Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = '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 RRXA003520Bulkhead · damagedDURING A MAINTENANCE VISIT FOUND GILLINER ATTACH ANGLE & BULKHEAD ATTACH HOLES BROKEN OUT ON THE AFT LWR CARGO BILGE AT STA 1320 AND L31L TO L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 12, 2000 · N795FT · Doug DC873F · Fuselage Main, BulkheadSDR RRXA003519Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE "C-PIT" DOOR FWD FRAME (DOOR COVER), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 12, 2000 · N795FT · Doug DC873F · Cargo/Baggage DoorsSDR RRXA003529Bracket · wornDURING A MAINTENANCE VISIT FOUND A WORN "T-BOLT" RETAINING BRACKET (TOP SIDE) NR 5 BOTTOM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 11, 2000 · N795FT · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA003528Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER "D-PIT" AT STA 1458-1466 AND L31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 11, 2000 · N795FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003527Skin · dentedDURING A MAINTENANCE VISIT FOUND NUMEROUS DENTS TO THE "C-PIT" DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 11, 2000 · N795FT · Doug DC873F · Cargo/Baggage DoorsSDR RRXA003526Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND FASTENERS & UNDER DOUBLER SPLICE AT STA 960 TO 980 TOP OF LONGERON 24L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 11, 2000 · N795FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003525Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE PRESS WEB & FITTING AT THE LT W/W STA 940 AND L24L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 11, 2000 · N795FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003524Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE BOTH SIDES OF DOUBLER SPLICE ON THE LT W/W BATHTUB FITTING AT STA 940 AND L24L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 11, 2000 · N795FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003523Cowling · dentedDURING A MAINTENANCE VISIT FOUND TWO DENTS ON THE NR 3 ENGINE NOSE COWL AT 6:30 AND 7 O'CLOCK POSITIONS, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 11, 2000 · N795FT · Doug DC873F · Engine Cowling SystemSDR DHL200080203CSupport · crackedAT C CHECK; MAIN CARGO COMPARTMENT LT CUSP LINE SUPPORT CRACKED 1/2 INCH NEAR UPPER CUSP EXTRUSION FS 1547.00. PERFORMED STOP DRILL IAW SRM 53-2-0 FIG 1B, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-3-0Dec 9, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2000801156Valve · failedNR 2 ENGINE ANTI ICE VALVE DOES NOT IND OPEN. DEFERRED THE NR 2 NOSE COWEL ANTI ICE VALVE PER MEL 30-20 CAT C, ASSIGNED DMI 3397.S/P 30-20 C/W, VALVE SECURED IN THE OPEN POSITION. STATUS - OPEN.Dec 9, 2000 · N801DH · Doug DC873F · Engine Anti-Icing SystemSDR RRXA003535Seat Track · tornDURING A MAINTENANCE VISIT FOUND A TEAR TO THE FLOOR TRACK 2ND FROM RT SIDE AT GALLEY SERVICE DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 8, 2000 · N795FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003534Seat Track · tornDURING A MAINTENANCE VISIT FOUND A TEAR TO THE FLOOR TRACK AT R21S AT STA 1590-1660, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 8, 2000 · N795FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003533Seat Track · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE CENTER FLOOR TRACK AT STA 320, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 8, 2000 · N795FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003532Seat Track · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE FLOOR TRACK 3RD FROM LT SIDE OF CABIN AT STA 400, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 8, 2000 · N795FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003531Seat Track · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE 1ST SEAT TRACK AT GALLEY SERVICED DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 8, 2000 · N795FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003530Bulkhead · damagedDURING A MAINTENANCE VISIT FOUND TORN OUT AND BENT SCREW HOLES TO THE AFT LWR CARGO COMPT RT BULKHEAD AT STA 1320, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 8, 2000 · N795FT · Doug DC873F · Fuselage Main, BulkheadSDR UPS00834556Coupling · leakingINSPECTION TYPE:N/A PIREP-FUEL LEAKING FROM RH WING ***SUPPLEMENTAL MRR*** FOUND GAMA COUPLING LEAKING RT INBD WING REPAIRED COUPLINGDec 8, 2000 · N801UP · Doug DC873F · Aircraft Fuel Distribution SystemSDR DHL200080223CAngle · brokenAT C CHECK; LWR FUSELAGE SHOWS ANGLE BROKEN STA 730.000 SPAR 33LT. REMOVED BROKEN ANGLE IAW SRM 51-3-0 PG 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED ANGLE IAW SRM 51-3-0, PG 1. REF: N/R 2347.Dec 7, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003803Gusset · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO GUSSETT AT STA 980 AND INSIDE RT MAIN GEAR WHEEL, 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 51-1-4.Dec 6, 2000 · N795FT · Doug DC873F · Wing, Attach FittingsSDR RRXA003536Strut · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN LANDING GEAR SHOCK STRUT ASSY RETRACT PIN BOSS & RETRACT PIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW MA-AI-32Dec 6, 2000 · N795FT · Doug DC873F · Main Landing Gear Strut/Axle/TruckSDR DHL200080233CAngle · crackedAT C CHECK; VERTICAL STAB. L/E INTERIOR ANGLE CRACKED (1/2 INCH) AT STA ZFS 179.750. PERFORMED STOP DRILL IAW SRM 55-2-0 FIG 2, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 55-2-0, FIG 2. REF: N/R 2811.Dec 6, 2000 · N802DH · Doug DC873F · Vertical StabilizerSDR DHL200080226CStructure · crackedAT C CHECK; FWD CARGO COMPT. REAR DOOR FWD LWR PART CRACKED 4 INCH. PERFORMED STOP DRILL IAW SRM 52-2-3 FIG 10A, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 52-2-3, FIG 10A. REF: N/R 2832.Dec 6, 2000 · N802DH · Doug DC873F · Cargo/Baggage DoorsSDR DHL200080225CFitting · crackedAT C CHECK; VERTICAL STABILIZER REAR SPAR TO FITTING CRACKED 2 INCHES, 2 RT 320.230. REMOVED FITTING IAW SRM 51-1-21 PG 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, INSTALLED FITTING IAW SRM 51-1-21 PG 1. REF: N/R 2342.Dec 6, 2000 · N802DH · Doug DC873F · Vertical Stabilizer, Attach FittingsSDR DHL200080217CStructure · wornAT C CHECK; RT WING TO FUSELAGE LOWER FAIRING 711 RIB DOUBLER WORN STA 610 XCW 63 RT. CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0, FIG 1F. REF: N/R 1832.Dec 6, 2000 · N802DH · Doug DC873F · Aerodynamic FairingsSDR RRXA003540Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE I/B SLOT PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 6, 2000 · N795FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003539Access Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER TANK UPPER LT ACCESS PANEL IN CABIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 6, 2000 · N795FT · Doug DC873F · Wing, Plate/SkinSDR RRXA003538Pressure Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON CEILING L/H MLG W/W Y AT STA 960 X-66, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 6, 2000 · N795FT · Doug DC873F · Fuselage Main, BulkheadSDR RRXA003537Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AT LONGERON 24 FITTING ON LOWER FOOT AT STA 940 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 6, 2000 · N795FT · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA001086Longeron · corrodedCORROSION AT 33R LONGERON STA 160 TO STA 180. ACCOMPLISHED TEMPORARY REPAIR PER M1206001 AND M1207001 REPAIR IS TO INSPECTED EVERY 50 CYCLES ACCOMPLISH PERMANENT SRM REPAIR NO LATER THAN 300 CYCLESDec 6, 2000 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL200080234CHinge · brokenAT C CHECK; LT WING I/B FLAP COVER UPPER PART SHOWS HINGE BROKEN AT STA 97. REMOVED AND REPLACED HINGE IAW SRM 51-1-21 PG 1. REF: N/R 1957.Dec 5, 2000 · N802DH · Doug DC873F · Trailing Edge FlapsSDR DHL200080205CPlate · crackedAT C CHECK; FWD PASSENGER DOOR THRESHOLD PLATE CRACKED. WELDED THRESHOLD PLATE IAW DPS 10.225. REF: N/R 0811.Dec 5, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080204CPlate · crackedAT C CHECK; RT REAR DOOR THRESHOLD PLATE CRACKED. WELDED THRESHOLD PLATE IAW DPS 10.229. REF: N/R 0802.Dec 5, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2000803139Fuse · unserviceableNO SPOILER PRESS DURING TAXI OUT RAN ALT PROCEDURE BUT NO CHANGE.R&R SPOILER PUMP CURRENT LIMITER OPS NORMAL PER M/M 27-62-00.Dec 5, 2000 · N803DH · Doug DC873F · Hydraulic Pressure IndicatorSDR RRXA003652Support · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO FLOOR SUPPORT ON L/H FLANGE AT STA Y-1745 AND BL-0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 Dec 4, 2000 · N603AL · Doug DC873F · Fuselage Main, Floor BeamSDR DHL200080224CDoor Frame · damagedAT C CHECK; LWR FUSELAGE NR 2 ACCESS DOOR FRAME BROKEN. REMOVED FRAME IAW SRM 51-1-21 PG 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED FRAME IAW SRM 51-1-21 PG 1. REF: N/R 2469.Dec 4, 2000 · N802DH · Doug DC873F · Fuselage Main, StructureSDR RRXA003541Skin · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BOTTOM T/E OF L/H ELEVATOR AT XE 60 TO XE 94, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Dec 4, 2000 · N795FT · Doug DC873F · Elevator, Plate/SkinSDR DHL200180257CStructure · crackedVERTICAL STAB L/E INTERIOR 1/2 INCH CRACK AT STA ZFS 123.000. STOP DRILLED CRACK PER SRM 55-2-0. FABRICATED DOUBLER PER SRM 55-2-0. CLEANED,TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 55-2-0Dec 3, 2000 · N802DH · Doug DC873F · Horizontal Stabilizer StructureSDR DHL200080227CWeb · crackedAT C CHECK; MAIN CARGO COMPT. RT CUSP LINE DEFORMED AND CRACKED 1/2 INCH AT STA 260. REMOVED RH CUSP LINE IAW SRM 53-2-0 FIG 1B, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED CUSP LINE IAW SRM 53-2-0 FIG 1B. REF: N/R 2831.Dec 3, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080231CCargo Track · wornAT C CHECK; MAIN CARGO COMPT. FLOOR TRACK 2 LT WORN AT STA FS 1585. CUTOUT AFFECTED AREA IAW SRM 53-2-3 PG 17&19, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED NEW TRACK IAW SRM 53-2-3 PG 17 & 19. REF: N/R 1411.Dec 2, 2000 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL200080221CFloor Support · crackedAT C CHECK; AFT CARGO COMPARTMENT FLOOR SUPPORT CRACKED STA 1280 BETWEEN LONGERON 35RH AND 35LH. REMOVED CRACKED FLOOR SUPPORT IAW SRM 51-1-21 PG 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-21. REF: N/R 2118.Dec 2, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003807Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LAV FLOOR PANEL AT STA 35-55 AND X=40 TO X=50, 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 Dec 1, 2000 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA003548Plate · gougedDURING A MAINTENANCE VISIT FOUND GOUGES IN TWO PLACES ON THE R/H HORIZ STAB RUB PLATE AFT SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Dec 1, 2000 · N795FT · Doug DC873F · Horizontal Stabilizer StructureSDR RRXA003547Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMGE ON RT CUSP AT Y-STA -55 X-66 Z-0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Dec 1, 2000 · N795FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003546Longeron · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LONGERON 24 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 1, 2000 · N795FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003545Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT LONGERON 24 AT SUPPORT FITTING AT STA 920 AND X-66 Y-920 Z-9, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 1, 2000 · N795FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003544Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TOP OF RT LONGERON 24 AT STA 902 X=59 Y=902 Z=10 INCH, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 1, 2000 · N795FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003543Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE NR 1 STRINGER ON THE RT WING UPPER SKIN AT STA 727, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 1, 2000 · N795FT · Doug DC873F · Wing, Plate/SkinSDR RRXA003542Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER RT WING CENTER SECTION L/E AT STA XFS 304, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Dec 1, 2000 · N795FT · Doug DC873F · Wing, Plate/SkinSDR RRXA003809Fairing · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H FLAP FAIRING AT STA. XW98, DAMAGE WITHIN ALLOWABLE LIMITS IAW DC-8 SRM 53-2-01F /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION Nov 30, 2000 · N795FT · Doug DC873F · Aileron Tabs
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