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 RRXA11171Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO A-PIT DOOR RAMP I/B SUPPORT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG#97May 28, 2001 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11170Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT DOOR RAMP SKIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21D AND DWG#97540May 28, 2001 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11169Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FLOOR SUPPORT ANGLE AT STA.1280 AND L31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK606-749.May 27, 2001 · N606AL · Doug DC873F · Fuselage Main, StructureSDR RRXA11168Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FLOOR SUPPORT ANGLE AT STA.1300 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK 606-749.May 27, 2001 · N606AL · Doug DC873F · Fuselage Main, StructureSDR RRXA11167Skin · scratchedDURING A MAINTENANCE VISIT FOUND SCRATCH DAMAGE TO LT WING O/B FLAP LOWER SKIN AT STA. XRS410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0, 51-1-26, 51-1-21A, 57-May 27, 2001 · N606AL · Doug DC873F · Trailing Edge FlapsSDR RRXA11278Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TOR/H WW STIFFNER AT STA.933 AND BL0-BL7, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 5May 26, 2001 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA11166Doubler · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO AFT ACCY COMP. CUSP MEMBRANCE AT STA.158-1600 AND RBL48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0 FIGMay 26, 2001 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11165Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H INBOARD FLAP O/B END Z ANGLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 57-7-May 26, 2001 · N606AL · Doug DC873F · Trailing Edge FlapsSDR DHL2001805012Adi · defectiveAUTOPILOT WILL NOT TRACK GLIDESLOPE. 1 DOT OUTSIDE 5 MI, 1.5 DOT INSIDE 5 MI. REMOVED AND REPLACED HORIZON FLT INDICATOR. OPERATIONAL CHECK FOUND GOOD. OK FOR SERVICE (F/O SIDE).May 26, 2001 · N805DH · Doug DC873F · Integrated Flight SystemSDR DHL2001805011Controller · malfunctionedAUTOPILOT IN HDG MODE, RIGHT TURN 35 DEG BANK, LEFT TURN 25 DEG BANK. REMOVED AND REPLACED AUTOPILOT CONTROLLER. PERFORMED OPERATIONAL CHECK IAW MM 22-20-0. OK FOR SERVICE.May 26, 2001 · N805DH · Doug DC873F · Flight ControllerSDR DHL2001807022Autopilot Sys · malfunctioned1) STEADY WARNING HORN DURING CLIMBOUT WITH GEAR UP AND FLAPS RETRACTED. AIR TURNBACKED TO ORD. 2) TROUBLESHOOTING FOUND ITEM RELATED TO AUTOPILOT DMI 5739. SEE ITEM 2D FOR AUTOPILOT CORRECTIVE ACTION. AT THIS TIME AUTOPILOT WARNING HORN OPERATES NORMMay 25, 2001 · N807DH · Doug DC873F · Autopilot SystemSDR RRXA11175Clip · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO L/H WING #4 SPOILER O/B HINGE FITTING CLIP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-May 25, 2001 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA11164Aileron · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H INBOARD AILERON T/E WEDGE BETWEEN TRIM AND CONTROL TAB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IMay 24, 2001 · N606AL · Doug DC873F · Aileron Control SystemSDR UPS01835992Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK.May 24, 2001 · N852UP · Doug DC873F · Emergency LightingSDR DHL2001801006Adi · defectiveF/O ADI JUMPING UP & DOWN FROM 2 DEG TO 7 DEG AT A TIME. ALL PHASES OF FLIGHT. REMOVED AND REPLACED F/O ADI INDICATOR. OPS CHECK GOOD PER 34-29-0.May 22, 2001 · N801DH · Doug DC873F · Integrated Flight SystemSDR DHL2001804009Autopilot Sys · malfunctionedAUTOPILOT MADE AN UNCOMMANDED DESCENT FROM 4000 FT LEVEL FLIGHT. COULD NOT DUPLICATE ON GROUND. AUTOPILOT CHECKS GOOD IAW DC-8 MM 22-10-0. BITE CHECK ALSO GOOD.May 19, 2001 · N804DH · Doug DC873F · Autopilot SystemSDR DHL2001805010Actuator · failedCONTROL WHEELS TRIM SWITCHES INOP. REMOVED AND REPLACED LT ROTARY ACT PER DC-8 MM 27-41-10.May 18, 2001 · N805DH · Doug DC873F · Stabilizer ActuatorSDR DHL2001805009Actuator · failedCONTROL WHEELS TRIM SWITCHES INOPERATIVE. REMOVED AND REPLACED LEFT LONG TRIM ACTUATOR. OP CHECKS GOOD PER M/M.May 18, 2001 · N805DH · Doug DC873F · Stabilizer ActuatorSDR UPS01835894Pressure Panel · crackedINSPECTION TYPE:N/A LEFT MLG W/W WEB PANEL CRACKED. *S/D* REPAIRED PER SRM 51-1-5.May 16, 2001 · N804UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS01835999Skin · corrodedINSPECTION TYPE:C1,3 RIGHT WING L/E LOWER SKIN IS CORRODED BEYOND LIMITS AT XFS 372.75 TO XFS 379. REPAIRED SKIN IAW 8110-3 APPROVED DH SK 880-554.May 15, 2001 · N880UP · Doug DC873F · Wing, Plate/SkinSDR DHL2001801005Gyro · erraticCAPT ADI ERRATIC INTERMITTENT +/- 5 DEG PITCH WITH GYRO FLAG AND BOW TIE ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED NR 1 VERTICAL GYRO. OPS CHECKS GOOD IAW DC-8 MM 34-25-1.May 15, 2001 · N801DH · Doug DC873F · Attitude Gyro and Indicating SystemSDR UPS01836008Pressure Panel · corrodedINSPECTION TYPE:C1,3 RT NOSE TUNNEL UPPER PRESSURE WEB IS CORRODED BEYOND LIMITS STA-16 AT RBL 20. REPAIRED WEB IAW 8110-3 APPROVED DH SK 880-304.May 11, 2001 · N880UP · Doug DC873F · Fuselage Main, BulkheadSDR DHL2001805008Pin · draggingAILERON TRIM FROZEN AT CRUISE ALT FL310. INSPECTED & FOUND GUIDE PIN RT AILERON TRIM DRUM DRAGGING. R&R GUIDE PIN & GROMMETS IAW DC-8 MM 27-10-0. OPS CK OK ON GROUND. READY FOR SERVICE.May 10, 2001 · N805DH · Doug DC873F · Aileron Tab Control SystemSDR UPS01835859Angle · crackedINSPECTION TYPE:C1,3 LT WING L/E. VERTICAL ATTACH ANGLE IS CRACKED AT XS 520. REMOVED,FABRICATED, AND REPLACED ANGLEMay 9, 2001 · N880UP · Doug DC873F · Wing Miscellaneous StructureSDR DHL2001803005Indicator · faultyAUTOPILOT WHEN IN HEADING SELECT MODE DIVERGES IN ROLL. FOUND ON STEP 7A & 7B AT ROLL COMPUTER BITE CHECK, MM 22-12-0 PG 101-107, FAILED FULL SCALE RIGHT STOP WHEN SELECTING CAPT''S NAVIGATION INFO VIA NAV SELECT BUTTON. AUTOPILOT CONTROL PANEL ROLL COMPUTER BMay 9, 2001 · N803DH · Doug DC873F · Attitude Gyro and Indicating SystemSDR DHL2001805007Jackscrew · lack of lubeAT CRUISE ALT FL330 AILERON TRIM KNOB FROZEN IN POSITION. UNABLE TO TRIM AILERONS. REMAINED FROZEN UNTIL BELOW 10,000 FEET MSL. LUBED AILERON TRIM JACK SCREWS IAW DC8 M/M 12-81-1. OPS CKS GOOD.May 9, 2001 · N805DH · Doug DC873F · Aileron Tab Control SystemSDR UPS01835986Intercostal · crackedINSPECTION TYPE:C2,3 RIGHT WING L/E INTERCOSTAL IS CRACKED AT XS 454.976. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5769857 AND SRM 57-1-0, 51-1-20D, 51-1-21.May 8, 2001 · N880UP · Doug DC873F · Wing Miscellaneous StructureSDR DHL2001805006Trim Tab · lack of lubeAILERON TRIM KNOB FROZEN IN POSITION WILL NOT MOVE. FIRST NOTED IN DESCENT AT FL240. REMAINED FROZEN TO APPROX 11000. INSPECTED AND LUBED CONTROL TRIM TAB. NO DEFECTS FOUND. PERFORMED OPS CK OK IAW M/M 27-10-0. READY FOR SERVICE.May 8, 2001 · N805DH · Doug DC873F · Aileron Tab Control SystemSDR UPS01836004Angle · crackedINSPECTION TYPE:C1,3 STA -99 LT SIDE BULKHEAD CAP ANGLE IS CRACKED. REPAIRED ANGLE IAW 8110-3 APPROVED DH SK 880-270.May 6, 2001 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835886Fitting · crackedINSPECTION TYPE:C1,3 STA 683 AT L36R SIDE FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING.May 6, 2001 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA11026Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LH WING CENTER LE UPPER SKIN AT STA XFS341 TO XFS354, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAWMay 5, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA11025Skin · dentedDURING A MAINTENANCE VISIT FOUND DENTED DAMAGE TO C-PIT CROSS SLIDE DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 52-1-0, 51-1-21.May 5, 2001 · N602AL · Doug DC873F · Cargo/Baggage DoorsSDR UPS01835876Skin · corrodedINSPECTION TYPE:C1,3 LT I/B AILERON FWD UPPER SKIN CUTOUT AT XA 458 IS CORRODED BEYOND LIMITS. REPAIRED SKINMay 5, 2001 · N880UP · Doug DC873F · AileronsSDR UPS01835817Regulator · inoperativeCREW PREFLIGHT -CAPTAINS O2 REGULATOR FAILED. R&R CAPTS 02 REGULATORMay 5, 2001 · N813UP · Doug DC873F · Crew Oxygen SystemSDR UPS01836003Pressure Panel · corrodedINSPECTION TYPE:C1,3 RIGHT NOSE TUNNEL UPPER PRESSURE WEB IS CORRODED BEYOND LIMITS AT STA -80 TO -99 AT RBL 36. REPAIRED WEB IAW SRM 53-2-0 FIG 1D.May 4, 2001 · N880UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS01835888Web · crackedINSPECTION TYPE:C1,3 STA 80 SUBFLOOR IS CRACKED AT LBL 10. REPAIRED SUBFLOOR.May 4, 2001 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835887Frame · crackedINSPECTION TYPE:C1,3 STA 60 FRAME CRACKED UNDER DOUBLER AT RBL 24 REPAIRED FRAME.May 4, 2001 · N880UP · Doug DC873F · Fuselage Main, FrameSDR DHL2001802007Adc · faultyAUTOPILOT WILL NOT RESPOND AND LEVEL OFF DURING FLIGHT. ALT HOLD PORTION OF AUTOPILOT DEFERRED IAW MEL 22-8-2E. PLACARD INSTALLED. WAS UNABLE TO DUPLICATE ON GROUND. REPLACED DADC IAW DHL DC-8 SM 34-11-0 AND 22-10-0. PN OFF AND ON 9B-81010-15, SN OFF 15037, SMay 4, 2001 · N802DH · Doug DC873F · Air Data ComputerSDR UPS01836006Frame · corrodedINSPECTION TYPE:C1,3 STA 1140 FRAME IS CORRODED AND HAS MISDRILED HOLES BETWEEN LONG 32L TO 32R. REPAIRED FRAME IAW 8110-3 APPROVED DH SK 880-085.May 3, 2001 · N880UP · Doug DC873F · Fuselage Main, FrameSDR UPS01835988Frame · crackedINSPECTION TYPE:C2,3 STA 1394 FRAME IS CRACKED AT LONG 34R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.May 3, 2001 · N880UP · Doug DC873F · Fuselage Main, FrameSDR UPS01835987Frame · crackedINSPECTION TYPE:C2,3 STA 1400 FRAME IS CRACKED AT LONG 34R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.May 3, 2001 · N880UP · Doug DC873F · Fuselage Main, FrameSDR UPS01835881Fitting · crackedINSPECTION TYPE:C1,3 STA 1230 BANANA FITTING IS CRACKED AT L33R. REMOVED AND REPLACED FITTING IAW DWG 3755847 AND SRM 51-1-20DMay 3, 2001 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835879Fitting · crackedINSPECTION TYPE:C1,3 STA 1240 L35L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758498 AND SRM 51-1-21May 3, 2001 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835878Intercostal · crackedINSPECTION TYPE:C1,3 STA 1677 INTERCOSTAL IS CRACKED AT LT CUSP. REMOVED,FABRICATED,AND REPLACED INTERCOSTAL IAW DWG 9753254 AND SRM 51-1-20DMay 3, 2001 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835872Intercostal · corrodedINSPECTION TYPE:C1,3 STA 1340-1360 L31L INTERCOSTAL IS CORRODED BEYOND LIMITS. REMOVED,FABRICATED,AND REPLACED INTERCOSTAL IAW DWG 5751516 AND SRM 51-1-20DMay 3, 2001 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835846Fitting · crackedINSPECTION TYPE:C1,3 STA 830 L22L FITTING IS CRACKED. REMOVED AND REPALCED FITTING IAW DWG 4753360 AND SRM 51-1-20D, 51-1-21May 3, 2001 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835842Fitting · crackedINSPECTION TYPE:C1,3 STA 1240 L33R FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514,AND SRM. 51-1-20DMay 3, 2001 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835814Light · inoperativeEMERGENCY EXIT ARM/DISARM LIGHT INOPERATIVE. RELAMPED AND OPS CHECK GOODMay 3, 2001 · N812UP · Doug DC873F · Emergency LightingSDR UPS01835795Switch · inoperativeINSPECTION TYPE: PREFLT, FOUND DURING EMERGENCY LIGHT TEST. SWITCH INTERNALLY BAD DUE TO LIGHTS REMAIN ON WITH SWITCH ON OFF OR DISARMED POSITION. RESET TO S.W. MAKE LIGHT TO TURN OFF. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH AT OVERHEAD PANEL I/A/W WDM. May 3, 2001 · N802UP · Doug DC873F · Emergency LightingSDR DHL2001804008Seat Belt · broken2ND OFFICER SEAT BELT BROKEN. REINSTALLED RT LAP BELT IAW DC-8 MM 25-11-6. OPS CK OK.May 3, 2001 · N804DH · Doug DC873F · Flight Compartment Equipment
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