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 UPS03840019Skin · crackedINSPECTION TYPE:C-2 CRACK INDICATION THROUGH PAINT AT RT AFT TYPE 2 EMERGENCY EXIT DOOR CUTOUT UPPER AFT CORNER STA 1340 L12R. REMOVED FASTENERS IN REPAIR AREA, CUTOUT CRACKED AREA OF OUTER SKIN AND FABRICATED -15 DOUBLER -17 DOUBLER AND -19 FILLER IAW TINCO SDR UPS03840083Skin · crackedINSPECTION TYPE: C-2, R1 UPPER FWD DOOR JAMB CORNER EXTERNAL FUSELAGE SKIN CRACKED AT FASTENER HOLE OF FIRST FASTENER ROW AT APPROX 45 DEGREES POINT OF CORNER RADIUS. REMOVED DAMAGE AREA, FABBED FILLER, DOUBLER, TRIPLER IAW DC8 SRM 53- 2-0 AND REVISION 53-15SDR UPS03840080Skin · crackedINSPECTION TYPE: C-2, L2 LWR FWD DOOR JAMB CORNER EXTERNAL FUSELAGE SKIN CRACKED AT SECOND FASTENER HOLE BELOW TRIMOUT. ROUTED OUT CRACKED AREA IAW DC8 SRM 53-2-0. VERIFIED CRACK REMOVED IAW NDT SPM 06-10-01.001. FABBED -7 & -9 DOUBLERS AND -19 FILLER IAW SDR UPS03840008Skin · crackedINSPECTION TYPE: C-2, FUSELAGE EXTERIOR SKIN CRACKED STA 1750 L15L-16L. CONFIRMED CRACK WITH HFEC IAW NDT SPM 06-10-01. FABRICATED FILLER AND DOUBLERS IAW DC8 SRM 53-2-1, ALODINED AND PRIMED IAW DC8 SRM 51-1- 8, INSTALLED FILLER AND DOUBLERS IAW DC8 SRM 51-SDR UPS03840088Skin · crackedINSPECTION TYPE: C-2, L2 UPPER AFT DOOR JAMB CORNER HAS A CRACK FOUND WITH NDT. CUT OUT CRACKED AREA IAW DC8 SRM 53-2-0 FIG 18. VERIFIED CRACK REMOVAL IAW MD NDT SPM 06-10-01.001. FABIRCATED AND INSTALLED DOUBLER, TRIPLER AND SKIN FILLER IAW DC8 SRM 53-2-0SDR UPS03840076Door Frame · crackedINSPECTION TYPE: C-2, R1 LOWER AFT DOOR JAMB CORNER HAS A CRACK FOUND WITH NDT. REMOVED DAMAGE IAW DC8 SRM 53-2-0. FABBED FILLER, DOUBLER, TRIPLER IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 53-2-0.SDR DHL2002801024Smoke Detector · malfunctioned7 MAIN DECK SMOKE DETECT WILL NOT TEST. REPORTED ON PREFLIGHT (P/N 30-231-4). RELAMPED 7 MAIN SMOKE DETECT AND RESECURED CONNECTOR PLUG. NO HELP. DEFERRED FURTHER TROUBLESHOOTING AND REPAIR PER MEL 26.6 CAT. "C". PLACARD INSTALLED DMI #11389.SDR DHL2002805054Engine · malfunctionedNR 1 ENGINE FAILED TO ACCELERATE ON TAKE OFF. ABORTED AT 60 KIAS., TOGW. 177.0, OAT. -1 DEGREE C., PRESSURE ALTITUDE 1163. PERFORMED ENGINE CHECK PER JRH ACCELERATION DECELERATION CHECKED OK, POWER MANAGEMENT CONTROL (PMC) CHECK FAILED, PER JRH 13.4 & 15.2,SDR IXXA0200155OEngine · malfunctionedAFTER TAKEOFF FROM MEM, THE FLIGHT CREW NOTICED NR 1 ENGINE INDICATIONS STARTED FLUCTUATING. AFTER ENGINE IDLE DOWN NO CHANGE IN ENGINE INDICATION, THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND SHUTDOWN THE NR 1 ENGINE. THE FLIGHT CONTINUED TO DFW FOR AN USDR DHL2002873003Bracket · failedNR 3 ENGINE SHORT CIRCUIT LIGHT ILLUMINATES INTERMITTENTLY. REMOVED AND REPLACED FIRE LOOP ATTACH BRACKET NR 3 ENGINE AT HIGH STAGE BLEED VALVE AREA PER SRM 51-1-0 AND 51-3-0, OPS CHECKS GOOD.SDR DHL2002873002Control Unit · failedLOWER CARGO SMOKE DETECTOR (AD4338-B). REPORTED ON PREFLIGHT. DEFERRED FURTHER TROUBLESHOOTING AND REPAIR PER MEL 26-10-1 CAT. "C" SMOKE DETECTOR (AD4338-B) DMI 11310. PLACARD INSTALLED. REF. DMI #11310: LOWER CARGO SMOKE DETECTION (AD4338-B), REPORTED ONSDR DHL2002806015Hose1) DURING CRUISE, HYDRAULIC SYSTEM PRESSURE WENT TO ZERO. HYDRAULIC QUANTITY WENT TO THE "AUX" LEVEL. AILERON AND RUDDER CONTROL MANUEL LIGHT ILLUMINATED. (NOTE: DHL EVENT REPORT DATED 12-18-2002 STATES EMERGENCY WAS DECLARED.)2) FOUND LT BOGIE TRIM HYDRAULISDR UPS02839984Amplifier · inoperativeNUMEROUS MAIN DECK SMOKE DETECTORS INOPERATIVE. REMOVED AND REPLACED SMOKE DETECTOR AMPLIFIER. ALL DETECTORS TEST OK.SDR UPS02839982Battery Pack · inoperativeINSPECTION TYPE: PFLT, EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. CHECKS OK.SDR DHL2002801023Smoke Detector1) LOWER SMOKE DETECTOR FB6863 FALSE WARNING.2) TROUBLESHOT SYSTEM FOUND FB6863 SDU BAD. REMOVED AND REPLACED UNIT REPROGRAMMED SYSTEM IAW M/M 26-16-01 AND ST 300.SDR DHL2002801022Smoke Detector · will not testNR 3 CARGO SMOKE DETECTOR WILL NOT TEST. DEFERRED PER MEL 26-6-1. DMI #11218.SDR UPS02839977Connector · failedINSPECTION TYPE: PFLT, EMERGENCY LIGHT DISARM CHECK INOPERATIVE. REPLACED CONNECTOR PLUG P01-1345. SYSTEM CHECKS GOOD IAW M/M 33-50-01SDR DHL2002807014Connector · dirtyAFTER GEAR EXTENSION ANTI-SKID INOP LIGHT CAME ON. GEAR WAS CYCLED, THEN WHEN GEAR WAS PUT DOWN AGAIN ANTI-SKID LIGHT REMAINED EXTINGUISHED. CLEANED CANNON PLUG CONNECTORS AND PERFORMED OPS CHECK OF ANTI-SKID SYSTEM IAW 32-43-4. OPS CHECKED NORMAL.SDR DHL2002807013Wire1) AFTER GEAR EXTENSION, NOSE GEAR LIGHT DID NOT COME ON. GEAR WAS CYCLED. NOSE GEAR LIGHT DID NOT COME ON. APPROACH WAS ABORTED AND DURING GO AROUND GEAR LIGHT CAME ON.2) CLEANED CONNECTOR OPS CHECKED GOOD IAW M/M 32-30-0. FOUND AND REPAIRED BROKEN WIRE IAWSDR UPS02839968Door · damagedINSPECTION TYPE: PFLT, RT FUSELAGE NOSE W/W BELOW VENT DOOR SHEET METAL REPAIR. FERRIED TO TCO. REMOVED DAMAGE IAW DC8 SRM 51-1-21,OUT OF LIMITS IAW DC8 SRM 53-2-0. HEAT TREATED SPLICE CHANNEL & REPAIR SPLICE FABBED SPLICE CHANNEL & REPAIR SPLICE IAW DC8 DWSDR DHL2002801021Bulb1) #14 SMOKE DETECTOR DOES NOT TEST.2) REMOVED AND REPLACED #14 SMOKE DETECTOR TEST LIGHT BULB. OPS CHECKED GOOD PER DC-8 M/M 26-10-6.SDR UPS02839952Battery Pack · dischargedINSPECTION TYPE: ASV, EMERGENCY BATTERY PACK LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER 33-50-00 OPS NORMAL.SDR UPS02839951Light · inoperativeINSPECTION TYPE: ASV, EMERGENCY LIGHTS INOPERATIVE. REPAIRED OPEN AT P1-1345 PIN 11 AS REQUIRED REF WDW 33-50-01. SYSTEM OPS NORMAL.SDR DHL2002807012Smoke Detector · malfunctionedAMBER ANNUNCIATOR ON CARGO COMPARTMENT SMOKE DETECTOR ILLUMINATED IN FLIGHT. CODE AD7515 DISPLAYED. RECONFIGURED LOWER CARGO SDU'S PER SMM 26-15-0. OPS NORMAL.SDR DHL2002801020Seat · lack of lubeSECOND OFFICER SEAT DIFFICULT TO SLIDE FORE/AFT. LUBED SECOND OFFICER SEAT, CHECKED OPERATION IAW MM 25-11-6 OK.SDR UPS02839936Skin · corrodedINSPECTION TYPE: ASV, BULGE LT SIDE RUDDER. RUDDER HAS SKIN BULGE AT APPROX 4 FEET BELOW TIP AND 8 INCHES FROM TRAILING EDGE (BETWEEN LOWER STATIC WICKS) ON LT SIDE OF RUDDER. REMOVED RUDDER IAW MM 27-21-01 P401-P406 INSPCTED VERTICAL STRUCTURE FOR RUDDER SSDR DHL2002807011Seat · malfunctionedCAPTAINS SEAT WHEN IN MOST FOWARD POSITION WILL NOT LOCK. ADUSTED FORE AND AFT LOCK PINS. SEAT CHECKED OK IAW 25-11-1.SDR UPS02839921Battery · dischargedINSPECTION TYPE:N/A DURING BITE CHECK, EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. RECYCLED BREAKER AND CHECK AGAIN. EMERGENCY LIGHTS DID NOT ILLUMINATE SECOND TIME. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER MM 33-50-01 OPS CHECK GOOD.SDR IXXA0200113OActuator · defectiveEN ROUTE FROM DFW TO IAH, THE DOOR NOT LATCHED LIGHT REMAINED ILLUMINATED DURING THE GEAR UP LATCH CHECK. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO IAH FOR AN UNEVENTFUL LANDING. MAINTENANCESDR IXXA0200112OSwitch · looseENROUTE FROM DFW TO TOL, THE LANDING GEAR LIGHT REMAINED ILLUMINATED FOLLOWING LANDING GEAR EXTENSION. THE FLIGHT CREW RECYCLED THE GEAR AND THE LIGHT FLICKERED THEN REMAINED ILLUMINATED. THE CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED FOR AN UNEVENTFUL LSDR UPS02839899Battery Pack · dischargedINSPECTION TYPE:ASV EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, CKS OK.SDR IXXA0200109OCylinder · defectiveENROUTE FROM LAX TO TOL, THE LANDING GEAR DOOR NOT LATCHED LIGHT REMAINED ILLUMINATED FOLLOWING LANDING GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR AND THE LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED SDR DHL2002804012Engine · slowRTO A/C WT. 260.0, 9 DEG. C., PRESSURE ALTITUDE SL. ATTEMPTED ROLLING TAKE OFF, NR 4 ENGINE SLOW TO SPOOL. CAPTAIN DECIDED TO RESTART TAKE OFF. AIRSPEED < 20 KTS.SDR DHL2002873001Battery · inoperativeEMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY RACK ASSEMBLY. OPS CHECKS OK IAW M/M 33-50-2.SDR DHL2002804011Fire Loop · malfunctionedNR 1 FIRE HANDLE AND BELL ILLUMINATED AND SOUNDED APPROXIMATELY 3 MINUTES. AFTER ENGINE SHUTDOWN COMPLIED WITH ENGINE FIRE CHECKLIST. NO INDICATION OF FIRE. BOTTLE NOT FIRED. ENGINE VISUALLY INSPECTED BY MAINTENANCE DURING OCCURRENCE. FOUND PYLON FIRE DETSDR DHL2002805053Current Limiter · failedAFTER LANDING WITH LEFT PACK ON, LEFT TEMPERATURE ROSE RAPIDLY AND BURNING ODOR FILLED COCKPIT. FOUND PHASE 1 (F1-1) CURRENT LIMITER BLOWN. REMOVED AND REPLACED. OPERATED PACK FOR MORE THAN 10 MINUTES, NO FAULT FOUND. SYSTEM OPS CHECKED NORMAL IAW M/M 21-55SDR IXXA0200091OFitting · looseEN ROUTE FROM TOL TO ANC, THE FLIGHT CREW NOTICED A DECLINE IN THE MAIN HYDRAULIC QUANTITY SYSTEM. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO ANC FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED A LOOSE FITTING ASDR UPS02839808Seat · malfunctionedINSPECTION TYPE:N/A FE SEAT WILL NOT LOCK IN POSITION. R&R SEAT OPS CK GOOD W/REF TO MM 25-11-02.SDR UPS02839800Slide · inoperativeMAIN CABIN EXIT SLIDE INOP M247198. REPLACED SLIDE CONTAINER AND SLIDE PER MM-25-60-01SDR UPS02839807Battery Pack · inoperativeOPS CK OF EMERGENCY LIGHTS FAILED TO LIGHT UP GLARESHIELD COCKPIT DOME, LAV / COURIER DOME, FWD ENTRANCE. REPLACED EMERGENCY LIGHT BATTERY PACK OPS CK GOOD.SDR UPS02839801Battery Pack · inoperativeEMERGENCY LIGHTS FAILED OP CHECK. REMOVED AND REPLACED BATTERY PACK.SDR DHL2002806014Relay1) #3 ENG "B" LOOP FAILS TO TEST #3 ENG "B" LOOP SELECTED, FIRE WARNING LIGHT WILL START TO LIGHT AND WILL FAIL TEST2) INSTALLED RELAY R2-7003. XFERRED TO DMI 10693 PER MEL 26-2-3 CAT C XFERRED TO DMI 10693 ON LG PG 3193773) REF DMI # 10693 (# 3 ENG. "B" FSDR UPS02839649Battery Pack · dischargedINSPECTION TYPE:ASV EMERGENCY LIGHT SYSTEM INOP. R&R EMERGENCY LIGHT BATTERY PACK OPS CK OK PER DC8 MM 33-50-00.SDR DHL2002805052Wire1) DURING TAXI IN, NOTED ELECTRICAL BURNING SMELL IN CABIN ENTRY AREA2) REPAIRED BROKEN WIRE AT RADIO RACK C/B PER MM 20-50-1. FUEL FLOW C/B REPLACED, LOOSE CONTACTS, AND OPS CK'D PER MM 73-30-1 OK. INSTALLED NEW WATER SEPERATOR BAGS & LEAK CK'D PER MM 21-5SDR UPS02839641Skin · corrodedINSPECTION TYPE:N/A RIVETS POPPED DUE TO CORROSION BETWEEN STA 120 & 130 LONGERON 31R 2 LAP SEAM. REMOVED CORRODED SECTION OF FINGER DOUBLER & SKIN. VERIFIED CORROSION REMOVED ACCOMPLISHED REPAIR PER SRM 53-2-1SDR DHL2002804010Smoke Detector1) #5 SMOKE DETECTOR WILL NOT TEST2) R&R #5 SMOKE DETECTOR IAW M/M 26-10-5. OPS CHECK GOODSDR IXXA0200076OStriker · dirtyAFTER TAKE OFF FROM RMS, THE LANDING GEAR DOOR NOT LATCHED LIGHT REMAINED ILLUMINATED FOLLOWING LANDING GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR AND THE LIGHT WAS EXTINGUISHED. THE FLIGHT CONTINUED TO GSO FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPESDR DHL2002801019Wire · shortedDURING SERVICE CHECK NR 3 ENGINE FIRE DETECTION SHORT LIGHT ALWAYS ILLUMINATED IN B LOOP POSITION. REPLACED WIRE 4W5123C16 FROM R5-7001 TO R5-7007 OPS CHECKED GOOD PER M/M 26-10-0.SDR DHL2002804009Indicator1) REJECTED TAKEOFF AT APPROX. 90 KTS DUE TO NO AIRSPEED INDICATIONS ON CAPT. OR F/O'S AIRSPEED INDICATIONS. NORMAL BRAKING & REVERSE USED.2) PERFORM AISPEED INDICATOR FUNCTIONAL CK BOTH CAPT & F/O CKS GOOD IAW DC 8 MMS 34-11-00. PERFORM PITOT LEAK TEST WISDR UPS02839535Angle · crackedINSPECTION TYPE:SP ANGLE IS CRACKED ON COCKPIT SUBFLOOR STA -100 AT RBL 32. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5616101, AND SRM 51-1-20D.
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