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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DHL2004807007Handle · looseLEFT FWD ENTRY DOOR INTERIOR DOOR HANDLE HAS PLAY. REMOVED HANDLE & TIGHTENED HARDWARE, REINSTALLED HANDLE, OPS CHECK NORMAL MM 52-14-1. NO PARTS REPLACED.SDR DHL2004806001Line · loosePARKING BRAKE WILL NOT HOLD PRESSURE WHEN BRAKES ARE SET. FOUND LINE SEEPING ON OUTBOARD ANTI SKID CONTROL VALVE. TIGHTENED LINE, LEAK CHECK GOOD PER 20-13-0, BRAKES OPS CHECK GOOD PER MM 32-40-0. NO COMPONENT REMOVAL.SDR DHL2004801006Line · leakingIN FLIGHT NR 2 ENGINE OIL QUANTITY INDICATED LESS THAN 2 QUARTS, PERFORMED OIL QUANTITY LOW ABNORMAL PROCEDURE AND INFLT ENGINE SHUTDOWN ABNORMAL PROCEDURE, WIND MILLING STARTED AT 0818 ZULU OIL PRESSURE 3 PSI OIL PRESSURE WAS 20 PSI WHEN ENGINE WAS SHUTDOWN. SDR IXXA060163SDoubler · crackedDURING ROUTINE C-CHECK FOUND LT WING TRAILING EDGE NR 4 SPOILER BAY THIRD RIB FROM FLAP HINGE FORWARD OB SIDE DOUBLER CRACKED AND MISSING FASTENERS. REMOVED DOUBLER. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIRSDR IXXA060162SRib · gougedDURING ROUTINE C-CHECK, FOUND LT WING TRAILING EDGE NR 4 SPOILER BAY THIRD RIB FROM FLAP HINGE FORWARD OB SIDE GOUGED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS IAW SSDR IXXA060161SSpoiler · gougedDURING ROUTINE C CHECK FOUND LT WING NR 3 SPOILER PANEL IB TRAILING EDGE GOUGED IN TWO PLACES. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, TRIMMED, AND TREATED. APPLIED ADHEASIVE, AND CURED. SEALED EDGES AND PRIMED. IAW SRM 57-7-0, 51-1-8, 51-1-15, ANDSDR IXXA060160SSpoiler · gougedDURING ROUTINE C CHECK FOUND LT WING NR 2 SPOILER PANEL LOWER OB TRAILING EDGE GOUGED. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, TRIMMED, AND TREATED. APPLIED ADHESIVE, AND CURED. SEALED EDGES AND PRIMED. IAW SRM 57-7-0, 51-1-8, 51-1-15, AND 51-1-9A.SDR IXXA060159SPanel · dentedDURING ROUTINE C CHECK FOUND LT WING LOWER TRAILING IB FIXED PANEL HAS DENT AFT OF MAIN LANDING GEAR STRUT. REMOVED FASTENERS AS NEEDED TO REMOVE PANEL. REMOVED DAMAGE. FABRICATED REPAIR PARTS, TRIMMED, TREATED, APPLIED ADHESIVE, PERFORMED HOT BOND, INSTALLED SDR IXXA060158SAngle · crackedDURING ROUTINE C CHECK FOUND LT WING AFT WING ROOT, AT STATION XFS-950,AND XW-0, ANGLE PLATE CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED NEW ANGLE AND NEW FASTENERS.SDR IXXA060157SAngle · gougedDURING ROUTINE C-CHECK, FOUND LEFT WING ROOT XFS-970, XW-0 ANGLE GOUGED AT AFT END, NUMBER 1 FLAP ROLLER TRACK. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, DEBURRED, TRIMMED, TREATED, PRIMED. INSTALLED NEW ANSDR IXXA060122SSkin · dentedDURING ROUTINE C-CHECK FOUND RIGHT WING OUTBOARD AILERON UPPER SURFACE DENTED. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT RIGHT WING OUTBOARD AILERON UPPER SURFACESDR IAAX060114SSill · tool damageDURING ROUTINE C-CHECK FOUND AFT ENTRANCE DOOR SILL HAS TOOLING DAMAGE AT STATION 1620 LONGERON 20 LT. REMOVED DAMAGE. FABRICATED REPAIR PART. LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT STA 1620 LONGERON 20 LT IAW SSDR IXXA060108SLongeron · crackedDURING ROUTINE C-CHECK FOUND STATION 120 TO 140 LONGERON 35 LT CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVED DAMAGED LONGERON SECTION. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND FASTENERS WET WITH SEASDR IXXA060107SSplice · crackedDURING ROUTINE C CHECK FOUND LONGERON 31 RIGHT OUTBOARD SIDE CENTER SPLICE CRACKED FROM STATION 460 TO STATION 476. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED SPLICE. FABRICATED NEW SPLICE, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED NEW SPLICE ASDR IXXA060106SFrame · corrodedDURING ROUTINE C-CHECK FOUND FORWARD CARGO COMPARTMENT FRAME CORRODED OUT OF LIMITS AT STATION 280 BETWEEN LONGERON 32 RT AND LONGERON 34 RT. REMOVED FASTENERS AS NEEDED TO REPLACE FRAME SEGMENTS. FABRICATED NEW FRAME SEGMENTS, AND REPAIR ANGLES. LOCATED, DRILSDR UPS04842741Keelbeam · crackedINSPECTION TYPE:C-3 LEFT W/W AT KEEL BEAM AT FS 922 TO 936 HAS A CRACK. REPAIRED IAW REO GO9853.SDR UPS04842740Fitting · corrodedINSPECTION TYPE: C-3, R/S CUSP FRAME 35 FWD & AFT CUSP FITTING ARE CORRODED AT FLOOR AT BOLTS B6 69. REMOVED CUSP FITTINGS FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. DRILLED NEW FITTING IAW DC8 SRM 51-3-2. ALODINED & PRIMED IAW DC8 SRM 51-1- 8. INSTALLESDR UPS04842599Longeron · crackedINSPECTION TYPE: C2, LONG 12 LT CRACKED AT STA 1746. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONG SECTION FROM STA 1740 TO 1766 & INSTALLED SPLICE FITTING IAW SRM 53-2-2 FIG 11.SDR UPS04842598Longeron · crackedINSPECTION TYPE:C2 STA 1756, LONG 14 LT CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONG SECTION FROM STA 1746 TO STA 1766. INSTALLED SPLICE FITTING AND STRAPS IAW SRM 53-2-2 FIG 10.SDR IXXA060156SMembrane · crackedDURING ROUTINE C-CHECK, FOUND LEFT WING LEADING EDGE 522A BAY INBOARD AND FORWARD OF PANEL CUT OUT ANTI-ICE DISCHARGE MEMBRANE CRACKED AT HOLES 3 PLACES .5 INCH EACH XFS395. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED REPAIR PART, LOCATED, DRILSDR IXXA060151SSkin · crackedDURING ROUTINE C CHECK, FOUND NUMBER 1 ENGINE PYLON AFT INBOARD SIDE ADAPTER PANEL CRACKED AT FORWARD UPPER PYLON SPAR ATTACH POINT APPROXIMATELY 1/2 INCH. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED DOUBLERS, LOCATED, DRILLED, TRIMMED, DEBURRESDR IXXA060150SPanel · crackedDURING ROUTINE C CHECK, FOUND NUMBER 1 ENGINE PYLON AFT PYLON ADAPTER PANEL CRACKED APPROXIMATELY 2 1/2 INCHES AT FORWARD ACCESS PANEL. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSDR IXXA060143SFloor Support · crackedDURING ROUTINE C CHECK, FOUND FLOOR SUPPORT FLANGE HAS 5 EACH CRACKS AT STATION 1280 LONGERON 31 RIGHT AND 29 LEFT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FLOOR SUPPORT FLANGE. WELDED CRACKS IAW DC8 DPS 10.225. INSTALLED REPAIRED FLANGE AT AT STATIONSDR IXXA060142SFloor Support · corruptedDURING ROUTINE C CHECK, FOUND FLOOR SUPPORT FLANGE CRACKED AT STATION 1160 LONGERON 31 RIGHT. REMOVED DAMAGE, FABRICATED DOUBLER AND FILLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED FILLER AND DOUBLER AND NEW FASTENERS AT AT STATION 116SDR IXXA060141SFloor Support · gougedDURING ROUTINE C CHECK, FOUND LEFT FLOOR TRACK FLANGE GOUGED AT STATION 1080. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED NEW FLANGE, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED NEW FLANGE AND NEW FASTENERS AT LEFT HAND FLOORSDR IXXA060113SSill · misdrilledDURING ROUTINE C-CHECK FOUND RT SERVICE DOOR SILL (FRAME, WEB AND ANGLE) AT STATION 196 LONGERON 11 RT HAS A FASTENER HOLE DOUBLE DRILLED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTASDR UPS04842739Frame · corrodedINSPECTION TYPE: C-3, AC COMPT STA 55 LONG 30-31 RIGHT CORR AT INTERSECTION OF FRAME TO T/R BOX LEG ANGLE. RECEIVED FRAME SECTION AND SPLICES FROM STRUCTURE CENTER WORK ACCOMPLISHED ON TIMCO N/R 5001. FAB 4 EA SPLICES 2-19 & 2-17 IAW TR 53-125, THEN HEAT TRESDR UPS04842690Longeron · corrodedINSPECTION TYPE: C-3, MID ACC COMPT CORRODED LONG 31 RT STA 640-668. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED SECTION LONGERON STA 610 TO 710 IAW DC8 SRM 51-1-20D. RECEIVED, LOCATED & DRILLED UP LONGERON NR 2646610, IAW DC8 SRM 51-SDR UPS04842654Skin · corrodedINSPECTION TYPE:C2 LEFT HORIZONTAL STAB L/E IS CORRODED AT XFS 178.5. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS OR CORROSION AT CUTOUT, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 55-2-1 FIG 4.SDR UPS04842652Doubler · damagedINSPECTION TYPE:C2 RIGHT UPPER HORIZONTAL STAB LEADING EDGE HAS ELONGATED HOLES BETWEEN XFS 47.5 TO XFS 110.0. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AND INTERNAL DOUBLER IAW DWG 5644330 AND SRM 55-2-1 FIG 4.SDR UPS04842604Skin · corrodedINSPECTION TYPE: C2, LEFT HORIZONTAL STAB LEADING EDGE UPPER SKIN IS CORRODED XFS 272.5. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55-2-1 FIG 4.SDR UPS04842595Rib · crackedINSPECTION TYPE: C2, LEFT HORIZONTAL STAB UPPER RIB IS CRACKED AT XFS 47.5. REMOVED AND REPLACED ANGLE IAW DWG 5654549 AND SRM 51-1-20D.SDR UPS04842551Fan · failedSMOKE IN COCKPIT PASSING 25,000 BEGAN TO FILL THE COCKPIT WITH STRONG ELECTRICAL FIRE SMELL. DECLARED EMERGENCY AND LANDED ASAP. FOUND RECIRC FAN INTERNAL FAILURE. REMOVED RECIRC FAN 67302. INSTALLED NEW FAN IAW 21-01-2, OPS CHECK NORMAL. OK FOR CONTINUEDSDR IXXA060140SCusp Web · crackedDURING ROUTINE C CHECK, FOUND A CRACKED CUSP BETWEEN STATION 980 AND 1000 AT LONGERON 21 RIGHT. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER AT STATION 980 AND 1000 AT LONGERON 21 RISDR IXXA060139SSupport · crackedDURING ROUTINE C CHECK, FOUND RIGHT AFT LOWER CARGO TUNNEL; STATION 1000 RIGHT UPPER HORIZONTAL SIDE WALL SUPPORT CRACKED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT RIGHT ASDR IXXA060103SCusp Web · crackedDURING ROUTINE C-CHECK FOUND FORWARD CARGO COMPARTMENT BETWEEN STATION 80 AND STATION 100 LONGERON 21 RT 10 INCHES FROM OB CUSP WEB CRACKED. REMOVED DAMAGE. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, DEBURED, PRSDR UPS04842645Frame · crackedINSPECTION TYPE: C2, STATION 55 FRAME IS CRACKED AT LONG 24R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER AND REPAIR SPLICES IAW SRM 53-2-0 FIG 2.SDR UPS04842641Frame · crackedINSPECTION TYPE: C2, STATION 55 FRAME IS CRACKED AT LONG 24L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER AND SPLICES IAW SRM 53-2-0 FIG 2.SDR IXXA0400066OUplock · lack of lubeON DEPATURE FROM KBDL TO KTOL GEAR UPLATCH CHECK FAILED. THE GEAR NOT LATCHED LIGHT CAME ON AND NOSE GEAR CAME OUT OF THE WHEEL WELL. CREW COMPLETED FLIGHT TO KTOL AND LANDED WITH OUT INCIDENT. MAINTENANCE JACKED AIRCRAFT, INSPECTED, CLEANED AND LUBED UPLATSDR IXXA060155SDrive Link · crackedDURING ROUTINE C-CHECK, FOUND LEFT WING INBOARD FORWARD FLAP DRIVE LINK ASSEMBLY CRACKED AT ACTUATOR ATTACH POINT -J-, AT WING STATION XW-97.906. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FLAP LINK ASSEMBLY. RECEIVED NEW FLAP DRIVE LINK ASSEMBLY, AND INSSDR UPS04842620Seat Track · brokenINSPECTION TYPE: C, LUG BROKEN POS 3 LEFT O/B SEAT TRACK PLANK NEXT TO LOCK. REMOVED AND REPLACED SEAT TRACK PLANK SECTION FS-200 TO FS-265-00.SDR DHL2004804003Bulb · faultyAFTER T/O DOOR NOT LATCHED LIGHT ILLUMINATED, RAN ABNORMAL PROCEDURE, LIGHT REMAINED LIT. PROCEEDED AT .65 M - 230 KTS PER PROCEDURE. TROUBLESHOT AND FOUND FAULTY BULB ON DOORS NOT LATCHED LAMP. REMOVED AND REPLACED BULB. PERFORMED LANDING GEAR DOOR OPS CHSDR UPS04842477Window Frame · corrodedINSPECTION TYPE:N/A SEVERAL AREAS OF CORROSION ON CTR WINDSHIELD LOWER FRAME. CHECKED CORROSION PITTING WITH DIAL DEPTH GAUGE, DEEPEST FITTING IS .020 REMOVED ALL PITTING IAW SRM 51-1-4-8. ULTRASOUND AREAS. FOUND .077 REMAINING. BLEND CORROSION IAW SRM 53-02-SDR DHL2004805005Pump · malfunctioned25 MIN AFTER SETTING CRUISE THRUST, FL 360, ENGINE NR 1 FLAMED OUT. ENGINE INSTRUMENTS NORMAL, DESCENDED TO FL 240 AND INITIATED IN-FLIGHT ENGINE START PROCEDURE, ENGINE START NORMAL, CLIMBED BACK TO FL 360. ALL ENGINE INDICATIONS NORMAL. COMPLETED ALL EMERGENSDR UPS04842480Longeron · corrodedINSPECTION TYPE: C-2, FWD BAG PIT, L28L CORROSION BETWEEN FS 320 & 340. REMOVED CORR FROM L28L SIDE OF VERTICAL LEG AT FS 325, 330 & 335. ORIG THICKNESS VERTICAL LEG .063 IAW DAC DWG 9754913 MAT'L REMOVED .015, AMT REMAINING .048. OUT OF LIMITS. FAB -31 REPSDR DHL2004809006Sensor · cloggedNR 4 ENG ROLLED BACK AT 0300Z; WINDMILL N2 = 12 PERCENT, N1 = 28 PERCENT, OIL PRESSURE = 3 PSI, OIL QTY = 16 QTS. FOUND RT CDP SENSOR CLOGGED. CLEARED BLOCKAGE, PERFORMED POWER RUN, OPS CHECKED SERVICEABLE. TROUBLESHOT NR 4 ENG, ENG LOSES POWER OR FLAMES OUSDR UPS04842542Skin · corrodedINSPECTION TYPE: C-2, MARKER BEACON MOUNT AREA HAS HEAVY CORROSION (SKIN). BLEND CORROSION FOUND OUT OF LIMITS. REMOVED LT LOWER STRESS PANEL MAT ID 7075-T6, -.071, PO 434977.6 FOR DOUBLER IAW REO GO 9816. FAB REPAIR DOUBLERS IAW REO GO9816. ALODINED & PRISDR UPS04842378Control Panel · failedN/A DURING TAXI OUR AND JUST BEFORE TAKEOFF, WE GOT A BUSS POWER FAIL LIGHT AND NR 4 GEN UNPARRALLED LIGHT ON. SMOKE BEGAN TO ACCUMULATE IN THE COCKPIT. TAXIED BACK TO RAMP. FOUND NR 4 GCP TO HAVE A HARD FAILURE. SUSPECT NR 4 GCP AS CAUSE OF SMOKE. RAN A/C PNSDR UPS04842541Seat Track · corrodedINSPECTION TYPE:C-2, MAIN CABIN FS AT 995 SEAT TRACK -E- HAS CORROSION BETWEEN LUGS. REMOVED CORROSON FOUND TO BE OUT OF LIMITS. REMOVED FLOORBOARD 1000 TO 1060. CUT SEAT TRACK FROM STA 830 TO 1100 IAW EO DC8 5320517C DWG DC8 53B 003. MAT ID SEAT TRACK 277SDR UPS04842449Seat Track · corrodedINSPECTION TYPE:C-2 MAIN CABIN FS AT 995 SEAT TRACK "E" HAS CORROSION BETWEEN LUGS. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. CUT SEAT TRACK EO DC8-5320-5167C DWG DC8-53B-003. LOCATED, DRILL AND DEBURRED SEAT TRACK PLUS 2 SPLICE FITTING SEAT TRACK. ALODINE
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