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 IXXA0400031SSkin · damagedDURING ROUTINE C-CHECK INSPECTION FOUND RT WING INBD FLAP UPPER PANEL HAS INTERM REPAIR, STA XW 28.000-XW 86.000 MAJOR REPAIR. REPAIRS ARE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIG 2 PAGE 2. REMOVED INTERM REPAIR ISDR IXXA0400028SSkin · corrodedDURING ROUTINE INSPECTION RIGHT WING CTR L/E UPPER SKIN SURFACE CORRODED (STA XFS 341.500-416.500) MAJOR REPAIR. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D, REMOVED CORROSION FROM UPPER SKIN SURFACE OF LT WING CIR L/E IAW DC8 SRM 51-1-8 PG 1SDR UPS04841958Socket · looseINSPECTION TYPE: ASN, DOOR ENTRY AND EMERGENCY LIGHTING FIXTURE NOT SECURED. SECURED DOOR ENTRY AND EMERGENCY LIGHTING TO HOUSING.SDR IXXA0400033SDoor Frame · crackedDURING ROUTINE C-CHECK INSPECTION AFT PASSENGER DOOR RT UPPER JAMB CORNER WITH .5 INCH CRACK IN IT, STA 1660.000. REPAIRS ARE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 18, FABRICATED FILLER, DOUBLER, TRIPLER IAW DC8 SRM 51-1-8B. APPLIED SDR IXXA0400018SSkin · corrodedDURING A ROUTINE C-CHECK CORROSION WAS DETECTED ON RT WING OUTBOARD LEADING EDGE INNER SECTION UPPER SKIN SURFACE. MAINTENANCE REMOVED DAMAGED SKIN, FABRICATED DOUBLER, CLEANED, TREATED AND PRIMED AREA AT INNER FACE OF DOUBLER. MAINTENANCE THEN INSTALLED DOUBLSDR DHL2004805001Engine · malfunctionedON TAKEOFF ROLL NR 1 ENGINE ROLLED BACKED TO IDLE. CHECKED NR 1 ENGINE MAIN ENGINE CONTROL (MEC) CONTROL RODS, INSPECTED INLET & EXHAUST, CHECKED SPECIFIC GRAVITY, FOUND OK IAW CFM M/M 72-00-00. PERFORMED POWER ASSURANCE CHECK IAW JRH 13.3, FOUND OK. UNABLESDR IXXA0400036SSkin · damagedDURING ROUTINE C-CHECK INSPECTION FOUND TEMPORARY REPAIR OF FUSELAGE EXTERIOR SKIN STATION 1459.000-1512.000 L-31L TO L-34L. REPAIR ACCOMPLISHED, REMOVED DAMAGED AREA IAW DC8 SRM 53-2-1 PG 107-108 FIG 7. FABRICATED FILLER & DOUBLER & FINGER DOUBLER IAW DC8 SSDR UPS04841989Pad · corrodedDROP CORROSION ABOVE WING BOTTLE BOLT, LOCATED IN RIGHT W/W FWD BULKHEAD, UPPER O/B CORNER. REMOVED RIGHT OVERWING EMERGENCY HATCH AND PANEL 292F TO FOM. REMOVED CORRODED PAD FROM RIGHT WHEEL WELL IAW DC8 SRM 51-1-20D. INSTALLED PAD AND PANEL 292F IAW DC8 SSDR UPS04841955Wing Root · corrodedRIGHT WING ROOT HAS CORROSION (EXFOLIATION). A/C FERRIED TO TCO DEFERRED (276424) AND TRANSFERRED TO NRC 469644 RMVD RH OVERWING EMERGENCY HATCH TO FOM. RMVD R/H OVERWING TO FUSELAGE FILLET PNL 292F TO FOM. RMVD CORRODED PAD FR R/H W/W IAW DC8-SRM 51-1 -20. SDR DHL2004809001Fan · noisyON TAKEOFF AND AT CRUISE ALTITUDE, RECIRCULATION FAN IS LOUD & VIBRATION IS FELT UNDERFLOOR NEAR LAV NOISE DECREASES WITH FAN OFF. DEFERRED RECIRCULATION FAN, PLACARD INSTALLED. AT FL 330, 30 MINUTES INTO FLT, NOTED BURNING ODOR IN FLOOR AREA NEAR LAV MID CASDR IXXA0400043SFitting · corrodedDURING A ROUTINE C CHECK FOUND A-CARGO DOOR FITTING CORRODED AT STA 300.00 L34R TO L33R. REPAIR ACCOMPLISHED. REMOVED CORROSION ON CARGO DOOR FITTING STATION 300.00 IAW 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG.2M, REMOVED FITTING, FABRICATED NESDR IXXA0400024SSkin · wornDURING A ROUTINE C-CHECK INSPECTION RIGHT INBOARD FLAP UPPER PANEL DOUBLER HAS WEAR OUT OF LIMITS STA XW.104.000-110.000 MAJOR REPAIR. MAINTENANCE PERFORMED MAJOR REPAIR IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 51-1-21A PG 1-4. FABRICATED NEW PLATING SDR IXXA0400062SSkin · crackedDURING A ROUTINE C CHECK INSPECTION FOUND RT FUSELAGE AFT LOWER CARGO COMPARTMENT FWD DOOR PLATING LOWER SIDE CRACKED AND WEAR DAMAGE BETWEEN STA 1160.00 TO 1220.00.REPAIR WAS ACCOMPLISHED. PERFORMED MAJOR REPAIR IAW DWG V22-R12. REMOVED DAMAGE SKIN SEGMENT ANSDR IXXA0400061SPlate · elongatedDURING A ROUTINE C-CHECK INSPECTION FOUND LT OB SLOT VANE UPPER SURFACE ELONGATEED HOLES STA X0200 67.000 (ON REPAIR DOUBLER). REPAIR WAS ACCOMPLISHED. FASTENERS AND THE EXISTING REPAIR DOUBLER WERE REMOVED IAW DC8 SRM 51-1-21 PG 1 AND 51-3-0 PG 1. DAMAGED SKISDR IXXA0400060SSkin · corrodedDURING C CHECK INSP FOUND LT WING IB LE UPPER SKIN SURFACE CORRODED STA XFS 207.00-212.00. REPAIR WAS ACCOMPLISHED. DAMAGED SKIN ALONG WITH FASTENERS AND CORROSION WERE REMOVED AND FOUND OUT OF LIMITS IAW DC8 SRM. AN NDT INSPECTION WAS PERFORMED IAW DC8 NDT SSDR IXXA0400059SPlate · corrodedDURING A ROUTINE C-CHECK INSPECTION FOUND RT HORIZONTAL STABILIZER LE EXTENAL PART CORRODED STA XFS 341.250. REPAIR WAS ACCOMPLISHED. FASTENERS AND CORROSION WERE REMOVED ALONG WITH THE DAMAGED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1-20D PG1, 51-1-21 PG.SDR IXXA0400044SSkin · corrodedDURING A ROUTINE C-CHECK RT FUSELAGE FORWARD LOWER CARGO COMPARTMENT FWD DOOR PLATING LOWER SIDE INTERIM REPAIR BETWEEN STA FS 280.00 AND FS 340.00. REPAIR ACCOMPLISHED. REMOVED TEMPORARY REPAIR IAW DC8 SRM 51-1-21 PG 1. PERFORMED NDT INSPECTION IAW NDT SPM PASDR IXXA0400023SSkin · wornDURING A ROUTINE C-CHECK FOUND RIGHT OUTBOARD FLAP UPPER PANEL DOUBLER HAS WEAR OUT OF LIMITS, STATION 159.00 - 213.00. MAINTENANCE REMOVED SKIN SEGMENT WITH DOUBLER ON IT. IN ACCORDANCE STRUCTURAL REPAIR MANUAL CHAPTER 57-1-0 AND 57-7-1 FIG 4 AREA WAS CLEANSDR IXXA0400022SSkin · damagedDURING ROUTINE C-CHECK INSPECTION FOUND L/E HOLES ELONGATED ON UPPER SKIN SURFACE, STA XFS 526.000. REPAIR ACCOMPLISHED PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-1 PG 1, DC8 SRM 57-3-3. REMOVED UPPER SKIN SURFACE OF LT WING CTR L/E STA SXF 526.00 IAW DC8 SRM 5SDR IXXA0400049SPlate · corrodedDURING A ROUTINE C-CHECK INSPECTION FOUND CORROSION ON RT OUTER WING IB L/E OUTER PLATING AROUND STA XFS 710.00. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS IAW SRM 51-1-20D PG 21, 51-1-21 PG. 1,51-3-0 PG 1. THE CORROSION AND DAMAGED SKIN WAS REMOVED AND FOUNDSDR UPS04841946Cable · brokenAILERON BINDING ON RIGHT TURN. LEFT AILERON BUSSING CABLE BROKEN AT I/B OF AILERON. INSTALLED LEFT .125 INCH BUSS CABLE PER MM 27-13-22 UP TO STEP (H) ACCOMPLISHED REMAINING STOPS AND ADJUSTED PER MM 27-10-17-5.SDR IXXA0400063SSkin · corrodedDURING A ROUTINE C CHECK INSPECTION FOUND LT OB WING LE OB SECTION SKIN CORRODED STA XW 761.000. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS AND CORROSION ALONG WITH THE DAMAGED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1-20D PG 21, 51-1-21 PG.1, 51-3-0 PG.1SDR IXXA0400058SPlate · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RT INNER WING CTR. LE SLOT OUTER PLATING CORRODED. STA.XW257.000-XFS 310.250. REPAIR WAS ACCOMPLISHED. FASTENERS AND CORROSION WERE REMOVED ALONG WITH THE DAMAGED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1-21 PG. 1, 5SDR IXXA0400057SSkin · corrodedDURING A ROUTINE C CHECK RT WING OB L/E OUTER SECTION UPPER SKIN SURFACE CORRODED, STA. XW 761.000. REPAIR WAS ACCOMPLISHED. FASTENERS AND CORROSION WERE REMOVED ALONG WITH THE DAMAGED AREA IAW SRM 51-1-20D PG 21., 51-3-0 PG. 7, 51-1-21 PG 1. AN NDT INSPECTIONSDR IXXA0400052SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RT WING OB L/E INNER SECTION UPPER SKIN SURFACE CORRODED , STA. XW 485.000. REPAIR WAS ACCOMPLISHED. CORROSION, FASTENERS AND THE DAMAGED AREA WAS REMOVED IAW DC8 SRM 51-1-21 PG1, 51-1-20D PG21,51-3-0 PG.1, 51-1-8 PG 17-SDR IXXA0400050SPlate · corrodedDURING A ROUTINE C CHECK INSPECTION FOUND CORROSION AND CRACK DAMAGE IN FUSELAGE FORWARD CTR. SECTION LOWER PLATING STA. 580.00 L-36. REPAIR WAS ACCOMPLISHED. CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-2-0 PG2M. REMOVED FASTENERS AND DAMAGED SECTSDR IXXA0400048SSkin · crackedDURING A ROUTINE C CHECK FUSELAGE EXTERIOR SKIN WITH 1INCH CRACK AND CORROSION IN IT, STA 1080.000 L-34R. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS ALONG WITH THE CORROSION. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2M. REMOVED THE DAMAGED SECTION IAW DWG V22-R09SDR IXXA0400047SVane · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND RT WING L/E OB VANE CORRODED, ELONGATED HOLES AROUND STA. XOLDS 6.224. REPAIRS WERE ACCOMPLISHED IAW DWG V22-RO6, REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 21, REMOVED CORROSION IAW SRM 51-1-8 PAGE 11 1SDR IXXA0400035SDoor Frame · crackedDURING ROUTINE C-CHECK FOUND FUSELAGE NOSE FWD PASSENGER DOOR UPPER FWD CORNER HAS INTERIM REPAIR STATION 25.0001-9L. REPAIR ACCOMPLISHED IAW DC8 SRM 53-2-0, PAGE 2-5. TR 53-182. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. MEASURED CRACK 5.250 INCH, FOUND SDR IXXA0400027SSkin · corrodedDURING ROUTINE C-CHECK FOUND RT WING OUTBOARD L/E INNER SECTION UPPER SKIN SURFACE CORRODED, STATION XW 485.000- XFS 710. REPAIR IS ACCOMPLISHED. REMOVED FASTENER IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 57-2-1 FIG 44. REMOVED CORROSION FROM UPPER SKIN SURFACE OF SDR IXXA0400026SSkin · corrodedDURING C-CHECK INSPECTION FOUND LEFT OUTBOARD WING L/E INBOARD SECTION WITH CORROSION ON SEVERAL AREAS OF UPPER SKIN SURFACE (STA XW 485.000-XPS 710.000). PERFORMANCE MAJOR REPAIR IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 56-2-1 FIG 44. REMOVED CORROSISDR UPS04841891Regulator · leakingF/O OXYGEN REGULATOR LEAKING. REMOVED AND REPLACED 02 BOTTLE IAW MM 12-70-01-3, NO LEAKS NOTED.SDR IXXA0400051SSkin · corrodedDURING A ROUTINE C CHECK INSPECTION FOUND LT WING OB L/E INNER SECTION UPPER SKIN SURFACE CORRODED, STA.XW. 485.000. REPAIR WAS ACCOMPLISHED. REMOVED DAMAGED AREA IAW DWGV22-R01 INCLUDING FASTENERS AND CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-1-21 PG.1, 5SDR IXXA0400025SSkin · crackedDURING ROUTINE C-CHECK INSPECTION A CRACK WAS DETECTED AT THE RIGHT FUSELAGE TAIL SECTION BETWEEN STATION 1750.00 AND 1752.00, L14R-L15R. REPAIR ACCOMPLISHED, REMOVED FASTENERS AND DAMAGE AREA IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 53-2-1 FIGURE 7. SDR DHL2004873003Spring Assy · defectiveDURING TAKEOFF, TAKEOFF TRIM SETTING OF 4.1 INITIAL ROTATION NORMAL AFTER GEAR RETRACTION ACFT PITCHED UP SLOWLY TO 20 DEG. PITCH UP & WAS REQUIRED TO PUT FWD PRESSURE ON CONTROL WHEEL TO APPROX 1.5 UNITS OF TRIM, LANDED WITH 4.0 UNITS OF TRIM. PERFORMED ELESDR DHL2004807004Odor · detectedTOP OF DESCENT STRONG ODOR, INCREASE IN CABIN FLOW ODOR GOES AWAY. OPERATED LT AND RT PACKS AT VARIOUS SETTINGS IAW 21-50-0. NO ODORS NOTED. OPS GOOD.SDR DHL2004807003Switch · malfunctionedREJECTED T/O AFTER T/O WARNING HORN SOUNDED AFTER ADVANCING THRUST LEVERS, WT 264.0, OAT 26 DEGREES CELSIUS, SPEED 5 KTS. (P/N: H14-1008) REMOVED AND REPLACED SPOILER T/O WARNING SWITCH PER M/M 27-63-1. OPS CHECKED OK IAW 27-63-0. PERFORM UNSCHEDULED MAINTESDR DHL2004807002Warning Light · false indicationREJECTED T/O AT 110 KNOTS DUE TO SLOT LIGHT ILLUMINATION, 264 MTOW, 24 DEGREES TEMP, NORMAL ZONE. CHECK BRAKE TEMPERATURES DO TO REJECTED T/O. CHECKED BRAKE TEMPERATURES PER AOM 4.1 PAGE 18. CHECKED OK. PERFORMED UNSCHEDULED MX INSPECTION DUE REJECTED T/O.SDR DHL2004806589Floorbeam · crackedFWD CARGO COMPT FLOORBEAM WITH 0.250 CRACK IN IT, STA 200.000 LBL 32 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. CUT OUT FLOORBEAM DAMAGED AREA. INSPECTED FOR CRACKS IAW DC8 NDT SPM PART 6-10-01-001. FABRICATED 2EA ANGLE DOUBLER FWD/AFT (70SDR DHL2004806587Floorbeam · crackedMAIN CARGO COMPT FLOORBEAM CRACKED 0.250 AT STA 180.000 LBL 32. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. TRIMMED OUT DAMAGED AREA ON FLOORBEAM. INSPECTED FOR CRACKS. NO CRACK FOUND. CLEANED, TREATED AND PRIMED AREA. FABRICATED ANGLE DOUBLERS 2EA (7075-SDR DHL2004806588Floorbeam · crackedMAIN CARGO COMPT FWD CENTER SECTION FLOORBEAM CRACKED 3.000 AT STA 140.000 LBL 32. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. CUT OUT FLOORBEAM DAMAGED AREA. INSPECTED FOR CRACK IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK FOUND. FABRICATED 2EA ANGLE DOUBSDR DHL2004806586Floorbeam · crackedMAIN CARGO COMPT FWD CTR SECTION FLOORBEAM CRACKED 0.500 STA 120.000, LBL 32 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. CUT OUT FLOORBEAM DAMAGED AREA. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 6-10-01-001. FABRICATED 1EA SPACER (7075-SDR DHL2004806567Clip · crackedAFT ACCY COMPT CLIP CRACKED 1.000 STA 660.000 L-22L. REMOVED CRACKED CLIP ON AFT ACCY COMPT STA 660.000, L-22L IAW SRM 51-1-20D PG 21, SRM 53-1-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW SRM 51-1-20D PG 9.SDR DHL2004806573Rib · crackedRUDDER STRUCTURAL RIB CRACKED 2.000 AT STA ZR 101.000 (REF CTR DAMPER). REMOVED CRACKED RIB IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21 PG 1.SDR UPS04841818Coalescer Bag · dirtyODOR OF SMOKE IN COCKPIT. DURING DEPARTURE UNKNOWN ORIGIN MAYBE COMING FROM PACKS LT READ 80 DEGREES, RT READ 200 DEGREES ALL OTHER GAUGES READ NORMAL, T/S FOUND WATER SEPERATOR VERY DIRTY INDICATION WAS A PACK OVERHEAT RAN PACKS ON GROUND WITH NO ODOR OF SSDR DHL2004801003Switch · malfunctionedMAIN CARGO DOOR SYSTEM-A LIGHT ILLUMINATED IN FLIGHT. ACCOMPLISHED MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT EMERGENCY PROCEDURE. PRESSURIZATION NORMAL. CONTINUED FLIGHT REPEAT WRITE-UP. ITEM TRANSFERRED TO DMI LOG PER MEL 52-2-1 DMI 15651 PLACARD INSTALSDR DHL2004801002Warning Light · false indicationMAIN CARGO DOOR SYSTEM-A LIGHT ILLUMINATED AT FL240. ACCOMPLISHED MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT EMERGENCY PROCEDURE. PRESSURIZATION NORMAL. CONTINUED FLIGHT. INSPECTED MAIN CARGO DOOR VENT SYSTEM. PERFORMED OPS CHECK OF DOOR SYSTEM AND FOUNDSDR UPS04841817Engine · flamed outNR 1 ENGINE FLAMED OUT AT TOP OF DESCENT WHEN POWER REDUCED. ENGINE READINGS WERE NORMAL W/ WINDMILLING RPM OF 22 PERCENT N2. RESTART AT FL 200 WAS NORMAL. T/S IAW MM 71-00-00 FAULT 51 GEN. INSP CK FLT IDLE, SPECIFIC GRAVITY SETTING. MAGNETIC CHIP DETECTORS SDR UPS04841812Battery · inoperativeEMERGENCY LIGHTS STAY ON CONTINOUSLY WHEN IN ARMED POSITION. LIGHT WILL NOT ILLUMINATE. WHEN SWITCH SELECTED TO DISARM CHECK. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT & PERFORMED ADJ/ TEST IAW MM 33-50-01-2. OPS CHECK GOOD.SDR UPS04841813Engine · flamed outUPON THROTTLE REDUCTION TO IDLE FOR DESCENT FROM FL 370 M .80, NR 1 ENGINE FLAMED OUT. ENG READINGS WERE NORMAL WITH WINDMILLING RPM OF 22 PERCENT N2. RESTART AT FL300 WAS NORMAL. T/S IAW MM 71-00-00 FAULT 51 GENERAL INSP, CK FLT IDLE, SPECIFIC GRAVITY SETT
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