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 RRXA991386Finger Dougler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BULGE AND RIVETS POPPED ON FINGER DOUBLER AT STA -82 TO STA -67 RIGHT HAND SIDE BL 60 RIGHT, 10 BELOW COCKPIT FLOOR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.SDR UPS99829976Fitting · crackedINSPECTION TYPE:C-1, CROSS SLIDE RAMP MOUNT ATTACH FIG CRACKED FS 340 ABOVE L 35L. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC8-SRM 53-2-0 & 51-1-20D.SDR UPS99829893Fitting · crackedINSPECTION TYPE:C1, LONGERON END FITTING IS CRACKED L-10R FWD SIDE OF FRAME 680. REMOVED CRACKED FITTING. RECEIVED, LOCATED AND DRILLED NEW FITTING AT STA 680 AND L-10R IAW DC-8 SRM 51-3-2. INSTALLED FITTING IAW DC- 8 SRM 51-1-20D. TORQUED BOLT IAW DC-8 SRSDR UPS99829892Fitting · crackedINSPECTION TYPE:C1, LONGERON END FITTING IS CRACKED L6L FWD SIDE OF FRAME 680. REMOVED CRACKED FITTING. RECEIVED NEW FITTING (P/N 3779762-501N). LOCATED DRILLED AND DEBURRED NEW FITTING. INSTALLED NEW FITTING, TORQUED BOLT.SDR UPS99829891Fitting · crackedINSPECTION TYPE:C1, LONGERON END FITTING IS CRACKED L4L FWD SIDE OF FRAME 680. REMOVED CRACKED FITTING. RECEIVED NEW FITTING (P/N 3779762-501N). LOCATED DRILLED AND DEBURRED FITTING. INSTALLED NEW FITTING, TORQUED BOLT.SDR UPS99829772Battery Pack · dischargedINSPECTION TYPE:N/A, DURING PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK NORMAL.SDR RRXA991413Skin · chafedDURING A MAINTENANCE VISIT, FOUND LEFT WING CENTER L/E HAS SCREWS AND WASHERS WEARING INTO SKIN BY I/B SLOT DOOR AT STA 250.000. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER FROSDR UPS99829894Fitting · crackedINSPECTION TYPE:C1, INTERCOSTAL FITTING FWD SIDE OF FS 1140 FRAME ABOUT I/B HALF OF LONGERON 33 RT IS CRACKED. REMOVED CRACKED FITTING, RECEIVED NEW FITTING (P/N 4758514-521N). LOCATED, DRILLED AND DEBURRED NEW FITTING. INSTALLED NEW FITTING.SDR RRXA991595Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BETWEEN STA 50 AND STA 70, AND AT LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-21. SDR UPS99829959Fitting · crackedINSPECTION TYPE:C-1, BANANA FITTING FS 1220 LONGERON 29-33 RT IS CRACKED. REMOVED OLD FITTING. RECEIVED NEW FITTING, DRILLED HOLES, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.SDR UPS99829958Fitting · crackedINSPECTION TYPE:C-1, BANANA FITTING FS 1228 LONGERON 29-33 RT IS CRACKED. REMOVED OLD FITTING, RECEIVED NEW FITTING. DRILLED HOLES, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.SDR UPS99829896Fitting · crackedINSPECTION TYPE:C, INTERCOSTAL FITTING, AT FS 1228 ABOVE O/B HALF OF LONGERON 33 RT IS CRACKED ON UPPER AFT LEG. REMOVED INTERCOSTAL FITTING IAW DC-8 SRM 51-1-20D, RECEIVED FITTING NR 4758514-519N PO NR 294625 AND DRILLED UP IAW DC-8 SRM 51-1-20D, INSTALLED FSDR UPS99829895Fitting · crackedINSPECTION TYPE:C1, LONGERON 36 AT FS 1270 SPLICE FITTING IS CRACKED. RECEIVED, LOCATED AND DRILLED NEW LONGERON SPLICE FITTING (P/N 375922 2-1) IAW DC-8 SRM 51-3-2. INSTALLED NEW FITTING IAW DAC DWG NR 5750322.SDR UPS99829971Fitting · crackedINSPECTION TYPE:C-1, LONG 24R FITTING AT STA 920 IS CRACKED ON AFT SIDE DOT L122. REMOVED FABRICATED AND INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, DC8 SRM 51-3-0, 51-1-20D. INSTALLED SPOILER PULLEY BRACKET AND UPLOCK ASSEMBLY IAW DC8 SRM 51-3-0 AND MM 32-31-SDR RRXA991409Skin · gougedDURING A MAINTENANCE VISIT FOUND SMALL GOUGE IN SKIN FWD OF EXTERNAL POWER RECEPTACLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED GOUGE. FABRICATED AND INSTALLED ANGLE IAW FAA APPROVED TENNESSEE TECHNICASDR RRXA991406Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, FUSELAGE SKIN BY AFT CARGO DOOR STA 1445, LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW FAA APPROVED TENNESSDR RRXA991405Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACKS, FUSELAGE SKIN AT STA 1400, AT DOOR LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW FAA APPROED TENNESSEE TECHSDR RRXA991402Skin · crackedDURING A MAINTENANCE VISIT, FOUND A-PIT DOOR CUT-OUT BOTTOM SKIN CRACK AND CHIPPED OFF, ALSO GOUGES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW FAA APPROVED TENNESDR RRXA991393Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LOWER SKIN AT STA 1420, LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW FAA APPROVED TENNESSEE TECHNISDR RRXA991391Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN UNDER A PIT DOOR CORRODED AND MISSING LAYER AT STA 320, LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS SDR RRXA991601Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN, AT STA 1688, FLOOR PANEL A CORRODED AND CRACKED AT LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOORBOASDR RRXA991616Support · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CUSP FRAME SUPPORT AND WEB AT STA 25 AND LONGERON 25 RIGHT FLOOR LEVEL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DCSDR RRXA991408Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREW PULLING THROUGH SKIN LEFT WING CENTER L/E I/B EDGE 45 FWD FRONT SPAR AT STA XFS 285.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER ISDR RRXA991135Pin · damagedDURING A MAINTENANCE VISIT FOUND SPIRALED TOP AND BOTTOM HOLES, LEFT MLG RETRACT PIN BOSS THROUGH BOLT HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. SMOOTHED BORE, FLAP PEENED HOLE IAW FAA APPROVED TENNESSEE TSDR RRXA991134Pin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RT MLG, RETRACT CYL. A PIN REPAIR PER CUSTOMER REQUEST IAW MA AI 3210-01:03 S/B 32-102, REF AD 71-25-09. ACCOMPLISHED INSPECTION, FOUND CORROSION, IN PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGEDSDR RRXA991133Pin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LT MLG, RETRACT CYL A-PIN REPAIR PER CUSTOMER REQUEST IAW MA A13210-01:03 S/B 32-102 REF. AD 71-25-09. ACCOMPLISHED INSPECTION FOUND CORROSION IN PIN BOSS.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TRSDR RRXA991132Fitting · gougedDURING A MAINTENANCE VISIT FOUND GOUGE, RIGHT ELEV, RT GEAR TAB ASSY, I/B FITTING GOUGED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. BLENDED GEARED TAB I/B FITTING IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3 DASDR RRXA991131Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, NR 1 PYLON, I/B TRIPLER (ANGLE) CRACKED 1.5. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM.. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED ANGLES IAW DC8 SRM 51-1-6 AND 51-1-7, 51-1-20D.SDR RRXA991130Fastener · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE, RIGHT WING, FASTENER DAMAGED INSIDE NR 4 ALT FUEL TANK BY NR 4 PYLON AT XW 463 STR 58 LOWER SURFACE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. FASTENER OK AS IS IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETSDR RRXA991129Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, B-PIT LEFT FWD BETWEEN STA 460 AND STA 480 LEFT AT LONGERON 31 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLERS AND DOUBLERS SDR RRXA991128Float Box · twistedDURING A MAINTENANCE VISIT FOUND TUBE TWISTED, RIGHT WING, NR 4 A FLOAT BOX WELDED TUBE TWISTED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED FLOAT BOX, WELDED TUBE IN PLACE IAW FAA APPROVED TENNESSEE TECH SDR RRXA991126Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN, JUST FWD OF TAIL SKID AT STA 1746, LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOUBLER IAW DC8 SRM 53-2-1, INSTALLED FSDR RRXA991125Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOORBEAM UNDER SEAT TRACK 3 ABOVE LONGERON 32 LEFT AT STA 1700. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROSDR RRXA991124Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, L/E BETWEEN NR 3 AND NR 4 ENG JUST O/B OF STALL WARNING TRANSDUCER BETWEEN XSF 385 AND XFS 388. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSSDR RRXA991123Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, FUSELAGE, LOWER ATTACH FITTING IN BOX FRAME AT STA 280, LONGERON 27 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-8 AND SDR RRXA991121Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR SUPPORT UNDER CLIP NUTS AT STA 1746 BETWEEN BL 1-1/2 LEFT AND 20-1/2. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED H CHANNEL AND INSTALLED IAW DCSDR RRXA991120Floorbeam · corrosionDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR SUPPORT AT STA 1726, BL 31 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED H CHANNEL AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-8. (CORROSIONSDR RRXA991119Floorbeam · crackedDURING A MAINTENANCE VISIT FOUND CORROSION CRACKS, FUSELAGE, FLOOR SUPPORTS AT STA 1700 BL 29 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED H CHANNEL AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-8. (COSDR RRXA991118Floorbeam · crackedDURING A MAINTENANCE VISIT FOUND CORROSION CRACKS, FUSELAGE, FLOOR SUPPORTS, AT STA 1680 BL 35 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED H CHANNEL AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-8. (CSDR RRXA991117Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, NR 3 STUB WING, UPPER SURFACE EMANATING FROM RIVET 2 FWD OF FRONT SPAR AT STA XS 227.335. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DSDR RRXA991116Floorbeam · crackedDURING A MAINTENANCE VISIT FOUND CORROSION CRACKS, FUSELAGE, FLOOR SUPPORTS, AT STA 1680, BL 14 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW SUPPORT AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-8SDR RRXA991115Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING L/E, AROUND SCREW HOLES LEFT WING L/E CENTER SECTION UPPER SURFACE BETWEEN XFS 304.000 TO XFS 397.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED ASDR RRXA991114Frame · crackDURING A MAINTENANCE VISIT FOUND A CRACK, FUSELAGE A PIT FRAME DOOR BETWEEN BOLTS AT STA 280, BETWEEN LONGERONS 26 RIGHT AND LONGERON 27 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FRAME PER DWG SDR RRXA991113Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING L/E, I/B L/E TANK UPPER SURFACE AROUND SCREW HOLES BETWEEN XFS 151.205 AND XFS 157.500. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FSDR RRXA991112Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING L/E, TANK UPPER SURFACE AT SCREW HOLES BETWEEN STA XFS 95.000 AND XFS 101.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICASDR RRXA991111Support · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, FUSELAGE, C/D PIT DIVIDER AND SUPPORT FORMER CRACKED AND TORN. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PARTITION IAW FAA APPROVED TENNESSEE SDR RRXA991110Guard · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, CABIN, LONG SECTION OF MAIN CARGO SEAL GUARD BUMP RAIL AT STA 210 (EO). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. WELDED CRACKED AREA IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROSDR RRXA991109Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING L/E, IMPROPER REPAIR LEFT WING O/B L/E O/B SECTION LWR SURFACE BETWEEN STA 822.50 TO XFS 841.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSDR RRXA991108Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, LEFT WING, O/B FLAP LOWER SURFACE SKIN BULGED AND 2 CRACK 3 BELOW L/E, JUST UNDER CENTER HINGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLESDR RRXA991107Flange · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, RIGHT WING, O/B FLAP, NR 3 WEDGE I/B LOWER MOUNTING FLANGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NUT PLATE IAW FAA APPROVED TENNESSEE TECH
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