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 UPS07850639Door · looseINSPECTION TYPE:N/A CAPT ESCAPE ROPE DOOR LOOSE, ROPE FELL OUT. ROLLED, INSTALLED ESCAPE ROPE. RESECURED ESCAPE ROPE DOOR, OK TO CONTINUE.Sep 11, 2007 · N802UP · Doug DC873F · Emergency EquipmentSDR UPS07850636Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK PER MM 33-50-01-2. OPS CHECKS NORMAL.Sep 10, 2007 · N851UP · Doug DC873F · Emergency LightingSDR UPS07850635Battery Pack · faultyINSPECTION TYPE:N/A DURING PREFLIGHT EMERGENCY LIGHTS BATTERY CHARGING C/B POPPED AND WOULD NOT RESET. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK PER MM 33-50-01-2. SYSTEM OPS CHECKS GOOD.Sep 8, 2007 · N812UP · Doug DC873F · Emergency LightingSDR UPS07850683Skin · corrodedINSPECTION TYPE:C1 CORROSION ON FUSELAGE EXTERIOR L35L, STA 1075. REPAIRED DAMAGED EXTERIOR FUSELAGE SKIN AT STA L35L, STA 1075 IAW SAA EA 008-5330-01-A1087, UPS RAA DC8-53-20656, AND FAA FORM 8100-9.Sep 6, 2007 · N874UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07850620Control Panel · inoperativeINSPECTION TYPE:N/A F/E PANEL EMERGENCY CONTROL LIGHT PANEL HAS 4 OR 6 LIGHTS INOP. DEF 358150 ASSIGNED. *SDR FILED OPEN* DEFERRED F/E EMERGENCY ELECT CONTROL LIGHTING PANEL REF MEL 33-1 PART REQ A 847094.Sep 6, 2007 · N807UP · Doug DC873F · Emergency LightingSDR IXXA070045OEngine · overtempDURING CLIMB-OUT FROM KTOL, THE CREW PERFORMED MAX POWER TAKEOFF TO COMPLY WITH SEVEN DAY REQUIREMENT. NR ONE EGT WENT TO 906 FOR 2 SECONDS AFTER ROTATION, (N1 POWER SET FOR MAX 91.5 AFTER ROTATION N1 INCREASED TO 93.0 AND EGT FOLLOWED). NUMBER 4 EGT WENT TOSep 6, 2007 · N605AL · Doug DC873F · Engine (Turbine/Turboprop)SDR UPS07850684Angle · corrodedINSPECTION TYPE:N/A REFER TO LOG PAGE 657107. UPON REMOVAL OF CAPT SIDE WINDOW FOUND CORROSION ON LOWER ZEE ANGLE. BLENDED ZEE ANGLE IAW MM IAW SRM 53-20.Sep 5, 2007 · N809UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07850621Slide · out of positionESCAPE SLIDE ON CAPTAIN'S SIDE FELL OUT. 10-8-07 REINSTALLED CAPTAIN'S ESCAPE TAPE (ROPE) AND LINING IAW DC8 MM 25-61-13-04.Sep 5, 2007 · N851UP · Doug DC873F · Escape SlideSDR UPS07850707Shear Tie · crackedINSPECTION TYPE:C2 SHEAR TIE CRACKED AT STA 1080 BETWEEN L22L AND L23L. REMOVED AND REPLACED SHEAR TIE AT STA 1080 L22L AND L23L IAW SRM 51-1-20D AND DWG 3750891.Sep 4, 2007 · N801UP · Doug DC873F · Fuselage Internal Mounting StructureSDR UPS07850723Frame · corrodedINSPECTION TYPE:C2 TAIL CONE LWR NAV LIGHT LENS FWD FRAME HEAVILY CORRODED AT STA 1973. REPAIRED TAIL CONE LOWER NAV LIGHT LENS FORWARD FRAME IAW SRM 51-01- 04, DWG 5704663-3, SRM 53-05-03, SRM 51-1-8 AND SRM 51-1-21.Aug 31, 2007 · N801UP · Doug DC873F · Aerodynamic FairingsSDR UPS07850604Skin · gougedINSPECTION TYPE:C2 LEFT ELEV UPPER SKIN GOUGED VERY INBOARD SIDE. DRILLED UP DAMAGED AREA ON LEFT ELEV UPPER SKIN IAW SRM 55-02-00 FIG 006. PLUGGED HOLE IN LEFT ELEV UPPER SKIN IAW SRM 55-02-00 FIG 006.Aug 30, 2007 · N801UP · Doug DC873F · Elevator, Plate/SkinSDR UPS07850603Skin · puncturedINSPECTION TYPE:C2 LEFT ELEV LWR SKIN PUNCTURED VERY INBOARD SIDE. DRILLED OUT DAMAGED AREA FOR REPAIR IAW SRM 55-02-00 FIG 006. PLUGGED HOLE ON LEFT ELEV SKIN IAW SRM 55-02-00 FIG 006.Aug 30, 2007 · N801UP · Doug DC873F · Elevator, Plate/SkinSDR UPS07850551Light · inoperativeEMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2 AND CHECKS GOOD PER SAME.Aug 29, 2007 · N819UP · Doug DC873F · Emergency LightingSDR UPS07850535Light · inoperativeEMERGENCY LIGHTS ON AT POWER TRANSFER, WOULD NOT GO OUT. 09-07-07 RESET DC EMERGENCY BREAKER. SYTEM OPS CKS OK REF MM 33-50-00-0.Aug 29, 2007 · N811UP · Doug DC873F · Emergency LightingSDR UPS07850659Fitting · gougedINSPECTION TYPE:C2 FLOORBEAM END FITTING HAS LARGE GOUGE AND CUT IN THE SIDE AT FS 8 AND RBL 30. REMOVED, FABRICATED AND INSTALLED FLOORBEAM END FITTING IAW SRM 51-01-20D, DWG 3895627, SRM 51-1-8, SRM 51-3-0 AND SRM 51-3-2.Aug 26, 2007 · N801UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS07850497Light · inoperativeINSPECTION TYPE:N/A FRONT FWD ENTRANCE EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT, OPS CHECK OK PER MM 33-50-02.Aug 25, 2007 · N810UP · Doug DC873F · Emergency LightingSDR UPS07850711Skin · chafedINSPECTION TYPE:C2 L1 DOOR OUTSIDE DOOR HANDLE IS CHAFING ON DOOR EXTERNAL SKIN. REPAIRED L1 DOOR SKIN HANDLE CUTOUT IAW UPS EO DC8-5210-8162.Aug 23, 2007 · N801UP · Doug DC873F · Passenger/Crew DoorsSDR UPS07850710Intercostal · crackedINSPECTION TYPE:C2 WEB UNDER BAYONET FITTING IS CRACKED, L-1 DOOR. REMOVED, FABRICATED, AND INSTALLED WEB INTERCOSTAL UNDER BAYONET FITTING ON L-1 DOOR IAW DWG 5615403, AND SRM 51-01-20D.Aug 22, 2007 · N801UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07850709Stiffener · crackedINSPECTION TYPE:C2 FITTING CRACKED AT TOP OF VERTICAL STAB SPAR, BETWEEN LT AND RT SPAR CAPS. REPAIRED STIFFENER ON VERTICAL STAB SPAR IAW DWG 4651109 AND SRM 51-1-20 D.Aug 22, 2007 · N801UP · Doug DC873F · Vertical Stabilizer Miscellaneous StructureSDR UPS07850663Spar Cap · corrodedINSPECTION TYPE:C2 CORROSION ON VERTICAL STAB REAR SPAR CAP, RIGHT SIDE NEAR STA ZR=100. REPAIRED DAMAGED SPAR CAP ON VERTICAL STAB REAR SPAR CAP AT STA ZR=100 IAW SAA EA 008-5520-01-A1067, UPS RAA DC8-55-20108, AND FAA FORM 8100-9.Aug 22, 2007 · N801UP · Doug DC873F · Vertical Stabilizer, Spar/RibSDR UPS07850662Spar Cap · corrodedINSPECTION TYPE:C2 EXFOLIATING CORROSION ON VERTICAL STAB RIGHT AFT SPAR AT STA ZV299. REPAIRED DAMAGED VERTICAL STAB SPAR CAP AT STA ZV299 IAW SAA EA 008- 5520-01-A1074, UPS RAA DC8-55-20110, AND FAA FORM 8100-9.Aug 22, 2007 · N801UP · Doug DC873F · Vertical Stabilizer, Spar/RibSDR UPS07850537Longeron · corrodedINSPECTION TYPE:C2 STA 1766 L28R CORROSION OUT OF LIMITS. REMOVED L28R FROM STA 1690-1766 IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT LONGERON L28R AT STA 1690-1766 IAW SRM 53-05-03 AND SRM 51-1-21.Aug 22, 2007 · N801UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07850665Fitting · crackedINSPECTION TYPE:C2 LEFT INBOARD FLAP ACTUATOR FITTING IS CRACKED, STA 97. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR FITTING AT STA 97 IAW DWG 7981564, AND DC8 AMM 20-16-00.Aug 21, 2007 · N801UP · Doug DC873F · Wing, Attach FittingsSDR UPS07850595Skin · dentedINSPECTION TYPE:C2 LEFT ELEV UPPER SKIN DENTED AT T/E STA XE200. CUT OUT DAMAGED AREA ON LEFT ELEV STA XE 200 IAW SRM 55-02-01 FIG 10. FABRICATED AND INSTALLED REPAIR DOUBLER AT LEFT ELEV STA XE 200 IAW SRM 55-02-01 FIG 10. CALCULATED WEIGHT AND BALANCE IAWAug 21, 2007 · N801UP · Doug DC873F · Elevator, Plate/SkinSDR UPS07850594Skin · dentedINSPECTION TYPE:C2 RIGHT ELEV UPPER SKIN DENTED AT STA XE 200. CUT OUT DAMAGED AREA ON RIGHT ELEV SKIN AT STA XE 200 IAW SRM 55-02-01, FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XE 200 IAW SRM 55-02-01-0. CALCULATED WEIGHT AND BALANCE IAW SRM 51-04-08-0 Aug 21, 2007 · N801UP · Doug DC873F · Elevator, Plate/SkinSDR UPS07850590Seat Track · damagedINSPECTION TYPE:C2 COCKPIT 1ST OBSERVERS SEAT TRACK HOLES ARE ELONGATED AT STA -32. REMOVED AND REPLACED 1ST OBSERVERS SEAT TRACK AT STA -32 IAW SRM 51-03-00, AND SRM 51-01-24.Aug 21, 2007 · N801UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07850583Skin · cutINSPECTION TYPE:C2 LEFT ELEV UPPER SKIN CUT AT T/E NEAR STA XE 147. CUT OUT DAMAGED AREA AT LEFT ELEV UPPER SKIN STA XE 147 IAW SRM 55- 02-01. FABRICATED AND INSTALLED REPAIR DOUBLER AT LEFT ELEV UPPER SKIN STA XE 147 IAW SRM 55-04-01, AND SRM 55-02-01.Aug 21, 2007 · N801UP · Doug DC873F · Elevator, Plate/SkinSDR UPS07850582Finger Doubler · corrodedINSPECTION TYPE:C2 COCKPIT SUBFLOOR FINGER DOUBLER CORRODED OUT OF LIMITS AT STA -80. REMOVED COCKPIT SUBFLOOR FINGER DOUBLER AT STA -80 IAW SRM 51-01-21. FABRICATED AND INSTALLED REPAIR FINGER DOUBLER AT STA -80 IAW DWG 5612298, AND SRM 51-1-20D.Aug 21, 2007 · N801UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07850575Skin · dentedINSPECTION TYPE:C2 4 DENTS ON LEFT ELEV UPPER SKIN BETWEEN STA XE 36 AND XE 57. DRILLED OUT DENTS ON LEFT ELEV UPPER SKIN AT STA XE 35 AND XE 36 IAW SRM 55-02-00. FABRICATED AND INSTALLED REPAIR DOUBLER AT LEFT ELEV STA XE 35-XE 36 IAW SRM 55-02-01-0 FIG 010Aug 21, 2007 · N801UP · Doug DC873F · Elevator, Plate/SkinSDR UPS07850538Doubler · failedINSPECTION TYPE:C2 FOUND INTERNAL DOUBLER CUT IN TWO PLACES L28R, STA 1720. REMOVED INTERNAL DOUBLER AT STA 1720, L28R IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR INTERNAL DOUBLER AT STA 1720 L28R IAW DWG 5649328, AND SRM 51-1-21.Aug 21, 2007 · N801UP · Doug DC873F · Fuselage Main, StructureSDR IXXA07SMN224SStructure · misrepairedDURING ROUTINE C CHECK INSPECTION, FS 1345, LONGERON 30.5 LEFT. DOUBLER BELOW AND AFT OF AFT EMERGENCY EXIT DOOR. REPAIR NUMBER 606 AL-R36. PROBLEM: SIDE 2, 2ND ROW EXCEEDS MAS RIVET SPACING. DISPOSITION: ADD RIVETS TO BRING INTO LIMITS OR UPGRADE.Aug 21, 2007 · N606AL · Doug DC873F · Fuselage Main, StructureSDR IXXA07SMN223SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO LT CUSP EXTRUSION, FITTING WITH CORROSION AT STA 80.000, L-21L.Aug 21, 2007 · N606AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN225SLongeron · misrepairedDURING ROUTINE C CHECK INSPECTION, FS 1367, LONGERON 30.5 LEFT, DOUBLER BELOW AND AFT OF AFT EMERGENCY EXIT DOOR. REPAIR NUMBER 606AL-R37. PROBLEM: SIDE 2 ENDS ON LONGERON WITHOUT FINGER DOUBLER. DISPOSITION: UPGRADE IAW SRM.Aug 21, 2007 · N606AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07850637Attach Fitting · corrodedINSPECTION TYPE:C2 SUBFLOOR ATTACH FITTING HEAVY CORROSION AROUND BOLT AREA AT STA 920 RBL 65. REMOVED AND REPLACED SUBFLOOR ATTACH FITTING AT STA 920 AND RBL 65 IAW SRM 51-03-02-0, SRM 51-3-0, SRM 51-1-20D, AND SRM 51-1-8.Aug 20, 2007 · N801UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07850584Slide · unserviceableINSPECTION TYPE:C2 ESCAPE SLIDE HAS FRAYED AREAS ALONG GIRT BAR AND DUE DATE STICKER NOT READABLE. REMOVED AND REPLACED NEW EMERGENCY ESCAPE SLIDE.Aug 20, 2007 · N801UP · Doug DC873F · Escape SlideSDR UPS07850597Doubler · chafedINSPECTION TYPE:C2 OVERSIZED HOLE, 2 SHEARED RIVETS IN CHAFE STRIP AND ATTACH FLANGE ON I/B END OF LEFT HORIZONTAL STAB L/E. REMOVED OUTER RUB STRIP DOUBLERS ON I/B END OF LEFT HORIZONTAL STAB L/E IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLERS ANDAug 18, 2007 · N801UP · Doug DC873F · Horizontal Stabilizer Miscellaneous StructureSDR UPS07850588Fitting · crackedINSPECTION TYPE:C2 CRACK ON L17L END FITTING, 60 COMPT STA 1772. REMOVED AND REPLACED LONGERON END FITTING AT STA 1772 L17L IAW SRM 51-01-20D, 51-03-02-0, AND SRM 51-1-11.Aug 17, 2007 · N801UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA07SMN217SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT AFT FITTING SHOWS CRACK 2" BETWEEN STA 1220.000 AND L-19R. REPLACED CRACKED FITTING WITH NEW FITTING IAW DC8 SRM 51-1-20D.Aug 17, 2007 · N606AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN222SSpar · crackedDURING ROUTINE C CHECK INSPECTION, NR 2 MAIN TANK WEB OF CENTRAL SPAR (LWR SIDE) CRACKED 2 1/2" AT STA XRS 172.000 BETWEEN S-61 AND S-62.Aug 17, 2007 · N606AL · Doug DC873F · Wing SparSDR IXXA07SMN212SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING INBD FLAP UPPER SKIN SHOWS DENT AT XW 88.000.Aug 17, 2007 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA07SMN211SLongeron Splice · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT LONGERON SPLICE FITTING CRACKED AT STA 1690.000 L-36.Aug 17, 2007 · N606AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA07SMN221SSpar Cap · crackedDURING ROUTINE C CHECK INSPECTION, NR 2 MAIN TANK LOWER CAP OF CENTER SPAR 3" CRACKED AT STA ZRS 172.000 BETWEEN S-61 AND S-62.Aug 17, 2007 · N606AL · Doug DC873F · Wing SparSDR IXXA07SMN214SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, LT HORIZONTAL STABILIZER, POINTS OF CORROSION ON UPPER SKIN FROM STA XE 28.843 TO STA XE 30.000.Aug 17, 2007 · N606AL · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR IXXA07SMN216SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT FWD FITTING SHOWS CRACK 1" BETWEEN STA 1152.000 AND L-20R.Aug 17, 2007 · N606AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN218SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT AFT FITTING SHOWS CRACK 2" AT STA 759.000 AND L-18.8L.Aug 17, 2007 · N606AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN215SFitting · crackedDURING ROUTINE C CHECK INSPECTION, RT HORIZ STABILIZER FITTING SHOWS CRACK 2" FRONT PART AT STA NFS 60.000.Aug 17, 2007 · N606AL · Doug DC873F · Horizontal Stabilizer, Attach FittingsSDR IXXA07SMN220SSpar · crackedDURING ROUTINE C CHECK INSPECTION, NR 1 MAIN TANK CTR SPAR WEB LWR SIDE, CRACK 4" AT STA XRS 255.000 BETWEEN S-61 AND S-62.Aug 17, 2007 · N606AL · Doug DC873F · Wing SparSDR IXXA07SMN219SSpar · crackedDURING ROUTINE C CHECK INSPECTION, NR 1 MAIN TANK, CTR SPAR LWR CAP, CRACKED 3" AT STA XRS 255.000 BETWEEN S-61 AND S-62.Aug 17, 2007 · N606AL · Doug DC873F · Wing SparSDR IXXA07SMN213SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING INNER FLAP, UPPER SKIN SHOWS DENT BETWEEN STA XF 112.000 TO STA XF 120.000.Aug 17, 2007 · N606AL · Doug DC873F · Trailing Edge FlapsSDR UPS07850705Cusp Web · damagedINSPECTION TYPE:C2 CUSP HAS DEEP BLEND OUT AT L21L AT STA 1130. REPAIRED CUSP AT STA 1130 L21L IAW SRM 53-02-05-0.Aug 16, 2007 · N801UP · Doug DC873F · Fuselage Miscellaneous Structure
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