Douglas DC-8-73F
Service difficulty reports · 15,471
Newest first. General aviation reporting is voluntary.
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UPS99830396Fitting · crackedINSPECTION TYPE:C123, THE LONGERON 3R END FITTING AT FS 680 WAS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.SDR UPS99830361Fitting · crackedINSPECTION TYPE:C123, FS 1152 BETWEEN LONG 32R AND 33R, THE FRAME TO SKIN TIE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3755847 AND SRM 51-1-20D.SDR UPS99830360Fitting · crackedINSPECTION TYPE:C123, FS 980 TO 988, THE LONG 22L END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED THE FITTING IAW DWG 3753235 AND SRM 51-1-20D.SDR UPS99830342Fitting · crackedINSPECTION TYPE:C1, FS 798 FLOORBEAM AT RBL 24, THE FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-3-0.SDR UPS99830496Doubler · corrodedINSPECTION TYPE:C123, CORROSION FOUND ON FUSELAGE INTERNAL SKIN BETWEEN LONG 32R & 33R AT FS 1638. CUT OUT THE DAMAGED AREA AND REPAIRED THE INTERNAL SKIN IAW DH SK867-507.SDR UPS99830495Intercostal · corrodedINSPECTION TYPE:C123, HEAVY CORROSION ON THE INTERCOSTAL AND END CLIP AT FS 80 TO 100 AT LONG 25R. REMOVED, FABRICATED AND REPLACED THE INTERCOSTAL AND CLIP IAW SRM 53-4-1 & 51-1-20D.SDR UPS99830478Seat Track · corrodedINSPECTION TYPE:C3 STA 1580 TRACK F CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW D C8 SRM 53-2-3. FABRICATED AND INSTALLED SEAT TRACK, STRAPS AND STRIPS I AW DC8 SRM 53-2-3 AND 51-1-20D.SDR UPS99830451Seat Track · corrodedINSPECTION TYPE:C3, STATION 990 TRACK I HAS CORROSION DOWN CENTER. FABRICATED AND INSTALLED 2 SEAT TRACK SPLICES IAW DC8 SRM 53-2-3 AND 51-1-8.SDR UPS99830340Doubler · crackedINSPECTION TYPE:C1, RT WING L/E LWR INTERNAL SKIN DOUBLER AT XFS 597.5 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-20D & 51-1-21.SDR UPS99830338Skin · crackedINSPECTION TYPE:C1, RT WING L/E LWR SKIN AT XFS 597.5 IS CRACKED AT THE DRAIN HOLE. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4087.SDR UPS99830548Floor Beam · corrodedINSPECTION TYPE:C3, CORROSION AND POPPED RIVETS AROUND FASTENERS ON FLOOR SUPPORT BEAM FS 920 LT SIDE OF FUSELAGE. FABBED ANGLE ON TIMCO OPS 50017, SHOT PEENED IAW DC8 SRM 51-1-4A. DRILLED AND SLOTTED CRACK IN FLOORBEAM IAW REO 06663 REV B. FABBED DOUBLER ASDR UPS99830395Seat Track · crackedINSPECTION TYPE:C123, SEAT TRACK AT FS 280, RBL 45 IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED THE SEAT TRACK IAW SRM 53-2-3.SDR UPS99830394Skin · crackedINSPECTION TYPE:C123, LT WING L/E LWR SKIN AT XFS 597.5 IS CRACKED AT THE DRAIN HOLE AND ONE RIVET HOLE. STOP DRILLED CRACKS AND REPAIRED SKIN IAW EO DC8-5720-4087-B.SDR UPS99830337Skin · crackedINSPECTION TYPE:C1, LT WING L/E UPPER SKIN AT XS 518 IS CRACKED AT 1 SCREW HOLE. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.SDR UPS99830488Longeron · crackedINSPECTION TYPE:C3, AFT PIT FS 1270 LONGERON 34R HAS AN 8 INCH CRACK. REMOVED CRACKED LONGERON NR 34R STD 1270-1350 IAW DC8 SRM 51-1-20D. RECEIVED NEW LONGERON NR 3758593-1. DRILLED UP IAW DC8 SRM 51-1-20D. INSTALLED IAW DC8 SRM 51-1-20D.SDR UPS99830450Longeron · crackedINSPECTION TYPE:C3, FUS-1270 LONGERON 34L HAS AN 8 INCH CRACK. REMOVED LONGERON 34L IAW DC8 SRM 51-1-20D, RECEIVED NEW FITTING (P/N 3758593-1) AND INSTALLED LONGERON 34L IAW DC8 SRM 51-1-20D.SDR UPS99830586Elevator · lightning strikeINSPECTION TYPE:C3 LIGHTNING STRIKE ON RT ELEVATOR T/E AT STA XE290 GEN RFTS. REMOVED DAMAGED MATERIAL AND ID MAT IAW REO 06684. FABRICATED AND INSTALLED DOUBLER AND FILLER BOND AND SEAL IAW REO 06684 AND SRM 55-4-0, DC8 MM 27-30-02 AND 27-30-03.SDR UPS99830459Fairing · crackedINSPECTION TYPE:C3, NR 4 PYLON NOZZLE FAIRING HAS CRACKED FORMER. FABRICATED AND INSTALLED REPAIR IAW TIMCO REO NR 06674, HEAT TREATED REPAIR ANGLE AND CLIP IAW DAC DWG 9756774 GEN NOTE 23 AND TIMCO REO NR 0667 4, DC8 SRM 51-1-21.SDR RRXA991276Egt Indicator · malfunctionedON TAKEOFF, NR 4 ENGINE EGT WENT TO 929 DEGREES C AT 91 PERCENT N, OAT ON ATIS 35 DEGREES C, 29 DEGREES C FROM TOWER 120 KIAS, TARGET N1 91.8. REMOVED AND REPLACED NR 4 ENG EGT INDICATOR, CHECKED PMC, CHECKED INLETS AND EXHAUST FOR DAMAGE, CHECKED VSV'S AND VSDR UPS99830585Mechanism · corrodedINSPECTION TYPE:C3 LT MLG BOSS CORRODED. REMOVED CORROSION BY REAMING BOSS DIA 1.8134. RESHOP PEEN DIA 1.838 5 IAW DC8 SRM 32-1-1. MANUFACTURED BUSHING IAW DAC SB NR 32-102. INS TALLED BUSHING AND RETRACT PIN IAW REO 801UP-46-21373 AND DC8 SRM 51-3-0.SDR UPS99830447Web · corrodedINSPECTION TYPE:C3, LT HORIZ STAB INTERIOR WEB STA EX 99 CORROSION. FABRICATED AND INSTALLED NEW PANEL ASSY, (P/N 5651747-59) IAW DAC DWG 5651747 AND DC8 SRM 51-1-24 & 51-1-21.SDR UPS99830552Frame · corrodedINSPECTION TYPE:C3, AFT PIT FS 1040 CORROSION ON LOWER SURFACE OF UPPER FRAME FLANGE AT L31R. REMOVED FLOORBEAM, SUPPORT, END FITTING, INTERCOSTALS, FRAME ANGLE, FRAME CAP AND FRAME SECTION. LOCATE NEW FRAME SECTION, DRILLED AND REAMED EXISTING HOLES AND INSSDR UPS99830549Fitting · crackedINSPECTION TYPE:C3, STA 70 L36 STANCHION FITTING CRACKED. REPLACED CHANNEL (P/N 5613064-107), FITTING (P/N 4646944-501). FABBED PLATE IAW DAC DWG 5613064. FABBED LT STANCHION PER DAC DWG 5613064. LOCATED AND DRILLED NEW RT STANCHION & FITTING. INSTALLED NSDR UPS99830483Angle · corrodedINSPECTION TYPE:C3 MAIN CARGO SUB FLOOR, FLOOR SUPPORT ANGLE CRACKED AND GOUGED AT STA 8 RBL 6 DOT G-956. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW REO 06672. REPAIRED WEB IAW DC8 SRM 53-2-0.SDR UPS99830458Support · corrodedINSPECTION TYPE:C3, MAIN CARGO SUB FLOOR AT STA 40 RT SIDE UNDER WEB FLOOR SUPPORT CORRODED DOT G-949. FABRICATED AND INSTALLED BEAM AND ALL ASSOCIATED FASTENERS IAW DC8 DRAWING 5615180.SDR UPS99830446Seat Track · corrodedINSPECTION TYPE:C3, MAIN CABIN CARGO SUB FLOOR AT RBL 27 SEAT TRACK CORRODED STA 55 DOT G952. FABRICATED AND INSTALLED SEAT TRACK AND PANEL IAW DC8 DRAWING 588958 8 AND DC8 SRM 51-3-0.SDR UPS99830481Frame · corrodedINSPECTION TYPE:C3 RT CUSP AT STA 1360 CUSP TO FRAME FITTING CORRODED DOT G-932. REMOVED CORROSION PER DC8 SRM 51-1-8, 53-2-0, FOUND TO BE OUT OF LIMITS PER DC8 SRM 53-2-0. ROUTED OUT DAMAGED FLANGE TO REMOVE CORROSION DAMAGE IAW DC8 SRM 53-2-0. ROATE OUT OSDR UPS99830476Floorbeam · corrodedINSPECTION TYPE:C3 FWD PIT FS 100 RBL 41 FLOORBEAM CORRODED. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW DC8 SRM 51-7-1 FIG 13 AND DC8 SRM 51-2-0, FIG 50 ORG 125. FABRICATED AND INSTALLED DOUBLER IAW REO- 06665, DC8 SRM 51-1-20. INSTALLED FLOORBOARD SECTIONS IASDR UPS99830455Fitting · corrodedINSPECTION TYPE:C3, RT CUSP AT FRAME STA 540 FRAME TO CUSP FITTING CORRODED DOT G-921. FABRICATED AND INSTALLED FITTING (P/N 4597643-2N), PO 300243 IAW DC8 S RM 51-1-24, 51-3-0 & 51-3-1 PG 1.SDR UPS99830449Frame · corrodedINSPECTION TYPE:C3 AFT PIT INTERNAL DOOR FRAME CORRODED FABRICATED AND INSTALLED INTERCOSTAL AND 2 EACH PULLET BRACKET IAW D AC DWG #9754947 & DC8 SRM 51-1-20D & 51-3-0. ***CPCP***SDR UPS99830309Longeron · corrodedINSPECTION TYPE:C123, AFT PIT STA 1340 L27R CORRODED. FABRICATED AND INSTALLED NEW LONGERON SECTION AND NEW SPLICE P/N DC8 -53B-900-3 IAW DC8 SRM 53-2-2, 51-1-24 AND 51-1-21D.SDR UPS99830308Rib · crackedINSPECTION TYPE:C123, R/W O/B CTR L/E STA XFS 622 RIB CRACKED AT LWR AFT END. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 57-2-0 AND 51-1-20D.SDR UPS99830307Rib · crackedINSPECTION TYPE:C123, R/W O/B CTR L/E STA XFS 579 RIB CRACKED AT UPPER AFT END. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 57-2-0 AND 51-1-20D.SDR UPS99830306Rib · crackedINSPECTION TYPE:C123, RW OUTBOARDB LE RIB CRACKED AT LWR AFT END STA XFS 804. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 57-2-0 FIG 2, AND 51-1- 21.SDR UPS99830305Skin · gougedINSPECTION TYPE:C123, INNER SKIN GOUGED ON RT FWD SERVICE DOOR, AT AFT UPPER CORNER, ADJACENT TO LIGHTENING HOLE. FABRICATED AND INSTALLED DOUBLER, ATTACH ANGLE AND TWO FILLERS IAW DC8 SRM 52-2-3, 52-3-1 FIG 1, 51-9-0 AND 51-3-0.SDR UPS99830582Fitting · crackedINSPECTION TYPE:C3 RT AFT TYPE 1 DOOR FWD TORQUE BOX STA 1300 L12R HAS CORROSION/CRACK. PERFORMED HFEC IAW MIL-SID-271F TO VERIFY CRACK. REMOVED FITTING FROM A/C. LOCATED, DRILLED AND REAMED NEW FITTING IAW DC8 SRM 51-3-2 AND D AC DWG NR 3755819. INSTALLEDSDR UPS99830562Rib · crackedINSPECTION TYPE:C3, RIB CRACKED AT FASTENER AND FASTENER WORKING UNDER RT FWD FILLET PANEL STA 822 X-55. FABRICATED DOUBLER, STOP DRILLED CRACK, INSTALLED DOUBLER. ALL WORK ACCOMPLISHED IAW DC8 SRM 53-8-3, 51-9-0, 53-2-0, 51-1-8 & 53-2-0.SDR UPS99830487Skin · misrepairedINSPECTION TYPE:C3, L-Z DOOR UPPER AFT CORNER OF SKIN HAS PREVIOUS REPAIR NOT PER SRM. ROUTED OUT AREA IAW DC8 SRM 53-2-0 FIG 18. FORMED DOUBLERS AND FILLER PER DC8 SRM 53-2-0 FIG 18. LOCATED, DRILLED AND TRIMMED DOUBLERS IAW DC8 SRM 53-2-0 FIG 18. INSTALLSDR UPS99830486Fitting · corrodedINSPECTION TYPE:C3, FWD PIT STA 320 BETWEEN LONG 34R AND 35R, INSIDE DOOR TORQUE BOX, Z FITTING IS CORRODED. REMOVED Z FITTING IAW DC8 SRM 51-1-20D. FABRICATED REPAIR ANGLES IAW DC8 SRM 53-2-0. INSTALLED REPAIR ANGLES AND Z FITTINGS IAW DC8 SRM 51-1-20D.SDR UPS99830304Doubler · crackedINSPECTION TYPE:C123, RIB CRACKED AT FASTENER AND FASTENER WORKING UNDER RT FWD LOWER FILLET PANEL STA 822 X-55. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 53-2-0 AND 51-1-21.SDR UPS99830302Angle · crackedINSPECTION TYPE:C123, FWD LWR FILLET AREA FILLET PNL ATTACH BRACKET CRACKED AT STA 680 LONGERON 31R-32R. FABRICATED AND INSTALLED ANGLE FROM 7075-T6.063. ALUMINUM IAW DC8 S RM 53-8-0, 51-1-20D, AND 53-2-0.SDR UPS99830214Battery · dischargedCOCKPIT EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW M/M 33-50-01, OP'S CK NORMAL OK FOR SERVICE.SDR RRXA991392Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LOWER EXTERIOR SKIN BETWEEN STA 1420 AND STA 1440, AT LONGERON 36 PREVIOUS REPAIR DOUBLER SHEARED FASTENER AND CORROSION EMANATING FROM UNDER DOUBLER. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED,SDR UPS99830564Frame · corrodedINSPECTION TYPE:C3, RT FWD PIT STA 260 FROM LONG 34R TO 35L FRAME IS CORRODED. REMOVED GILLINER SUPPORT L/R SIDE AT LS 260, FOUND FRAME SECTION OUT OF LIMITS. REMOVED INTERCOSTAL, DRILLED NEW FRAME SEGMENT A/C IAW DC8 SRM 51-3-2. FABBED AND INSTALLED FRAME SDR UPS99830553Angle · crackedINSPECTION TYPE:C3, APB FLOORBOARD SUPPORT ANGLE CRACKED AND EXFOLIATED AT LBL 7. BLENDED SUPPORT ANGLE IAW DC8 SRM 51-1-8. FOUND OUT OF LIMITS IAW DC 8 SRM 53-2-0. FABBED NEW ANGLE IAW DRW NR 5753522. REMOVED PULLEY BRACKET ASSY AT STA 1766 SYS LTSD. REMSDR UPS99830482Longeron · corrodedINSPECTION TYPE:C3 EXFOLIATION INSIDE THE LONGERON CHANNEL. SPLICED IN A NEW LONGERON IAW DC8 SRM 51-1-20D AND 53-3-2.SDR UPS99830202Battery Pack · dischargedEMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK P/N ON/OFF 5708458-503 S/N ON 2024 S/N OFF 783.SDR UPS99830176Battery · dischargedEMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LTS BATTERY PACK IAW MM33-50-01. SYS OPS CHECKS NORMAL P/N ON 60-1223-5 OFF 5708458-503 S/N ON 219 S/N OFF 2045.SDR RRXA991725Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-3 BETWEEN Y=280 TO Y=580 AND X=40. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED SDR RRXA991723Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-1 BETWEEN Y=280 TO Y=580 AND X=30. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED
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