Douglas DC-8-61

Service difficulty reports · 942

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 = 'DC861'
  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 95ZZZM137Skin · corrosionDURING C-CHECK ON FUSELAGE RING ANGLE, CORROSION REPAIR ON FS 1680 IAW EO 9505073 WAS NECESSARY TO ACCOMPLISH A FUSELAGE SKIN CUTOUT AT FS 1680, BETWEEN L26L TO L26R TO ACCOMPLISH RING ANGLE REPAIR. AFTER COMPLETION OF RING ANGLE REPAIR, INSTALLED A .071 7075May 26, 1995 · N27UA · Doug DC861 · Fuselage Main, Plate/SkinSDR 95ZZZM136Angle · corrosionDURING C-CHECK, CORROSION DAMAGE FOUND ON THE FUSELAGE RING ANGLE AT FS 1680 BETWEEN L28R TO L33L. REMOVED AND REPLACED RING ANGLE AND INSTALLED TWO SPLICES IAW EO 9505073.May 26, 1995 · N27UA · Doug DC861 · Fuselage Miscellaneous StructureSDR 95ZZZM135Frame · corrodedDURING C-CHECK, CORROSION WAS FOUND ON THE FUSELAGE FRAME AT FS 1400 BETWEEN L34R AND L35L. REMOVED AND REPLACED FUSELAGE FRAME AT FS 1400, INSTALLED STRAP DOUBLER AND ACCOMPLISHED REPAIR SPLICE ON FUSELAGE FRAME IAW EO 9505071.May 26, 1995 · N27UA · Doug DC861 · Fuselage Main, FrameSDR ABXA9500517Skin · crackedDURING D-CHECK AND COMPLIANCE OF ASB A55-16, FOUND THE RIGHT HORIZONTAL STABILIZER OUTBOARD UPPER CENTER SKIN PLANK CRACKED AT BOLT HOLES 10 AND 11. REMOVED AND REPLACED THE RIGHT HORIZONTAL STABILIZER IAW DC-8 MM CHAPTER 55.May 16, 1995 · N849AX · Doug DC861 · Horizontal Stabilizer, Plate/SkinSDR ABXA9500444Seal · defectiveAT APPROXIMATELY 26,000 FT, 7 PSID, AND 4,500 FT CABIN, THE CABIN RATE OF CLIMB INDICATOR WENT FROM 500 TO 2500 FPM ASCENT. REGAINED CONTROL OF CABIN AT APPROXIMATELY 18,000 FT AND 3 PSID. AIRCRAFT CONTINUED TO ATL. RE-INSTALLED SEAL IN RETAINER ON MAIN CARMay 16, 1995 · N849AX · Doug DC861 · Cargo/Baggage DoorsSDR BUFA9513Lift Transducer · defectiveFLT 792 - STALL WARNING CAME ON RIGHT AFTER ROTATION, STALL WARNING STILL ON AT 220 KTS IN LEVEL FLIGHT, ALL OTHER INDICATIONS NORMAL. RETURNED TO MMMX. REMOVED AND REPLACED STALL WARNING LIFT TRANSDUCER, SYSTEM OP CHECK NORMAL PER MM 34-16. (W)May 14, 1995 · N161DB · Doug DC861 · Stall Warning SystemSDR ABXA9500405Angle · crackedDURING D-CHECK, FOUND THE NR 1 PYLON LEADING EDGE INTERIOR CRACKED AT STA 237. REPAIRED IAW ABX REA D854-11007.May 10, 1995 · N849AX · Doug DC861 · Nacelle/Pylon StructureSDR ABXA9500404Spar · corrodedDURING D-CHECK, FOUND RIGHT FORWARD RUDDER SPAR CORRODED AT STATION ZR 284 AND ZR 330 TO 338. REPAIRED IAW ABX REA D855-11005.May 10, 1995 · N849AX · Doug DC861 · Rudder, Spar/RibSDR ABXA9500403Skin · crackedDURING D-CHECK, FOUND THE DOOR CUTOUT AT STATION 320 TO 340 BOTTOM CORNER CRACKED. REPAIRED CRACKED FUSEAGE SKIN AT C1 DOOR IAW ABX REA D853-11002.May 10, 1995 · N849AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA9500402Hinge Fitting · chaffedDURING D-CHECK, FOUND THE RIGHT INBOARD HINGE INBOARD HALF WORN. REPAIRED CHAFED AND WORN HINGE FITTINGS IAW ABX REA D857-11001MR.May 10, 1995 · N849AX · Doug DC861 · Trailing Edge FlapsSDR ABXA9500401Jamb · crackedDURING D-CHECK, FOUND THE FORWARD PIT AFT DOOR LOWER JAMB CRACKED AND DENTED WITH NUMEROUS AREAS OF CORROSION. REPAIRED IAW ABX REA D853-10998MR.May 10, 1995 · N849AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA9500400Frame · crackedDURING D-CHECK, FOUND FRAME AND WEB AT RIGHT FORWARD SERVICE DOOR DENTED AND CRACKED. REPAIRED FRAME AND WEB IAW ABX REA D853-11169.May 10, 1995 · N849AX · Doug DC861 · Service DoorsSDR ABXA9500399Frame · crackedDURING D-CHECK, FOUND THE AFT PIT FRAME AT STATION 1100 CRACKED AT LONGERON 36. REPAIRED IAW REA D853-11165.May 10, 1995 · N849AX · Doug DC861 · Fuselage Main, FrameSDR ABXA9500398Spar · crackedDURING D-CHECK, FOUND NR 2 AND NR 3 PYLONS WITH CRACKS ON THE UPPER SPAR CAP. REPAIRED IAW ABX REA D854-11147.May 10, 1995 · N849AX · Doug DC861 · Nacelle/Pylon StructureSDR ABXA9500397Skin · crackedDURING D-CHECK, FOUND NR 2 PYLON OUTBOARD LOWER SURFACE AND INNER SKIN CRACKED. REPAIRED IAW ABX REA D857-11163.May 10, 1995 · N849AX · Doug DC861 · Nacelle/Pylon, Plate/SkinSDR ABXA9500396Longeron · crackedDURING D-CHECK, FOUND LONGERON SPLICE AT STATION 1410 WITH CRACK UNDER FRAME. REPAIRED LONGERON IAW ABX REA D853-11139.May 10, 1995 · N849AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA9500395Skin · corrodedDURING D-CHECK, FOUND BELLY SKIN AT STATION 1050 TO 1350, LONGERON 34L TO 35L CORRODED. REPAIRED BELLY SKIN IAW ABX REA D853-11143.May 10, 1995 · N849AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA9500394Doubler · missingDURING D-CHECK, FOUND REPAIR AT STATION 8 TO 25, LONGERON 24L TO 25L MISSING FINGER DOUBLERS. REPAIRED LONGERON IAW ABX REA D853-11013.May 10, 1995 · N849AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA9500393Corner · damagedDURING D-CHECK, FOUND THE LEFT AFT ENTRY DOOR UPPER CORNER OF CUT OUT TO HAVE A REPAIR THAT DOES NOT HAVE AN SRO DRAWING. REPAIRED IAW REA D853-11171.May 10, 1995 · N849AX · Doug DC861 · Passenger/Crew DoorsSDR ABXA9500392Frame · crackedDURING D-CHECK, FOUND THE FRAME AT STATION 1400, LONGERON 36R AND 34R, CORRODED AND CRACKED IN TWO PLACES. REPAIRED FRAME IAW ABX REA D853-11164.May 10, 1995 · N849AX · Doug DC861 · Fuselage Main, FrameSDR ABXA9500387Panel · corrodedDURING D-CHECK, FOUND LEFT WING LEADING EDGE OUTBOARD CLOSING PANEL CORRODED. REPAIRED PANEL IAW ABX REA D857-11142.May 10, 1995 · N849AX · Doug DC861 · Wing, Plate/SkinSDR ABXA9500386Door Jamb · corrodedDURING D-CHECK, FOUND FORWARD AND AFT DOOR JAMB ON THE CENTER SERVICE DOOR STA 1080 TO 1120 CORRODED. REPAIRED IAW ABX REA D853-11006.May 10, 1995 · N849AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA9500391Hinge Fitting · chafedDURING D-CHECK, FOUND THE INBOARD HALF OF THE RIGHT INBOARD FLAP HINGE WORN AND CHAFED. REPAIRED HINGE FITTING IAW REA D857-11001MR.May 5, 1995 · N849AX · Doug DC861 · Trailing Edge FlapsSDR ABXA9500390Skin · crackedDURING D-CHECK, FOUND THE DOOR CUTOUT AT STATION 320 TO 340 AFT BOTTOM CORNER CRACKED. REPAIRED CRACKED FUSELAGE SKIN AT C1 LOWER DOOR SILL IAW ABX REA D853-11002.May 5, 1995 · N849AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA9500389Spar Cap · crackedDURING D-CHECK, FOUND THE NR 4 PYLON INBOARD SPAR CAP CRACKED IN TWO PLACES. REPAIRED CRACKED SPAR CAP IAW REA D854-11009MR.May 5, 1995 · N849AX · Doug DC861 · Nacelle/Pylon StructureSDR ABXA9500388Door Jamb · crackedDURING D-CHECK, FOUND THE FORWARD CARGO PIT'S AFT DOOR JAMB CRACKED AND DENTED WITH NUMEROUS AREAS OF CORROSION. REPAIRED DOOR JAMB IAW ABX REA D583-10998MR.May 5, 1995 · N849AX · Doug DC861 · Cargo/Baggage DoorsSDR BUFA9511Oil Press Light · illuminatedFLT LIC035 - SVMI-KMIA - NR 2 ENGINE OIL PRESS LIGHT CAME ON AT 310 VERIFIED BY OIL PRESS INDICATOR AND OIL QUANTITY. SHUT NR 2 ENGINE DOWN, COMPLETED PROPER CHECK LIST AND PROCEDURE. (W)Apr 17, 1995 · N161DB · Doug DC861 · Engine Oil PressureSDR ABXA9500333Fire Element · defectiveDURING CRUISE, THE NUMBER FOUR ENGINE FIRE LIGHT ILLUMINATED AND THE FIRE BELL SOUNDED. THE ENGINE WAS SECURED AND A FIRE BOTTLE WAS DISCHARGED. DURING THE WINDMILLING PROCEDURE, THE FIRE LIGHT FLICKERED MOMENTARILY. THE FLIGHT CONTINUED WITHOUT FURTHER INCApr 14, 1995 · N847AX · Doug DC861 · Fire DetectionSDR ABXA9500331Fire Loop · looseDURING CRUISE, THE NR FOUR ENGINE FIRE WARNING LIGHT ILLUMINATED. THE ENGINE WAS SECURED AND THE FIRE BOTTLES WERE DISCHARGED. LIGHT REMAINED ON. FLIGHT REROUTED TO DEN. LANDED WITHOUT INCIDENT. FOUND LOWER FIRE LOOP LOOSE AND CONNECTOR FULL OF OIL. SECUApr 13, 1995 · N847AX · Doug DC861 · Fire DetectionSDR 95ZZZX1934Door · openWINDSOR LOCKS, CN - DURING CLIMB, HEARD BANG AND AIRCRAFT YAWED LEFT. DUMPED FUEL TO LANDING WEIGHT. RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. INSPECTION OF AIRCRAFT REVEALED NO DAMAGE. AFTER SHUT DOWN, NOTED LT CASCADE DOORS ON NR 1 ENGINE OPEN. RApr 5, 1995 · N29UA · Doug DC861 · Engine Thrust ReverserSDR ABXA9500310Hinge Pins · lack of lubeTHE FIRST OFFICER'S SLIDING WINDOW VERY DIFFICULT TO OPEN. CLEANED AND LUBED HINGE PINS AND LATCHING MECHANISM. WINDOW OPS CHECKED GOOD IAW DC-8 MM CHAPTER 56.Apr 4, 1995 · N848AX · Doug DC861 · Flight Compartment WindowsSDR ABXA9500302Link · crackedDURING COMPLIANCE OF A.D. 88-10-07, S.B. 27-246, A.S.B. 27-269 HAD CRACK INDICATION AT POINT J INBOARD SIDE RIGHT HAND FLAP LINK. REPLACED LINK IAW DC8 MM 27-51-4.Apr 4, 1995 · N843AX · Doug DC861 · Trailing Edge FlapsSDR BUFA9508Retract Mech · lack of lubeMBJ/MIA - FLT AJM9037 - LANDING GEAR HANDLE DOWN, ALL UNSAFE LIGHTS ON F/E PANEL ON, HYDRAULIC PRESSURE AND QUANTITY NORMAL, NO GREEN LIGHTS, HAD TO GO AROUND, GEAR HANDLE UP, RED LIGHTS OUT, GEAR HANDLE DOWN, RED, THEN 3 GREEN, HYDRAULIC NORMAL. INSPECTED LAMar 30, 1995 · N161DB · Doug DC861 · Landing Gear Retraction/Extension SystemSDR BUFA9512Torque Tube · bentMGG/MIA - FLT CWC 148 - MAIN CARGO DOOR ALTERNATE LOCKING PINS VERY HARD TO REMOVE. INSPECTED, FOUND TORQUE TUBE BENT. REPLACED TORQUE TUBE AND RE-RIGGED CARGO DOOR LATCHES, PERFORMED OPS CHECK PER CARGO DOOR MM, OPS CHECK OKAY. DOOR WAS INSPECTED PER RII RMar 29, 1995 · N915BV · Doug DC861 · Cargo/Baggage DoorsSDR BUFA 9506Cowling · missingIAH-BNA - FLT 127 - THE NR 3 ENGINE, AFT COWLING MISSING ON POST FLIGHT WALK AROUND. ACFT INSPECTED WITH REFERENCE TO ACMM PROCEDURES AND DETERMINED IN SAFE AND AIRWORTHY CONDITION FOR MAINTNENANCE FERRY FLIGHT TO MQY. REPAIRED PYLON APRON PER DC-8 SRM 54-2-Feb 28, 1995 · N161DB · Doug DC861 · Engine Cowling SystemSDR ABXA9500070Mfd Display Unit · defectiveDURING CRUISE, THE MULTIFUNCTION DISPLAY WENT BLACK AND MADE A 'GROWLING' NOISE. THERE WAS A SMELL OF SMOKE IN THE COCKPIT; CREW PULLED THE CIRCUIT BREAKER. REMOVED AND REPLACED THE MFD. SYSTEM OPS CHECKED GOOD IAW DC 8 MM CHAPTER 34.Feb 8, 1995 · N850AX · Doug DC861 · Central DisplaySDR ABXA9500069Hyd Hose · rupturedON SHORT FINAL, THE HYDRAULIC FLUID QUANTITY LEVEL DROPPED TO THE STANDPIPE LEVEL AFTER GEAR AND FLAP EXTENSION. LEVEL REMAINED THERE AFTER LANDING. FOUND THE RIGHT GEAR UNLOCK BOGIE TRIM LINE RUPTURED. REMOVED AND REPLACED THE HYDRAULIC LINE IAW DC 8 MM CHFeb 8, 1995 · N841AX · Doug DC861 · Hydraulic System, MainSDR CKSA95004Skin · corrosionYIP - DURING B-CHECK, INSPECTION FOUND EVIDENCE OF SKIN CORROSION AT STA 140 BETWEEN STRINGERS 26 AND 27R. REMOVED CORROSION AND INSTALLED REPAIR PER DC-8 SRM 53-2-1. (W)Jan 25, 1995 · N816CK · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA9500059Indicator Assy · dirtyON TEST FLIGHT OUT OF GSO, THE LEFT AND RIGHT GEAR VISUAL DOWNLOCK INDICATORS SHOWED DOWN AND LOCKED WITH GEAR RETRACTED. RECYCLED GEAR AND HAD SAME INDICATION. REMOVED AND REINSTALLED LEFT AND RIGHT GEAR VISUAL DOWNLOCK INDICATORS IAW DC-8 MM CHAPTER 32. SJan 24, 1995 · N851AX · Doug DC861 · Landing Gear Position and WarningSDR ABXA9500054Seat · won't lockCAPTAIN'S SEAT DOES NOT LOCK IN THE FORE AND AFT POSITION. PIN DOES NOT ENGAGE IN RAIL. REMOVED AND REPLACED CAPTAIN'S SEAT AFTER RETURN FLIGHT TO ILN. SEAT OPS CHECKED GOOD, IAW DC8 MM CHAPTER 25.Jan 19, 1995 · N842AX · Doug DC861 · Flight Compartment EquipmentSDR BUFA9501Retract Mech · out of adjustMQY - AIR RETURN, FLIGHT LEVEL 330, 0155Z. HEARD AND FELT VIBRATION IN COCKPIT, DESCENT TO FLIGHT LEVEL 190 AND 230 KNOTS, GEAR UP LATCH CHECK, SMALL CHANGE IN VIBRATION. NO WARNING LIGHTS ON, LANDING GEAR LEVER UP. JACKED ACFT AND ACCOMPLISHED NOSE GEAR REJan 6, 1995 · N161DB · Doug DC861 · Landing Gear Door Retract SectionSDR CKSA94353Tubine Blade · failedKMCI - FLT 59901 - ON CLIMB-OUT, NR 3 ENGINE HAD A SUDDEN DROP IN EPR ACCOMPANIED BY SEVERE VIBRATION. ENGINE IMMEDIATELY SHUT DOWN. REMOVED AND REPLACED NR 3 IAW AIA DC-8 MIP-1 SECTION 9. C/W TRIM RUN ALL SYSTEMS. OPS CHECKS NORMAL IAW AIA MIP-1 SECTION 1Jan 3, 1995 · N812CK · Doug DC861 · Turbine Section
Back to Douglas DC-8-61