Douglas DC-10-30F

Service difficulty reports · 1,152

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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"

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SDR 08FDEA00634Support · misrepairedREWORK OF JOB CARD E8-5340-7-3305 PT4 (INSPECT HORIZONTAL STABILZER SECTION PIVOT SUPPORT AD 96-25-15) STEP 3-A. SHOULD HAVE HAS 6 EACH ADDED HOLES, ONLY 5 WERE DRILLED. REPAIRED HORIZONTAL STAB PIVOT SUPPORT IAW FEDEX EA 8-5340-116955. MAJOR REPAIR.Feb 27, 2008 · N315FE · Doug DC1030F · Fuselage Main, KeelSDR ARWA20080204Engine · stalledDURING ROTATION, NR 3 ENGINE SUFFERED COMPRESSOR STALL AND THE TOWER AND VICINITY AIRCRAFT NOTED FIRE COMING OUT OF ENGINE AFT END. REMOVED AND REPLACED NR 3 ENGINE IN ACCORDANCE WITH ARROW AIR WORK CARD 143R7101M AND DC-10 M/M 71-00-00. PERFORMED ENGINE RUNFeb 23, 2008 · N478CT · Doug DC1030F · Engine (Turbine/Turboprop)SDR 08FDEA00579Attach Fitting · damagedDURING DEPARTURE, PRIOR TO FLAPS RETRACTION RIGHT FLAP TAPES MOVED FROM 20 PERCENT TO 28 PERCENT. AIRCRAFT REQUIRED SIGNIFICANT RT AILERON TO KEEP WINGS LEVEL. ON ARRIVAL AT KMEM, A CONTROLLABILITY CHECK WAS PERFORMED WHEN FLAPS WERE EXTENDED TO 22' RIGHT FLFeb 22, 2008 · N317FE · Doug DC1030F · Trailing Edge FlapsSDR 08FDEA00569Cargo Track · gougedWHILE ACCOMPLISHING "C" CHECK AT TIMCO, THE OUTBOARD RAIL OF THE CARGO LOADING SYSTEM AT 3L POSITION WAS FOUND WITH DAMAGE AT ITS FWD EDGE. TRIM AWAY THE FWD END OF THE SUBJECT RAIL TO REMOVE THE DAMAGE. RESTORE THE ORIGINAL END PROFILE BY COPING FROM THE Feb 22, 2008 · N315FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00555Floor Panel · delaminatedMAIN CABIN FLOORBOARD AT APPROX LBL-60, BETWEEN STA 1239 TO 1321 IS DELAMINATED. MAT ID A402H35039-003 PO 590899.1. FABRICATED NEW BOARD, MAT ID POTTING COMPOUND 1619 A/B PO 666417.3. INSERT SLS 5094A3-400-2 PO 595255, INSERT SLP 5094A3-2 PO 595242. ADHEFeb 21, 2008 · N315FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA00554Floor Panel · delaminatedMAIN CABIN FLOOR PNL FROM STA 1341, LBL-20 FWD EDGE IS DELAMINATED. MAT ID A402H PO590899.1 IAW FEDEX DWG SRZ 25-005 REV F. FABBED FLOOR PNL IAW FEDEX DWG SRZ 25-005 REV F. MAT ID POTING COMP 1619 A/B PO 606417.3. INSERT SLS 5094A3-400-2 PO 595225, INSERFeb 21, 2008 · N315FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA00553Floor Panel · delaminatedMAIN CABIN FLOORBOARD AT APPROX LBL-90, BETWEEN STA 1481 TO 1561 IS DELAMINATED. MAT ID A402H35039-003 PO 5990899.1. POTTING COMPOUND 1619 A/B PO 606417.3, INSERT SLS 5094A3-400-2 PO 595225, INSERT SLP 5094A3-2 PO 595242. ADHESIVE EPIBOND 420 A/B PO 594846.Feb 21, 2008 · N315FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA00552Floor Panel · delaminatedMAIN CABIN CABIN FLOORBOARD AT APPROX LBL-20, BETWEEN STA 495 TO 615 IS DELAMINATED. MAT ID A420H PO 590899.1 IAW FEDEX DWG SRZ 25-005 REV F. FABBED FLOORBOARD PNL IAW FEDEX DWG SRZ 25-005 REV F. MAT ID POTTING COMP 1619 A/B PO 6064173. INSERT SLS 5094A3Feb 21, 2008 · N315FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA00526Indicator · inoperativeR-1 SLIDE DISARM LIGHT IS INTERMITTENT. REMOVED AND REPLACED R-1 DOOR "SLIDE DISARMED" ANNUNCIATOR IAW DC10 AMM 33-00- 00-2. OPS CHECK GOOD IAW DC10 AMM 52-70-00-2. MINOR REPAIR.Feb 20, 2008 · N315FE · Doug DC1030F · Escape SlideSDR 08FDEA00527Power Supply · inoperativeEMERGENCY LIGHTS DO NOT OPERATE CORRECTLY AND FAILED TEST. REMOVED AND REPLACED EMERGANCY LIGHTS BATTERY POWER SUPPLY IAW AMM 33-51-01-2. OPS CHECK GOOD IAW AMM 33-51-01-2. LOCATED BEHIND PANEL 231 AC, CEILING PANEL AFT OF LEFT FWD PASSENGER DOOR. MINFeb 20, 2008 · N315FE · Doug DC1030F · Emergency LightingSDR 08FDEA00519Throttle Cable · failedNR 2 THROTTLE STUCK AT HIGH POWER SETTING AT CRUISE ALTITUDE. ALL ATTEMPTS TO THAW LINKAGES WERE UNSUCCESSFUL. NR 2 ENGINE WAS SHUT DOWN ON APPROACH TO KMEM. AFTER LANDING THROTTLE OPERATED NORMALLY. REMOVED AND REPLACE NR 2 ENGINE THROTTLE CABLE AND THROTFeb 20, 2008 · N560FE · Doug DC1030F · Power LeverSDR 08FDEA00518Bracket · corrodedMAIN CABIN WEB STA 590 TO STA 695 BRACKET HAS NUMEROUS NICKS. FABRICATED NEW - 13 CLIP IAW DWG ACA 7216 REV L. ALODINED CLIP IAW MD/DC-10-30 SRM 51-21-01 PG 25, VOL II. PRIMED CLIP IAW MD/DC-10-30 SRM 51-21-01 PG 21, VOL II. PAINTED CLIP IAW MD/DC-10-30 SRFeb 19, 2008 · N315FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 08FDEA00516Bracket · damagedWEB SUPPORT BRACKET ACA 7218-31 HAS TOOLING MARKS. BLENDED TOOLING MARKS ON WEB SUPPORT BRACKET IAW SRM 51-21-02, VOL II. ORIGINAL MATERIAL THICKNESS .090 IAW DWG ACA 7218 REV E MATERIAL LOSS .068, OUT OF LIMITS IAW SRM 53-00-01, VOL I. FABRICATED NEW ACA 7Feb 19, 2008 · N315FE · Doug DC1030F · Fuselage Main, Attach FittingsSDR 08FDEA00495Panel · chafedNR 3 PYLON AFT "V" PANEL NR 488 GL, ATTACHMENT HOLES CHAFFED. BLENDED DAMAGED AREAS, MAXIMUM DEPTH .055 IAW SRM 54-00-01, FIG 1A VOL I. FABRICATION PER EA NR 8-5480-118437. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II, PG 21-24. INSTALLED DOUBLER AND FILLFeb 18, 2008 · N315FE · Doug DC1030F · Nacelle/Pylon, Plate/SkinSDR 08FDEA00499Floorboard · delaminatedMAIN CABIN FLOORBOARD AT APPROX BL-0 BETWEEN STA 495 TO 615 IN DELAMINATED. FABRICATED NEW FLOOR BOARD PANEL STA 495 TO 615, POTTED EDGES, COMPLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS, APPLIED NON-SKID AND PART MARKED IAW SRZ 25-005 REV F. INSTFeb 18, 2008 · N315FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA00498Floorboard · delaminatedMAIN CABIN FLOORBOARD AT APPROX LBL - 90, BETWEEN STA 595 TO 675 IS DELAMINATED. FABRICATED NEW FLOORBOARD STA NR 595 - 675. POTTED EDGES, COMPLETED CURE AND SANDED, INSTALLED INSERTS, APPLIED NON-SKID MARKED MANUAL IAW SRZ 25-005 REV F. INSTALLED IAW SRM 5Feb 18, 2008 · N315FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA00497Retainer · tornCTR CARGO DOOR FWD LOWER L/E SEAL RETAINER IS BROKEN (INTERIOR). REMOVED AND INSTALLED RETAINER IAW DC-10 SRM 51-35-01, VOL II. MAT ID .032 7075-T6 PO NR 547197.3 AND FABBED IAW DAC DWG ANB 7328. ALODINE AND PRIME IAW DC-10 SRM 51-21-01, VOL II. PART MARKEFeb 18, 2008 · N315FE · Doug DC1030F · Cargo/Baggage DoorsSDR 08FDEA00496Wire · brokenBY R-1 DOOR AIR BOTTLE TERMINAL BLOCK 53-901 HAS BROKEN WIRES AND TERMINAL BLOCK. REPLACED TERMINAL STRIP 53-901 IAW WDM 33-52-01. OP'S CHECKED EMERGENCY EXIT LIGHTS IAW 33-51-01-2, OPS CHECK GOOD. MINOR REPAIR.Feb 18, 2008 · N315FE · Doug DC1030F · Electrical Power System WiringSDR 08FDEA00494Seat Track · gougedMAIN CABIN SEAT TRACK SCALLOPS ARE GOUGED FROM STA 1461 TO 1521 BL 48L. REMOVED AND REPLACED DAMAGED SEAT TRACK IAW FEDEX DWG NR NEA 6022 REV AM. INSTALLED SPLICE HAT AND 2 SPLICE PLATES IAW MD-10 / DC-10 SRM 53-70-00, VOL I. ALODINED/PRIMED AND TOP COAT IAFeb 18, 2008 · N315FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00493Beam · crackedCABIN OVERWING DOOR LT SIDE AFT UPPER STOP FITTING IS CRACKED. REMOVED AND REPLACED BEAM IAW FEDEX DWG NR ADA 3462 REV AE AND MD-10/DC-10 SRM 51-31-01, VOL II.Feb 18, 2008 · N315FE · Doug DC1030F · Passenger/Crew DoorsSDR 08FDEA00459Floorboard · damagedMAIN CABIN FLOORBOARD AT APPROX RBL-20, BETWEEN STA 1821 TO 1761 IS SPONGY. FABBED FLOORBOARD, LOCATED AND POTTED INSERTS, POTTED AND SANDED THE EDGES AND APPLIED THE ANTI-SKID IAW DWG SRZ-005 REV F. INSTALLED FLOORBOARD IAW SRM 51-31-01 VOL II.Feb 15, 2008 · N315FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA00458Floor Panel · delaminatedUPPER CARGO COMPARTMENT, AFT SECTION, LT SIDE AT STA 1741, THE O/B PANEL NR 281 FE (ORANGE) (MARKED AS "14L") IS DELAMINATED AND HAS TWO SMALL PUNCTURES. FABRICATED NEW FLOOR PANEL 281FE, POTTED EDGE, COMPLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTSFeb 15, 2008 · N315FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA00457Floor Panel · delaminatedMAIN CABIN FLOOR PNL AT STA 1481 TO 1561, LBL 40 FWD CORNER DELAMINATED. FABRICATED NEW FLOOR PANEL STA 1481 TO 1561, POTTED EDGES, COMPLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX SRZ 25-005 REV F.Feb 15, 2008 · N315FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA00456Floorboard · damagedMAIN CABIN FLOORBOARD AT LBL - 20, BETWEEN STA 1821 TO 1881 IS SPONGY. FABBED FLOORBOARD IAW SRZ-25-005 REF F. INSTALLED FLOORBOARD IAW SRM 51-31-01 VOL II. LOCATED, DIRLLED HOLES. INSTALLED INSERTS, INSTALLED ANTISKID IAW DWG SRZ 25-005 REV F. INSTALFeb 15, 2008 · N315FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA00455Floorboard · delaminatedMAIN CABIN FLOORBOARD AT APPROX RBL-90, BETWEEN STA 800 TO 850 IS DELAMINATED. REMOVED FLOORBOARD IAW AMM 53-21-01-2. FABBED FLOORBOARD IAW SRZ-25-005 REV F. LOCATED HOLES FOR INSERTS IAW DWG SRZ 25-005 REV F. POTTED EDGES AND STARTED CURE IAW DWG SRZ 25-0Feb 15, 2008 · N315FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA00454Floorboard · damagedMAIN CABIN FLOORBOARD AT APPROX LBL 38, BETWEEN STA 595 TO 675 IS WARPED. FABBED FLOORBOARD PANEL AT STA 595-675 IAW DWG SRZ 25-005 REV F. LOCATED HOLES, COUNTERBORED HOLES, POTTED INSERTS, POTTED EDGES, CURED EDGES, SANDED EDGES, APPLIED ANTI-SKID IAW Feb 15, 2008 · N315FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA00453Floor Panel · damagedCABIN FLOOR PANEL AT STA 555 RBL 8.5 TO 27.5 HAS EDGE DAMAGE AND HOLES. FABRICATED NEW FLOOR PANEL STA 555, POTTED EDGES, COMPETED CURE AND SANDED EDGE POTTING, INSTALLED INSERTS AND APPLIED ANTI-SKID IAW FEDEX DWG SRZ 25-005 REV F. THIS IS A MINOR RFeb 15, 2008 · N315FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA00452Floorboard · delaminatedMAIN CABIN FLOORBOARD AT APPROX RBL-20, AT APPROX BETWEEN STA 899 TO 979 IS DELAMINATED. FABBED NEW FLOORBOARD STA 899 TO 979, POTTED EDGES, COMPLETED CURE AND SANDED. INSTALLED INSERT , APPLIED ANTI-SKID, MARKED PNL IAW FEDEX DWG SRZ 25-005 REV F. THIS IFeb 15, 2008 · N315FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA00448Beam · crackedFWD CARGO COMPT PERFORMED REWORKING IAW EO 8-2550-7-2354 P1 ON BEAM FOUND CRACK. REPAIRED BEAM IAW SRM 53-60-01 FIG 3 VOL I.Feb 15, 2008 · N306FE · Doug DC1030F · Fuselage Main, StructureSDR 08FDEA00447Strap · bentAFT PIT, AFT BULKHEAD STRAP 187 CA (NWJ 6006-19)(MARKED AS B2/C2) IS DAMAGED, BENT, HAS ELONGATED FASTENER HOLES AND IS CORRODED. FORMED HAT SECTION PER DAC DWG NWJ 6006 REV C AND FEDEX GMM 7-0-1001 PG 2. FABBED HAT SECTION PER FEDEX GMM 7-0-1001 AND DAC DWGFeb 14, 2008 · N315FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 08FDEA00446Strap · bentAFT PIT, AFT BULKHEAD STRAP 187 CA (NWJ 6006-19)(MARKED AS B4/C4) IS DAMAGED, BENT, HAS 4 ELONGATED FASTENER HOLES AND IS CORRODED. MINOR REPAIR. FORMED HAT SECTION PER DAC DWG NWJ 6006 REV C AND FEDEX GMM 7-0-1001, PG 2. FABBED HAT SECTION PER FEDEX GMM Feb 14, 2008 · N315FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 08FDEA00445Support · wornAFT PIT, AFT BULKHEAD STRAP 187EA (NWJ6006-35) (NWJ6006-25NC) (MARKED AS "A2-A4) STRAP IS CRACKED ON THE (A2 END), HAS CORROSION, IS DENTED AND ALL 4 FASTENER HOLES ARE GOUGED. FORMED SUPPORT PER DAC DWG NWJ6006 REV C AND FEDEX GMM 7-0-1001, PG 2. FABRICATEDFeb 14, 2008 · N315FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 08FDEA00444Panel · corrodedRT WING TANK PLATE PANEL NR 634 AT IS CORRODED. MACHINED NEW FUEL PANEL (545) IAW DAC DWG ARB 0872 REV AV AND ALODINED AND PRIMED, 545 FUEL PANEL IAW DPS 4.50 -127 AND MIL-C-5541 AFTER FINDING ORIGINAL PANEL WAS UNDER LIMITS AFTER CORROSION REMOVAL.Feb 14, 2008 · N315FE · Doug DC1030F · Fuel StorageSDR G60A200800029Bulkhead · dentedAFT CARGO FWD BULKHEAD RT POST HAS DENT IN MID SECTION 3 CRACKS.Feb 8, 2008 · N607GC · Doug DC1030F · Fuselage Main, BulkheadSDR G60A200800028Tail Cone · crackedTAILCONE CRACKED APPROX 1 INCH AT UPPER RT SIDE IN WEB.Feb 8, 2008 · N607GC · Doug DC1030F · Aerodynamic FairingsSDR G60A200800027Attach Angle · crackedLT PYLON UPPER OUTBOARD SIDE STA YN214 ATTACH ANGLE CRACKED.Feb 8, 2008 · N607GC · Doug DC1030F · Nacelle/Pylon, Attach FittingsSDR G60A200800026Skin · crackedFWD CARGO DOOR CUTOUT AFT EDGE FUSELAGE SKIN CRACKED APPROX 1/4".Feb 8, 2008 · N607GC · Doug DC1030F · Fuselage Main, Plate/SkinSDR G60A200800025Bulkhead · crackedFWD CARGO COMPT AFT BULKHEAD HAS 2 CRACKS APPROX 1".Feb 8, 2008 · N607GC · Doug DC1030F · Fuselage Main, BulkheadSDR G60A200800024Structure · crackedAFT CARGO FWD BULKHEAD INBD POST HAS 2 CRACKS AT TOP CORNER.Feb 8, 2008 · N607GC · Doug DC1030F · Fuselage Main, BulkheadSDR G60A200800023Rib · crackedFOUND LT PYLON PNL 437FL RIB CRACKED.Feb 8, 2008 · N607GC · Doug DC1030F · Nacelle/Pylon, Frame/Spar/RibSDR G60A200800022Floor Support · crackedFWD CARGO COMPT STA 1009 LWR SIDEWALL FLOOR SUPPORT LWR END CRACKED 1 1/2".Feb 8, 2008 · N607GC · Doug DC1030F · Fuselage Miscellaneous StructureSDR G60A200800021Rib · crackedRT WING REFUEL/DEFUEL BAY OUTBD RIB LWR AFT END CRACKED 1.5 INCH.Feb 8, 2008 · N607GC · Doug DC1030F · Wing, Rib/BulkheadSDR G60A200800020Skin · crackedLT WING TIP TOP SIDE OUTBD AFT END SKIN CRACKED APPROX 5".Feb 8, 2008 · N607GC · Doug DC1030F · Wing, Plate/SkinSDR G60A200800018Rib · crackedFOUND LT L/E SLAT NR 1 RIB CRACKED AT STA XIS 177.Feb 7, 2008 · N606GC · Doug DC1030F · Leading Edge DevicesSDR G60A200800019Rib · crackedFOUND LT L/E SLAT NR 1 RIB CRACKED AT STA XIS 183.Feb 7, 2008 · N606GC · Doug DC1030F · Leading Edge DevicesSDR G60A200800017Rib · crackedFOUND LT L/E SLAT NR 1 RIB CRACKED AT STA XIS 201.Feb 7, 2008 · N606GC · Doug DC1030F · Leading Edge DevicesSDR G60A200800016Rib · crackedFOUND LT L/E SLAT NR 1 RIB CRACKED AT STA XIS 189.Feb 7, 2008 · N606GC · Doug DC1030F · Leading Edge DevicesSDR G60A200800015Skin · crackedNR 2 PYL PANEL 437HL HAS CRACKS.Feb 7, 2008 · N606GC · Doug DC1030F · Nacelle/Pylon, Plate/SkinSDR G60A200800014Panel · crackedNR 2 ENG PYLON PANEL 437DR HAS CRACK NEAR BASE OF FIN.Feb 7, 2008 · N606GC · Doug DC1030F · Nacelle/Pylon, Plate/SkinSDR G60A200800013Angle · crackedRT INBOARD FLAP INBOARD LWR CLOSE OUT PANEL HAS CRACKED ANGLE.Feb 7, 2008 · N606GC · Doug DC1030F · Trailing Edge Flaps
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