Douglas DC-10-30F
Service difficulty reports · 1,152
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 = '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 04FDEA03389Filter · cloggedAFTER T/O DURING LANDING GEAR RETRACTION, OBSERVED BOTH NR 1 AND 3 ENG FUEL FILTER PRESSURE DROP LIGHTS WERE ILLUMINATED. AFTER SELECTING CLIMB POWER. THE NR 3 LIGHT EXTINGUISHED AND NR 1 REMAINED ILLUMINATED. LEVELED OFF AT 5000 FT AND WHEN THE POWER WAS SDR WLDA2004106Structure · vibrationDAY/BRU ABORTED TAKEOFF AT 70 KTS DUE TO VIBRATION. INSPECTED ALL WHEELS AND BRAKES, FLAPS AND SPOILERS, NOSE GEAR AND NR 1 & 3 INLETS, NO DEFECTS NOTED. REVERIFIED ALL TIRE PRESSURE, ALL CHECKED NORMAL.SDR 2004FA0000909Retainer · mislocatedDURING A ROUTINE "A-CHECK", FINNAIR FAA REPAIR STATION WAS REQUESTED TO PERFORM FAN BLADE LUBRICATION OF POSITION NR 3 ENGINE ON DA-10,N303WL. INSPECTION OF THE FAN BLADES REVEALED THAT ALL FAN BLADE SPACERS WERE IMPROPERLY INSTALLED. THE SPACER RETAINER LIPSDR 04FDEA03050Door Frame · gougedFUSELAGE CORROSION/GOUGES ON MAIN CARGO DOOR FRAME. COMPLIED WITH EA 8-5310-82067. FUSELAGE CORROSION GOUGES ON MAIN CARGO DOOR FRAME.SDR 04FDEA02868Blanket · burnedIN CENTER ACCESSORY COMPARTMENT AT THE LT AND RT FUSELAGE FEED THROUGH FOR THE PNEUMATIC SUPPLY DUCTS 1-2 AND 1-3 HAVE FUSELAGE INSULATION BLANKETS SEVERELY BURNED AROUND THE DUCT. A/C FUSELAGE WAS INSTALLED WITH OLD TYPE OF INSULATION BLANKET. (P/N 392945SDR 04FDEA02772Fitting · nickedLEFT HAND WING PYLON AFT ATTACH CLEVIS FITTING FORWARD LOBE HAS NICK. BLENDED AREA IAW DC10 SRM 57-00-01 VOL I, FOUND TO BE WITH IN LIMITS IAW DC10 SRM 57-00-01 VOL I, AND EA 8-5742-81464, PRIMED IAW DC10 SRM 51-21-01 VOL II. REMOVED APPROXIMATELY 0.060 INCHSDR 04FDEA02774Pipe · brokenAFT CARGO COMPARTMENT HEATING PIPE BROKEN AT STA 1910. REMOVED PIPING LINE FOR REPAIR IAW DC10 MM 20-10-01. CUT OUT AND FABRICATED AND WELDED IN NEW SECTION IAW FEDEX EA 8-2140-81471. INSTALLED PIPING AT AFT CARGO COMPARTMENT IAW DC10-30 MM 20-10-01, LEAK CSDR 04FDEA02773Skin · damagedREPAIR DOUBLER ON RIGHT HAND FUSELAGE STA 1781 TO 1815 BETWEEN L-29R AND L-30R, NOT IAW DC10-30 SRM. REMOVED REPAIR DOUBLERS IAW DC10-30 SRM 51-33-01 VOL II AND 51-35-01 VOL II. FABRICATED FINGER DOUBLERS AND EXTERNAL DOUBLERS AND INSTALLED IAW DC10-30 SRM 5SDR 04FDEA02771Ventilator Panel · crackedNR 3 PYLON VENT PANEL 487 DR HAS SEVERAL CRACKS. ROUTED OUT CRACKS IN WELDED AREA, FABRICATED FILLER AND WELDED IAW FEDEX EA 8-5480-31457. REMOVED AND REPLACED CRACKED BRACKET, FABRICATED BRACKET IAW DOUGLAS DWG AUB 7054, REINSTALLED SKIN IAW DC10-30 SRM 51SDR 04FDEA02722Bushing · wornNR 3 PYLON THRUST LINK PYLON LUGS HAS 2 WORN BUSHINGS. REMOVED AND REPLACED IAW FEDEX DC10 CMM 20-20-07.SDR 04FDEA02720Bearing · corrodedNR 3 PYLON TOMBSTONE FITTING UPPER BEARING PITTED. REMOVED AND REPLACED NR 3 PYLON UPPER SPHERICAL BEARING IAW DC10-30 MM 54-40-02-2.SDR 04FDEA02718Bearing · migratedNR 1 ENG PYLON AFT SPHERICAL BEARING ATTACH BOLT TORQUE STRIP BROKEN & THE BEARING MIGRATES. REMOVED AND REPLACED BEARING IAW DC 10-30 FEDEX MM 54-40-02-2, REMOVED CORROSION IAW DC10-30 FEDEX MM 54-40-02, REMOVED FUEL DRAIN LINE IAW FEDEX DC 10-30 MM 0- 50-01SDR 04FDEA02717Fitting · migratedNR 3 ENGINE PYLON AFT SPHERICAL BEARING MIGRATES. REMOVED SPHERICAL BEARING IAW DC10-30MM FEDEX 54-40-02 HONED HOLE IAW DC 10-30 FEDX AMM 54-40-02-2, REMOVED DRAIN LINE IAW FEDEX DC10-30 MM 54-10-00, REMOVED NUT STRIPS IAW DC10-30 FEDEX SRM 51-31-01, INST NSDR 04FDEA02716Seat Track · crackedMAIN CABIN, CARGO SEAT TRACK HAS 2 CRACKS AT LBL 24 & STA 1009 TO 1059 (MRK). REMOVED 2 FLOORBOARDS. REMOVED AND REPLACED SEAT TRACK IAW 51-31-01 VOL 2 OF FEDEX DC10-30 SRM MAT ID FOR SEAT TRACK 7929147-1350 IAW FEDEX DC10-30 SRM 53-42-01 FIG 4 SH1 VOL 3 MATSDR 04FDEA02715Seat Track · corrodedR/S AFT PIT STA 1841 TO 1902 OUTBOARD FLANG OF SEAT TRACK CORRODED. REMOVED CORROSION ON SEAT TRACK IAW FEDEX DC10-30 SRM 51-21-01 VOL 2 PG 21. FOUND TO BE OUT LIMITS, IAW FEDEX DC10 SRM 53-70-00 PG 21 VOL I, MAKE NEW SEAT TRACK IAW DAC DWG AGA3855, TREATMENSDR 04FDEA02713Floorbeam · corrodedAFT PIT STA 1902 FLOOR SUPPORT FRAME T-CAP CORRODED UPPER SURFACE. REMOVED FRAME T-CAP IAW DC10 SRM 51-35-01 VOL 2. CORROSION OUT OF LIMITS IAW FEDEX DC10 SRM 53-00-01 VOL I, PG 8. MATERIAL FOR T-CAP ANGLE IS 7075-T6 .063 P/O 353160.4 IAW DC 10 SRM 53-16-01SDR 04FDEA02712Floorbeam · corrodedAFT PIT STA 1902, 20 LBL TO 20 RBL FLOOR SUPPORT FRAME CORRODED TOP SIDE OF T-CAP. REMOVED FRAME T-CAP IAW DC10 SRM 51-35-01 VOL 3, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL I. REMOVED DAMAGE IAW DC10 SRM 53-00-01 VOL I. FAB FILLER DOUBLER IAW DC1SDR 04FDEA02711Bearing · migratedNR 3 ENGINE AFT MOUNT O/B VERTICAL LINK HAS BOTH BEARINGS MIGRATING. REMOVED UNSERVICABLE NR 3 AFT ENGINE MOUNT, INSTALLED SERVICEABLE NR 3 AFT ENGINE MOUNT ASSEMBLY IAW DC10-30 MM 71-20-01-03.SDR 04FDEA02699Fitting · corrodedNR 1 PYLON TOMBSTONE FITTING UPPER BEARING STIFF AND PITTED. REMOVED UPPER SPHERICLE BEARING FROM NR 1 PYLON TOMBSTONE CHECKED DIAMETRICAL CLEARANCE OF NEW BEARING INSIDE DIA AND PLUG IS .0001 MAX CLEARNCE .012. CLEARANCE CHECK OK IDENTIFIED MOUNT BOLT TO BESDR 04FDEA02649Fitting · migratedNUMBER 1 ENGINE PYLON AFT SPHERICAL ATTACH BOLT TORQUE STRIPE BROKEN AND THE BEARING IS MIGRATING. REMOVED BEARING IAW DC10MM 54-40-02, REMOVED CORROSION IAW DC10 MM 54-40-02. REMOVED AFT BULKHEAD FITTING AUB 7025-33 IAW DC10-30 SRM 51-31-01 VOL II, LOCATED,SDR 04FDEA02648Fitting · migratedNUMBER 3 ENGINE PYLON AFT SPHERICAL BEARING MIGRATING. REMOVED SPHERICAL BEARING HONED HOLE REMOVED AFT BULKHEAD FITTING, LOCATED AND DRILLED NEW FITTING IAW DAC DWG AUB 7025, INSTALLED NEW FITTING P/N AUB 7025-33 IAW DAC DWG AUB 7025 IAW FEDEX DC10 SRM 51-38SDR 04FDEA02651Hinge Fitting · corrodedLEFT WING INBOARD FLAP, OUTBOARD HINGE SUPPORT, PIVOT ATTACH POINT, INBOARD BORE PITTED AND CORRODED. REMOVED CORROSION, ORIGINAL DIAMETER 1.240, FINAL DIAMETER 1.2819, MATERIAL REMOVED .0419 IS BEYOND LIMITS. FABRICATED OVERSIZED BUSHING, INSTALLED AND HONESDR 04FDEA02650Hinge Fitting · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE SUPPORT, PIVOT ATTACH POINT, INBOARD BORE CORRODED. REMOVED CORROSION, ORIGINAL DIAMETER 1.1885 FINAL DIAMETER 1.3817, FOUND TO BE OUT OF LIMITS. FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED TO FINAL INSIDE DIAMETESDR 04FDEA02645Liner · crackedAFT LOWER CARGO COMPARTMENT FORWARD THRESHOLD ATTACH EAR IS CRACKED. WELD REPAIRED AFT CARGO DOOR LINER IAW FEDEX EA 8-5320-81459. REFERENCE N/R N00682.SDR 04FDEA02646Panel · delaminatedRIGHT WING PANEL 635 GL DELAMINATED AND ONE GOUGE. REPAIRED PANEL 635 GL BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC DWG ARC2008 AND FEDEX EA 8-5750-81442. REFERENCE N/R N00239.SDR 04FDEA02641Doubler · tornLEFT WING LEADING EDGE CAVITY, CORRUGATED SKIN TORN ABOVE ANTI-ICE TELESCOPE DUCT, STA XORS 372. REMOVED AND INSTALLED TELESCOPING DUCT IAW DC10 MM 30-11-01-2. REPAIRED DAMAGED SKIN IAW FEDEX EA 8-5710-81456 STEP 1-10, REFERENCE N/R N00730.SDR 04FDEA02640Panel · delaminatedLEFT WING LOWER TRAILING EDGE PANE 541KB DELAMINATED INTERIOR SURFACE. REMOVED INNER SKIN, OUTER SKIN, DOUBLER AND CORE IAW FEDEX EA 8-5750-81445. BONDED NEW INNER SKIN, OUTER SKIN DOUBLER AND CORE IAW FEDEX EA 8-5750-81445 AND TPS 1001 REV E, REFERENCE N/R SDR 04FDEA02639Roller · corrodedLEFT WING INBOARD FLAP INBOARD TRACK 1 EACH AFT UPPER SMALL ROLLER IS PITTED. REMOVED AND REPLACED LEFT HAND INBOARD FLAP INBOARD TRACK AFT UPPER SMALL LOAD ROLLER IAW FEDEX EA> 8-5750-81449. ORIGINAL COPY OF EA 8-5750-81449 IS ATTACHED TO FEDEX N/R N00910, SDR 04FDEA02605Connector · miswiredAT C-CHECK, NR HYD SYS SHUTOFF VALVE FAILED THE OP'S CK. THE ELECTRIC ELEVATOR SHOV FAILED TO MOVE TO THE CLOSED POSITION. NR 3 ELEVATOR OFF ALERT SHOWS. T/S AND FOUND CONNECTOR P10- 548B MISPINNED. WIRE E204-125-20 WAS IN HOLE NR 9 AND NOT NR 2 AS CALLSDR 2004F00236Fuse Link · shearedRT OB SLAT RETAINER MECHANISM MECHANICAL FUSE SHEARED. (REFERENCE MM 27-83-08 PAGE 202 FIGURE 201) REFERENCE NON-ROUTINE 39546.SDR 2004F00237Sleeve · crackedNR 3 ENGINE IB THRUST REVERSER EXTRUDED TORQUE RING, AT THE LEADING EDGE OF TRANSLATING SLEEVE, CRACKED AROUND FASTENER HOLE AT 10 O'CLOCK (REVERSER DEPLOYED). REFERENCE NON-ROUTINE 39502.SDR 2004FA0000678Fuse Pin · shearedRT WING OB SLAT CONTROL MECHANISM HAS ANTI-DROOP FUSE PIN SHEARED. REFERENCE NON-ROUTINE 39501.SDR 2004FA0000679Attach Fitting · corrodedLOWER AFT WING TO CENTER BOX ATTACH SKATE FITTING IS EXFOLIATED, LT WHEEL WELL, FUSELAGE STATION 1366 TO 1381. REFERENCE NON-ROUTINE NR 39431.SDR 04FDEA01935Spar · damagedRT WING STATION XW255.000, LOWER SPAR BEAM OUTBOARD HOLE "C" ON PAGE 9 OF 18 OF EO 8-5750-7-5001 PART 2, HOLE HAS TOOLING DAMAGE. REAMED HOLE TO FINAL SIZE OF 1.0022, ALODINE BORE IAW EA 8-5710-77571, FABRICATED BUSHING IAW EA 8-5710-77571, PERFORMED FPI INSPSDR 04FDEA01871Warning Light · illuminatedUPON LOWERING GEAR FOR LANDING, GOT "ANTI SKID L FAIL" ALERT, WENT MISSED APPROACH AND RAISED GEAR. LOWERED GEAR A SECOND TIME AND GOT SAME ALERT. FOLLOWED CHECKLIST BY TURNING ANTI-SKID OFF, THEN BACK TO ARM. ALERT WENT OUT. TESTED ANTI-SKID AND ALERT SSDR 04FDEA01130Bulb · faultyENG 1 OIL TEMP HIGH, TEMP 226; ABOVE RED LINE. READJUSTED POWER, TEMP REMAINED ABOVE RED LINE. SHUT DOWN NR 1 ENGINE AND LANDED. OIL TEMP SLOWLY RETURNED TO A LOWER SETTING. OIL PRESSURE & QTY NORMAL. NO VIBRATIONS. RAN ENG NR 1, OIL TEMP AT 4 MIN WAS 14SDR G6OA042704Coalescer Bag · contaminatedSMOKE IN COCKPIT FROM PILOT AND COPILOT FOOT WELL.SDR 04FDEA00575Access Panel · corrodedCORROSION ON FUEL TANK ACCESS 534CB, AT MATING SURFACE. RECEIVED NEW PANEL P/N ARB0872-507, TO BE INSTALLED ON WORK CARD 575I5503-01.SDR 04FDEA00574Hinge · corrodedREWORK RT OUTBD FLAP OUTBD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION WRITTEN FOR CLARIFICATION JPF. REMOVED BUSHING & CORROSION IAW DC10 CMM 57-44-09, FINAL HOLE SIZE 1.192, FOUND OUT OF LIMITS. FABRICATED BUSHING IAW DC10 CMM 57-44-09 AND EO 8-5SDR 04FDEA00573Hinge · damagedREWORK BARREL NUT HOLE NR 10 IS LARGER THAN CMM LIMIT ON RT WING O/B-I/B FLAP HINGE FITTING. CLARIFICATION OF N01776. N01776 & N02167 REMOVED BUSHING & OPEN BORE TO .748 IAW DC10 MM 57-44-08, HEAT TREATED BUSHING MAT'L IAW DPS 5.00-2 & DPS 1.05.5, ETCHED BSDR 04FDEA00572Seat Track · corrodedMAIN CABIN AT FS 835 - 870 AT LBL 8.5 SEAT TRACK HAS CORROSION AFT INBOARD FLANGE. REMOVED CORRECTED SECTION OF SEAT TRACK. FABRICATED NEW SECTION OF SEAT TRACK AND INSTALLED IAW DC10 SRM 53-42-01 VOL 1, DC10 SRM 53-70-00 VOL 1 AND DC10 SRM 51-21-01 VOL 2.SDR 04FDEA00571Shear Tie · corrodedAFT LWR CARGO COMPARTMENT FS 1971 AFT SIDE OF FRAME BETWEEN L-51L AND L-51R SHEAR TIE IS CORRODED. REMOVED SHEAR TIE, INTERCOSTAL, CLIPS AND SPLICE FRAME. CORROSION ON SHEAR TIE FOUND OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL 1. INSTALLED NEW SHEAR TIE, INTERSDR 04FDEA00570Bulkhead · corrodedFWD NOSE WHEEL WELL BULKHEAD FWD SIDE HAS A CORRODED STRAP. REMOVED CORRODED STRAP. STRAP FOUND TO BE AN EXISTING REPAIR. FABRICATED REPAIR IAW DC10 SRM 53-00-01 VOL 1. INSTALLED IAW DC10 SRM 51-33-01 VOL 2, CORROSION FOUND TO BE LEVEL 2.SDR 04FDEA00569Bulkhead · corrodedFWD NOSE WHEEL WELL BULKHEAD FWD SIDE HAS A CORRODED STRAP. REMOVED CORRODED STRAP. STRAP FOUND TO BE AN EXISTING REPAIR. FABRICATED REPAIR IAW DC10 SRM 53-00-01 VOL 1. INSTALLED IAW DC10 SRM 51-33-01 VOL 2, CORROSION FOUND TO BE LEVEL 2.SDR 04FDEA00568Access Panel · corrodedPITTING INSIDE SEAL GROOVE/MATING SURFACE ON FUEL TANK ACCESS PANEL 638BB. PITTING OUT OF LIMITS. REPLACED PANEL 638BB IAW DC10 MM 28-00-00-2.SDR 04FDEA00553Hinge · corrodedRIGHT OUTBOARD FLAP OUTBOARD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION. DURING EO 5750-7-5000, CORROSION WAS FOUND IN THE 2 RIGHT OUTBOARD FLAP HINGE FITTING NR 5 OUTBOARD MOUNTING HOLES. THE SUBJECT CORROSION WAS REMOVED TO A FINAL DIAMETER OF 1SDR 04FDEA00552Hinge · corrodedRIGHT OUTBOARD FLAP INBOARD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION. DURING C-CHECK INSPECTION CORROSION WAS FOUND IN THE INNER BORE OF ARC0538-501 OUTBOARD FLAP FORWARD CLEVIS FITTING. THE SUBJECT CORROSION WAS REMOVED BY OVERSIZING THE SUBJECSDR 04FDEA00551Hinge Fitting · corrodedRIGHT OUTBOARD FLAP OUTBOARD HINGE FITTING AUCT MOUNT POINT HOLE HAS CORROSION AT BORE 5 A&B. DURING EO 8-5750-7-5000, CORROSION WAS FOUND IN THE 2 RT FLAP OUTBOARD HINGE FITTING NR 5 OUTBOARD MOUNTING HOLES. THE SUBJECT CORROSION WAS REMOVED TO A FINAL DIAMSDR 04FDEA00550Mount · corrodedDURING C-CHECK INSPECTION, CORROSION WAS FOUND IN THE CENTER BORE OF THE ANB7016-6 RT INBOARD FLAP DRIVE BEARING MOUNT BORE. THE SUBJECT CORROSION WAS REMOVED BY OVERSIZING THE SUBJECT HOLE TO 1.0210 INCH DIA. REMOVED FITTING IAW DC10 SRM 51-31-00 VOL II. RSDR 04FDEA00549Hinge · corrodedLEFT OUTBOARD FLAP INBOARD FWD HINGE AT REAR SPAR OUTBOARD LWR MOUNT HOLE CORRODED AT BORE NR 3. REWORK LEFT OUTBOARD FLAP INBOARD FWD HINGE AT REAR SPAR OUTBOARD LWR MOUNT HOLE CORRODED AT BORE NR 3. REMOVED BUSHING AND CORROSION IAW CMM 57-44-8. FABRICATE
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