Douglas DC-8F-54
Service difficulty reports · 194
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 = 'DC8F54' 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 = 'DC8F54' 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 DHL2001806509Light · crackedC-CHECK-FWD CARGO BAY LIGHT BASE CRACKED 1 INCH AT STA.100 LBL.17. REMOVED FASTENER IAW.SRM.51-1-21. FABRICATED DOUBLER IAW SRM 53-2-0 FIG.2 CLEANED,TREATED & PRIMED IAW.SRM.51-1-88 INSTALLED DOUBLER & FASTENERS (NEW) IAW.SRM51-1-21 PAGE 21 STATUS CLOSEDSDR ARWA0010101Hydraulic Line · leakingDURING DESCENT AT THE INITIAL PHASE OF THE APPROACH LOSS HYDRAULIC FLUID AND PRESSURE. INITIATED PHASE I AND ABNORMAL IAW PROCEDURES. AFTER CLEARING THE ACTIVE DURING TAXI, LOSS HYDRAULIC BRAKE PRESSURE. AIR BRAKE PRESSURE APPLIED. FOUND PRESSURE LINE TO ESDR ARWA0001004Pin · brokenFLIGHT LEAVING OUT OF MIA TO KM, WHEN LANDING GEAR SELECTED UP; CREW HEARD LOUD BANG IN AFT AIRCRAFT; FOLLOWED BY UNSAFE RED GEAR LIGHT AND LOSS OF HYDRAULIC FLUID. FOUNDED LT MAIN GEAR RETRACTING ACTUATOR BROKEN PIN. DURING REPLACEMENT OF THE LT RETRACT PIN SDR ARWA0001003Panel · corrodedDURING B CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION ON LT WING UPPER INNER WING L/E SLANT PANEL. REPAIR CORROSION CRACK IAW EO 0010181.SDR ARWA0001002Longeron · corrodedDURING B CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION CRACK AT LONGERON L-24 BETWEEN FS 960 AND 980. REPAIRED CORROSION CRACK IAW BOEING MESSAGE INW-LIM-00-00142H.SDR ARWA0001001Skin · corrodedDURING B CHECK INSPECTION FOUND THE FOLLOWING:CORRODED C3 CARGO DOOR LOWER EDGE OUTER SKIN BETWEEN BS 1130 AND BS 1160. REPAIRED CORROSION CRACK IAW DRAWING AS1121-IR.SDR ARAWA000901Fuel Control · malfunctionedON APPROACH TO SKCL, NR 4 ENGINE FAILED. PERFORMED EMERGENCY PROCEDURES AS PER FINE AIR PROCEDURES. LANDING WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 ENGINE FUEL CONTROL IAW MM 73-22-00. REMOVED AND REPLACED NR 4 ENGINE DRIVEN FUEL PUMP IAW MM 73-01-01. SDR 20001208AP006Fitting · crackedDURING AN INSPECTION FOUND THE FOLLOWING, CRACKED LEFT MLG AUXILIARY SPAR FITTING. REPLACED AUXILIARY SPAR FITTING IAW DOUGLAS DRAWING NR 5802630. (M)SDR 20001208AP002Spar Cap · crackedDURING AN INSPECTION OF THE PYLON FOUND FORWARD SPAR CRACK AT STATION XFS 550. REPAIRED FORWARD PYLON IAW DOUGLAS DRAWING NR 5802712. (M)SDR 20001208AP001Fitting · crackedDURING AN INSPECTION FOUND THE FOLLOWING, CRACKED FITTING LEFT SIDE LONGERON 24. REPLACED CRACK LONGERON FITTING IAW DOUGLAS DRAWING NR 5802709. (M)SDR 20001208AP003Ballast · overheatedSHORTLY AFTER TAKEOFF FROM MGA EN ROUTE TO MIA CREW NOTICED STRANGE SMELL IN COCKPIT, SMOKE WAS DETECTED IN COCKPIT AND MAIN CARGO COMPARTMENT. RETURNED BACK TO MGA WITHOUT INCIDENT, FOUND NR 4 GENERATOR VOLTAGE REGULATOR CRACKED AND OVERHEATED PRODUCING SMOKSDR 2000ZZZX465Skin · corrodedDURING B-CHECK INSPECTION, FOUND THE FOLLOWING: 4.5 INCH CRACK IN RIGHT INBOARD FORWARD LOWER WING SKIN AT STA XRS 210 BETWEEN 66 AND 67. REPAIRED CRACK IAW BOEING SERVICE ENGINEERING ROD SKETCH 99-08-13 AND SRM 57-2-1 FIGURE 35, FINE AIRLINES EA G5730-02:00SDR 2000ZZZX459Ballast · failedAFTER TAKEOFF FROM MIA, EXPERIENCED SMOKE AND ELECTRICAL ODOR IN THE COCKPIT; RETURNED TO MIA AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED THE BALLAST FOR THE FIRST OFFICER LIGHT WAS OVERHEATED. REPLACED BALLAST AND RETURNED AIRCRAFT TO SERVICE. (X)SDR 2000ZZZX472Fcu · inoperativeDURING SHORT FINAL, NR 3 ENGINE FLAMEOUT; FUEL ON NR 3 TANK WAS 5800; SUSPECT FCU MALFUNCTION. CHANGED AND TESTED FCU UNIT IAW PW MM 72-0. (X)SDR 2000ZZZX473Line · leakingFLT 790 - ON DESCENT INTO MIA FROM POS, REPORTED LOSS OF HYDRAULIC FLUID DOWN TO STANDPIPE. PERFORMED EMERGENCY CHECKLIST. DECLARED EMERGENCY AND LANDED FULL FLAPS AT MIA WITHOUT INCIDENT. FOUND NR 2 ENGINE DRIVE HYDRAULIC PUMP LINE LEAKING, RE-TORQUED LINESDR 2000ZZZM231Spar · crackedDURING D-CHECK INSPECTION, FOUND 4 INCH CRACK IN RIGHT LOWER SPAR CAP AT XCW 69.5. REPAIRED ACCOMPLISH IAW BOEING SERVICE ENGINEERING FAX FAS-MIA-99-0010RR AND SRO8570012 PER FINE AIR EA G5710-02, 00. (M)SDR 2000ZZZX464Floorbeam · corrodedDURING B-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORROSION DAMAGE UPPER FLANGE AT STA FS 1380 RBL 38. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA G5310-02:00. (X)SDR 2000ZZZX461Floorbeam · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORROSION DAMAGE STA FS 1480. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA G5310-03:00. (X)SDR 2000ZZZX460Floorbeam · corrodedDURING B-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORROSION DAMAGE STA FS 1480. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA G5310-01:00. (X)SDR 2000ZZZM248Skin · crackedDURING D-CHECK INSPECTION, FOUND LEADING UPPER CAP CRACKED. REPAIRED CRACK ON WING RIGHT IAW FINE AIRLINES EA NR G5711-02:00. (M)SDR TC8A99005Line · leakingNO FLIGHT, RETURN TO RAMP TO SERVICE HYDRAULICS. HYDRAULICS DROPPED APPROXIMATELY 5 GALLONS ON TAXI OUT. SERVICED HYDRAULICS, FIXED LEAK ON NR 3 ENGINE.SDR 99ZZZM231Switch · failedDURING CRUISE GEAR UNSAFE LIGHT ILLUMINATED. CYCLED GEAR AND RECEIVED THREE GREEN LIGHTS FOR LANDING GEAR. LANDED AT MIA WITHOUT INCIDENT. GROUND INSPECTION REVEALED RIGHT MAIN LANDING GEAR DOOR NOT FULLY CLOSED. REPLACED LEFT AND RIGHT DOOR MICROSWITCHES, LSDR 2000ZZZX463Skin · corrodedDURIGN C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION DAMAGE AT STA XE149 HORIZONTAL STABILIZER, LEFT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EO 9800071. (X)SDR 2000ZZZX462Skin · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION DAMAGE AT STA XE 133 TO 246 ELEVATOR LEFT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EO 9811091. (X)SDR 2000ZZZX467Floorbeam · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORRROSION DAMAGE AT STA FS 940. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EO 9810211. (X)SDR 2000ZZZX466Floorbeam · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORRROSION DAMAGE AT STA FS 820 - FS 859, LEFT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EO 9810161. (X)SDR RRXA98506Pump · failedHYD QUANTITY LOSS INFLIGHT. FOUND NR 2 ENG HYD PUMP INTERNAL SEALS ALLOWING FLUID TO FLOW INTO NR 2 ENG OIL SUPPLY. DRAINED, FLUSHED ENG OIL TANK 2 TIMES. REMOVED AND REPLACED OIL FILTER AND ENG HYD PUMP. PERFORMED LEAK CK OF ENG OIL AND HYD SUPPLY, NONE NSDR TC8A98076Blade · dentedCOMPRESSOR STALL NR 3 ENGINE DURING TAKEOFF ROLL, APPROXIMATELY 60 KNOTS, ANTI-ICE OFF. INSPECTED COMPRESSOR AND TURBINE IAW PW 72-0, PG 118, NO DEFECTS NOTED. INSPECTED INLET, FOUND 1 BLADE DENTED, BLENDED AND INSPECTED IAW PG 602/604.SDR TC8A98069Voltage Reg · failedTRIP# 02707. DISCREP: #2 GENERATOR SHOWS UNBALANCED LOAD. CORR. ACTION: TRANSFERRED TO DMI 8809 AS PER MEL 24-1 CAT C. PLACARD INSTALLED, SPECIAL PROCEDURES COMPLIED WITH. 10/27/98 REMOVED AND REPLACED VOLTAGE REGULATOR IAW 24-5-11, OPS CHECKS GSDR TC8A98068Terminal · damagedTRIP NR 02692, DURING TAXI, NR 1 AND NR 3 GENERATOR UNPARALLELED, VOLTS AND FREQS OK. AIRCRAFT FERRIED TO KYIP. TROUBLESHOT SYSTEM, REPLACED TERMINALS AT WIRE NR X56024 (NR 3 GCR). SYSTEM OPS GOOD IAW DMM 24-10-0.SDR 99ZZZM29Strut · crackedCREW REPORTED FINDING A HYDRAULIC LEAK ON NOSE LANDING GEAR DURING PRE-FLIGHT GYE. FOUND CRACK IN NLG OLEO OUTER CYLINDER APPROX 6 INCH FROM TOP, APPROX 1.5 INCH LONG UNDER DATA PLATE. REPLACE NLG OLEO ASSEMBLY PER MM 32-2-0. (M)SDR ZIAA98039Skin · corrodedYIP - BELLY AT APPROXIMATELY FS 600, REINFORCING PLATE HAS SEVERAL POPPED RIVETS. REMOVED PLATE DUE TO CORROSION. REMOVED SKIN DAMAGE DUE TO CORROSION. REPAIRED SKIN IAW ZANTOP DRAWING SKA95008-1 REVISION A. SEALED EDGES WITH CS3204 B1/2. (M)SDR TC8A98053Bleed Valve · replacedMULTIPLE COMPRESSOR STALLS ON CLIMBOUT, 6,000 FT ON NR 1 ENG. REMOVED AND REPLACED NR 1 PRBC VALVE, OPS CHECKS OK IAW 75-30-3.SDR TC8A98046Connector · dirtyTRIP NR 02268, NR 1 TURBO COMPRESSOR WOULD NOT TEST. CLEANED CANNON PLUG AND RESET, OPS CHECK GOOD IAW M/M 21-10-2.SDR 98ZZZM564Fitting · crackedFOUND RIGHT MAIN LANDING GEAR SUPPORT FITTING CRACKED. REMOVED AND REPLACED RIGHT MAIN GEAR FITTING PER IAW DOUGLAS DC8 MLG FITTING REPLACEMENT GUIDE AND RECOVERY AND MOD SERVICES NR CI-735. (M)SDR TC8A98042Fitting · crackedON TAXI UPON FLIGHT CONTROL CHECK, SPOILER PUMP PRESSURE INDICATION WENT TO ZERO. FOUND FITTING AT SPOILER SUPPLY LINE CRACKED. REPLACED FITTING IAW MM 27-62-0, OPS CHECK NORMAL.SDR TC8A98041Compressor · stalledLOUD, PRONOUNCED, SUSPECTED ENGINE COMPRESSOR STALL ON RT SIDE DURING TAKEOFF PASSING 70 KIAS, ABORT INITIATED. INSPECTED NR 3 AND NR 4 ENGINES FOR DAMAGE, NONE NOTED. LUBED SURGE BLEED VALVE ON NR 3 AND NR 4 ENGINES. RAN ENGINES IAW 71-00, NO COMPRESSOR STSDR 98ZZZM870Unknown · odorON ARRIVAL GYE, REPORTED SMOKE ODOR FROM UNKNOWN SOURCE IN COCKPIT AND CABIN. ON GROUND, RAN ENGINES AND PRESSURIZED AIRCRAFT TO CHECK NASI PNEUMATIC FLOW CONTROL SYSTEM IAW STC ST466CH. NO SMOKE ODOR WAS NOTED IN AIRCRAFT. AIRCRAFT WAS RETURNED TO SERVICE SDR TC8A98040Compressor · stalledINITIATED ABORT PASSING 80 KNOTS BECAUSE OF SUSPECTED COMPRESSOR STALL OR BLOWN TIRE. RETURNED TO THE BLOCKS, LET BRAKES COOL, INSPECTED BRAKES AND TIRES IAW M/M 32-40-1. ALSO RAN UP ALL FOUR ENGINES IAW 71-00, COULD NOT DUPLICATE COMPRESSOR STALL, ENGINE RSDR TC8A98036Oil Tank · looseON CLIMB-OUT AT APPROX 10000 FEET, NR 3 ENGINE FIRE WARNING BELL AND LIGHTS. PERFORMED ENGINE SHUTDOWN. FOUND MIDDLE STRAP ON ENGINE OIL TANK LOOSE AND IN CONTACT WITH LT FAN DOOR FIRE WARNING LOOP. SECURED CLAMP, PERFORMED ENGINE RUN-UP AND FIRE WARNING TESDR 98ZZZM498Line · brokenIN CRUISE BOG TO MIA EXPERIENCED LOSS OF HYDRAULIC QTY. EXECUTED ABNORMAL PROCEDURES AND LANDED MIA WITHOUT INCIDENT. AIRCRAFT TOWED OFF RUNWAY. INSPECTION REVEALED A BROKEN HYDRAULIC LINE IN THE LEFT WHEEL WELL. REPLACED HYDRAULIC LINE, SERVICED SYSTEM ANDSDR CKSA98349Plug · mislocatedON CLIMBOUT, BURNING SMELL NOTED IN COCKPIT. FO'S AUDIO PANEL CB POPPED. AFTER 5 MIN COOL DOWN, CB RESET AN IMMEDIATELY POPPED AGAIN. BURNING SMELL DISIPATED. FOUND FO'S MIC JACK SHORTING OUT DUE TO LOCATION OF MOUNTING BRACKET. RELOCATED AS REQUIRED. SYSDR 98ZZZM686Line · brokenON TAXI AFTER LANDING MIA, FLT 364 - REPORTED LOSS OF HYDRAULIC QUANTITY TO AUX LEVEL WITH LOW BRAKE PRESSURE LIGHT ILLUMINATED AND NO EFFECTIVE BRAKING OR STEERING. REPLACED BROKEN HYDRAULIC LINE AT LEFT BOGIE TRIM CYLINDER IAW MM 13-6-2. OPS CHECKED NORMALSDR RRXA98225Nut · missingFLAP SPLIT ON APPROACH. A/C ROLLS TO LEFT AT 10 DEG PERFORMED A ZERO FLAP LNDG. REPLACED MISSING NUTS ON FLAP TRACK ON LEFT FLAP, OPS CHECKS NORMAL, NO SPLIT NOTED ON GROUND OPS CHECK.SDR TC8A98027Brake · locked upON TAXI OUT, AIRPLANE SHUDDERED AND CAME TO A STOP, WOULD NOT MOVE. REMOVED AND REPLACED NR 6 BRAKE ASSY, LEAK CHECK OPS CHECKED OK PER M/M 32-42-1.SDR CKSA98336Hydraulic Line · leakingDURING CRUISE, LOSS OF HYDRAULIC FLUID ON QUANTITY INDICATOR (5.8 GALLONS). ACCOMPLISHED AIA EMERGENCY PROCEDURES. ON POSTFLIGHT, DISCOVERED NR 2 ENGINE LEAKING HYDRAULIC FLUID. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC LINE. OPS CHECK OK ON ENGINE RUN UPSDR RRXA98082Engine · failedNR 4 ENG LOUD BANG, HEAVY VIBRATION, DECAYING N1, N2 AND INCREASING EGT, ACCOMPANIED BY VIOLENT YAW TO THE RIGHT. HEAVY VIBRATION FELT WITH THROTTLE ADVANCEMENT. PREPARED AIRCRAFT FOR THREE ENGINE FERRY, INSPECTED AIRCRAFT AND FOUND IT SAFE FOR THE FLIGHT INSDR RRXA98079Static Hose · collapsedCAPT'S ALTIMETER IS STUCK AT 500 FEET. FOUND STATIC HOSE ASSY FROM CAPTS STATIC SOURCE SELECTOR TO MANIFOLD MOUNTED ON BACK OF INSTRUMENT PANEL TO BE PARTIALLY COLLAPSED. REMOVED AND REPLACED LINE SYSTEM CK NORMAL. PITOT STATIC LEAK CHECK PERFORMED.SDR RRXA98078Hyd Line · failedAT FL 35.0 LOST HYD FLUID TO STAND PIPE AUX LEVEL. PERFORMED HYD FLUID OR PRESS LOSS CHECKLIST. FOUND PRESSURE LINE ON NR 3 ENGINE RUPTURED. REMOVED AND REPLACED SAID LINE. ALSO, REPLACED SUCTION LINE AS PRECAUTIONARY. LEAK CK'D SYSTEM CHECKED GOOD. HYD SDR RRXA98073Fire Element · shortedCLIMBING THROUGH 13000 FT, NR 2 ENG FIRE WARNING CAME ON. SHUT DOWN ENGINE AND FIRE WARNING WENT OUT. TESTED FIRE WARNING AND TEST WAS INOP, DISCHARGED AGENT AFTER APPROX 30 SEC FIRE TEST WAS GOOD. RII FOUND NR 2 ENG UPPER AFT FIRE WARNING ELEMENT SHORTING
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