# Service difficulty reports: N823BX, cancelled Apr 14, 2014 A list on [N823BX, cancelled Apr 14, 2014](https://openairdocs.org/deregistered/N823BX-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 3 · 137 reports - [SDR IXXA110019O](https://openairdocs.org/sdr/IXXA110019O.md): Connector · dirty · Feb 10, 2011 · N823BX · Doug DC871F · Engine Oil System Wiring > DURING 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. O - [SDR IXXA110014S](https://openairdocs.org/sdr/IXXA110014S.md): Skin · cracked · Feb 5, 2011 · N823BX · Doug DC871F · Wing, Plate/Skin > DURING INSP FOR AD2008-26-07 AND SB DC8-57A102 FOUND LT WING LOWER SKIN CRACKED AT STRINGER 62 IN THE 14TH FASTENERS ROW OTBD FROM STA XW408 CENTERLINE PROPAGATING APPROX.300 FWD AND.050 AFT. REPAIR WAS ACCOMPLISHED IAW SRM 57-2-1 FIGURE 45 TR NUMBER 57-1 - [SDR IXXA100014O](https://openairdocs.org/sdr/IXXA100014O.md): Bulb · burned out · Feb 12, 2010 · N823BX · Doug DC871F · Landing Gear Position and Warning > DURING APPROACH, NOSE GEAR LIGHT DID NOT ILLUMINATE UPON GEAR EXTENSION. CREW CYCLED NOSE GEAR AND VISUALLY CHECKED THE GEAR WAS DOWN AND LOCKED, THEY LANDED WITHOUT FURTHER INCIDENT. MX FOUND TOP LIGHT BULB BURNED OUT AND BOTTOM LIGHT WAS INTERMITTENT WHEN P - [SDR IXXA100013O](https://openairdocs.org/sdr/IXXA100013O.md): Rheostat · failed · Feb 11, 2010 · N823BX · Doug DC871F · Passenger Compartment Lighting > DURING DESCENT, THE OVERHEAD LIGHTS WENT OUT, FOLLOWED BY SMOKE AND FUMES THEN OVERHEAD SWITCH PANEL INTEGRAL LIGHTS CIRCUIT BREAKER POPPED AND SMOKE AND FUMES CLEARED. THE CREW LANDED WITHOUT FURTHER INCIDENT. MX REPLACED OVERHEAD LIGHT PANEL RHEOSTAT, NO HEL - [SDR IXXA100009O](https://openairdocs.org/sdr/IXXA100009O.md): Vbv · out of rig · Jan 26, 2010 · N823BX · Doug DC871F · Turbine Engine Compressor Section > DURING POWER REDUCTION TO CRUISE POWER, NR 2 ENG COMPRESSOR STALLED. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX PERFORMED TROUBLESHOOTING FAULT 41 AND FOUND VBV'S OUT OF RIGGING. THEY RERIGGED THE VBV'S AND REPLACED CIT SENSOR. OPS CHECK GOOD IAW - [SDR IXXA090029O](https://openairdocs.org/sdr/IXXA090029O.md): Relay · defective · Apr 29, 2009 · N823BX · Doug DC871F · Windshield/Door Rain/Ice Removal > UPON DESCENT INTO KTOL, THE CREW PUSHED IN ANTI FOGGING CIRCUIT BREAKER AND THE CREW DETECTED SMOKE, THE CREW PULLED THE CIRCUIT BREAKER AND SMOKE ODOR DIMINISHED. THE CREW LANDED IN KTOL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RELAY. OPERATIONAL CHE - [SDR IXXA080026O](https://openairdocs.org/sdr/IXXA080026O.md): Engine · flamed out · Oct 18, 2008 · N823BX · Doug DC871F · Engine (Turbine/Turboprop) > DURING CLIMBOUT FROM KPDX AT 39000 FT NUMBER 4 ENGINE FLAMED OUT, AIRSPEED UNKNOWN, MACH.78, ALT 36.0, RAT UNKNOWN, WT 220.0 WEATHER CLEAR NO FIRE WARNING. GENERATOR WENT OFF LINE, OIL PRESS LIGHT ON, IGNITION OFF, FUEL FEED NOT CHANGED, WINDMILLING OIL PRES - [SDR IXX2008F00097](https://openairdocs.org/sdr/IXX2008F00097.md): Engine · flamed out · Sep 16, 2008 · N823BX · Doug DC871F · Engine (Turbine/Turboprop) > DURING CRUISE, AT 36,000 FT WITH POWER REDUCTION NR 2 ENGINE FLAMED OUT WITH 1-2 PSI OIL PRESSURE ATTEMPTED INFLIGHT RESTART, NO FUEL FLOW AND NO IGNITION. THE CREW PERFORMED INFLIGHT ENGINE SHUTDOWN PROCEDURE. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINT I - [SDR IXX2008F00096](https://openairdocs.org/sdr/IXX2008F00096.md): Engine · flamed out · Sep 16, 2008 · N823BX · Doug DC871F · Engine (Turbine/Turboprop) > DURING CRUISE AT 36,000 FT WITH POWER REDUCTION NR 2 ENGINE FLAMED OUT, WITH 1-2 PSI OIL PRESSURE ATTEMPTED INFLIGHT RESTART, NO FUEL FLOW AND NO IGNITION. THE CREW PERFORMED INFLIGHT ENGINE SHUTDOWN PROCEDURE. THE CREW LANDED WITHOUT FURTHER INCIDENT. OPEN ( - [SDR IXX2008F00095](https://openairdocs.org/sdr/IXX2008F00095.md): Fire Warning · malfunctioned · Sep 11, 2008 · N823BX · Doug DC871F · Fire Detection > DURING CRUISE, NR 2 FIRE WARNING CAME ON INTERMITTENTLY. THE CREW SHUTDOWN NR 2 ENGINE, WAS UNABLE TO ACCOMPLISH FIRE WARNING TEST. THE CREW DISCHARGED 1 FIRE BOTTLE, ACCOMPLISHED FIRE WARNING TEST. SEVERAL MINUTES LATER NR 2 FIRE WARNING CAME ON AGAIN, THE - [SDR IXXA08SMN186S](https://openairdocs.org/sdr/IXXA08SMN186S.md): Finger Doubler · corroded · Jun 5, 2008 · N823BX · Doug DC871F · Fuselage Main, Structure > DURING ROUTINE D CHECK INSPECTION, FOUND TOP SURFACE OF MAIN LANDING GEAR WHEEL WELL PRESSURE PANEL FINGER DOUBLER CORRODED AT STATION 941.000 TO STATION 958.000 LEFT BOTTOM LINE 5 TO RIGHT BOTTOM LINE 5. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FING - [SDR IXXA060216O](https://openairdocs.org/sdr/IXXA060216O.md): Transceiver · faulty · Jun 7, 2006 · N823BX · Doug DC871F · Weather Radar System > APPROXIMATELY ONE HOUR INTO CRUISE FROM KMIA TO SKCL, THE WEATHER RADAR INDICATED WEAK SIGNAL THEN STARTED SPOKING AND SPOTTING. AT ONE HOUR AND TEN MINUETS INTO FLIGHT THE WEATHER RADAR WENT COMPLETELY GREEN. THE CREW ELECTED TO RETURN TO KMIA AND PERFORMED - [SDR IXXA06RNG048S](https://openairdocs.org/sdr/IXXA06RNG048S.md): Skin · corroded · May 18, 2006 · N823BX · Doug DC871F · Horizontal Stabilizer, Plate/Skin > DURING ROUTINE C CHECK, FOUND CORROSION ON HORIZONTAL STABILIZER UPPER SKIN LEADING EDGE FROM STATION XFS 178.00 TO STATION 203.750 TO THE RIGHT HAND REAR. DAMAGED AREA WAS CLEANED AND EXTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 55-018. - [SDR IXXA06RNG046S](https://openairdocs.org/sdr/IXXA06RNG046S.md): Skin · corroded · May 3, 2006 · N823BX · Doug DC871F · Leading Edge Devices > DURING ROUTINE C CHECK FOUND CORROSION OUT OF LIMITS ON INBOARD EXTENDED LEADING EDGE UPPER SKIN, STATION XFS 13.750 - 20.000 RIGHT. PERMANENT REPAIR WAS PERFORMED IAW EWO ATI 57-084. - [SDR IXXA06RNG047S](https://openairdocs.org/sdr/IXXA06RNG047S.md): Panel · misaligned · Apr 26, 2006 · N823BX · Doug DC871F · Wing, Plate/Skin > DURING ROUTINE C CHECK, FOUND SLOT PANEL AFT HOLES DO NOT ALIGN UP WITH THE HOLES IN THE WING ON CENTER EXTENDED LEADING EDGE AROUND LOWER SKIN RIGHT HAND. DAMAGED AREA WAS CLEANED, REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW EWO ATI 57-085. - [SDR IXXA06RNG044S](https://openairdocs.org/sdr/IXXA06RNG044S.md): Skin · misrepaired · Apr 20, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK, FOUND AN IMPROPER REPAIR AT STATION 1430, LONGERON 34 RIGHT, EXTERNAL DOUBLER BELOW D-PIT DOOR OPENING. ALSO AT FUSELAGE LOWER SECTION SKIN, FROM STATION 1360 TO 1580, LONGERON 36 TO 31 RIGHT AND LEFT FOUND CORROSION. REMOVED AND REPL - [SDR IXXA06RNG045S](https://openairdocs.org/sdr/IXXA06RNG045S.md): Repair · improper · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLERS EXTERNAL SKIN, STA 78 LONGERON 35.5 RT. REMOVED IMPROPER REPAIR, REMOVED DAMAGE, CLEANED, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND CUT OUT AND NO CRACKS FOUND, REPAIR DOUBLERS AND - [SDR IXXA060473S](https://openairdocs.org/sdr/IXXA060473S.md): Repair · improper · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 1696 LONGERON 16.5 LEFT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FINGE - [SDR IXXA060472S](https://openairdocs.org/sdr/IXXA060472S.md): Repair · improper · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 1696 LONGERON 16.5 RIGHT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FING - [SDR IXXA060471S](https://openairdocs.org/sdr/IXXA060471S.md): Repair · improper · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 1705 LONGERON 36. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FINGER DOUBL - [SDR IXXA060470S](https://openairdocs.org/sdr/IXXA060470S.md): Repair · improper · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 1694 LONGERON 35 RIGHT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FINGER - [SDR IXXA060469S](https://openairdocs.org/sdr/IXXA060469S.md): Repair · improper · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 555 LONGERON 35.5 LEFT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FINGER - [SDR IXXA060468S](https://openairdocs.org/sdr/IXXA060468S.md): Repair · improper · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 1394 LONGERON 35.75 RIGHT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FIN - [SDR IXXA060467S](https://openairdocs.org/sdr/IXXA060467S.md): Repair · improper · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 1280 LONGERON 35.75 LEFT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FING - [SDR IXXA060465S](https://openairdocs.org/sdr/IXXA060465S.md): Repair · improper · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 1143 LONGERON 35.75 RIGHT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FIN - [SDR IXXA060466S](https://openairdocs.org/sdr/IXXA060466S.md): Repair · improper · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 615 LONGERON 36. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FINGER DOUBLE - [SDR IXXA060464S](https://openairdocs.org/sdr/IXXA060464S.md): Repair · improper · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 546 LONGERON 35.75 RIGHT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FING - [SDR IXXA060463S](https://openairdocs.org/sdr/IXXA060463S.md): Repair · improper · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 404 LONGERON 35.75 RIGHT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FING - [SDR IXXA060462S](https://openairdocs.org/sdr/IXXA060462S.md): Repair · improper · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 223 LONGERON 35.5 RIGHT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FINGE - [SDR IXXA060460S](https://openairdocs.org/sdr/IXXA060460S.md): Repair · improper · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 105 LONGERON 35.75 RIGHT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FING - [SDR IXXA06RNG036S](https://openairdocs.org/sdr/IXXA06RNG036S.md): Skin · misrepaired · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK, FOUND AN IMPROPER REPAIR ON FUSELAGE SKIN AT STATION 1450 BETWEEN LONGERONS 30 - 31 RIGHT, REPAIR PROXIMITY ISSUE WITH D-PIT DOOR BOTTOM DOUBLER. IMPROPER REPAIR WAS REMOVED, NEW FILLER AND EXTERNAL DOUBLER WERE FABRICATED AND INSTALLE - [SDR IXXA06RNG035S](https://openairdocs.org/sdr/IXXA06RNG035S.md): Skin · misrepaired · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND AN IMPROPER REPAIR ON FUSELAGE SKIN AT STATION 30 BETWEEN LONGERONS 6 - 7 LEFT. IMPROPER REPAIR WAS REMOVED; NEW EXTERNAL DOUBLER AND FINGER DOUBLER WERE FABRICATED AND INSTALLED IAW EWO ATI 53-063. FAA FORM 8110-3 WAS ISSUED APPR - [SDR IXXA06RNG034S](https://openairdocs.org/sdr/IXXA06RNG034S.md): Skin · misrepaired · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND AN IMPROPER REPAIR ON FUSELAGE SKIN AT STATION 54 LONG 28 -30 LEFT. EXISTING REPAIR WAS REMOVED; NEW EXTERNAL DOUBLER & FILLER WERE FABRICATED AND INSTALLED IAW EWO ATI 53-062. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. - [SDR IXXA06RNG033S](https://openairdocs.org/sdr/IXXA06RNG033S.md): Skin · misrepaired · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK, FOUND AN IMPROPER REPAIR ON SKIN AT STATION 1752 LONGERON 16.5 - LEFT. IMPROPER REPAIR WAS REMOVED AND FINGER DOUBLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW EWO ATI 53-060 AND SRM 53-2-5 FIGURE 14A. - [SDR IXXA06RNG032S](https://openairdocs.org/sdr/IXXA06RNG032S.md): Skin · misrepaired · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK AN IMPROPER REPAIR AT PASSENGER WINDOW STATION 1310 LONGERON 16 RIGHT. IMPROPER REPAIR WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED & INSTALLED IAW EWO ATI 53-059 AND SRM 53-2-0 FIGURE 22A. THIS REPAIR CONSTITUTES A MAJOR REPAIR. - [SDR IXXA06RNG031S](https://openairdocs.org/sdr/IXXA06RNG031S.md): Skin · misrepaired · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND TWO IMPROPER REPAIRS ON PASSENGER WINDOW; STATION 1472 LONGERON 16.5 RT AND STATION 1479 LONGERON 14.5 RT. BOTH IMPROPER REPAIRS WERE REMOVED AND PERMANENT REPAIRS WERE PERFORMED IAW EWO ATI 53-058 AND SRM 53-2-0 FIGURE 22A. THIS - [SDR IXXA06RNG030S](https://openairdocs.org/sdr/IXXA06RNG030S.md): Skin · misrepaired · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND AN IMPROPER REPAIR ON PASSENGER WINDOW, AT STATION 1290 LONGERON 17.5- RIGHT HAND.CORRECTIVE ACTION: IMPROPER REPAIR WAS REMOVED AND PERMANENT REPAIR WAS PERFORMED IAW EWO ATI 53-057 AND SRM 53-2-0 FIG 22A. THIS REPAIR CONSTITUTES - [SDR IXXA06RNG029S](https://openairdocs.org/sdr/IXXA06RNG029S.md): Skin · misrepaired · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK, FOUND AN IMPROPER REPAIR ON SKIN OF PASSENGER WINDOW, STATION 1310 LONGERON 16 RIGHT. IMPROPER STRUCTURAL REPAIR AT STATION 1310 LONGERON 16 RIGHT WAS REMOVED AND PERMANENT REPAIR DOUBLER WAS INSTALLED IAW EWO ATI 53-056 AND SRM 53-2-0 - [SDR IXXA06RNG025S](https://openairdocs.org/sdr/IXXA06RNG025S.md): Skin · misrepaired · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Structure (General) > DURING ROUTINE C CHECK, AN IMPROPER REPAIR ON SKIN AT STATION 479, LONGERON 28-RIGHT. DAMAGED SKIN SECTION WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 53-055 AND SRM 53-2-5 FIGURE 14A. THIS REPAIR CONSTITUTES A MAJOR REPAIR. - [SDR IXXA06RNG024S](https://openairdocs.org/sdr/IXXA06RNG024S.md): Skin · misrepaired · Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK, FOUND AN IMPROPER REPAIR AT STATION 282 AT LONGERON 25.5R. DAMAGED SKIN SECTION WAS REMOVED AND EXTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 53-061. - [SDR IXXA06RNG050S](https://openairdocs.org/sdr/IXXA06RNG050S.md): Skin · misrepaired · Apr 18, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR AT STATION 8.00 LONGERON 33 RIGHT. REMOVED EXISTING REPAIR. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS. IAW TAMPA ENGINEERING WORK ORDER EWO ATI 53-052 DA - [SDR IXXA06RNG049S](https://openairdocs.org/sdr/IXXA06RNG049S.md): Skin · misrepaired · Apr 18, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR AT STATION 8.00 LONGERON 33 LT. REMOVED EXISTING REPAIR. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS. IAW TAMPA ENGINEERING WORK ORDER EWO ATI 53-052 DATE - [SDR IXXA060461S](https://openairdocs.org/sdr/IXXA060461S.md): Repair · improper · Apr 18, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 172 LONGERON 35.75 RIGHT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FING - [SDR IXXA060459S](https://openairdocs.org/sdr/IXXA060459S.md): Repair · improper · Apr 16, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 78 LONGERON 35.5 RIGHT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FINGER - [SDR IXXA06RNG022S](https://openairdocs.org/sdr/IXXA06RNG022S.md): Fitting · cracked · Apr 15, 2006 · N823BX · Doug DC871F · Wing, Attach Fittings > DURING ROUTINE C CHECK, FOUND A CRACK ON THE OUTBOARD FLAP STATION XFS 339.723, INBOARD FITTING LEFT HAND. STOP DRILLED THE END OF THE CRACK. REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-075. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. - [SDR IXXA06RNG013S](https://openairdocs.org/sdr/IXXA06RNG013S.md): Skin · improper · Apr 10, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING INSPECTION CHECK FOUND A IMPROPER REPAIR ON PRESSURE SKIN STA 80 TO 10 LONGERON 33 AND 34 RT. IMPROPER REPAIR WAS REMOVED AND NEW REPAIR DOUBLER AND FINGER DOUBLER WERE FABRICATED AND INSTALLED IAW EWO ATI 53-050 AND SRM 53-2-5 FIGURE 14A. - [SDR IXXA06RNG018S](https://openairdocs.org/sdr/IXXA06RNG018S.md): Skin · misrepaired · Apr 9, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING INSPECTION CHECK FOUND TWO IMPROPER REPAIRS ON NOSE SKIN AT STA 8 LONGERON 33 RT AND STA 8 LONGERON 33 LT. DAMAGED SKIN SECTION WAS REMOVED AND EXTERNAL DOUBLER WERE FABRICATED AND INSTALLED IAW EWO ATI 53-052. FAA FORM 8110-3 WAS ISSUED APPROVING THI - [SDR IXXA06RNG014S](https://openairdocs.org/sdr/IXXA06RNG014S.md): Skin · misrepaired · Apr 9, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING INSPECTION CHECK FOUND A IMPROPER REPAIR ON PRESSURE SKIN STA 460 TO 480 LONGERON 30 - 31 RT. PERMANENT REPAIR WAS PERFORMED BY FABRICATING AND INSTALLING DOUBLER AND FINGER DOUBLER IAW EWO ATI 53-049 AND SRM 53-2-5 FIGURE 14A. - [SDR IXXA06RNG052S](https://openairdocs.org/sdr/IXXA06RNG052S.md): Rib · cracked · Apr 8, 2006 · N823BX · Doug DC871F · Wing, Rib/Bulkhead > DURING ROUTINE C CHECK FOUND LT WING TRAILING EDGE UPPER RIB CRACKED AT STA XOLID 6.225. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED, REPAIR PARTS. IAW TAMPA ENGINEERING WORK ORDER EWO ATI 57-081 DATED MAY - [SDR IXXA06RNG051S](https://openairdocs.org/sdr/IXXA06RNG051S.md): Rib · cracked · Apr 8, 2006 · N823BX · Doug DC871F · Wing, Rib/Bulkhead > DURING ROUTINE C CHECK FOUND LT WING TRAILING EDGE UPPER RIB CRACKED AT STATION XFS 304.0. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED, REPAIR PARTS. IAW TAMPA ENGINEERING WORK ORDER EWO ATI 57-077 DATED A Next page: https://openairdocs.org/deregistered/N823BX-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 = 'N823BX' AND deregistration_id = 'N823BX-2014-04-14' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N823BX-2014-04-14/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.