Douglas DC-8-62
Service difficulty reports · 2,778
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 = 'DC862' 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 = 'DC862' 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 95ZZZZ148Support · corrodedLEVEL 2 CORROSION/AFT CABIN SQUARE FLOOR SUPPORT FRAME IS CORRODED BETWEEN BS 1586 AND BS 1574. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.SDR 95ZZZZ147Window · corrodedLEVEL 2 CORROSION/MAIN CABIN WINDOW NR 18R HAS CORROSION ON INSIDE SURFACE OF FRAME. FABRICATED AND INSTALLED REPAIR PER RICH REPAIR SKETCH 5164-6.SDR 95ZZZZ146Web · corrodedLEVEL 2 CORROSION/AFT CARGO COMPARTMENT CIRCUMFERRENTIAL WEB CORRODED AT BS 1540 FROM 34L TO 34R. REMOVED CORROSION AND REPLACED SPLICE PLATE PER SRM 51-1-0.SDR 95ZZZZ145Floor Support · corrodedLEVEL 2 CORROSION/AFT CARGO COMPARTMENT OVERHEAD FLOOR SUPPORT CORRODED BETWEEN BS 1460 AND BS 1500, 12 INCHES LBL. CLEANED CORROSION AND FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.SDR 95ZZZZ144Angle · corrodedLEVEL 2 CORROSION/AFT CABIN FLOOR SUPPORT ANGLE AT BS 1520 IS CORRODED FROM 12 INCHES RBL TO 45 INCHES LBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.SDR 95ZZZW242Frame · corrodedLEVEL 2 CORROSION, CIRCUMFERRENTIAL FRAME IS CORRODED AT BS 1574 BETWEEN LONGERON 24 RT AND 26 RT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0.SDR 95ZZZW241Fitting · corrodedLEVEL 2 CORROSION, LONGERON 30 LT END BATHTUB FITTING IS CORRODED AT BS 1606L. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.SDR 95ZZZW240Frame · corrodedLEVEL 2 CORROSION, AFT CABIN LOWER CIRCUMFERRENTIAL FRAME 'J' FLANGES ARE CORRODED, UPPER AND LOWER AT BS 1586 FROM LONGERON 24L TO 24R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0.SDR 95ZZZW239Floorbeam · corrodedLEVEL 2 CORROSION, AFT CABIN FLOORBEAM CAP AT BS 1574 IS CORRODED FROM 36 INCHES LBL TO 36 INCHES RBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.SDR 95ZZZW238Longeron · corrodedLEVEL 2 CORROSION, LONGERON 36 IS CORRODED AT BS 1550. REMOVED CORROSION, FABRICATED AND INSTALLED REPAI ER SRM 53-2-2.SDR 95ZZZW237Longeron · corrodedLEVEL 2 CORROSION, LONGERON 36 IS CORRODED 6 INCHES FWD AND AFT OF BS 1574. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2.SDR 95ZZZW236Longeron · corrodedLEVEL 2 CORROSION, LONGERON 36 IS CORRODED BETWEEN BS 1606 AND BS 1585. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2.SDR 95ZZZW235Longeron · corrodedLEVEL 2 CORROSION, LONGERON 32 RT IS CORRODED BETWEEN BS 1606 AND 1585. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2.SDR 95ZZZW234Floorbeam · corrodedLEVEL 2 CORROSION, AFT CABIN FLOORBEAM CAP IS CORRODED AT BS 1440 FROM 45 INCHES LBL TO 45 INCHES RBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.SDR 95ZZZW233Fitting · corrodedLEVEL 2 CORROSION, LONGERON 30 RT END BATHTUB FITTING IS CORRODED AT PRESSURE BULKHEAD BS 1606R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.SDR 95ZZZW323Connector · looseDURING PREFLIGHT FOUND NR 2 ENGINE FIRE WARNING SYSTEM INOP. RESET CANNON PLUG, NR 2 ENGINE FIRE WARNING SYSTEM OK, CHECKED GOOD IAW MM 26-10.SDR 95ZZZW209Skin · corrodedL/E BETWEEN NR 3 AND 4 ENGINE HAS CORROSION LEVEL II AND DELAMINATION OF FASTENER HOLES (UPPER) XFS 304 TO XFS 416. REF N/R 1102 W/O NR 950007.SDR 95ZZZW208Support Plate · crackedL/E BETWEEN NR 3 AND 4 ENGINE AT XFS341.500 RIB LOWER SUPPORT PLATE HAS TWO CRACKS EMANATING FROM FASTENER HOLES. REF N/R 1101 WO NR 950007.SDR 95ZZZW210Eel Pwr Supply · inoperativeDURING ROUTINE MAINTENANCE CHECK, FOUND BATTERY PACK FOR EMERGENCY LIGHTS DEAD. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD IAW MM 33-10.SDR 95ZZZW211Eel Battery Pack · dischargedBATTERY PACK FOR EMERGENCY LIGHTS IS DEAD. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL IAW DC8MM 33-10-00/33-50-00.SDR 95ZZZW207Spar · corrodedCENTER TANK (WING) TOP AFT SPAR FLANGE (CAP) HAS LEVEL II CORROSION ON TOP OF HORIZONTAL FLANGE AROUND FASTENER HEADS AT BL 23L FS 857 REF N/R NR 5086.SDR BUFA9505Start Valve · failedDURING CLIMB THROUGH FL 260, PRECAUTIONARY ENGINE SHUT DOWN DUE TO NR 2 START VALVE OPEN. FOUND PRESSURE RELIEF CONTROL VALVE FAILED NR 2 ENGINE. REPLACED PRESSURE RELIEF CONTROL VALVE. OPS CHECK GOOD IAW MM 36-12-2. AIRCRAFT RETURNED TO SERVICE. (X)SDR BUFA9504Hyd Fitting · leakingDURING FINAL APROACH, ACFT HYDRAULIC PRESSURE DROPPED DOWN TO 500-600. FOUND HYDRUALIC LINE FITINGS AT LT MLG RETRACT ACTUATOR, PN 57740355507, LEAKING. REPLACED PACKING AT SAME FITTINGS. LEAK CHECK C/W IWA MM 29-01. AIRCRAFT RETURNED TO SERVICE. (X)SDR 95ZZZW253Seat Track · corrodedLEVEL 2 CORROSION, SEAT TRACK CORRODED FROM BS 150 RT TO BS 1540 RT, 39 INCHES RBL. REMOVED DAMAGED TRACK, FABRICATED REPAIR, CLEANED AREA, TREATED, PRIMED AND INSTALLED REPAIR AS PER SRM 51-10-00 AND 51-1-8.SDR 95ZZZW252Seat Track · corrodedLEVEL 2 CORROSION, SEAT TRACK CORRODED FROM BS 1500 RT TO BS 1540 RT 25 INCHES RBL. REMOVED DAMAGED TRACK, FABRICATED REPAIR, CLEANED AREA TREATED, PRIMED AND INSTALLED REPAIR AS PER SRM 51-1-8 AND 51-10-0.SDR 95ZZZW251Skin · corrodedLEVEL 2 CORROSION, FUSELAGE RT EXTERIOR SKIN AT WINDOW NR 14R HAS CORROSION AROUND FASTENERS. REMOVED WINDOW, REMOVED CORROSION, FABRICATED REPAIR, TREATED, PRIMED AND INSTALLED REPAIR AND WINDOW AS PER SRM 51-1-8, DRAWING RCH D85310-5015 AND MM 56-20-00.SDR 95ZZZW250Longeron · corrodedLEVEL 2 CORROSION, LONGERON 28 LT END FITTING IS CORRODED AT BS 1530 LT. REMOVED 'L' AND REMOVED CORROSION, FABRICATED REPAIR AND INSTALLED REPAIR AS PER SRM 51-1-8 AND 53-2-8.SDR 95ZZZW249Longeron · corrodedLEVEL 2 CORROSION, LONGERON 22 RT END FITTING CORRODED AT BS 1530 RT. REMOVED CORRODED END FITTING, TREATED NEW FITTING AND INSTALLED AS PER SRM 51-1-8 AND 51-1-00.SDR ABXA9500068Door Target · looseUPON GEAR RETRACTION, CREW HAD AN UNSATISFACTORY GEAR UPLATCH INDICATION. RECYCLED GEAR THREE TIMES, LEFT GEAR DOOR LIGHT ILLUMINATED. COMPLIED WITH ALTERNATE PROCEDURE AND LIGHT WENT OUT. CLEANED AND LUBED LEFT MLG DOOR UPLATCH MECHANISM. PERFORMED OPERATSDR IXXA199516Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND OUTBOARD OF THE NR 1 ENGINE, UPPER PLATING OF THE WING AT XS-00. THE AREA CORROSION WAS BLENDED BEYOND SRM LIMITS AND REQUIRED REPAIR. REPAIR WAS ACCOMPLISHED IAW SKETCH SKA 95002-2, WHICH WAS FAA DER APSDR IXXA199515Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND LEFT MLG TORQUE TUBE SUPPORT FITTING CRACKED BEYOND REPAIRABLE LIMITS. THE FITTING WAS REMOVED AND REPLACED IAW DOUGLAS SRM AND SB 53-61. (X)SDR IXXA199514Frame · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND AT FS 930 WINDOW FRAME LEFT SIDE. THE CORROSION WAS REMOVED AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED IAW SKETCH SKA95002-8, WHICH WAS FAA DER APPROVED, AND E.O. 53-DC8-132. (X)SDR IXXA199513Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS NOTED BETWEEN LONGERONS 34.5 LT TO 34.5 RT, BETWEEN FS 980 AND FS 1087. CORROSION REMOVAL ON THE INTERNAL SKIN WENT BEYOND SRM LIMITS. REPAIR OF THE ARA WAS ACCOMPLISHED IAW SKETCH SKA 95002-7, AND E.O. 53-DC8SDR IXXA199512Longeron · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND CORROSION REMOVAL IN A LOCALIZED AREA IN THE RADIUS OF LONGERON 35 RT, STA 587-STA 592 WAS BLENDED BEYOND SRM LIMITS. REPAIR OF THE LONGERON WAS ACCOMPLISHED IAW SKETCH SKA95002-5, WHICH WAS FAA DER APPROVED, AND E.O. SDR IXXA199511Longeron · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON LONGERON 32 RT FS 973. CORROSION BLEND OUT OF THE LONGERON WENT BEYOND SRM LIMITS. REPAIR OF THE LONGERON WAS ACCOMPLISHED BY INSTALLING REPAIR DOUBLERS IAW SKA93002-3, WHICH WAS FAA DER APPROVED, ANDSDR IXXA199510Skin · corrodedDURING ROUTINE 'C' CHECK INSPECTION, UPPER LEFT WING SKIN CORROSION WAS FOUND. CORROSION REMOVAL WENT BEYOND LIMITS OF THE DOUGLAS SRM. REPAIR WAS ACCOMPLISHED AFTER REMOVAL OF ALL CORROSION IAW SKETCH SKA95002-2, AND E.O. 57-DC8-126. AFFECTED AREA WAS STR SDR 95ZZZW246Skin · corrodedLEVEL 2 CORROSION, RT WING L/E O/B SLOT CUTOUT FWD SKIN HAS SURFACE CORROSION I/B SIDE. CUT OUT CORROSION AND INSTALLED DOUBLER PER SRM 51-2-1.SDR 95ZZZW245Fitting · corrodedLEVEL 2 CORROSION, LONGERON 26 RT END FITTING IS CORRODED AT STA 1530. REMOVED AND REPLACED DAMAGED SECTION OF LONGERON PER SRM 51-1-0.SDR 95ZZZZ83Skin · corrodedLEVEL 2 CORROSION, LEADING EDGE PANEL FOR SLOT DOORS NR 2, NR 3 AND NR 4 HAS INTERGRANULAR CORROSION AT INBD END. REMOVED CORROSION FABRICATED AND INSTALLED DOUBLER PER SRM 53-2-1.SDR 95ZZZZ82Skin · corrodedLEVEL 2 CORROSION, FUSELAGE SKIN ABOVE WINDOW 19L HAS CORROSION AROUND FASTENER HEAD. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 51-1-8 AND RIAA DRAWING NR RCH D85310-5015.SDR 95ZZZZ81Circumferential · corrodedLEVEL 2 CORROSION, AFT CARGO COMPARTMENT CIRCUMFERRENTIAL END IS CORRODED AT STA 1140, LONGERON 33 CENTER OF DOORWAY. CLEANED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 51-1-8.SDR 95ZZZZ80Skin · corrodedLEVEL 2 CORROSION, FUSELAGE RT SIDE EXTERIOR SKIN AT WINDOW NR 14R HAS CORROSION AROUND FASTENERS. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 51-1-2.SDR 95ZZZZ79Circumferential · corrodedLEVEL 2 CORROSION, AFT CARGO COMPARTMENT CIRCUMFERENTIAL LOWER FLANGE AND VERTICAL SIDEWALL SUPPORT ARE CORRODED AT STATION 1340 BETWEEN LONGERONS 27R AND 26L. REMOVED CORRODED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 54-4-20.SDR 95ZZZZ78Skin · corrodedLEVEL 2 CORROSION, RT WING L/E JUST OUTBOARD OF NR 4 ENGINE PYLON HAS BULGING CORROSION AROUND SCREW HEADS AND SKIN CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1.SDR 95ZZZZ73Skin · corrodedLEVEL 2 CORROSION, RT WING L/E UPPER SURFACE PANEL AFT OF OUTBOARD SLOT HAS CORROSION AROUND SCREW HEADS. REMOVED CORRODED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1.SDR ABXA9500065Hose · leakingHYDRAULIC QUANTITY WENT TO STANDPIPE LEVEL ON APPROACH. REMOVED AND REPLACED THRUST REVERSER HYDRAULIC PUMP PRESSURE HOSE WHICH WAS LEAKING. SYSTEM OPS CHECKED GOOD IAW DC 8 MM CHAPTER 78.SDR 95ZZZZ77Circumferential · corrodedLEVEL 2 CORROSION, AFT CARGO COMPARTMENT AT STATION 1240 CIRCUMFERENTIAL HAS CORROSION ON UPPER AND LOWER FLANGES FROM LONG 35 LT TO 34 RT. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-0.SDR 95ZZZZ76Skin · corrodedLEVEL 2 CORROSION, RT WING L/E UPPER SURFACE PANEL OUTBOARD OF NR 4 PYLON HAS CORROSION AROUND SCREW HEADS. REMOVED DAMAGED AREA AND FABRICATED AND INSTALLED REPAIR PER SRM 51-1-20.SDR 95ZZZZ75Skin · corrodedLEVEL 2 CORROSION, RT WING NR 3 AUX FUEL TANK HAS BULGING CORROSION AROUND SCREW HEADS. REMOVED CORRODED SECTION AND REPAIRED PER SRM 57-2-1.SDR 95ZZZZ74Skin · corrodedLEVEL 2 CORROSION, RT WING LEADING EDGE STATION 223.5 TO 257.5 HAS BULGING CORROSION. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 57-2-1.
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