# Service difficulty reports: N830BX, cancelled Apr 14, 2014

A list on [N830BX, cancelled Apr 14, 2014](https://openairdocs.org/deregistered/N830BX-2014-04-14.md).

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

Page 1 of 4 · 177 reports

- [SDR IXXA11SMN094S](https://openairdocs.org/sdr/IXXA11SMN094S.md): Skin · dented · Jun 14, 2011 · N830BX · Doug DC871F · Elevator, Plate/Skin
  > DURING 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. PE
- [SDR IXXA11SMN093S](https://openairdocs.org/sdr/IXXA11SMN093S.md): Skin · corroded · Jun 10, 2011 · N830BX · Doug DC871F · Landing Gear Doors
  > DURING 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
- [SDR IXXA11SMN092S](https://openairdocs.org/sdr/IXXA11SMN092S.md): Skin · cracked · Jun 8, 2011 · N830BX · Doug DC871F · Elevator, Plate/Skin
  > DURING 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
- [SDR IXXA11SMN091S](https://openairdocs.org/sdr/IXXA11SMN091S.md): Skin · corroded · Jun 8, 2011 · N830BX · Doug DC871F · Horizontal Stabilizer, Plate/Skin
  > DURING 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, PRIMED
- [SDR IXXA11SMN090S](https://openairdocs.org/sdr/IXXA11SMN090S.md): Web · worn · Jun 8, 2011 · N830BX · Doug DC871F · Engine Thrust Reverser
  > DURING 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
- [SDR IXXA11SMN089S](https://openairdocs.org/sdr/IXXA11SMN089S.md): Web · worn · Jun 8, 2011 · N830BX · Doug DC871F · Engine Thrust Reverser
  > DURING 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 REPAI
- [SDR IXXA11SMN088S](https://openairdocs.org/sdr/IXXA11SMN088S.md): Skin · corroded · Jun 8, 2011 · N830BX · Doug DC871F · Wing, Plate/Skin
  > DURING 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,
- [SDR IXXA11SMN086S](https://openairdocs.org/sdr/IXXA11SMN086S.md): Skin · corroded · Jun 8, 2011 · N830BX · Doug DC871F · Wing, Plate/Skin
  > DURING 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, SRM
- [SDR IXXA11SMN085S](https://openairdocs.org/sdr/IXXA11SMN085S.md): Fitting · cracked · Jun 8, 2011 · N830BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING 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
- [SDR IXXA11SMN084S](https://openairdocs.org/sdr/IXXA11SMN084S.md): Fitting · cracked · Jun 8, 2011 · N830BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING 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,
- [SDR IXXA11SMN087S](https://openairdocs.org/sdr/IXXA11SMN087S.md): Skin · dented · Jun 7, 2011 · N830BX · Doug DC871F · Trailing Edge Flaps
  > DURING 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. INSTALLE
- [SDR IXXA11SMN083S](https://openairdocs.org/sdr/IXXA11SMN083S.md): Support Fitting · cracked · Jun 7, 2011 · N830BX · Doug DC871F · Wing, Control Surface Attach Fittings
  > DURING 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
- [SDR IXXA11SMN082S](https://openairdocs.org/sdr/IXXA11SMN082S.md): Fitting · cracked · Jun 6, 2011 · N830BX · Doug DC871F · Fuselage, Landing Gear Attach Fittings
  > DURING 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, SPLI
- [SDR IXXA11SMN081S](https://openairdocs.org/sdr/IXXA11SMN081S.md): Skin · misrepaired · Jun 6, 2011 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING 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 REPAIR
- [SDR IXXA11SMN080S](https://openairdocs.org/sdr/IXXA11SMN080S.md): Strap · corroded · Jun 6, 2011 · N830BX · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING 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 N
- [SDR IXXA11SMN079S](https://openairdocs.org/sdr/IXXA11SMN079S.md): Support Fitting · cracked · Jun 6, 2011 · N830BX · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR IXXA11SMN078S](https://openairdocs.org/sdr/IXXA11SMN078S.md): Angle · cracked · Jun 6, 2011 · N830BX · Doug DC871F · Nacelle/Pylon Miscellaneous Structure
  > DURING 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 DOUB
- [SDR IXXA11SMN077](https://openairdocs.org/sdr/IXXA11SMN077.md): Fitting · cracked · Jun 6, 2011 · N830BX · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING 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
- [SDR IXXA11SMN076S](https://openairdocs.org/sdr/IXXA11SMN076S.md): Skin · corroded · Jun 6, 2011 · N830BX · Doug DC871F · Landing Gear Doors
  > DURING 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 IAW
- [SDR IXXA11SMN075S](https://openairdocs.org/sdr/IXXA11SMN075S.md): Structure · misrepaired · Jun 3, 2011 · N830BX · Doug DC871F · Fuselage Main, Structure
  > DURING 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 DOUB
- [SDR IXXA11SMN072S](https://openairdocs.org/sdr/IXXA11SMN072S.md): Skin · misrepaired · Jun 2, 2011 · N830BX · Doug DC871F · Emergency Exits
  > DURING 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 AND
- [SDR IXXA11SMN071S](https://openairdocs.org/sdr/IXXA11SMN071S.md): Skin · misrepaired · Jun 2, 2011 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING 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,
- [SDR IXXA11SMN070S](https://openairdocs.org/sdr/IXXA11SMN070S.md): Skin · misrepaired · Jun 2, 2011 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING 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. INSTALLE
- [SDR IXXA110035O](https://openairdocs.org/sdr/IXXA110035O.md): Control Cable · out of rig · Apr 28, 2011 · N830BX · Doug DC871F · Turbine Engine Compressor Section
  > DURING 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
- [SDR IXXA110022S](https://openairdocs.org/sdr/IXXA110022S.md): Skin · dented · Feb 14, 2011 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING PREFLIGHT FOUND LT SIDE BELLY SKIN TO BE (DENTED AND CRACKED) AT STA 55 BETWEEN 15" TO 19.2500" FROM CTR LINE. OPEN
- [SDR IXXA110008O](https://openairdocs.org/sdr/IXXA110008O.md): Instrument Panel · unsecure · Jan 26, 2011 · N830BX · Doug DC871F · Instrument Panel
  > DURING TAKEOFF ROLL AT 68 KTS THE F/O INSTRUMENT PANEL SLID OUT. THE TAKEOFF WAS ABORTED AND THE CREW RETURNED TO PARKING. MX SECURED THE F/O INSTRUMENT PANEL AND PERFORMED THE REJECTED TAKEOFF INSP. THE ACFT WAS RETURNED TO SERVICE IAW MM 31-10-2 AND MM 13
- [SDR IXXA100046O](https://openairdocs.org/sdr/IXXA100046O.md): Steering Sys · inoperative · Sep 17, 2010 · N830BX · Doug DC871F · Landing Gear Steering System
  > DURING TAKEOFF, F/O HAD NO RESISTANCE IN RUDDER PEDAL AND NO NOSE WHEEL STEERING. THE CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX INSPECTED THE F/O RUDDER PEDAL ASSY, OPS CHECK GOOD IAW MM 27-23-28, 27-20-03 AND 27-23-29. ACFT WAS
- [SDR IXXA090060O](https://openairdocs.org/sdr/IXXA090060O.md): Connector · dirty · Oct 20, 2009 · N830BX · Doug DC871F · Air Conditioning System Wiring
  > DURING CRUISE, THE RT BLEED VALVE'S DO NOT SHUT OFF INDIVIDUALLY, BUT WHEN THEY ARE SHUT OFF PRESSURE DROP'S TO 10 PSI, MANIFOLD TEMP IS 10 TO 20 DEGREE CELSIUS, RT PACK SEEMS TO BE INOPERATIVE. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX CLE
- [SDR IXXA090057O](https://openairdocs.org/sdr/IXXA090057O.md): Fuel Filter · clogged · Oct 14, 2009 · N830BX · Doug DC871F · Engine Fuel Distribution
  > DURING CLIMB OUT NR 1 ENGINE FLAMED OUT. THE CREW ACCOMPLISHED FLAME OUT IN FLIGHT START CHECKLIST. THE NR 1 ENGINE STARTED ALL PARAMETER NORMAL. CREW LANDED WITHOUT FURTHER INCIDENT. MX PERFORMED TROUBLESHOOTING FAULT 51 AND REPLACED ENGINE FUEL FILTER. OP
- [SDR IXXA090027O](https://openairdocs.org/sdr/IXXA090027O.md): Mechanism · dirty · Apr 22, 2009 · N830BX · Doug DC871F · Landing Gear Door Retract Section
  > AFTER TAKEOFF AND GEAR RETRACTION FROM KDFW, A SEVERE VIBRATION WAS FELT IN THE NOSE GEAR AREA. THE CREW RECYCLED THE LANDING GEAR AND THE CONDITION PERSISTED. THE CREW RETURNED TO KDFW AND LANDED WITHOUT INCIDENT. MAINTENANCE OBSERVED THE LEFT NOSE GEAR DO
- [SDR IXXA090006O](https://openairdocs.org/sdr/IXXA090006O.md): Detector · malfunctioned · Feb 20, 2009 · N830BX · Doug DC871F · Fire Detection
  > DURING CRUISE FROM KLAX, NR 4 ENGINE FIRE WARNING ILLUMINATED. THE CREW PERFORMED COM EMERGENCY PROCEDURES, THE CREW DISCHARGED NUMBER ONE FIRE BOTTLE, AFTER TWO MINUTES FIRE WARNING ILLUMINATED AGAIN AND DISCHARGED NR 2 FIRE BOTTLE. THE CREW SHUT NR 4 ENGIN
- [SDR IXXA090004O](https://openairdocs.org/sdr/IXXA090004O.md): Connector · contaminated · Feb 6, 2009 · N830BX · Doug DC871F · Fire Protection System Wiring
  > DURING CRUISE FROM KTOL NR 4 ENGINE FIRE WARNING INTERMITTENTLY GOING OFF, THEN CAME ON STEADY. THE CREW SHUTDOWN NUMBER FOUR ENGINE, LIGHT IN HANDLE REMAINED ON UNTIL FL 18,000 ON DESCENT. THE CREW DISCHARGED BOTH FIRE BOTTLES. THE CREW LANDED IN KDEN WITH
- [SDR IXXA080036O](https://openairdocs.org/sdr/IXXA080036O.md): Computer · defective · Dec 10, 2008 · N830BX · Doug DC871F · Autopilot System
  > DURING CLIMB-OUT OF KTOL WITH RUDDER POWER ON, YAW DAMPER ON AND AUTO PILOT ON THE RUDDER HAD A LEFT RUDDER INPUT. THE CREW TURNED THE AUTO PILOT OFF AND THE CONDITION REMAINED, TURNED THE YAW DAMPER OFF AND NO CHANGE. THE LEFT INPUT WENT AWAY ONLY WHEN RUDD
- [SDR IXX2008F00109](https://openairdocs.org/sdr/IXX2008F00109.md): Skin · misrepaired · Aug 18, 2008 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, FOUND LOWER AFT FUSELAGE BELLY FWD OF AFT BASKET DOOR HAS IMPROPER REPAIR AT STA FS1142 LONGERON 35.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECT
- [SDR IXX2008F00104](https://openairdocs.org/sdr/IXX2008F00104.md): Skin · corroded · Aug 8, 2008 · N830BX · Doug DC871F · Horizontal Stabilizer, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND RT HORIZ STABILIZER AFT PANEL CORRODED AT STA XF 195.963. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTNERS AS NEEDED TO PERFORM REPAIR. REMOVED CORRODED SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PART AS NEE
- [SDR IXX2008F00116](https://openairdocs.org/sdr/IXX2008F00116.md): Skin · misrepaired · Aug 7, 2008 · N830BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSPECTION, FOUND RT OTBD FLAP EXHAUST GATE LOWER SKIN HAS IMPROPER REPAIR. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW F
- [SDR IXX2008F00114](https://openairdocs.org/sdr/IXX2008F00114.md): Skin · misrepaired · Aug 7, 2008 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND LT AFT CORNER OF A PIT DOOR OPENING HAS IMPROPER REPAIR AT STA FS340, LONGERON 31 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAI
- [SDR IXX2008F00112](https://openairdocs.org/sdr/IXX2008F00112.md): Skin · misrepaired · Aug 7, 2008 · N830BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSP, FOUND RT OTBD FLAP LOWER SKIN HAS IMPROPER REPAIR AT STA XF 238.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW
- [SDR IXX2008F00115](https://openairdocs.org/sdr/IXX2008F00115.md): Skin · misrepaired · Aug 6, 2008 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND AFT LOWER FUSELAGE AFT OF OUTFLOW VALVE HAS IMPROPER REPAIR AT STA FS1688, LONGERON 35.75 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK, NO
- [SDR IXX2008F00111](https://openairdocs.org/sdr/IXX2008F00111.md): Skin · misrepaired · Aug 6, 2008 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND FWD LWR FUSELAGE AFT OF AFT ADF ANTENNA HAS IMPROPER REPAIR AT STA FS 172 LONGERON 35.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK AND N
- [SDR IXX2008F00101](https://openairdocs.org/sdr/IXX2008F00101.md): Skin · misrepaired · Aug 6, 2008 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK, FOUND DOUBLER FWD OF A-PIT DOOR ON LWR CENTERLINE, HAS IMPROPER REPAIR AT FS220, LONGERON 36. REMOVED FASTNERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP, NO CRACK, NO CORROSION FO
- [SDR IXX2008F00117](https://openairdocs.org/sdr/IXX2008F00117.md): Fitting · cracked · Aug 5, 2008 · N830BX · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSP, FOUND AFT CARGO COMPARTMENT SPLICE FITTING CRACKED AT STA 1040.00-1060.000 LONGERON 31 RIGHT. REMOVED CRACKED SPLICE FITTING. FABRICATED SPLICE FITTING. PERFORMED NDT INSP. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PR
- [SDR IXX2008F00113](https://openairdocs.org/sdr/IXX2008F00113.md): Skin · misrepaired · Aug 5, 2008 · N830BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSP, FOUND LT OTBD FLAP UPPER SKIN HAS IMPROPER REPAIR AND AT STA XF420.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND P
- [SDR IXX2008F00110](https://openairdocs.org/sdr/IXX2008F00110.md): Fitting · cracked · Aug 5, 2008 · N830BX · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT SPLICE FITTING CRACKED AT STA 1040.000-1060.000 LONGERON 31 LT. REMOVED CRACKED SPLICE FITTING. FABRICATED SPLICE FITTING. PERFORMED NDT INSP. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED, A
- [SDR IXX2008F00105](https://openairdocs.org/sdr/IXX2008F00105.md): Skin · cracked · Aug 5, 2008 · N830BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, FOUND RT WING UPPER SKIN CRACKED AT STRINGER 8 STA XW 408.00. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFOMRED NDT INSP. NO CRACK AND NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, AND FILLE
- [SDR IXX2008F00103](https://openairdocs.org/sdr/IXX2008F00103.md): Skin · dented · Aug 5, 2008 · N830BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND RT WING INBD L/E UPPER SKIN DENTED AT STA SFS 120.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, DOUBLER, ANGLES, FILLER, AND FAIRING. PERFORMED HEAT TREATMENT TO REPAIR ANG
- [SDR IXX2008F00102](https://openairdocs.org/sdr/IXX2008F00102.md): Skin · misrepaired · Aug 5, 2008 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK, FOUND LWR FWD FUSELAGE BELLY AFT OF FWD BASKET DOOR HAS IMPROPER REPAIR AT STA FS403, LONGERON 35.5 LT. REMOVED FASTNERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, REPAIR
- [SDR IXX2008F00100](https://openairdocs.org/sdr/IXX2008F00100.md): Skin · misrepaired · Aug 5, 2008 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, FOUND LT FWD FUSELAGE AFT AND BELOW EMERGENCY EXIT DOOR HAS IMPROPER REPAIR AT FS 447 LOGN 25.5 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, EXTERNAL
- [SDR IXX2008F00099](https://openairdocs.org/sdr/IXX2008F00099.md): Skin · misrepaired · Aug 5, 2008 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, FOUND AFT LOWER FUSELAGE AFT AND BELOW L-2 AND R-2 DOORS HAS IMPROPER REPAIR AT STA FS 1695, LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. REPA
- [SDR IXX2008F00107](https://openairdocs.org/sdr/IXX2008F00107.md): Seat Track · damaged · Jul 30, 2008 · N830BX · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE C-CHECK INSPECTION, FOUND P-1-5 SEAT TRACK DAMAGED. REMOVED DAMAGED TRACK SEGMENT. FABRICATED SPLICES. CLEANED, TREATED, AND PRIMED AREA AND SPLICES. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-7-1, FIG 4, SHEET 1 ITEM C, SRM 51-2-0,

Next page: https://openairdocs.org/deregistered/N830BX-2014-04-14/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N830BX' AND deregistration_id = 'N830BX-2014-04-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N830BX-2014-04-14/reports

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