Douglas DC-8-73F

Service difficulty reports · 15,471

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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 = 'DC873F'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR RRXA010009Light · malfunctionedNR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT 3900 FEET, M.8 249 KIAS OIL PRESS 42, PSI IDLE 32 PSI. LIGHT REMAINED ILLUMINATED AS POWER REDUCED FROM CRUISE TO IDLE POWER. INFLIGHT SHUTDOWN PERFORMED IAW QRH. AFTER SHUTDOWN OIL PRESSURE LIGHT REMAINEFeb 11, 2001 · N961R · Doug DC873F · Engine Oil PressureSDR UPS01834948Frame · crackedINSPECTION TYPE:IN P32 DOOR UPPER AFT RADIUS FRAME CRACK. *S/D* REMOVED AND REPLACED NR 32 PIT DOOR ASSY PER DC8-MM 52-32-01, OPS CHK AND LEAK CK GOOD.Feb 9, 2001 · N874UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS01835169Floorbeam · corrodedINSPECTION TYPE:C1/3, FLOORBEAM HAS CORROSION UNDER PREVIOUS REPAIR. REPAIRED IAW REO-G07863.Feb 7, 2001 · N810UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS01834906Aileron · bindingINSPECTION TYPE:IN AILERONS BINDING CYCLED AILERONS, POWER AND FLIGHT SPOILER HYDRAULIC PUMP AND CYCLED FLAPS, AILERONS, AND SPEEDBRAKES. OPS CK OK. NO BINDING FOUND. A/C OK FOR SERVICE. IAW MM 27-10-00Feb 7, 2001 · N874UP · Doug DC873F · Aileron Control SystemSDR UPS01835165Rib · crackedINSPECTION TYPE:C1/3, RIGHT O/B FIXED L/E HAS CRACK ON L/E OF MATING SURFACE AT FASTENER ATTACH HOLES. FABBED NEW -8 ANGLE AND -11 DOUBLER IAW DAC DWG 9753297, LOCATED AND DRILLED NEW -4 RIB IAW DC-8 SRM 51-1-24. INSTALLED -8 ANGLE, -11 DOUBLER & -4 RIB IAW Feb 6, 2001 · N810UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS01834979Battery Pack · dischargedINSPECTION TYPE:IN ON PDC FOUND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01. OPS CHECKS GOOD.Feb 5, 2001 · N868UP · Doug DC873F · Emergency LightingSDR DHL2001802002Connector · shortedDURING CRUISE, NR 2 ENGINE FIRE WARNING ACTIVATED. PERFORMED ENG FIRE CHECKLIST, FIRE LEVER LIGHT REMAINED ILLUMINATED AND FIRE BELL SOUNDED INTERMITTENTLY ON A LOOP. SWITCHED TO B-LOOP AND EXPERIENCED NO FURTHER FIRE WARNINGS. B-LOOP SHORT TESTED OK. ENGIFeb 5, 2001 · N802DH · Doug DC873F · Fire DetectionSDR UPS01834855Socket · inoperativeINSPECTION TYPE:IN, LOADING CARGO SMOKE DET SYSTEM WOULD NOT TEST. BAD LIGHT SOCKET. REMOVED AND REPLACED TEST LAMP ASSY BASE, OPS CHECKS NORMAL.Feb 3, 2001 · N819UP · Doug DC873F · Detection SystemSDR UPS01835168Fitting · crackedINSPECTION TYPE:C1/3, FITTING CRACKED STA 1690 LONG 30R. REPLACED FITTING IAW DC8 SRM 51-1-20D. RETORQUED BOLT DC8 SRM 51-3-1 TABLE 3.Feb 2, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001802001Fire Loop · malfunctionedCLIMBING THROUGH 12,000, NR 2 ENG FIRE WARNING ILLUMINATED, PERFORMED CHECKLIST AND RETURNED TO CVG. OIL PRESS= 30 PSI, WINDMILL TIME= 17 MINUTES, A LOOP WOULD NOT TEST, B LOOP DID TEST OK. INSPECTED ENGINE AND COWLING FOR EVIDENCE OF FIRE, OVERTEMP, INSPECTFeb 2, 2001 · N802DH · Doug DC873F · Fire DetectionSDR RRXA003602Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO THE L/H WING BOTTOM T/E PANEL AT STA XRS 419 TO XRS 435, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLEFeb 1, 2001 · N795FT · Doug DC873F · Wing, Plate/SkinSDR UPS01835194Pressure Panel · corrodedINSPECTION TYPE:C1/3, LEFT NWW TUNNEL BOTTOM OF PRESSURE WEB AT FS -67 FROM CUSP TO I/B STIFFENER CORRODED. WEB REPAIRED IAW REO G07874.Feb 1, 2001 · N810UP · Doug DC873F · Fuselage Main, StructureSDR UPS01835167Shear Tie · corrodedINSPECTION TYPE:C1/3, SHEAR TIE AT FS 1746, BETWEEN L28R AND L26R CORRODED. REMOVED SHEAR TIE, FABBED NEW SHEAR TIE PER DAC DWG 5612148. ALODINED, PRIMED PER DC8 SRM 51-1-8. INSTALLED PER DC8 SRM 51-1-21D.Feb 1, 2001 · N810UP · Doug DC873F · Fuselage Main, StructureSDR UPS01835121Bulkhead · corrodedINSPECTION TYPE:C1/3, LEFT NWW TUNNEL, BOTTOM OF PRESSURE WEB AT FS -67 FROM CUSP TO INBD STIFFENER CORRODED. WEB REPAIRED IAW REO-G07874.Feb 1, 2001 · N810UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS01835056Support Fitting · crackedINSPECTION TYPE:C1/3, TAIL SKID SUPPORT FITTING CRACKED AT FS 1753 LONG 36. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND DAC DWG 375086 5.Feb 1, 2001 · N810UP · Doug DC873F · Fuselage, Landing Gear Attach FittingsSDR RRXA010006Engine · fodON WALK-AROUND FOUND FOD ON NR 3 ENGINE.Feb 1, 2001 · N795FT · Doug DC873F · Turbine Engine Air Inlet SectionSDR RRXA010005Tab · vibrationELEVATOR CONTROL HAS VIBRATION WHICH INCREASES WITH AIRSPEED ABOVE 250 KTS ANY DOWNWARD PRESSURE ON THE YOKE WILL CAUSE THE YOKE TO KICK BACK (AUTOPILOT OFF) (PTC ON/OFF MADE NO DIFFERENCE). REMOVED AND REPLACED ELEV LOUD FEEL CENTERING MECHANISM IAW DC-8 M/MFeb 1, 2001 · N602AL · Doug DC873F · Elevator Tab Control SystemSDR UPS01834831Fitting · crackedINSPECTION TYPE:IN, LT W/W OUTBOARD FWD BULKHEAD HAS 4 CRACKS AROUND HYD LINE BULKHEAD FTG (MARKED). *S/D* REMOVED DAMAGED MATERIAL. INSTALLED DOUBLER PER SRM 53-2-0 FIG 23.Feb 1, 2001 · N840UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS01834830Structure · looseINSPECTION TYPE:IN, KEEL BEAM STRUCTURE BETWEEN MAIN GEAR DOORS LOOSE.Feb 1, 2001 · N840UP · Doug DC873F · Fuselage Main, KeelSDR RRXA010034Mechanism · out of adjAFTER T/O ACFT DIDN'T GROUND SHIFT; COULD NOT RETRACT MLG. ADJUSTED NOSE GEAR GROUND SHIFT MECHANISM IAW DC-8 M/M CH 32-23-01, OP CHKS GOOD.Jan 31, 2001 · N795FT · Doug DC873F · Landing Gear Retraction/Extension SystemSDR UPS01835053Doubler · corrodedINSPECTION TYPE:C1/3, FS 1800 L28R LONG DOUBLER CORRODED. DRILLED NEW DOUBLER PER DC8 SRM 53-5-3. ALODINED AND PRIMED PER DC8 SRM 51-1-8. INSTALLED PER DC8 SRM 51-1-21.Jan 31, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835140Web · corrodedINSPECTION TYPE:C1/3, COCKPIT SUBFLOOR RT O/B SIDE BETWEEN FS -50.6 & FS -38.6 CORROSION ON FINGER WEB O/B AND BELOW F/E CONTROL PANEL LOWER PULLEY BRACKET ASSY. FABBED FINGER DOUBLERS -21 -27 -25 DOUBLERS FILLER AND -23 SPLICE IAW DAC DWG SRO 8530026. INSTAJan 30, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835051Gusset · crackedINSPECTION TYPE:C1/3, AFT PIT FS 1240 GUSSET AT L35R CRACKED. REMOVED DAMAGED GUSSET, FABRICATED NEW GUSSET IAW DAC DWG 9754949. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. GUSSET TO BE INSTALLED ON UPS NR 304036 TIMCO NR 21036.Jan 30, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01834819Battery Pack · dischargedINSPECTION TYPE:IN, EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM 33. OPS CK GOOD.Jan 30, 2001 · N852UP · Doug DC873F · Emergency LightingSDR UPS01835057Gusset · crackedINSPECTION TYPE:C1/3, AFT PIT FS 1050 GUSSET L31L CRACKED. REMOVED AND REPLACED GUSSET IAW DC8 SRM 51-1-20D.Jan 29, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01834804Battery Pack · dischargedINSPECTION TYPE:IN, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK ASSEMBLY. CHECKED GOOD.Jan 29, 2001 · N894UP · Doug DC873F · Emergency LightingSDR UPS01835137Frame · corrodedINSPECTION TYPE:C1/3, AFT PIT FS 1240 FRAME CORRODED BETWEEN L36 AND L34R. *S/D* MAT ID FOR REPAIR ANGLES .080 7075-0 IAW REO G07850 CORROSION ON FRAME FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED AND DRILLED REPAIR ANGLES IAW DC8 SRM 51-1-24. ALOJan 27, 2001 · N810UP · Doug DC873F · Fuselage Main, FrameSDR UPS01835138Frame · corrodedINSPECTION TYPE:C1/3, AFT PIT FS 1240 FRAME CORRODED BETWEEN L36 AND L34R. MAT ID FOR REPAIR ANGLES .080 7075-0 IAW REO-G07850 CORROSION ON FRAME FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED AND DRILLED IAW DC8 SRM 51-1-24. ALODINED AND PRIMED REPAJan 27, 2001 · N810UP · Doug DC873F · Fuselage Main, FrameSDR UPS01835133Fitting · crackedINSPECTION TYPE:C1/3, FWD ACC COMPT AT FS 56 - 70 RT CUSP AT LONG 21R IS CORRODED AND CRACKED. *S/D* REMOVED AND REPLACED FITTING P/N 3610130501N IAW DC8 SRM 51-1-21 & 51-3-0.Jan 26, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835136Skin · corrodedINSPECTION TYPE:C1/3, EXTERIOR FUSELAGE SKIN HAS LG CORROSION BULGE AT LAP SEAM STA 1875.0 S-32-R. REPLACED SKIN PER DAC DWG 5649329.Jan 26, 2001 · N810UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS01835135Bulkhead · crackedINSPECTION TYPE:C1/3, RT HORIZ STAB JACKSCREW FWD MOUNTING BULKHEAD HAS CRACKS THAT HAVE GONE THROUGH STOP DRILLS 2 EACH. REPAIRED IAW DC8 SRM 53-2-0 FIG 23.Jan 26, 2001 · N810UP · Doug DC873F · Horizontal Stabilizer StructureSDR UPS01835131Longeron · crackedINSPECTION TYPE:C1/3, FWD LWR CARGO AT FS 440 - 460 LONG 34R IS CRACKED AT SPLICE FITTING. REMOVED AND REPLACED LONGERON 34R IAW DC8 SRM 51-1-20 DC8 SRM 51-1-21.Jan 26, 2001 · N810UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS01835054Fitting · crackedINSPECTION TYPE:C1/3, AFT PTI Z-FITTING CRACK AT STA 1220 BETWEEN L30L AND L29L IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20. REMOVED AND REPLACED FITTING. ALODINED AND PRIMED SPLICE IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20.Jan 26, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835047Fitting · corrodedINSPECTION TYPE:C1/3, FWD LWR CARGO PIT AT FS 340 - 350 INSIDE X-SLIDE DOOR AFT TORQUE BOX AT LONG 34R - 35R FITTING IS CORRODED. REMOVED CORROSION OUT OF LIMITS IAW DC8 SRM 51-1-8. REMOVED AND REPLACED FITTING IAW 51-1-20D DC8 SRM.Jan 26, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835132Frame · crackedINSPECTION TYPE:C1/3, FWD BAG PIT CRACK UNDER UPPER FLANGE OF FRAME 420 AT LONG 29L. REMOVED SUPPORT, FABBED SUPPORT, ALODINED, PRIMED AND INSTALLED CHANNEL SUPPORT IAW DAC DWG 3773159 DC8 SRM 51-1-21 & 51-1-8.Jan 25, 2001 · N810UP · Doug DC873F · Fuselage Main, FrameSDR UPS01835128Fitting · corrodedINSPECTION TYPE:C1/3, FWD LWR CARGO PIT AT FS 280 AT LONG 33R Z-FITTING IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED REPAIR DOUBLER IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTAJan 25, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835052Fitting · crackedINSPECTION TYPE:C1/3, MAIN CABIN L21RT SHORT FRAME TO CUSP FITTING CRACKED AT FS 1170. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.Jan 25, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835050Splice · crackedINSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1040 - 1060 LONG 35L IS CRACKED AT SPLICE FITTING. REMOVED AND REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D.Jan 25, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01834773Control Cable · contaminatedINSPECTION TYPE: IN, AILERON POWER S/O LEVER FROZEN. CLEANED AND LUBED AILERON HYD S/O CABLES GOING THRU BULKHEAD IN LT W/W CABLES HAD BUILD UP OF ANTI CORROSION COMPOUND. SYS OPS CKS GOOD PER MM 27-10-00.Jan 25, 2001 · N868UP · Doug DC873F · Aileron Control SystemSDR UPS01835126Fitting · corrodedINSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1220 - 1230 INSIDE X-SLIDE DOOR AFT TORQUE BOX AT LONG 33R Z-FITTING IS CORRODED. REMOVED Z-FITTING FOR ACCESS IAW DC8 SRM 51-1-20D. REMOVED CORROSION LONGERON AND PRIMED IAW DC8 SRM 51-1-8. Z-FITTING. REMOVED Jan 24, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835123Web · crackedINSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1160 - 1220 AT LONG 26L WEB SKIN IS PUNCTURED AND CRACKED. REMOVED DAMAGED WEB, FABBED NEW WEB IAW DAC DWG 9753776. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED WEB IAW DC8 SRM 51-1-21.Jan 24, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835120Fitting · corrodedINSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1160 BETWEEN L33R-L34R Z-FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.Jan 24, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835118Fitting · corrodedINSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1160 BETWEEN LONG 29L-30L Z-FITTING IS CORRODED. Z-FITTING OUT OF LIMITS IAW DC8 SRM 53-2-0. RCVD FITTING P/N 375584-2- 2N PO 699381 MAT ID FOR REPAIR ANGLES BAC 1505-101167 EXTRUSION .12 5 7075-T6571 IAW DC8 SRMJan 24, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835049Fitting · crackedINSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1200 BETWEEN LONG 27L-28L Z-FITTING IS CRACKED. REMOVED AND REPLACED FITTING. ALODINED AND PRIMED SPLICE IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20.Jan 24, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835045Fitting · crackedINSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1150 - 1160 AT LONG 33R Z-FITTING IS CRACKED. REMOVED CRACKED Z-FITTING, BACK UP FITTING DOOR JAMB FITTING AND ANGLE SPLICE. LOCATED AND DRILLED, DEBURRED NEW Z-FITTING INSTALLED NEW Z-FITTING BACK UP FITTING DOOJan 24, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835044Splice Plate · corrodedINSPECTION TYPE:C1/3, AFT PIT LONGERON 36 SPLICE PLATE CORRODED AT FS 1270. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED AND DRILLED IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.Jan 24, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835038Torque Box · crackedINSPECTION TYPE:C1/3 MAIN CABIN FS 390 L12RT TORQUE BOX WEB CRACKED. FABBED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 1D, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED WITH HI-LOKS IAW DC8 SRM 51-1-20D.Jan 24, 2001 · N810UP · Doug DC873F · Fuselage Main, StructureSDR UPS01835037Splice Plate · crackedINSPECTION TYPE:C1/3 AFT PIT, LONGERON 34L SPLICE PLATE CRACKED AT FS 1270. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.Jan 24, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835036Splice Plate · crackedINSPECTION TYPE:C1/3 AFT PIT LONGERON 31L SPLICE PLATE CRACKED AT FS 1270. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOCATED AND DRILLED FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.Jan 24, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835035Splice Plate · crackedINSPECTION TYPE:C1/3 AFT PIT LONGERON 31L SPLICE PLATE CRACKED AT FS 1270. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, LOCATED AND DRILLED FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.Jan 24, 2001 · N810UP · Doug DC873F · Fuselage Miscellaneous Structure
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