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 UPS08851765Floorboard · crackedINSPECTION TYPE:C2 FLT DECK PANEL 682A HAS DOUBLE DRILLED HOLES WITH NO ED AND ALL HAT CHANNELS CHAFED. FABRICATED AND INSTALLED 1 WEB AND 6 HAT CHANNELS IAW DWG 56935 7 AND S275589.SDR UPS08851758Floor Panel · corrodedINSPECTION TYPE:C2 FLT, DECK FLOOR PNL 678 HAS MANY BADLY BUCKED RIVETS WITH SOME HAT CHANNEL RADIUS, ALSO CORROSION AROUND FASTENER HOLES. FABRICATED FLT DECK FLOOR PANEL NR 678 IAW SRM 57-07-00 FIG 049B.SDR UPS08851741Seat Track · gougedINSPECTION TYPE:C2 CABIN STA 1520 LBL60 SEAT TRACK GOUGED. CABIN SEAT TRACK AT STA 1520 AND LBL 60, REPAIRED IAW EO DC8-5340-7779-B.SDR UPS08851751Floorboard · damagedINSPECTION TYPE:C2 COCKPIT FLOORPANEL 680 HAS LARGE FIELD REPAIR, DAMAGE CHANNELS AND SKIN. FABRICATED COCKPIT FLOORPANEL 680 IAW DWG 3619352 AND S2755898, SRM 51 -1-8 AND SRM 51-01-21.SDR UPS08851737Panel · corrodedINSPECTION TYPE:C2 COCKPIT FLOOR PNL 676E HAS CORROSSION. REPAIRED COCKPIT FLOOR PNL, BY FABRICATION IAW SRM 53-07-03 FIG 001.SDR UPS08851736Floor Support · crackedINSPECTION TYPE:C2 FLOOR PNL F25 HAS CRACKED U-CHANNEL. REPAIRED FLOOR PANEL F25 IAW SRM 53-07-03 FIG 001, SRM 51-1-21 AND SRM 51-1-8.SDR UPS08851694Skin · dentedINSPECTION TYPE:N/A DENT APPROX 12 INCHES ABOVE MAIN STATIC PORT ON RT SIDE OF A/C. INSPECTED PER EO DC8-5330-28630-A. NO FURTHER DEFECTS NOTED. A 30 DAYS PERM REPAIR ACCOMPLISHED HFEC OF AREA PER DC8 SPM 06-10-01-001, NO CRACKS DETECTED. OK FOR SERVICE.SDR UPS08851687Beam · crackedINSPECTION TYPE:N/A AFT PRESS BULKHEAD J BEAM CRACKED. REMOVED FASTENERS 6" L & R OF BL 0 FOR ACCESS FOR FOM. REPAIRED PER EO DC8-5310-6598-C. MATCH DRILLED 3 REPAIR ANGLES AND CLIPS. ACCOMPLISHED APPENDIX B STEPS 7 - 12.SDR UPS08851672Latch · brokenINSPECTION TYPE:N/A EMERGENCY ESCAPE SLIDE HAS BROKEN LATCH. SLIDE INOP FOR CREW ENTRY DOOR. DEFERRED CREW ENTRY DOOR SLIDE PER MEL 52-7-4. SLIDE IS SECURED IN SUITCASE. REMOVED SLIDE COVER AND ROUTED TO SHEET METAL. REMOVED AND REPLACED LATCH REF DCI SRMSDR IXXA08SMN069SLink · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FLAP MECHANISM OF INNER WING FORWARD LINK CRACKED AT STATION 3.000 RIGHT. REMOVED REPLACED INNER WING FORWARD LINK OF FLAP MECHANISM IAW OHM 27-27-1 PAGE 4. PERFORMED OPS CHECK TO ALL FLIGHT CONTROLS. GOOD IAW DC8 MASDR IXXA08SMN068SDrive Link · bentDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LINK AT FLAP DRIVE LINK BENT AT STATION 3.000. REMOVED AND REPLACED LEFT WING FLAP DRIVE LINK IAW DC8 MAINTENANCE MANUAL 20-16-0 PAGE 202. PERFORMED OPS CHECK TO ALL FLIGHT CONTROLS. OPERATIONAL CHECK GOOD SDR UPS08851613Gauge · unserviceableESCAPE SLIDE PRESSURE GAUGE NOT VISIBLE. REPOSITIONED SLIDE IN CASE FOR PRESSURE GAUGE TO READABLE FROM WINDOW.SDR UPS08851598Lamp · inoperativeGLARESHIELD HAS ONE EMERGENCY LIGHT INOP. RELAMPED AND TESTED IAW MM 33-13-00-2. OPS CHECK GOOD.SDR UPS08851593Cowling · dentedINSPECTION TYPE:IN NR 3 ENG I/B FAN COWL HAS 1 EA DENT AT L/E AT APPROX 7 O'CLOCK POS. INSPECTED DENT FOUND TO BE 2" DIA BY .045" DEEP WITH DISBOND. PERMANENT REPAIR WITHIN ONE WEEK PER EO DC8 7110 4284 C. TRANSFERRED TO D3681 89.SDR UPS08851569Hose · chafedTHE CREW EXPERIENCED A HYDRAULIC LEAK. AFTER RUNNING THE CHECKLIST, DECLARED AN EMERGENCY AND CONTINUED TO PHL. AFTER APPROX 20 MIN IN CRUISE, LOST HYD QTY DOWN TO AUX AT THE "X" AND AIL CTRL MANUAL AND RUDDER CTRL MANUAL LTS ILLUM. RAN LOSS OF HYD FLUID/PRSDR UPS08851588Circuit Breaker · failedON PREFLIGHT, EMERGENCY EXIT LIGHTS CAME ON WHEN ARMED. FOUND EMERGENCY EXIT LIGHT CONTROL C/B BAD. REMOVED AND REPLACED SAME PER MANUAL 20-60-01. SYS OPS CKS PER MM 33-50-02-2. OK FOR SERVICE.SDR UPS08851587Battery · malfunctionedEMERGENCY LIGHTS CAME ON AT TAKEOFF WITH THE SWITCH IN THE "ARMED" POSITION. THE LEFT EMERGENCY BUSS WAS OPERATING NORMAL. T/S EMERGENCY EXIT LIGHT SYSTEM. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY AND RELAY UNIT PER MM 33-50-01-2. SYSTEM OPS CKS GSDR UPS08851568Circuit Breaker · inoperativeON PREFLIGHT, EMERGENCY LIGHTS WILL NOT DISARM. FOUND EMERGENCY EXIT LIGHT CONTROL C/B BAD. REMOVED AND REPLACED SAME PER DOUGLAS STANDARD MANUAL 20-60-01. SYS OPS CKS NORMAL PER MM 33-50-02-2. OK FOR SERVICE.SDR UPS09854453Slide · out of positionINSPECTION TYPE:N/A ESCAPE SLIDE FELL OUT OF HOLDER. DEFERRED SLIDE PER MEL M393690 ASSIGNED. INSTALLED EVACUATION SLIDE IAW M/M 25 60 01 2. THIS CLEARS M393690.SDR UPS08851558Doubler · crackedWING INTERNAL DOUBLER CRACKED ABOVE NR 4 FILL VALVE. ACCOMPLISHED STEPS 6A1 THRU 6A4 ON PRELIMINARY EO NR DC8-5730-28500-A DATED 1-28-08. ACCOMPLISHED STEP 6AS-6AG. OK TO INSTALL REPAIR. COMPLETED REMAINING STEPS THRU 6A(9) OF EO DC8-5730-28500.SDR UPS08851577Skin · crackedSKIN CRACK AT UPPER EDGE NEAR AFT CURVE OF L1 DOOR APPROX 1/2 INCH LINEAR, PARALLEL TO T/E OF DOOR. PERFORMED INTERIM REPAIR IAW UPS EO NR DC8-5210-28486-A PARAGRAPH 6A. PERM REPAIR OR PART REPLACEMENT WITHIN 25 FLIGHT CYLES. D367801 ASSIGNED BY AMC.SDR DHLA200800009Fire Detector · malfunctionedFLT 160, DURING START OF DESCENT, NR 1 ENG FIRE WARNING LIGHT ILLUMINATED AND WARNING BELL ACTIVATED INTERMITTENTLY FOR 5 SECS IN DESENT "A LOOP' PER MEL 26-2-3 CAT C MDDR NR 31535 PLACARD INSTALLED, S/P COMPLIED WITH M/M 26-10-0. R7R FIRE DETECTOR CONTROL BOSDR UPS08851559Lamp · inoperativeFLIGHT DECK EMERGENCY LIGHTS INOP. RELAMPED, OPS CHECK GOOD PER MM 33-50-02-2-2.SDR UPS08851552Light · inoperativeGLARESHIELD HAS ONE EMERGENCY LIGHT INOP. RELAMPED AND TESTED IAW MM 33-13-00-2. OPS CHECK GOOD.SDR IXXA080004OSwitch · defectiveDURING CLIMB FROM KTOL, AFTER GEAR WAS RETRACTED DOOR NOT LATCH LIGHT CAME ON, THE CREW CYCLED THE GEAR THE LIGHT STAYED ON. THE CREW ACCOMPLISHED UPLATCH CHECK AND CYCLED THE GEAR A SECOND TIME THE LIGHT STAYED ON. THE CREW CLIMB TO 32,000 FEET CYCLED THE GSDR DHLA200800031Fire Detector · malfunctionedFLT NR 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. DEFERRED PER MEL 26-2-3 A-LOOP DMI NR 31485 PLACARD INSTALLED CAT C B-LOOP OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 26-10-0. REMOVED AND RESDR DHL2007873539Floorbeam · damagedMAIN CARGO COMPT FLOORBEAM MISDRILLED HOLE AT STA 781.500 LBL.38.125 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-11-08 EVA D853-00038 REV IR DATED 01-09-08, SEMAN DWG ED-4676 DATED 01-05-08. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUSDR DHL2007873538Skin · crackedLT OUTER WING OTBD L/E UPPER SKIN CRACKED 1" AT STA XW 761.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM DATED 01-12-08 EVA D857-00037 REV IR DATED 01-08-08 REV IR SEMAN DWG NR ED-4670 DATED 12-12-07. REMOVED FASTENERS IAW SRM 51-1-21 SRM 51-1-20D.SDR DHL2007873531Skin · damagedLT WING INBD L/E LWR SKIN HOLES ELONGATED AT STA XILD 42. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-11-08 EVA D857-00033 REV IR DATED 01-04-08 SEMAN DWG ED-4624 DATED 01-03-08. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION PLUS FABRICSDR DHL2007873528Bracket · crackedLT ELEVATOR CONTROL TAB BRACKET CRACKED STA 75. REMOVED AND REPLACED LT ELEV CONTROL TAB BRACKET AT STA 75 IAW SRM 51-1-21, SRM 51-1-20D. REFER TO NR 107757 FOR FLT CONTROL OPS CHECK, AND NR 107816 FOR WEIGHT AND BALANCE.SDR UPS08851545Light · inoperativeON SHUTDOWN CHECKLIST, EMERGENCY EXIT LIGHTS DOES NOT ILLUMINATE. IN DISARM POSITION LIGHT WILL NOT PRESS TO TEST. RELAMPED EMERGENCY EXIT INDICATION LIGHT PER STD PRACTICES. OPS CHECKS NORMAL.SDR IXXA080003OConnector · looseDURING CRUISE FROM KTOL NUMBER THREE FIRE WARNING LIGHT STARTED TO FLICKER AND HORN SOUNDED. THE CREW TESTED NUMBER THREE ENGINE FIRE WARNING NO BELL OR LIGHT, PERFORMED FIRE DAMAGED CHECK LIST PULL FIRE HANDLE FORWARD TEST FIRE WARNING TESTED GOOD ALL ENGINESDR DHLA200800032Fire Detector · malfunctionedFLT NR 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. DEFERRED PER MEL 26-2-3 A-LOOP DMI NR 31485, PLACARD INSTALLED CAT C B-LOOP. OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 26-10-0. REMOVED ANDSDR DHLA200800030Fire Detector · malfunctionedFLT NR 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. DEFERRED PER MEL 26-2-3 A-LOOP DMI NR 31485 PLACARD INSTALLED CAT C B-LOOP OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 26-10-0. REMOVED AND RESDR DHL2007873530Skin · corrodedCORROSION BETWEEN SKIN INSERT SURROUNDING "A" LWR CARGO DOOR JAMB AND PLATING AT BS 280 L-24R TO L-28R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-21-08 EVA D853-00036 REV IR, SEMAN DWG NR ED-4678-1. REMOVED FASTENERS IAW SRM 51-1-21 SRM 51-1-20D. SDR UPS08851544Structure · missingAPPROX 3/8 BY 1 INCH PIECE OF SHEETMETAL MISSING ON T/E OF WING. LOCATED ON LT WING INBD OF NR 3 SPOILER PANEL. ACCOMPLISHED EO DC8-5730-28460A.SDR DHLA200800008Fire Warning · malfunctionedFLT 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. DEFERRED PER MEL 26-2-3 A-LOOP DMI NR 31485 PLACARD INSTALLED CAT C B-LOOP, OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 26-10-0. REMOVED AND REPSDR DHL2007873537Skin · corrodedLT WING CTR L/E EXT SKIN SHOWS CORROSION AT STA XFS 341.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA-FORM 8110-3 DATED 01-14-08 EVA D857-00034 REV IR DATED 01-05-08 SEMAN DWG ED-4677-1 DATED 01-03-08. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED CORROSISDR UPS08851524Skin · chafedLEFT WING INBOARD LATERAL CONTROL SPOILER LOWER SURFACE IS CHAFFED ALONG T/E. INSTALLED NEW SPOILER ASSEMBLY IAW DC8 AMM 27-61-01-2, PARAGRAPH 3B STEPS 1 THROUGH 6.SDR DHL2007873521Bracket · brokenRT AIL BRACKET ASSY BROKEN (MAJOR REPAIR) INBD AIL. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED BROKEN FITTING IAW SRM 57-1-0 PG 1 SRM 51-1-21 SRM 51-1-20D. CLEANED, TREATED, PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21 SRM 51SDR DHL2007873519Frame · crackedLT WING L/E CONSTANT SECTION UPPER FORMER CRACKED 1 1/4" STA XCW 69.000. REMOVED CRACKED FORMER IAW SRM 51-1-20D, SRM 51-3-0. FABRICATED NEW FORMER (AL7075"0" 0.090") IAW SRM 57-3-3 FIG. 1, DOUGLAS DWG 5769646. HEAT TREATED FORMER FROM 7075"0" TO 7075T6 IAWSDR DHL2007873529Angle · crackedNR 3 ENG ANGLE CRACKED 2" STA YN 163.535 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 01-08-08 BOEING MSG NR 1-746231818-2 DATED 01-09-08. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED NDT INSP TO VERIFY CRACK DO NOT EXTSDR DHL2007873520Skin · delaminatedNR 1 RT SPOILER UPPER SKIN DELAMINATED. REMOVED AND REPLACED NR 1 RT SPOILER IAW MM 27-61-1 PG 201-206. REFER TO NR 107757 FOR OPS CHECK.SDR UPS08851495Girt Bar · dirtyGIRT BAR JAMS ON RIGHT SIDE. CLEANED DEBRIS FROM GIRT BAR FLOOR LATCH AND LUBED. OPS CHECKS GOOD.SDR UPS08851446Battery Pack · inoperativeEMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY. OPS CHECK GOOD, REF AMM 33-50-01-2, P/N ON 60-1223-5, S/N ON 341.SDR DHL2007873523Skin · wornRT OUTBD FLAP UPPER SKIN WORN AT STA XF 210.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-14-08 EVA NR 0857-00032 REV IR DATED 01-05-08 SEMAN DWG ED-4680 DATED 01-02-08. REMOVED DAMAGE SKIN SEGMENT IAW SRM 51-1-21. FABRICATED NEW SSDR DHL2007873517Fitting · crackedLWR FUSELAGE END FITTING CRACKED 8" STA 719.000 L-34R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-SDR DHL2007873543Floorbeam · damagedMAIN CARGO COMPT FLOORBEAM MISDRILLED HOLE AT STA 680.000 LBL 15.187 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-15-08, DWG AE85-53-101 REV IR DATED 12-28-07,EVA D85300030 REV IR DATED 01-02-08. CUT OUT DAMAGED SECTION AND FABRICATED SDR DHL2007873541Floorbeam · damagedAFT CARGO COMPT FLOORBEAM 1/4" MISDRILLED HOLE AT STA 1040.000 RBL 56" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-15-08 EVA D85300031 REV IR DATED 01-04-08 DWG AE85-53-102 REV IR DATED 01-03-08. REMOVED FASTENERS IAW SRM 51-1-20D. FSDR DHL2007873527Skin · misrepairedRT OUTBD AILERON UPPER SKIN HAS A NON-STANDARD REPAIR AT STA XA 653.000, MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 4 PG9. REMOVED PANEL PLATING WITH NON-STANDARD REPAIR ON IT IAW SRM 57-1-0 PG1 SRM 51-1-21. FABRICATED PLATING, DOUBLER IAW SRM
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