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 UPS06847468Odor · detectedELECTRICAL ODOR ON F/O'S SIDE OF COCKPIT TROUBLESHOOTING IN PROGRESS COULD NOT SMELL ANY TYPE OF ELECTRICAL ODOR WHEN OPERATING ALL FOUR ENGINES.Jul 28, 2006 · N807UP · Doug DC873F · Air Distribution SystemSDR IXXA06SMN241SStructure · misrepairedDURING ROUTINE C CHECK INSPECTION, EMPENNAGE RT HORIZONTAL STABILIZER INBD L/E FWD PART WITH NON STANDARD REPAIR, XFS 141.250 - XFS 147.500.Jul 28, 2006 · N605AL · Doug DC873F · Horizontal Stabilizer StructureSDR UPS06847710Skin · corrodedINSPECTION TYPE: C1-3 D-PIT BELLY SKIN REQUIRES REPLACEMENT DUE TO OUT OF LIMITS CORROSION AT L35R-36 STA 1490-1350. REMOVED AND REPLACED BELLY SKIN AT STA 1490-1350 L31L-L31R IAW SRM 51-1-20D, 51-1-21.Jul 27, 2006 · N806UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS06847465Fire Warning · false indicationDIVERSION, LOWER FWD CARGO FIRE WARNING DISPLAYED. RE-SET C/B B1-119 MAIN W/W AND FWD CARGO LIGHTS. OPS CHECK OK. THIS CLEARS D330218.Jul 27, 2006 · N801UP · Doug DC873F · Fire DetectionSDR UPS06847648Attach Fitting · crackedINSPECTION TYPE:C1/3 NR 1 MAIN TANK REAR SPAR ATTACH TEE FITTING AT XW-408 HAS A 4 INCH CRACK. REMOVED AND REPLACED ATTACH TEE FITTING AT XCW-408 NR1 MAIN TANK.Jul 26, 2006 · N806UP · Doug DC873F · Wing, Attach FittingsSDR IXXA060597SSkin · damagedDURING PRE-FLIGHT INSPECTION FOUND A HOLE ON THE RT IB FLAP TRAILING EDGE. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DRAWING NR AB84-57-100 DATED 7/28/06, AND DACO SRM 57-2-1.Jul 26, 2006 · N602AL · Doug DC873F · Trailing Edge FlapsSDR IXXXA060597SSkin · damagedDURING PRE-FLIGHT INSPECTION FOUND A HOLE ON THE RIGHT HAND INBOARD FLAP TRAILING EDGE. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS PER COTNEY DRAWING NUMBER AB84-57-100 DATED 7/28/06,Jul 26, 2006 · N602AL · Doug DC873F · Trailing Edge FlapsSDR UPS06847592Skin · corrodedINSPECTION TYPE:N/A COMPLY WITH DMI D-329976: FUSELAGE SKIN CORRODED AT STA 8 AND LONGERON 28R. REFERENCE UPS EO DC8 5330-24757-A DTD.7-25-06. REMOVED DAMAGED (CORRODED) AREA. FABRICATED AND INSTALLED REPAIR DOUBLERS, FILLERS, AND FINGER DOUBLERS AT STA 8 Jul 26, 2006 · N811UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS06847640Splice · crackedINSPECTION TYPE: C1,3 LONGERON SPLICE FITTING CRACKED AT STA 1260 TO 1280 L35L. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20DJul 25, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847418Skin · bulgedBULGED SKIN ON LOWER EXT SKIN AFT OF AC BAY. POPPED RIVETS. WILL FERRY (#9002) TO SAA FOR REPAIR. TRANS. TO NRC 123458 PLEASE VOID THIS ENTRY SEE UPS06847592 FOR CORRECTIVE ACTION COMPLETED BY SAT MAJOR MX.Jul 25, 2006 · N811UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA060480OTransmitter · failedDURING CRUISE FROM KSJC TO KRFD, THE NR 3 ENGINE LOW OIL PRESSURE LIGHT CAME ON. THE CREW RETARDED THE THROTTLE TO IDLE AND THE LIGHT REMAINED ON. THE ENGINE OIL PRESSURE, QUANTITY, AND TEMPERATURE WERE NORMAL. THE CREW DECIDED TO SHUT DOWN THE ENGINE AS A Jul 25, 2006 · N602AL · Doug DC873F · Engine Oil Indicating SystemSDR DHL2006807006Duct · looseLEFT PACK PRODUCED SMOKE IN COCKPIT NO DUCT OVERHEAT OR PACK TRIP. FOUND ACM DISCHARGE DUCT NO SECURED RESECURED DUCT OPS CHECK GOOD ACM OP CHECKS NORMAL IAW 21-55-1.Jul 22, 2006 · N807DH · Doug DC873F · Air Distribution SystemSDR UPS06847603Fitting · crackedINSPECTION TYPE:C1-3 60 HOLE APPROX STA 1800 LONGERON 24L END FITTING IS CRACKED. REMOVED DRILLED UP, AND INSTALLED END FITTING AT STA 1800 L24L IAW SRM 51-1-21, AND SRM 51-1-20D.Jul 21, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847574Longeron · crackedINSPECTION TYPE:C1-3 CRACKED LONGERON L34R FS 1270 IN C-PIT. REMOVED AND REPLACED LONGERON AT STA 1270 - 1350 L34R IAW SRM 51-1-20D.Jul 21, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2006809506Floorbeam · corrodedAFT ACCY COMPT FLOORBEAM CORRODED STA 1620.000 LBL 10". PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1 SHEET 9, 12, TR NR 51-130 DATE 06-26-04. REMOVED FASTENERS IAW SRM 51-1-20D. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PJul 20, 2006 · N809DH · Doug DC873F · Fuselage Main, Floor BeamSDR UPS06847651Drag Angle · crackedINSPECTION TYPE:C1, 3 POSSIBLE CRACKS ON BULKHEAD FWD OF CENTER SPAR UPPER BOLT IB DRAG ANGLE. REMOVED, FABRICATED AND INSTALLED DRAG ANGLE IAW SRM 51-1-21, DWG 5615767 AND 51-1-20D.Jul 19, 2006 · N806UP · Doug DC873F · Nacelle/Pylon, Main FrameSDR UPS06847379Longeron · crackedINSPECTION TYPE: C3 60 COMPT L17R HAS 3 INCH CRACK STA 1770 (GOING UNDER END FITTING). REMOVED LONGERON AT STA 1770 L17R. FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21, 51-1-20D, 51-3-0 AND 53-5-03 FIG 5.Jul 19, 2006 · N803UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847378Longeron · crackedINSPECTION TYPE: C3 COMPT 60 L17L HAS A 3 INCH CRACK STA 1770 (GOING UNDER END FITTING). REMOVED LONGERON, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-20D, 53-5-03 FIG 5.Jul 19, 2006 · N803UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2006809507Panel · crackedNR 4 PYLON INBD ADAPTER PANEL 1" CRACK STA YN 323.000 LT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 70 SB 54-93 CONDITION V. REMOVED FASTENERS FROM REPAIR AREA AND ATTACH PARTS IAW DC8 70 SB 54-93, SRM 51-1-21, SRM 51-3-0. FABRICATED DOUBLERS (4) (AL707Jul 18, 2006 · N809DH · Doug DC873F · Nacelle/Pylon Miscellaneous StructureSDR UPS06847521Longeron · crackedINSPECTION TYPE:C1-3 MAIN CABIN LONGERON END FITTING CRACKED AT STA 905 L9L. REMOVED AND REPLACED LONGERON END FITTING AT STA 905 L9L IAW SRM 51-1-20D, AND SRM 51-01-23-0.Jul 18, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847441Longeron Splice · crackedINSPECTION TYPE:C1-3 LONGERON SPLICE FITTING CRACKED AT STA 900 TO 920 L1. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 900 TO 920 LONGERON 1 IAW SRM 51-01-20D, AND SRM 51-01-20D.Jul 18, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847358Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY BATTERY PACK IAW AMM 33-50-01-2. EMERGENCY LIGHTS TEST SERVICEABLE IAW AMM 33-50-01-2. P/N ON 5708458-503, S/N ON FT002; P/N OFF 5708458-503, S/N OFF 368.Jul 18, 2006 · N867UP · Doug DC873F · Emergency LightingSDR DHL2006809508Skin · delaminatedLT WING NR 4 FLAP VANE INTERNAL SKIN DELAMINATED. REMOVED AND REPLACED NR 4 LT FLAP VANE IAW MM 27-51-14 PG 201-202. REFER TO NR 058548 FOR OPS CHECK.Jul 17, 2006 · N809DH · Doug DC873F · Trailing Edge FlapsSDR DHL2006809505Skin · damagedLT INBD FLAP UPPER SKIN HAS AN INTERIM REPAIR (STA XW 104.000 - 106.000). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED PANEL PLATING WITH EXISTING INTERIM REPAIR IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PANEL PLATING WITH PLATING (AL2024T3 0Jul 17, 2006 · N809DH · Doug DC873F · Trailing Edge FlapsSDR DHL2006809504Fitting · crackedNR 1 LT STUB WING FITTING 3" CRACK STA XW 454.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0. REMOVED CRACKED FITTING IAW SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-Jul 17, 2006 · N809DH · Doug DC873F · Wing Miscellaneous StructureSDR UPS06847583Longeron · crackedINSPECTION TYPE:C1-3 CRACKED LONGERON L35L FS 1270 C-PIT. REMOVED AND REPLACED LONGERON AT STA 1270 L35L IAW SRM 51-1-20D.Jul 17, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847581Longeron · crackedINSPECTION TYPE:C1-3 CRACKED LONGERON AT L36 FS 1270 IN C-PIT. REMOVED AND REPLACED LONGERON FROM STA 1270 - 1350 L36 IAW SRM 51-1-20D.Jul 17, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847522Finger Doubler · corrodedINSPECTION TYPE:C1-3 9 SHEARED RIVETS ON FINGER DOUBLER IN COCKPIT SUBFLOOR, STA -130 LBL 20. REMOVED CORRODED FINGER DOUBLER IN COCKPIT SUBFLOOR AT STA -130 LBL 20 IAW SRM 51-01-21. FABRICATED AND INSTALLED FINGER DOUBLER IN COCKPIT SUBFLOOR AT STA -130 LBLJul 17, 2006 · N806UP · Doug DC873F · Fuselage Main, StructureSDR UPS06847747Skin · corrodedINSPECTION TYPE:C1 3 HEAVY CORROSION BETWEEN FUSE SKIN AND FINGER DOUBLER AT STA 1670 L31R IN AFT ACC COMPT. REPAIRED FUSELAGE SKIN FROM FS 1660 TO 1680 IAW SAA EA 008-5330-01- A0329 REV A AND UPS RA DC8-53-20579.Jul 16, 2006 · N806UP · Doug DC873F · Fuselage Main, StructureSDR UPS06847639Fitting · crackedINSPECTION TYPE: C1, 3 CRACKED BATHTUB FITTING AT FS 270 L34R IN A-PIT. REMOVED AND REPLACED BATHTUB FITTING. IAW SRM 51-1-20DJul 15, 2006 · N806UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS06847638Longeron · corrodedINSPECTION TYPE: C1,3 AT STA. 270 L33L IS BLOWN OUT. REMOVED WEB, BATHTUB FITTING AND LONGERON. FABRICATED AND INSTALLED LONGERON, SPLICE FITTING,BATHTUB FITTINGS AND REPAIR ANGLES. IAW SRM 51-1-20D, 51-1-21,53-02-00 FIG. 10,51-3-2,53-02-02, DWG 9754913Jul 15, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847526Splice · crackedINSPECTION TYPE:C1-3 L31L AT STA 200 TO STA 180 SPLICE IS CRACKED. REMOVED AND REPLACED SPLICE FITTING AT STA 200-180 L31L IAW SRM 51-1-20D, AND SRM 51-03-02.Jul 15, 2006 · N806UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS06847646Doubler · brokenINSPECTION TYPE: C1/3 INTERNAL DOUBLER BROKEN AT 6:00 AND 12:00 POSITION UNDER EXTERIOR MAIN CARGO DOOR ACCESS PLATE FOR NR 4 LATCH FABRICATED AND INSTALLED -1 AND -2 INTERNAL DOUBLERS IAW SAA EA 008-5320-01-A0331 DTD.05 AUG 2006 MFG DRAWING NR 5772790-637 REVJul 14, 2006 · N806UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS06847584Shear Tie · crackedINSPECTION TYPE:C1-3 MAIN CABIN STA 1740 L14L SHEAR TIE CRACKED. REMOVED SHEAR TIE AT STA 1740 L14L IAW SRM 51-01-20D. FABRICATED AND INSTALLED SHEAR TIE AT STA 1740 L14L IAW SRM 51-03-02, 51-1-20D AND DWG 5772706.Jul 14, 2006 · N806UP · Doug DC873F · Fuselage Internal Mounting StructureSDR UPS06847547Cusp Web · crackedINSPECTION TYPE:C1 CUSP CORRODED AT STA 440 L21R AND POSSIBLE CRACK. HFEC INSP FOUND 1 INCH CRACK. CUT OUT DAMAGED AREA OF CUSP AT STA 370 - 479 IAW SRM 53-02-05-0 FIG 015A. INSTALLED CUSP SEGMENT AT STA 370 - 470 L21R IAW SRM 53-02-05-0 FIG 015.Jul 14, 2006 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06847439Seat Track · wornC1-3 FE'S FWD SEAT TRACK LOCK PINS HOLES WORN. REMOVED AND REPLACED FE'S FWD SEAT TRACK IAW SRM 51-03-00,51-01-22 AND SRM 51-03-00.Jul 14, 2006 · N806UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06847435Seat Track · wornC1-3 2ND OBSERVERS AFT SEAT TRACK LOCKPIN HOLES WORN. REMOVED AND REPLACED 2ND OBSERVERS AFT SEAT TRACK IAW SRM 51-3-0 51-01-24.Jul 14, 2006 · N806UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06847334Smoke Goggles · scratchedCAPT'S SMOKE GOGGLES SCRATCHED. REMOVED AND REPLACED CAPTAIN'S SMOKE GOGGLES. OK TO CONTINUE.Jul 14, 2006 · N852UP · Doug DC873F · Emergency EquipmentSDR UPS06847696Spar Cap · crackedINSPECTION TYPE:C1-3 LT MLG WHEEL WELL FRONT SPAR CAP STA 857 LBL 36 HAS A CRACK BETWEEN BOLTS. REPAIRED LT MLG WHEEL WELL FRONT SPAR CAP AT STA 857 LBL 36 IAW SAA EA NR 008-5710-01-A0299, UPS EO NR DC8-5710-24870, DOUGLAS DWG SRO 8570009.Jul 13, 2006 · N806UP · Doug DC873F · Wing SparSDR UPS06847641Longeron · corrodedINSPECTION TYPE: C1,3 AIR CONDITIONING COMPT, L36 IS CORRODED AND CRACKED AT STA.35. REMOVED, FABRICATED AND INSTALLED LONGERON AT FS 35 L36.Jul 13, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847582Fitting · crackedINSPECTION TYPE:C1-3 LONGERON END FITTING CRACKED AT STA 65 L31L. REMOVED AND REPLACED LONGERON END FITTING AT STA 65 L31L IAW SRM 51-3-0, 51-1-21, AND SRM 51-3-2.Jul 13, 2006 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06847527Rib · crackedINSPECTION TYPE:C1-3 LT CENTER WING L/E UPPER RIB CRACKED AT XFS 497. STOP DRILLED CRACKED RIB AT LT L/E WING STA XFS 497 IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED DOUBLERS ON RIB AT LT L/E WING STA XFS 497 IAW SRM 57-03-03 FIG 5, AND SRM 51-1-20D.Jul 13, 2006 · N806UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS06847447Rib · crackedRT CENTER L/E UPPER RIB AT XFS 415 IS CRACKED. STOP DRILLED CRACK ON RIB AT LT L/E STA XFS 415 IAW SRM 57-2-0. FABRICATED AND INSTALLED REPAIR ANGLES AT LT L/E STA XFS 415 IAW SRM 57-03-03 FIG 5 AND SRM 57-02-00.Jul 13, 2006 · N806UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS06847446Longeron · crackedINSPECTION TYPE:C1-3 RT AFT MAIN CABIN FS 1750 L14R CRACKED AT CANTED FRAME REMOVED CRACKED LONGERON SECTION AT STA 1750 L14R IAW SRM 53-02-02-0 FI FIG 10. FABRICATED AND INSTALLED LONGERON SECTION AT STA 1750 L14R IAW SRM 53-02-02-0 FIG 10, AND SRM 53-05Jul 13, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847444Rib · crackedLEFT WING CENTER L/E RIB CRACKED AT XFS 328. STOP DRILLED CRACK AT LT WING L/E RIB AT STA XFS 328 IAW SRM 51-03-02. FABRICATED AND INSTALLED REPAIR ANGLES AT LT L/E WING STA XFS 328 IAW SRM 57-03-03 FIG 5, AND SRM 57-02-00.Jul 13, 2006 · N806UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS06847438Rib · crackedLT CENTER LE UPPER RIB CRACKED AT XFS 304. STOP DRILLED CRACK ON RIB ANGLE IAW SRM 57-2-0 AT STA XFS 304. FABRICATED AND INSTALLED REPAIR ANGLES AT STA L/WING STA XFS304 IAW SRM 57-02-0, AND 51-01-20D.Jul 13, 2006 · N806UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS06847410Rib · crackedFOUND LT CTR LE UPPER RIB CRACKED AT XS 491. SET HOLE TERMINATED CRACK. FABRICATED AND INSTALLED 2. REPAIR DOUBLERS IAW SRM 57-02-00 FIG 002 SHT 2, 51-01-20D AND 51-1-15.Jul 13, 2006 · N806UP · Doug DC873F · Leading Edge DevicesSDR UPS06847409Rib · crackedINSPECTION TYPE:C1,3 LT WING CTR LE LWR IB CRACKED AT XFS 347. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-02-00 FIG 002, 57-02-03 FIG 005 AND 51-1-20D.Jul 13, 2006 · N806UP · Doug DC873F · Leading Edge DevicesSDR UPS06847407Rib · crackedRT CENTER LE UPPER RIB AT XFS 415 IS CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 002, 51-1-21 AND 51-1-20D. SAT PREVIOUSLY SENT THIS WRITEUP WITH WRONG TAIL NR.Jul 13, 2006 · N806UP · Doug DC873F · Leading Edge DevicesSDR UPS06847406Rib · crackedLT CENTER LE UPPER RIB CRACKED AT XFS 334. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLES 2 IAW SRM 57-02-00 FIG 002, 57-03-03 FIG 005 AND 51-1-20D.Jul 13, 2006 · N806UP · Doug DC873F · Leading Edge Devices
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