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 DHL2004806548Longeron · crackedFUSELAGE TAIL SECTION L-17L, STA 1770.000 CRACKED 2.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5. REMOVED DETERIORATED SECTION IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAJan 12, 2004 · N806DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2004806549Longeron · crackedFUSELAGE TAIL SECTION L-17R, STA 1770.000 CRACKED 3.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5. REMOVED DETERIORATED LONGERON SECTION IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMEJan 12, 2004 · N806DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2004806559Cargo Track · wornUPPER CARGO COMPT NR 4 FLOOR TRACK LUGS WORN (STA 1680.000-1702.000). REMOVED NR 4 FLOOR TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK SEGMENT IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW SRM 53-2-3 PG 49-Jan 11, 2004 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806560Cargo Track · wornNR 4 FLOOR TRACK LUG WORN STA 990.000-930.000 (MAIN CARGO COMPT). TRIMMED OUT DETERIORATED TRACK SEGMENT IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED SPLICES (7075-T6AL 0.100) (7075-T6AL 0.125) (7075-T6AL 0.160) IAW Jan 10, 2004 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS04841832Splice · corrodedINSPECTION TYPE: C1, AFT PIT STA 1260-1280 LONG 36 SPLICE CORROSION CENTER OF SPLICE PLATE. REMOVED SPLICE PLATE IAW DC8 SRM 51-3-0 AND 51-1-20D. RECEIVED NEW FITTING SPLICE P/N 3759222-1N PO 0, LOCATED AND DRILLED IAW DC8 SRM 51-3-0 AND 51-1-20D. INSTALLEJan 10, 2004 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04841831Support Fitting · crackedINSPECTION TYPE: C1, AFT PIT STA 1140 L35L SUPPORT FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOCATED NEW FITTING AND DRILLED EXISTING FASTENER HOLES IAW DC8 SRM 51-3-2 AND 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D.Jan 10, 2004 · N814UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS04841830Longeron · corrodedINSPECTION TYPE: C1, AFT PIT STA 1540 L27L CORROSION ON UNDERSIDE OF FLANGE. REMOVED FITTING IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW DC8 SRM 51-1-8. CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED NEW FITTING AND DRILLED EXISTING HOLES Jan 10, 2004 · N814UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS04841829Web · corrodedINSPECTION TYPE: C1, STA 900 RT CUSP AREA WEB HAS SIGNS OF CORROSION. FOUND FINGER DOUBLER & WEB OUT OF LIMITS; CORROSION ON FLOORBEAM FS 879 FOUND DURING CORROSION REMOVAL. CUTOUT -3 WEB; REMOVED CORROSION ON FLOORBEAM (IN LIMITS); DYE PEN PANEL (NO CRACKS)Jan 10, 2004 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04841828Frame · corrodedINSPECTION TYPE:C1 RIGHT WHEEL WELL AFT OTBD SIDE CANTED FRAME HAS SEVERAL AREAS OF CORROSION. REMOVED -3 FRAME WHICH WAS CORRODED BEYOND LIMITS IAW DC8 SRM 53-2-0. FABBED NEW CANTED FRAME CLIP, SPLICE AND DOUBLER IAW REO G09664 AND DAC DWG 5646444. ALODINEJan 10, 2004 · N814UP · Doug DC873F · Fuselage Main, FrameSDR DHL2004806545Skin · crackedAFT SERVICE DOOR JAMB WITH 1.000 INCH CRACK IN UPPER FWD CORNER, STA 1620.000 L-11R TO L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 17 SHEET 3, DWG SRO8530021, DWG 5750776, TR 53-184. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGEJan 10, 2004 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004806536Fitting · crackedFWD CARGO COMPT FITTING PAD CRACKED 1.000, L-28L, STA 300.000. REMOVED CRACKED FITTING PAD IAW SRM 51-3-0 PG 1-2. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0 PG 1-2.Jan 9, 2004 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2004806539Fitting · crackedMAIN CARGO COMPT CUSP EXTRUSION AFT FITTING CRACKED 2.000, STA 1177.000, L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1 IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. Jan 9, 2004 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS04841703Bleed Valve · inoperativeNR 2 AND NR 3 ENGINES AT IDLE DUE TO COMPRESSOR STALLS ENG NR3 FOUND CRACKS GURNS & MISSING MATERIAL ON STATOR OF LPT ACCESS THRU 517. BOROSCOPE 72-00-00 P 620, 72-31-00 72-54. ENGINE NR 2 COMPLIED WITH VISUAL & BOROSCOPE INSPECTION OF NR 2 ENG POST STALL, Jan 9, 2004 · N813UP · Doug DC873F · Compressor Bleed ValveSDR IXXA0400006OWarning Light · illuminatedWHEN LANDING GEAR WAS EXTENDED THE ANTI-SKID INOP LIGHT AND LAO AND LAI LIGHTS ILLUMINATED. LAO AND LAI LIGHT REMAINED ILLUMINATED IN MANUAL ON THE SKID MONITOR PANEL. RECYCLED MAIN LANDING GEAR, ANTI-SKID CONTROL SWITCH AND RESET CIRCUIT BREAKER, NO HELP. CREJan 9, 2004 · N606AL · Doug DC873F · Brake Anti-Skid SectionSDR UPS04841701Warning Light · illuminatedFIRE WARNING ILLUMINATED ON PIT 34. ON DESCENT APPROX 5 MINS AFTER SELECTING TAIL DEICE THE LOWER CARGO FIRE LIGHT ILLUMINATED SECURED TAIL DEICE AND ACCOMPLISHED EMERGENCY CHECKLIST. RAN TAIL DEICE SYS AFTER SEVERAL MINS HAD LOWER CARGO IRE LIGHT ON F/O PAJan 9, 2004 · N804UP · Doug DC873F · Fire DetectionSDR UPS04841827Seat Track · crackedINSPECTION TYPE: C1, SEAT TRACK CRACKED AT STA 145. BLENDED CRACKED SEAT TRACK IAW DC8 SRM 53-2-3, OUT OF LIMITS IAW DC8 SRM 53-2-3 AND 53-2-0. REMOVED DAMAGED SEAT TRACK IAW DC8 SRM 51-3-0 & 51- 3-1. LOCATED, DRILLED NEW SEAT TRACK AND SPLICE IAW DC8 SRM 5Jan 8, 2004 · N814UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806530Angle · crackedRIGHT MLG W/W CEILING ANGLE WITH 0.500 CRACK IN IT, STA 865.000 RBL 46. REMOVED DAMAGED CEILING ANGLE IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW ANGLE (7075-T6AL 0.071) IAW SRM 53-2-0 PG 1-2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTAJan 8, 2004 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04841700Slide · dislodgedEVACUATION SLIDE ON MAIN ENTRY DOOR FELL OUT OF THE CASE O/B CLIP. OK TO CONTINUE IN SERVICE IAW MEL 57-7-4.Jan 8, 2004 · N810UP · Doug DC873F · Escape SlideSDR DHL2004801001Door · lack of lubeMAIN CABIN DOOR WAS VERY DIFFICULT TO OPEN. LUBRICATED MAIN CABIN DOOR IAW DC-8 M/M 52-11-1. OPERATES NORMAL AT THIS TIME.Jan 8, 2004 · N801DH · Doug DC873F · Passenger/Crew DoorsSDR UPS04841826Shear Tie · crackedINSPECTION TYPE: C1, UPPER CARGO BETWEEN STA 1000-1020 AT LONG 13L SHEAR TIE IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. FABRICATED NEW SHEAR TIE IAW DC8 SRM 53-4-1 FIG 51 AND 51-1-24. HEAT TREAT TO 7075-T6 .080 IAW TPS 1003 REV A. ALODINJan 7, 2004 · N814UP · Doug DC873F · Fuselage Main, StructureSDR DHL2004806531Skin · crackedRIGHT INNER WING OUTBOARD EXTENDED L/E SLOT SKIN CRACKED 4.000 AT STA XILD 42.000. REMOVED CRACKED SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (7075-T6AL 0.071) IAW SRM 57-3-3 PG 11. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFACE IAW SRM Jan 7, 2004 · N806DH · Doug DC873F · Leading Edge DevicesSDR DHL2004806529Cargo Track · wornUPPER CARGO COMPT NR 5 FLOOR TRACK LUGS WORN (STA 1680.000 - 1702.000). CUT OUT NR 5 FLOOR TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. FABRICATED 3 EA SPLICES (7075T6AL 0.100) (7075T6AL 0.125) (7075T6AL 0.160) IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREJan 7, 2004 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806542Cargo Track · wornUPPER CARGO COMPT NR 2 FLOOR TRACK LUGS WORN (STA 1590.000-1610.000). TRIMMED NR 2 FLOOR TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. FABRICATED 3 EA SPLICES (7075-T6AL 0.100) (7075T6AL 0.125) (7075-T6AL 0.160) IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED ANJan 7, 2004 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806535Skin · crackedFUSELAGE NOSE SECTION EXTERIOR SKIN CRACKED 0.250 AT STA 53.000 L-30L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 13. REMOVED EXISTING REPAIR IAW SRM 51-1-20D PG 21. TRIMMED OUT CRACKED AREA IAW SRM 53-2-0 FIG 13. FABRICATED FILLER (2024T3AL Jan 7, 2004 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004806523Rib · crackedRIGHT STUB WING FORMER CRACK 0.250, STA XFS 535.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.040) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B PG 16, 17. INSTALLED AJan 7, 2004 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2004806524Frame · crackedRIGHT STUB WING FORMER CRACK 0.250, STA XFS 548.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (ALCLAD 2024T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B PG 16, 17. INSTALLED ANGJan 7, 2004 · N806DH · Doug DC873F · Wing SparSDR UPS04841825Door Frame · crackedINSPECTION TYPE: C1, R2 DOOR UPPER AFT DOOR JAMB CORNER HAS CRACKED INTERNAL DOUBLER AND L1 1R, FOUND BY RADIOGRAPHY. FAB DOUBLERS & FILLERS -19, -21, -23, & -25 IAW DC8 SRM 53-2-0. TRIMMED EXTERIOR SKIN AND INTERNAL DOUBLER IAW DC8 SRM 53-2-0 TR 130. REMOJan 6, 2004 · N814UP · Doug DC873F · Fuselage Main, StructureSDR UPS04841824Angle · corrodedINSPECTION TYPE: C1, SHEARED RIVET HEAD, BULGE & CORRODED SHEAR WEB ABOVE & BELOW L21R CUSP MAIN CABIN COURIER AREA FS 25. REMOVED FRAME FITTING AND FLOOR SUPPORTS TO FOM, REMOVED CUSP ANGLES AND FABRICATED NEW ANGLE IAW DC8 SRM 53-3-3 AND DAC DWG 5888479. AJan 6, 2004 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04841823Doubler · misrepairedINSPECTION TYPE: C1, L1 DOOR UPPER FWD CORNER REPAIR IS NOT PER SRM. REMOVED EXISTING DOUBLERS ABOVE L1 DOOR UPPER FWD CORNER IAW DC8 SRM 51-1-21. FABBED -15 & -17 DOUBLERS IAW DC8 SRM 53-2-0 FIG 15, TR 53-182. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLJan 6, 2004 · N814UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004806534Cargo Track · wornUPPER CARGO COMPT NR 2 FLOOR TRACK LUGS WORN (STA 1550.000-1590.000). REMOVED DAMAGED SEGMENT OF FLOOR TRACK NR 2 (STA 1550.000-1590.000) IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK SEGMENT IAW SRM 51-1-8B. INSTALLED NEW TRACK SEJan 6, 2004 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806528Cargo Track · wornUPPER CARGO COMPT NR 3 FLOOR TRACK LUGS WORN (STA 1680.000-1702.000). CUT OUT NR 3 FLOOR TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. FABRICATED 3 EA SPLICES (7075T6AL 0.100) (7075T6AL 0.125) (7075T6AL 0.160) IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATJan 6, 2004 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806513Cargo Track · wornMAIN CARGO COMPT NR 1 FLOOR TRACK LUG WORN AT STA 270.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED CHANNEL AND PLUG IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1.Jan 6, 2004 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806516Cargo Track · wornMAIN CARGO COMPT NR 4 FLOOR TRACK LUG WORN STA 390.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED PLUG AND CHANNEL IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1.Jan 6, 2004 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806538Cargo Track · wornMAIN CARGO COMPT NR 7 FLOOR TRACK LUG WORN, STA 210.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED CHANNEL AND PLUG IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1.Jan 6, 2004 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806527Skin · dentedLEFT WING OUTBOARD FLAP T/E DENTED AT STA XF 391.000. REMOVED DENTED T/E IAW SRM 51-1-21 PG 1. FABRICATED NEW T/E (6061T6AL 0.032) IAW SRM 57-1-0 PG 1, SRM 57-7-1 PG 2. CLEANED, TREATED AND PRIMED INTERNAL AREA IAW SRM 51-1-8B. INSTALLED NEW T/E WITH NEW FJan 6, 2004 · N806DH · Doug DC873F · Trailing Edge FlapsSDR DHL2004806526Frame · crackedRT OUTER WING OUTBOARD L/E FORMER 0.250 INCH CRACK, STA XFS 785.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGJan 6, 2004 · N806DH · Doug DC873F · Wing SparSDR DHL2004806525Frame · crackedRIGHT INNER WING CTR L/E FORMER 1.000 INCH CRACK, STA XFS 385.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED REINFORCING ANGLE (2024T3 0.040) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED RJan 6, 2004 · N806DH · Doug DC873F · Wing SparSDR DHL2004806533Angle · crackedRT WING STUB WING SUPPORT ANGLE CRACKED 2.000 AT STA XILD 42.000. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW SUPPORT ANGLE AL7075-T6 0.063 IAW SRM 57-2-0 PG 1-2. CLEANED, TREATED AND PRIMED AREA AND SUPPORT ANGLE IAWJan 6, 2004 · N806DH · Doug DC873F · Leading Edge DevicesSDR UPS04841822Skin · nickedINSPECTION TYPE: C1, LEFT WING L/E HAS NICKS AT XFS114. REMOVED DAMAGED AREA IAW REO G09663, FABBED NEW DOUBLER FILLER IAW REO G09663, ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED FASTENERS IAW DC8 SRM 51-1-27.Jan 5, 2004 · N814UP · Doug DC873F · Wing, Plate/SkinSDR DHL2004806521Rib · crackedRIGHT OUTER WING L/E FORMER CRACK 0.500, STA XFS 660.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B Jan 5, 2004 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2004806515Cargo Track · wornUPPER CARGO COMPT NR 7 FLOOR TRACK LUG WORN, STA 190.000. CUT OUT DAMAGED SECTION OF NR 7 FLOOR TRACK IAW SRM 53-2-3 PG 17. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED CHANNEL AND PLUGS IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1.Jan 5, 2004 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS04841821Fitting · corrodedINSPECTION TYPE: C1, RIGHT MLG WW L24R AT STA 879 VERT BATHTUB FITTING HAS CORROSION ON FWD SIDE. REMOVED CORROSION & FOUND TO BE BEYOND ALLOWABLE LIMITS IAW DC8 SRM 53 -2-0 FIG 1F. REMOVED FITTING, FABRICATED REPAIR SPLICES AND INSTALLED NEW FITTING AND SPLJan 4, 2004 · N814UP · Doug DC873F · Fuselage, Landing Gear Attach FittingsSDR UPS04841820Fitting · gougedINSPECTION TYPE: C1, FWD PIT CROSS-SLIDE DOOR T-BOLT FITTINGS GOUGED 6 EACH. BLENDED OUT LATCH FITTING IAW DC8 SRM 51-1-8 OUT OF LIMITS IAW DAC DWG 3754051. RECEIVED, LOCATED, & DRILLED 6 EACH LATCH FITTINGS IAW DC8 SRM 51-1-24 AND 51-3-2. ALODINED & PRIMEJan 4, 2004 · N814UP · Doug DC873F · Cargo/Baggage DoorsSDR DHL2004806517Rib · crackedRIGHT OUTER WING OUTBOARD L/E FORMER CRACKED 0.250 AT STA XFS 791.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (2024T3 AL 0.032) IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER Jan 4, 2004 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2004806520Rib · crackedRIGHT WING STUB WING FORMER CRACKED 2.000 AT STA XFS 272.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER AND AREAJan 4, 2004 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2004806510Seat Track · damagedFLIGHT COMPT F/E AFT SEAT TRACK WITH ELONGATED HOLES. REMOVED F/E AFT SEAT TRACK WITH ELONGATED HOLES IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK ASSY IAW SRM 51-3-0 PG 1.Jan 4, 2004 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806522Frame · crackedRIGHT OUTER WING OUTBOARD L/E FORMER CRACK 0.250, STA XFS 785.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANJan 4, 2004 · N806DH · Doug DC873F · Wing SparSDR DHL2004806519Rib · crackedLEFT WING STUB WING FORMER UPPER INTERNAL PART CRACKED 0.500 AT STA XRS 537.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED DOUBLER (2024-T3AL 0.032) IAW SRM 53-2-0 PG 2E. CLEANED, TREATED AND PRIMED IAW SRM 51-1Jan 3, 2004 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2004873001Trim Motor · malfunctionedAFTER ROTATION AIRCRAFT RAPIDLY PITCHED UP TO 20 DEG ACTUATING THE STICK SHAKER. CREW PUSHED FULL UP ON CONTROL WHEEL TO FORWARD STOP. F/O ACTIVATED TRIM FROM 5.3 TO ZERO. RETURNED TO NORMAL CLIMB ATTITUDE. TRIM WAS 10 TO 2 DEG FOR CRUISE, 4.0 FOR APPROACHJan 2, 2004 · N873SJ · Doug DC873F · Stabilizer ActuatorSDR UPS04841710Fitting · crackedINSPECTION TYPE: C3, STATION 1228 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D.Dec 31, 2003 · N702UP · Doug DC873F · Fuselage Main, Attach Fittings
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