Douglas DC-8-62

Service difficulty reports · 2,778

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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.

SDR 99T64R288ARSkin · dentedNR 2565 - DENT EXTERIOR RT FUSELAGE FORWARD OF D-PIT DOOR BETWEEN L24R AND L27R STA 1200 - STA 1240. REMOVED DAMAGED AREA IAW DC-8 SRM 53-2-1. FABRICATED DOUBLERS AND INSTALLED IAW EC-8 SRM IAW DC-8 SRM'S 53-2-1 AMND 51-1-20D. REF: ARROW AIR, ARWA. (X)Apr 7, 1999 · N1808E · Doug DC862 · Fuselage Main, Plate/SkinSDR 99T64R270ARSkin · corrodedNR 0328 - RT WING UPPER LEADING EDGE, TRAILING EDGE LIGHT SURFACE CORROSION EMANATING FROM SCREW HOLE XW 693,XFS 766.250. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FILLERS AND DOUBLERS, INSTALLED PER EO 99-051 AND 99-061 WITH APROVED FAA FORM 8110-3 Apr 7, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R242ARSkin · crackedNR 0888 - NR 2 PIT DOOR OPENING LOWER EDGE SKIN CRACKED AT EDGE STA 520. CUT OUT DAMAGED AREA AND REPAIRED PER EO 99-049 WITH APPROVED FAA FORM 8110-3 DATED 3-8-99. REF: ARROW AIR, ARWA. (X)Apr 7, 1999 · N1808E · Doug DC862 · Fuselage Main, Plate/SkinSDR 99T64R256ARSkin · corrodedNR 0901 - RT WING UPPER SURFACE NR 3 INBOARD STUB WING CORROSION EXFOLIATION TRAILING EDGE AND CORROSION EMANATING FROM SCREW HOLES XW 257.500 TO XW 223.500. CUT OUT 2 EACH DAMAGED AREAS, FABRICATED DOUBLER REPAIRS AND INSTALLED PER EO 99-023 AND 99-061, TASKApr 6, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R254ARWeb · damagedNR 1253 - RT INBOARD FLAP WELL WEB, FASTENERS PULLED THROUGH XCW 69.5 BS 980 - BS 1020. REMOVED WEB, FABRICATED NEW WEB AND INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)Apr 6, 1999 · N1808E · Doug DC862 · Wing Miscellaneous StructureSDR 99T64R347ARPlate · corrodedFOUND CORROSION ON RIGHT OUTBOARD WING LEADING EDGE INBOARD SEGMENT ALONG TRAILING EDGE FASTENERS. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO 99-033. (M)Apr 1, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R287ARBulkhead · crackedNR 2348 - POSSIBLE CRACK IN WEB OF AFT PRESSURE BULKHEAD APPROXIMATELY 15 INCHES INBOARD OF L10R. CRACK CONFIRMED BY NDT. ROUTED OUT CRACK IAW DC-8 SRM 53-2-5. FABRICATED FILLERS AND DOUBLERS IAW DC-8 SRM 53-2-5. INSTALLED IAW DC-8 SRM'S 51-1-21 AND 51-1-2Apr 1, 1999 · N1808E · Doug DC862 · Fuselage Main, BulkheadSDR 99T64R244ARLongeron · crackedNR 1153 - CORROSION AND CRACKED LONGERON 36 BETWEEN FRAMES 1320 - 1340. REMOVED DAMAGED SECTION OF L36, FABRICATED REPAIR PARTS AND INSTALLED PER EO 99-055 WITH APPROVED FAA FORM 8110-3 DATED 3-11-99. REF: ARROW AIR, ARWA. (X)Apr 1, 1999 · N1808E · Doug DC862 · Fuselage Main, Longeron/StringerSDR 99T64R285ARFrame · corrodedNR 1498, CORROSION FRAME 1140 UPPER CHORD, WEB SHEER TIE FROM L33R - L31L. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FRAME SPLICES IAW DC-8 SRM 53-2-9. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED IAW DC-8 SRM 53-2-0. ARROW AIR (M)Mar 31, 1999 · N1808E · Doug DC862 · Fuselage Main, FrameSDR 99T64R246ARSkin · misinstalledNR 1780, RT HORIZONTAL STABILIZER OUTBOARD L/E TOP OUTBOARD DOUBLER REMOVE/REPLACE AND INSTALL WITH CONICAL WASHERS. FABRICATED DOUBLERS IAW DC-8 SRM 51-1-4 ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, AND INSTALLED IAW DC-8 SRM'S 55-2-1, 51-1-21, AND 51-1-4. REMar 31, 1999 · N1808E · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR 99T64R238ARKeel Beam · corrodedNR 0310 - CORROSION SIDE KEEL BEAM INSPECTION PLATES RT WW FROM GEAR DOOR ACTUATOR CYLINDER AFT STA 920 - STA 980. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FLAP PEENED TREATED AND PRIMED, FILLED WITH PRC 1422 PER EO 99-035 ADN EO 99-061 WITH APPROVED FAA FORM Mar 30, 1999 · N1808E · Doug DC862 · Fuselage Main, KeelSDR 99T64R354ARPlate · damagedREMOVED L-2 DOOR SCUFF PLATE AND INSPECT EXPOSED AREA. REMOVED SCUFF PLATE, INSPECTED AREA. NO CORROSION NOTED. PLUGGED EXISTING HOLES TREATED AND RPIMED PER EO 99-053. (M)Mar 29, 1999 · N1808E · Doug DC862 · Passenger/Crew DoorsSDR 99T64R378ARSkin · corrodedNR 0735 - MID ACC. COMPT CORROSION - SKIN L34R - L35L STA 680. REMOVED CORROSION, FABRICATED FILLERS AND DOUBLERS AND INSTALLED PER EO 99-040 WITH APROVED FAA FORM 8110-3 DATED 3-4-99. REF: ARROW AIR, ARWA. (X)Mar 29, 1999 · N1808E · Doug DC862 · Fuselage Main, Plate/SkinSDR 99T64R294ARSkin · corrodedNR 0382 - PREVIOUS CORROSION BLEND OUT STRINGER 11 RT WING STA XW 408. REMOVED PAINT, FASTENERS AND CORROSION IAW DC-8 SRM'S 51-1-8 AND 51-1-20D. REMAINING SKIN THICKNESS IS ACCEPTABLE IAW DACO DOCUMENT M-7200-99-02208 ITEM 4. TREATED AND PRIMED IAW SRM 51-Mar 29, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR ARWA990307Oil Pump · failedMIA - NR 4 ENGINE OIL PRESSURE DROPPED TO 32 PSI. SHUTDOWN ENGINE AS PER ABNORMAL CHECKLIST. WINDMILL SPEEDS WERE N1, 13.5 PERCENT, N2 21 PERCENT, OIL PRESS 3 PSI. AIRCRAFT RETURNED TO MIAMI WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 ENGINE OIL PUMP ASSY Mar 25, 1999 · N1804 · Doug DC862 · Turbine Engine Oil SystemSDR 99T64R373ARPlate · lightning strikeLIGHTNING STRIKE HOLE TOP TRAILING EDGE RUDDER. CUT OUT DAMAGE, FABRICATED FILLERS AND DOUBLERS PER EO 99-030 AND INSTALLED PER EO 99-030 AND DC-8 SRM 51-1-21. (M)Mar 24, 1999 · N1808E · Doug DC862 · Rudder, Plate/SkinSDR 99T64R377ARPlate · corrodedCUSTOMER REQUEST EVALUATE REPAIR ON FUSELAGE SKIN STATION 445-L22R. REMOVED DAMAGED/CORROSION AREA. FABRICATED FILLERS AND DOUBLERS AND INSTALLED PER EO 99-042 WITH APPROVED FAA FORM 8110-3 DATED 3-2-99. (M)Mar 24, 1999 · N1808E · Doug DC862 · Fuselage Main, Plate/SkinSDR ABXA9900249O Ring · failedDURING CRUISE, HYDRAULIC SYSTEM QUANTITY DECREASED. PERFORMED LOSS OF HYDRAULICS EMERGENCY PROCEDURES. REPLACED O-RING ON NR 3 ENGINE DRIVEN HYDRAULIC PUMP.Mar 24, 1999 · N805AX · Doug DC862 · Hydraulic System, MainSDR 99T64R239ARFitting · corrodedNR 0542 - RT HORIZONTAL STABILIZER, BATH TUB FITTING CORRODED STA XE77. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED STRAP REPAIR AND INSTALLED PER EO 99-045 APPROVED FAA FORM 8110-3 DATED 3-2-99. REF: ARROW AIR, ARWA. (X)Mar 22, 1999 · N1808E · Doug DC862 · Horizontal Stabilizer StructureSDR 99T64R284ARSkin · corrodedNR 1966, LEFT WING OUTBOARD LEADING EDGE OUTBOARD SECTION, CORROSION STATION 878. REMOVED CORROSION IAW DC-8 SRM 51-1-8. CUT OUT DAMAGED AREA IAW DC-8 SRM 57-2-0. FABRICATED DOUBLER IAW DC-8 SRM 57-2-1. TREATED AND PRIMED IAW DC-8 51-1-8. INSTALLED DOUBLEMar 20, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR ARWA990306Retract Mech · lack of lubeMIA - FLT 656 - AIR TURNBACK, ON UPLATCH CHECK, GEAR NOT LATCHED LIGHT ON. PROCEEDED WITH ABNORMAL CHECKLIST. WITH ENGINE PUMPS OFF, GEAR NOT LATCHED LIGHT CAME ON ABOUT 1 OR 2 MINUTES LATER. UNABLE TO DUMP FUEL ELECTRICALLY, MANUAL STARTED THEN GOT EXTREMELYMar 19, 1999 · N810BN · Doug DC862 · Landing Gear Retraction/Extension SystemSDR 99T64R374ARAngle · corrodedFOUND CORROSION ON CUSP LINE RIGHT LINE L21R FROM STATION 208-270. REMOVED CORROSION, CUT OUT DAMAGED AREA FABRICATED FILLER AND PLUG AND INSTALLED PER EO 99-061, WITH APPROVED FAA FORM 8110-3 DATED 6/14/99. (M)Mar 18, 1999 · N1808E · Doug DC862 · Fuselage Miscellaneous StructureSDR 99T64R379ARSkin · corrodedNR 066 - CORROSION ON VERTICAL STABILIZER UPPER AND LOWER ATTACH RUSTY SCREWS STA 185. REMOVED CORROSION, FABRICATED FILLERS AND DOUBLERS AND INSTALLED PER EO 99-046 WITH APPROVED FAA FORM 8110-3 DATED 3-3-99. REF: ARROW AIR, ARWA. (X)Mar 13, 1999 · N1808E · Doug DC862 · Vertical Stabilizer, Plate/SkinSDR 99T64R369ARPlate · corrodedTOP LEFT WING CORROSION ON SKIN AND SCREW RUSTY INBOARD END WING L/E BETWEEN 1 AND 2 PYLONS, XFS 291.500. REMOVED CORROSION, FABRICATED DOUBLER AND FILLER AND INSTALLED PER EO 99-061 AND 99-031. (M)Mar 11, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R380ARFastener · missingNR 0557 - NR 2 PYLON LOWER SURFACE 2 EACH FASTENERS MISSING OUTBOARD SIDE ABOVE TAILPIPE. YN 219 AND YN 300. REAMED HOLES TO -197/-199 DIAMETER. INSTALLED MS21141 - V06 FASTENER PER EO 99-036 WITH APPROVED FAA FORM 8110-3 DATED 2-24-99. REF: ARROW AIR, ARMar 11, 1999 · N1808E · Doug DC862 · Nacelle/Pylon, Plate/SkinSDR 99T64R375ARPlate · corrodedLT OUTBOARD STUB WING CORROSION. REMOVED CORROSION, FABRICATED FILLERS, DOUBLERS AND INSTALLED PER EO 99-034 WITH APPROVED FAA FORM 8110-3 DATED 3-3-99. (M)Mar 9, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR ABXA9900285Skin · corrodedDURING C-CHECK, FOUND LEVEL-2 CORROSION AROUND LEADING EDGE SCREW HOLE FORWARD OF INBOARD END OF OUTBOARD SLOT PANEL, RIGHT WING. REPAIRED IAW ABX REA D827-26073MR.Mar 9, 1999 · N802AX · Doug DC862 · Wing, Plate/SkinSDR 99T64R384ARSpar · corrodedNR 2569 - VERTICAL STABILIZER REAR SPAR LT TIP FAIRING ATTACH POINT ABOVE STA ZV299 HAS CORROSION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. DYE PENETRANT BLENDED AREA NO CRACKS EXIST, FLAP PEENED AND TREATED AREA PER EO 99-044 AND 99-061 WITH APPROVED FAA FORMMar 9, 1999 · N1808E · Doug DC862 · Vertical Stabilizer, Spar/RibSDR RRXA991475Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BL 36 LEFT BETWEEN STA 640 AND STA 720. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER REPAIR IAW DC8 SRM 51-1-Mar 6, 1999 · N995CF · Doug DC862 · Fuselage Floor PanelSDR ARWA990304Wheel · failedMIA - FLT 807 - BLOCK TURN BACK, AT THE BEGINNING OF TAKEOFF HEARD A LOUD NOISE FROM LEFT MLG WHEEL WELL. RETURNED TO RAMP. MAINTENANCE FOUND NR 6 MLG WHEEL INBOARD HALF FLANGE HAD SEPARATED AND TIRE WAS MISSING. WHEEL PARTS AND TIRE WERE RECOVERED. NR 6 MMar 6, 1999 · N802BN · Doug DC862 · Wheel/Ski/FloatSDR 99T64R376ARSkin · corrodedFOUND CORROSION ON SKIN BETWEEN STATION 1480-1500 LT AT L32L. REMOVED CORROSION, FABRICATED FILLERS, DOUBLERS AND INSTALLED PER EO 99-043, WITH APPROVED FAA FORM 8110-3 DATED 3-1-99. (M)Mar 5, 1999 · N1808E · Doug DC862 · Fuselage Main, Plate/SkinSDR 99T64R372ARPlate · corrodedFOUND CORROSION SKIN BETWEEN STATION 1480-1500 RT L28R. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOUBLERS AND INSTALLED PER EO 99-039. (M)Mar 5, 1999 · N1808E · Doug DC862 · Fuselage Main, Plate/SkinSDR 99T64R388ARSkin · misrepairedNR 1071 - EVALUATE SKIN REPAIR AND CORRECT IF REQUIRED BETWEEN L29L - L28L BETWEEN FRAMES 1340-1360 LT. REMOVED DAMAGED SKIN, FABRICATED FILLER AND DOUBLER AND INSTLLED PER EO 99-028. (M)Mar 5, 1999 · N1808E · Doug DC862 · Fuselage Main, Plate/SkinSDR ABXA9900290Web · corrodedDURING C-CHECK, FOUND UPPER CARGO COMPARTMENT RIGHT CUSP WEB AT STATION 477 CORRODED. REPAIRED CUSP WEB IAW ABX REA D853-26780MR.Mar 4, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous StructureSDR 99T64R271ARSkin · corrodedNR 0507 - TWO EACH, CORROSION BULGES AROUND FASTENERS LT WING LEADING EDGE LOWER SKIN INBOARD T/E XFS 297.500. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FILLER/DOUBLER AND INSTALLED PER EO 99-037 WITH APPROVED FAA FORM 8110-3 DATED 2-25-99. REF: ARMar 4, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R364ARPlate · corrodedLEFT HORIZ STAB LEADING EDGE CORROSION ALONG SCREW ROW TOP STATION XFS 166 TO 328. REMOVED CORROSION, FABRICATED FILLERS AND DOUBLERS AND INSTALLED PER EO 99-061 AND 99-025. (M)Mar 3, 1999 · N1808E · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR 99T64R382ARSkin · corrodedNR 0324 - TOP INBOARD STUB WING CORROSION AROUND SCREWS LT WING. REMOVED CORROSION, FABRICATED FILLERS AND DOUBLERS AND INSTALLED PER EO 99-027 AND 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)Feb 26, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R381ARSkin · corrodedNR 0281 - LT OUTBOARD LEADING EDGE CORROSION ON SKIN AROUND SCREWS. REMOVED CORROSION, FABRICATED FILLERS AND DOUBLERS AND INSTALLED PER EO 99-029 AND 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)Feb 26, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R366ARSkin · corrodedRIGHT WING OUTBOARD STUB WING UPPER TRAILING EDGE CORRODED BEYOND LIMITS XFS 566.250. REMOVED CORROSION, FABRICATED DOUBLER AND FILLER AND INSTALLED PER EO 99-032 AND 99-061. (M)Feb 25, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR ABXA9900291Pan · crackedDURING C-CHECK, FOUND CRACK IN FORWARD SERVICE DOOR PAN AT SECOND DOOR STOP FROM BOTTOM, FORWARD SIDE OF DOOR. REPAIRED IAW ABX REA D853-27050MR.Feb 24, 1999 · N802AX · Doug DC862 · Service DoorsSDR ABXA9900284Skin · crackedDURING C-CHECK, FOUND LOWER SURFACE OF RIGHT OUTBOARD LEADING EDGE CRACKED AT SCREW HOLES AT STATIONS FS 743, 746, 762, 765, 768, 771 AND 780. REPAIRED IAW DC8 SRM 57-2-1.Feb 24, 1999 · N802AX · Doug DC862 · Wing, Plate/SkinSDR ABXA9900283Skin · crackedDURING C-CHECK, FOUND CRACK IN FUSELAGE SKIN AT UPPER AFT CORNER OF LEFT AIRCRAFT PASSENGER DOOR CUTOUT. REPAIRED IAW DC8 SRM 53-2-0.Feb 24, 1999 · N802AX · Doug DC862 · Fuselage Main, Plate/SkinSDR ABXA9900282Skin · crackedDURING C-CHECK, FOUND SKIN CRACKED AT RIGHT AFT CORNER OF RIGHT FORWARD SERVICE DOOR CUTOUT. REPAIRED IAW DC8 SRM 53-2-0.Feb 24, 1999 · N802AX · Doug DC862 · Fuselage Main, Plate/SkinSDR ABXA9900274Angle · crackedDURING C-CHECK, FOUND NR 2 PYLON INBOARD VERTICAL ATTACH ANGLE CRACKED AFT OF FOOTSTOOL FITTING. REPAIRED IAW DC8 SRM 54-22.Feb 24, 1999 · N802AX · Doug DC862 · Nacelle/Pylon StructureSDR ABXA9900277Longeron · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION ON LONGERON 33 RIGHT AT STATION 1500. REPLACED LONGERON 33 RIGHT IAW DC8 SRM 51-1-21 AND 51-1-20D.Feb 23, 1999 · N802AX · Doug DC862 · Fuselage Main, Longeron/StringerSDR ABXA9900129Line · looseAFTER TAKEOFF AND PASSING 4000 FEET, THE HYDRAULIC RESERVOIR LOW PRESSURE LIGHT ILLUMINATED, ACCOMPANIED BY DECAYING FLUID QUANTITY. PERFORMED LOSS OF HYDRAULICS EMERGENCY CHECKLIST. TIGHTENED LOOSE LINE ON NR 2 HYDRAULIC PUMP. BLED SYSTEM, PERFORMED OPS ANFeb 22, 1999 · N801AX · Doug DC862 · Hydraulic System, MainSDR ABXA9900296Fitting · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION ON FRAME TO CUSP ATTACH FITTING AT STATION 1458 RIGHT. REPLACED FITTING IAW DC8 SRM 51-3-0 AND 51-1-21.Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9900295Frame · crackedDURING C-CHECK, FOUND FRAME CRACKED AT STATION 1180 RIGHT, AT FLOOR LEVEL. REPAIRED FRAME IAW DC8 SRM 53-2-0.Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Main, FrameSDR ABXA9900294Fitting · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION ON FITING AT 1180, RIGHT SIDE OF CUSP. REPLACED FITTING IAW DC8 SRM 51-3-0 AND 51-1-21.Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9900293Fitting · crackedDURING C-CHECK, FOUND FUSELAGE FRAME FITTING CRACKED AFT SIDE AT BOTTOM OF LONGERON 11 RIGHT, STATION 682. REPLACED FRAME FITTING IAW DC8 SRM 51-3-0 AND 51-1-21.Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
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