Douglas DC-8-72

Service difficulty reports · 201

Newest first. General aviation reporting is voluntary.

Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IXXA05SMN290SFitting · corrodedDURING ROUTINE C-CHECK INSPECTION, FWD ACCY COMPT INTERNAL PART FITTING CORRODED AT STA 270.000, L-34 (RT). REMOVED CORROSION FROM 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 CRACKED FITTING IAW DC-8 SRMDec 29, 2005 · N722CX · Doug DC872 · Fuselage Main, Attach FittingsSDR IXXA05SMN304SSkin · dentedDURING ROUTINE C-CHECK INSPECTION, EXTERNAL FUS FWD CARGO COMPT AFT CARGO DOOR SKIN WITH (06EA) DENTS. 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 SECTDec 29, 2005 · N722CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05SMN293SSkin · damagedDURING ROUTINE C-CHECK INSPECTION, RT OB FLAP HAS A NON STANDARD REPAIR ON UPPER SKIN, STA XF 210.000PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4, TR NR 57-94, EO SEMAN NR 20051460 DATED 12-16-05. REMOVED DAMAGED PLATING IAW SRM 57-1-0, SRM 51-1-21. FABRICATED Dec 29, 2005 · N722CX · Doug DC872 · Trailing Edge FlapsSDR IXXA05SMN289SFitting · corrodedDURING ROUTINE C-CHECK INSPECTION, FWD ACCY COMPT INTERNAL PART FITTING CORRODED AT STA 270.000, L-30 (RT)REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2A. REMOVED CORRODED FITTING IAW SRM 51-1-21. CLEANED, Dec 29, 2005 · N722CX · Doug DC872 · Fuselage Miscellaneous StructureSDR IXXA05SMN309SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE.- CRACKED 3, L-17L STA 1617.000. PERFORMED MAJOR REPAIR IAW SRM 53-5-2 FIG. 5. REMOVED CRACKED L-17L IAW SRM 53-1-0, SRM 51-1-20D. FABRICATED NEW LONGERON (EXTRUSION P/N S1616757) IAW SRM 53-5-2 FIG. 5 (SHEET 1)Dec 29, 2005 · N722CX · Doug DC872 · Fuselage Main, Longeron/StringerSDR IXXA05SMN308SLongeron · crackedDURING ROUTINE C-CHECK INSPECTION, AFT FUS CRACKED 2, STA FS 1617.000 L.17R. PERFORMED MAJOR REPAIR IAW SRM 53-5-2 FIG. 5. REMOVED CRACKED L-17R IAW SRM 53-1-0, SRM 51-1-20D. FABRICATED NEW LONGERON (EXTRUSION P/N S1616757) IAW SRM 53-5-2 FIG. 5 (SHEET 1) ITDec 29, 2005 · N722CX · Doug DC872 · Fuselage Main, Longeron/StringerSDR IXXA05SMN299SSkin · corrodedDURING ROUTINE C-CHECK INSP, LT WING OB L/E CORRODED, XFS 566.250 (LWR SURFACE) PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05582 DATE 12-23-05, DWG NR ED 4126 DATE 12-21-05 EO NR 20051457 DATE 12-23-05 REMOVED FASTENERS IAW SRM 51-1-21, DC8 SRM 51-1-20D . Dec 29, 2005 · N722CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05SMN297SRepair · misinstalledDURING ROUTINE C CHECK INSPECTION, LT WING.- OB L/E HAS NON STANDARD REPAIR, XW 762.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06006 DATED 01-05-06 REMOVED NON-STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D DC8 SRM 51-3-0 REMOVED DAMAGED SECTION IAW DWDec 29, 2005 · N722CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05SMN296SVane · damagedC-CHECK INSPECTION, LT WING INBD FLAP VANE HOLES ELONGATED, XILD 42. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED DAMAGED SECTION. PERFORMED NDT INSPECTION. FABRICATED REPAIR DOUBLER (AL7075T60.070) & FILLER (AL7075T60.063) & INTERNAL DOUBLER (AL7075Dec 29, 2005 · N722CX · Doug DC872 · Trailing Edge FlapsSDR IXXA05SMN294SSkin · wornDURING ROUTINE C-CHECK INSPECTION, RT OB FLAP UPPER SKIN WORN, STA XF 224.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 2Q. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW SRM 57-2-1 FIG. 2Q. FABRICATED EXTERNAL REPAIR DOUBLER (ALCLAD 2024 TDec 29, 2005 · N722CX · Doug DC872 · Trailing Edge FlapsSDR IXXA05SMN288SFrame · crackedDURING ROUTINE C-CHECK INSP, FWD ACCY COMPT INTERNAL PART BETWEEN L-25L AND L-24L, AT STA 255.000 HAS FRAME CRACKED (1.5 INCH). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG.74 (SHEET 1,3). REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED SECTION. FABRICATED EXDec 29, 2005 · N722CX · Doug DC872 · Fuselage Main, FrameSDR IXXA05SMN287SSkin · corrodedC-CHECK INSPECTION, EXTERNAL FUS LWR EXTERNAL SKIN CORRODED BETWEEN L33 AND L35R, STA 480.000 STATION 500. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SECTION. PERFORMED NDT INSPECTION. FABRICATED RDec 29, 2005 · N722CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05SMN302SSkin · corrodedDURING INSPECT, LT WING CTR L/E CORRODED, XFS 422.750. PERFORMED REPAIR IAW FAA FORM 8110-3 # 05587 DATE 12-29-05, SEMAN DWG # ED 4127 DATE 12-28-05 AND EO SEMAN # 20051458 DATE 12-29-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED CORROSION IAW DC-8 SRM Dec 29, 2005 · N722CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05SMN301SSkin · corrodedDURING INSPECT, LT WING OTBD L/E HAS NON STANDARD REPAIR, XW 485.000. PERFORMED REPAIR IAW FAA FORM 8110-3 # 05582 DATE 12-23-05, SEMAN DWG # ED 4125 DATE 12-22-05 AND EO SEMAN # 20051456 DATE 12-23-05. REMOVED NON STANDARD REPAIR IAW DC-8 SRM 51-1-21, DC-8 SDec 29, 2005 · N722CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05SMN300SSkin · corrodedDURING INSPECT, LT WING CTR L/E LWR PART SKIN CORRODED, XFS 341.000. PERFORMED REPAIR IAW FAA FORM 8110-3 NR 05586 DATE 12-28-05, SEMAN DWG NR ED 4124 DATE 12-22-05, EO SEMAN NR 20051455 DATE 12-28-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21, DC-8 SRM 51-3-0. Dec 29, 2005 · N722CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05SMN298SSkin · corrodedDURING INSPECT, LT WING CTR L/E EXT LWR SKIN CORRODED, XFS 304.000. PERFORMED REPAIR IAW FAA FORM 8110-3 NR 05586 DATE 12-28-05, SEMAN DWG NR ED 4123 DATE 12-27-05 AND EO SEMAN NR 20051454 DATE 12-28-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 AND DC-8 SRM 51-Dec 29, 2005 · N722CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05SMN295SVane · damagedDURING INSPECT, LT WING OUTBD VANE FWD HOLES ELONGATED, XOLDO 66.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05586 DATE 12-28-05, SEMAN DWG NR ED 4121 DATE 12-23-05 AND EO SEMAN NR 20051452 DATE 12-28-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVEDDec 29, 2005 · N722CX · Doug DC872 · Trailing Edge FlapsSDR IXXA05SMN285SRepair · improperDURING INSP, RT INBD FLAP FWD UPPER SURFACE HAS NO STANDARD REPAIR (STA XW 37.000-48.000). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05580 DATE 12-21-05, SEMAN DWG NR ED 4129 DATE 12-20-05, EO SEMAN 20051444 DATE 12-21-05. REMOVED REPAIR IAW DC-8 SRM 51-Dec 29, 2005 · N722CX · Doug DC872 · Trailing Edge FlapsSDR IXXA05SMN283SFitting · crackedDURING ROUTINE C CHECK INSPECTION, NR 2 ENGINE COWL DOOR RAIL FITTING CRACKED 1, AT STA 254.324 (RT SIDE). REMOVED FASTENERS IAW DC8 SRM 51-3-0, DC8 SRM 51-1-21, DC8 SRM 51-1-21A. PERFORMED STOP HOLE, FABRICATED DOUBLER (17-4PH STAINLESS FLAT BAR) IAW ENG SHDec 16, 2005 · N722CX · Doug DC872 · Nacelle/Pylon, Main FrameSDR IXXA05SMN276SRepair · misinstalledDURING C CHECK, LT INBD AIL LWR SKIN HAS NO STANDARD REPAIR (STA XA 543.000-551.000). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-8-1 FIG 1. REMOVED PANEL PLATING WITH NON STANDARD REPAIR ON IT IAW DC8 SRM 57-1-0, DC8 SRM 51-1-21. FAB`D NEW PLATING (AL2024T30 0.02Dec 16, 2005 · N722CX · Doug DC872 · AileronsSDR IXXA05SMN280SSkin · dentedDURING ROUTINE C-CHECK INSPECTION, EXTERNAL FUS LWR EXTERNAL SKIN DENTED L-232, STA 356.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 05582 DATE 12-23-05, SEMAN DWG ED 4116 DATE 12-20-05, EO SEMAN 20051439 DATE 12-23-05. FABRICATED REPAIR DOUBLER & (03 EDec 16, 2005 · N722CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05SMN282SSkin · dentedC-CHECK INSPECTION, EXTERNAL FUS LWR EXTERNAL SKIN DENTED BETWEEN L-23 & L-24L STA 403. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, DAMAGED FRAME SEGMENT. FABRICATED NEW FRAME SEGMENT, (02 EA) ANGLES. HEAT TREATED FRAME SEGMENT & ANGLES. CLEANED, TREATED ADec 16, 2005 · N722CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05SMN279SHeat Exchanger · crackedDURING ROUTINE C-CHECK INSP, RT AFT HEAT EXCHANGER LT LWR CORNER CRACKED .5 INCH APPROX. PERFORMED MAJOR REPAIR IAW NR 05580 DATE 12-21-05, DWG NR ED 4114 DATE 12-17-05, EO 20051435 DATE 12-21-05. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAWDec 16, 2005 · N722CX · Doug DC872 · Air Distribution SystemSDR IXXA05SMN278SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, FWD PASSENGER DOOR LWR SKIN CRACKED 1 INCH APPROX. PERFORMED MAJOR REPAIR IAW SRM 52-2-0 FIG. 4 (SHEET 3). REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.050”) IAW SRM 52-2-0 FIG. 4 (SHEET 3),Dec 16, 2005 · N722CX · Doug DC872 · Passenger/Crew DoorsSDR IXXA05SMN277SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, REPAIR ON EXT SKIN OF FWD PASSENGER DOOR HAS IMPROPER FASTENERS PERFORMED MAJOR REPAIR IAW SRM 52-2-0 FIG. 4 (SHEET 3). REMOVED EXISTING REPAIR IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.050”) IAW SRM 52-2-0Dec 16, 2005 · N722CX · Doug DC872 · Passenger/Crew DoorsSDR IXXA05SMN281SSkin · dentedDURING ROUTINE C CHECK INSPECTION, EXTERNAL FUS.- LWR EXTERNAL SKIN DENTED, L-22L STA 364.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05582 DATE 12-23-05, SEMAN DWG NR ED 4116 DATE 12-20-05, EO SEMAN 20051439 DATE 12-23-05. REMOVED EXISTING REPAIR DOUDec 16, 2005 · N722CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05SMN275SSkin · corrodedDURING C CHECK , LT OUTBD AIL LWR SKIN CORRODED, STA XA 722.000. PERFORMED REPAIR IAW FAA FORM 8110-3 NR 05580 DATE 12-21-05, SEMAN DWG NR ED 4119 DATE 12-20-05 & EO SEMAN NR 20051449 DATE 12-21-05. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITSDec 15, 2005 · N722CX · Doug DC872 · AileronsSDR IXXA05SMN270SSkin · corrodedDURING C CHECK, 2 CORRODED AREAS FOUND ON LOWER FUSELAGE NOSE SECTION AT FOLLOWING LOCATION BS 217 BETWEEN L32 & 31R, BS 223 BETWEEN L32R & 32L, DUE CHANGE. PERFORMED REPAIR IAW DC-8 SRM 53-2-1. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND OUT OF LIMITS IAW DDec 15, 2005 · N722CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05SMN274SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, DURING ROUTINE C-CHECK INSPECTION, LT IB AIL LWR SKIN CORRODED, STA 593.000. PERFORMED MAJOR REPAIR IAW SRM 52-2-0 FIG. 4 (SHEET 3). REMOVED EXISTING REPAIR IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.050”)Dec 15, 2005 · N722CX · Doug DC872 · AileronsSDR IXXA05SMN273SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, LT OB FLAP SKIN CRACKED .5, STA XF 212.000 PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 2Q, EO NR 20051445 DATED 12-15-051. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW SRM 57-2-1 FIG. 2Q. FABRICATED EXTERNALDec 15, 2005 · N722CX · Doug DC872 · Trailing Edge FlapsSDR IXXA05SMN269SSkin · damagedDURING ROUTINE C-CHECK INSP, LT FWD PASSENGER DOOR DAMAGE. SKIN AT REAR LOWER CORNER HAS BEEN DAMAGED (INCH LONG CUT), NEED TO BE REPAIRED PERFORMED REPAIR IAW AD 2000-20-08, S/B 53-075, DWG NR SR08530021, 5750776, SRM 53-2-0 FIG. 15. TR NR 53-128, 53-196 DATDec 15, 2005 · N722CX · Doug DC872 · Passenger/Crew DoorsSDR IXXA05SMN272SSkin · damagedDURING INSPECT, LT OB FLAP UPPER SURFACE HAS NO STANDARD REPAIR, STA XF 347.000. PERFORMED MAJOR REPAIR, DWG NR ED 4118 DATE 12-20-05, EO 20051446 DATE 12-21-05. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21. REMOVED DAMAGED SEGMENT IAW DWG ED-4118. PERFORMEDec 15, 2005 · N722CX · Doug DC872 · Trailing Edge FlapsSDR IXXA05SMN271SWindshield · crackedDURING C-CHECK INSPECTION, COCKPIT LT LATERAL WINDSHIELD CRACKED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05580. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED CORROSION IAW DC-8 RM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRN 57-2-0 PAGE 16Dec 15, 2005 · N722CX · Doug DC872 · Flight Compartment WindowsSDR IXXA05RNG098SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION AT RIGHT WING LOWER SKIN OF CENTER EXTENDED LEADING EDGE AROUND WING STATION XFS 360.250, RT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERFORMED IAW ASTME 797-01 AND IT WAS FOUNDNov 4, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG097SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON UPPER SKIN AT CENTER EXTENDED LEADING EDGE AROUND STA XW 257.500-LT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERFORMED IAW ASTME 797-01 AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRNov 3, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG096SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON ON UPPER SKIN AT PYLON NR 2 LEADING EDGE UPPER SKIN, LT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERROMED IAW ASTME 797-01 AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PAGENov 3, 2005 · N721CX · Doug DC872 · Nacelle/Pylon, Plate/SkinSDR IXXA05RNG094SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON UPPER SKIN AT OB EXTENDED LEADING EDGE AROUND STA. XFS 791.250 TO 816.000 - LT. DAMAGED AREA WAS CLEANED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-2-1 FIGURE 38 AND EWO ATI-57-059.Oct 31, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG099SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON CENTER EXTENDED LEADING EDGE LOWER SKIN AROUND STA XFS 710.50-RT. DAMAGED AREA WAS BLENDED OUT AND A REINFORCEMENT DOUBLER WAS FABRICATED AND INSTALLED IAW EO ATI-092905 AND EWO ATI-57-063. FAA FORM 8110-3 WAS Oct 28, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG093SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON THE UPPER SKIN AT OB PYLON NR 4-RT. DAMAGED AREA WAS CLEANED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-2-1 FIG 38 AND EWO ATI 57-058.Oct 28, 2005 · N721CX · Doug DC872 · Nacelle/Pylon, Plate/SkinSDR IXXA05RNG090SSkin · corrodedDURING INSPECTION CHECK CORROSION WAS FOUND ON INNER EXTENDED LEADING EDGE OUTER UPPER SKIN AROUND STA XFS 207.500 - RT. DAMAGED AREA WAS BLENDED OUT AND REINFORCEMENT DOUBLER WAS FABRICATED AND INSTALLED IAW EO ATI-092305 AND EWO ATI-57-055. FAA FORM 8110-3 Oct 28, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG089SSkin · corrodedDURING INSPECTION CHECK, CORROSION WAS FOUND ON CENTER EXTENDED LEADING EDGE OUTER LOWER SKIN AROUND STA XFS 304.00 - RT. DAMAGED AREA WAS REMOVED AND A REINFORCEMENT DOUBLER WAS FABRICATED AND INSTALLED IAW EO ATI-092205 AND EWO ATI-57-054. FAA FORM 8110-3 Oct 28, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG092SSkin · corrodedDURING INSPECTION CHECK, CORROSION FOUND ON UPPER SKIN AT OUTBOARD PYLON NR 3 RT. UPPER SKIN AT OUTBOARD PYLON NR 3 WAS REPAIRED IAW SRM 57-2-1 FIG 38 AND EWO ATI-57-057.Oct 28, 2005 · N721CX · Doug DC872 · Wing, Center BoxSDR IXXA05RNG091SSkin · corrodedDURING INSPECTION CHECK, FOUND CORROSION ON UPPER SKIN AT OUTBOARD EXTENDED LEADING EDGE AROUND STA XFS 591.250 - 603.750 - RT. CORROSION WAS REMOVED IAW SRM DC8 51-1-8 PAGE 20 AND THICKNESS WAS FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PAGE 16 AND ASTME 79701. Oct 28, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG088SSkin · corrodedDURING INSPECTION CHECK, FOUND CORROSION ON CENTER EXTENDED LEADING EDGE OUTER LOWER SKIN AROUND STA XOLDI 6.225 - RT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20 AND THICKNESS WAS FOUND OUT OF LIMITS IAW SRM 57-2-0 PAGE 16 (MAX: 0.063 IN, MIN: 0.035 IN)Oct 28, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG114SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON RT WING CENTER LE UPPER EXTERIOR SURFACE, STA XW 408.343. SKIN WAS REPLACED IAW MFG DRAWING 5769857, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7 AND PROTECTIVE TREATMENT WAS APPLIED IAW SRM 51-1-8 PAGE 13-16Oct 27, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG100SPanel · corrodedDURING INSPECTION CHECK, FOUND CORROSION ON HORIZONTAL STABILIZER TRAILING EDGE LOWER AND UPPER PANEL. REPAIR ACCOMPLISHED, REMOVED PANEL AND STIFFENER, FABRICATED AND INSTALLED NEW PANEL AND STIFFENER IN ACCORDANCE WITH DRAWINGS 55-05467-1, 55-05467-2, 55-05Oct 14, 2005 · N721CX · Doug DC872 · Horizontal Stabilizer Miscellaneous StructureSDR IXXA05RNG116SSkin · corrodedDURING INSPECTION CHECK WAS FOUND LT OB FLAP T/E PANEL LWD INNER SKIN WITH CORROSION AND BONDED DOUBLER DELAMINANTED, STA XW2-XW91. SKIN ON LT IB FLAP WAS FABRICATED AND INSTALLED IAW MFG DRAWING 5652277, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7.Sep 28, 2005 · N721CX · Doug DC872 · Trailing Edge FlapsSDR IXXA05RNG115SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON LT IB FLAP T/E PANEL LWD OUTER SKIN, STA XW3 TO XW91.LT IB FLAP T/E PANEL LWD OUTER SKIN WAS REPLACED IAW MFG DRAWING 5652277, AND RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7.Sep 28, 2005 · N721CX · Doug DC872 · Trailing Edge FlapsSDR IXXA05RNG113SPanel · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON LT OB FLAP T/E PANEL LWD INNER SKIN, STA XF 415. SKIN WAS REPLACED IAW MFG DRAWING 5654758 (STA XW 407-XF415) AND RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7.Sep 28, 2005 · N721CX · Doug DC872 · Trailing Edge FlapsSDR IXXA05RNG112SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION AND BONDED DOUBLERS DELAMINATED ON LT OB FLAP T/E UPPER INNER SKIN, STA XF 309.0 TO 333.0. SKIN WAS REPLACED IAW MFG DRAWING 5642970, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7 AND PROTECTIVE TREATMENT WAS APPSep 28, 2005 · N721CX · Doug DC872 · Trailing Edge Flaps
Back to Douglas DC-8-72