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 RRXA97026Axle · crackedEXCESSIVE NOSE WHEEL SHIMMY DURING TAXI AND LANDING. WHILE CHANGING LT NOSE TIRE FOUND AXLE CRACKED. WHILE CHANGING LT NOSE TIRE FOR NOSE WHEEL SHIMMY FOUND THE AXLE CRACKED. REMOVED AND REPLACED NLG PISTON-AXLE ASSEMBLY AND LT NOSE TIRE ASSEMBLY. INSTALLEFeb 6, 1997 · N8177U · Doug DC871F · Nose/Tail Landing Gear Strut/AxleSDR UPS97821955Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY LIGHTS DIDN'T TEST ON PREFLIGHT. REPLACED EMERGENCY LIGHT BATTERY PACK.Feb 5, 1997 · N772UP · Doug DC871F · Emergency LightingSDR UPS97822188Extrusion · crackedINSPECTION C-CHECK, RT WING LE OUTBOARD, OUTBOARD SIDE UNDER SLOTED DOOR EXTRUSION, CRACKED. FABRICATED REPAIR DOUBLER SHIM. REPLACEMENT ANGLE IAW REO 02750. ALODINED AND PRIMED IAW DC8 SRM 51-1-8D. INSTALLED REPAIR DOUBLER AND SHIM IAW REO 02750 AND INSTAJan 31, 1997 · N708UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS97822187Fitting · crackedINSPECTION C-CHECK, FLAP ATTACHED BOLTS AT STA 410.01 MAIN LEFT WING INBOARD AND OUTBOARD LEAKING. REMOVED FLAPS HINGE FITTING AND STRUCTURE TO ACCESS REPAIR AREA, CRACKED INNER AND OUTER VERTICAL STIFFENERS. REMOVED CRACKED LOWER BULKHEAD CAP FITTING, REAMEJan 29, 1997 · N708UP · Doug DC871F · Trailing Edge FlapsSDR UPS97822186Fitting · crackedINSPECTION C-CHECK, AFT PIT X SLIDE DOOR FWD TORQUE BOX HAS CRACKED Z FITTING, STA 1160 BETWEEN LONG 35R AND L34R. REMOVED Z FITTING, FABRICATED REPAIR ANGLES IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED Z FITTING AND REPAIRED ANGLEJan 28, 1997 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97822185Longeron · corrodedINSPECTION C-CHECK, LONG 29L CORRODED AT AFT PIT SLIDE DOOR FWD TORQUE BOX, STA 1150-1160. REMOVED DAMAGED LONG SECTION IAW DC8 SRM S53-2-2D. CUT EXTERNAL SKIN TO ACCESS LONGERON IAW DC8 SRM D53-2-1 FIG 7. FABRICATED NEW SKIN DOUBLER AND FILLER PER DC8 SRMJan 28, 1997 · N708UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS97822184Fitting · crackedINSPECTION C-CHECK, AFT LOWER CARGO, FS 1220, Z FITTING ON TORQUE BOX CRACKED APPROX 2.375 INCHES, BETWEEN LONG 32R AND 34R. REMOVED LONG SECTION ON LONG 32R AT FS 1220 TO ACCESS FITTING. ALODINED AND PRIMED ENDS OF CUT LONG IAW DC8 SRM 51-1-8. DRILLED AND Jan 28, 1997 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97822183Fitting · crackedINSPECTION C-CHECK, AFT LOWER FS 1220 Z FITTING CRACKED APPROX 2.75 AT LONGERON 34R. REMOVED CRACKED Z FITTING, FABRICATED NEW Z FITTING AND SPLICED PIECES IAW DC8 SRM 53-2 FIG 2G. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED WITH HI-LOKS IAW DC8 SRM 5Jan 28, 1997 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97822064Frame · corrodedINSPECTION TYPE-C/CK, STA 1600 FRAME CORRODED AND SPLICE FITTING CORRODED BETWEEN LONG 33L AND 33R. REMOVED FASTENERS, CORROSION, DAMAGED FRAME SECTION, FABRICATED NEW FRAME SECTION AND SPLICES, ALODINED AND PRIMED PARTS, INSTALLED NEW FRAME SECTION AND SPLJan 28, 1997 · N708UP · Doug DC871F · Fuselage Main, FrameSDR UPS97821927Skin · corrosionINSPECTION TYPE-C, REMOVED AND REPLACED BELLY SKIN AFT OF STA 1690. REMOVED AND REPLACED SKIN (P/N 5649329-75N2) IAW SRM 51-1-21 FROM STRINGER 28L TO 28R, BS 1690 TO 1890.Jan 28, 1997 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS97822182Skin · crackedINSPECTION C-CHECK, AFT FUSELAGE SKIN CRACKED APPROX 3 INCHES LONG, STA 1700 L17R. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND FILLER AND FINGER DOUBLERS IAW DC8 SRM 53-2-1 FIG 7. ALODINED AND PRIMED PARTS IAW DC8 SRM 51-1-8. INSTALLED AND SEALED REPAIR PAJan 27, 1997 · N708UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS97822181Skin · crackedINSPECTION C-CHECK, AFT 6 FUSELAGE SKIN CRACKED APPROX 1.5 INCHES LONG, STA 1734, L17L. FABRICATED FILLER PLATE, SKIN DOUBLER AND FINGER DOUBLERS IAW DC8 SRM 53-2-1D. ALODINED AND PRIMED PART AND SKIN IAW DC8 SRM 51-1-8. INSTALLED REPAIRED PARTS IAW DC8 SRMJan 27, 1997 · N708UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS97821966Fitting · crackedINSPECTION TYPE-C, HORIZONTAL FITTING AFT SIDE OF FRAME 822.5 AT STR 22L CRACKED. REMOVED DAMAGED FITTING IAW SRM 51-1-20, FABRICATED FITTING AND INSTALLED AT FRAME 822.5 OF STR 22L.Jan 25, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821894Fitting · crackedINSPECTION TYPE: C. HORIZONTAL FITTING CRACKED AT FWD SIDE OF FRAME 834.5 AT STR. 22R. REMOVED DAMAGED FITTING IAW SRM 51-1-20. FABRICATED FITTING AND INSTALLED AT FRAME IAW SRM 51-1-29D.Jan 25, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821911Intercoastal · crackedINSPECTION TYPE: C. NR 1 PIT STA 260-270 AT STR 33L INTERCOASTAL BETWEEN FRAMES HAS A HOLE AND 2 CRACKS IN RADIUS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-0.Jan 24, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821909Shear Tie · crackedINSPECTION TYPE: C. SHEAR TIE AT STA 1040 BETWEEN STR 31-32 CRACKED AT RADIUS. REMOVED DAMAGE, FABRICATED REPAIR PART AND INSTALLED IAW SRM 53-2-0 AND 51-1-20D.Jan 24, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821913Skin · crackedINSPECTION TYPE: C. LT WING CENTER L/E UPPER SKIN AT STA 339.5 IS CRACKED AT A SCREW HOLE, .7 INCHES LONG ON BOTH SIDES OF HOLE. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-2-1.Jan 23, 1997 · N706UP · Doug DC871F · Wing, Plate/SkinSDR UPS97821912Angle · crackedINSPECTION TYPE: C. LT WING L/E SLOT VANE ATTACH ANGLE I/B END IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM'S 51-1-21, 57-1-1, 51-1-4, 51-1-21, AND DOUGLAS DWG 5769891.Jan 23, 1997 · N706UP · Doug DC871F · Leading Edge DevicesSDR UPS97821848Catalytic Conv · cloggedINSPECTION TYPE-N/A, STRONG FUMES EYE BURNING/SMELL IN COCKPIT WHEN LEFT OR RIGHT PACK TURNED ON. TURNED BOTH PACKS OFF ONE AT A TIME AND RETURNED TO RFD. THE SMELL WAS VERY STRONG. UPON AIR TURNBACK, FOUND BOTH OZONE CATALYTIC CONVERTERS TO BE CLOGGED. DEJan 23, 1997 · N708UP · Doug DC871F · Cabin Cooling SystemSDR UPS97821869Angle · crackedINSPECTION TYPE: C. LT WING SECTION BETWEEN PYLONS AT CENTER AFT OF PART HAS L/E RIB SUPPORT ANGLE CRACKED ON LOWER AFT END. STOP DRILLED CRACK AND INSTALLED REPAIR IAW 57-2-0.Jan 22, 1997 · N706UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS97821836Coalescer Bag · contaminatedINSPECTION TYPE-N/A, BOTH LEFT AND RIGHT PACK PRODUCING DIESEL SMELL AND CAUSING EYE BURNING AND HEADACHE. SECURED RT PACK TO CONTINUE FLIGHT. SMELL VERY BAD WITH ANTI-ICE ON, SMELLS LIKE EXHAUST GAS. SUSPECT GROUND EQUIPMENT CONTAMINATION, FOUND WATER SEPAJan 22, 1997 · N708UP · Doug DC871F · Humidity Control SystemSDR UPS97821936Doubler · crackedINSPECTION TYPE-C, RT WING L/E INTERNAL LOWER DOUBLER AND STRAP CRACKED AT RIB XFS435. REMOVED DAMAGED AREA AND FABRICATED DOUBLER AND STRAP AND INSTALLED IAW SRM 51-1-21.Jan 21, 1997 · N706UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS97821929Skin · crackedINSPECTION TYPE-C, LT FUSELAGE SKIN BS 1746 LONGERON 16 WAS FOUND TO HAVE 3 CRACKS AFTER REMOVAL OF DOUBLERS. CUT OUT DAMAGED AREAS, INSTALLED FILLERS AND DOUBLERS IAW DHC SK 706 -117B REF, ENGINEERING FILE NR DC8-53-1736.Jan 21, 1997 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS97821928Skin · crackedINSPECTION TYPE-C, LT WING CENTER L/E SKIN AT STA XW258 IS CRACKED AT ONE FASTENER HOLE THE CRACK IS APPROX 1 INCH LONG. STOP DRILLED CRACK AND REPAIRED PER SRM ADDENDUM EO DC8-5720-7767-A.Jan 21, 1997 · N706UP · Doug DC871F · Wing, Plate/SkinSDR UPS97821915Fitting · crackedINSPECTION TYPE: C. FITTING AT STA 1090, STR 30R IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM'S 51-3-0 AND 51-1-21.Jan 21, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821905Stringer · corrodedINSPECTION TYPE: C. STA 1180 TO 1190 HAS CORROSION REMOVAL OUT OF LIMITS. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS DOUBLER, FILLER, AND SPLICE ANGLE AND INSTALLED IAW DHC SK706-731. REF UPS EFN FILE NR DC8-53-1735.Jan 20, 1997 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS97821945Fitting · crackedINSPECTION TYPE-C, STA 1690 STR 36 END FITTING IS CRACKED. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21.Jan 19, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821918Fitting · crackedINSPECTION TYPE: C. STA 1690 STR 25L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0, 51-1-21 51-1-20D.Jan 19, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821917Fitting · crackedINSPECTION TYPE: C. FUSELAGE STA 1690 LONGERON 33R END FITTING EXFOLIATED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-1-21.Jan 19, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821914Attach Fitting · crackedINSPECTION TYPE: C. ATTACH FITTING AT STR 24L, F.S. 1690 CRACKED ON UPPER FLANGE FASTENER HOLE. REMOVED AND REPLACED ATTACH FITTING PER SRM'S 53-1-0, 51-1-21, 51-1-20 D.Jan 19, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821864Longeron · crackedINSPECTION TYPE: C. STR 24L FWD OF STA 1690 IS CRACKED. REMOVED DAMAGED SECTION OF LONGERON STA 1675-1689, FABRICATED AND INSTALLED REPAIR SECTION IAW SRM 53-2-2, 53-4-1, AND 51-1-21.Jan 19, 1997 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS97821962Longeron · crackedINSPECTION TYPE-C, FS 1691, LONG 30R IS CRACKED. REMOVED AND REPLACED STR 30R FROM STA 1690 TO 1766 IAW SRM 53-2-2 FIG 10 AND SRM 51-3-0.Jan 18, 1997 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS97821961Longeron · corrodedINSPECTION TYPE-C, FS 1765, LONG 34R IS CORRODED. REMOVED AND REPLACED STRINGER 34R FROM STA 1690 TO 1766 IAW SRM 53-2-2 FIG 10 AND SRM 51-1-21.Jan 18, 1997 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS97821944Fitting · brokenINSPECTION TYPE-C, FUSELAGE STA 1690 STR 34R 2ND FITTING FLANGE BROKEN OFF. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-1-21.Jan 18, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821935Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB AT STA XFS 442.185 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND INSTALLED REPAIR PER DC8 SRM 57-2-0.Jan 18, 1997 · N706UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS97821868Rib · crackedINSPECTION TYPE: C. LT WING L/E SECTION BETWEEN PYLONS HAS UPPER L/E RIB CRACKED AT THE AFT END ABOVE SLOT ACTUATOR. STOP DRILLED CRACK AND INSTALLED REPAIR IAW DC8 SRM 57-2-0.Jan 18, 1997 · N706UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS97821867Rib · crackedINSPECTION TYPE: C. LT WING L/E SECTION BETWEEN PYLONS HAS LOWER L/E RIB CRACKED AT THE AFT END, BELOW AND AFT OF SLOT ACTUATOR. STOP DRILLED CRACK PER SRM 57-2-0 AND INSTALLED REPAIR IAW DC8 SRM 57-2-0.Jan 18, 1997 · N706UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS97821865Rib · crackedINSPECTION TYPE: C. LEFT WING L/E O/B SECTION HAS 1 EA LWR L/E RIB CRACKED INSIDE 2ND ACCESS PANEL O/B OF I/B END. STOP DRILLED CRACK . NDT VERIFIED CRACK TERMINATED. FABRICATED AND INSTALLED REPAIRS PER UPS SRM 57-2-0 FIG. 2 AND DC8 S.R.M. 06-00-00.Jan 17, 1997 · N706UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS97821934Splice · corrodedINSPECTION TYPE-C, AFT TEE CHORD SPLICE STA 1690 LBL 12 SEVERLY EXFOLIATED. REMOVED EXISTING SPLICE, FABRICATED REPLACEMENT SPLICE ANGLE IAW DWG 3642778, DRILLED AND INSTALLED IAW SRM 51-30-1.Jan 16, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821933Longeron · corrodedINSPECTION TYPE-C, LONGERON 36 CORRODED AT STA 1690. REMOVED CORRODED SECTION OF LONGERON 36 FROM STA 1690 TO STA 1730 PER SRM 53-2-2. FABRICATED AND REPLACED LONGERON PER SRM 53-2-2 AND 51-3-0.Jan 16, 1997 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA97012Drag Angle · damagedDURING MAINTENANCE VISIT, FOUND DRAG ANGLE (P/N 5803961-502) WITH SHEARED RIVETS AND DAMAGE, AT NR 4 PYLON XW=467 AND STRINGER 63. FABRICATED AND INSTALLED 7075T-6AL BUSHINGS IN STRINGER, WING SKIN, WING DOUBLER T-DOUBLER AND 17-7PH TH-170 BUSHING IN DRAG ANGJan 16, 1997 · N8091U · Doug DC871F · Wing Miscellaneous StructureSDR UPS97821939Angle · corrodedINSPECTION TYPE-C, ANGLE HAS EXFOLIATION CORROSION AT RT MLG W/W TOP FWD STA 858 AND STA 930. REMOVED CORROSION, FLAP PEENED, INSTALLED FREEZE PLUG AND REPAIRED STRAP PER DHC SK-706-663, REF UPS ENGINEERING FILE NR DC8-53-1734, DPS 4.999-2, AND SRM 51-1-8, SRJan 15, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821907Rib · crackedINSPECTION TYPE: C. LT WING O.B. L/E SECTION HAS 6 L/E RIBS CRACKED AT AFT END. STOP DRILLED L/E RIBS, FABRICATED AND INSTALLED REPAIR PARTS PER SR M 57-2-0 AND 51-1-20D.Jan 15, 1997 · N706UP · Doug DC871F · Wing, Rib/BulkheadSDR RRXA97018Beam · corrodedDURING A-MAINTENANCE VISIT, FOUND CORROSION DAMAGE ON BEAM (P/N 9779445) IN FORWARD CARGO COMPARTMENT, AT Y=320. ALSO, STRAP INSTALLED ON LWR HORIZONAL LEG OF BEAM HAD TO BE CUT OUT TO CLEAN-UP ALL CORROSION ON BEAM. TIMCO REO-02608 INSTALLED REPAIR ANGLE ASJan 15, 1997 · N8091U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA97006Skin · damagedA/C ARRIVED AT MCN ON FERRY FLIGHT FOR REPAIR OF 4' BY 5' HOLE WITH TEMPORY REPAIR AT Y=277 BELOW AND AFT OF MAIN CARGO DOOR. REMOVED TEMPORARY REPAIR, FABRICATED NEW DOUBLER AND INSTALLED REPAIR IAW PER APPROVED COTNEY ENGINE SKETCH B87-R02.Jan 15, 1997 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA009Jamb Frame · corrodedDURING C-CHECK, FOUND CORROSION DAMAGE ON JAMB FRAME (P/N 5750195) IN AFT CARGO COMPARTMENT BASKET DOOR AT Y= 1170 AND LONGERON 36. DAMAGE WAS REMOVED AND TRIMMED OUT. FABRICATED FILLER FROM 7075 AND REINFORCEMENT ANGLE FROM .080 7075-0, HEAT-TREATED TO T-6 Jan 15, 1997 · N8091U · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821940Doubler · corrodedINSPECTION TYPE-C, INTERNAL DOUBLER EXFOLIATED OUT OF LIMITS, VARIOUS AREAS FROM BS 1610 TO 1690 STRINGERS 25L TO 31L. REMOVED FASTENERS AND INTERNAL DOUBLER PER SRM 51-1-20. REMOVED CORROSION AND TREATED SKIN PER SRM 51-1-8. SKIN WITHIN LIMITS PER SRM 53-2-Jan 14, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA9700013Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, THE LOWER FORWARD CARGO DOOR RIGHT GUIDE FITTING WAS FOUND TO BE CRACKED. REPAIR ACCOMPLISHED BY REMOVAL OF EXISTING FITTING, FABRICATION AND INSTALLATION OF A NEW DOOR GUIDE FITTING IN ACCORDANCE WITH ENGINEERING ORDER 52-DJan 14, 1997 · N825BX · Doug DC871F · Cargo/Baggage DoorsSDR UPS97821941Fitting · corrodedINSPECTION TYPE-C, CENTER WING BOX UPPER SURFACE FWD RT CORNER FITTING HAS EXFOLIATION CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 10.Jan 13, 1997 · N706UP · Doug DC871F · Wing Miscellaneous StructureSDR RRXA97017Fitting · corrodedDURING A-MAINTENANCE VISIT, FOUND SEPARATOR NET SUPPORT FITTING (P/N 5711283-514) DAMAGED BEYOND ECONOMICAL REPAIR. REPLACEMENT PART UNAVAILABLE, BLANK FORGING UNAVAILABLE. TIMCO REO-02606 PROVIDES AUTHORITY TO FABRICATE NEW FITTING IAW DOUGLAS DRAWING NR 57Jan 13, 1997 · N8091U · Doug DC871F · Fuselage Miscellaneous Structure
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