Douglas DC-8-71F

Service difficulty reports · 8,938

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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 = 'DC871F'
  ORDER BY difficulty_date DESC"

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SDR UPS01836570Fitting · corrodedINSPECTION TYPE:C1/3 AFT PIT FS 1220 L32R-L33R ZEE FITTING HAS CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND MAT'L OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED FITTING IAW DC8 SRM 51-1-20D. RECEIVED NEW FITTING P/N 3755840-1 LOCATED AND DRILLED HOLES IAWJul 12, 2001 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836519Floor Support · corrodedINSPECTION TYPE:C1/3 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT.Jul 12, 2001 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836479Fitting · corrodedINSPECTION TYPE:C1/3 STA 1220 L35L TO L34L Z FITTING CORRODED. REMOVED AND REPLACED FITTINGJul 12, 2001 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836523Seat Track · corrodedINSPECTION TYPE:C1/3 SEAT TRACK E AT STA 980 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK.Jul 10, 2001 · N750UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS01836343Seat Track · corrodedINSPECTION TYPE:C1,3 STA 470 TRACK G HAS CORROSION DOWN CTR. FOUND TO BE BEYOND ALLOWABLE LIMITS IAW DC8 SRM 53-2-3 FIG 12.Jul 10, 2001 · N750UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS01836341Intercostal · crackedINSPECTION TYPE:C1,3 INTERCOSTAL CRACKED IN FWD END OF UPPER RADIUS LONG 31L STA 1620 - 1640 AFT ACCESSORY COMPT.Jul 10, 2001 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836217Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK.Jun 30, 2001 · N755UP · Doug DC871F · Emergency LightingSDR UPS01836191Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY PACK DISCHARGED. REMOVED AND REPLACED EMERGENCY BATTERY PACK, CKS OK P/N ON-OFF 5708458-503, S/N OFF FT L 158 ON 2085.Jun 25, 2001 · N797UP · Doug DC871F · Emergency LightingSDR RRXA010054Accumulator · failedSPOILER PUMP INOP. FOUND SPOILER ACCUMULATOR BLADDER BLOWN AND SPOILER RESERVIOR EMPTY. REMOVED AND REPLACED SPOILER ACCUMULATOR AND SERVICED SPOILER RESERVOIR IAW MM 29-12-02. SPOILER PUMP OP CK GOOD IAW M/M 27-63-25.Jun 23, 2001 · N8085U · Doug DC871F · Drag Control SystemSDR UPS01836162Tire · wornINSPECTION TYPE:N/A BTB - REJECTED TAKEOFF AT80 KIAS DUE TO VIOLENT SHAKING AND THUMPING SOUNDS DURING TAKEOFF ROLL. SUSPECTED BLOWN NOSE TIRE. FOUND LEFT AND RIGHT NOSE TIRES WORN UNEVEN. SUSPECT OUT OF ROUND PER MM 32-50-00. REMOVED AND REPLACED LEFT ANDJun 22, 2001 · N706UP · Doug DC871F · TireSDR 0100037OWarning System · activatedPRIOR TO ROTATION AIRCRAFT EXPERIENCED ABNORMAL EXHAUST GAS TEMPERATURE INDICATION. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO PARKING. NO FURTHER ABNORMALITIES OCCURRED.Jun 20, 2001 · N824BX · Doug DC871F · Engine EGT/TIT Indicating SystemSDR UPS01836203Skin Panel · corrodedINSPECTION TYPE:C2 RIGHT RUDDER PANEL IS CORRODED BEYOND LIMITS AT ZR 253. REMOVED, FABRICATED, AND REPLACED SKIN IAW DWG 5655077 AND EO M-5100-11491-B.Jun 14, 2001 · N705UP · Doug DC871F · Rudder, Plate/SkinSDR UPS01836061Control Column · lack of lubeINSPECTION TYPE:N/A DURING FLIGHT CONTROL CHECK ELEVATOR EXHIBITED NON-UNIFORM MOVEMENT WHICH RELEASED FROM FORWARD POSITION AS YOKE TRAVELED FROM ITS MOST FWD POSITION AFT STOP AFT IT STOPPED ITS TRAVEL FOR 1-2 SECONDS FROM CONTINUED TO NORMAL POSITION *S/D*Jun 12, 2001 · N709UP · Doug DC871F · Control Column SectionSDR UPS01836074Rib · crackedINSPECTION TYPE:C2,3 LEFT WING OUTBOARD L/E RIBS ARE CRACKED AT XFS 722.5, XFS 728.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Jun 8, 2001 · N705UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS01836073Rib · crackedINSPECTION TYPE:C2,3 LEFT WING OUTBOARD L/E RIBS ARE CRACKED AT XFS 791.25, XFS 755.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Jun 8, 2001 · N705UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS01836072Rib · crackedINSPECTION TYPE:C2,3 LEFT WING O/B RIB IS CRACKED AT XFS 653. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Jun 8, 2001 · N705UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS01836133Fitting · crackedINSPECTION TYPE:C2,3 RIGHT HORIZONTAL STAB T-FITTING AT I/B LOWER SECTION FWD OF FRONT SPAR IS CRACKED AT APPROX 47.5. REMOVED AND REPLACED FITTING IAW DWG 3701427 AND SRM 51-1-20D, 51-1-21.Jun 7, 2001 · N705UP · Doug DC871F · Horizontal Stabilizer StructureSDR UPS01836131Intercostal · crackedINSPECTION TYPE:C2,3 RIGHT WING CENTER L/E INTERCOSTAL IS CRACKED AT XS 454.976. REMOVED AND REPLACED INTERCOSTAL IAW DWG 5769857 AND SRM 57-1-0, 51-1-20D, 51-1-21.Jun 7, 2001 · N705UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS01836023Pump · leakingINSPECTION TYPE:N/A HYD LOSS DOWN TO APPROX 6 GAL BYPASSED PUMPS. RAN LOSS OF HYD FLUID OR PRESS AND WAS ABLE TO CONFIGURE WITH GEAR AND FULL FLAPS - FLUID LEAKING AFTER LANDING RT SIDE R-R RUDDER STANDBY PUMP PN 57155A. OPS AND LEAK CHECKED OK. DURINJun 7, 2001 · N706UP · Doug DC871F · Hydraulic Pump, AuxiliarySDR IXXA0100036OHinge Pin · wornIN ROUTE FROM RDU TO TOL AFTER GEAR RETRACTION LANDING GEAR DOOR UNSAFE LIGHT ILLUMINATED. FLIGHT CREW CYCLED THE LANDING GEAR, WARNING INDICATION REMAINED THE SAME. FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENACE INSPECTED THE LANDING GEAR WHICHJun 6, 2001 · N826BX · Doug DC871F · Landing Gear Position and WarningSDR UPS01836210Skin Panel · corrodedINSPECTION TYPE:C2 RUDDER TRAILING EDGE IS CORRODED BEYOND LIMITS AT APPROX ZR 168 P/N 5655077-80, JUST ABOVE RUDDER TAB. REMOVED, FABRICATED AND REPLACED RUDDER SKIN PANEL IAW DWG 5655077 AND SRM 51-1-21.Jun 6, 2001 · N705UP · Doug DC871F · Rudder, Plate/SkinSDR UPS01836209Frame · corrodedINSPECTION TYPE:C2 STA 1400 FRAME IS CORRODED BEYOND LIMITS AT LONG 35R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.Jun 6, 2001 · N705UP · Doug DC871F · Fuselage Main, FrameSDR UPS01836208Frame · corrodedINSPECTION TYPE:C2 STA 1360 FRAME IS CORRODED BEYOND LIMITS AT LONG 36. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.Jun 6, 2001 · N705UP · Doug DC871F · Fuselage Main, FrameSDR UPS01836207Frame · corrodedINSPECTION TYPE:C2 STA 1340 FRAME IS CORRODED BEYOND LIMITS AT LONG 36. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.Jun 6, 2001 · N705UP · Doug DC871F · Fuselage Main, FrameSDR UPS01836202Fitting · crackedINSPECTION TYPE:C2 STA 1150 AT LONG 33R BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847 AND SRM 51-1-20D.Jun 6, 2001 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836201Fitting · crackedINSPECTION TYPE:C2 STA 1260-1280 LONG 34R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759222 AND SRM 51-1-20D.Jun 6, 2001 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836198Fitting · crackedINSPECTION TYPE:C2 STA 1228 LONG 31R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754916 AND SRM 53-1-0, 51-1-20D.Jun 6, 2001 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836196Splice · crackedINSPECTION TYPE:C2 STA 1260 - 1280 LONG 35L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759258 AND SRM 51-1-20D, 51-1-21.Jun 6, 2001 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836127Fitting · corrodedINSPECTION TYPE:C23 STA 1160 LONG 35L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755845 AND SRM 53-2-0 FIG 2D.Jun 6, 2001 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836065Splice · crackedINSPECTION TYPE:C2,3 STA 1040 - 1060 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 53-1-0, 51-1-20D.Jun 6, 2001 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836064Splice · crackedINSPECTION TYPE:C2,3 STA 1040 - 1060 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 53-1-0, 51-1-20D.Jun 6, 2001 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836130Doubler · brokenINSPECTION TYPE:C2,3 RIGHT WING OUTBOARD L/E STUB WING LOWER INTERNAL DOUBLER IS BROKEN AT XOLDO 67.5. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5802736 AND SRM 57-2-1 FIG 14A.Jun 5, 2001 · N705UP · Doug DC871F · Wing, Plate/SkinSDR UPS01836128Splice · crackedINSPECTION TYPE:C2,3 STA 380 - 400 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 53-1-0, 51-1-20D.Jun 5, 2001 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836067Doubler · crackedINSPECTION TYPE:C2,3 RIGHT WING OUTBOARD L/E UPPER INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 57-1-0, 51-1-20D, 51-1-21.Jun 5, 2001 · N705UP · Doug DC871F · Wing, Plate/SkinSDR UPS01836066Rib · crackedINSPECTION TYPE:C2,3 RIGHT WING OUTBOARD L/E HAS CRACKED UPPER RIB AT XFS 572.5, AND LOWER RIB AT XFS 566.25. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Jun 5, 2001 · N705UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS01836204Doubler · corrodedINSPECTION TYPE:C2 STA -60 AT LBL 53 SUBFLOOR FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5612298 AND SRM 51-1-20D, 51-1-21.Jun 4, 2001 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836200Fitting · crackedINSPECTION TYPE:C2 STA 1190 LONG 21R RT CUSP TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754918 AND SRM 51-1-20D, 51-3-0.Jun 4, 2001 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836068Rib · damagedINSPECTION TYPE:C2,3 RIGHT WING OUTBOARD L/E RIB WEB IS TORN AT XW 761. REMOVED, FABRICATED, AND REPLACED WEB IAW DWG 5769467 AND SRM 57-1-0, 51-1-21.Jun 4, 2001 · N705UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS01836063Skin · corrodedINSPECTION TYPE:C2,3 RIGHT WING INBOARD L/E LOWER SKIN HAS INTERGRANULAR CORROSION AT XFS193. REPAIRED SKIN IAW EO DC8-5720-7767-A.Jun 4, 2001 · N705UP · Doug DC871F · Wing, Plate/SkinSDR UPS01836212Seat Track · damagedINSPECTION TYPE:C2 MAIN CABIN SEAT TRACK HAS BROKEN SCALLOPS AND PLUG GOUGED BETWEEN STA 765-781 LBL 24. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.Jun 3, 2001 · N705UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS01836211Seat Track · damagedINSPECTION TYPE:C2 MAIN CABIN SEAT TRACK SCALLOPS ARE BROKEN AT STA 1600 RBL 48. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.Jun 3, 2001 · N705UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS01836206Seat Track · corrodedINSPECTION TYPE:C2 MAIN CABIN SEAT TRACK IS CORRODED BEYOND LIMITS AT STA 610 LBL 59. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.Jun 3, 2001 · N705UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS01836205Skin · corrodedINSPECTION TYPE:C2 STA 61-63 INNER SKIN IS CORRODED BEYOND LIMITS, BETWEEN LONG 36 AND LONG 35R. REPAIRED SKIN IAW 8110-3 APPROVED DH SK 705-086.Jun 3, 2001 · N705UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS01836199Fitting · crackedINSPECTION TYPE:C2 STA 804 RIGHT KEEL BEAM FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750727 SRM 51-1-20D, 51-1-21, 51-3-0.Jun 3, 2001 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS01836197Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XW 0. REPAIRED SKIN IAW SRM 57-2-1 FIG 20.Jun 3, 2001 · N705UP · Doug DC871F · Wing, Plate/SkinSDR UPS01836129Skin · crackedINSPECTION TYPE:C2,3 RIGHT WING UPPER SKIN IS CRACKED AT STA XW 402 AT STRINGER 10. REPAIRED SKIN IAW SRM 57-2-1 FIG 21.Jun 3, 2001 · N705UP · Doug DC871F · Wing, Plate/SkinSDR UPS01836075Skin · crackedINSPECTION TYPE:C2,3 LEFT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 10. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.Jun 3, 2001 · N705UP · Doug DC871F · Wing, Plate/SkinSDR UPS01836071Skin · crackedINSPECTION TYPE:C2,3 TRANSFERRED FROM LOG PAGE 9645247, REF DMI D-188382 CRACK ON LEFT WING L/E OUTBOARD OF NR 2 PYLON AT XW 257. REPAIRED SKIN IAW DC8-5720-4087 APPX C.Jun 1, 2001 · N705UP · Doug DC871F · Wing, Plate/SkinSDR IXXA0100026Door · out of rigEN ROUTE FROM TOL TO BDL, THE LANDING GEAR DOOR UNSAFE WARNING LIGHT ILLUMINATED AFTER A SUCCESFUL GEAR UP LATCH CHECK WAS PERFORMED. THE FLIGHT RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE MAIN LANDING GEAMay 25, 2001 · N826BX · Doug DC871F · Landing Gear Door Retract SectionSDR IXXA0100052SLongeron · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON LONGERON 36 AT FUSELAGE STATION 621. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION NEW LONGERON SPLICE FITTING IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINMay 18, 2001 · N822BX · Doug DC871F · Fuselage Main, Longeron/Stringer
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