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 RRXA991698Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E BETWEEN Y=280 TO Y=580 AND X=45. 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 DSDR UPS99830555Web · corrodedINSPECTION TYPE:C3, FITTING CRACKED INSIDE RT FWD SERVICE DOOR TORQUE BOX AT LWR FWD CORNER OF DOOR FRAME. REMOVED WEB TO GAIN ACCESS TO FITTING AND FOUND WEB & ANGLE TO BE CORRODED BEYOND LIMITS. REMOVED FITTING, FABBED NEW FITTING, NEW WEB AND ATTACH ANGLESDR UPS99830546Bulkhead Angle · corrodedINSPECTION TYPE:C3, CORROSION ON AFT PRESS BULKHEAD FLOORBOARD SUPPORT ANGLE ABOVE LONG 32R. EXFOLIATED BEYOND LIMITS IAW DC8 SRM 53-2-0. FABBED NEW ANGLE IAW DWR NR 5753522. LOCATED, DRILLED AND DEBURRED NEW ANGLE, OK TO TREAT IAW DC8 SRM 51-3-2.SDR UPS99830542Jamb · crackedINSPECTION TYPE:C3, MAIN CABIN R-1 DOOR JAM IS CRACKED AT STATION 190 L21R. REMOVED DAMAGED WEB, FABBED AND INSTALLED WEB IAW DC8 SRM 51-1-8, 53-2 -0, 51-1-21 & DAC DWG 5615700.SDR UPS99830480Fitting · crackedINSPECTION TYPE:C3 STA 680 L6R END FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.SDR UPS99830479Fitting · crackedINSPECTION TYPE:C3 STA 680 L10R END FTG CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.SDR UPS99830477Frame · crackedINSPECTION TYPE:C3 1 EA HOLE DRILLED THROUGH RT FWD SERVICE DOOR INNER SKIN IN CLOSE PROXIMITY TO ADJACENT RIVET LOCATED AT LOWER AFT CORNER OF DOOR. 51-9-0 INSTALLED FASTENERS IN PREVIOUS DOUBLER ON SKIN IAW DC8 SRM 5 1-1-2, SRM 51-1-20D. INSTALLED SEAL RETSDR UPS99830452Pan · damagedINSPECTION TYPE:C3, 1 HOLE IN AFT SIDE OF RT FWD SERVICE DOOR PAN AT APPROX LONG 14R DOT S815. FABRICATED AND INSTALLED DOUBLER, FILLER AND SEAL RETAINER IAW DC8 SRM 52-2-0, 51-1-9 & 51-3-0.SDR UPS99830251Intercostal · crackedINSPECTION TYPE:C1, THE INTERCOSTAL AT FS 1240 AND LONGERON 33L IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL IAW DWG 5751516 AND SRM 51-1-21.SDR RRXA991175Line · leakingEN ROUTE TO TJBQ LOSS OF HYDRAULICS, PERFORMED LOSS OF HYD. CHECKLIST PER QRH. FOUND RUDDER PUMP PRESSURE LINE LEAKING, REPLACED LINE. LEAK AND OPS CHECKED NORMAL. SERVICED HYD RESV.SDR UPS99830541Skin · corrodedINSPECTION TYPE:C3, FUSELAGE SKIN EXTERIOR BULGED STA 620 L33R-L34R DOT S851. REMOVED CORROSION AND FOUND SKIN TO BE BEYOND ALLOWABLE LIMITS. REMOVED SKIN AND INTERNAL DOUBLERS. FABBED AND INSTALLED NEW SKIN AND DOUBLERS IAW DC8 SRM 53-4-1, 51-1-8, 51-1-20DSDR UPS99830453Fitting · corrodedINSPECTION TYPE:C3, 2 FITTINGS STA 1180 LONG 35 AND LONG 34 RT CORRODED. REMOVED Z FITTINGS IAW DC8 SRM 51-1-20D, INSTALLED NEW FITTINGS (P/N #3755841-50IN) (P/N 3755843-50) IN IAW DCI SRM 51-1-20D.SDR UPS99830303Angle · crackedINSPECTION TYPE:C123, FWD LWR FILLET AREA, FILLET ATTACH ANGLE CRACKED, STA 680 L31L-L32L. FABRICATED AND INSTALLED ANGLE IAW DC8 SRM 53-2-0, 51-1-20D.SDR RRXA991398Strut Pin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RT MLG RETRACT CYL A-PIN REPAIR/INSP IAW MA-A1 3210-01-03, S/B 32-102. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED EYE BOLT, RETRACT PIN AND REMOVED CORROSION FSDR RRXA991397Strut Pin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT MLG RETRACT CYL A-PIN REPAIR/INSP IAW MA-A1 3210-01-03, S/B 32-102. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED EYE BOLT, RETRACT PIN, REMOVED CORROSION FRSDR UPS99830460Longeron · crackedINSPECTION TYPE:C3, LT WHEEL WELL, STA 879, LONG 24, EXTERIOR FACE HAS 4 INCH CRACK. FABRICATED AND INSTALLED ANGLE IAW TIMCO REO NR 06638. INSTALLED FRAME FITTING FS 879 IAW DC8 SRM 51-1-20D, AND 51-3-0.SDR RRXA991404Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING UPPER SKIN AT STA 107.000 STR 9. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLUG AND DOUBLER IAW DC8 SRM 57-2-1.SDR RRXA991385Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LOWER CARGO COMPARTMENT BETWEEN STA 1020 AND STA 1060, AND BETWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT, ON SKIN. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-SDR RRXA991172O Ring · failedAT TIME 14:13-Z ON BOTH HYD PUMPS WITH RES LOW PRESS LT ON. AUX PUMP WOULD ONY BUILD UP TO 1000 PSI, QUANITY STAYED AT 3/4. FLAPS SHOWED A SPLIT WHEN SYSTEM PRESSURIZED IN THE BYPASS POSS. FOUND BLOWN O-RING ON SLOT CONTROL VALVE. REPLACED O-RING ON SLOT CSDR UPS99830213Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT XCW 69 IS CRACKED AT THE UPPER END. STOP DRILLED CRACK AND REPAIRED IAW 57-2-0 FIG 2.SDR RRXA991483Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766 BETWEEN LONGERONS 10 LEFT AND LONGERON 11 LEFT, APPROX 2-1/2, BETWEEN BL 25.0 RIGHT AND BL 27.250 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRMSDR RRXA991481Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766, I/B AREA BETWEEN LONGERONS 10 RIGHT AND LONGERON 11 RIGHT, A 2.75 CRACK BETWEEN BL 24.750T LEFT AND BL 27.250 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA SDR UPS99830250Shear Tie · crackedINSPECTION TYPE:C1 FS 1060 BETWEEN LONGERON 35R AND 36, THE SHEAR-TIE IS CRACKED. CUT OUT DAMAGED SECTION AND REPAIRED SHEAR-TIE IAW SRM 53-2-0 FIG 2B.SDR RRXA991490Skin · dentedDURING A MAINTENANCE VISIT FOUND DENT, NR 1 ENGINE RING COWL AT 5 O'CLOCK POSITION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. CUT ACCESS HOLE, STRAIGHTENED DENT WITHIN LIMITS DC8 SRM 71-5-2. FABRICATED AND INSTSDR RRXA991426Support · damagedDURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY AT STA 339.723 LEFT AND RIGHT POSITIONS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINK SUPPORT ASSY IAW DC8 M/M SDR RRXA991713Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL BETWEEN Y=968 TO Y=973 AND BETWEEN X=45 TO X=59. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FSDR RRXA991712Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL BETWEEN Y=949 TO Y=952 AND BETWEEN X=45 TO X=59. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FSDR UPS99830249Fitting · crackedINSPECTION TYPE:C1 AT FS -12, LONGERON 33L FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4640111 AND SRM 51-1-20D, 51-1-21, AND 51-3-0.SDR UPS99830248Longeron · corrodedINSPECTION TYPE:C1 BETWEEN FS 35 AND 8 LONGERON 36 IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG 3615532 AND SRM 51-1-20D.SDR UPS99830245Seat Track · corrodedINSPECTION TYPE:C1 DOUBLE SEAT TRACK AT FS 440, RBL 48, IS CORRODED OUT BEYOND LIMITS. CUT OUT DAMAGED SECTION AND SPLICED IN A NEW SECTION OF SEAT TRACK IAW SRM 53-2-3.SDR RRXA991752Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERIOR SKIN PANEL BETWEEN Y=857 TO Y=980 AND LONGERON 36. 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 APPRSDR RRXA991684Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERNAL SKIN BETWEEN Y=857 TO Y=980 AND LONGERON 36. REMOVED DAMAGE SKIN, TREATED AREA IAW DC-8 SRM. FABRICATED AND INSTALLED NEW SKIN PANEL IAW DC-8 SRM 53-3-0.SDR RRXA991407Sump Heater · failedDURING A MAINTENANCE VISIT FOUND BURN, LEFT CENTER FUEL DRAIN HEATER BURNED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED SUMP HEATER BLANKET IAW DC8 M/M 28-10-3. OPS CHECKS GOOD IAW DC8 M/M 2SDR UPS99830247Fitting · corrodedINSPECTION TYPE:C1 FS 1220 TO 1230, LONGERON 31R END FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-3-0.SDR UPS99830246Fitting · corrodedINSPECTION TYPE:C1 FS 1160, BETWEEN LONGERON 32R AND 33R, THE BATH TUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 5-1-20D.SDR RRXA991427Skin · crackedDURING A MAINTENANCE VISIT, FOUND CRACK IN ACCESS PLATE LAND RIGHT WING FUEL TANK PLATE 505E AT STA 191.000. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED IAW DC8 SRM 57-2-1 AND IAW FAA APPROVED TENNESSEE TSDR RRXA991414Access Panel · crackedDURING A MAINTENANCE VISIT FOUND CRACK IN ACCESS PLATE LAND RIGHT WING, FUEL TANK PLATE 505E AT STA 191.000. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS FROM 7075-T6 .160 LOT NR 3SDR UPS99830237Jamb · crackedINSPECTION TYPE:C1 FS 270, THE MAIN CARGO DOOR LOWER DOOR JAMB IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE JAMB IAW DWG 5772786 AND SRM 51-1-20D AND 51-1-20.SDR UPS99830236Fitting · crackedINSPECTION TYPE:C1 FS 834 AT LONGERON 18L, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.SDR RRXA991509Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION BLISTER AT STA 1766, LONGERON 10 RIGHT, 24 LEFT OF RBL ON STAB FRONT SPAR ANGLED WEB DIRECTLY BEHIND AFT BULKHEAD INSIDE ACCESS HOLE 60. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRSDR RRXA991505Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AT STA 718, LONGERON 35 RIGHT ON EXTERNAL SKIN UNDER FWD FILLET PANEL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FAA APPSDR UPS99830290Floorbeam · corrodedINSPECTION TYPE:C1 FS 879, RBL 12, THE CABIN FLOORBEAM HAS HEAVY CORROSION. REPAIRED FLOORBEAM IAW DH SK866-318.SDR UPS99830289Floorbeam · corrodedINSPECTION TYPE:C1 FS 717, RBL 30, THE FLOORBEAM HAS HEAVY CORROSION. REPAIRED FLOORBEAM IAW DH SK866-291.SDR UPS99830235Doubler · crackedINSPECTION TYPE:C1 RT WING L/E LOWER SKIN INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE AT XFS 572.5. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21 AND 51-1-20D.SDR UPS99830234Rib · crackedINSPECTION TYPE:C1 LT WING L/E RIB AT XS 461.372 IS CRACKED AT THE AFT LOWER FASTENER. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS99830233Rib · crackedINSPECTION TYPE:C1 LT WING L/E RIB AT XFS 385.25 IS CRACKED AT THE AFT LOWER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830232Rib · crackedINSPECTION TYPE:C1 LT WING L/E LOWER RIB AT XOLDI 6.225 IS CRACKED AT THE AFT FASTENER. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR RRXA991711Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-3 BETWEEN Y=940 TO Y=980 AND X=50. 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 RRXA991619Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, A PIT DOOR HINGED SILL GUARD RAMP FWD SUPPORT ANGLE LWR END BOLT HOLE AND CRACKED BETWEEN STA 280 AND STA 320. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRSDR UPS99830288Floorbeam · crackedINSPECTION TYPE:C1 FS 140, LBL 44, THE FLOORBEAM IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW DH SK866-902.
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