Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = 'DC873F'
  ORDER BY difficulty_date DESC"

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SDR DHLA201000096Skin · deformedLT OTBD AIL LWR PLATING DEFORMED STA XA 741.000 PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 4. REMOVED DEFORMED NOSE PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-3-0. FABRICATED NEW NOSE PLATING (AL2024T3 0.032") IAW SRM 57-8-1 FIG. 4 ITEM "H". CLEANED, TRESep 2, 2010 · N804DH · Doug DC873F · AileronsSDR DHLA201000128Cargo Track · wornUPPER CARGO COMPT.-NR3 TRACK LUGS WORN (STA 1670.000 - 1702.000). PERFORMED MAJOR REPAIR IAW SRM 53-2-3, FIG 12, SHEET 1, PG 49-50. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT EXTRUSION PN S277Sep 1, 2010 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHLA201000127Cargo Track · wornUPPER CARGO COMPT.- NR4 TRACK LUG WORN (STA 57.000 - 110.000). PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG 12, SHEET 1, PG 49-50. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT EXTRUSION PN S2772660 Sep 1, 2010 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHLA201000114Rib · damagedREMOVE DAMAGED RIB IN RT FLAP WELL STA XW 90 AND REPAIR IAW APPROVED DATA PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 10-06-10, EVA D857-00357 REV IR DATED 09-01-10. REMOVED DAMAGED RIB & EXISTING REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED WEB Sep 1, 2010 · N804DH · Doug DC873F · Trailing Edge FlapsSDR DHLA201000109Skin · nickedRT OTBD FLAP UPPER SKIN NICK, STA XF 227.000 PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-04-10 EVA D857-00377 REV IR DATED 09-22-10. REMOVED DAMAGED PLATING AND EXISTING SPLICE IAW SRM 51-1-21, SRM 51-3-0. FABRICATED NEW PLATING SEGMENT (AL2024T3 0.071Sep 1, 2010 · N804DH · Doug DC873F · Trailing Edge FlapsSDR DHLA201000097Seat Track · wornUPPER CARGO COMPT.- NR3 TRACK LUGS WORN STA 1670.000 - 1702.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-3, FIG 12, SHEET 1, PG 49-50. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT EXTRUSION IAW SRM Sep 1, 2010 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHLA201000095Seat Track · wornUPPER CARGO COMPT.- NR 4 TRACK LUG WORN STA 57.000 - 110.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG. 12 SHEET 1 PG 49-50. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT EXTRUSION IAW SRM 53-2-3Sep 1, 2010 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHLA201000131Skin · corrodedFUS LWR SKIN CORRODED, STA 160.000 L-35R - L-36 PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7, SHEET 25,23,24 TR 53-203, DATED JAN 21-2008. REMOVED CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0, PG 2P. REMOVED EXISTING REPAIR NEAR CORROAug 31, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA201000118Skin · crackedRT INBD FLAP WELL.- WEB CRACKED 1" STA XF 75.000 PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 10-04-10, EVA D857-00375 REV IR DATED 09-21-10. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER REPAIR STRAP IAW DWG ES-D85700375-001-D REV IR DATED 9-21-10.Aug 31, 2010 · N804DH · Doug DC873F · Trailing Edge FlapsSDR DHLA201000110Skin · misrepairedPERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-11-10, EVA D85500374 REV IR DATED 09-28-10. REMOVED RUB PLATE IAW SRM 51-1-21. CUT OUT DAMAGED AREA + FABRICATED (3EA) FILLERS & INTERNAL REPAIR DOUBLER IAW DWG ES D85500374-001-D REV IR DATED 09-28-10. HEAT Aug 31, 2010 · N804DH · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHLA201000106Skin · crackedREMOVED & REPLACED EXISTING REPAIR ON LT WING T/E AT STA XW 47.000 UTILIZING APPROVED DATA. (REF REPAIR REPORT LW011) REMOVED EXISTING REPAIR AND CUT OUT DAMAGED AREA IAW SRM 57-2-3 PAR 5. FABRICATED DOUBLER (AL7075T6 0.020") IAW SRM 57-3-3 PG 36. BONDED DOUBLAug 31, 2010 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHLA201000103Skin · damagedREMOVED AND REPLACED EXISTING REPAIR LOCATED ON RT HORZ STABILIZER AT XE 159.000 UTILIZING APPROVED DATA (REF REPAIR REPORT HS002) PERFORMED MAJOR REPAIR IAW SRM 55-3-1, FIG 1, SHEET 1-2. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICAAug 31, 2010 · N804DH · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHLA201000093Skin · corrodedFUSELAGE LOWER SKIN CORRODED STA 160.000 L-35R-L-36. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG. 7 SHEET 25,23,24 TR 53-203 DATED. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED EXISTING REPAIR NEAR CORRODED AREA Aug 31, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA201000117Frame · wornNR 3 ENG LT T/R STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE AT STA YN 203.000 (BETWEEN 6 AND 9 O'CLOCK POS) PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR10502 DATED 10-08-10, EVA D878-00368 REV IR DATED 09-15-10. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAug 30, 2010 · N804DH · Doug DC873F · Engine Thrust ReverserSDR DHLA2010001416Skin · misrepairedR & R 3 EXISTING REPAIRS LOCATED ON AFT LOWER BELLY BETWEEN STA 1300-1370.000 LONGERON 36 UTILIZING APPROVED DATA. REF REPAIR REPORT F039, F040 & F041 PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-05-10, EVA D853-00370 REV IR DATED 09-15-10. REMOVED EXIAug 30, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA201000113Skin · delaminatedLT ELEVATOR GEARED TAB DELAMINATED. R & R LT ELEVATOR GEARED TAB IAW MM 27-30-3 PG 201-204. REFER TO NR 265752 FOR OPS CHECK.Aug 30, 2010 · N804DH · Doug DC873F · Elevator, Tab StructureSDR DHLA201000108Frame · wornNR 2 ENG LT THRUST REVERSER STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE AT STA YN 203.000 (BETWEEN 6 AND 9 O'CLOCK POS) PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 10486 DATED 09-29-10, EVA-D878-00372 REV IR DATED 09-16-10. CUT OUT DAMAGED AREA. FABRICATED Aug 30, 2010 · N804DH · Doug DC873F · Engine Thrust ReverserSDR DHLA201000104Frame · wornNR 3 ENG RT T/R STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE STA YN 202.000 (BETWEEN 5 AND 6 O'CLOCK POS). PERFORMED MAJOR REPAIR IAW FORM 8110-3 NR 10471 DATED 09-22-10, EVA D878-00371 REV IR DATED 09-15-10. CUT OUT DAMAGED AREA, FABRICATED FRAME SEGMENT IAAug 30, 2010 · N804DH · Doug DC873F · Engine Thrust ReverserSDR DHLA201000112Skin · delaminatedNR 3 LEFT SPOILER UPPER SKIN DELAMINATED R & R NR3 LT SPOILER IAW MM 27-61-1 PG 201-204. REFER TO NR 265753FOR, OPS CHECK.Aug 29, 2010 · N804DH · Doug DC873F · SpoilersSDR DHLA201000125Skin · dentedRT INBD FLAP UPPER PLATING DENTED STA XW 68. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DENTED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING (AL2024T3 0.025") & BONDED DOUBLER (AL2024T3 0.020") IAW SRM 57-7-1 FIG 1 ITEM "A" & "L"Aug 28, 2010 · N804DH · Doug DC873F · Trailing Edge FlapsSDR DHLA201000123Skin · misrepairedINSPECT EXISTING REPAIR ON RT FUSELAGE AT FS-2. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 1D, SHEET 3. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG. 1D SHEE T3, SRM 53-3-3 FIG. 1 ITEM "A" SRM 51-9-0 FIG. 68Aug 28, 2010 · N8004D · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA2010000122Skin · misrepairedINSPECT EXISTING REPAIR ON RT FUSELAGE STA FS - 17. PERFORMED MAJOR REPAIR IAW SRM 53-2-0, FIG 1 D, SHEET 3 REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21 FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG 1D, SHEET 3, SRM 53-3-3 FIG 1 ITEM "A", SRM 51-9-0 FIGAug 28, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA201000121Skin · misrepairedINSPECT EXISTING REPAIR ON FUS STA -156 FOR CONFORMITY WITH SRM, CONDITION AND SECURITY. IF REPAIR COMPLIES, NOTE DETAILS ON NON ROUTINE. IF REPAIR DOES NOT CONFORM, R & R UTILIZING APPROVED DATA. REF REPAIR REPORT (F011). STRIPPED REPAIR AREA IAW MM 51-20Aug 28, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR 2010F00223Skin · damagedINSPECT EXISTING REPAIR ON FUS STA -156 FOR CONFORMITY WITH SRM, CONDITION AND SECURITY. IF REPAIR COMPLIES, NOTE DETAILS ON NON ROUTINE. IF REPAIR DOES NOT CONFORM, R & R UTILIZING APPROVED DATA. REF REPAIR REPORT (F011). STRIPPED REPAIR AREA IAW MM 51-20-0 Aug 28, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA201000101Skin · dentedRT INBD FLAP UPPER PLATING DENTED STA XW 68 PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DENTED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING & BONDED DOUBLER IAW SRM 57-7-1 FIG 1, ITEM "A" & "L". BONDED BOTH PARTS WITH HYSOL IAW Aug 28, 2010 · N804DH · Doug DC873F · Trailing Edge FlapsSDR DHLA2010000100Skin · misrepairedREMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG. 1D SHEET 3, SRM 53-3-3 FIG. 1 ITEM "A" SRM 51-9-0 FIG 68A. CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR DOUBLER IAW SRM 53-Aug 28, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA201000094Skin · misrepairedPERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 1 D, SHEET 3 REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21 FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG 1D SHEET 3, SRM 53-3-3 FIG 1 ITEM "A", SRM 51-9-0 FIG 68 A CLEANED, TREATED AND PRIMED AREA & REPAIR DOUBLEAug 28, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA201000089Bulb · inoperativeCOCKPIT LIGHTING HAS ONE EMERGENCY EXIT LIGHT BULB INOP IN CEILING. ACFT WAS GROUNDED. R & R BULB ON COCKPIT CEILING LIGHTING IAW MM 33-22-0. OPS CK OK.Aug 28, 2010 · N806DH · Doug DC873F · Emergency LightingSDR IXXA100043OSensor · defectiveDURING TAKEOFF, THE MAX AIRSPEED WARNING LIGHT AND CLACKER CAME ON. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX REPLACED THE OVERSPEED LIMIT SENSOR. OPS CHECK GOOD IAW MM 34-11-0. ACFT WAS RETURNED TO SERVICE.Aug 26, 2010 · N602AL · Doug DC873F · Airspeed/Mach IndicatorSDR DHLA201000086Connector · shortedENGINE FIRE NR 4 COMPLETED ENGINE FIRE CHECK LIST. ENGINE WINDMILL 30 MIN IAW CREW VERBAL, OIL PRESSURE POSITIVE. AN EMERGENCY WAS DECLARED. ACFT WAS GROUNDED. T/S AND FOUND LT & RT CORE UPPER CONNECTOR HAS 1800 OHM SHORT TO GROUND R & R CONNECTORS (PN 8782Aug 18, 2010 · N873SJ · Doug DC873F · Fire Protection System WiringSDR DHLA201000071Battery Pack · inoperativeEMERGENCY LIGHT BATTERY DEAD. ACFT WAS GROUNDED. R & R EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-1, OPS CK GOOD.Aug 14, 2010 · N804DH · Doug DC873F · Emergency LightingSDR IXXA100039OIndicator · defectiveDURING CLIMB OUT, STANDBY ATTITUDE INDICATOR INOPERATIVE, THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED THE STANDBY ATTITUDE INDICATOR. OPS CHECK GOOD IAW MM34-28-0. ACFT WAS RETURNED TO SERVICE.Aug 12, 2010 · N602AL · Doug DC873F · Attitude and Direction Data SystemSDR DHLA201000067Pump · malfunctionedON LEVEL OFF AT 370, NR 3 ENG FAILED. NORMAL OIL PRESSURE, TEMP & FUEL PRESSURE, ENG N1 & N2 REMAINED ROTATING. PERFORMED ENG FAIL CHECKLIST & INFLT ENG START. ENG OPS RESTORED. R & R NASH PUMP IAW MM 73-10-6, GROUND CHECKS GOOD. ALSO MM 71-00 TROUBLESHOOTIAug 10, 2010 · N806DH · Doug DC873F · Fuel Boost PumpSDR DHLA201000068Rib · damagedON LANDING, NR8 MAIN TIRE BLEW CAUSING DAMAGE. ON POST FLIGHT INS FOUND RT WING RIB AT STA XW 90.000 DAMAGED. DEFECT RESOLUTION: REPAIRED RIB IAW EVA 085700356-001-D.Aug 8, 2010 · N804DH · Doug DC873F · Wing, Rib/BulkheadSDR IXXA100038OCompressor · bird ingestionDURING TAKEOFF, CREW EXPERIENCE A COMPRESSOR STALL ON RT SIDE. THEY ABORTED TAKEOFF AND RETURNED TO BLOCKS. MX INSPECTED BOTH NR (3) AND NR (4) ENGINE AND FOUND EVIDENCE OF A BIRD STRIKE ON NR (4) ENGINE. THEY PERFORMED BORESCOPE INSP, COMPLIED WITH CFM 56, FAug 3, 2010 · N603AL · Doug DC873F · Turbine Engine Compressor SectionSDR DHLA201000065Skin · corrodedFUSELAGE SKIN CORRODED AT FS 1281.0 AND 1260, LONGERON 36, BL 0. CUT OUT CORRODED AREAS OF SKIN THAT EXCEEDED DAMAGE LIMITATIONS. FABRICATED 2EA REPAIR FILLERS AND 1EA REPAIR DOUBLER AND INSTALLED IAW SRM 53-2-1, FIG 7, SHEETS 11, 13, 23 & 24. THIS IS A CLAJul 26, 2010 · N805DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA201000066Fire Detector · malfunctionedPROBLEM DESCRIPTION: NR 4 FIRE WARNING ILLUMINATED PERFORMED EMERGENCY PROCEDURES FIRED ONE BOTTLE. EMERGENCY WAS NOT DECLARED BY FLIGHT CREW. ACFT WAS GROUNDED. R & R THE RT FAN FIRE DETECTOR (PN 898463), NR 4 PYLON FIRE DETECTION WIRING (4W7004, 4W7005, 4WJul 23, 2010 · N873SJ · Doug DC873F · Fire DetectionSDR DHLA201000083Skin · corrodedNOSE SECTION LWR PLATING SHOWS CORROSION FS 12.000 L-36 PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 3,4,23,24. TR 53-203 DATED 01-21-08. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED AREA + FABRICATEJul 20, 2010 · N803DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA201000087Skin · corrodedSKIN CORRODED STA 520.000 L34R PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 07-16-10, EVA D853-00356 REV IR DATED 07-27-10. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED AREA AND FABRICATED REPAIR DOUJul 8, 2010 · N803DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA201000080Longeron Fitting · crackedLONGERON END FITTING BATHTUB FITTING CRACK 3.5" STA 902.125, L-4L PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1. REMOVED CRACKED BATHTUB FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BATHTUB FITTING IJul 8, 2010 · N803DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHLA201000079Longeron Fitting · crackedLONGERON END FITTING BATHTUB FITTING CRACK 2.5" STA 902.125, L-5L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1. REMOVED CRACKED BATHTUB FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BATHTUB FITTING Jul 8, 2010 · N803DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHLA201000076Skin · wornRIGHT INBD AILERON UPPER PLATING WORN STA XA 474.000 PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 1. REMOVED WORN PLATING IAW SRM 57-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 57-8-1 FIG. 1 ITEM "E". CLEANED, TREATED AND PRIMED AREA + NEWJul 8, 2010 · N803DH · Doug DC873F · AileronsSDR DHLA201000075Doubler · crackedNOSE SECTION ACCESS DOOR 2 INTERNAL DOUBLER CRACKED STA-156.0000. PERFORMED MAJOR REPAIR IAW EVA D853-00350, REV IR DATED 07-15-10. REMOVED EXISTING REPAIR IAW SRM 51-1-20D, SRM 51-1-21. VISUALLY INSPECTED REWORKED AREA. NO CRACK, NO CORROSION FOUND. FABRICATJul 8, 2010 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHLA201000072Splice · crackedFUS TAIL SECTION.- SPLICE FITTING CRACKED 1" STA 1766.00 L-17L PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED END FITTING IAW SRM 51-3-0 PG 1, SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW END FITTING IAW SRM 51-1-11Jul 8, 2010 · N803DH · Doug DC873F · Fuselage Main, StructureSDR DHLA201000084Splice · crackedAFT CARGO COMPT.- SPLICE FITTING CRACKED 6" (STA 1140.000 - 1160.000 L36) PERFORMED MAJOR REPAIR IAW JC EC-02172-001 W/O 9440. REMOVED SPLICE FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED, PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTINGJul 6, 2010 · N803DH · Doug DC873F · Fuselage Main, StructureSDR DHLA201000082Skin · corrodedLOWER FUSELAGE SKIN CORRODED STA 670.000 - 680.000, L36 - L35L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR10380 DATED 08-09-10, EVA D853-00355 REV IR DATED 07-19-10. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOJul 6, 2010 · N803DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA201000078Cargo Track · wornUPPER CARGO COMPT.- NR 6 TRACK LUGS WORN (STA 560.000 - 610.000) PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG 14, SHEET 1, PG 49-50. REMOVED EXISTING SPLICES AND CUT OUT TRACK DAMAGED SEGMENT IAW SRM 53-2-3 FIG. 14 SHEET 1, SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATEDJul 6, 2010 · N803DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHLA201000073Rib · crackedRIGHT INBD FLAP T/E RIB CRACKED 1", STA XW -5.000 REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOPHOLE AND FABRICATED REPAIR ANGLE (AL2024T3 0.071") IAW SRM 57-2-0 PG 9-10, SRM 57-5-2 FIG. 5 SHEET 1, SRM 51-9-0 FIG 68A. CLEANED, TREATED AND PRIMED AREA + REPAJul 6, 2010 · N803DH · Doug DC873F · Trailing Edge FlapsSDR DHLA201000081Skin · damagedRT OTBD FLAP UPPER SKIN HOLE ELONGATED AND WORN STA XF 203.000 - 213.000 PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4, TR 57-94 DATED 10-01-02. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING IAW SRM 57-7-1 FIG 4, TR 57-94 ITEM Jul 2, 2010 · N803DH · Doug DC873F · Trailing Edge FlapsSDR DHLA201000077Longeron · crackedLONGERON 24R CRACKED 1.5" STA FS 900.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG 5, SHEET 1, 13, 14, 15, 16, 25, 26, 27 TR 53-123 DATED 05-15-01. REMOVED FASTENERS IAW SRM 51-1-20D. PERFORMED STOP HOLE AND FABRICATED 2 REPAIR ANGLES, & 2 SHIMS IAW SRM 53-Jul 1, 2010 · N803DH · Doug DC873F · Fuselage Main, Longeron/Stringer
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