Douglas DC-8-73F

Service difficulty reports · 15,471

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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"

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SDR UPS05844461Brace · corrodedINSPECTION TYPE:C1 FLOORBEAM & BRACE APPEAR HEAVILY CORRODED IN COCKPIT SUBFLOOR AT FWD PRESSURE WEB STA -129 LBL 33. REMOVED FLOORBEAM BRACE, FABRICATED REPLACEMENT FLOORBEAM BRACE IAW DWG 5597992, AND INSTALLED IAW DC-8 SRM 51-1-20D.Apr 25, 2005 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844456Splice · crackedINSPECTION TYPE:C1 B-PIT BETWEEN STA 480-460 L31L SPLICE FITTING CRACKED. REMOVED CRACKED SPLICE FITTING, FABRICATED REPLACEMENT FITTING IAW DWG 3750257, AND INSTALLED IAW DC-8 SRM 51-1-20D.Apr 25, 2005 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844447Fitting · crackedINSPECTION TYPE:C1 C-PIT DOOR STOP FWD SIDE BANANA FITTING CRACKED AT STA 1180 L26L. REMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D, 51-1-21, AND 51-1-20A.Apr 25, 2005 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844446Fitting · crackedINSPECTION TYPE:C1 C-PIT DOOR CUTOUT BANANA FITTING CRACKED AT STA 1160 L32R. REMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D.Apr 25, 2005 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844444Fitting · crackedINSPECTION TYPE:C1 INSIDE DOOR 62 POGO STICK FITTING CRACKED .5 INCH LONG AT STA 1875 L36. REMOVED AND REPLACED POGO STICK FITTING IAW DC-8 SRM 51-1-20D AND 51-3 -0.Apr 25, 2005 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844439Fitting · crackedINSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 673 L8L. REMOVED AND REPLACED LONGERON END FITTING IAW DC-8 SRM 51-1-20D AND 51 -1-21.Apr 25, 2005 · N880UP · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2005807516Splice · crackedAFT CARGO COMPT SPLICE FITTING CRACKED 2.000 (STA 1040.000 - 1060.000, L-31L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TOApr 24, 2005 · N807DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2005807509Longeron · crackedAFT FUSELAGE SECTION L-17L CRACK 2.000 AT STA 1766.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5. REMOVED CRACKED LONGERON IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. FABRICATED NEW LONGERON (EXTRUSION 7075 Apr 24, 2005 · N807DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844455Fitting · crackedINSPECTION TYPE:C1 CRACKED FLOORBEAM FITTING AT A-PIT DOOR JAMB AT FS 340. REMOVED CRACKED FLOORBEAM FITTING, FABRICATED REPLACEMENT IAW DWG 975 4022, AND INSTALLED IAW DC-8 SRM 51-1-20D.Apr 24, 2005 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844506Longeron · corrodedINSPECTION TYPE: C1, SEVERE CORROSION ON FRAME/ANGLE AT FS 380 (LONGERON) LBL 33. REMOVED CORROSION ON LONGERON AND FOUND OUT OF LIMITS IAW DC-8 SRM 51-1-8. INSTALLED LONGERON SPLICE FITTING IAW DC-8 SRM 51-1-20D.Apr 23, 2005 · N880UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2005873001Line · leakingLOSS HYDRAULICS ON ROLL OUT AFTER LANDING HYDRAULIC LEVEL DROPPED TO AUX LEVEL. FOUND LT HYDRAULIC LINE ON BOGIE TRIM CAL. LEAKING ON LET GEAR. REMOVED AND REPLACED HYDRAULIC LINE IAW 32-33-1. SERVICED RESERVOIR, OPS AND LEAK CK OK LINE PIN 17001.Apr 23, 2005 · N873SJ · Doug DC873F · Hydraulic System, MainSDR UPS05844504Fitting · corrodedINSPECTION TYPE: C1, MAIN CABIN FRAME TO CUSP FITTING HAS HEAVY CORROSION AT STA 1580 L21L. REMOVED AND REPLACED CUSP FITTING AT STA 1580 L21L IAW DC-8 SRM 51-1-20D AND 51-3-0.Apr 22, 2005 · N880UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844464Fitting · corrodedINSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX AT STA 879.375 L20L SIDE FRAME FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED STA 879 FUSELAGE FRAME FITTING IAW DC-8 SRM 51-1-20D AND 51-1-21.Apr 22, 2005 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844463Finger Doubler · corrodedINSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX FINGER DOUBLER HAS SEVERAL SHEAR HEAD FASTENERS AND POSSIBLE CORROSION UNDER THE DOUBLER AT STA 865 BL 0. REMOVED FINGER DOUBLER AND FOUND OUT OF LIMITS, CENTER WING BOX PRESSURE WEB FOUND IN LIMITS AFTER CORROSIOApr 22, 2005 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844462Finger Doubler · corrodedINSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX SUBFLOOR FINGER DOUBLER HAS SHEAR HEAD FASTENERS AND POSSIBLE CORROSION UNDER THE DOUBLER AT STA 915 BL 0. REMOVED FINGER DOUBLER AND FOUND OUT OF LIMITS. CENTER WING BOX PRESSURE WEB FOUND WITHIN LIMITS AFTER COApr 22, 2005 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844452Longeron · crackedINSPECTION TYPE:C1 LONGERON CRACKED .5 INCH LONG AT STA 1746 L5R. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D.Apr 22, 2005 · N880UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844440Fitting · crackedINSPECTION TYPE:C1 A CARGO DOOR CUTOUT LOWER AFT BANANA FITTING HAS .5 INCH CRACK. REMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D.Apr 22, 2005 · N880UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844438Fitting · crackedINSPECTION TYPE:C1 A CARGO DOOR CUTOUT LOWER FWD BANANA FITTING CRACKED. REMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D AND 51-3-2.Apr 22, 2005 · N880UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844460Floorbeam · corrodedINSPECTION TYPE:C1 MAIN CABIN FLOORBEAM HEAVY CORRODED AT STA 1700 RBL 34. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. FABRICATED AND INSTALLED FLOORBEAM REPAIR IAW DC-8 SRM 53-2-0 FIG 1G, 51-1-20D, AND 51-3-0.Apr 21, 2005 · N880UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS05844459Angle · corrodedINSPECTION TYPE:C1 MAIN CARGO DOOR UNDER THRESHOLD 17 INCHES FWD OF AFT CUTOUT LWR ANGLE ATTACH JUST FWD OF AFT LATCH SPOOL HAS EXFOLIATION CORROSION. REMOVED AND REPLACED ANGLE IAW DC-8 SRM 51-1-21 AND 51-3-0.Apr 21, 2005 · N880UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS05844458Longeron · crackedINSPECTION TYPE:C1 LONGERON CRACKED .5 INCH LONG AT STA 1746 L16L. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10.Apr 21, 2005 · N880UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844457Attach Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN AT STA 1280 L18R FRAME ATTACH FITTING CRACKED .5 INCH LONG. REMOVED CRACKED FITTING, FABRICATED REPLACEMENT FITTING IAW DWG 475041 9, AND INSTALLED IAW DC-8 SRM 51-1-20D.Apr 21, 2005 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844453Attach Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN STA 1230 L18R FRAME ATTACH FITTING .5 INCH CRACK. REMOVED CRACKED FITTING, FABRICATED REPLACMENT FITTING IAW DWG 4750419, AND INSTALLED IAW DC-8 SRM 51-1-20D.Apr 21, 2005 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844451Longeron · crackedINSPECTION TYPE:C1 LONGERON CRACKED 1 INCH LONG AT STA 1746 L15L AND STA 1726 L15L. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTINGS IAW DC-8 SRM 53-2-2 FIG 10 AND 51-3-2.Apr 21, 2005 · N880UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844450Longeron · crackedINSPECTION TYPE:C1 LONGERON 14R CRACKED .25 INCH LONG AT STA 1757. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D.Apr 21, 2005 · N880UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844449Longeron · crackedINSPECTION TYPE:C1 LONGERON 15R CRACKED 1 INCH LONG AT STA 1757. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D.Apr 21, 2005 · N880UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844448Longeron · crackedINSPECTION TYPE:C1 RIGHT LONGERON 16R CRACKED 2 INCHES LONG AT STA 1756. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D.Apr 21, 2005 · N880UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844445Attach Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN AT STA 1160 L19R FRAME ATTACH FITTING CRACKED .5 INCH LONG. REMOVED AND REPLACED FRAME ATTACH FITTING IAW DC-8 SRM 51-1-20D.Apr 21, 2005 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844441Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN AT STA 1160 L18R FRAME ATTACH FITTING CRACKED 1 INCH LONG. REMOVED AND REPLACED FRAME ATTACH FITTING IAW DC-8 SRM 51-1-20D.Apr 21, 2005 · N880UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844437Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN STA 1180 L20R FRAME ATTACH FITTING CRACKED .5 INCH LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.Apr 21, 2005 · N880UP · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2005801006Plug · looseRT GEAR DOOR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION WENT OUT AFTER APPROX 2 MINUTES INTERMITTENT AFTER THAT UNTIL UPLATCH CHECK WHEN IT REMAINED OFF. INSPECTED RT GEAR DOOR SWITCH FOUND DEUTCHE PLUG NOT LATCHED, CLEANED AND RESECURED PLUG PERFORMED DOApr 21, 2005 · N801DH · Doug DC873F · Landing Gear Position and WarningSDR DHL2005807506Skin · damagedRIGHT RUDDER EXTERNAL SKIN INTERIM REPAIR (STA ZR 253.000 - 265.218). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-6-1 PG 2. REMOVED PLATING SEGMENT WITH INTERIM REPAIR ON IT IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING SEGMENT AND FINGER DOUBLER (AL2Apr 20, 2005 · N807DH · Doug DC873F · Rudder, Plate/SkinSDR DHL2005807514Cargo Track · deterioratedMAIN CARGO COMPT NR 2 TRACK LUGS DETERIORATED, STA 1210.000. CUT OUT NR 2 TRACK DAMAGED SECTION IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED AND TREATED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND PLUG IAW SRM 53-2-3, SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1.Apr 20, 2005 · N807DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005807513Cargo Track · deterioratedMAIN CARGO COMPT NR 3 TRACK LUGS DETERIORATED, STA 863.000. CUT OUT NR 3 TRACK DAMAGED SECTION IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED AND TREATED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND PLUG IAW SRM 53-2-3, SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1.Apr 20, 2005 · N807DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005807512Cargo Track · wornMAIN CARGO COMPT NR 2 TRACK LUG WORN, STA 689.000. CUT OUT NR 2 TRACK DAMAGED SECTION, STA 689.000 IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED AND TREATED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND PLUG IAW SRM 53-2-3 SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1.Apr 20, 2005 · N807DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005807500Frame · crackedNR 1 LT STUB WING FORMER CRACK 0.500, STA XW 540.000. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. PERFORMED STOP HOLE AND FABRICATED REINFORCING ANGLE (ALCLAD 7075-T6 0.063) IAW SRM 57-2-0. CLEANED, TREATED AND PRIMED REINFORCING ANGLE AND AREA IAW SRM 51-1-8Apr 19, 2005 · N807DH · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844436Rib · crackedINSPECTION TYPE: C1, RT WING L/E UPPER RIB CRACKED 1 INCH LONG AT XFS 841.25. REPAIRED IAW DC-8 SRM 57-3-3 AND SRM 51-1-21.Apr 19, 2005 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844366Fitting · corrodedINSPECTION TYPE: C1, TEE BOLT FITTING FROM A-PIT DOOR STA 285 HAS CORROSION AND MISDRILLED HOLES. REMOVED AND REPLACED TEE BOLT FITTING IAW SRM 51-3-0 & 51-1-20D.Apr 18, 2005 · N810UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS05844314Battery Pack · inoperativeEMERGENCY LIGHTS BATTERY INOP. REMOVED AND REPLACED BATTERY PACK PER DC-8 AMM CH 33-50-01-2, OPS GOOD.Apr 15, 2005 · N867UP · Doug DC873F · Emergency LightingSDR UPS05844282Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHTS BATTERY DEAD. REMOVED AND REPLACED BATTERY PACK PER DC-8 AMM CH 33-50-01-2. OP CHECKS GOOD.Apr 15, 2005 · N867UP · Doug DC873F · Emergency LightingSDR DHL2005807504Bracket · crackedNR 1 ALT TANK BOOSTER PUMP FWD BRACKET CRACKED. REMOVED CRACKED BRACKET AND INSTALLED A NEW ONE IAW SRM 51-1-20D PG 21-9. TORQUED NUT IAW SRM 51-3-1 PG 2A.Apr 14, 2005 · N807DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2005807503Frame · crackedRIGHT WING INBOARD L/E UPPER FORMER 0.250 CRACK, STA XFS 207.500. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. PERFORMED STOP HOLE AND FABRICATED REINFORCING ANGLE (AL7075T6 0.050) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND REINFORCING ANGLE Apr 14, 2005 · N807DH · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844376Floorboard · corrodedMAIN CABIN , CORROSION ON FLOORBOARD STA 1560,1600 AND 1660, LBL35. REMOVED CORROSION FOUND OUT OF LIMITS, INSTALLED REPAIR DOUBLERS IAW 51-1-8, 53-02-00, 53-02-03 FIG 10 AND 51-1-21.Apr 12, 2005 · N810UP · Doug DC873F · Fuselage Floor PanelSDR UPS05844310Floorboard · corrodedINSPECTION TYPE:C1 REMOVED CORROSION ON FLOORBOARD F86 AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0, 53-2-3 FIG 10, AND 51-1-8.Apr 12, 2005 · N810UP · Doug DC873F · Fuselage Floor PanelSDR UPS05844285Floorboard · corrodedINSPECTION TYPE: C1, LOWER SURFACE OF CABIN FLOORBOARD CORRODED FROM STA 1555 TO 1563 & BL 0 TO RBL 9. BLENDED OUT OF LIMITS AND REPAIRED IAW SRM 53-02-03, 51-1-8, 51-1-21, 51-3-0 AND 51-1-15.Apr 12, 2005 · N810UP · Doug DC873F · Fuselage Floor PanelSDR UPS05844270Engine · flamed outNR 4 ENGINE FLAME OUT IN CRUISE FLT ENROUTE TO PHL. RESTART UNSUCCESSFUL. FUEL PRESSURE ON S/O PANEL DROPPED FROM 35 PSI TO 20 OIL TEMP & QTY NORMAL OIL PRESS DROPPED TO 18 PSI AFTER FLAMEOUT. R&R NR 4 ENGINE, MAIN ENGINE CONTROL (MEC) IAW MM 73-20-01-4. PERFApr 12, 2005 · N809UP · Doug DC873F · Engine (Turbine/Turboprop)SDR DHL2005807501Cargo Track · wornMAIN CARGO COMPT NR 5 TRACK LUGS WORN STA 1680.000. CUT OUT TRACK DAMAGED SEGMENT AND FABRICATED SPLICES (AL7075T6 0.160) (AL7075T6 0.125) (AL7075T6 0.100) IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLEApr 11, 2005 · N807DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS05844301Spar · crackedINSPECTION TYPE: C2, FOUND POSSIBLE CRACK JUST I/B OF XCW 46 ON LOWER FRONT SPAR CAP VERTICAL ANGLE INSIDE RT CTR FUEL TANK. NDT VERIFIED CRACK APPROX 3 INCH LONG PER NDTSPM 06=10-01.001. CRACK RUNS FROM FASTENER HOLE TO FASTENER HOLE. REPAIRED CRACK IAW DCApr 11, 2005 · N819UP · Doug DC873F · Wing SparSDR UPS05844289Skin · crackedINSPECTION TYPE:C2 C-PIT DOOR UPPER AFT CORNER HAS CRACK IN FIRST FASTENER HOLE ABOVE FITTING ATTACH LIP UNDER INTERIOR SKIN. REPAIRED C-PIT DOOR IAW DC-8 SRM 52-2-0 FIG 2.Apr 10, 2005 · N819UP · Doug DC873F · Cargo/Baggage DoorsSDR DHL2005807502Cargo Track · damagedMAIN CARGO COMPT NR 4 TRACK LUGS DETERIORATED STA 1700.000. CUT OUT DAMAGED SECTION AND FABRICATED SPLICES (AL7075T6 0.160) (AL7075T6 0.125) (AL7075T6 0.100) IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTAApr 8, 2005 · N807DH · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
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