Douglas DC-10-30F
Service difficulty reports · 1,152
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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 = 'DC1030F' 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 = 'DC1030F' 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 07FDEA02556Vent · malfunctionedPDIS: RCVD CABIN RATE ON DEPARTURE. A/C WOULD NOT PRESSURIZE. CHANGED CONTROLLER TO MANUAL NO CHANGE. OUTFLOW VALVE INDICATED CLOSED ENTIRE TIME ON SYNOPTIC PAGE AND ON PNL. ON SYNOPTIC "CLOSED" INDICATOR IN AMBER BUT VALVE INDICATOR WAS CLOSED. RETURNESDR 07FDEA02555Motor · failedPDIS: AFTER DEPARTURE, CLIMBING THROUGH 8000 FT RECEIVED "CABIN RATE" ALERT. LEVELED AT 10,000 FT THEN RECEIVED " CABIN ALTITUDE ALERT. REFER TO QRH PROCEDURE, NO CHANGE. A/C PRESSURIZED TO OUTSIDE PRESSURE AT 10,000 FT THROUGH LANDING. OUTFLOW VALVE SHOWESDR G6OA200700003Fire Warning · activatedNR 1 ENGINE FIRE WARNING IN FLIGHT.SDR G6OA200700005Fire Warning · activatedNR 1 ENGINE FIRE WARNING IN FLIGHT.SDR G6OA200700004Fire Warning · activatedNR 1 ENGINE FIRE WARNING IN FLIGHT.SDR G6OA200700002Hose · chafedNR 1 ENGINE RIGHT HYDRAULIC PUMP MAIN SUPPLY LINE CHAFED THROUGH CAUSING RAPID LOSS OF NR 1 SYSTEM HYDRAULICS.SDR ARWA20070704Tire · failedNR 7 TIRE BLEW DURING LANDING AT SEGU. REMOVED AND REPLACED NR 7 MAIN WHEEL ASSEMBLY AND BRAKE ASSEMBLY AS PER M/M 32-41-03 AND 32-43-01; ALSO NR 8 TIRE INSPECTED AND FOUND SERVICEABLE TO BE DISPATCHED IN ACCORDANCE WITH ARROW AIR GMM 5-23-7, SECTION "C".SDR 07FDEA02370Access Panel · missingCTR CARGO DOOR ACCESS PANEL FOR VENT DOOR MISSING ON ARRIVAL INTO PDX. OIL: NO RESTRICTION LOWER CENTER CARGO DOOR VENT DOOR MISSING. (OK PER EA 8-5230-113246), (CK AFTER EA FLT) INSPECTED SCRATCH PER SMP 51-80-01 AND DOOR ALL WITHIN LIMITS. COMPLIED WISDR 07FDEA02299Engine · failedRETURN TO RAMP DUE TO INABILITY TO SHUT DOWN APU. FOUND PORTIONS OF N1 HAD EXITED DOWN PASSED APU AIR INLET BOOT AT CLAMPS, SLICED THRU APU PRESSURE OIL LINE AND THEN BECAME LODGED INTO APU COMPARTMENT ACCESS DOOR. APU REF WRI 52-40 2307 FOR THE APU ACCESS SDR G6OA200700001Fire Warning · activatedNR 2 ENGINE FIRE INDICATION AT FL280 WITH LOOP-B SELECTED. ENGINE SHUTDOWN AND AGENT DISCHARGED.SDR 07FDEA02078Fire Warning · illuminatedPDIS:304 EN ROUTE FROM KMEM TO TLC AT FL340, RECEIVED LEVEL 3 CRG FIRE LWR FWD. ACCOMPLISHED PHASE ONE AND REFERRED TO THE RED TABS. THE CKLIST DIRECTED US TO LAND AT THE NEAREST SUITABLE AIRPORT, LANDED KCRP. ACN RELEASED FOR SERVICE PER MEL/CDL: 26-22-01-SDR ARWA20070502Tire · failedPOST FLIGHT FOUND NR 5 TIRE SHREDDED AND DAMAGE TO AIRCRAFT AND NR 1 ENGINE. [SUP 06-01-07] REMOVED AND REPLACED NR 6 MAIN WHEEL ASSEMBLY IN ACCORDANCE WITH DC-10 M/M 32-41-01.SDR ARWA20070501Blades · damagedJUST PRIOR TO ROTATION, DURING TAKEOFF ROLL, A/C SUDDENDLY BEGAN TO VIBRATE, AND DURING INITIAL CLIMB VIBRATION WAS DETERMINED TO BE COMING FROM NR 1 ENGINE. ENGINE WAS SHUTDOWN. [SUP 06-01-07] PERFORMED FULL BOROSCOPE INSPECTION AND FOUND COMPRESSOR SECTIOSDR CLCA2007F0002Clamp · wornAT APPROX 6000 FT NR 2 ENGINE FIRE INDICATION. FOUND CLAMP TO PRECOOLER MANIFOLD WORN.SDR 07FDEA01675Skin · damagedAIRCRAFT HAS DAMAGE TO SKIN P/N ACA3109-1 AT STA 603 BETWEEN LONGERONS 47 AND 48 AND P/N ACA3039-513 CLIP AND NCA 6313-17 LONGERON 47, AS A RESULT OF A FIRE OF THE EXTERNAL POWER WIRING. EXTERNAL POWER WIRING ALSO HAS DAMAGE. REF N/R 004, CUT OUT DAMAGED ARSDR 07FDEA00859Rudder · damagedDURING AUTOPILOT TEST DAMAGED LOWER RUDDER AFT T/E. REPAIRED T/E SECTION IAW SRM 55-30-00 VOL 1 FIG 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I031562/N01562 AND IAW SRM 55-30-00 VOL 1 FIG 2.SDR 07FDEA00857Skin · corrodedFOUND LT WING L/E FOUND CORROSION WITH EXF ON SKIN FIXED PANEL AT STA XOS 910-930. REPAIRED SACRIFICIAL DOUBLER IAW SRM 57-10-00 FIG 19D SHT 1 VOL 1. TOUCHED UP IAW SRM 51-21-01 VOL 2 PAG 21-25 AND SRM 51-21-02 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVESDR 07FDEA00593Skin · crackedLT HORIZ STAB OUTER SECTION UPPER AFT SKIN PANEL FOUND 1 CRACK 2, 5" LONG. REPAIRED CRACKED SKIN PANEL IAW SB 55-18 AND EA NR 8-5510-103679. WORKED IN CONJUNCTION WITH NRC N00898/I030898.SDR 07FDEA00556Seat Track · crackedFOUND MAIN CABIN CRACK 12" LONG ON TRACK X=27 BTWN STA 1079 AND 1099. REMOVED FLOOR PANEL IAW MM 53-21-01-2. REMOVED SEAT TRACK SPLICE AT STA 1129 IAW SRM 51-33-01 VOL 2. CUT AND REPLACED SEAT TRACK SECTION AT STA 1069 IAW SRM 53-70-00 FIG 1 SHEET 1-2. REISDR G60A200800011Skin · corrodedFOUND CORROSION LEFT WING DROOP LEADING EDGE INBD UPPER SKIN.SDR 07FDEA00071Pump · inoperativeON CLIMB-OUT PASSING 16,000', GOT HYD LEVEL 1 ALERT WITH HYD NR 1, NR 2, NR 3 PUMPS OFF. FOUND C/B POPPED. RESET AND IT POPPED AGAIN. RETURNED TO BASE(SJU) MEL 10JAN07. ACN RELEASED FOR SERVICE PER MEL/CDL: 29-11-01 CATEGORY: C EXPIRATION: 20JAN07 "MEL 2SDR 06FDEA04288Duct · rupturedT/O AT SJC NR 2 THROTTLE MUCH FURTHER FWD THAN 1 AND 3 EGT NR 2 CREEPING UP, MAX TEMP = 880' C PULLED NR 2 THROTTLE BACK EVEN W/ 1 AND 3 GOT FIRE WARN, THROTTLE IDLE. SHUT DOWN ENGINE, FIRED BOTTLE NR 1 AS A PRECAUTION. DIVERT TO KOAK. DURING T/O N2 FOR ALSDR ARWA20061201Bleed Valve · malfunctionedNR 3 PNEUMATIC TEMPERATURE HIGH, LIGHT ON; TEMP AT RED LINE. FOUND NR 3 ENGINE FAN AIR VALVE STICKING CLOSED; REMOVED AND REPLACED NR 3 ENGINE FAN AIR VALVE IN ACCORDANCE WITH M/M 36-13-03; ALSO REMOVED AND REPLACED HIGH STAGE TEMPERATURE SENSOR IN ACCORDANCESDR ARWA20061104B-Nut · looseLOSS OF HYDRAULIC FLUID IN SYSTEM NR 3 ACCOMPANIED BY "HYDRAULIC SYSTEM NR 3 ELEVATOR OFF LIGHT". FOUND HORIZONTAL STABILIZER UPPER PRIMARY TRIM CONTROL VALVE PRESSURE LINE B-NUT LOOSE; TIGHTENED PRIMARY TRIM CONTROL VALVE PRESSURE LINE "B" NUT IN ACCORDANCE SDR 06FDEA03937Wire Harness · burnedGROUND POWER IS INTERMITTENT. POWER SHUTS DOWN WHEN A LOAD IS APPLIED. FOUND BURNT "C" PHASE OUTPUT CABLE (C501-21-00C) OF GROUND SERVICE RELAY. REPLACED DAMAGED C501-21-00C CABLE BETWEEN EXTERNAL POWER CONTACTOR R2-218 AND 53-517 REF W/D 24-41-01 PG 703 SHSDR ARWA20061003Seal · missingLOG PAGE NR 125045. UNABLE TO CONTROL PRESSURE IN NORM, AUT, IN MAN CABIN START CLIMB WITH OUTFLOW VALVE FULLY CLOSED. FOUND SEAL MISSING ON OUT-FLOW BUTTERFLY VALVE; INSTALLED SEAL; ON OPERATIONAL CHECK FOUND NORMAL IAW MM 21-30-00.SDR WRLA2006099Attach Bracket · corrodedDURING "C" CHECK IN RME FOUND 5 EA ATTACH BRAKETS CORRODED ON RIGHT O/B FLAP VANE. INSTALLED 5 SERVICABLE ATTACH BRAKETS ON RIGHT FLAP VANE IAW DC10 MM 57-52-02.SDR WRLA2006098Seat Track · corrodedITEM: DURING (C) CHECK IN RME FOUND RT OB TRACK HAS EXFOLIATING CORROSION JUST AFT OF R1 DOOR LAV AREA FUSELAGE STA 466.500. REMOVED RT OB TRACK ON MAIN DECK AND REPLACED AS REQUIRED IAW SRM 53-70-00.SDR ARWA20060802Flap System · lack of lubeWHEN SELECTING FLAP 15, THE FLAP DISAGREE LIGHT CAME ON AND HAD A SLIGHT ROLL TO THE RIGHT. PERFORMED ABNORMAL CHECK FOR NO FLAPS. LUBED LT & RT WING FLAP AND SLAT SYSTEM IAW MM 12-21-04. PERFORMED TEST FLAP MECHANICAL CONTROL AND TEST FLAP HYDRAULIC ACTUATSDR WRLA200637Smoke · detectedFEW SECONDS AFTER NR 3 ENG STARTER WAS ACTIVATED (BUTTON LOCKED) AND LIGHT ILLUMINATED; NOTICED SMOKE WAS COMING OUT OF THE OVERHEAD ANNUNCIATOR PANEL. ABORTED START AND START BUTTON PULLED. ALL POWER WAS TURNED OFF AND SMOKE CEASED.SDR 06FDEA02849Support · corrodedTHE RT INBD AILERON SUPPORT ASSY ACTUATOR FRAME, O/B BARREL NUT BOLT HOLE IS CORRODED. REAMED BARREL NUT BOLT HOLE TO 0.925 DIA" TO REMOVE CORROSION. REQUESTED EA AILERON SUPPORT SUPPORT ASSY ACTUATOR "A" FRAME BOLT HOLE REPAIRED PER EA 8-5740-102045.SDR WRLA2006017Spar Cap · damagedDURING "C" CHECK IN SAT, AIRCRAFT SUSTAINED AN IMPACT DAMAGE TO LT HORIZONTAL STAB FWD SPAR CAP UPPER CHORD AREA, DIRECTLY ABOVE THE FOURTH (FROM INBD) ACCESS HOLE IN FWD SPAR. DAMAGE LENGTH IS APPROX 11.0" LONG. REMOVED DAMAGE FROM HORIZONTAL STAB FWD SPAR SDR WRLA2006035Floorbeam · corrodedDURING "C" CHECK IN SAT FOUND EXFOLIATED CORROSION AT FLOOR BEAM IN STA 1781 RBL 57 (CORROSION ON AFT WEB OF BEAM). FABRICATED BEAM REPAIR SECTION. TREATED,PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-00-01 FIG 9.SDR WRLA2006018Skin · damagedDURING "C" CHECK IN SAT, CENTER CARGO DOOR CUTOUT AT FS 1781 BELOW STR 42 AT EXISTING REPAIR DOUBLER AND EXISTING A/C SKIN STRUCTURE HIT AND PUSHED INTO FRAME 1781 (LOWER T/E OF DOOR CUTOUT). REMOVED HEATER TUBES FROM AFT TQ BOX FS 1781-1787 BETWEEN 538R-542RSDR WRLA2006032Plate · corrodedDURING "C" CHECK IN SAT FOUND NR 1 ENG LEFT FAN COWL CENTER U BOLT PLATE HAS FRETTING CORROSION. REMOVED CORROSION FROM BOLT PLATE, MATERIAL LOSS WAS 0.030 FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-00-01 FIG 1A. FABRICATED NEW BOLT PLATE, TREATED AND PRIMED. SDR WRLA2006036Repair · misinstalledLEFT FUSELAGE SKIN BETWEEN STA 515-535 LONG 28 TO LONG 32 HAS A SKIN SPLICE REPAIR WITH 3EA FREEZ PLUGS INSTALLED, REQUEST TO INSTALL EXTERNAL REPAIR DOUBLER THAT WAS REMOVED, MATERIAL THIKNESS .090. FABRICATED DOUBLER PER EA 010-5320-11-A0302. TREATED, PRIMESDR WRLA2006034Access Panel · corrodedDURING "C" CHECK IN SAT FOUND LEFT WING I/B T/E ACCESS PANEL 541CR HAS THREE AREAS OF CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 IN ALL THREE AREAS. FABRICATED REPAIR DOUBLERS AND BONDED THE 3 AREAS IAW SRM 51-71-00. SEALED AND PRIMED REPSDR WRLA2006033Rub Strip · corrodedDURING "C" CHECK IN SAT FOUND NR 1 ENG LT CORE COWL FWD RUB STRIP AND RH CORE COWL AFT RUB STRIP HAVE CORROSION. REMOVED & REPLACED NR 1 ENG LT CORE COWL FWD RUB STRIP FROM 6 TO 12 O'CLOCK POSITION AND REMOVED & REPLACED RT CORE COWL AFT RUB STRIP FROM 3 TO 6SDR WRLA2006030Skin · corrodedDURING "C" CHECK IN SAT FOUND RIGHT WING NR 4 SPOILER HAS LIGHT CORROSION IN SEVERAL AREAS ON UPPER SURFACE. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 FIG 1A, REMOVED DAMAGED AREA AND CLEANED SURFACE IAW SRM 51-71-00 PAR 4, FABRICATED REPAIR PARTS, SDR WRLA2006031Nose Cowl · crackedDURING "C" CHECK IN SAT FOUND NR 1 ENG NOSE COWL UPPER RH INNER ACOUSTICAL PANEL LOWER FWD CORNER HAS A COMBINATIONOF CRACK .7" CIRCUMFERENTIAL THAT EXTENDS BEYOND 2 FASTNERS AND .6" LONGITUDINAL AND CORROSION. DAMAGE FOUND TO BE TOO EXCESSIVE PER DC10 SRM VOLSDR CLC2006F00007Odor · detectedCREW EXPERIENCED A BOOM SOUND FROM LOWER EXE COMPT. IN CRUISE SHORTLY AFTER CREW BEGAN TO SMELL WHAT APPEARED TO BE EITHER FUMES OR A TRACE OF SMOKE IN COCKPIT. NO ABNORMAL ELECTRICAL CONDITION EXISTED AT THE F/E STATION, EMERGENCY PROCESS WAS FOLLOWED. BY SDR 06FDEA1767Actuator · faultedNR 1 A/P DISENGAGE AFTER T/O. RE-ENGAGED 1 TIME WITH IMMEDIATE DISENGAGED AGAIN. PERFORMED NR 1 AND 2 FCC TEST PER MD 10-30 MM 22-00-00-5. FOUND LIB AILERON ACTUATOR AT FAULT. ALSO, NR 1 AND 2FCC AND AFSCP. REMOVED AND REPLACED 2 FCC, AFSCP AND LIB AILEROSDR 06FDEA1696Shear Tie · corrodedCENTER LWR FUSELAGE FRAME SHEAR TIES AND SKIN HAS LIGHT CORROSION FROM STA 1510 TO 1518 STR 47L TO STR 47R. COMPLIED WITH FEDEX EA E8-5330-96467, FUSELAGE CORROSION IN SKIN AND INTERNAL BULKHEAD TEE, STA 1521 REPAIR.SDR ARWA20060402Compressor · dirtyBETWEEN 50 AND 60 PERCENT N1 NR 3 ENGINE HEAVY VIBRATION. REMOVED, CLEANED, LUBRICATED AND RE-INSTALLED FIRST STAGE FAN ROTOR BLADES IN ACCORDANCE WITH DC-10 A/M/M PAGE 811, M/M 72-21-00; RAN NR 3 ENGINE AT IDLE P/P AND MAX. NO EVIDENCE OF VIBRATION AT ANY SSDR 06FDEA1445Repair · unknownFOUND FLUSH REPAIR LOCATED AT STA 859 L32R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FABRICATED DOUBLER IAW DWG 7097 REV.U. FABRICATED FILLER IAW DC10-30 SRM 53-20-00 FIG 13 SHT 4. INSSDR CLC2006F00004Duct · brokenON CLIMB OUT, NR 1 ENGINE FIRE DETECTOR ILLUMINATED. RETURNED TO DEPARTURE, INSPECTION OF AC ENGINE FOUND BLOWN DUCT. REMOVED AND REPLACED DUCT. (K)SDR CLC2006F00002Duct · brokenON CLIMB OUT- NR 1 ENGINE FIRE DETECTOR ILLUMINATED. RETURNED TO DEPARTURE AIRPORT. INSPECTION OF AREA (ENGINE) FOUND BLOWN DUCT. REPLACED ENGINE. (K)SDR CLC2006F00001Pump · inoperativeAFTER TAKEOFF, RETURNED, REV MOTOR PUMP( RMP ) BLUE LIGHT ON. DURING CLIMB OUT. REMOVED AND REPLACED 2-3 REV PUMP. AFT SHUTOFF VALVE ACTUATOR IAW MM. OPS CHECK OK. (K)SDR CLC2006F00003O-Ring · leakingIN FLIGHT, JUST BEFORE DESCENT, NR 1 HYD QUANTITY DROPPED TO 1 GALLON. CREW PERFORMED IRREGULAR CHECKLIST PROCEDURES, NORMAL, IN CONTACT WITH FLIGHT CONTROL, IT WAS ADVISED FOR MAINTENANCE THAT A RETURN WAS CONSIDERED, CREW AWS FLIGHT CONTROL DECIDED BEST TO SDR ARWA20060205Indicator · inoperativeNO AIR SPEED ON FIRST OFFICER'S SIDE; TAKEOFF ABORTED AT 90 KTS. PERFORMED ADC BOX SELF TEST NO FLAG SHOWED TO AIR SPEED INDICATOR IN ACCORDANCE WITH DC-10 M/M 34-13-00; MAINTENANCE CONTROL ADVISED.
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