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 RRXA98224Connector · looseON 2 MILE FINAL NOSE GEAR LIGHT WENT OUT, RECYCLED GEAR, NO LIGHT BELOW 1,000 FT. GPWS SOUNDED, WENT AROUND, RECYCLED GEAR. GOT THREE GREEN, VERIFIED BY LOOKING THRU NOSE GEAR HOLE. SECURED LOOSE CONNECTOR AT DOWN LATCH SWITCH. ELECTRICAL AND VISUAL CHK GOSDR UPS98827578Jamb · crackedINSPECTION TYPE-C/CK, MAIN CARGO DOOR AFT JAMB DRILLED HOLE IS CRACKED AND A PIECE IS BROKEN OFF. MATERIAL ID FOR REPAIR .063 2024 T4 IAW DOUGLAS DWG 57772787, HEAT TREATED MATERIAL FROM 2024-0 TO 2024 T4 IAW TPS-1003 REV A. MATERIAL ID FILLER .063 2024 T4 SDR UPS98827091Floorbeam · corrodedINSPECTION TYPE:C/CK FLOORBEAM FUSELAGE STATION 1700, SEVERLY CORRODED BLO TO LBL 3. REMOVED DAMGED AREA FROM BEAM. FABRICATED INTERNAL DOUBLER, ANGLE, AND FILLER AND SHIMS IAW REO-04822. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 SRSDR UPS98827470Web · crackedINSPECTION TYPE-C/CK, LEFT HAND INBOARD AILERON, INBOARD WEB, CENTER ACCESS PANEL MATING SURFACE OF THE WEB IS TORN AND CRACKED. FABRICATED REPAIR DOUBLERS AND ALODINED AND PRIMED IAW REO 04825 AND DC8 SRM 51-1-8. INSTALLED REPAIR IAW REO 04825 AND DC8 SRM 5SDR UPS98827061Fitting · crackedINSPECTION TYPE:C+S2 IN NR 3 MAIN TANK JUST OUTBD OF XRS74 LOWER STRINGER NR 51 IS CRACKED IN TWO SEPARATE PLACES ON THE FWD SIDE AND BETWEEN 3 FASTENERS ON THE AFT SIDE. REMOVED CRACKED END FITTING. DRILLED NEW FITTINGS IAW 51-3-2. INSTALLED FITTINGS IAW DSDR UPS98827060Fitting · crackedINSPECTION TYPE:C+S2 IN NR 3 MAIN TANK ON INBD SIDE AT APPROX STA XRS 66 TO APPROX XRS 61 LOWER STRINGER NR 51 IS CRACKED ON THE AFT SIDE. REMOVED END FITTING IAW DAC DWG 3704841 PART NR 3704841-501. DRILLED NEW FITTING IAW DC8 SRM 51-3-2. ALODINED AND PRIMSDR UPS98827059Frame · corrodedINSPECTION TYPE:C+S2 FS 1725 LONGERON 16R FRAME IS CORRODED/EXFOLIATED NEXT TO LONGERON ATTACH BOLTS. FABBED ANGLE IAW REO-04829 AND INSTALLED IAW DC8 SRM 51-1-21D.SDR RRXA98302Link · gougedDURING A MAINTENANCE VISIT, FOUND LEFT WING, FLAP LINK GOUGED, AT STA 340. AFTER DAMAGE BLEND-OUT, NO DC-8 SRM LIMITS GIVEN. LIMITATIONS APPROVED IAW FAA APPROVED TIMCO ENGINEERING SKETCH REO-4787.SDR UPS98827579Skin · damagedINSPECTION TYPE-C/CK, RT WING CENTER LEADING EDGE INBOARD UPPER SKIN 2 SCREW COUNTERSUNK DAMAGED. FABRICATED BUSHING IAW REO 04899, FABRICATED REPAIR DOUBLER IAW REO 04899. INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-21, INSTALLED REPAIR BUSHING IAW DC8 SRM 51SDR UPS98827467Web · brokenINSPECTION TYPE-C/CK, MAIN CARGO DOOR FWD BETWEEN LIGHTENING HOLES 4, 5 HAVE EDGES BROKEN OUT INSIDE. FABRICATED WEB REPAIR, FRAME REPAIR ANGLE AND REPAIR SPLICE ANGLE IAW REO 04929, INSTALLED WEB REPAIR AND ANGLE IAW REO 04929 AND DC8 SRM 51-1-20D, AND 51-1SDR UPS98827089Seat Track · corrodedINSPECTION TYPE:C/CK CORROSION SEAT TRACK D ON UPPER/LOWER SURFACE OF TOP FLANGE AT FUSELAGE STATION 1700. CUT OUT DAMGED SECTION OF TRACK IAW DC8 SRM 51-1-24. DRILLED NEW SPLCIE SECTION IAW DC8 SRM 51-1-24. INSTALLED NEW SPLICE SECTION AND NEW SEAT TRACK SSDR UPS98827088Seat Track · corrodedINSPECTION TYPE:C/CK STATION 1220 RBL 25 SEAT TRACK SPLIT WITH CORROSION. FABRICATED SEAT TRACK IAW DC8 SRM 53-2-3, ALODINED AND PRIMED IAW DC 8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-3-0.SDR UPS98827058Shear Tie · crackedINSPECTION TYPE:C+S2 AFT BANANA FITTING CRACKED AT C-1 DOOR FS 370 AT LONGERON 32R. REMOVED CRACKED FITTING LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2, INSTALLED FITTING IAW DC8 SRM 51-1-20D.SDR UPS98827057Fitting · corrodedINSPECTION TYPE:C+S2 FS 280 LONG 35R -36 ZEE FITTING IS CORRODED. INSTALLED NEW FITTING IAW DC8 SSRM 51-1-20D.SDR UPS98826797Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK OK. (P/N 60-1223-5) (S/N 262) OFF, (P/N 5708458-503) (S/N PTL 1005) ON.SDR RRXA98301Bulkhead · damagedDURING A MAINTENANCE VISIT, ONE EACH FASTENER HOLE WAS DAMAGED DURING DRILLING OPERATION OF DC-8 SRM 53-2-5 FIGURE 14A, SHEET 4, REPAIR TO AFT PRESSURE BULKHEAD BETWEEN LONGERONS 10 LEFTAND 12 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ESDR RRXA98300Fitting · crackedDURING A MAINTENANCE VISIT, FOUND LONGERON 11 RIGHT END FITTING (PN: 4611284-502) CRACKED, AT STA 70. REMOVED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING BY MATERIAL SUBSTITUTION IAW FAA APPROVED TIMCO DER ENGINEERING SKETSDR UPS98827125Stiffiner · crackedINSPECTION TYPE:C/CK COMPLIED WITH FWD BULKHEAD VIEWS FROM CABIN FLOOR STATION 683 X= -2 3 TOP OF VERTICAL STIFFENER BRACKET CRACKED. MATERIAL ID 2024-0 IAW DWG 5773275, HEAT TREATED 2024-0 TO 2024 T4, .100 IAW TPS- 1003 FABRICATED IAW DC8 SRM 51-1-4 AND 51-SDR UPS98827090Floorbeam · corrodedINSPECTION TYPE:C/CK FLOORBEAM AT STATION 1580 HAS CORROSION ON FWD LIP IN THE AREA OF LONGERON 22 AND 23 LEFT. REMOVED CORROSION FROM FLOORBEAM MAT REMOVED 50 PERCENT IAW DC8 SRM 53-2-0. FABRICATED FILLER AND 2 ANGLE DOUBLER REPAIR IAW REO 04839 ALODINED ASDR UPS98827056Longeron · corrodedINSPECTION TYPE:C+S2 CORROSION ON LONGERON 30R AT STA 1540. REMOVED CORROSION IAW DC8 SRM 51-1-8. MATERIAL FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. MAT ID 7075-T6 .050 PO NR 260338, 7075-T6 .080 PO NR 262218, 7075-T6 .160 PO NR 254127 IAW DC8 SRM 53-2-SDR UPS98827055Web · crackedINSPECTION TYPE:C+S2 VERT STAB CLOSEOUT WEB AT ST ZR297 IS CRACKED. CLEANED AREA IAW DC8 SRM 51-1-8. PERFORMED HFEC IAW MIL-STD-271F ON VENT CLOSE OUT WEB ZR297 AFTER CLEANING AREA FOUND CORROSION AROUND RIVET. REMOVED RIVET IAW DC8 SRM 51-1-21. REMOVED COSDR UPS98827054Fitting · crackedINSPECTION TYPE:C+S2 VERT STAB AFT SPAR STA ZR297 FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-24 AND 51-1-20D.SDR UPS98827053Floorbeam · crackedINSPECTION TYPE:C+S2 CABIN STA 760 X=23 FLOORBEAM FITTING ON AFT SIDE CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.SDR UPS98827052Floorbeam · crackedINSPECTION TYPE:C+S2 CABIN STA 702 X=23 AT CABIN FLOORBEAM UPPER CHORD UNDER SEAT TRACK CRACKED. REMOVED AND REPLACED FITTING SUPPORT IAW DC8 SRM 51-1-20D.SDR UPS98827051Fitting · crackedINSPECTION TYPE:C+S2 CABIN-STA 702 X=69 (CUSP) AT FLOORBEAM ATTACH FITTING CRACKED. REMOVED OLD FITTING DRILLED UP NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D.SDR UPS98827050Stiffener · crackedINSPECTION TYPE:C+S2 CABIN STA 683, X=0 ABOVE C/W BOX VERT STIFFENER CRACKED. MAT ID IAW DOUGLAS DWG-5773275 -1002024-0 PO NR 185371, HEAT TREATED ANGLE FROM 2024-0 .100 TO 2024-T4 .100 IAW TPS -1003. REV AS FABBED ANGLE IAW DC8 SRM 51-1-24. ALODINED AND PRSDR UPS98827049Stringer · corrodedINSPECTION TYPE:C+S2 FS 450 LONG 31R CORRODED AND CHIPPED METAL ALONNG EDGES AND FASTENER HOLES AT THE FWD END OF FITTING. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW WITH DC 8 SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. BLESDR RRXA98295Floorbeam · corrosionDURING A MAINTENANCE VISIT, FOUND FLOORBEAM WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 1700. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-04SDR RRXA98293Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MAIN CARGO DOOR JAMB FRAMES WITH MIS-DRILLED HOLES, AT STA 270 AND STA 280. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH ENGINEERING SKETCH REO-04753.SDR UPS98827594Linkage Box · crackedINSPECTION TYPE-C/CK, LEFT HAND HORIZONTAL STABILIZER OUTBOARD GEAR TAB LINKAGE BOX CRACKED AND GOUGED XRS 216. REMOVED TAB LINKAGE COVER IAW DC8 SRM 51-1-21, WELDED BOX IAW DC8 1 0.301 AND DAC DWG 5652086, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, REINSTALLED SDR UPS98827469Strap · crackedINSPECTION TYPE-C/CK, VERTICAL STABILIZER TO FUSELAGE STRAP, RIGHT HAND SIDE HAS A CRACK AT FASTENERS HOLE FUSELAGE STATION 1765. FABRICATED REPAIR ANGLE AND FILLERS AND ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED FILLER AND REPAIR ANGLE IAW DC8 SRM 51-SDR UPS98827048Spar · crackedINSPECTION TYPE:C+S2 LT HORIZONTL STAB I/B GEAR TAB LINKAGE BOX CRACKED AND GOUGED XRS 137. REMOVED AND REPLACED IB GEAR TAB LINKAGE BOX IAW DC8 SRM 51-1-21 WELDED EFFECTED AREAS IAW DPS 10.225. ALODINED AND PRIMED IAW DC8 SRM 51 -1-8.SDR UPS98827047Spar · crackedINSPECTION TYPE:C+S2 RT HORIZONTAL STABILIZER OB GEAR TAB LINKAGE BIX CRACKED AND GOUGED XRS 216. REMOVED RT OB HORIZONTAL STAB GEAR TAB LINKAGE BOX IAW DC8 SRM 51-1- 21 WELDED BOX IAW DPS 10.225 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. REINSTALLED BOX IAW DSDR UPS98827045Angle · corrosionINSPECTION TYPE:C+S2 CORROSION ON RIGHT WING TRAILING EDGE PANEL SUPPORT ANGLE AT XRS 558 .00. ORDER NEW ANGLE RECEIVED NEW ANGLE DRILLED HOLES AND INSTALLED ANGLE IAW DC8 SRM 51-1-21.SDR UPS98827593Longeron · crackedINSPECTION TYPE-C/CK, LONGERON 35 LEFT CRACKED FUSELAGE STATION 290. REMOVED AND REPLACED LONGERON 35 LEFT IAW DC8 SRM 51-1-20D AND 51-1-24.SDR UPS98827044Door · crackedINSPECTION TYPE:C+S2 LT MLG DOOR CRACKED AT FWD AND AFT DRAIN HOLES OBS EDGE, 2 PLACES LT MLG INBD DOOR, MAT ID 7075-T6 .050 SUBSTITUTED TO 2024-0 .050 HEAT TREATED TO T4 FABRICATED, ALODINED AND INSTALLED ALL IAW DC8 SRM 52-6-1, TP91003 REV A 51-1-8 AND 51-1SDR UPS98827043Frame · corrosionINSPECTION TYPE:C+S2 FRAME STA 80 HAS DAMAGE AT L21RT. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED SPLICE REPAIR ANGLES AND FRAME SEGMENT IAW DC8 SRM 53-2-0. ALODINED AND PRIMED SPLICE REPAIR ANGLE AND FRAME SEGMENT. INSTALLEDSPLICE REPAIR ANGLES AND FRAMSDR UPS98827468Skin · crackedINSPECTION TYPE-C/CK, L-2 DOOR AT FWD LOWER CORNER HAS CRACKED LINE ABOUT 4 INCHES LONG. CUT OUT DAMAGED IAW REO 04856, FABRICATED FILLERS IAW DC8 SRM 53-2-0, 51-1-24, AND REO 04856. FABRICATED DOUBLERS IAW DC8 SRM 53-2-0 AND REO 04856 AND INSTALLED FILLERS SDR UPS98827041Skin · crackedINSPECTION TYPE:C+S2 RW UPPER INBD AFT SKIN PANEL AT APPROX STA XCW 69.500 IS CRACKED. CUT ATTACHMENT ANGLE TO FWD END OF CRACK, BLENDED AREA OF CRACK IAW DC8 SRM 57-20-0 FIG 7 FOUND TO BE WITHIN LIMITS, PERFORMED HFEC IAW MIL-STD-271F. FOUND NO CRACKS AFTERSDR UPS98826828Intercostal · crackedINSPECTION TYPE:C, INTERCOSTAL AT LONG 33R BTWN STA 1160-1180 IS CRACKED AND HAS LIGHT CORROSION. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9754949 AND SRM 51-1-20D.SDR RRXA983138Angle · corrosionDURING A MAINTENANCE VISIT, FOUND CROSS SLIDE DOOR, COVER ATTACH ANGLE WITH CORROSION BEYOND LIMITS IAW DC-8 SRM, AT STA 280 BETWEEN LONGERONS 27 RIGHT AND 36. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAASDR RRXA98297Fitting · crackedDURING A MAINTENANCE VISIT, FOUND LONGERON 14 RIGHT END FITTING (PN: 4611181-1) CRACKED, BETWEEN STA 55 AND STA 70. REMOVED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING BY MATERIAL SUBSTITUTION IAW FAA APPROVED TIMCO DER ENSDR RRXA98296Fitting · crackedDURING A MAINTENANCE VISIT, FOUND LONGERON 14 LEFT END FITTING (4611181-1) CRACKED, BETWEEN STA 70 TO STA 80. REMOVED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING BY MATERIAL SUBSTITUTION, IAW FAA APPROVED TIMCO DER ENGINEESDR RRXA98294Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FRAME WITH MIS-DRILLED HOLES, AT STA 1080 BETWEEN LONGERONS 5 LEFT TO 8 LEFT. REMOVED DAMAGED SECTIONS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-04762.SDR RRXA98291Skin · misdrilledDURING A MAINTENANCE VISIT, FOUND LEFT ELEVATOR SKIN ASSEMBLY AND TE CLOSING CHANNEL AT STA XE=200.258 HAD A DOUBLER DRILLED HOLE. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR STRAP AND FILLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-0474SDR RRXA98143Frame · corrosionDURING A MAINTENANCE VISIT, FOUND MULTIPLE CORROSION AREAS ON FRAME AT STA 1680 BETWEEN LONGERONS 9 LEFT TO 9 RIGHT. REMOVED DAMAGED SECTIONS, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKESDR RRXA98142Frame · crackedDURING A MAINTENANCE VISIT, FOUND CRACK ON FRAME AT STA 120 AT LONGERON 6 LEFT. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04759.SDR DHL98803001Wire · brokenNR 4 ALT QUAN LOW LIGHT ILLUMINATED. USED ABNORMAL PROCEDURE AND LIGHT WOULD NOT EXTINGUISH. NR 4 ALT SHUT OFF VALVE CLOSED AND LIGHT WOULD NOT EXTINGUISH WHILE USING ABNORMAL PROCEDURE. FOUND BROKEN WIRE AT CANNON PLUG P1-113 TO ALT NR 4 REFILL SOLENOID. SDR UPS98827580Pan · crackedINSPECTION TYPE-C/CK, R1 DOOR JAMB AFT LOWER PAN REPAIR IS CRACKED. REMOVED DAMGED SECTION, FABRICATED PAN SECTION SPLICE ANGLE IAW RE O 04777. FABRICATED SEAL DEPRESSOR IAW DAC 5615700. RECEIVED EXTERNAL STRAP FROM SHOP (P/N 3887438-501) PER REO 04777 AND SDR UPS98826827Fitting · crackedINSPECTION TYPE:C, FITTING AT STA 1180, LONG 35L IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758497 AND SRM 51-3-0.
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