N821BX, cancelled May 1, 2014

Service difficulty reports · 177

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N821BX' AND deregistration_id = 'N821BX-2014-05-01'
  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 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 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 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 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 FittingsSDR IXXA11SMN033SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT BATHTUB FITTING CRACKED AT STA 857.000 LONGERON 8 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 AND SRM Feb 5, 2011 · N821BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA11SMN032SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FORWARD FITTING CRACKED AT STA 857.000 LONGERON 19 RT. REMOVED CRACKED AFT FITTING. CLEANED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D AND SRM 51-3-1.Feb 5, 2011 · N821BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA11SMN031SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STA 798.000 LONGERON 11 RT. REMOVED CRACKED AFT FITTING. CLEANED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D AND SRM 51-3-1.Feb 5, 2011 · N821BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA11SMN029SDoor Frame · crackedDURING ROUTINE C-CHECK INSP, FOUND FWD CARGO DOOR JAMB CRACKED AT STA FS 330.000 BETWEEN LONGERON 32 LT AND 33 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR TRIPLER, REPAIRFeb 4, 2011 · N821BX · Doug DC871F · Fuselage Main, StructureSDR IXXA11SMN021SWeb · crackedDURING ROUTINE C-CHECK INSP FOUND RUDDER RIB WEB CRACKED AT STA ZR 106.00. REMOVED CRACKED WEB. FABRICATED NEW WEB. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIRED PARTS. APPLIED SEALANT TO FAYING SURFACES. PERFORMED RUDDER BALANCE. FOUNFeb 4, 2011 · N821BX · Doug DC871F · Rudder StructureSDR IXXA11SMN027SWeb · crackedDURING ROUTINE C-CHECK INSP, FOUND RUDDER WEB LT SIDE CRACKED AT STA ZR 65.000. REMOVED CRACKED WEB. FABRICATED NEW WEB. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIRED PARTS. INSTALLED REPAIRED PARTS IAW SRM CHAPTER 55-2-3, FIG 5, SRM 55-Feb 4, 2011 · N821BX · Doug DC871F · Rudder StructureSDR IXXA11SMN022SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND NR 1 ACCESSORY COMPARTMENT AIR CONDITIONING SKIN HAS CORROSION AT STA 70.000 LONGERON 33 RT AND LONGERON 34 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRIFeb 3, 2011 · N821BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA11SMN026SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND RT WING OTBD AILERON LOWER SKIN HAS DENTS AT STA XA 678.000 - XA 752.000. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED WEFeb 3, 2011 · N821BX · Doug DC871F · AileronsSDR IXXA11SMN025SSkin · dentedDURING ROUTINE C-CHECK INSP, FOUND RT WING OTBD FLAP UPPER SKIN SHOWS DENTS AT STA XF 380.000. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALFeb 3, 2011 · N821BX · Doug DC871F · Wing, Plate/SkinSDR IXXA11SMN024SSkin · dentedDURING ROUTINE C CHECK INSP FOUND RT WING OTBD FLAP UPPER SKIN SHOWS DENTS AT STA XF 408.343. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLFeb 3, 2011 · N821BX · Doug DC871F · Trailing Edge FlapsSDR IXXA11SMN023SSkin · wornDURING ROUTINE C-CHECK INSP FOUND RT WING OTBD FLAP SKIN WORN AT STA XRS 162.263. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED, PAINTED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS ANDFeb 3, 2011 · N821BX · Doug DC871F · Trailing Edge FlapsSDR IXXA11SMN020SStringer · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING NR 1 MAIN FUEL TANK STR CRACKED AT STA XW 408.000 AND STR 60. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED SPLICES FITTING, EXTRUSION. CLFeb 2, 2011 · N821BX · Doug DC871F · Wing, Longeron/StringerSDR IXXA11SMN018SSupport Bracket · crackedDURING ROUTINE C-CHECK INSP FOUND NR 1 ENG THRUST REVERSER SUPPORT FRAME CRACKED AT STA YN 202.000 . REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED FRAME SEGMENT. CLEANED, TREATED, PRIMED AREA AND REPAIRED PARTS. INSTALLED NEW Feb 1, 2011 · N821BX · Doug DC871F · Engine Thrust ReverserSDR IXXA11SMN017SSkin · crackedDURING ROUTINE C-INSP FOUND LT WING LOWER INNER SKIN CRACKED AROUND STRINGER 60 AT STA XW 408.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND FILLER. CFeb 1, 2011 · N821BX · Doug DC871F · Wing, Plate/SkinSDR IXXA110010SStringer · crackedDURING ROUTINE B-CHECK INSP FOR ACCOMPLISHING AD 2008-26-07 FOUND LT WING AT STA XW 408.343 STR 60 CRACKED. MX PERFORMED FERRY FLIGHT INSP IAW GMM 3.117, FOR THE REPAIR.Jan 16, 2011 · N821BX · Doug DC871F · Wing, Longeron/StringerSDR IXXA11009SSkin · crackedDURING ROUTINE B-CHECK INSP FOR ACCOMPLISHING AD 2008-26-07 FOUND LT WING LOWER SKIN CRACKED AT STA XW408.343, STRINGER 60. MX PERFORMED FERRY FLIGHT INSP IAW GMM 3.117, FOR THE REPAIR.Jan 16, 2011 · N821BX · Doug DC871F · Wing, Plate/SkinSDR IXXA100049OUplock · out of adjustDURING CLIMBOUT, WHILE THE CREW PERFORMING CLIMB CHECK LIST, THE UP LATCH CHECK FAILED WITH RED DOOR LIGHT ON. THEY CYCLED THE GEARS WITH NO HELP. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX DEFERRED THE UPLATCH SYS IAW MEL 32-14-01 TO BE ACCOMPLISSep 24, 2010 · N821BX · Doug DC871F · Landing Gear Position and WarningSDR IXXA100048OSwitch · out of adjustDURING CLIMBOUT,THE GEAR DOOR NOT LATCH LIGHT CAME ON. THE CREW CYCLED THE GEARS AND THE LIGHT REMAINED ON. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX ADJUSTED THE STRIKER SWITCH AND LUBED BOTH DOOR UPLATCH MECHANISMS. OPS CHECK GOOD IAW UAL MM Sep 24, 2010 · N821BX · Doug DC871F · Landing Gear Position and WarningSDR IXXA100035OPin · brokenAFTER TAKEOFF LANDING GEAR UNSAFE LIGHT CAME ON, THE CREW CYCLED GEAR LIGHT WENT OUT. ONE HR INTO FLIGHT DOOR NOT LATCH LIGHT CAME ON THEN WENT OUT, THE LANDING GEAR UNSAFE LIGHT REMAINED ON DURING FLIGHT. UPON GEAR EXTENSION, A LOUD BANG WAS HEARD, GOT (3) GRMay 25, 2010 · N821BX · Doug DC871F · Landing Gear Retraction/Extension SystemSDR IXXA090062OIndicator · defectiveDURING TAKEOFF, THE CAPT'S AIRSPEED INDICATOR HAD NO INDICATION. CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS. MX REPLACED CAPT'S AIRSPEED INDICATOR. OPS CHECK GOOD IAW UAL MM 30-30-04. ACFT WAS RETURNED TO SERVICE.Oct 22, 2009 · N821BX · Doug DC871F · Airspeed/Mach IndicatorSDR IXXA090031OTransducer · defectiveDURING CRUISE, AN UNCOMMANDED RUDDER KICK WITH NO MOVEMENT OF PEDALS. THE CREW DIVERTED TO KDFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DEFERRED THE AUTOPILOT SYSTEM. MAINTENANCE IN KTOL REPLACED THE LINEAR POSITION TRANSDUCER. OPERATIONAL CHECK Jun 9, 2009 · N821BX · Doug DC871F · Autopilot SystemSDR IXXA080031OAccess Panel · misinstalledDURING CLIMB-OUT FROM KBDL, THE CREW HEARD LOUD NOISE OF AIR FROM CAPT'S SIDE. THE CREW RETURNED TO KBDL WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND EMERGENCY ACCESS PANEL TO CAPT CLEARVIEW WINDOW HAD COME OUT AND FELL DOWN INTO FUSELAGE. MAINTENANCE REINSTNov 5, 2008 · N821BX · Doug DC871F · Fuselage Main, StructureSDR IXXA080029OEngine · flamed outAFTER LEVEL OFF AT 37,000 FT DURING THROTTLE REDUCTION NUMBER THREE ENGINE FLAMED OUT. THE CREW PERFORMED INFLIGHT START AT 22,000 FT, RESTART NORMAL. THE CREW LANDED IN KTOL WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED CFM FAULT 51, TROUBLESHOT TREE, CLOct 29, 2008 · N821BX · Doug DC871F · Engine (Turbine/Turboprop)SDR IXX2008F00018Connector · contaminatedFLT NR: ATN 807/KBRI TO KMSP. DURING CRUISE FROM KBFI THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL CAME ON. THE FIRE WARNING LIGHT WENT OUT AND THE BELL STOPPED RINGING. THE CREW SUCCESSFULLY TESTED THE SYSTEM AND PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN, AJul 18, 2008 · N821BX · Doug DC871F · Fire Protection System WiringSDR IXX2008F00013Fire Warning · false activationDURING CRUISE, THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL CAME ON. THE FIRE WARNING LIGHT WENT OUT AND THE BELL STOPPED RINGING. THE CREW TESTED THE SUCCESSFULLY TESTED THE SYSTEM AND PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN, AFTER ONE HOUR MORE OF FLIGHT Jul 18, 2008 · N821BX · Doug DC871F · Fire DetectionSDR IXX2008F00006Transducer · defectiveDURING CLIMB OUT, AT 240 KIAS WITH A 9 DEGREE PITCH NOSE UP STICK SHAKER CAME ON STEADY. IT CYCLED ON AND OFF RANDOMLY FOR 15 MINUTES UNTIL LANDING. STALL WARNING TEST SWITCH WAS TOGGLED WITH NO EFFECT. THE CREW LANDED WITH NO FURTHER INCIDENT. MAINTENANCEJul 10, 2008 · N821BX · Doug DC871F · Navigation SystemSDR IXXA08SMN183SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 1731 LONGERON 35.5 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND CORROSION FOUND. Apr 19, 2008 · N821BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA08SMN182SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 1694 LONGERON 27 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. CLEANED, TRApr 19, 2008 · N821BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA08SMN179SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT AND RIGHT INNER WING TRAILING EDGE STRUCTURE HAS IMPROPER REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. INSTALLED REPAIR PART KIT ON LT AND RT INNER WING TRAILING EDGE STRUCTURE. CLOSED MLG DOORS AND RApr 19, 2008 · N821BX · Doug DC871F · Wing, Plate/SkinSDR IXXA08SMN177SFrame · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FRAME FLANGE CRACKED AT STATION 1580.000 LONGERON 20 LEFT TO LONGERON 21 LEFT. REMOVED DAMAGED SEGMENT OF FRAME. FABRICATED SEGMENT OF FRAME, ANGLES. PERFORMED HEAT TREATMENT TO REPAIR PARTS. Apr 19, 2008 · N821BX · Doug DC871F · Fuselage Main, FrameSDR IXXA08SMN176SCargo Track · deterioratedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 5 TRACK LUGS DETERIORATED BETWEEN STATION 70.000 AND STATION 210.000. REMOVED DAMAGED SEGMENT OF TRACK AND EXISTING SPLICES. CLEANED, TREATED AND PRIMED AREA AND EXISTING SPLICES. INSTALApr 19, 2008 · N821BX · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
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