Douglas DC-8-72

Service difficulty reports · 201

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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 = 'DC872'
  ORDER BY difficulty_date DESC"

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SDR IXXA06SMN055SPlate · unknownFWD LAVATORY DRAIN MAST BLANKING PLATE AT 460 BL O REPLACES 53-DC8-928. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 09-21-05, AT SKETCH FO3-RO5 REV. B DATED 09-21-05, EO SEMAN 2006112 DATE 01-05-06. REMOVED (02 EA) EXISTING DRAIN MAST IAW DC-8 SRM 51-3-0Jan 26, 2006 · N722CX · Doug DC872 · Aircraft StructuresSDR IXXA06SMN056SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, RT WING NR 4 WING DOUBLER LWR SKIN CRACKED .25 INCH, XS 520.222. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1A FIG 1 PAGE 3. REMOVED CRACKED DOUBLER IAW DC8 SRM 51-1-20D. STOP DRILLED CRACK. FABRICATED EXTERNAL REPAIR DOUBLEJan 26, 2006 · N722CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA06SMN028SAileron · corrodedDURING ROUTINE C-CHECK INSPECTION, RT WING INBOARD AILERON WITH CORROSION AND NON STANDARD REPAIR IN LOWER PLATING AT STA XA 550.00. PERFORMED MAJOR REPAIR. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED EXISTING PANEL PLATING (CORRODED) + REPAIR NON STANDJan 12, 2006 · N722CX · Doug DC872 · AileronsSDR IXXA06SMN033SSkin · corrodedDURING C CHECK INSPECT, RT WING INBD FLAP UPPER SKIN CORRODED AT STA XW 1.00. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 1. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PG 16. REMOVED CORRODED PANEL PLATING IAW DJan 12, 2006 · N722CX · Doug DC872 · Trailing Edge FlapsSDR IXXA06SMN032SSkin · corrodedDURING C CHECK INSPECTION, LT RUDDER EXTERNAL SKIN CORRODED, STA ZR 257.906. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-6-1. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 55-2-0 PG 12. REMOVED CORRODED PLATING IAW DC8 SRM 55-1-0Jan 12, 2006 · N722CX · Doug DC872 · Rudder, Plate/SkinSDR IXXA06SMN031SFloorbeam · corrodedDURING C CHECK, MAIN CARGO COMPT FLOORBEAM UPPER FLANGE CORRODED AT STA 1548.000 BL 0. PERFORMED MAJOR REPAIR IAW DC8 SRM 51-2-1 FIG 1 (SHEET 8), TR NR 51-130 DATED 01-26-04. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 53-Jan 12, 2006 · N722CX · Doug DC872 · Fuselage Main, Floor BeamSDR IXXA06SMN030SSkin · corrodedDURING C CHECK INSPECTION, LT OTBD FLAP, T/E INTERNAL PART LWR SKIN CORRODED XF 415.000 XF 435.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4, TR NR 57-94 DATE 10-01-02. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57Jan 12, 2006 · N722CX · Doug DC872 · Trailing Edge FlapsSDR IXXA06SMN015SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT INTERNAL SKIN CORRODED BETWEEN STA 570.000 AND STA 580.000, L-29R - L-26R. REMOVED CORROSION FROM FWD CARGO COMPT INTERNAL SKIN (SAT 570.000, 580.000, L-29R TO L-29R TO L-26R) IAW DC-8 SRM 51-1-8 PAGES 17-18 Jan 5, 2006 · N722CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA06SMN007SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, RT RUDDER EXTERNAL SKIN CORRODED, STA ZR 319.063. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-6-1 FIG 1. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 55-2-0 PAGE 12. REMOVED CORRODED PANEJan 5, 2006 · N722CX · Doug DC872 · Rudder, Plate/SkinSDR IXXA06SMN026SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, RT RUDDER EXTERNAL SKIN CORRODED, STA ZR 276.531. PERFORMED MAJOR REPAIR. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 55-2-0 PAGE 12. REMOVED CORRODED PANEL PLATING IAW DC-8 SRM 55-Jan 5, 2006 · N722CX · Doug DC872 · Rudder, Plate/SkinSDR IXXA06SMN024SFitting · corrodedDURING ROUTINE C-CHECK INSPECTION, FWD ACCY COMPT FITTING CORRODED AT STA 270.000, L-29 (RT). REMOVED CORROSION ON FITTING 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 51-1-21. CLEAJan 5, 2006 · N722CX · Doug DC872 · Fuselage Miscellaneous StructureSDR IXXA06SMN021SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT STRUCTURE UNDER CROSS-SLIDE DOOR -B- HAS CRACKED FITTING STA 540.000 BETWEEN L-26L AND L-27L. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED Jan 5, 2006 · N722CX · Doug DC872 · Fuselage Miscellaneous StructureSDR IXXA06SMN013SLongeron · crackedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT L-34L CRACKED BETWEEN STA 600.000 AND STA 620.000. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED LONGERON SEGMENT. FABRICATED SPLICES (02 EA) (EXTRUSION BAR 7075 T6 51) FABRICATED NEW LONGERON SEGMENT Jan 5, 2006 · N722CX · Doug DC872 · Fuselage Main, Longeron/StringerSDR IXXA06SMN027SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT CARGO COMPT SPLICE FITTING CRACKED 1 1/2" BS 1180.000 - 1200.000, L-36). REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51-1-20D. CLEANED, TREATED, PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW DC8 SRM Jan 5, 2006 · N722CX · Doug DC872 · Fuselage Main, Attach FittingsSDR IXXA06SMN022SSkin · crackedDURING C CHECK, RT WING OTBD L/E LWR PART SKIN CRACKED ½, XFS 710.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06014 DATED 01-11-06, SEMAN DWG ED-4144 DATED 01-06-06, EO SEMAN NR 20051569 DATED 01-11-06. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 5Jan 5, 2006 · N722CX · Doug DC872 · Leading Edge DevicesSDR IXXA06SMN018SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, RT VERT STAB SKIN CORRODED, AT STA ZR 101.856. REMOVED LEVEL 1 CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. MEASURED: THICKNESS 0.025, BLEND OUT 0.002, REMAINING MATERIAL 0.023 FOUND WITHIN ALLOWABLE LIMITS IAW DC-8 SRM 55-2-Jan 5, 2006 · N722CX · Doug DC872 · Vertical Stabilizer, Plate/SkinSDR IXXA06SMN017SFloorbeam · corrodedDURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPT - FLOORBEAM UPPER FLANGE CORRODED; STA 1500.000 RBL 42 - RBL 50. PERFORMED MAJOR REPAIR IAW DC8 SRM 51-2-1 FIG 1 (SHEET 9), TR 51-130 DATED 01-26-04. REMOVED FASTENERS IAW DC8 SRM 51-1-21. REMOVED DAMAGED SJan 5, 2006 · N722CX · Doug DC872 · Fuselage Main, Floor BeamSDR IXXA06SMN016SFloorbeam · corrodedDURING C CHECK INSPECT, AFT CARGO COMPT BEAM FLOOR WEB CORRODED , STA 1440.000 RBL 45. PERFORMED MAJOR REPAIR IAW DC8 SRM 51-2-1 FIG 1 (SHEET 2, 12), TR 51-130 DATED 01-26-04. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG Jan 5, 2006 · N722CX · Doug DC872 · Fuselage Main, Floor BeamSDR IXXA06SMN014SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT L-33L CRACKED, STA 600.000 - STA 620.000. REMOVED CORROSION FROM FWD CARGO COMPT INTERNAL SKIN (SAT 570.000 – 580.000, L-29R TO L-29R TO L-26R) IAW DC-8 SRM 51-1-8 PAGES 17-18 (MATERIAL THICKNESS: 0.063”, BLEJan 5, 2006 · N722CX · Doug DC872 · Fuselage Main, Longeron/StringerSDR IXXA06SMN012SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, RT WING CTR L/E LWR EXTERNAL SKIN CORRODED AT STA XFS 435.789. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06007 DATED 01-06-06, SEMAN DWG ED-4142 DATED 01-04-06, ED SEMAN 2005 1554 DATED 01-06-06. REMOVED CORROSION IAW DC8 Jan 5, 2006 · N722CX · Doug DC872 · Wing, Plate/SkinSDR IXXA06SMN011SSkin · crackedDURING C-CHECK INSPECTION, LT WING - UPPER SKIN CRACKED .5 INCH, AT STA XRS 110.000, S-16. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06006 DATED 01-05-06, SEMAN DWG ED-4141 DATED 01-03-06, EO SEMAN 20051523 DATED 01-05-06. REMOVED FASTENERS. CUT OUT DAMAGEJan 5, 2006 · N722CX · Doug DC872 · Wing, Plate/SkinSDR IXXA06SMN010SRepair · misinstalledDURING C CHECK INSPECT, EXTERNAL FUSELAGE LT AFT HEAT EXCHANGER RT LWR CORNER HAS NON STANDARD REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05582 DATED 12-23-05 SEMAN DWG NR ED-4131 DATED 12-20-05, ED SEMAN NR 2005 1436 DATED 12-23-05. REMOVED NON STJan 5, 2006 · N722CX · Doug DC872 · Aircraft StructuresSDR IXXA06SMN009SLongeron · corrodedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT - L-36 CORRODED AT STA 286.000. REMOVED LEVEL I CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18 MEASURED: THICKNESS: 0.120, BLEND OUT: 0.003, REMAINING THICKNESS: 0.117. FOUND WITHIN ALLOWABLE LIMITS IAW DC-8 SRM Jan 5, 2006 · N722CX · Doug DC872 · Fuselage Main, Longeron/StringerSDR IXXA06SMN002SFitting · corrodedDURING ROUTINE C-CHECK INSPECTION, NR 3 ENGINE - RAIL FITTING CORRODED, YN 278.000 AT 12 O'CLOCK POSITION (LT SIDE). REMOVED AND REPLACED NR 3 ENGINE LT TRANSLATING COWL IAW CFM 56 MM 78-31-20 PAR 3A-3B, PG 402, 422. REFER TO JC SVC-7003-7104 FOR OPS CHECK.Jan 5, 2006 · N722CX · Doug DC872 · Engine Thrust ReverserSDR IXXA06SMN001SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, LT OUTBD FLAP T/E UPPER SURFACE HAS NO STANDARD REPAIR, STA XF 403.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4, TR 57-94 DATE 10-01-02. REMOVED PANEL PLATING WITH NON STANDARD REPAIR IAW DC8 SRM 57-1-0, DC8 SRM 51-Jan 5, 2006 · N722CX · Doug DC872 · Trailing Edge FlapsSDR IXXA06SMN008SSkin · crackedDURING ROUTINE C CHECK INSPECTION, NR 12 ACCESS DOOR EXTERNAL SKIN CRACKED 1/2". PERFORMED MAJOR REPAIR IAW DC-8 SRM 52-8-2 FIG 1 (SHEET 1), BOEING MESSAGE NR 1-151096062-2 DATED 01-12-06. REMOVED DAMAGED SKIN IAW DC-8 SRM 52-1-0 PAGE 1, DC-8 SRM 51-1-21. FJan 5, 2006 · N722CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA06SMN006SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RT RUDDER EXTERNAL SKIN CORRODED, STA ZR 110.750. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-6-1 FIG 1. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 57-2-0 PAGE 12. REMOVED CORRODED PANEJan 5, 2006 · N722CX · Doug DC872 · Rudder, Plate/SkinSDR IXXA06SMN003SFitting · corrodedDURING ROUTINE C-CHECK INSPECTION, NR 3 ENGINE - RAIL FITTING CORRODED AT 12 O' CLOCK POSITION, YN 278.000 (RT SIDE). REMOVED LEVEL I CORROSION FROM RAIL FITTING IAW DC-8 SRM 51-1-8 PAGES 17-18 (MATERIAL THICKNESS: 0.130, BLEND OUT: 0.005, REMAINING THICKNESSJan 5, 2006 · N722CX · Doug DC872 · Engine Thrust ReverserSDR IXXA06SMN025SVane · damagedDURING C-CK, LT WING OTBD FLAP VANE HOLES ELONGATED , XOLDI 6.224. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05587 DATED 12-29-05 SEMAN DWG NR ED-4122 DATED 12-28-05, ED SEMAN NR 2005 1453. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-Jan 5, 2006 · N722CX · Doug DC872 · Trailing Edge FlapsSDR IXXA06SMN023SSkin · dentedDURING ROUTINE C CHECK INSPECTION, ON RIGHT OUTBOARD FLAP, A SMALL DENT WAS FOUND ON UPPER SKIN AT STA XF 217, DUE TIME CHANGE. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4, TR 57-94, EO SEMAN 20051460 DATED 12-16-05. REMOVED DAMAGED PLATING IAW DC8 SRM Jan 5, 2006 · N722CX · Doug DC872 · Trailing Edge FlapsSDR IXXA06SMN019SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, LT OUTBD AIL LWR SKIN CORRODED, STA XA 726.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-8-1 FIG 4. REMOVED CORROSION FROM LT OTBD AIL LWR SKIN, STA 726.000 IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 57Jan 5, 2006 · N722CX · Doug DC872 · AileronsSDR IXXA06SMN005SSkin · crackedDURING ROUTINE C CHECK INSPECTION, RT OTBD FLAP PANEL UPPER SKIN CRACKED 1", AT STA XF 415.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-5 FIG 1 (SHEET 1-2). REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW DC-8 SRM 57-2-5 FIG 1. FAB`D NJan 5, 2006 · N722CX · Doug DC872 · Trailing Edge FlapsSDR IXXA06SMN004SSkin · dentedDURING ROUTINE C CHECK INSPECTION, RT OUTBD FLAP PANEL LWR SKIN DENTED, AT STA XF 420.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG 2Q. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW DC-8 SRM 57-2-1 FIG 2Q. FABRICATED EXTERNAL REJan 5, 2006 · N722CX · Doug DC872 · Trailing Edge FlapsSDR IXXA05SMN321SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, MAIN CARGO COMPT FITTING CRACKED 3, AT STA 1530.000, L-26R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING WITH HI-LOKS IAW DC-8 SRM 51-1-20D, DC-Dec 29, 2005 · N722CX · Doug DC872 · Fuselage Miscellaneous StructureSDR IXXA05SMN305SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION, RT WING - T/E LWR SKIN NON STANDARD REPAIR, XW 762.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-0 FIG 2A (SHEET 1), TR 57-84 DATED 08-01-00. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW DC-8Dec 29, 2005 · N722CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05SMN314SRepair · improperDURING ROUTINE C-CHECK INSPECTION, RT WING L/E HAS NON STANDARD REPAIR, XFS 761.695. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, 06014 DATED 01-1-06, SEMAN DWG ED-4135 DATED 01-06-06, ED SEMAN 2005 1472 DATED 01-11-06. REMOVED NON STANDARD REPAIR IAW DC8 SRDec 29, 2005 · N722CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05SMN307SLongeron · crackedDURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPT L-36 CRACKED 1.5 (STA 1180.000-1190.000). PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CRACKED LONGERON SEGMENT IAW DC-8 SRM 53-2-2- FIG 13 (SHEET 3, 4). FABRICATED NEW LONGERON SEGMENT P/N S2753715 EDec 29, 2005 · N722CX · Doug DC872 · Fuselage Main, Longeron/StringerSDR IXXA05SMN303SDoor Frame · crackedDURING ROUTINE C-CHECK INSPECTION, MAIN CARGO DOOR FRAME FORMER CRACKED 2, STA 470.000 L-21L. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 1B (SHEET 3). REMOVED FASTENERS IAW DC8 SRM 51-1-20D. PERFORMED STOP HOLE. FABRICATED ANGLE DOUBLER (7075 O 0.125) IDec 29, 2005 · N722CX · Doug DC872 · Fuselage Main, StructureSDR IXXA05SMN322SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT FITTING CRACKED 3, AT STA 1530.000, L-24R. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FITTING WITH FASTENERS (HI-LOKS) IAW DC8 SRM 51-1Dec 29, 2005 · N722CX · Doug DC872 · Fuselage Main, Attach FittingsSDR IXXA05SMN318SSkin · crackedDURING ROUTINE C CHECK, RT WING OTBD INNER L/E CRACKED .500 XFS 710.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06007 DATED 01-06-06, SEMAN DWG ED-4139 DATED 01-04-06, EO SEMAN NR 20051476 DATED 01-06-06. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRMDec 29, 2005 · N722CX · Doug DC872 · Leading Edge DevicesSDR IXXA05SMN317SVane · damagedDURING ROUTINE C CHECK INSPECTION, RT WING L/E SLOT VANE HOLE ELONGATED, XILD 42. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06007 DATED 01-06-06, SEMAN DWG ED-4138 DATED 01-06-06, EO SEMAN NR 20051475 DATED 01-06-06. REMOVED EXISTING REPAIR DOUBLER IAW DDec 29, 2005 · N722CX · Doug DC872 · Leading Edge DevicesSDR IXXA05SMN306SFitting · crackedDURING C CHECK, MAIN CARGO COMPT FRAME FITTING 3 CRACK, STA 980.000 L-17R TO L-18R. PERFORMED REPAIR IAW DC8 SRM 53-2-0 FIG 7. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED FRAME FITTING SEGMENT (CRACKED) IAW DC8 SRM 53-2-0 FIG 7.. FAB`D SPLICE ANGLE, FIDec 29, 2005 · N722CX · Doug DC872 · Fuselage Main, Attach FittingsSDR IXXA05SMN320SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, MAIN CARGO CMPT - WING CENTER SECTION FITTING CRACKED 3, AT STA 822.500, L-22R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D. FABRICATED NEW FITTING IAW ATI REPAIR SPECIFICATION 2003-05, DOUGLAS DWG 4753360. PERFORMED NDTDec 29, 2005 · N722CX · Doug DC872 · Fuselage Main, Attach FittingsSDR IXXA05SMN319SRepair · corrodedDURING ROUTINE C-CHECK INSPECTION, RIGHT RUDDER REPAIR DOUBLER EDGES CORRODED, STA ZR 61.156. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-6-1 FIG 1, EO SEMAN 20051480 DATED 12-20-05. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SEMANDec 29, 2005 · N722CX · Doug DC872 · Rudder, Plate/SkinSDR IXXA05SMN316SVane · damagedDURING C-CHECK, RT WING - L/E SLOT VANE HOLE ELONGATED, XOLDI 6.225. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 05587 DATED 12-29-05, SEMAN DWG ED-4137 DATED 12-28-05, ED SEMAN 2005 1474 DATED 12-29-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC-8 SRM 51-3-0.Dec 29, 2005 · N722CX · Doug DC872 · Leading Edge DevicesSDR IXXA05SMN315SRepair · misinstalledDURING C-CHECK, RT WING - L/E SLOT VANE HAS NON STANDARD REPAIR, XOLDO 66. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 05586 DATED 12-28-05, SEMAN DWG ED-4136 DATED 12-23-05, ED SEMAN 2005 1473 DATED 12-28-05. REMOVED NON STANDARD REPAIR. REMOVED DAMAGED SECDec 29, 2005 · N722CX · Doug DC872 · Leading Edge DevicesSDR IXXA05SMN313SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, RIGHT WING - INBOARD L/E LWR PART HAS NON STANDARD REPAIR, XFS 63.750. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06006 DATED 01-05-06, SEMAN DWG ED-4133 DATED 02-06-06, ED SEMAN 2005 1470 DATED 01-05-06. REMOVED EXISTING NDec 29, 2005 · N722CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05SMN312SRepair · misinstalledDURING ROUTINE C-CHECK, RT WING - CTR L/E LWR PART HAS NON STANDARD REPAIR, XFS 304.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06006 DATED 01-05-06, SEMAN DWG ED-4134 DATED 01-04-06, ED SEMAN 2005 1471 DATED 01-05-06. REMOVED NON STANDARD REPAIR IAW DC8Dec 29, 2005 · N722CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05SMN311SFitting · corrodedDURING ROUTINE C-CHECK INSPECTION, NR 4 ENGINE - LEFT T/R RAIL FITTING CORRODED AT 12 O`CLOCK POSITION (THRUST REVERSER). REMOVED LEVEL I CORROSION FROM RAIL FITTING IAW DC-8 SRM 51-1-8 PAGES 17-18 (MATERIAL THICKNESS: 0.133, BLEND OUT: 0.003, REMAINING THICKDec 29, 2005 · N722CX · Doug DC872 · Engine Thrust ReverserSDR IXXA05SMN310SFitting · corrodedDURING ROUTINE C-CHECK INSPECTION, NR 4 ENGINE RIGHT T/R RAIL FITTING CORRODED AT 12 O`CLOCK POSITION (THRUST REVERSER). REMOVED LEVEL I CORROSION FROM RAIL FITTING IAW DC-8 SRM 51-1-8 PAGES 17-18 (MATERIAL THICKNESS: 0.133, BLEND OUT: 0.003, REMAINING THICKNDec 29, 2005 · N722CX · Doug DC872 · Engine Thrust Reverser
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