# Service difficulty reports: N828BX, cancelled May 1, 2014

A list on [N828BX, cancelled May 1, 2014](https://openairdocs.org/deregistered/N828BX-2014-05-01.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 · 147 reports

- [SDR IXXA110003S](https://openairdocs.org/sdr/IXXA110003S.md): Skin · cracked · Jan 14, 2011 · N828BX · Doug DC871F · Wing, Plate/Skin
  > DURING SKIN INSP FOR AD 2008-26-07, FOUND A.5 INCH CRACK ON LT WING LOWER SKIN AT STRINGER 58. MX PERFORMED INSP FOR FERRY FLIGHT FOR PERMANENT STORAGE IAW GMM 3.117.
- [SDR IXXA100015O](https://openairdocs.org/sdr/IXXA100015O.md): Plug · unsecure · Feb 16, 2010 · N828BX · Doug DC871F · Turbine Engine Oil System
  > DURING CRUISE, THE CREW SHUTDOWN NR 1 ENG DUE TO LOSS OF OIL QUANTITY. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND THE STARTER FILLER PLUG OFF. THEY REINSTALLED FILLER PLUG AND LOCKED SERVICED ENGINE. OPS CHECK GOOD IAW AMM 80-10, AMM 12-10.
- [SDR IXXA090042O](https://openairdocs.org/sdr/IXXA090042O.md): Fuel Control · out of rig · Aug 27, 2009 · N828BX · Doug DC871F · Fuel Controlling System
  > DURING TAKEOFF, NR 4 ENG WOULD NOT MAKE PWR. ONCE AIRBORNE HAD TO PUSH THROTTLE PAST OTHER THROTTLES NR 4 EGT WENT TO 907 DEGREE. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED NR 4 ENG AND FOUND VSV'S AND VBV OUT OF RIG. MX ACCOMPLIS
- [SDR IXXA090041S](https://openairdocs.org/sdr/IXXA090041S.md): Tee Fitting · cracked · Aug 24, 2009 · N828BX · Doug DC871F · Fuselage Main, Bulkhead
  > DURING INSP IAW AD2007-21-18 AND SB DC8-53A081 FOUND RT AFT PRESSURE BULKHEAD TEE FITTING CRACKED. STOP DRILLED CRACK IAW SRM 53-2-5.
- [SDR IXXA080035O](https://openairdocs.org/sdr/IXXA080035O.md): Connector · defective · Dec 8, 2008 · N828BX · Doug DC871F · Engine Oil System Wiring
  > DURING CRUISE FROM KTOL NUMBER THREE ENGINE OIL PRESSURE STABILIZED AT 50 PSI THEN FLUCTUATED BETWEEN 20-60 PSI FOR A SHORT TIME, THEN STABILIZED AGAIN AT 50 PSI. THE CREW RETURNED TO KTOL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED OIL PRESSUR
- [SDR IXXA080028O](https://openairdocs.org/sdr/IXXA080028O.md): Wire · broken · Oct 21, 2008 · N828BX · Doug DC871F · Navigation System Wiring
  > DURING TAKEOFF FROM KTOL F/O'S FLIGHT DIRECTOR FLAG IN ADI AND GYRO FLAG CAME IN VIEW. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS. MAINTENANCE SMART BOX WIRE NUMBER 2TN49B22 BROKEN AT R50-972 PIN 35. MAINTENANCE REPAIRED WIRE 2TN49B22. OPERATIONAL CH
- [SDR IXXA080027O](https://openairdocs.org/sdr/IXXA080027O.md): Comparator · defective · Oct 21, 2008 · N828BX · Doug DC871F · Integrated Flight System
  > DURING CLIMBOUT FROM KTOL, CAPT'S RMI, GYRO FLAG, AND F/O'S GLIDESLOPE IN HSI, FLIGHT DIRECTOR IN ASI FLAG ALL IN VIEW. THE CREW RETURNED TO KTOL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED SMART BOX. OPERATIONAL CHECK GOOD IAW DC8 MAINTENANCE
- [SDR IXX2008F00094](https://openairdocs.org/sdr/IXX2008F00094.md): Connector · damaged · Sep 6, 2008 · N828BX · Doug DC871F · Fire Protection System Wiring
  > DURING CRUISE, NR (2) FIRE WARNING LIGHT CAME ON STEADY, THE CREW SHUTDOWN NR (2) ENGINE AND DISCHARGED (1) FIRE BOTTLE, LIGHT WENT OUT. (20 MINUTES OUT, NR (2) FIRE WARNING LIGHT CAME BACK ON MOMENTARILY AND FIRE LOOPS WOULD ONLY TEST INTERMITTENTLY, THE CR
- [SDR IXX2008F00022](https://openairdocs.org/sdr/IXX2008F00022.md): Fire Detector · false activation · Jul 16, 2008 · N828BX · Doug DC871F · Fire Detection
  > FLT ATN 819/KDFW TO KTOL/TAT 87593/TAC 36428. DURING CLIMBOUT FROM KDFW NR 4 FIRE WARNING LIGHT CAME ON, THE CREW SHUTDOWN NR 4 ENGINE AND DISCHARGED BOTH FIRE BOTTLES THE LIGHT REMAINED ON. THE CREW RETURNED TO KDFW AND LANDED WITHOUT INCIDENT. MAINTENANCE
- [SDR DHL2008F00016](https://openairdocs.org/sdr/DHL2008F00016.md): Fire Warning · activated · Jul 16, 2008 · N828BX · Doug DC871F · Fire Detection
  > FLT NR ATN 819 / KDFW TO KTOL. DURING CLIMBOUT FROM KDFW NR 4 ENGINE FIRE WARNING LIGHT CAME ON, THE CREW DISCHARGED BOTH FIRE BOTTLES AND LIGHT REMAINED ON. THE CREW RETURNED TO KDFW AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION IN WORK. (A)
- [SDR IXXA080006O](https://openairdocs.org/sdr/IXXA080006O.md): Fire Loop · loose · Feb 19, 2008 · N828BX · Doug DC871F · Fire Detection
  > DURING CRUISE FROM KPHL TO KTOL, NUMBER FOUR ENGINE SHORT LIGHT CAME ON WITH NO FIRE TEST INDICATION, THE CREW ACCOMPLISHED EMERGENCY PROCEDURES AND SHUT DOWN NUMBER FOUR ENGINE. THE CREW LANDED AT KTOL WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND RIGHT
- [SDR IXXA070051O](https://openairdocs.org/sdr/IXXA070051O.md): Fire Loop · false activation · Oct 5, 2007 · N828BX · Doug DC871F · Fire Detection
  > DURING CRUISE FROM KTOL TO KMCI, NR 4 ENGINE WAS SHUT DOWN FOR A SHORT CIRCUIT LIGHT ON WITH NO FIRE LIGHT OR ALARM BELL DURING TEST. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED NUMBER 4 FIRE LOOPS, NO DEFECTS NOTED. OPERATIONAL CHECK WAS GOOD.
- [SDR IXXA070050O](https://openairdocs.org/sdr/IXXA070050O.md): Relay · failed · Oct 3, 2007 · N828BX · Doug DC871F · Fire Detection
  > THIRTY MINUTES AFTER TAKEOFF FROM KTOL NR 4 FIRE WARNING LIGHT CAME ON, THE CREW DISCHARGED BOTH NR 4 ENGINE FIRE BOTTLES INTO ENGINE, THE FIRE WARNING LIGHT WENT OUT AFTER THE SECOND BOTTLE WAS DISCHARGED. 5 MINUTES LATER FIRE WARNING WAS INTERMITTENT, NR 4
- [SDR IXXA070049O](https://openairdocs.org/sdr/IXXA070049O.md): Fire Loop · defective · Oct 2, 2007 · N828BX · Doug DC871F · Fire Detection
  > DURING CLIMB-OUT FROM KTOL, THE CREW NOTICED NUMBER 4 FIRE WARNING LIGHT WAS INTERMITTENT. THE CREW RETURNED TO KTOL WITHOUT INCIDENT. MAINTENANCE INSPECTED NUMBER FOUR FIRE WARNING SYSTEM AND REPLACED LEFT AFT FIRE LOOP, OPERATIONAL CHECK WAS GOOD IAW DC8 M
- [SDR IXXA07SMN153S](https://openairdocs.org/sdr/IXXA07SMN153S.md): Skin · misrepaired · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT AFT FUSELAGE SKIN PANEL AND SKIN SPLICES OF LONGERON 27 LEFT AT STATION 1699. REMOVED EXISTING EXTERNAL REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN, EXT
- [SDR IXXA07SMN154S](https://openairdocs.org/sdr/IXXA07SMN154S.md): Floorbeam · corroded · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Floor Beam
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FLOORBEAM WEB CORRODED AT STATION 960.000 RT BOTTOM LINE 40". REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, REMOVED CORROSION. FOUND OUT OF LIMIT. FABRICATE REPAIR ANGLES OF EXTRUSION. CLEANE
- [SDR IXXA07SMN155S](https://openairdocs.org/sdr/IXXA07SMN155S.md): Fitting · corroded · Apr 21, 2007 · N828BX · Doug DC871F · Wing Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD SLOT VANE FITTING WITH CORROSION AT STATION XILD 0.7095. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. FABRICATED NEW FITTING. CLEANED, TREATED AND PRIMED AREA AND FITTING. AP
- [SDR IXXA07SMN156S](https://openairdocs.org/sdr/IXXA07SMN156S.md): Skin · corroded · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT AFT FUSELAGE SKIN PANEL AND SKIN SPLICES OF LONGERON 28RIGHT AT STATION 1690. REMOVED EXISTING EXTERNAL REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN,
- [SDR IXXA07SMN143S](https://openairdocs.org/sdr/IXXA07SMN143S.md): Doubler · cracked · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND EXTERNAL FUSELAGE NOSE SECTION RIGHT AFT PRIMARY HEAT INTERCHANGER AFT LOWER CORNER DOUBLER CRACKED AT STATION -12 LONGERON 27 RIGHT. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER. CLEANED TREATED AND PRIMED ARE
- [SDR IXXA07SMN142S](https://openairdocs.org/sdr/IXXA07SMN142S.md): Skin · misrepaired · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR LOCATED AT FS 1725 LONGERON 16.5 RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT T
- [SDR IXXA07SMN138S](https://openairdocs.org/sdr/IXXA07SMN138S.md): Longeron · misrepaired · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR INSTALLED AT A-PIT BASKET DOOR, RIGHT FORWARD JAMB CORNER AT STATION 293 LONGERON 30 RIGHT. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER, TRIPLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PAR
- [SDR IXXA07SMN137S](https://openairdocs.org/sdr/IXXA07SMN137S.md): Longeron · misrepaired · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR INSTALLED AT A-PIT BASKET DOOR, RIGHT AFT JAMB CORNER AT STATION 327 LONGERON 30 RIGHT. REMOVED EXISTING REPAIR. FABRICATED DOUBLER, TRIPLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED
- [SDR IXXA07SMN140S](https://openairdocs.org/sdr/IXXA07SMN140S.md): Longeron · misrepaired · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, IMPROPER REPAIR LOCATED AT STATION 1581 LONGERON 23 RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN, EXTERNAL DOUBLER, AND INTERNAL DOUBLER. C
- [SDR IXXA07SMN139S](https://openairdocs.org/sdr/IXXA07SMN139S.md): Longeron · misrepaired · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION 445, LONGERON 27.5 RIGHT. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, EXTERNAL DOUBLER AND INTERNAL DOUBLER, CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SU
- [SDR IXXA070029S](https://openairdocs.org/sdr/IXXA070029S.md): Skin · misrepaired · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT AFT FUSELAGE SKIN PANEL AND SKIN SPLICES OF LONGERON 28 RIGHT AT STATION 1690. REMOVED EXISTING EXTERNAL REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN,
- [SDR IXXA07SMN135S](https://openairdocs.org/sdr/IXXA07SMN135S.md): Skin · misrepaired · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT AFT FUSELAGE SKIN PANEL AND SKIN SPLICES OF LONGERON 28 LEFT AT STATION 1690. REMOVED EXISTING EXTERNAL REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN,
- [SDR IXXA07SMN141S](https://openairdocs.org/sdr/IXXA07SMN141S.md): Longeron · misrepaired · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR LOCATED AT STATION 1.600 LONGERON 28 RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN, EXTERNAL DOUBLER, INTERNAL DOUB
- [SDR IXXA07SMN146S](https://openairdocs.org/sdr/IXXA07SMN146S.md): Skin · cracked · Apr 21, 2007 · N828BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP CRACKED ON UPPER PART EXTERNAL COATING AT STATION XW 104.00. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT
- [SDR IXXA07SMN150S](https://openairdocs.org/sdr/IXXA07SMN150S.md): Frame · cracked · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Frame
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FRAME FLANGE WITH A CRACK AT STATION 1580.000 LONGERON 21LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED FRAME SEGMENT. FABRICATED NEW FRAME SEGMENT. PERFORMED HEAT TREATM
- [SDR IXXA07SMN158S](https://openairdocs.org/sdr/IXXA07SMN158S.md): Frame · cracked · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Frame
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FRAME WITH A CRACK AT STATION 1260.000 LONGERON 34 RIGHT TO LONGERON 35 LEFT. REMOVED CRACKED FITTING. FABRICATED FRAME FITTING, SPLICES, AND DOUBLER. PERFORMED HEAT TREATMENT. PERFORMED NDT IN
- [SDR IXXA07SMN144S](https://openairdocs.org/sdr/IXXA07SMN144S.md): Hook · cracked · Apr 21, 2007 · N828BX · Doug DC871F · Passenger/Crew Doors
  > DURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE AT NOSE SECTION FORWARD PAX DOOR HOLD OPEN HOOK, WAS CRACKED AT STATION 15.000 LONGERON 16 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM THE REPAIR. REMOVED DAMAGED AREA. PERFORMED INSPECTION NDT IN
- [SDR IXXA07SMN136S](https://openairdocs.org/sdr/IXXA07SMN136S.md): Fitting · corroded · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage, Landing Gear Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR WHEEL WELL JOINT FITTING WITH CORROSION AT STATION 940.000 LONGERON 24 RIGHT. REMOVED CORROSION. FOUNDED OUT OF LIMITS REMOVED CORRODED FITTING. FABRICATED FRAME FITTING, SPLICES AND DOUBLER.
- [SDR IXXA07SMN145S](https://openairdocs.org/sdr/IXXA07SMN145S.md): Fitting · corroded · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND BATH TUB FITTING CORRODED, BETWEEN STATION 70.000 AND STATION 80.000 LONGERON 35 RIGHT. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW D
- [SDR IXXA07SMN147S](https://openairdocs.org/sdr/IXXA07SMN147S.md): Skin · dented · Apr 21, 2007 · N828BX · Doug DC871F · Elevator, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR. UPPER SKIN DENT WITH CRACK AT STATION XE 156.468 AND STATION XE 161.375. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL REPAIR PARTS. BONDED PART
- [SDR IXXA07SMN148S](https://openairdocs.org/sdr/IXXA07SMN148S.md): Longeron · cracked · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TAIL SECTION LONGERON 17 RIGHT HAND, WITH A CRACK AT STATION 1766.000 TO STATION 1794.000. REMOVED CRACKED LONGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW LONGERON IAW DC8 SRM 53-5-1 PAGE 22 FIGURE
- [SDR IXXA07SMN149S](https://openairdocs.org/sdr/IXXA07SMN149S.md): Longeron · cracked · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TAIL SECTION LONGERON 17 LEFT HAND, WITH A CRACK AT STATION 1766.000 TO STATION 1794.000. REMOVED CRACKED LONGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW LONGERON IAW DC8 SRM 53-5-1 PAGE 22 FIGURE
- [SDR IXXA07SMN152S](https://openairdocs.org/sdr/IXXA07SMN152S.md): Fitting · corroded · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAD CORROSION ON FITTING ABOVE MAIN LANDING GEAR WHEEL WELL CEILING BETWEEN STATION 960.000 - 980.000 LEFT BOTTOM LINE 40”. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CL
- [SDR IXXA07SMN151S](https://openairdocs.org/sdr/IXXA07SMN151S.md): Fitting · corroded · Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, IN MAIN CARGO COMPARTMENT, FOUND CORROSION ON FITTING ABOVE MAIN LANDING GEAR WHEEL WELL CEILING BETWEEN STATION 960.000 - 980.000 RIGHT BOTTOM LINE 40". REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. C
- [SDR IXXA07SMN157S](https://openairdocs.org/sdr/IXXA07SMN157S.md): Skin · misrepaired · Apr 21, 2007 · N828BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN HAD A NON STANDARD REPAIR AT STATION XFS 426.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA PERFORMED NDT INSPECTION. NO CRACK OR CORROSION AFTER NDT TEST.
- [SDR IXXA07SMN159S](https://openairdocs.org/sdr/IXXA07SMN159S.md): Fitting · cracked · Apr 11, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO BILGE INTERIOR FITTING CRACKED AT STATION 1260.000 LONGERON33 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. CLEANED TREATED AND PRIMED
- [SDR IXXA07SMN160S](https://openairdocs.org/sdr/IXXA07SMN160S.md): Fitting · cracked · Apr 11, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO BILGE INTERIOR FITTING CRACKED AT STATION 1260.000 LONGERON 35 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING PERFORMED NDT. NO CRACK OR CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND REP
- [SDR IXXA060609O](https://openairdocs.org/sdr/IXXA060609O.md): Oil Filter · dirty · Nov 8, 2006 · N828BX · Doug DC871F · Turbine Engine Oil System
  > DURING CRUISE FROM KTOL TO KSJC, NUMBER 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED ALL OTHER PARAMETERS WERE NORMAL. THE CREW SHUTDOWN THE ENGINE AND CONTINUED TO KSJC WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND TH
- [SDR IXXA060172O](https://openairdocs.org/sdr/IXXA060172O.md): Fire Detector · shorted · Mar 9, 2006 · N828BX · Doug DC871F · Fire Detection
  > AT CRUISE FL 36.0 NR 3 ENGINE SHORT CIRCUIT LIGHT BEGAN FLASHING. FIRE WARNING WOULD NOT TEST, ENGINE SHUTDOWN PER COM PROCEDURE. THE CREW ELECTED TO RETURN THE AIRCRAFT TO TOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED CONNECTOR FROM FORWARD SIDE OF
- [SDR IXXA060171O](https://openairdocs.org/sdr/IXXA060171O.md): Connector · corroded · Feb 28, 2006 · N828BX · Doug DC871F · Fire Protection System Wiring
  > DURING FLIGHT 834 FROM TOL TO SJC APROX 50 MIN INTO FLIGHT, NR 3 ENG SHORT CIRCUIT AMBER LIGHT CAME ON. PERFORMED ABNORMAL CHECK LIST. THE LIGHT DID NOT EXTINGUISH, NOR DID THE FIRE WARNING TEST. PERFORMED ENGINE SHUTDOWN OTHER THAN FIRE DAMAGE. THE CREW E
- [SDR IXXA0600037O](https://openairdocs.org/sdr/IXXA0600037O.md): Sensing Element · defective · Jan 17, 2006 · N828BX · Doug DC871F · Fire Detection
  > ON FLIGHT ATN833 FROM KSJC TO KRFD, NR 3 ENGINE FIRE WARNING LIGHT AND BELL CAME ON DESCENT TO KRFD. COMPLY WITH COMPANY PROCEDURES WIND MILLING TIME 30 MINUTES AND OIL PRESSURE WAS 20 PSI. CREW ELECTED TO LAND AT KTOL AND LANDED WITHOUT INCIDENT. MAINTENAN
- [SDR IXXA0500215O](https://openairdocs.org/sdr/IXXA0500215O.md): Radio · malfunctioned · Dec 27, 2005 · N828BX · Doug DC871F · HF Communications System
  > ON FLIGHT 362 FROM KTOL TO KEWR NR 1 HF CONTINOUSLY ATTEMPTED TO TUNE ON ALL FREQUENCES WITH THE SAME RESULTS. THEN HF RADIO NR 2 WAS KEYED TO TUNE, THE AUTOPILOT KICKED OFF CAUSING THE AIRCRAFT TO YAW AND PITCH. DUE TO INTENDED FLIGHT PLAN, CREW ELECTED TO
- [SDR IXXA0500118O](https://openairdocs.org/sdr/IXXA0500118O.md): Bulb · loose · Nov 22, 2005 · N828BX · Doug DC871F · Engine Indicating System
  > DURING A TAKEOFF ROLLOUT AT 110KTS, NR 3 ENGINE OIL PRESSURE LIGHT CAME ON. TAKEOFF WAS REJECTED. OIL PRESSURE AND QUANTITY INDICATED NORMAL BUT LIGHT REMAINED ON UNTIL THE ENGINE WAS SHUTDOWN. CREW RETURNED TO BLOCKS. MAINTENANCE DEFERRED THIS IAW MEL 79-6 (C
- [SDR IXXA0500104O](https://openairdocs.org/sdr/IXXA0500104O.md): Blade · leaking · Aug 23, 2005 · N828BX · Doug DC871F · Turbine Engine Oil System
  > NR 2 ENG SHUTDOWN FOR LOSS OF OIL QTY. OIL PRESS DROPPED. OIL TEMP STABLE. SHUTDOWN NR 2 ENG. WINDMILL OIL PRESS DROPPED & QTY INCREASED. TEMP STABLE. NO WINDMILLING PRESS. LOW PRESS LIGHT ILLUM. LANDED W/OUT INCIDENT. R&R NR 2 ENG, OPS & LEAK CHK GOOD. ACFT
- [SDR IXXA0500103O](https://openairdocs.org/sdr/IXXA0500103O.md): Engine · malfunctioned · Aug 19, 2005 · N828BX · Doug DC871F · Engine (Turbine/Turboprop)
  > DURING CRUISE FROM KPHL TO KTOL THE NR 2 ENGINE FLUCTUATED EGT FOLLOWED BY A INSTANTANEOUS EGT TEMPERATURE INCREASE. OIL PRESSURE FLUCTUATED BUT NO LOSS. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN THEN LANDED IN KTOL WITHOUT INCIDENT. AN INSPECTION IS
- [SDR IXXA0500097O](https://openairdocs.org/sdr/IXXA0500097O.md): Tube · broken · Aug 18, 2005 · N828BX · Doug DC871F · Engine Oil System (Airframe Furnished)
  > !DURING CLIMBOUT FROM KTOL TO KPHL THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. PRESSURE WAS AT 14 PSI AND FLUCTUATING AND OIL QUANTITY DEPLETING SLOWLY. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. CREW LANDED IN KPHL WITHOUT INCIDENT. MAINTENA

Next page: https://openairdocs.org/deregistered/N828BX-2014-05-01/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 = 'N828BX' AND deregistration_id = 'N828BX-2014-05-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N828BX-2014-05-01/reports

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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.