Douglas DC-8-73

Service difficulty reports · 821

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 = 'DC873'
  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 UPS01836979Fitting · crackedINSPECTION TYPE: C1, STA. 280 ABOVE LONG. 27R FLOORBEAM SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 9754024,AND SRM. 51-1-21, 51-3-0Sep 21, 2001 · N867UP · Doug DC873 · Fuselage Miscellaneous StructureSDR UPS01836977Longeron · crackedINSPECTION TYPE: C1, STA. 965 LONG. 24R IS CRACKED ON BOTTOM SIDE. REPAIRED LONGERON I.A.W. SRM. 53-2-2 FIG. 5Sep 21, 2001 · N867UP · Doug DC873 · Fuselage Main, StructureSDR UPS01836984Frame · corrodedINSPECTION TYPE: C1, STA. 1160 FRAME IS CORRODED BEYOND LIMITS BETWEEN LONG. 4L TO 5L. REPAIRED FRAME I.A.W. DC8-53A-011Sep 20, 2001 · N867UP · Doug DC873 · Fuselage Main, FrameSDR UPS01836981Fitting · crackedINSPECTION TYPE: C1, STA. 902 LONG. 18L INTERCOSTAL TO FRAME AFT FITTING IS CRACKED REMOVED,FABRICATED,AND REPLACED FITTING I.A.W. DWG. 4779496,AND SRM. 51-1-20DSep 20, 2001 · N867UP · Doug DC873 · Fuselage Miscellaneous StructureSDR UPS01836980Fitting · crackedINSPECTION TYPE: C1, STA. 902 LONG. 18L INTERCOSTAL TO FRAME FITTING IS CRACKED REMOVED,FABRICATED,AND REPLACED FITTING I.A.W. DWG. 3779498,AND SRM. 51-1-20DSep 20, 2001 · N867UP · Doug DC873 · Fuselage Miscellaneous StructureSDR UPS01836978Fitting · crackedINSPECTION TYPE: C1, STA. 859 LONG. 18L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING I.A.W. DWG. 4750420,AND SRM 51-1-20DSep 20, 2001 · N867UP · Doug DC873 · Fuselage Miscellaneous StructureSDR UPS01836982Stiffener · corrodedINSPECTION TYPE: C1, STA. 1215-1220 DIAGONAL STIFFENER IS CORRODED AT LONG. 33R. REMOVED AND REPLACED STIFFENER I.A.W. DWG. 375794,AND SRM. 51-1-20DSep 19, 2001 · N867UP · Doug DC873 · Fuselage Miscellaneous StructureSDR UPS01836974Skin · corrodedINSPECTION TYPE: SP, RIGHT WING UPPER SKIN BLENDOUT IS BEYOND LIMITS AT ACCESS PANEL 505B AT APPROX. STA. XRS489 AT STRINGER 7. REPAIRED SKIN I.A.W. SRM. 57-2-1 FIG. 36Sep 17, 2001 · N814UP · Doug DC873 · Wing, Plate/SkinSDR DHL2001802011Smoke Detector · will not test1) NR 6 SMOKE DETECTOR LIGHT WILL NOT COME ON FOR TEST. NR 7 SMOKE DETECTOR LIGHT WILL NOT GO OUT AFTER TEST. 2) RELAMPED NR 6 SMOKE DETECTOR PER SMM 26-15-00.OPS CHECK OK. RELAMPED NR 7 SMOKE DETECTOR PER SMM 26-15-00.OPS CHECK OK. STATUS: CLOSEDSep 17, 2001 · N802DH · Doug DC873 · Smoke DetectionSDR UPS01836954Stiffener · corrodedINSPECTION TYPE: C2, LONGERON STIFFENER EXFOLIATED. REMOVED AND REPLACED STIFFENER IAW RFTS 801UP-19-21236Sep 16, 2001 · N801UP · Doug DC873 · Fuselage Miscellaneous StructureSDR UPS01836943Pan · corrodedINSPECTION TYPE: C2, AFT CROSS SLIDE DOOR UNDER AFT LIFT HANDLE DOOR FRAME. CUT & REMOVED SECTION OF DOOR PAN IAW REO G08404 FAB NEW SECTION IAW RE O G08404 ALODINE & PRIME IAW DC8 SRM 51-1-8 INSTALLED IAW REO G08404 FAB REPAIR ANGLE IAW REO G08404 ALODISep 16, 2001 · N801UP · Doug DC873 · Cargo/Baggage DoorsSDR UPS01836942Pressure Panel · crackedINSPECTION TYPE: C2, COCKPIT SUBFLOOR PRESSURE WEB IS CRACKED AT STA. -67 AT RBL. 60 REPAIRED WEB I.A.W. SRO 8520026Sep 14, 2001 · N852UP · Doug DC873 · Fuselage Floor PanelSDR UPS01836951Floorbeam · corrodedINSPECTION TYPE: C2, FLC FS 70 FLOORBEAM AT RBL 32 CORRODED FABBED REPAIR ANGLES IAW TIMCO SRM STD 5310-001 ALODINED & PRIMED IA W DC8 SRM 51-1-8. INSTALLED REPAIR ANGLES IAW 51-1-20 INSTALLED 2 EA FLOOR PANELS IAW DC8 SRM 51-3-0Sep 10, 2001 · N801UP · Doug DC873 · Fuselage Main, Floor BeamSDR UPS01836950Splice · crackedINSPECTION TYPE: C2, REMOVE INTERCOSTAL AT LEFT WING STA 340 TO ACCESS FWD DRIVE LINK BOLT. REMOVED INTERCOSTAL & WEB IAW DC8 SRM 51-1-21. MAT ID FOR ANGLE DOUBLER DMS 1592 TITANIUM .040 PO 300420 IAW REO G08396 & SHIMS 7075-T6 .040 PO 362742 & 7075-T6 .06Sep 10, 2001 · N801UP · Doug DC873 · Wing Miscellaneous StructureSDR UPS01836941Frame · corrodedINSPECTION TYPE:C2 STA. 8 FRAME IS CORRODED BEYOND LIMITS BETWEEN LONG. 24R-29R REMOVED,FABRICATED AND REPLACED CHORD I.A.W. 8110-3 APROVED DH SK 852-708Sep 10, 2001 · N852UP · Doug DC873 · Fuselage Main, FrameSDR UPS01836949Floorbeam · corrodedINSPECTION TYPE: C2, FLOORBEAM CORRODED IN FWD UPPER FLANGE APPROX 10 INCHES FROM LT CUSP AT FS 1080. CUT OUT DAMAGED FLOORBEAM SECTION. FABRICATED NEW SECTION & REPAIR A NGLES. REMOVED TAIL DEICE AIR LINE. INSTALLED NEW SECTION & REPAIR S PLICES IAW DC8 Sep 9, 2001 · N801UP · Doug DC873 · Fuselage Main, Floor BeamSDR UPS01836948Floorbeam · corrodedINSPECTION TYPE: C2, FLOORBEAM CORRODED IN FWD UPPER FLANGE APPROX 10 INCHES FROM LT CUSP AT FS 1080. CUT OUT DAMAGED FLOORBEAM SECTION. FABRICATED NEW SECTION & REPAIR A NGLES. REMOVED TAIL DEICE AIR LINE. INSTALLED NEW SECTION & REPAIR S PLICES IAW DC8 Sep 9, 2001 · N801UP · Doug DC873 · Fuselage Main, Floor BeamSDR UPS01836944Attach Angle · corrodedINSPECTION TYPE:C2 MAIN CABIN FLOOR PNL ATTACH ANGLE HAS CORROSION AROUND NP'S AND MISDRILLED HOLES AT STA 25 AND BW LBL 14-LBL23 IN FRONT L RADIO RACK BLEND AREA TO RMV CORROSION FOUND OUT OF LIMITS IAW 53-2-1 RMVD FLR SUPPORT IAW DC8 SRM 51-1-20D FABBED Sep 8, 2001 · N801UP · Doug DC873 · Fuselage Miscellaneous StructureSDR UPS01836947Frame · crackedINSPECTION TYPE: C2, FRAME IS CRACKED REPAIR IAW DC8 SRM 53-2-0 FIG 2Sep 7, 2001 · N801UP · Doug DC873 · Fuselage Main, FrameSDR DHL2001803011Smoke Detector · inoperativeDURING PREFLIGHT NR 3 SMOKE DETECTOR WOULD NOT TEST.Aug 29, 2001 · N803DH · Doug DC873 · Smoke DetectionSDR DHL2001802010Smoke Barrier · tornVAPOR BARRIER HAS 2 TEARS. INTERIM REPAIR PERFORMED ON VAPOR BARRIER PER DHL ENGINEERING MEMO MEM-01-0002 BARRIER DEFFERED IAW MEL GMM 3.5.Aug 8, 2001 · N802DH · Doug DC873 · Emergency EquipmentSDR DHL2001803010Proximity Sensor · dirtyDURING LANDING GEAR UPLATCH CHECK DOORS NOT LATCHED LIGHT AND RIGHT GEAR DOOR UNSAFE LIGHT REMAINED ILLUMINATED ABNORMAL PROCEDURE PERFORMED. CLEANED GREASE OFF RIGHT GEAR DOOR PROX SENSOR. GROUND OPS CHECK DOOR, OK PER 32-31-04.Aug 2, 2001 · N803DH · Doug DC873 · Landing Gear Position and WarningSDR DHL2001803009Wheel · defectiveDURING TAXI OPTNS ACFT DRIFTS RIGHT REQUIRING CONSTANT LEFT NOSE WHEEL STEERING INPUTS TO MAINTAIN CENTERLINE. REMOVED & REPLACED BOTH LEFT & RIGHT NOSE WHEEL ASSEMBLIES AS PER MM 32-40. OK FOR SERVICE.Jul 28, 2001 · N803DH · Doug DC873 · Wheel/Ski/FloatSDR DHL2001803008Smoke · detectedSMOKE IN COCKPIT DURING CLIMB SHORTLY AFTER TURNING ON ENGINE ANTI-ICE. PERFORMED APPROPRIATE CHECK LIST AND SMOKE CLEARED.PERFORMED ENGINE RUN PER JRH CHAP 11 COULD NOT DUPLICATE SMOKE IN COCKPIT PERFORMED PNEUMATIC SYS CHECK REF JRH 12.2 LT MANIFOLD IS HIGH Jul 25, 2001 · N803DH · Doug DC873 · Air Distribution SystemSDR DHL2001803567Fitting · crackedC-CHECK-R/H MLG- 3/4 CRACK IN JOINT TRAPEZOIDAL FITTING WITH LONGERON 24 AT STA. 902.000CORRECTIVE ACTION-REPAIRED CRACK ON TRAPEZOIDAL FITTING STA. 902.000 L-24R IAW FAX SEV- LIM-01-00073 H EO. SEMON# 200176 PER S/B 53-61 REV. 3 ACCOMPLISHMENT INSTRUCTIONS, CJul 10, 2001 · N803DH · Doug DC873 · Fuselage Main, Longeron/StringerSDR DHL2001803566Control Cable · frayedC CHECK - FIRST OFFICER'S LT. BRAKE NR 85 RUN CABLE FRAYED. REMOVED AN REPLACED FRAYED RUN CABLE NR 85 AND PERFORMED ADJUSTMENT AN TEST OF WHEEL BRAKE SYSTEM IAW. MM 32-41-0 PAGE 201-205.Jul 10, 2001 · N803DH · Doug DC873 · Landing Gear Brake SystemSDR DHL2001803559Door · wornR/H NLG MID DOOR OF NLG WITH WEAR ON LOWER SKIN.REMOVED R/H NLG MID DOOR PER SRM 51-3-0 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW MID DOOR PER SRM 51-3-0.OPS CHKD PER M/M32-30-0 PG 1.Jul 10, 2001 · N803DH · Doug DC873 · Landing Gear DoorsSDR DHL2001803564Skin · damagedLT WING EXTERNAL FLAP LOWER SKIN SHOWS 2 INCH DENT AND 4 INCH DEEP SCRATCH STA XW.159 (XF 213 TO 169).Jul 8, 2001 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2001803561Skin · crackedLT WING L/E LOWER SKIN SURFACE SHOWS 1.500 INCH CRACK AT STA XFS 597.500.Jul 8, 2001 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2001803560Skin · crackedRT WING LOWER SKIN SURFACE SHOWS 1 INCH CRACK AT STA XFS 300.Jul 8, 2001 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2001803558Skin · dentedRT ELEVATOR UPPER SKIN SHOWS DENTS XF 271.000 TO XH 283.000.Jul 8, 2001 · N803DH · Doug DC873 · Elevator, Plate/SkinSDR DHL2001803557Skin · dentedLEFT WING EXTERNAL FLAP LOWER SKIN SHOWS .75 INCH (2 EA) DENTS AT STA XW 230.00.Jul 8, 2001 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2001803554Skin · damagedLT ELEVATOR LOWER PART SHOWS SKIN DEFLECTED AT XE 94.500 TO XE 112.906.Jul 8, 2001 · N803DH · Doug DC873 · Elevator, Plate/SkinSDR DHL2001803553Skin · damagedLT ELEVATOR LOWER PART SHOWS SKIN DEFLECTED BETWEEN STA XE 288.375 TO XE 297.2347.Jul 8, 2001 · N803DH · Doug DC873 · Elevator, Plate/SkinSDR DHL2001803552Skin · dentedRT ELEVATOR LOWER SKIN SHOWS 2 INCH DENT BETWEEN STA XE 256.250 AND XE 260.937.Jul 8, 2001 · N803DH · Doug DC873 · Elevator, Plate/SkinSDR DHL2001803563Skin · dentedRT ELEVATOR UPPER PART SHOWS SKIN WITH 1/2 IN 3 EA DENTS FROM XE 55.062 TO XE 39.531.Jul 6, 2001 · N803DH · Doug DC873 · Elevator, Plate/SkinSDR DHL2001803562Doubler · wornAFT CARGO COMPT AFT DOOR JAMB PATCH WORN AT STA 1440.00 L-29 TO L-32R.Jul 6, 2001 · N803DH · Doug DC873 · Fuselage Main, StructureSDR DHL2001803556Skin · damagedRT ELEVATOR LOWER PART SHOWS SKIN DEFLECTED FROM XE.65.156 TO XE.117.599.Jul 6, 2001 · N803DH · Doug DC873 · Elevator, Plate/SkinSDR DHL2001803551Skin · damagedRT ELEVATOR LOWER SKIN DEFLECTED STA XE 132-246.Jul 6, 2001 · N803DH · Doug DC873 · Elevator, Plate/SkinSDR DHL2001803550Skin · crackedRT WING L/E LOWER SKIN SHOWS .5 INCH CRACK AT XW 485.000.Jul 6, 2001 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2001803539Door Frame · crackedLT MAIN LANDING GEAR DOOR,1 IN CRACK IN DOOR FRAME ANGLE AT STA 960.00.Jul 6, 2001 · N803DH · Doug DC873 · Landing Gear DoorsSDR DHL2001803538Torque Tube · crackedRT WING O/B SLOT TORQUE TUBE CRANK (LT SIDE) SHOWS CRACK. REMOVED AND REPLACED RIGHT O/B SLOT TORQUE TUBE CRANK PER OHM 27-37-4 PAGE 1-2, SRM 51-3-1 PG 1 ON NON ROUTINE 1385 FOR OPS CHK.Jul 5, 2001 · N803DH · Doug DC873 · Trailing Edge Flap Control SystemSDR DHL2001803543Fitting · crackedRT EXTERNAL FLAP HINGE SUPPORT INNER FITTING AT XF 409 SHOWS 0500 IN LENGTH CRACK ON LOWER SURFACE.Jul 4, 2001 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2001803542Fitting · crackedRT EXTERNAL FLAP HINGE SUPPORT INNER FITTING AT XF 409 SHOWS 0500 IN LENGTH CRACK ON LOWER SURFACE.Jul 4, 2001 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2001803541Angle · crackedNOSE LANDING GEAR WHEEL WELL .5 IN CRACK ON FRAME REINFORCING ANGLE STA 119, L-33R.Jul 4, 2001 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2001803540Angle · crackedNOSE LANDING GEAR WHEEL WELL .25 IN CRACK ON FRAME REINFORCING ANGLE, STA 119.L-33L.Jul 4, 2001 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2001803544FittingMAIN CARGO JOINT FITTING WITH INTERCOSTAL L-22.RH SHOWS 5 IN BREAK AT STA FS 834.000.REMOVED BROKEN FITTING PER SRM 51-1-20D.PG 21.CLEANED TREATED AND PRIMED PER SRM 51-18B.INSTALLED NEW FITTING PER SRM51-1-20D PG 9Jul 3, 2001 · N803DH · Doug DC873 · Fuselage Structure (General)SDR DHL2001803565Rib · crackedC-CHECK - RT I/B FLAP JOINT INNER RIB SHOWS 4 EA CRACKS 1 INCH AT XW 129.000. PERFORMED STOP HOLE, FABRICATED REINFORCING ANGLE, AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2.Jul 2, 2001 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2001803501Seat Track · brokenFWD CARGO COMPARTMENT-R/H TRACK LUGS BROKEN AND WORN AND POINTS OF CORROSION BETWEEN STA 160.00 AND 260.00.REMOVED DAMAGED TRACK(STA 160-260)PER SRM 51-3-0 PAGE 1. CLEANED TREATED AND PRIMED PER SRM 51-1-8 B.INSTALLED NEW TRACK (P/N S2955978)PER SRM 51-3-0 PAGJul 2, 2001 · N803DH · Doug DC873 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2001803500Seat Track · brokenDURING C CHK FOUND FWD CARGO COMPARTMENT R/H TRACK LUGS BROKEN WORN AND POINTS OF CORROSION BETWEEN STA 70.000 AND STA 160.000.REMOVED DAMAGED TRACK(STA70-160)PER SRM 51-1-88.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-88.INSTALLED NEW TRACK P/N S 2955978 PERJul 2, 2001 · N803DH · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
Back to Douglas DC-8-73