Douglas DC-8-73F

Service difficulty reports · 15,471

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Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS02838653Fitting · crackedINSPECTION TYPE:C1 AFT PIT FS 1160 C3 DOOR RAMP PANEL SUPPORT FITTING AT L27L L36 IS CRACKED. REMOVED SUPPORT FITTING LOCATED AND DRILLED HOLES IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.May 29, 2002 · N803UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838650Fitting · crackedINSPECTION TYPE:C1 AFT PIT FS 1160 C3 DOOR RAMP PANEL SUPPORT FITTING AT L27L - L34 IS CRACKED. REMOVED SUPPORT FITTING LOCATED & DRILLED HOLES IAW DC8 SRM 51-1-24 INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.May 29, 2002 · N803UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838590Skin · crackedINSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB CORNER CRACKED AT FASTENER HOLE EXTERNAL FUSELAGE SKIN LENGTH APPROX .25 TO .3125 INCH LONG. FOUND BY EDDY CURRENT. REPAIRED DOOR JAMB IAW DC8 SRM 53-2-0 FIG 16.May 28, 2002 · N803UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS02838623Seat Track · crackedINSPECTION TYPE:C1 MAIN CABIN STA STA 1334 AND BL 0 SEAT TRACK IS CRACKED. R&R DAMAGED SECTION OF SEAT TRACK IAW UPS EO DC8-5320-5767May 27, 2002 · N803UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS02838622Fitting · crackedINSPECTION TYPE:C1 LONGERON FITTING CRACKED STA 680-11R. R&R FITTING IAW DC8 MM 51-1-21 & 51-1-24.May 27, 2002 · N803UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838618Floorbeam · chafedINSPECTION TYPE:C1 FLOORBEAM AT STA 717 CHAFED BETWEEN RBL 0-24. REPAIRED FLOORBEAM IAW DC8 SRM 53-2-0 TR 53-124.May 27, 2002 · N803UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS02838593Plate · crackedINSPECTION TYPE:C1 MCD AFT VERT SCUFF PLATE AND DOUBLER ARE CRACKED STA 272 AND L10L. FABBED DOUBLER IAW DC8 SRM 51-1-8, INSTALLED DOUBLER IAW DC8 SRM 51-1-21.May 27, 2002 · N803UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS02838592Floorbeam · chafedINSPECTION TYPE:C1 FLOORBEAM AT STA 742 CHAFED BETWEEN RBL 0-24. REPAIRED FLOORBEAM IAW DC8 SRM 53-2-0 TR 53-124.May 27, 2002 · N803UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS02838591Floorbeam · chafedINSPECTION TYPE:C1 FLOORBEAM AT STA 759 CHAFED BETWEEN RBL 0-24. REPAIRED FLOORBEAM IAW DC8 SRM 532-0 TR 53-124.May 27, 2002 · N803UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS02838657Skin · dentedINSPECTION TYPE:C1 DENT IN RT HORIZ STAB LE 35 INCHES O/B AT ROOT. REMOVED DAMAGED AREA DENT FOUND TO BE OUT OF LIMITS. FABBED REPAIR DOUBLER IAW SRM 55-2-1. INSTALLED DOUBLER IAW SRM 51-1-21.May 26, 2002 · N803UP · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR UPS02838621Floorbeam · corrodedINSPECTION TYPE:C1 MAIN CABIN FLOORBEAM CORRODED AROUND NUTPLATE STA 980 LBL 10. REPLACED SECTION OF FLOORBEAM CAP IAW DC8 SRM 53-2-0 TR 53-124May 26, 2002 · N803UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS02838687Longeron · crackedINSPECTION TYPE:C1, LONGERON 36 IS CRACKED UNDER FLANGE AT APPROX FS 1272. REMOVED LONGERON SECTION, 2 LONGERON SPLICES, SPLICES FOUND IN LIMITS IAW 53-2-0. LOCATED & DRILLED NEW LONGERON SECTION, INSTALLED NEW LONGERON SECTION AND 2 LONGERON SPLICE IAW DC8 May 25, 2002 · N803UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS02838686Longeron · crackedINSPECTION TYPE:C1 AFT PIT FS 1480 L34L LONGERON IS CRACKED. REMOVED CRACKED LONGERON AND REPLACED LONGERON SECTION IAW DC8 SRM 53-2-2 FIG 4A & 51-1-20D.May 25, 2002 · N803UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS02838659Longeron · crackedINSPECTION TYPE:C1 LONGERON 36 CRACKED UNDER FLANGE AT APPROX FS 1272. REMOVED LONGERON SECTION (2) LONGERON SPLICES, SPLICES FOUND TO BE IN LIMITS IAW SRM 53-2-0. LOCATED & DRILLED NEW LONGERON SECTION, INSTALLED NEW LONGERON SECTION AND 2 LONGERON SPLICES May 25, 2002 · N803UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS02838658Longeron · crackedINSPECTION TYPE:C1 AFT PIT FS 1480 L34L LONGERON IS CRACKED. REMOVED CRACKED LONGERON AND REPLACED LONGERON SECTION IAW DC8 SRM 53- 2-2 FIS 4A & 51-4-20D.May 25, 2002 · N803UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS02838620Floor Support · corrodedINSPECTION TYPE:C1 MAIN CABIN FLOOR SUPPORT AT STA 1762 RBL 11 HAS DRILL STARTS WITH CORROSION. REMOVED FLOOR BOARD SUPPORT IAW DC8 SRM 51-1-20D. FABBED FLOOR BOARD SUPPORT IAW DC8 SRM 53-7-1 AND INSTALLED SUPPORT IAW DC8 SRM 51-1-20DMay 25, 2002 · N803UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838619Door Frame · crackedINSPECTION TYPE:C1 L2 DOOR LWR FWD CORNER CRACKED, FOUND BY X-RAY INSPECTION. REPAIRED AREA IAW DC8 SRM 53-2-0 FIG 18.May 25, 2002 · N803UP · Doug DC873F · Fuselage Main, StructureSDR UPS02838604Door Frame · damagedINSPECTION TYPE:C1 RT FWD DOOR UPPER FWD ELONGATED HOLE ON FRAME. FABBED DOUBLER IAW DAC DRW 5615762 AND INSTALLED SAME IAW DC8 SRM 51-1-21.May 25, 2002 · N803UP · Doug DC873F · Service DoorsSDR UPS02838546Web · crackedINSPECTION TYPE:C1 AFT PIT STA 1400 L33R & L34R WEB LIGHTENING HOLE CRACKED/SPLIT. CUT OUT DAMAGE PER DC8 SRM 53-2-0. INSTALLED PER DC8 SRM 51-1-21.May 25, 2002 · N803UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2002805048Sliding Window1) CAPT SLIDING WINDOW STICKS @ 50% OPEN WILL NOT OPEN FULLY2) ADJUSTED MICARTA RUB BLOCK FOR CLEARANCE PER MM 56-10-3 OP CKS OKAYMay 25, 2002 · N805DH · Doug DC873F · Flight Compartment WindowsSDR UPS02838467Accumulator · leakingINSPECTION TYPE:N/A ATB NO BRAKES ON LT SIDE OF A/C FROM THE CAPTS, F/O, POS, WHILE TAXING HYD BRAKE PRESS IS LOW AND FWD ACCUMULATOR IS FLAT. UPON INVESTIGATION FOUND HYD FLUID COMING OUT OF FWD BRAKE ACCUMULATOR. REMOVED AND REPLACED FWD BRAKE ACCUMULATOR May 25, 2002 · N804UP · Doug DC873F · Master Cylinder/Brake ValveSDR UPS02838660Frame · corrodedINSPECTION TYPE:C1 AFT CARGO BAY FRAME CAP IS CORRODED STA 1060 STRINGER 36. CORROSION OUT OF LIMITS IAW 53-2-0. REMOVED FRAME CAP. FAB REPAIR ANGLE IAW UPS EO DC8-5310-11728-A. INSTALLED FRAME CAP REPAIR IAW DC8 SRM 51-1-20D & 51-1-21E.May 24, 2002 · N803UP · Doug DC873F · Fuselage Main, FrameSDR UPS02838627Frame · corrodedINSPECTION TYPE:C1 AFT CARGO BAY CORRODED UNDER NUTPLATE ON FRAME STA 1020 STRINGER 34R. REMOVED CORROSION, OUT OF LIMITS. FABBED DOUBLER & FILLERS. INSTALLED DOUBLERS & FILLER GUSSETS & CLIP IAW EO DC8-5310-11728 DWG DC8-53A-011 SRM 53-2-0 51-1-8 51-1-24 51May 24, 2002 · N803UP · Doug DC873F · Fuselage Main, FrameSDR UPS02838626Frame · corrodedINSPECTION TYPE:C1 AFT CARGO BAY FRAME IS CORRODED STA 1100 STR 36. REMOVED CORROSION, REMOVED DAMAGED SECTION OF FRAME, FABBED REPAIR ANGLE FILLERS & REPAIR STRAP LOCATED DRILLED REPAIR PARTS & INSTALLED REPAIR ANGLE FILLERS & REPAIR STRAP IAW UPS EO DC8-53May 24, 2002 · N803UP · Doug DC873F · Fuselage Main, FrameSDR UPS02838598Outflow Valve · corrodedINSPECTION TYPE:C1 AFT ACCY COMPT CABIN AIR OUTFLOW NOZZLE VALVE HAS CORROSION AROUND AREA. CORROSION ON NOZZLE VALVE OUT OF LIMITS. REMOVED AND REPLACED NOZZLE IAW DC8 MM 21-31-04, OPS CHECKED IAW DC8 MM 21-31-04.May 24, 2002 · N803UP · Doug DC873F · Pressure Regulator/Outflow ValveSDR UPS02838624Angle · crackedINSPECTION TYPE:C1 RT WING FLAPWELL ATTACH ANGLE AT XW0 REAR SPAR CRACKED. FABBED ANGLE IAW DAC DWG 5651221 & INSTALLED ANGLE AND SKIN PANEL IAW DC8 SRM 51-1-21 51-3-0.May 23, 2002 · N803UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS02838577Support Fitting · crackedINSPECTION TYPE:C1 AFT PIT C3 DOOR RAMP PANEL FOLDING DOOR SUPPORT FITTING IS CRACKED. REMOVED PANEL AND FOUND SKIN CRACK FABRICATE NEW SKIN IAW DAC DWG 97540 58. ALODINED & PRIMED IAW DC8 SRM 51-1-8. REMOVED SUPPORT FITTING LOCATED NEW FITTING AND DRILLED May 23, 2002 · N803UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838376Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ON AT ALL TIMES. DISARM CHECK NORMAL. REMOVED AND REPLACED EMERGENCY BATTERY PACK.May 23, 2002 · N880UP · Doug DC873F · Emergency LightingSDR UPS02838673Seat Track · damagedINSPECTION TYPE:C1 POS 13 O/B SEAT TRACK DAMAGED AT SPLICE INTERIM REPAIR C/W PER EO DC8 -5310-15957A. CUT OUT DAMAGED TRACK IAW DC8 SRM 53-2-3. LOCATED AND DEBURRED SPLICE, ALODINED & PRIMED, FABBED, LOCATED, DRILLED & INSTALLED.May 22, 2002 · N803UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS02838390Battery Pack · dischargedINSPECTION TYPE:C13 EMERGENCY LIGHT BATTERY DEAD. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK GOOD IAW UPS DC8 MM 33-50-01.May 21, 2002 · N818UP · Doug DC873F · Emergency LightingSDR UPS02838379Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ON AT ALL TIMES. DISARM CHECK NORMAL. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW 33-50-01, CHECKS GOOD.May 21, 2002 · N880UP · Doug DC873F · Emergency LightingSDR UPS02838354Battery · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ON AT ALL TIMES. DISARM CHECK NORMAL. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW 33-50-01.May 21, 2002 · N880UP · Doug DC873F · Emergency LightingSDR DHL2002807007Fire Loop · failedNR 2 ENG B-LOOP SHORT CIRCUIT LIGHT ILLUMINATED. CHECKED LOOPS WITH A MEGER. FOUND LT & RT B-CORE DETECTOR LOOPS WITH LOW ISOLATION. REPLACED BOTH SIDES OF CORE DET LOOP AND TESTED SYSTEM PER M/M 26-10-1, ALL CKS GOOD.May 18, 2002 · N807DH · Doug DC873F · Fire DetectionSDR DHL2002807006Ground Wire · damagedNR 2 B-LOOP SHORT LIGHT ON. FOUND AND FIXED STRIKING SOCKET AND GROUND WIRE AT ENGINE NR 2 LOOP-B. OPS CHECK GOOD IAW MM 26-10-4.May 17, 2002 · N807DH · Doug DC873F · Fire Protection System WiringSDR UPS02838385Door Frame · crackedINSPECTION TYPE:C13 R2 UPPER AFT DOOR JAMB CORNER CRACKED 2ND OR 3RD LAYER AND INNER LAYER CRACKED. REPAIRED IAW EO DC8 5330-12075G.May 16, 2002 · N818UP · Doug DC873F · Fuselage Main, StructureSDR DHL2002801012Fire Loop1) ON T/O MASTER FIRE LIGHT ILLUMINATED AND BELL SOUNDED.REJECTED T/O ,BELIEVED TO BE #2 ENG RAN ENGINE FIRE EMERGENCY CHECKLISTAND SHUTDOWN #2MAX SPEED AT REJECT 70 KIAS2) FOUND #2 B-LOOP GIVING FALSE FIRE INDICATION.DEFERRED #2 ENG B-LOOP PER MEL 26-2-3 DMMay 15, 2002 · N801DH · Doug DC873F · Fire DetectionSDR DHL2002801011Fire Loop1) WHEN SELECTING NO.2 ENG "B" LOOP, FIRE WARNING ACTIVATED INSTANTANEOUSLY. (WITHOUT SELECTING SHORTED LOOP OR FIRE WARN TEST)2) REPLACED CONNECTOR ON "B" LOOP. SYS LOOP P1-7050. SYS CHKS GOOD PER DC-8 MM 26-10-1May 14, 2002 · N801DH · Doug DC873F · Fire DetectionSDR UPS02838230Battery Pack · dischargedINSPECTION TYPE:N/A GLARESHIELD AND EMERGENCY OVERHEAD LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM 33-50-01. OPS CHECKS GOOD.May 13, 2002 · N803UP · Doug DC873F · Emergency LightingSDR DHL2002804006Skin · crackedSTA 310, 10 INCHES ABOVE A-PIT DOOR HANDLE HAS A .25 INCH CRACK THROUGH SKIN STA 1190, C-PIT DOOR 10 INCHES BELOW DOOR HANDLE HAS A CRACK. INSTALLED MAJOR REPAIR A-PIT DOOR 10 INCHES ABOVE HANDLE PER BOEING MESSAGE DHL-CVG-02-00026H & DRAWING. REF A/DHLL0205May 13, 2002 · N804DH · Doug DC873F · Cargo/Baggage DoorsSDR DHL2002804005Skin · crackedSTA 310 10 INCHES BELOW DOOR HANDLE HAS .45 CRACK THOUGH SKIN A-PIT DOOR. INSTALLED MAJOR REPAIR A-PIT DOOR 10 INCHES BELOW DOOR HANDLE PER BOEING MESSAGE DHL-CVG-02-00026H & DRAWING REF A DHLL020510/2 REF B FAX REPAIR SKETCH.May 13, 2002 · N804DH · Doug DC873F · Cargo/Baggage DoorsSDR UPS02838391Seat Track · corrodedINSPECTION TYPE:C13 SEAT TRACK E AT STA 1140 CORRODED AT POSITION-B. REMOVED AND REPLACED SECTION OF SEAT TRACK IAW DC8 SRM 53-2-3 AND UPS EO DC8-5320-5167C.May 10, 2002 · N818UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 2002FA0000725Longeron · corroded(LONGERON) FOUND DURING (D) CHECK INSPECTION, STA960 AND LONGERON 24L AFTER FITTING REMOVAL, FOUND CORROSION ON LONGERON 24 AT FASTENER HOLES.May 8, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/StringerSDR 2002FA0000722Web · corroded(WEB SKIN) FOUND DURING (D) CHECK INSPECTION, RIGHT W/W STA. 980 CNAT BULKHEAD WEB SKIN AND ANGLES HAS SURFACE CORROSION FROM LONGERON 24 TO LONGERON 27R.May 8, 2002 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR 2002FA0000721Longeron · corroded(LONGERON 24) FOUND DURING (D) CHECK INSPECTION, LEFT WHEEL WELL STA. 902 FITTING AND LONGERON 24 CORROSION EMINATING FROM BETWEEN FITTING AND LONGERON LOWER SURFACE.May 8, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2002801010Fire Loop1) ¥2 ENGINE FIRE WARNING CAME ON ERRATICALLY AND INTERMITTENTLY WHEN ON "B" LOOP. NORMAL INDICATION WHEN ON "A" LOOP2) CHECKED ¥2 ENGINE FIRE WARNING SYSTEM R&R "B" CORE LOOP CONNECTOR P1-8059 IAW WD.26-01-01.TESTED OPERATION OF BOTH LOOPS FOUND OMay 8, 2002 · N801DH · Doug DC873F · Fire DetectionSDR UPS02838380Fitting · crackedINSPECTION TYPE:C13 AFT PIT FS 1152 INTERCOSTAL FITTING AT L33R IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D, RECD LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED IAW DC8 SRM 51-1-20D.May 7, 2002 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838260Keelbeam · corrodedINSPECTION TYPE:C2 FWD LOWER CARGO L36 CORRODED BETWEEN FS 620 & FS 640. REPAIR FWD LWR CARGO L36 LT IAW REO G08587 REV A & UPS EO DC8-5300-1 6674-B.May 7, 2002 · N804UP · Doug DC873F · Fuselage Main, KeelSDR 2002FA0000726Floorbeam · corroded(FLOORBEAM) FOUND DURING (D) CHECK INSPECTION. CORROSION AT STA 920. 63 INCHES LEFT OF CENTER, FLOORBEAM.May 6, 2002 · N961R · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2002807005Smoke Detector · will not testNR 4 SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED NR 4 SMOKE DETECTOR, SYS TEST OK IAW 26-10-5.May 4, 2002 · N807DH · Doug DC873F · Smoke DetectionSDR DHL2002806011Structure · brokenCAPT'S SLIDING WINDOW VERY DIFFICULT TO OPEN AND CLOSE. BROKEN TRIM ALONG BOTTOM OF WINDOW. FOUND INTERIOR TRIM INTERFERING WITH WINDOW. SECURED INTERIOR TRIM IAW DC8 MM 20-20-0. BOTTOM WINDOW TRIM NOT BROKEN, TWO SEPARATE PIECES.May 4, 2002 · N806DH · Doug DC873F · Flight Compartment Windows
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