047](https://openairdocs.org/sdr/DHLA201000047.md): Doubler · corroded · Mar 6, 2010 · N802DH · Doug DC873 · Fuselage Main, Plate/Skin
  > FWD ASSY COMPT. JACK PAD INTERNAL DOUBLER CORRODED STA 70.000 L-36. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED JACK PAD DOUBLER IAW SRM 51-1-21. CLEANED, T
- [SDR DHLA201000038](https://openairdocs.org/sdr/DHLA201000038.md): Frame · worn · Mar 6, 2010 · N802DH · Doug DC873 · Engine Thrust Reverser
  > NR 4 ENG RT T/R FIXED STRUCTURE FRAME WORN STA YN 206.000 AT 5 O'CLOCK POS PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-16-10, EVA D878-00309 REV IR DATED 03-31-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED AREA AND FABRICATED NEW F
- [SDR DHLA201000051](https://openairdocs.org/sdr/DHLA201000051.md): Longeron Fitting · cracked · Mar 4, 2010 · N802DH · Doug DC873 · Fuselage Main, Longeron/Stringer
  > LWR FUSELAGE L-34L END FITTING CRACKED 3" STA 780.000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1. REMOVED CRACKED END FITTING IAW SRM 53-1-0 PG 1, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW END FITTING WITH SAME FASTENERS IA
- [SDR DHLA201000046](https://openairdocs.org/sdr/DHLA201000046.md): Longeron Fitting · cracked · Mar 4, 2010 · N802DH · Doug DC873 · Fuselage Main, Longeron/Stringer
  > LWR FUSELAGE L-34R END FITTING CRACKED 3" STA 780.000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED END FITTING IAW SRM 53-1-0, PG 1. SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW END FITTING WITH SOME FASTENERS
- [SDR DHLA201000042](https://openairdocs.org/sdr/DHLA201000042.md): Frame · worn · Mar 4, 2010 · N802DH · Doug DC873 · Nacelle/Pylon, Frame/Spar/Rib
  > NR3 ENG LT T/R FIXED STRUCTURE FRAME WORN STA YN 203.000 AT 7 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW FORM 8110-3, DATED 04-16-10, EVA D878-00307 REV IR DATED 03-30-10. REMOVED FASTENERS IAW SRM 51-1-221, SRM 51-3-0. CUT OUT DAMAGED AREA AND FABRICATED NEW FR
- [SDR DHLA201000041](https://openairdocs.org/sdr/DHLA201000041.md): Frame · worn · Mar 4, 2010 · N802DH · Doug DC873 · Nacelle/Pylon, Frame/Spar/Rib
  > NR3 ENG T/R FIXED STRUCTURE FRAME WORN STA YN 203.000 AT 5 O'CLOCK POS. RT PERFORMED MAJOR REPAIR IAW FORM 8110-3, DATED 04-16-10, EVA D878-00308 REV IR DATED 03-31-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED AREA AND FABRICATED NEW FRAM
- [SDR DHLA201000039](https://openairdocs.org/sdr/DHLA201000039.md): Angle · cracked · Mar 4, 2010 · N802DH · Doug DC873 · Nacelle/Pylon Miscellaneous Structure
  > NR3 ENG TO PYLON ANGLE CRACKED 10" AT 12 O'CLOCK POS STA YN 183.000-202.500. PERFORMED MAJOR REPAIR IAW FORM 8110-3 DATED 04-21-10 EVA D854-00305 REV IR DATED 03-23-10. CUT OUT DAMAGED AREA IAW SMN DWG ED-5104 REV 01 DATED 03-18-10. VISUALLY INSPECTED CUT OUT
- [SDR DHLA201000037](https://openairdocs.org/sdr/DHLA201000037.md): Structure · damaged · Mar 4, 2010 · N802DH · Doug DC873 · Engine Thrust Reverser
  > NR 2 ENG T/R TRANSLATING COWL HOLES ELONGATED STA 240.000 BETWEEN 6 AND 7 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW FORM 8110-3 DATED 04-20-10, EVA D878-00324 REV IR DATED 04-02-10. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED AREA AND FABRICATED (2EA) F
- [SDR DHLA201000050](https://openairdocs.org/sdr/DHLA201000050.md): Vane · delaminated · Mar 3, 2010 · N802DH · Doug DC873 · Trailing Edge Flaps
  > NR 4 LT FLAP VANE DELAMINATED. R & R NR 4 LT FLAP VANE IAW MM 27-51-14, PG 201-203. REFER TO NR 225817 FOR OPS CHECK.
- [SDR DHLA201000048](https://openairdocs.org/sdr/DHLA201000048.md): Skin · delaminated · Mar 3, 2010 · N802DH · Doug DC873 · Trailing Edge Flaps
  > RT WING FLAP JOINT DELAMINATED. REMOVED DELAMINATED JOINT FLAP IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED JOINT FLAP (REPAIRED CONDITION) IAW SRM 51-3-0 SRM 51-3-1 (TORQUE) (TORQUE WRENCH: SNAP ON, MODEL: QC1R200, SN 089620045
- [SDR 2010F00054](https://openairdocs.org/sdr/2010F00054.md): Cable · broken · Feb 27, 2010 · N802DH · Doug DC873 · Aileron Control System
  > RT AILERON BUS CABLE PN 3763151-501 BROKEN JUST OTBD OF THE RT INBD AILERON. FOUND LT AILERON ACTUATOR WAS INOPERATIVE THEREFORE PLACING HIGH TENSION ON THE BUS CABLE. QUARANTINED THE ACTUATOR AND CABLE ASSY UNTIL FURTHER INVESTIGATION.
- [SDR DHLA20100005](https://openairdocs.org/sdr/DHLA20100005.md): Transducer · malfunctioned · Feb 19, 2010 · N802DH · Doug DC873 · Stall Warning System
  > FLT NR 981, AT THE START OF THE TO ROLL (A/S <60 KTS) THE STICK SHAKER ACTIVATED. TROUBLESHOT FOUND LIFT TRANSDUCER BAD. R & R LIFT TRANSDUCER IAW MM 34-16-1 PERFORMED ADJUSTMENT TEST OF STALL WARN SYS IAW MMS 34-16-00 & 34-16-01, OPS NORMAL. ACFT WAS GROUND
- [SDR DHLA20100004](https://openairdocs.org/sdr/DHLA20100004.md): Stick Shaker · malfunctioned · Feb 18, 2010 · N802DH · Doug DC873 · Stall Warning System
  > STICK SHAKER ACTIVATED ON TAKEOFF ROLL, AT 60 KTS REJECTED TAKEOFF. PERFORMED STALL WARNING SYS TROUBLESHOOTING IAW MM 34-16-0. NO DEFECTS NOTED. FOUND NOSE STRUT AT 9 INCHES. SERVICED NOSE STRUT IAW MM 32-21-12. W&B NOTED TO BE ON THE AFT SIDE OF THE CG. HAD
- [SDR DHLA201000003](https://openairdocs.org/sdr/DHLA201000003.md): Lamp · inoperative · Jan 14, 2010 · N807DH · Doug DC873 · Emergency Lighting
  > DURING EMERGENCY LIGHTING CHECK, ONLY 2 OF THE 3 REQUIRED LTS ILLUMINATED ON INSTRUMENT PANEL GLARESHIELD. RELAMPED IAW MM 33-50. OPS CK OK IAW MM 33-5. FOUND DURING CHECK, ACFT WAS GROUNDED.
- [SDR IXXA10SMN019S](https://openairdocs.org/sdr/IXXA10SMN019S.md): Skin · misrepaired · Jan 11, 2010 · N603AL · Doug DC873 · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT STA FS 1480 LONGERON 33.5R RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED INTERNAL, EXTERNAL, DOUBLERS AND FILLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS.
- [SDR DHLA201000002](https://openairdocs.org/sdr/DHLA201000002.md): Strut · leaking · Jan 7, 2010 · N803DH · Doug DC873 · Nose/Tail Landing Gear Strut/Axle
  > AFTER PUSH BACK, MX REPORTED LEAK FROM NOSE GEAR. RII ITEM. ACFT IS GROUNDED- REPLACING NOSE GEAR ASSY.
- [SDR DHLA200900054](https://openairdocs.org/sdr/DHLA200900054.md): Spoiler Sys · malfunctioned · Nov 23, 2009 · N806DH · Doug DC873 · Drag Control System
  > REJECTED TAKEOFF DUE TO SPOILERS DEPLOYING ON TAKEOFF ROLL AT APPROX 60 KNOTS MAX SPEED ATTAINED 70 KNOTS 252,000 LBS TOW 22C 4880 PA NORMAL BRAKE ENERGY CHART. IAW MM PERFORMED SPOILER OPERATION CK INSPECTED RIGGING AND LINKAGE PERFORM SPOILER ELECTRICAL OPS
- [SDR DHLA2009805303](https://openairdocs.org/sdr/DHLA2009805303.md): Skin · cracked · Jul 11, 2009 · N805DH · Doug DC873 · Fuselage Main, Plate/Skin
  > 1 1/8 INCH CRACK ON FUSELAGE TAIL SECTION RT SIDE AT STA.1746.00,SR17R-S18R.
- [SDR DHLA200800033](https://openairdocs.org/sdr/DHLA200800033.md): Fire Detector · malfunctioned · Jun 5, 2009 · N802DH · Doug DC873 · Detection System
  > FLT NR 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. DEFERRED PER MEL 26-2-3 A-LOOP DMI NR 31485 PLACARD INSTALLED CAT C B-LOOP. OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 26-10-0. REMOVED AND
- [SDR DHLA200900031](https://openairdocs.org/sdr/DHLA200900031.md): Duct · blown · May 20, 2009 · N802DH · Doug DC873 · Pneumatic Distribution System
  > DURING TAKEOFF ROLL MASTER FIRE WARNING ON GLARESHIELD AND SECOND OFFICERS FIRE WARNING LIGHT AND FIREBELL, REJECTED TAKEOFF AT 100 KTS. NO LIGHT IN HANDLES, LIGHTS AND BELL EXTINGUISHED UPON STOPPING. FOUND 9TH BLEED AIR DUCT BLOWN. REPLACED DUCT ASSY PER
- [SDR DHLA200900029](https://openairdocs.org/sdr/DHLA200900029.md): Battery Pack · discharged · May 16, 2009 · N806DH · Doug DC873 · Emergency Lighting
  > EMERGENCY LIGHTS INOP. REMOVED AND REPLACED PACK ASSY EMERGENCY BATTERY, CHECKED OPS GOOD PER MM 33 50 0.
- [SDR DHLA200900026](https://openairdocs.org/sdr/DHLA200900026.md): Battery Pack · discharged · Apr 24, 2009 · N806DH · Doug DC873 · Emergency Lighting
  > DURING PREFLIGHT CHECK EMERGENCY LIGHTS DID NOT COME ON DURING BITE CHECK. RECHARGED BATTERY PACK IAW MM 33-50-21, CHECKED OPERATION OK.
- [SDR DHLA200900019](https://openairdocs.org/sdr/DHLA200900019.md): Bulb · inoperative · Apr 1, 2009 · N802DH · Doug DC873 · Emergency Lighting
  > WHEN EMERGENCY LIGHT SWITCH PLACED TO DISARM, EMERGENCY LIGHTS DISARM LIGHT FAILS TO ILLUMINATE. REMOVED AND REPLACED LIGHT BULB P/N 313. OPS CK GOOD IAW M/M 33-50-0.
- [SDR DHLA200800010A](https://openairdocs.org/sdr/DHLA200800010A.md): Pump · failed · Feb 5, 2009 · N806DH · Doug DC873 · Fuel Boost Pump
  > PASSING THROUGH 39600 FL ENG NR 4 FAILED AIRSPEED.79M DESCENDED TO 30FL AND RESTARTED WITH NORMAL OPERATION AFTER RESOLUTION. FOUND VSV OUT OF RIG. RIGGED NR 4 ENG VSV AND VBV PER MM 73-21-10. REMOVED AND REPLACED ENGINE DRIVEN FUEL BOOST PUMP (NASH) PER MM
- [SDR DHLA200800009A](https://openairdocs.org/sdr/DHLA200800009A.md): Fire Loop · malfunctioned · Feb 3, 2009 · N802DH · Doug DC873 · Fire Detection
  > WHILE TAXIING INTO BLOCKS IN ATLANTA WITH NR 1 AND 4 SHUTDOWN, FIREWARNING ACTIVATED ON NR 1, LOOP B. SWITCHING LOOP A, FIREWARNING WENT AWAY. DEFER PER MEL 26-2-3, CAT C DMI 34495, DDD 02-13-09. PLACARD INSTALLED
- [SDR DHLA200800007A](https://openairdocs.org/sdr/DHLA200800007A.md): Switch · stuck · Jan 27, 2009 · N873SJ · Doug DC873 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT ILLUMINATED IN FLIGHT. FOUND MASTER WARNING RESET SWITCH STICKING, LUBED SWITCH AND RELAMPED IAW MM 33-15-0, OPS CHECK IS GOOD, P/N 313.
- [SDR DHLA200800006A](https://openairdocs.org/sdr/DHLA200800006A.md): Fire Warning · illuminated · Jan 26, 2009 · N802DH · Doug DC873 · Fire Detection
  > ON TAXI IN NR 1 ENGINE FIRE LIGHT ILLUMINATED. ACCOMPLISHED ENGINE FIRE CHECK LIST. TRANSFERRED TO DMI LOG NR 34462, REF MEL 26-2-3 CAT C. PLACARDS INSTALLED.
- [SDR DHLA200800005A](https://openairdocs.org/sdr/DHLA200800005A.md): Wire Harness · failed · Jan 25, 2009 · N807DH · Doug DC873 · Fire Protection System Wiring
  > NR 4 ENGINE FIRE WARNING ILLUMINATED COMPLETED CHECKLIST. IFSD ENGINE NR 4, FOUND "A" LOOP CORE LT SIDE PYLON HARNESS PIN BROKEN. REPLACED CONNECTOR PER S/W/P 20-71-02. ALSO REPLACED HOT SECTION WIRE HARNESS PER POWERPLANT BUILDUP MAN 71-00-01-114A. REPLAC
- [SDR DHLA200800004A](https://openairdocs.org/sdr/DHLA200800004A.md): Element · failed · Jan 23, 2009 · N807DH · Doug DC873 · Fire Detection
  > WHILE IN A LOOP ENGINE FIRE LIGHT ON NR 4 ENGINE ILLUMINATED MOMENTARILY THEN WENT OUT SWITCHED TO B LOOP LIGHT STAYED OUT FOR THE DURATION OF THE FLT. REPLACED PYLON SENSING ELEMENT AND INBD CORE SENSING ELEMENT OPS CK IS GOOD IAW M/M 26-10-1, P/N OF PYLON S
- [SDR DHLA200900002](https://openairdocs.org/sdr/DHLA200900002.md): Socket · loose · Jan 15, 2009 · N873SJ · Doug DC873 · Emergency Lighting
  > EMERGENCY LIGHT DISARMED LIGHT INOP. RESECURED LOOSE LIGHT SOCKET OPS CK GOD PER MM 33-10-0.
- [SDR DHLA200800134](https://openairdocs.org/sdr/DHLA200800134.md): Fire Warning · illuminated · Dec 10, 2008 · N802DH · Doug DC873 · Fire Detection
  > FIRE INDICATION NR 1 ENG DURING APPROACH. FIRED BOTTLES INBOARD. NR 1 ENG FIRE LOOP B DEFERRED PER MEL 26-2-3 CT C DMI 34247. INSTALL PLACARD INST SPEC PROC C/W. MX NOTIFIED.
- [SDR DHLA200800128](https://openairdocs.org/sdr/DHLA200800128.md): Fan · burned · Nov 18, 2008 · N806DH · Doug DC873 · Air Distribution Fan
  > SMOKE IN CABIN AFT OF CABIN AFTER LANDING. REMOVED AND REPLACED CABIN AIR RECIRC FAN INSTALLED CABIN FAN TRANSFERED TO DMI LOG PER MEL21-16, PLACARD INSTALLED. A/C WAS GROUNDED.
- [SDR DHLA200800123](https://openairdocs.org/sdr/DHLA200800123.md): Connector · loose · Nov 6, 2008 · N802DH · Doug DC873 · Fire Protection System Wiring
  > DURING CRUISE FLT 370 ENG FIRE NR 4 IND/ FOLLOWED EMERGENCY PROCEDURES PER AOM / LANDED AT ATL / A&B LOOPS WERE CHK'D B LOOP STEADY IND / A LOOP INTERMITTENT. DEFERRED PER MEL 26-2-3 DMI 34020 ASSIGNED PLACARD INSTALLED REF: LG PG A02579 ITEM 1. NR 4 ENG FI
- [SDR DHLA200800113](https://openairdocs.org/sdr/DHLA200800113.md): Pump · failed · Oct 15, 2008 · N873SJ · Doug DC873 · Fuel Boost Pump
  > AT 45 MINUTES FROM SJU AT FL370 NR 1 ENGINE QUIT DURING DESCENT. AT FL250 DID AN INFLIGHT ENGINE RESTART. RESOLUTION DESCRIPTION: COMPLIED WITH T/S AS PER CFMI M/M 71-00-00 FAULT 51. NO DEFECTS NOTED. PERFORMED MAX ASSURANCE RUN IAW ASTAR JRH CHAP 11. AL
- [SDR DHLA200800112](https://openairdocs.org/sdr/DHLA200800112.md): Fire Warning · malfunctioned · Oct 9, 2008 · N807DH · Doug DC873 · Fire Detection
  > PRIOR TO DESCENT NR 3 FIRE WARNING HANDLE ILLUMINATED AND MASTER FIRE WARNING BELL SOUNDED INTERMITTENTLY THEN EXTINGUISHED FIRE LOOP TESTED OK. RESOLUTION DESCRIPTION: XFERRED TO DMI 33829 PER MEL 26-2-3 PLACARD NR 3 ENG "B" LOOP INOP. CAT C & MXC NOTIFIED
- [SDR DHLA200800105](https://openairdocs.org/sdr/DHLA200800105.md): Battery Pack · inoperative · Sep 30, 2008 · N803DH · Doug DC873 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT TEST ON PREFLT, ACFT GROUNDED. R&R BATTERY PACK ASSY, OPS CHECKED GOOD IAW 33-50-1.
- [SDR DHLA200800077](https://openairdocs.org/sdr/DHLA200800077.md): Engine · failed · Jun 27, 2008 · N803DH · Doug DC873 · Engine (Turbine/Turboprop)
  > AT TOP OF CLIMB NR 3 ENGINE FAILED FOLLOWED APPLICABLE PROCEDURES RELIGHT ATTEMPT UNSUCCESSFUL WIND MILLING OIL PRESSURE 2 PSI WIND MILLING TIME 2.55. PERFORMED T/S IAW DC8-70 M/M 71-00, ADJUSTED MEL SPECIFIC GRAVITY IAW MM 73-20-1. ADJUSTED PMC DROP IAW MM

Next page: https://openairdocs.org/model/douglas-dc-8-73/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 = 'DC873'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/douglas-dc-8-73/reports

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