Douglas DC-8-71F

Service difficulty reports · 8,938

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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 = 'DC871F'
  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 IXXA1100520Wire Harness · damagedDURING CLIMBOUT, NR 3 MAIN TANK BOOST PUMP C/B`S POPPED. THE CREW PERFORMED COM PROCEDURES, BUT NO HELP. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT AND FOUND NR 2 PIN RECESSED AT BOOST PUMP CONNECTOR PLUG. THEY REPLACED NR 3 MAAug 9, 2011 · N821BX · Doug DC871F · Fuel System WiringSDR IXXA110052OWire Harness · damagedDURING CLIMB OUT, NR 3 MAIN TANK BOOST PUMP C/B'S POPPED. THE CREW PERFORMED COM PROCEDURES, BUT NO HELP. THE CREW RETURNED TO DEPARTUE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT AND FOUND NR 2 PIN RECESSED AT BOOST PUMP CONNECTOR PLUG. THEY REPLACED NR 3 MAAug 9, 2011 · N821BX · Doug DC871F · Fuel System WiringSDR IXXA11SMN094SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR LOWER SKIN PANEL DENTED AT SEVERAL POINTS AT STA XE 246.000 - XH 285.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PEJun 14, 2011 · N830BX · Doug DC871F · Elevator, Plate/SkinSDR IXXA11SMN093SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND RT MLG INBD DOOR INNER SKIN CORRODED. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMER AREA AND REPAIR PARTS. INSTALLED NEW SKIN IAW SRM 51-1-8, SRM 52-2-0, SRM Jun 10, 2011 · N830BX · Doug DC871F · Landing Gear DoorsSDR IXXA11SMN092SSkin · crackedDURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR UPPER SKIN DENTED AND CRACKED AT STATION XE 246.000 - 285.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED RT Jun 8, 2011 · N830BX · Doug DC871F · Elevator, Plate/SkinSDR IXXA11SMN091SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT HORIZ STABILIZER T/E UPPER SKIN CORRODED AT STA XE 29.000 - 77.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INNER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMEDJun 8, 2011 · N830BX · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR IXXA11SMN090SWeb · wornDURING ROUTINE C-CHECK INSP FOUND NR 3 ENGINE THRUST REVERSER RT COWL FIXED STRUCTURE WEB FLANGE WORN AT STA YN 203.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED FRAME SEGMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR Jun 8, 2011 · N830BX · Doug DC871F · Engine Thrust ReverserSDR IXXA11SMN089SWeb · wornDURING ROUTINE C-CHECK INSP, FOUND NR 3 ENGINE THRUST REVERSER LT COWL FIXED STRUCTURE WEB FLANGE WORN AT STA YN 203.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED FRAME SEGMENT. CLEANED, TREATED, PRIMED AREA AND REPAIJun 8, 2011 · N830BX · Doug DC871F · Engine Thrust ReverserSDR IXXA11SMN088SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND RT WING UPPER SKIN CORRODED AT STA XW 55.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS INSTALLED NEW SKIN IAW SRM 51-1-8, SRM 57-2-0,Jun 8, 2011 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA11SMN086SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND LT WING T/E PANEL CORRODED AT STATION XW 55.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW SKIN IAW SRM 51-1-8, SRM 57-2-0, SRM 51-3-0, SRM 51-1-8B, SRMJun 8, 2011 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA11SMN085SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FWD BATHTUB FITTING CRACKED AT STA 680.000, LONGERON 9 RT. REMOVED CRACKED BATHTUB FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW BATHTUB FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D Jun 8, 2011 · N830BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA11SMN084SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FWD FITTING CRACKED AT STA 798.000, LONGERON 19 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING SRM 51-1-20D, SRM 51-1-0, SRM 51-1-8B, SRM 51-1-20D,Jun 8, 2011 · N830BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA11SMN087SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND RT OTBD FLAP UPPER EXTERNAL SKIN DENTED AT SEVERAL POINTS AT STA XF 415.000 - 440.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLEJun 7, 2011 · N830BX · Doug DC871F · Trailing Edge FlapsSDR IXXA11SMN083SSupport Fitting · crackedDURING ROUTINE C-CHECK INSP, FOUND RT WING FLAP LINK SUPPORT LT SIDE CRACKED AT STA XF 409.000. REMOVED HINGE CRACKED SUPPORT FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW HINGE SUPPORT FITTING IAW S/B 27-249, REV 1, SRM 51-3-0, SRM 51-1-21, SRM Jun 7, 2011 · N830BX · Doug DC871F · Wing, Control Surface Attach FittingsSDR IXXA11SMN082SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND RT MLG WHEEL WELL FITTING CRACKED AT STATION 879.375. REMOVED CRACKED FRAME FITTING. FABRICATED NEW FITTING, SPLICERS, SHIMS AND DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FITTING, DOUBLER, SPLIJun 6, 2011 · N830BX · Doug DC871F · Fuselage, Landing Gear Attach FittingsSDR IXXA11SMN081SSkin · misrepairedDURING ROUTINE C-CHECK INSP FOUND, IMPROPER REPAIR AT FWD BASKET DOOR OPENING FWD CTR LIP AT STATION FS 290, LONGERON 34.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIRJun 6, 2011 · N830BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA11SMN080SStrap · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND NLG WHEEL WELL LT TUNNEL COMPARTMENT STRAP CORRODED AT STA 8.000. REMOVED CORROSION. REMOVED DAMAGED STRAP SEGEMENT. FABRICATED STRAP SEGMENT AND SPLICE. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NJun 6, 2011 · N830BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA11SMN079SSupport Fitting · crackedDURING ROUTINE C-CHECK INSP FOUND NR 1 ALT TANK NR 6 FUEL PROBE FITTING SUPPORT CRACKED. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, AND SRM 51-3-1.Jun 6, 2011 · N830BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA11SMN078SAngle · crackedDURING ROUTINE C-CHECK INSP FOUND NR 4 PYLON INTERNAL ANGLE CRACKED AT STATION YN 321.397 AND STA XRS 495.665. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR ANGLE, STRAP DOUBJun 6, 2011 · N830BX · Doug DC871F · Nacelle/Pylon Miscellaneous StructureSDR IXXA11SMN077Fitting · crackedDURING ROUTINE C-CHECK INSP, FOUND RT MLG WHEEL WELL DOG HOUSE FITTING CRACKED AT STA 855.000, RT BOTTOM LINE 46. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-1-8B, SRM 51-1-0, SRM 51-3-0 AND SRM Jun 6, 2011 · N830BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA11SMN076SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND LT MLG INBD DOOR INNER SKIN CORRODED. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMER AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAWJun 6, 2011 · N830BX · Doug DC871F · Landing Gear DoorsSDR IXXA110044OStriker · bentDURING CRUISE, THE MLG DOOR LIGHT REMAINED ON. THE CREW CYCLED THE MAIN LANDING GEAR AND LIGHT REMAINED ON. WHEN AIRSPEED INCREASED TO 210 IAS LIGHT WENT OUT. THEY LANDED WITHOUT FURTHER INCIDENT. MX TROUBLESHOT AND FOUND THE RT GEAR DOOR STRIKER BENT. THJun 4, 2011 · N822BX · Doug DC871F · Landing Gear Position and WarningSDR IXXA11SMN075SStructure · misrepairedDURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT SMALL DRAIN DOUBLER FWD LOWER CENTER FUSELAGE FORWARD OF CENTER EQUIP DOOR AT STA FS 615 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED REPAIR EXISTING REPAIR. FABRICATED REPAIR DOUBJun 3, 2011 · N830BX · Doug DC871F · Fuselage Main, StructureSDR IXXA11SMN072SSkin · misrepairedDURING ROUTINE C-CHECK INSP FOUND IMPROPER DOUBLER REPAIR AT LT FWD FUSELAGE EMERGENCY EXIT DOOR AT STA FS 404 LONGERON 15.5 LT. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR DOUBLER. INSTALLED NEW FASTENERS ANDJun 2, 2011 · N830BX · Doug DC871F · Emergency ExitsSDR IXXA11SMN071SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTUIN FOUND IMPROPER DOUBLER REPAIR AT RT FWD FUSELAGE EMERGENCY EXIT DOOR AT STATION FS 392, LONGERON 16.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER. CLEANED, TREATED, Jun 2, 2011 · N830BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA11SMN070SSkin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND IMPROPER DOUBLER REPAIR, RT FWD FUSELAGE, 2 WINDOWS FWD OF EMERGENCY EXIT DOOR AT STATION FS 300 LONGERON 16 RT. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLEJun 2, 2011 · N830BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA110035OControl Cable · out of rigDURING LEVEL OFF, NR 3 ENGINE COMPRESSOR STALLED WHEN THROTTLES WERE RETARDED,(N1-93 PERCENT, N2-91 PERCENT, F/F-3100, OAT-44 DEGREES AND M-.80/300KIAS). THE CREW DIVERTED WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED TROUBLESHOOTING TREE NR 41, RERIGGED VSV AND Apr 28, 2011 · N830BX · Doug DC871F · Turbine Engine Compressor SectionSDR IXXAIXXA110031OEngine · power lossDURING CRUISE AT FL 380 IN CALM AIR, NR 2 ENG N1 RPM AND NR 2 RPM ROLLED BACKED TO 50 PERCENT N1 AND 85 PERCENT N2. EGT WAS 530°C FUEL FLOW DECREASED TO APPROX 700 LBS. OIL TEMP DECREASED TO ZERO AND OIL PRESS WAS AT 35 PSI FUEL PRESS FLUCTUATING BETWEEN 30 Mar 30, 2011 · N820BX · Doug DC871F · Engine (Turbine/Turboprop)SDR IXXA11SMN028SSkin · dentedDURING ROUTINE C-CHECK INSP, FOUND RT WING OTBD FLAP LOWER SKIN SCRATCH AND DENTS XF AT STA 174.000 TO XF 219.000. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM 57-7-1, Mar 4, 2011 · N821BX · Doug DC871F · Trailing Edge FlapsSDR IXXA110023OWire Harness · defectiveDURING CLIMBOUT FROM KTOL NR ONE EGT ANALOG AND DIGITAL READ OUTS DROPPED FROM 700 DEGREE TO 420 DEGREE WITH FLUCTUATION PLUS/ MINUS 5 DEGREE, N1 AND N2 SIMILAR TO THE OTHER 3 ENG. ALL 4 THROTTLES WERE ALIGNED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER Feb 18, 2011 · N822BX · Doug DC871F · Engine Indicating System WiringSDR IXXA110022SSkin · dentedDURING PREFLIGHT FOUND LT SIDE BELLY SKIN TO BE (DENTED AND CRACKED) AT STA 55 BETWEEN 15" TO 19.2500" FROM CTR LINE. OPENFeb 14, 2011 · N830BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA11SMN048SSpar Cap · crackedDURING ROUTINE C-CHECK INSP FOUND RT WING FRONT SPAR L/E LOWER CAP CRACKED AT STA XFS 500.233. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSP, NO DISCREPANCY FOUND. FABRICATED SPLICE ANGLES, EXTERNAL DOUBLER, STRAP. CLEANED, TREATED, PRIMFeb 11, 2011 · N821BX · Doug DC871F · Wing SparSDR U2RA449SPIM003Skin · corrodedRT HORIZ STAB BETWEEN XE 75.672 AND XE 147.906 T/E UPPER PANEL SKIN WITH CORROSION AROUND FASTENERS.Feb 11, 2011 · N872SJ · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR IXXA110019OConnector · dirtyDURING TAKEOFF, NR 1 ENG OIL PRESSURE LIGHT CAME ON INTERMITTENTLY, OIL TEMP AND PRESSURE GOOD ON FLIGHT ENGINEER PANEL. THE CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX CLEANED THE CONNECTOR PLUG ON DIFFERENTIAL PRESSURE WITH. OFeb 10, 2011 · N823BX · Doug DC871F · Engine Oil System WiringSDR IXXA11SMN047SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND RT MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 680.000 LONGERON 6, RT. REMOVED CRACKED FITTING. CLEANED AND APPLIED PRIMER TO AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, AND SRM 51-3-1.Feb 8, 2011 · N821BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA11SMN044SFloorbeam · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FLOORBEAM WEB CRACKED AT STA 960.000 LT BOTTOM LINE 56. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW EXTRUSION ANGLE AND FILLER. CLEANED TREATED, PRIMED AREA AND RFeb 7, 2011 · N821BX · Doug DC871F · Fuselage Main, Floor BeamSDR IXXA11SMN043SFitting · corrodedDURING ROUTINE C CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CORRODED AT STA 879.000, LONGERON-19 RT TO LONGERON-22 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE FITTING. CLEANED, TREATED, PRIMED AREA AND REPAIRED PARTS. APPLIED SEALANT TO FRFeb 7, 2011 · N821BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA11SMN041SRib · crackedDURING ROUTINE C-CHECK INSP, FOUND RT WING INBD FLAP RIB CRACKED AT STA XF 129.000. REMOVED DAMAGED RIB. FABRICATED NEW RIB. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIME AREA AND REPAIR PARTS. INSTALLED NEW RIB IAW SRM CHAP 57-7-1 FIGURE 2, SHEET 4, SRMFeb 7, 2011 · N821BX · Doug DC871F · Trailing Edge FlapsSDR IXXA11SMN038SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND SKIN CRACKED AT STA 55.000, 70.000 LONGERON 33 RT AND LONGERON 34 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER, FILLER AND FFeb 7, 2011 · N821BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA11SMN046SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND EMPENNAGE NR 60 ACCESS RT FITTING CRACKED AT STA 1766.000, LONGERON 19. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-1-8B, SRM 51-1-21, 51-3-0 AND 51-3-1.Feb 7, 2011 · N821BX · Doug DC871F · Horizontal Stabilizer, Attach FittingsSDR IXXA11SMN045SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND EMPENNAGE NR 60 ACCESS LT FITTING CRACKED AT STA 1766.000 LONGERON 19. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-1-8B, SRM 51-1-21, 51-3-0 AND 51-3-1.Feb 7, 2011 · N821BX · Doug DC871F · Horizontal Stabilizer, Attach FittingsSDR IXXA11SMN042SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FWD FITTING CRACKED AT STA 702.000 LONGERON 19 RT. REMOVED CRACKED FITTING.INSTALLED NEW FITTING IAW SRM 51-1-21D AND SRM 51-3-1.Feb 7, 2011 · N821BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA11SMN040SAngle · corrodedDURING ROUTINE C-CHECK INSP, FOUND FWD LOWER CARGO FWD DOOR AND JAMB INTERIOR CORRODED AT STA 335.000, LONGERON 36 TO LONGERON 35 RT. REMOVED DAMAGED ANGLE. FABRICATED REPAIR ANGLE, FILLER AND REPAIR STRAP. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTFeb 7, 2011 · N821BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA11SMN037SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT STA 1160.000. R & R AFT CARGO COMPARTMENT FITTING IAW SRM 51-1-20D.Feb 7, 2011 · N821BX · Doug DC871F · Fuselage Main, Attach FittingsSDR U2RA449SPIM004Drive Assy · crackedRUDDER TAB DRIVE SECTOR BROKEN.Feb 7, 2011 · N872SJ · Doug DC871F · Rudder Tab Control SystemSDR IXXA11SMN039SSkin · dentedDURING ROUTINE C-CHECK INSP, FOUND LT INBD FLAP UPPÈR SKIN SHOWS DENTS AT DIFFERENT LOCATIONS AT STATION XW 3.000 - XW 92.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND REPAIR DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND RFeb 6, 2011 · N821BX · Doug DC871F · Trailing Edge FlapsSDR IXXA11SMN030SDoor Frame · crackedDURING ROUTINE C-CHECK INSP FOUND LOWER FWD CARGO COMPARTMENT FRAME CRACKED AT STA 200.000 BETWEEN LONGERON-32 RT AND LONGERON -33 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. R & R EXTRUSION FRAME SEGMENT. FABRICATED SPLICE AND AFeb 5, 2011 · N821BX · Doug DC871F · Fuselage Main, StructureSDR IXXA11SMN036SCargo Track · brokenDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 2 TRACK LUGS BROKEN AT STA 1580.000 - STA 1600.000. REMOVED DAMAGED TRACK SEGMENT. CLEANED, TREATED, PRIMED AND PAINTED AREA. INSTALLED NEW TRACK SEGMENT IAW SRM 51-1-21, 53-2-3 FIG 8A, SRM 51-1-8B, Feb 5, 2011 · N821BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA11SMN035SCargo Track · brokenDURING ROUTINE C-CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT NR 4 TRACK LUGS BROKEN AT STA 320.000 - STA 340.000. REMOVED DAMAGED TRACK SEGMENT. CLEANED, TREATED, PRIMED AND PAINTED AREA. INSTALLED NEW TRACK SEGMENT IAW SRM 51-1-21, 53-2-3, SRM 51-1-8B, SRFeb 5, 2011 · N821BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA11SMN034SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 1690.000, LONGERON 21 LT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-18B, SRM 51-1-20D AND SRM 51-3-1.Feb 5, 2011 · N821BX · Doug DC871F · Fuselage Main, Attach Fittings
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