Douglas DC-8-72F

Service difficulty reports · 257

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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 = 'DC872F'
  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 IXX2008F00057Skin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE EXTERNAL SKIN HAS A CRACK AT STATION 1606.000-1604.000 LONGERON 10 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, INTERNAL FINGER DOUBLER, AND FILLJun 16, 2008 · N721CX · Doug DC872F · Fuselage Main, Plate/SkinSDR IXX2008F00052Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING CENTER LEADING EDGE UPPER SKIN HAS IMPROPER REPAIR AT STATION 285.250. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO COJun 16, 2008 · N721CX · Doug DC872F · Wing, Plate/SkinSDR IXX2008F00049Stiffener · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING TRAILING EDGE STIFFENER CRACKED AT STATION XW 19.000. REMOVED CRACKED STIFFENER. FABRICATED STIFFENER. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND STIFFENER.Jun 16, 2008 · N721CX · Doug DC872F · Wing Miscellaneous StructureSDR IXX2008F00030Finger Doubler · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND COCKPIT FINGER DOUBLER WITH CORROSION AT STATION FS 188.000-208.000 LT BOTTOM LINE 60. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK NO CORROSION FOUND FABRICATEDJun 16, 2008 · N721CX · Doug DC872F · Fuselage Miscellaneous StructureSDR IXX2008F00084Skin · wornDURING ROUTINE C CHECK INSPECTION, FOUND LT OUTBOARD FLAP SKIN ON EXHAUST GATE WORN AT STATION XF 250.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTAJun 14, 2008 · N721CX · Doug DC872F · Trailing Edge FlapsSDR IXX2008F00059Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD AILERON UPPER SKIN IMPROPER REPAIRS AT STATION XA 630.000-724.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED WITH HYJun 14, 2008 · N721CX · Doug DC872F · AileronsSDR IXX2008F00054Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD AILERON UPPER SKIN IMPROPER REPAIRS AT STATION XA 630.000-724.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED WITH HJun 14, 2008 · N721CX · Doug DC872F · AileronsSDR IXX2008F00051Skin · wornDURING ROUTINE C CHECK INSPECTION, FOUND LT OUTBOARD FLAP SKIN ON EXHAUST GATE WORN AT STATION XF 250.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTAJun 14, 2008 · N721CX · Doug DC872F · Trailing Edge FlapsSDR IXX2008F00070Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP UPPER PANEL HAS IMPROPER REPAIR AND DENTS AT STATION XW 3000 TO STATION XW 92.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND BONDED DOUBLER.Jun 13, 2008 · N721CX · Doug DC872F · Trailing Edge FlapsSDR IXX2008F00060Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP PANEL UPPER PART HAS IMPROPER REPAIR AT STATION 360.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIRJun 13, 2008 · N721CX · Doug DC872F · Trailing Edge FlapsSDR IXX2008F00055Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP PANEL UPPER PART HAS IMPROPER REPAIR AT STATION 360.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIRJun 13, 2008 · N721CX · Doug DC872F · Trailing Edge FlapsSDR IXX2008F00048Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP UPPER PANEL HAS IMPROPER REPAIR AND DENTS AT STATION XW 3000 TO STATION XW 92.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND BONDED DOUBLER.Jun 13, 2008 · N721CX · Doug DC872F · Trailing Edge FlapsSDR IXX2008F00086Skin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING LEADING EDGE LOWER SKIN CORRODED AT STATION XW 736.000-761.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLJun 12, 2008 · N721CX · Doug DC872F · Wing, Plate/SkinSDR IXX2008F00085Frame · crackedDURING ROUTINE C CHECK INSPECTION, FOUND ACCESSORY COMPARTMENT FRAME CRACKED AT STATION 255.000 LONGERON 25LT. REMOVED DAMAGED FRAME SEGMENT. FABRICATED NEW SEGMENT. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REJun 12, 2008 · N721CX · Doug DC872F · Fuselage Main, FrameSDR IXX2008F00083Bulkhead · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MIDDLE ACCESSORY COMPARTMENT BULKHEAD CRACKED AT STATION 680.000 LT BOTTOM LINE 20-30. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING DOUBLER AND SPLICE. REMOVED DAMAGED AREA. FABRICATED DOUBLER, DOJun 12, 2008 · N721CX · Doug DC872F · Fuselage Main, BulkheadSDR IXX2008F00076Longeron · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO BAY LONGERON 36 CORRODED AT STATION 1320.000-1340.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED LONGERON SEGMENT. FABRICATED SPLICE OF EXTRUSIJun 12, 2008 · N721CX · Doug DC872F · Fuselage Main, Longeron/StringerSDR IXX2008F00075Longeron Clip · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND AC COMPARTMENT CLIP CORRODED AT STATION 235.000 LONGERON 31LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED CLIP. FABRICATED NEW CLIP. CLEANED, TREATED AND PRIMED CLIP. INSTALLED CLIP IAW DC8 SRM 51-1-Jun 12, 2008 · N721CX · Doug DC872F · Fuselage Main, Attach FittingsSDR IXX2008F00069Skin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE EXTERNAL PART PRIMARY HEAT EXCHANGER LOWER AFT CORNER CRACKED AT STATION 188.000 LONGERON 27LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO COJun 12, 2008 · N721CX · Doug DC872F · Fuselage Main, Plate/SkinSDR IXX2008F00056Skin · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND FUSELAGE EXTERNAL PART PRIMARY HEAT EXCHANGER LOWER AFT CORNER CRACKED AT STATION 188.000 LONGERON 27LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO Jun 12, 2008 · N721CX · Doug DC872F · Fuselage Main, Plate/SkinSDR IXX2008F00053Fitting · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND ACND COMPARTMENT CLIP CORRODED AT STATION 235.000 LONGERON 31 LEFT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED CLIP. FABRICATED NEW CLIP. CLEANED, TREATED AND PRIMED CLIP. INSTALLED CLIP IAW DC8 SRM Jun 12, 2008 · N721CX · Doug DC872F · Fuselage Miscellaneous StructureSDR IXX2008F00043Longeron · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT LONGERON-36 CORRODED AT STATION 1320.000-1340.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEED TO PERFORM REPAIR. REMOVED DAMAGED LONGERON SEGMENT. FABRICATED SPLICE OF EJun 12, 2008 · N721CX · Doug DC872F · Fuselage Main, Longeron/StringerSDR IXX2008F00039Skin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING LEADING EDGE LOWER SKIN CORRODED AT STATION XW 736.000-761.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLJun 12, 2008 · N721CX · Doug DC872F · Wing, Plate/SkinSDR IXX2008F00038Stiffener · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING AUXILIARY SPARS STIFFENER CORRODED AT STATION XW 33.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED STIFFENER. FABRICATED STIFFENER. CLEANED, TREATED AND PRIMED AREA AND STIFFENER. INSTALLED Jun 12, 2008 · N721CX · Doug DC872F · Wing SparSDR IXX2008F00074Longeron Splice · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE SPLICE FITTING CRACKED AT STATION FS 1610.000 LONGERON 17RT. REMOVED CRACKED SPLICE FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-21, SRM 51-1-20D, DC8 SRM 51-1Jun 11, 2008 · N721CX · Doug DC872F · Fuselage Main, Longeron/StringerSDR IXX2008F00071Longeron · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND AFT FUSELAGE CRACKED AT STATION FS 1610.000 LONGERON 17 RT. REMOVED DAMAGED LONGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED LONGERON. IAW DC8 SRM 53-5-2 FIGURE 5 SHEET 1 PAGE 16 ITEM "B", DC8 SRM 51-1-8B, DC8 Jun 11, 2008 · N721CX · Doug DC872F · Fuselage Main, Longeron/StringerSDR IXX2008F00067Longeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE CRACKED AT STATION FS 1610.000 LONGERON 17 LT. REMOVED DAMAGED LONGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED LONGERON IAW DC8 SRM 53-5-2 FIGURE 5 SHEET 1 PAGE 16 ITEM "B", DC8 SRM 51-1-8B, DC8 SRJun 11, 2008 · N721CX · Doug DC872F · Fuselage Main, Longeron/StringerSDR IXX2008F00046Longeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE CRACKED AT STATION FS 1610.000 LONGERON 17LEFT. REMOVED DAMAGED LONGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED LONGERON. IAW DC8 SRM 53-5-2 FIGURE 5 SHEET 1 PAGE 16 ITEM "B", DC8 SRM 51-1-8B, DC8Jun 11, 2008 · N721CX · Doug DC872F · Fuselage Main, Longeron/StringerSDR IXX2008F00044Longeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE CRACKED AT STATION FS 1610.000 LONGERON 17 RIGHT. REMOVED DAMAGED LONGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED LONGERON IAW DC8 SRM 53-5-2 FIGURE 5 SHEET 1 PAGE 16 ITEM "B", DC8 SRM 51-1-8B, DC8Jun 11, 2008 · N721CX · Doug DC872F · Fuselage Main, Longeron/StringerSDR IXX2008F00040Fitting · crackedDURING ROURTINE C CHECK INSPECTION, FOUND AFT FUSELAGE SPLICE FITTING CRACKED AT STATION FS 1610.000 LONGERON 17RIGHT. REMOVED CRACKED SPLICE FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-21, SRM 51-1-20D, DC8 SRM Jun 11, 2008 · N721CX · Doug DC872F · Fuselage Miscellaneous StructureSDR IXX2008F00079Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON LT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND RJun 10, 2008 · N721CX · Doug DC872F · Wing, Plate/SkinSDR IXX2008F00047Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON LT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND RJun 10, 2008 · N721CX · Doug DC872F · Leading Edge DevicesSDR IXX2008F00087Skin · wornDURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP UPPER SKIN SHOWS WEAR AT STATION XF 211.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLJun 9, 2008 · N721CX · Doug DC872F · Trailing Edge FlapsSDR IXX2008F00082Skin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBD FLAP UPPER SKIN DENTED AT STATION XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FJun 9, 2008 · N721CX · Doug DC872F · Wing, Plate/SkinSDR IXX2008F00081Skin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD SLOT VANE LEADING EDGE HAS ELONGATED HOLES AT STATION XS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPJun 9, 2008 · N721CX · Doug DC872F · Wing, Plate/SkinSDR IXX2008F00078Skin · wornDURING ROUTINE C CHECK INSPECTION, FOUND LT WING OUTBOARD FLAP UPPER SKIN WORN AT STATION XF 211.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEWJun 9, 2008 · N721CX · Doug DC872F · Trailing Edge FlapsSDR IXX2008F00073Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING INBOARD FLAP UPPER SKIN HAS IMPROPER REPAIR AT STATION XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. Jun 9, 2008 · N721CX · Doug DC872F · Trailing Edge FlapsSDR IXX2008F00072Skin · misrepairedDURING ROUTINE C CHECK, FOUND IMPROPER REPAIR ON LT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095.000 AND XS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AJun 9, 2008 · N721CX · Doug DC872F · Wing, Plate/SkinSDR IXX2008F00068Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON RT WING OTBD SLOT VANE LEADING EDGE AT STATION XOLDO 67.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CJun 9, 2008 · N721CX · Doug DC872F · Wing, Plate/SkinSDR IXX2008F00061Skin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND NICKS RT WIND OUTBOARD FLAP UPPER SKIN AT STATION XF 345.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEWJun 9, 2008 · N721CX · Doug DC872F · Wing, Plate/SkinSDR IXX2008F00045Skin · wornDURING ROUTINE C CHECK INSPECTION, FOUND LT WING OUTBOARD FLAP UPPER SKIN WORN AT STATION XF 211.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEJun 9, 2008 · N721CX · Doug DC872F · Trailing Edge FlapsSDR IXX2008F00042Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD SLOT VANE LEADING EDGE HAS ELONGATED HOLES AT STATION XS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPJun 9, 2008 · N721CX · Doug DC872F · Leading Edge DevicesSDR IXX2008F00041Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING INBOARD FLAP UPPER SKIN HAS IMPROPER REPAIR AT STATION XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. Jun 9, 2008 · N721CX · Doug DC872F · Trailing Edge FlapsSDR IXX2008F00037Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON RT WING OUTBOARD SLOT VANE LEADING EDGE AT STATION XOLDO 67.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, Jun 9, 2008 · N721CX · Doug DC872F · Leading Edge DevicesSDR IXX2008F00036Skin · misrepairedDURING ROUTINE C CHECK, FOUND IMPROPER REPAIR ON LT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095.000 AND XS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AJun 9, 2008 · N721CX · Doug DC872F · Leading Edge DevicesSDR IXX2008F00034Skin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND NICKS RT WING OUTBOARD FLAP UPPER SKIN AT STATION XF 345.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEJun 9, 2008 · N721CX · Doug DC872F · Trailing Edge FlapsSDR IXX2008F00033Skin · wornDURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP UPPER SKIN SHOWS WEAR AT STATION XF 211.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLJun 9, 2008 · N721CX · Doug DC872F · Trailing Edge FlapsSDR IXX2008F00032Skin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP UPPER SKIN DENTED AT STATION XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEJun 9, 2008 · N721CX · Doug DC872F · Trailing Edge FlapsSDR IXX2008F00031Skin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND ELONGATED HOLES ON RT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING, FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REJun 9, 2008 · N721CX · Doug DC872F · Leading Edge DevicesSDR G412008F00001Fire Warning · false activationDURING CRUISE FROM KBWI NR 1 FIRE WARNING LIGHT AND BELL CAME ON MOMENTARILY THEN WENT OFF ENGINE WAS SHUTDOWN IAW COM PROCEDURE. THE CREW RETURNED TO KBWI AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HORSESHOE DETECTOR, LT CORE DETECTOR, RT CORE DETECTOJun 3, 2008 · N721CX · Doug DC872F · Fire DetectionSDR IXXA080020OMotor · defectiveDURING CLIMB-OUT FROM MLB AT FL350 NUMBER ONE ENGINE FLAMEOUT. THE CREW ACCOMPLISHED FLAMEOUT PROCEDURES AND DESCENDED TO FL210 FOR ENGINE RESTART. THE ENGINE RESTARTED NORMALLY AND THE CREW CONTINUED FLIGHT AND LANDED IN TOL WITHOUT INCIDENT. MAINTENANCE RMay 8, 2008 · N721CX · Doug DC872F · Fuel Controlling System
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