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 UPS06847093Frame · crackedINSPECTION TYPE:C1 D-PIT STA 1340 BETWEEN L30R-31R FRAME CRACKED AND CORRODED. CUT OUT DAMAGED AREA STA 1340 FRAME BETWEEN L30R-L31R IAW 51-1-21D, FABRICATED AND INSTALLED REPAIR SPLICES AND FRAME SEGMENT AT STA 1340 BETWEEN L30R-L31R IAW SRM 53-02-00 FIG 2, May 13, 2006 · N818UP · Doug DC873F · Fuselage Main, FrameSDR UPS06847064Fitting · crackedINSPECTION TYPE:C1 CRACK IN FITTING AT LT AFT OVERWING DOOR JAMB, UPPER AFT CORNER STA 824 L14L. REMOVED FITTING AT STA 824 L14L IAW SRM 51-3-0, AND 51-1-20D FABRICATED AND INSTALLED FITTING AT STA 824 L14R IAW DWG 4751643, AND SRM 51-3-2, AND SRM 51-1-20D.May 13, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846987Fitting · crackedINSPECTION TYPE:C1 3EA FITTINGS IN C-PIT DOOR TORQUE BOX CRACKED AT STA 1180-1200. REMOVED 3EA CRACKED TORQUE BOX FITTINGS IAW SRM 51-1-20D, INSTALLED NEW 3EA FITTINGS AT STA 1180-1200 C-PIT TORQUE BOX IAW SRM 51-1-24, 51-1-20D.May 13, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846981Longeron · crackedINSPECTION TYPE:C1 60 HOLE LONGERON 17L HAS PREVIOUS REPAIR, HOWEVER CRACK HAS EXTENDED PAST STOP DRILL. REMOVED DAMAGED L17L AT STA 1776 IAW SRM 51-1-21. FABRICATED AND INSTALLED LONGERON 17L AT STA 1766 IAW SRM 53-02-02-0, 51-3-02, AND SRM 51-1-20D.May 13, 2006 · N818UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847127Cusp Web · corrodedRT FWD TYPE 1 DOOR LWR DOOR JAMB CUSP IS CORRODED. REMOVED CUSP AT STA 370-470 L21R IAW SRM 53-2-5 FIG 15, MILLED AND INSTALLED REPAIR CUSP AT STA 370 - 470 L21R IAW SRM 53-2-5 FIG 15.May 12, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06847011Seat Track · corrodedINSPECTION TYPE:C1 MAIN CABIN SEAT TRACK HEAVY CORROSION AT STA 70 LBL 24. REMOVED DAMAGED SEAT TRACK FROM STA 45-130 LBL 24 IAW SRM 51-03-00, FABRICATED AND INSTALLED SEAT TRACK SPLICE FROM STA 45-130 IAW SRM 53-02-03-0 FIG 014, SRM 51-3-0, AND DWG S-2440463May 12, 2006 · N818UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06847125Fitting · crackedLEFT W/W TRAP FITTING CRACKED ALONG STA 902 FWD SIDE AT TOP VERTICAL BOLT THRU L24L. REMOVED AND REPLACED LEFT WHEEL WELL TRAP FITTING IAW SRM 51-1-20D, SRM 51-3-2, AND DC-8 AMM 51-03-01-0.May 11, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06847118Fitting · crackedFOUND A/C COMPT RT SIDE L33R END FITTING CRACKED AT FS 8.00. REMOVED AND REPLACED END FITTING ON LONGERON END FITTING L33R IAW SRM 51-1-21, 51-01-27 AND 51-1-8.May 11, 2006 · N818UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847096Cusp Web · crackedINSPECTION TYPE:C1 A-PIT LEFT STA 325 LWR CUSP HAS VISIBLE CRACK IN RADIUS. CUT OUT SECTION OF CUSP AT STA 325 - 275 L21L IAW SRM 53-02-05-0. FABRICATED AND INSTALLED 2 EA REPAIR ANGLES, -15 & -9 FRAME SPLICE DRILLED UP LEFT CUSP AND INSTALLED IAW SRM 53-04-May 11, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06847043Spar Cap · crackedINSPECTION TYPE:C1 WING CTR LOWER SPAR CAP CRACKED, LEFT W/W LBL 9-19 AND LBL 37-44. STOP DRILLED CRACKS AT WING LWR CTR SPAR CAP LBL 9-19 AND LBL 37-44. FABRICATED AND INSTALLED REPAIR PARTS AT WING CTR SPAR CAP LBL 9-19 AND LBL 37-44 IAW SRO8570009 REV A CMay 11, 2006 · N818UP · Doug DC873F · Wing SparSDR UPS06846909Light · inoperativeINSPECTION TYPE:N/A ON SHUTDOWN EMERGENCY EXIT LIGHTS DISARM CHECK FAIL TO GIVE PROPER INDICATION. LIGHT SHOULD ILLUMINATE. RELAMPED, OPS CHECKS GOOD.May 11, 2006 · N805UP · Doug DC873F · Emergency LightingSDR DHL2006873504Cargo Track · wornUPPER CARGO COMPT NR 2 TRACK LUG WORN (STA 1570.000 - 1610.000). CUT OUT NR 2 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. FABRICATED SPLICES (AL7075T6 0.100"/ 0.125"/0.160") IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51May 11, 2006 · N873SJ · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006873503Structure · crackedRIGHT WING OUTBOARD L/E OUTER SECTION FORMER 0.250 INCH CRACK STA XFS 822.500. PERFORMED STOP HOLE AND FABRICATED 2EA ANGLE DOUBLER (AL7075T6 0.025") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLEMay 11, 2006 · N873SJ · Doug DC873F · Wing Miscellaneous StructureSDR UPS06847126Cusp Web · corrodedFUS CUSP CORRODED AT FS 1310 AND 1340 RT FWD AND AFT SIDES OF T-1 DOOR. REMOVED CUSP AT STA 1310-1380 RT FUSELAGE IAW 51-1-21, AND SRM 51-3-0, MILLED AND INSTALLED CUSP SPLICE REPAIR AT STA 1310-1380 IAW SRM 52-2-0 FIG 15.May 10, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846986Fitting · crackedINSPECTION TYPE:C1 FRAME FITTING CRACKED AT FS 832, RT SIDE 19 INCHES ABOVE FLOOR PLANE. REMOVED FITTING AT STA 832 IAW SRM 51-1-20D, FABRICATED AND INSTALLED FRAME FITTING AT FS 832 IAW SRM 51-1-20D, AND DWG 3779874.May 10, 2006 · N818UP · Doug DC873F · Fuselage Main, FrameSDR UPS06846984Attach Fitting · crackedINSPECTION TYPE:C1 FRAME ATTACH FITTING CRACKED AT STA 1180 L17R. REMOVED CRACKED FITTING AT FRAME STA 1180 L17R IAW SRM 51-1-20D, DRILLED REPLACEMENT FITTING AND INSTALLED AT STA 1180 L17R IAW SRM 51-1-20D.May 10, 2006 · N818UP · Doug DC873F · Fuselage Main, FrameSDR UPS06846983Fitting · crackedINSPECTION TYPE:C1 FITTING CRACKED AT STA 670 L11R. REMOVED CRACKED FITTING AT STA 670 L11R IAW SRM 51-3-0, FABRICATED AND INSTALLED FITTING AT STA 670 L11R IAW DWG 5750540, SRM 51-3-2 AND SRM 51-1-20D.May 10, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846952Fitting · crackedINSPECTION TYPE:C1 LONGERON/FRAME TIE FITTING CRACKED AT FS 860 19" ABOVE FLOOR PLANK RT SIDE. REMOVED FRAME TIE FITTING AT FS 860 IAW SRM 51-1-20D. FABRICATED AND INSTALLED FRAME FITTING AT FS 860 IAW DWG 4750422, AND SRM 51-1-20D, AND SRM 51-1-8.May 10, 2006 · N818UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS06846951Fitting · crackedINSPECTION TYPE:C1 LONGERON TO FRAME FITTING CRACKED AT FS 855 19" ABOVE FLOOR PLANK RT SIDE. REMOVED CRACKED FITTING AT FS 855 IAW SRM 51-1-20D. FABRICATED AND INSTALLED FITTING AT FS 855 19" ABOVE FLOOR PLANK IAW DWG 3779498 AND SRM 51-1-20D, AND SRM 51-1-May 10, 2006 · N818UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS06846936Fitting · crackedINSPECTION TYPE:C1 LONGERON/FRAME TIE FITTING CRACKED AT FS 860 (RT SIDE 17" ABOVE FLOOR PANEL). REMOVED, FAB`D AND REPLACED LONGERON FITTING IAW SRM 51-1-21 AND 51-1-20D.May 10, 2006 · N818UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS06846865Fitting · crackedINSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 670 L6L. REMOVED END FITTING AT STA 670 L6L IAW SRM 51-1-20D, DRILLED UP AND INSTALLED END FITTING AT STA 670 L6L IAW SRM 51-03-02, AND SRM 51-1-20D.May 10, 2006 · N818UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2006873502Structure · crackedLEFT WING CTR L/E LWR FORMER 1 INCH CRACK STA XFS 341.500. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLERS (2EA) OF AL7075T6 0.032" IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERMay 10, 2006 · N873SJ · Doug DC873F · Wing Miscellaneous StructureSDR DHL2006873501Angle · crackedRIGHT WING CTR L/E LWR REINFORCING ANGLE CRACK STA XFS 341.500. PERFORMED STOP HOLE IAW SRM 57-2-0 PG 9-10. FABRICATED 2EA ANGLE DOUBLERS (AL7075T6 0.040") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLMay 10, 2006 · N873SJ · Doug DC873F · Wing Miscellaneous StructureSDR DHL2006873500Support Angle · crackedLEFT WING CTR L/E INTERIOR UPPER SUPPORT ANGLE 1 INCH CRACK STA XOLDI 6.225. REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (AL7075T6 0.063") IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANMay 9, 2006 · N873SJ · Doug DC873F · Wing Miscellaneous StructureSDR IXXA060180OEngine · fluctuatesIN FLIGHT NOTICED SLIGHT RUMBLE, NR 3 ENG N1 BEGAN TO FLUCUATE. ENG BEGAN TO ROLL BACK, ENG OIL PRESSURE LIGHT CAME ON. ENG SHUTDOWN, OIL PRESSURE WENT TO NEAR ZERO PSI. INSPECTED ENG INLET & EXHAUST, SPECIFIC GRAVITY, CHECKED MAGNETIC CHIP DETECTORS, FUEL May 9, 2006 · N604BX · Doug DC873F · Engine (Turbine/Turboprop)SDR UPS06846866Door Frame · crackedINSPECTION TYPE:C1 HFEC AND VISUAL INSP DETECTED A .250 INCH CRACK ON THE D-PIT UPPER FWD DOOR JAMB CORNER. CUT OUT DAMAGED AREA ON C-PIT UPPER FWD DOOR JAMB CORNER IAW SRM 53-02-00 FIG 021, FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER AT THE C-PIT UPMay 8, 2006 · N818UP · Doug DC873F · Fuselage Main, StructureSDR UPS06846787Fan · malfunctionedSMOKY ODOR NOTICED AT TOP OF DESCENT. SMOKE APPEARED WHEN DESCENDING THROUGH 18000'. AFTER FUMES EVACUATION PROCEDURE SMOKE DISSIPATED. SMELL RECURRED AT ABOUT 5000'. COCKPIT AND GALLEY AREA SMELL OF SMOKE AFTER SHUTDOWN. DEFERRED M324868. REMOVED AND REMay 4, 2006 · N880UP · Doug DC873F · Air Distribution FanSDR UPS06846778Lamp · inoperativeFOUND ENTRY DOOR LIGHT INOP. RELAMPED OPS CK NORMAL REF MM 33-31-01-2.May 2, 2006 · N866UP · Doug DC873F · Emergency LightingSDR UPS06846757A/C Pack · odorA BURN SMELL WAS NOTED IN THE COCKPIT APPROXIMATELY ONE HOUR AFTER LEVEL OFF. THE SMELL WENT AWAY IN APPROX 2 MINUTES. A SEARCH OF CABIN AT COURIER AREA FOUND NO OBVIOUS PROBLEMS. INSPECTED ALL ACCESSIBLE FLT DECK COMPT'S FOR ANY VISUAL DAMAGE OR ODORS. ADApr 25, 2006 · N852UP · Doug DC873F · Cabin Cooling SystemSDR UPS06846753Smoke Goggles · scratchedF/O'S SMOKE GOGGLES SCRATCHED AND FOGGY. REPLACED CAPTAIN'S SMOKE GOGGLES PER 25-60-05-2.Apr 25, 2006 · N805UP · Doug DC873F · Emergency EquipmentSDR UPS06846766Doubler · crackedINSPECTION TYPE:C1 EXTERIOR OF TAILSKID FAIRING JUST FWD OF DOUBLER HAS RIPPED FASTENER HOLE AND AFT EDGE IS GOUGED. REMOVED DOUBLER IAW SRM 53-2-0 FIG 1F. FABRICATED AND INSTALLED REPAIR DOUBLER,AND FILLER AT STA 1766 L34L TO L34R IAW SRM 53-02-01 FIG 7, 51Apr 23, 2006 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846985Skin · dentedINSPECTION TYPE:C1 COMPLY WITH MPI 17970 REGARDING PERM REPAIR TO DENT AFT OF LWR FWD PIT DOOR OPENING IAW ATTACHED WAN 1096454 AND MPI SUMMARY REPORT PAGE 1. REPAIRED DENT ON SKIN AFT SIDE OF -A- PIT DOOR CORNER IAW SAA EA 008-5320-01-A0189, DOUGLAS DWG 975Apr 21, 2006 · N818UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS06846728Transmitter · leakingON CLIMB-OUT OF BALTIMORE, APPROX 2 MIN INTO FLIGHT IT WAS NOTICED THAT THE HYD QTY APPROX 2 "MARKS" BELOW "AUX" RAN QRH FOR LOSS OF HYD FLUID/QTY, FOLLOWED ABNORMAL PROCEDURES, LANDED NORMALLY IN SDF. HYDRAULIC RESERVOIR SIGHT GOUGE SHOWS RESERVOIR FULL, INDApr 21, 2006 · N867UP · Doug DC873F · Hydraulic System, MainSDR DHL2006806001Bulb · inoperativeEMERGENCY LIGHTS DISARMED LIGHTS DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS SWITCH IS IN DISARMED PLACING SAI BATTERY SWITCH TO ARM ILLUMINATES EMERGENCY LIGHTS DISARMED LIGHTS. RELAMPED DISARMED LIGHT AND TESTED AS PER MM 33-50-0. ALL INDICATIONS NORApr 21, 2006 · N806DH · Doug DC873F · Emergency LightingSDR UPS06846756Intercostal · crackedFOUND CRACKED INTERCOSTAL AT FS 520 BELOW L31R. REMOVED CRACKED INTERCOSTAL AT FS 520 BELOW L31R IAW SRM 51-1-21. FABRICATED, DRILLED, REAMED AND INSTALLED INTERCOSTAL AT FS 520 L31R IAW DWG 51616520, SRM 51-3-2,51-01-08, AND SRM 51-01-20D-0.Apr 20, 2006 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846723Light · inoperativeEMERGENCY LIGHTING FAILED MX TEST. RESECURED GROUNDING WIRE/LUG,OPS CKS NORMAL IAW AMM 33-50-01-2.Apr 20, 2006 · N813UP · Doug DC873F · Emergency LightingSDR DHL2006801553Repair · unknownINSPECT REPAIR AT RT FWD FS 60.000 STR 28R FOR COMPLIANCE WITH CURRENT SRM. PERFORMED REPAIR IAW FAA FORM 8110-3 DATED 04-06-06, EO NR AST060320 DATED 03-24-06. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND NDT INApr 18, 2006 · N801DH · Doug DC873F · Standard Practices/StructuresSDR DHL2006801552Fitting · crackedFOUND UPPER CARGO COMPT FITTING 0.500" CRACK STA 702.875 L-13R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORApr 18, 2006 · N801DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2006801547Frame · misdrilledUPPER CARGO COMPT FRAME RIVETING EDGE DISTANCE ON LINING SPACER AT STA 742.250 L-20R NOT IN ACCORDANCE WITH SRM (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04/08/06, EO NR AST060314 DATED 03-20-06. REMOVED LINING SUPPORT SPACER IAW SRM 5Apr 17, 2006 · N801DH · Doug DC873F · Fuselage Main, FrameSDR DHL2006801550Frame · misdrilledUPPER CARGO COMPT FRAME INNER FLANGE MISDRILLED HOLE STA 280.000 L-15R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-22-06, EO# AST060303 DATED 03-16-06. REMOVED FASTENERS IAW SRM 51-1-21. VISUALLY INSPECTED AREA. NO CRACK OR CORROSIONApr 17, 2006 · N801DH · Doug DC873F · Fuselage Main, FrameSDR DHL2006801549Pressure Panel · corrodedLT MLG W/W HORIZONTAL PRESSURE PANEL CORRODED, STA 902.000 LBL 53" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-20-06, EO NR AST060305 DATED 03-16-06. REMOVED CORROSION FROM HORIZ PRESS PANEL IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMIApr 17, 2006 · N801DH · Doug DC873F · Fuselage Main, StructureSDR DHL2006801551Fitting · crackedNR 1 ALT TANK FITTING CRACK 2.500" STA 408.000 S-59. PERFORMED MAJOR REPAIR IAW SRM 57-1-0. REMOVED CRACKED FITTING IAW SRM 51-1-21A. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-12 PG 7-21. INSTALLEDApr 16, 2006 · N801DH · Doug DC873F · Wing, Attach FittingsSDR DHL2006801545Structure · damagedPERFORM PREVENTATIVE MODIFICATION TO THE AFT UPPER L1 DOOR CORNER IAW AD2000-20-08, SB 53-075, DRAWING SR 085300021. DOCUMENT REPAIR IN AIRCRAFT LOGBOOK AND ON 337 FORM. PERFORMED MAJOR REPAIR IAW AD2000-20-08 S/B 53-075, DOUGLAS DWG SR085300021. REMOVED FAApr 14, 2006 · N801DH · Doug DC873F · Passenger/Crew DoorsSDR DHL2006801546Frame · misdrilledMAIN CARGO COMPT FRAME RIVETING EDGE DISTANCE OF LINING SPACER AT STA 822.500 L-16.7R NOT IAW SRM. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-06-06, EO# AST060328 DATED 03-20-06. REMOVED LINING SUPPORT SPACER IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT Apr 14, 2006 · N801DH · Doug DC873F · Fuselage Main, FrameSDR DHL2006801548Skin · corrodedEXT SKIN CORRODED, STA 1420.000 - 1450.000 L-32R TO L-34R. PERFORMED MAJ REPAIR IAW SRM 53-4-1 FIG 17C SHEET 2, DACO DWG 5779936. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 FIG 1F SHEET 3. REMOVED EXISTING REPAIR DOUBLER Apr 14, 2006 · N801DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2006801543Frame · misdrilledMAIN CARGO COMPT FRAME RIVETING EDGE DISTANCE OF LINING SPACER AT STA 879.000 L-18L NOT IN ACCORDANCE WITH SRM (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-04-06, EO NR AST060321 DATED 03-20-06. REMOVED LINING SUPPORT SPACER AND CLIP IApr 13, 2006 · N801DH · Doug DC873F · Fuselage Main, FrameSDR DHL2006801533Frame · damagedMAIN CARGO COMPT FRAME RIVETING EDGE DISTANCE OF LINING SPACER AT STA 857.000 L-18R NOT IN ACCORDANCE WITH SRM (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-06-06, EO AST060325 DATED 03-20-06. REMOVED LINING SUPPORT SPACER AND CLIP IAW Apr 12, 2006 · N801DH · Doug DC873F · Fuselage Main, FrameSDR DHL2006801534Frame · misdrilledMAIN CARGO COMPT FRAME RIVETING EDGE DISTANCE OF LINING SPACER AT STA 879.375 L-13R NOT IN ACCORDANCE WITH SRM AND 1 MISDRILLED HOLE. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-04-06, EO NR AST060327 DATED 03-20-06. REMOVED LINING SUPPORT SPACER ANDApr 12, 2006 · N801DH · Doug DC873F · Fuselage Main, FrameSDR DHL2006801539Frame · damagedMAIN CARGO COMPT FRAME RIVETING EDGE DISTANCE OF LINING SPACER AT STA 940.000 L-18R NOT IN ACCORDANCE WITH SRM. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-04-06, EO NR AST060323 DATED 03-20-06. REMOVED LINING SUPPORT SPACER AND CLIP IAW SRM 51-1-21,Apr 12, 2006 · N801DH · Doug DC873F · Fuselage Main, FrameSDR DHL2006801538Frame · damagedMAIN CARGO COMPT FRAME RIVETING EDGE DISTANCE OF LINING SPACER AT STA 920.000 L-18L NOT IN ACCORDANCE WITH SRM. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-04-06, EO NR AST060322 DATED 03-20-06. REMOVED LINING SUPPORT SPACER AND CLIP IAW SRM 51-1-21,Apr 12, 2006 · N801DH · Doug DC873F · Fuselage Main, Frame
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