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 DHL2006804515Doubler · brokenFUSELAGE EXTERNAL POWER RECEPTACLE ACCESS DOOR INTERNAL DOUBLER BROKEN 3 INCHES STA -36.000 L-31.5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-3-3 FIG 1. REMOVED DAMAGED INTERNAL DOUBLER IAW SRM 53-1-0, SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW INTERJan 31, 2006 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2006804521Skin · crackedRIGHT RUDDER L/E PLATING CRACKED 0.75 INCH STA ZR 326.000 (MAJOR REPAIR) (DAMAGED). PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED DAMAGED PLATING IAW SRM 55-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 55-6-1 FIG 1 PG 2 ITEJan 31, 2006 · N804DH · Doug DC873F · Rudder, Plate/SkinSDR DHL2006804531Fitting · crackedAFT CARGO COMPT BILGE FITTING CRACKED 0.500 INCH AT STA 1180.000 L-35R. 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 (TJan 30, 2006 · N804DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2006804537Frame · corrodedAFT CARGO COMPT BILGE FORMER CORRODED STA 1180.000 L-35R. REMOVED FASTENERS IAW SRM 51-1-20D. REMOVED CORROSION FROM FORMER AT STA 1180.000 L-35R IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED SECTION AND FABRICATED FORJan 30, 2006 · N804DH · Doug DC873F · Fuselage Main, FrameSDR DHL2006804519Stiffener · crackedRIGHT HORIZONTAL STABILIZER STIFFENER CRACKED 1 INCH XFS 47.500. REMOVED CRACKED STIFFENER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED STIFFENER (AL7075"0" 0.063") IAW SRM 55-3-0 PG 8. HEAT TREATED FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TJan 29, 2006 · N804DH · Doug DC873F · Horizontal Stabilizer StructureSDR DHL2006804518Stiffener · crackedLT HORIZONTAL STABILIZER STIFFENER CRACKED 1 INCH XFS 47.500. REMOVED CRACKED STIFFENER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW STIFFENER (AL7075"0" 0.063") IAW SRM 55-3-0 PG 8. HEAT TREATED FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED TJan 29, 2006 · N804DH · Doug DC873F · Horizontal Stabilizer StructureSDR UPS06846111Fitting · crackedINSPECTION TYPE:C1 C-PIT STA 1240 L35R FWD FITTING JUST AFT OF TORQUE BOX IS CRACKED. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 51-1-20D AND DWG 3758495.Jan 27, 2006 · N852UP · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2006804512Bracket · crackedLEFT WING OUTBOARD SLOT MECHANISM NR 8 BRACKET CRACKED. REMOVED AND REPLACED BRACKET NR 8 FROM LT OUTBOARD SLOT MECHANISM IAW MM 20-16-0 PG 201-202, 207. REFER TO NR 044174 FOR OPS CHECK.Jan 26, 2006 · N804DH · Doug DC873F · Leading Edge DevicesSDR IXXA0600104OGyro · inoperativeDURING CLIMB OUT CAPTAINS EHSI FAILED. MULTIPLE FLAGS COMPUTER FLAGS HDG INT. CREW RETURNED AIRCRAFT TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED CAPT'S VG AND DG AND REPLACED WITH LTR-97 UNIT IAW APPLICABLE MM. THE OPERATIONAL CHECK GOOD AND Jan 25, 2006 · N604BX · Doug DC873F · Directional Gyro and Indicating SystemSDR DHL2006804508Angle · crackedITEM REF NR 044427: NR 1 LT T/R ANGLE CRACKED 1" STA YN 254.524 AT 12 O'CLOCK POS. REMOVED CRACKED ANGLE IAW SRM 51-1-21A. FABRICATED NEW ANGLE (TITANIUM AMS4911H0.020") IAW SRM 78-2-0. INSTALLED NEW ANGLE IAW SRM 51-1-21A.Jan 22, 2006 · N804DH · Doug DC873F · Engine Thrust ReverserSDR DHL2006804505Cargo Track · wornUPPER CARGO COMPT NR 2 TRACK LUG WORN, STA 1570.000 - STA 1610.000. CUT OUT DAMAGED TRACK SEGMENT IAW SRM 51-3-0 PG 1. FABRICATED SPLICES IAW SRM 53-2-3 FIG 14 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMJan 21, 2006 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06846009Autopilot Sys · malfunctionedNUMEROUS AUTOPILOT DISCONNECTS AFTER LEVEL OFF AND APPROACH. FD FLAG WAS INTERMITTENT AND EVENTUALLY BECAME VERY INTERMITTENT. SECURED FLT DIRECTOR AND AP. RVSM RESTRICTED. PER COMMENT ABOVE AND PERFORMED OPS CHECK FCC PER MM 2210-21-5 FCC OPS CHECK GOOD NJan 21, 2006 · N866UP · Doug DC873F · Autopilot SystemSDR IXXA06SMN052SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, EXTERNAL FUS FREON AFT + FWD LWR CORNER EXTERNAL IS NOT IAW SRM, STA 45.000 L-30L. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 13. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-20D, DC-8 SRM 51-3-0. REMOVED DAMAGED AREA IJan 19, 2006 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2006804506Floorbeam · maint errorMAIN CARGO COMPT FLOORBEAM HOLE MISDRILLED STA 620.000 LBL 10 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 1G, TR 53-124 DATED 09-30-01. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED REPAIR ANGLE AND PROTECTIVE STRAP IAW SRM 53-2-0 FIG 1G (SHEEJan 19, 2006 · N804DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2006804507Floorbeam · misdrilledITEM REF NR 043964: MAIN CARGO COMPT FLOORBEAM HOLE MISDRILLED STA 640.000 LBL 32.5" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 1G SHEET 1-2, TR NR 53-124 DATED 09-30-01. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED REPAIR ANGLE (EXTRUSION Jan 19, 2006 · N804DH · Doug DC873F · Fuselage Main, Floor BeamSDR IXXA06SMN053SSupport · crackedDURING ROUTINE C-CHECK INSPECTION, LT FLAP SUPPORT, STA 3.000 CRACKED 4. REMOVED AND REPLACED SUPPORT ASSY AT STA 3.000 (LT FLAP) IAW DC-8 SRM 51-1-21, DC-8 SRM 51-1-20D, DC-8 SRM 51-3-1, OPS CHECK.Jan 19, 2006 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA06SMN054SDrain Mast · pluggedDURING ROUTINE C-CHECK INSPECTION, INSTALLATION OF FWD LAV DRAIN MAST AT LWR CENTERLINE. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 ATI DWG H74-102 REV A, EO SEMAN 2006102 DATED 01-13-06. REMOVED EXISTING DRAIN MAST IAW DC8 SRM 51-3-0. FABRICATED REPAIR DOUJan 19, 2006 · N606AL · Doug DC873F · LavatoriesSDR UPS06846015Angle · crackedINSPECTION TYPE:C1 MAIN CARGO DOOR JAMB ANGLE STRUCTURE IS CRACKED AT AFT LWR CORNER. REMOVED DAMAGED ANGLE IAW SRM 51-1-21, FABRICATED AND INSTALLED MAIN CARGO DOOR JAMB ANGLE LWR CORNER IAW DC8 DWG 5772786, AND SRM 51-1-8, AND SRM 51-1-20DJan 18, 2006 · N852UP · Doug DC873F · Cargo/Baggage DoorsSDR DHL2006804502Skin · delaminatedLT WING NR 2 SPOILER UPPER SKIN DELAMINATED. REMOVED AND REPLACED NR 2 LT SPOILER PANEL IAW MM 27-61-1 PG 201-207. REFER TO NR 044174 FOR OPS CHECK.Jan 17, 2006 · N804DH · Doug DC873F · SpoilersSDR IXXA0500038OWarning System · activatedLANDING GEAR FAILED UPLATCH CHECK OUT OF KEWR. "GEAR NOT LATCHED" LIGHT STAYED ON. CREW RECYCLED GEAR AND LIGHT WENT OUT. LANDED IN KTOL WITHOUT INCIDENT. MAINTENANCE TRANSFERRED THIS TO DMI NR 33576 IN ACCORDANCE WITH DC8 MEL 32-16-0A CAT "A" WITH A NO FLJan 17, 2006 · N602AL · Doug DC873F · Landing Gear Position and WarningSDR IXXA06SMN035SSkin · dentedDURING ROUTINE CORRECTIVE ACTION, PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 2Q. REMOVED FASTENERS IAW DC8 SRM 51-1-21. TRIMMED OUT DAMAGED AREA. FABRICATED EXTERNAL REPAIR DOUBLER (AL 2024 T3 0.040) IAW DC-8 SRM 57-2-1 FIG 2Q, DC-8 SRM 57-7-1 FIG 4, TR Jan 16, 2006 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA06SMN047SSkin · crackedDURING C CHECK, EXT FUS D BELLY DOOR UPPER CORNER CRACKED ½ STA 1400.000 L.26. PERFORMED REPAIR IAW AD 2004-06-06, DOUG DWG SR 08530019, DWG 5750776, SB DC-8 53-078, DC-8 SRM 53-2-0. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. TRIMMED OUT DAMAGED AREA IAW DC-8Jan 16, 2006 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA06SMN043SFitting · crackedDURING ROUTINE C CHECK INSPECTION, LT MLG WW FITTING CRACKED STA 857.125 BETWEN L.23 AND L.24. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D. FABRICATED NEW FITTING IAW ATI REPAIR SPECIFICATION NR 2003-05, DWG DOUG NR 3646772. PERFORMED HEAT TREAMENT IAW DJan 16, 2006 · N606AL · Doug DC873F · Wing, Attach FittingsSDR IXXA06SMN037SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO MPT FITTING FRAME, BEAM CORRODED STA 1308.000 L21L. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTING IAW DC-8 SRM 51-1-20D. CLEANED, TJan 16, 2006 · N606AL · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2006804503Doubler · crackedRIGHT WING L/E UPPER PART ANGLE DOUBLER CRACKED XS 454.976. REMOVED CRACKED ANGLE DOUBLER IAW DC8 SRM 51-1-21. FABRICATED NEW ANGLE DOUBLER (AL 2024T3 0.063) IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE DOUBLER IAW Jan 16, 2006 · N804DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2006804504Skin · delaminatedLT WING NR 6 FLAP VANE LWR SKIN DELAMINATED. REMOVED AND REPLACED NR 6 LT FLAP VANE IAW MM 27-51-14 PG 201-202. REFER TO NR 044174 FOR OPS CHECK.Jan 16, 2006 · N804DH · Doug DC873F · Trailing Edge FlapsSDR DHL2006804501Frame · crackedRIGHT WING OUTBOARD L/E UPPER FORMER CRACKED 0.250" XFS 741.250. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED (2EA) ANGLE DOUBLER (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. PERFORMED STOP HOLE IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMJan 16, 2006 · N804DH · Doug DC873F · Leading Edge DevicesSDR IXXA06SMN046SBeam · crackedDURING ROUTINE C CHECK INSPECTION, NR 4 TRACK JOINT ANGLE WITH VERTICAL BEAM CRACKED 3, STA 1756.000 BL.0. REMOVED CRACKED JOINT ANGLE (FITTING) IAW DC-8 51-3-0. CLEANING, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW ANGLE (FITTING) IAW DC-8Jan 16, 2006 · N606AL · Doug DC873F · Fuselage Main, StructureSDR IXXA06SMN050SFrame · corrodedDURING C-CK, ALT CARGO MPT FRAME CORRODED STA 13.000 L.35R L.35 L.. PERFORMED REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT CORRODED FRAME SEGMENT. FABRICATED NEW FRAME SEGMENT, FABRICATED ANGLE & SPLICE IAW SRM. CLEANED, TRJan 16, 2006 · N606AL · Doug DC873F · Fuselage Main, FrameSDR IXXA06SMN049SSkin · crackedDURING C-CK, EXTERNAL FUS HEAT EXCHANGER CORNER WITH 03 CRACKS STA 14.000 STA 24.000 L27L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06018 DATE 01-17-06, SEMAN DWG NR ED 4155 DATE 01-11-06, EO SEMAN 2006040 DATE 01-17-06. REMOVED FASTENERS IAW DC-8 SRM 5Jan 16, 2006 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA06SMN045SSkin · dentedDURING ROUTINE C CHECK INSPECTION, RT WING OUTBOARD FLAP SKIN LWR PART DENTED 1 STA XF 390.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 3), TR NR 57-91 DATED 09-30-01. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED DAMAGED SECTION. FABRICATJan 16, 2006 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA06SMN042SSkin · damagedDURING ROUTINE C CHECK INSPECTION, RT IB FLAP UPPER SKIN HAS INTERN REPAIR XW 105.000. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 PAGE 1. REMOVED DAMAGED PLATING SEGMENT IAW SRM 57-1-0 PAGE 1, SRM 51-1-21. FABRICATED NEW PLATING SEGMENT (AL2024T3 0.040”) IAW SRM 5Jan 16, 2006 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA06SMN038SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIR CARGO MPT - NR 1 TRACK ATTACH FITTING CRACKED + FLOOR SUPPORT ANGLE CRACKED STA 1580.000 LBL.60. REMOVED CRACKED FITTING IAW SRM 51-3-0. FABRICATED NEW FITTING (ALCLAD 7075 T6 51) IAW ATI REPAIR SPECIFICATION NR 2005-0Jan 16, 2006 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR IXXA06SMN036SFloorbeam · corrodedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO MPT. ATTACH FITTING FRAME AND FLOOR BEAN CORRODED STA 640.000 L.216. REMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. CLEAN AND TJan 16, 2006 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR IXXA06SMN051SDoubler · wornDURING ROUTINE C-CHECK INSPECTION, NR 1 STUB WING DOUBLER LWR PART WORN STA XOLDO 67.750. PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG 1. REMOVED WORN DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED STOP DRILL. FABRICATED EXTERNAL REPAIR DOUBLER IAW SRM 57-2-1Jan 16, 2006 · N606AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN048SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, EXTERNAL FUSE HEAT EXCHANGER CORNER CRACKED STA 14.000 L27R. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED DAMAGED AREA IAW SEMAN DWG ED-4156. PERFORMED NDT INSPECTION IAW DC-8 NDT IAW DC-8 NDT SJan 16, 2006 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA06SMN044SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING UPPER SKIN SCRATCHED AND DENTED ON INBD FLAP BETWEEN XW 104.000 AND XW 122.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 PAGE 2. REMOVED DAMAGED PLATING IAW DC-8 SRM 57-1-0, DC-8 SRM 51-1-21. FABRICATED NEW PLATINJan 16, 2006 · N606AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN041SSkin · damagedDURING ROUTINE C-CHECK INSPECTION, RIGHT OUTBOARD FLAP UPPER SKIN HAS INTERN REPAIR XF 210.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 2Q. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED DAMAGED AREA. FABRICATED EXTERNAL REPAIR DOUBLER (AL2024T3 0.0Jan 16, 2006 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA06SMN040SSkin Panel · corrodedDURING ROUTINE C-CHECK INSPECTION, OUTBOARD OUTER L/E CORRODED XFS 710.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 38, TR 5785 DATED 11-22-00. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 57-2-1 FIG 2G. REMOVED Jan 16, 2006 · N606AL · Doug DC873F · Leading Edge DevicesSDR IXXA06SMN039SSkin · dentedDURING ROUTINE C-CHECK INSPECTION, RT OUTBOARD FLAP SKIN LWR PART DENTED AT SEVERAL SPOTS XF 345.000 - XF 404.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4, TR 57-94 DATED 10-01-02. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0, DC-8 SRM 51-1-21. FABRICJan 16, 2006 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA06SMN034SSkin · dentedDURING ROUTINE C-CHECK INSPECTION, DENT ON LWR SURFACE RT OUTBOARD FLAP STA XW 404.000 - 406.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 2), TR 57-91 DATED 09-30-01. REMOVED FASTENERS IAW DC8 SRM 51-1-21. REMOVED DAMAGED AREA. FABRICATED REJan 16, 2006 · N606AL · Doug DC873F · Trailing Edge FlapsSDR UPS06845978Skin · crackedINSPECTION TYPE:C1 LT WING I/B T/E POSSIBLE CRACK FROM TOP OF STOP DRILL. REMOVED PREVIOUS REPAIR DOUBLER. CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED 2 REPAIR DOUBLERS IAW SRM 51-1-21 ,51-3-0, 51-1-20D, 57-05-2 AND 57-02-0.Jan 12, 2006 · N852UP · Doug DC873F · Wing, Plate/SkinSDR DHL2006804500Support Angle · crackedRIGHT WING INBOARD L/E UPPER SUPPORT ANGLE CRACKED 2 INCHES, STA XFS 7.500. REMOVED CRACKED ANGLE IAW SRM 51-3-0. FABRICATED NEW ANGLE (AL7075T6 0.080") IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-3-0. Jan 11, 2006 · N804DH · Doug DC873F · Leading Edge DevicesSDR UPS06846017Angle · crackedINSPECTION TYPE:C1 ANGLE CRACKED AT STA 857 RBL 40 REMOVED CRACKED ANGLE IAW 51-1-20D, LOCATED AND DRILLED NEW ANGLE AND INSTALLED AT STA 857 RBL 40 IAW SRM 51-1-21 AND SRM 51-1-20D.Jan 11, 2006 · N852UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06845930Battery Pack · no testEMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER DC8 MM 33-50-00. OPS CK GOOD.Jan 10, 2006 · N880UP · Doug DC873F · Emergency LightingSDR UPS06846114Frame · crackedINSPECTION TYPE:C1 TAIL SEC 60 COMPT AFT PRESSURE BULKHEAD STA 1766 3RD "J" FRAME FROM BOTTOM HAS A 3" CRACK AT C/L. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 ANGLES, 4 CLIPS, 4 SHIMS AND WASHERS IAW SRM51-1-21,53-2-5 FIG 26, AND 51-1-20D.Jan 9, 2006 · N852UP · Doug DC873F · Fuselage Main, FrameSDR UPS06846105Spar · crackedINSPECTION TYPE:C1 3 POSSIBLE CRACKS ON FWD SIDE OF STA.680 BETWEEN FASTENERS COMMON LOWER SPAR AT RBL 13,18 AND 31. CUT OUT DAMAGED WEB. FABRICATED AND INSTALLED REPAIR DOUBLERS, FILLERS AND FINGER DOUBLER AT WEB STA. 680 IAW SRM 53-2-5 FIG 13, 51-1-21 AND Jan 9, 2006 · N852UP · Doug DC873F · Wing SparSDR UPS06845972Floor Support · corrodedINSPECTION TYPE:C1 CORROSION ON FLOORBOARD SUPPORT CHANNEL AT STA 852 LBL60, MAIN CARGO COMP. CUT OUT CORRODED AREA IAW SRM 51-1-8 AND 53-2-0 FIG 1F, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM 53-07-03, 53-02-00C, AND SRM 51-1-21 AND 51-1-20D.Jan 9, 2006 · N852UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846018Fitting · corrodedINSPECTION TYPE:C1 MAIN CARGO DOOR JAMB PLATE FITTING HAS HEAVY INTERGRANULAR CORROSION. REMOVED CORRODED FITTING IAW SRM 51-1-21 LOCATED AND DRILLED NEW FITTING AND INSTALLED AT MAIN CARGO DOOR JAMB IAW SRM 51-3-2, 51-1-21, AND SRM 51-3-0.Jan 8, 2006 · N852UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS06845977Attach Angle · crackedINSPECTION TYPE:C1 MAIN CARGO DOOR JAMB PLATE,THRESHOLD ATTACHED ANGLE CRACKED 1/4" AT FWD LATCH SPOOL. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ATTACH ANGLE IAW SRM 51-3-0 AND DWG NR 5772786. TVL # 7268745.Jan 8, 2006 · N852UP · Doug DC873F · Fuselage Main, Attach Fittings
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