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.

SDR UPS803199Skin · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACK (2EA) ON RT WING L/E LWR SURFACE AT XFS 591 AND 240. REPLACED SKIN PER SRM 57-2-0.May 10, 1995 · N874UP · Doug DC873F · Wing, Plate/SkinSDR UPS803198Fitting · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON NR 2 PYLON FOOT STOOL FITTING AT LWR I/B CORNER. REPLACED FITTING PER UPS EO FILE NR DC8-57-0551.May 10, 1995 · N874UP · Doug DC873F · Nacelle/Pylon StructureSDR UPS803197Skin · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON LT WING L/E, UPPER SURFACE, APPROX 12 FROM I/B SLOT, 28 FWD OF FRONT SPAR. INSTALLED REPAIR PER SRM 57-20-0.May 10, 1995 · N874UP · Doug DC873F · Wing, Plate/SkinSDR UPS803196Frame · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME FS 1000, BETWEEN LONGERONS 35L TO 35R. INSTALLED REPAIR PER UPS EO DC8-5310-6966A.May 10, 1995 · N874UP · Doug DC873F · Fuselage Main, FrameSDR UPS803174Eel · inopON PREFLIGHT CHECK, FLIGHT CREW FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSY. OPS CHECK OK.May 6, 1995 · N803UP · Doug DC873F · Emergency LightingSDR UPS803177Skin · cracked(SUPPLEMENTAL MRR) DURING DAILY CHECK, MAINTENANCE FOUND CRACK JUST FWD OF LT MLG DOOR. REMOVED FASTENERS, STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 51-1-20.May 5, 1995 · N866UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS803176Skin · cracked(SUPPLEMENTAL MRR) DURING DAILY CHECK, MAINTENANCE FOUND ONE CRACK APPROX 2 INCHES LONG AT STA 182, LONGERON 33. NOTE: CORROSION PRESENT. REMOVED FASTENERS, STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 51-1-20.May 5, 1995 · N866UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS803175Longeron · cracked(SUPPLEMENTAL MRR) DURING DAILY CHECK, MAINTENANCE FOUND TWO CRACKS APPROX 1.5 INCHES LONG EACH AT STA 81, LONGERON 33. NOTE: CORROSION PRESENT. REMOVED FASTENERS, STOP DRILLED CRACKS, INSTALLED DOUBLER PER SRM 51-1-20.May 5, 1995 · N866UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS803167Doubler · corrodedDURING 'C' CHECK, MAINTENANCE FOUND SKIN CORRODED AT FS 190 TO 450. REPLACED SKIN PANEL PER DOUGLAS DRAWING NR 5755271.May 5, 1995 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS803166Doubler · corrodedDURING 'C' CHECK, MAINTENANCE FOUND INNER DOUBLER CORRODED AT FS 220 TO 400, LONGERONS 35L TO 31R. REPLACED DOUBLERS PER DOUGLAS DRAWING NR 5755271, 9755878.May 5, 1995 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS803132Skin · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION AT LOWER SURFACE SKIN OF RT WING STA XFS 307. REPAIRED SKIN PER SRM 57-2-1, 51-1-8, 57-2-0.May 1, 1995 · N874UP · Doug DC873F · Wing, Plate/SkinSDR 95ZZZX3097Bulkhead · crackedFOUND 11 INCH CRACK AT THE LEFT SIDE OF BULKHEAD PRESSURE DOME AT BS 680. PERFORMED TEMPORARY REPAIR PER MCDONNELL DOUGLAS RECOMMENDATION.Apr 24, 1995 · N873SJ · Doug DC873F · Fuselage Main, BulkheadSDR UPS803122Gear Indication · malfunctionedPILOT REPORTED THAT AFTER TAKE OFF GEAR NOT LATCHED LIGHT REMAINED ILLUMINATED. RECYCLED GEAR AND COMPLIED WITH CHECKLIST BUT LIGHT REMAINED ON. DURING CHECK, NOSE GEAR WAS UP. PERFORMED GEAR UP LIMIT SWITCH CHECK PER MM 32-60-00. NO DEFECTS NOTED. PERFORApr 21, 1995 · N819UP · Doug DC873F · Landing Gear Position and WarningSDR UPS803016Eel Battery Pack · dischargedPILOT REPORTED, EMERGENCY LIGHTS CAME ON IN FLIGHT, ALL ELECTRICAL SYS GOOD. COULD NOT TURN OFF LIGHTS WITH ARM /DISARM SWITCH. REPLACED EMERGENCY BATTERY PACK ASSY.Apr 21, 1995 · N813UP · Doug DC873F · Emergency LightingSDR UPS802978J Beam · crackedWHILE IN 'B' CHECK, MAINTENANCE FOUND APPROX. 4 INCH CRACK ON NR 3 J-ANGLE, LWR RADIUS, AND APPROX. 4 INCH CRACK ON NR 4 J-ANGLE LWR RADIUS. ACCOMPLISHED UPS EO DC8-5310-6598B.Apr 19, 1995 · N801UP · Doug DC873F · Fuselage Main, BulkheadSDR DHL95805001Tire · failedON LANDING TIRES 1 AND 2 BLEW-OUT DURING ROLLOUT. TIRES 5 AND 6 BADLY WORN, WHEEL ASSEMBLIES 1, 2, 5, AND 6 CHANGED PER DC-8 MM 32-40-1. REPLACED 1 AND 2 BRAKES PER MM 32-42-1. FUNCTIONAL CHECK COMPLIED WITH PER MM. NO FURTHER DEFECTS NOTED.Apr 12, 1995 · N805DH · Doug DC873F · TireSDR 95ZZZW583Brakes · wornON LANDING, TIRES NR 1 AND NR 2 BLEW-OUT DURING ROLLOUT. TIRES NR 5 AND NR 6 BADLY WORN. TIRES NR 1, NR 2, NR 5 AND NR 6 CHANGED PER DC-8 MM 32-40-1. REPLACED NR 1 AND NR 2 BRAKE PER 32-42-1. FUNCTIONAL CHECK COMPLIED WITH PER MM. NO DEFECTS NOTED. REF 9Apr 12, 1995 · N805DH · Doug DC873F · BrakeSDR 95ZZZW582Tires · wornON LANDING, TIRES NR 1 AND NR 2 BLEW-OUT DURING ROLLOUT. TIRES NR 5 AND NR 6 BADLY WORN. TIRES NR 1, NR 2, NR 5 AND NR 6 CHANGED PER DC-8 MM 32-40-1. REPLACED NR 1 AND NR 2 BRAKE PER 32-42-1. FUNCTIONAL CHECK COMPLIED WITH PER MM. NO DEFECTS NOTED. REF 9Apr 12, 1995 · N805DH · Doug DC873F · TireSDR DHL95804001Retract Mech · malfunctionedON APPROACH, LANDING GEAR DID NOT EXTEND WHEN GEAR LEVER PLACED IN DOWN POSITION. RECYCLED, WORKED NORMALLY. JACKED AIRCRAFT AND PERFORMED 3 GEAR SWINGS, SEVERAL CYCLES. INSPECTED GEAR, NO DEFECTS NOTED. ALL GEAR SWINGS SUCCESSUL. COULD NOT DUPLICATE MALFApr 11, 1995 · N804DH · Doug DC873F · Landing Gear Retraction/Extension SystemSDR 95ZZZZ225Retract Mech · malfunctionedON APPROACH TO LANDING, GEAR DID NOT EXTEND WHEN GEAR LEVER PLACED IN DOWN POSITION, RECYCLED, WORKED NORMALLY. JACKED ACFT, PERFORMED 3 GEAR SWINGS, SEVERAL CYCLES. INSPECTED GEAR, NO DEFECTS NOTED. ALL GEAR SWINGS SUCCESSFUL. COULD NOT DUPLICATE. ALL WOApr 11, 1995 · N804DH · Doug DC873F · Landing Gear Retraction/Extension SystemSDR UPS802934Uplatch Mech · out of adjustPILOT REPORTED AFTER GO AROUND, GEAR DOOR NOT LATCHED LIGHT WOULD NOT EXTINGUISH. CYCLED GEAR, LIGHT REMAINED ON. FOUND LT AND RT MLG DOOR UPLATCH MECHANISM HOOK TO ROLLER CLEARANCE NON-EXISTANT, ADJ MAIN GEAR DOOR UPLATCH MECHANISM PER MM 32-31-04. OPS CK Apr 8, 1995 · N812UP · Doug DC873F · Landing Gear Door Retract SectionSDR UPS802820Angle · crackedWHILE IN 'C' CHECK, MAINTENANCE FOUND A CRACK ON RT VERT STAB TO FUSELAGE ATTACH ANGLE. INSTALLED REPAIR PER SRM 53-2-5.Apr 5, 1995 · N814UP · Doug DC873F · Fuselage, Stabilizer Attach FittingsSDR 95ZZZX2518Coupling · separatedFLT 3571 - UPON LANDING AT DABAI, NR 3 ENGINE FLAMED OUT. FOUND GAMMA COUPLING ON NR 3 FUEL TANK PRESSURE MANIFOLD SEPARATED, REPLACED SEAL AND ENGINE DRIVEN BOOST PUMP, RE-CONNECTED COUPLING, OPS CHECKED GOOD PER MM.Apr 4, 1995 · N875SJ · Doug DC873F · Engine Fuel DistributionSDR 95ZZZX1970Drive Link · crackedDURING AD 88-10-07, FLAP DRIVE LINK INSPECTION FOUND RIGHT STA 97 LINK DRIVE CRACKED.Apr 3, 1995 · N803DH · Doug DC873F · Trailing Edge Flap Control SystemSDR 95ZZZW552Foot Stool · crackedDURING AD 93-21-08 PYLON FOOT STOOL FITTING INSPECTION, NR 2 POSITION WAS FOUND TO BE CRACKED APPROX .45 INCHES. STOP DRILLED PER DOUGLAS TELEX REINSPECTION WEEKLY PER SB 57-99.Apr 3, 1995 · N803DH · Doug DC873F · Nacelle/Pylon StructureSDR 95ZZZX1857Connector · looseTTPP - ON DESCENT, NR 2 ENGINE HAD INTERMITTENT FIRE WARNING WITH SHORT CIRCUIT GROUND LIGHT. MAINTENANCE INSPECTED ENGINE AND FOUND LOOSE CANNON PLUG ON LOWER FIRE LOOP. TIGHTENED CANNON PLUG AND SYSTEM CHECKED NORMALLY. AIRCRAFT RETURNED TO SERVICE.Apr 2, 1995 · N870TV · Doug DC873F · Fire DetectionSDR UPS802808J Beam · crackedDURING B-CHECK, MAINTENANCE REPORTED TOP J-BEAM ON AFT PRESS BULKHEAD LT O/B END HAS CRACK ON TOP FLANGE AND LOWER FLANGE. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-5310-6598B.Apr 1, 1995 · N894UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS802786Door Track · crackedDURING 'C' CHECK, MAINTENANCE FOUND FWD DOOR TRACK CRACKED AT FS 1160, LONGERONS 24R AND 29R. REPAIRED TRACKS PER UPS EO DC8-53-1351.Mar 31, 1995 · N814UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS802785Frame · crackedDURING 'C' CHECK, MAINTENANCE FOUND RT WHEELWELL DOOR CUTOUT FRAME CRACKED ON FWD I/B CORNER. REPAIRED FRAME PER SRM 57-2-0.Mar 31, 1995 · N814UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS802784Skin · crackedDURING 'C' CHECK, MAINTENANCE FOUND RT WING LEADING EDGE LOWER SURFACE ATTACH HOLE SKIN CRACKED AT STA XFS 703. REPAIRED SKIN PER SRM 57-2-0.Mar 31, 1995 · N814UP · Doug DC873F · Wing, Plate/SkinSDR UPS802783Skin · delaminatedDURING 'C' CHECK, MAINTENANCE FOUND RT WING FLAP VANE DELAMINATED ON LOWER SURFACE NR 2 VANE. REPLACED VANE ASSY PER MM 27-51-14.Mar 31, 1995 · N814UP · Doug DC873F · Trailing Edge FlapsSDR UPS802782Skin · delaminatedDURING 'C' CHECK, MAINTENANCE FOUND RT WING FLAP VANE DELAMINATED ON LOWER SURFACE NR 3 VANE. REPLACED VANE ASSY PER MM 27-51-14.Mar 31, 1995 · N814UP · Doug DC873F · Trailing Edge FlapsSDR UPS802781Skin · delaminatedDURING 'C' CHECK, MAINTENANCE FOUND RT WING FLAP VANE DELAMINATED ON UPPER SURFACE NR 5 VANE. REPLACED VANE ASSY PER MM 27-51-14.Mar 31, 1995 · N814UP · Doug DC873F · Trailing Edge FlapsSDR UPS802780Skin · delaminatedDURING 'C' CHECK, MAINTENANCE FOUND LT WING NR 2 SPOILER DELAMINATED TOP AND BOTTOM SIDES AT I/B TRAILING EDGE. REPLACED SPOILER PANEL PER MM 27-61-1.Mar 31, 1995 · N814UP · Doug DC873F · SpoilersSDR UPS802779Skin · crackedDURING 'C' CHECK, MAINTENANCE FOUND CRACK IN FWD JACK POINT AT STA 70, LOWER BELLY SKIN. REPLACED SKIN PER UPS EO DC8-5330-6471.Mar 31, 1995 · N814UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS802778Frame · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON FWD SIDE OF FRAME AT FS 1320, LONGERONS 34-35R. REPAIRED FRAME PER SRM 53-2-0.Mar 31, 1995 · N814UP · Doug DC873F · Fuselage Main, FrameSDR UPS802777Fitting · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON B/T FITTING AT FS 1060, LONGERON 33R. REPLACED FITTING PER SRM 53-2-0, 51-1-20D.Mar 31, 1995 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS802776Fittings · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON B/T FITTINGS AT FS 1180, LONGERON 33-34R AND FS 1220, LONGERON 33R. REPLACED FITTINGS PER SRM 53-2-0, 51-1-20D.Mar 31, 1995 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS802775Fittings · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON B/T FITTINGS AT FS 1200 BETWEEN LONGERON 33-34R AND 33-34L. REPLACED FITTINGS PER SRM 53-2-0, 51-1-20D.Mar 31, 1995 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS802774Frame · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON BELTFRAME AT FS 200, LONGERON 29R. REPAIRED FRAME PER SRM 53-2-3.Mar 31, 1995 · N814UP · Doug DC873F · Fuselage Main, FrameSDR UPS802773Fitting · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON BELTFRAME END FITTING AT FS 1400, LONGERON 21R. REPLACED FITTING PER SRM 51-1-20D.Mar 31, 1995 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS802772Longeron · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION AND CRACK ON LONGERON 21L AT FS 395-415. FABRICATED AND INSTALLED REPAIR PER SRM 53-2-5.Mar 31, 1995 · N814UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS802745Panel · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT WING LEADING EDGE LOWER SURFACE PANEL 519A. REPLACED PANEL PER DRAWING NR 3646959.Mar 29, 1995 · N814UP · Doug DC873F · Wing, Plate/SkinSDR UPS802744Skin · corrodedWHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION BULGE AROUND RT AUX TANK UPPER ATTACH ANGLE SCREW ON SKIN AT STA XFS 29.6-33.35. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-57-0542.Mar 29, 1995 · N814UP · Doug DC873F · Wing, Plate/SkinSDR UPS802743Doubler · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON CENTER DOUBLER AT FS 902-920, BL 0, AT UPPER MAIN GEAR WHEELWELL PRESSURE DECK SURFACE. REPLACED DOUBLER PER SRM 51-1-21.Mar 29, 1995 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS802742Fittings · corrosionWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON 2 EA VERTICAL FLOOR BEAM STIFFENER FITTINGS AT FS 902 AND 940, BL 0. REPLACED FITTINGS PER SRM 51-1-20D.Mar 29, 1995 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS802658Doubler · corrodedWHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION ON RT WING L/E LWR SURFACE DOOR DOUBLER AT STA XFS 360-366. REPAIRED PER UPS EO FILE NR DC8-57-0539.Mar 14, 1995 · N813UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS802657Ribs · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND CRACKS ON LT WING, LWR SURFACE, UPPER RIBS 13, 29, 24, AND 14. REPAIRED PER MM 57-00-00.Mar 14, 1995 · N813UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS802656Bulkhead Beam · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON AFT PRESSURE BULKHEAD, 'J' BEAM, THIRD FROM TOP AT FS 1766, RBL 1, THRU ACCESS HOLE 60. REPAIRED PER SRM 53-2-0.Mar 14, 1995 · N813UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS802655Stiffener · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON NR 1 PYLON HORIZONTAL STIFFENER AT STA 364-942. REPAIRED PER UPS EO FILE NR DC8-54-0029.Mar 14, 1995 · N813UP · Doug DC873F · Nacelle/Pylon Structure
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