N825BX, cancelled May 1, 2014

Service difficulty reports · 249

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 = 'N825BX' AND deregistration_id = 'N825BX-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 IXX2008F00098Hydraulic System · lowDURING CRUISE FROM KSJC TO KRFD, FLT ENGINEER NOTICED HYDRAULIC QUANTITY INDICATOR WAS AT THE BOTTOM OF NORMAL QUANTITY, DID NOT DROP ANY FURTHER DURING THE REST OF THE FLT. THE CREW LANDED IN KTOL WITHOUT FURTHER INCIDENT. MX SERVICED HYDRAULIC SYS, OPS CHESep 23, 2008 · N825BX · Doug DC871F · Hydraulic System, MainSDR IXX2008F00091Hose · leakingAT TOP OF DECENT, THE ACFT LOST HYDRAULIC FLUID DOWN TO THE STAND PIPE. MAINT INSPECTED AND FOUND NR 3 ENGINE HYDRAULIC PUMP HOSE LEAKING, REPLACED NR 3 ENGINE HYDRAULIC PUMP HOSE. OPS CHECK GOOD IAW MM 29-16. AC WAS RETURNED TO SERVICE. (K)Aug 29, 2008 · N825BX · Doug DC871F · Hydraulic System, MainSDR IXX2008F00090Hydraulic System · failedAT TOP OF DECENT, THE ACFT LOST HYDRAULIC FLUID DOWN TO THE STAND PIPE. OPEN. (K)Aug 28, 2008 · N825BX · Doug DC871F · Hydraulic System, MainSDR IXX2008F00009Switch · brokenDURING CLIMB-OUT, OVER RIDE TOGGLE SWITCH BROKE OFF. AIRCRAFT RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED OVER RIDE SWITCH; OPS CHECK GOOD IAW UAL MM 74-20-36. (K)Jun 26, 2008 · N825BX · Doug DC871F · Electrical Power SystemSDR IXXA06SMN329SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER SKIN HAS NON STANDARD REPAIR AT STATION XW104.000. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN (AL 2024 T3 0.040”). CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNOct 6, 2006 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN320SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NR 4 ALTERNATE TANK CRACKED AT STATION XW485.000, CONFIRMED WITH NDT. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED TREATED AND PSep 25, 2006 · N825BX · Doug DC871F · Wing, Plate/SkinSDR IXXA06SMN321SFitting · crackedDURING ROUTINE C-CHECK INSPECTION FOUND FITTING CRACKED AT STA 1212.000 LONGERON 29 RT. REPLACED FITTING AT STA 1212.000 LONGERON 29 RT. IAW SRM 51-1-20D.Sep 25, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN323SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR UPPER SKIN HAS NON STANDARD REPAIR FROM STATION XE116.000 TO STATION XE79.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED BOTH PARTS WITH HYSOL IAW DSep 25, 2006 · N825BX · Doug DC871F · Elevator, Plate/SkinSDR IXXA06SMN325SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD FLAP LEADING EDGE UPPER SKIN WITH NON STANDARD REPAIR AT STATION XF211.000. REMOVED SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFACSep 25, 2006 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN326SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING OUTBOARD FLAP UPPER SKIN WITH NON STANDARD REPAIR AT STATION XF445.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PSep 25, 2006 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN327SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD FLAP UPPER SKIN WITH NON STANDARD REPAIR AT STATION XF360.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN, AND DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED ANDSep 25, 2006 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN319SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD AILERON LEADING EDGE SKIN CRACKED AT STATION XD525.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFACE. APPLIED SEALANT TO FAYING SURFACESep 25, 2006 · N825BX · Doug DC871F · Aileron Control SystemSDR IXXA06SMN328SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD FLAP UPPER SKIN HAS NON STANDARD REPAIR AT STATION XW105.000. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN (AL 2024 T3 0.050”), AND DOUBLER (AL 2024 T3 0.032”). BONDED SKIN AND DOSep 25, 2006 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN318SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND EXISTING DOUBLER IMPROPER AT STATION 600.000 LONGERON 30 RIGHT. REMOVED EXISTING DOUBLER. TRIMMED OUT DAMAGED AREA. FABRICATED EXTERNAL REPAIR DOUBLER (AL 7075 T6 0.125), INTERNAL FINGER DOUBLER (AL 7075 T6 0.050”), Sep 25, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN317SLongeron · corrodedDURING ROUTINE C-CHECK, INSPECTION FOUND LONGERON 32 LT CORRODED AT STA 610.000. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED FASTENERS AND REMOVED DAMAGED SECTION. FABRICATED NEW REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA. APPLIED SEALANT TO FAYING Sep 21, 2006 · N825BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA06SMN316SLongeron · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LONGERON 34 RIGHT CORRODED BETWEEN STATION 1566.000 AND STATION 1766.000. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED FASTENERS AND REMOVED DAMAGED SECTION. FABRICATED NEW REPAIR PARTS. CLEANED, TREATED AND PRIMSep 21, 2006 · N825BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA06SMN315SFrame · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND EXISTING FRAME REPAIR CORRODED AT STA 600 BETWEEN LONGERON 36 AND LONGERON 35 RT. REMOVED EXISTING REPAIR. FABRICATED NEW REPAIR DOUBLER. INTERNAL FINGER DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPASep 21, 2006 · N825BX · Doug DC871F · Fuselage Main, FrameSDR IXXA06SMN313SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND A NON STANDARD REPAIR ON NUMBER 2 PYLON AT STATION XAR0.000. REMOVED EXISTING NON STANDARD REPAIR FROM STATION XAR0.000 TO STATION XE60.000. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. BONDED PARTS WITH HYSOL. Sep 21, 2006 · N825BX · Doug DC871F · Nacelle/Pylon, Plate/SkinSDR IXXA06SMN314SSkin · crackedDURING ROUTINE C CHECK INSPECTION FOUND EXTERNAL SKIN CRACKED AT STATION 405.000, LONGERON 12 RIGHT. CORRECTIVE ACTION: REMOVED FASTENERS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND. CLEANED, TREATED ASep 21, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN312SClamp · improperDURING ROUTINE C CHECK INSPECTION, FOUND ON NUMBER 2 PYLON ACCESS DOOR NUMBER 297, GENERATOR FEEDER CABLES ATTACH CLAMP IMPROPER. REMOVED FASTENERS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, (AL 2024 T3 0.016). BONDED BOTH PARTS WITH HYSOL. CLEANED, Sep 21, 2006 · N825BX · Doug DC871F · Nacelle/Pylon, Attach FittingsSDR IXXA06SMN308SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND FITTING CRACKED STA 1220.000 BETWEEN LONGERON 27 RT AND LONGERON 29 RT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. HEAT TREATED NEW FITTING. PERFORMED NDT INSPECTION, NO CRACKS FOUND. CLEANED, TREATED AND PRISep 18, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN310SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT MAIN LANDING GEAR LEFT TRAPEZOIDAL FITTING WEB CRACKED AT STATION 902.000. REMOVED CRACKED TRAPEZOIDAL FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW TRAPEZOIDAL FITTING AND REINSTALLED INBOARD AND OUTSep 18, 2006 · N825BX · Doug DC871F · Fuselage, Landing Gear Attach FittingsSDR IXXA06SMN309SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FRAME FITTING CRACKED AT STATION FS 1160.000 LONGERON 27 RIGHT RBL 44. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. HEAT TREATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. CLEANED, TRSep 18, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN307SFitting · crackedDURING ROUTINE C-CHECK INSPECTION FOUND A CRACKED FITTING AT STATION 1260.000 LONGERON 35 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING (AL PLATE 7075 T6 51). PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA, AND FITTING. INSTALLED FITTING. IAW Sep 18, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN311SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND NON STANDARD REPAIR ON THE LEFT HAND SIDE OF THE RUDDER FROM STATION ZR 178.000 TO STATION ZR 188.781. REMOVED SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN (AL 2024 T3 0.040). CLEANED, TREATED, AND PRIMED AREA, Sep 18, 2006 · N825BX · Doug DC871F · Rudder, Plate/SkinSDR IXXA06SMN306SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR RIGHT HAND TRAPEZOIDAL FITTING OUTBOARD FLANGE CRACKED, AT STATION 902.000. REMOVED CRACKED TRAPEZOIDAL FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW TRAPEZOIDAL FITTING AND OUTBOARSep 15, 2006 · N825BX · Doug DC871F · Fuselage, Landing Gear Attach FittingsSDR IXXA06SMN300SSkin · crackedDURING ROUTINE C CHECK INSPECTION FOUND EXTERNAL SKIN CRACKED AT STATION -12 LONGERON 27 LEFT. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN305SFitting · crackedDURING ROUTINE C-CHECK INSPECTION FOUND A CRACKED FITTING AT STATION 240.000 LONGERON 36. REMOVED CRACKED FITTING. FABRICATED FITTING (AL PLATE 7075 T6 51). PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA, AND FITTING.Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN304SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND FITTING CORRODED AT STATION 75.000, LONGERON 29 LEFT. REMOVED CORROSION. FOUND OUT ALLOWABLE LIMITS. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-21, DC-8 SRM 5Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA06SMN301SFrame · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND FRAME WITH NON STANDARD REPAIR AT STATION 1580.000 BETWEEN LONGERON 20 LT AND LONGERON 21 LT. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, AFTER DAMAGE REMOVED, NO CRACKS OR CORROSION FOUND. FABRICSep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, FrameSDR IXXA06SMN303SLongeron · crackedDURING ROUTINE C-CHECK INSPECTION FOUND CRACKED LONGERON AT STATION 1770.000 LONGERON 17 LEFT. REMOVED DAMAGED LONGERON. CLEANED, TREATED, AND PRIMED AREA, AND NEW LONGERON. INSTALLED LONGERON (EXTRUSION P/N S1616757) IAW DC8 SRM 53-1-0, DC-8 SRM 51-1-20D, Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA06SMN302SLongeron · crackedDURING ROUTINE C-CHECK INSPECTION FOUND A CRACKED LONGERON AT STATION 1776.000 LONGERON 17 RIGHT. REMOVED CRACKED LONGERON. CLEANED, TREATED AND PRIMED AREA, AND NEW LONGERON. INSTALLED NEW LONGERON (EXTRUSION P/N S1616757) IAW DC8 SRM 53-5-1 FIG 7 SHEET 1 Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA06SMN293SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND EXISTING REPAIR AT STATION FS 29 LONGERON 9.75 LT, DOES NOT MEET CURRENT SRM CRITERIA. REMOVED EXISTING REPAIR. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED TREATED AND PRIMEDSep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN299SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE UPPER SKIN CRACKED AT STATION XFS360.000. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PARTS. APPLIED SEALANSep 12, 2006 · N825BX · Doug DC871F · Wing, Plate/SkinSDR IXXA06SMN286SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND EXISTING REPAIR AT STATION 370 LONGERON 30.5 RIGHT DOES NOT MEET DTA REQUIREMENTS OF MDC 91K0262 REPORT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. TREATED AND PRIMED AREA AND REPAIR PARSep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN292SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND PASSENGER DOOR UPPER AFT CORNER. REPAIR FALLS INTO GROUP 2 PER SERVICE BULLETIN DC 8 53.075, AND AD 2000-20-08 GROUP 2. WITHIN 2,000 LANDINGS OR 3 YEARS AFTER THE EFFECTIVE DATE ACCOMPLISH THE PREVENTATIVE MODIFICATIONSep 12, 2006 · N825BX · Doug DC871F · Passenger/Crew DoorsSDR IXXA06SMN296SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP EXISTING UPPER SKIN DOUBLER IMPROPER AT STATION, XW38.000. REMOVED EXISTING SKIN WITH EXISTING IMPROPER REPAIR. FABRICATED NEW SKIN WITH AL 2024 T3 0.025” AND BONDED DOUBLER AL 2024 T3 0.020”. BONDSep 12, 2006 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN295SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND LT WING IB FLAP EXISTING LOWER. SKIN DOUBLER IMPROPER FROM STATION XW2.000 TO XW91.000. REMOVED EXISTING SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PRIMED ARESep 12, 2006 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN289SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND EXISTING REPAIR AT STATION 1430 LONGERON 36 IN CLOSE PROXIMITY TO ANOTHER EXISTING REPAIR AT THE LOWER SIDE OF (D) PIT DOOR. INCORPORATED BOTH REPAIRS INTO ONE REPAIR. (D) PIT DOOR CORNER REPAIR. REMOVED EXISTING RESep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN287SSkin · misrepairedDURING ROUTINE, C-CHECK INSPECTION FOUND EXISTING REPAIR AT STATION 1384 LONGERON 35.5 RT DOES NOT MEET THE DTA REQUIREMENTS OF MDC 91K0262. REMOVED EXISTING REPAIR. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TOSep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN285SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER EXISTING REPAIR AT STATION 370 LONGERON 25.5 RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMESep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN284SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION 248, LONGERON 26 RIGHT. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREASep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN282SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION FOUND EXISTING REPAIR AT STATION 8 LONGERON 28.5 RIGHT DOES NOT MEET THE DTA REQUIREMENTS OD MDC 91K0262. REMOVED EXISTING REPAIR DOUBLER. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEASep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN294SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SLOT VANE SKIN HOLES ELONGATED AT STATION XS 250.000. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION AFTER DAMAGE REMOVED, NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR DOUBLER, INTERNSep 12, 2006 · N825BX · Doug DC871F · Leading Edge DevicesSDR IXXA06SMN288SSkin · misrepairedDURING ROUTINE C CHECK, MODIFY CARGO DOOR JAMB CORNERS AT STATION 1420 LONGERON 34.5 RIGHT IAW AD 2004-06-06. REMOVED EXISTING REPAIR. FABRICATED REPAIR PARTS. CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLEDSep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN283SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND EXISTING REPAIR DOES NOT MEET DTA REQUIREMENTS OF MDC 941K0262, AT STATION 8 LONGERON 32.5 LEFT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND. FABRICATED REPASep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN291SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND EXISTING DOUBLER AT STATION 1761 LONGERON 16.5 LT FAILED DTA REQUIREMENTS OF MDC 91K0262 REPORT. REMOVED EXISTING REPAIR DOUBLER. FABRICATED REPAIR DOUBLER, INTERNAL FINGER DOUBLER, AND FILLER. CLEANED, TREATED AND PRIMSep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN290SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND IMPROPER REPAIR DOUBLER AT BS 1752 LONGERON 16.5 LT. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, INTERNAL FINGER DOUBLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PASep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060457OTransmitter · failedDURING CRUISE FROM KTOL TO CYJT, CREW NOTICED THE HYDRAULIC PRESSURE DROPPED TO 2000 POUNDS OF PRESSURE. THE CREW ELECTED TO RETURN TO KTOL AND SAFELY LANDED. MAINTENANCE REPLACED THE HYDRAULIC PRESSURE TRANSMITTER. THE HYDRAULIC SYSTEM OPERATIONAL CHECK WAJul 15, 2006 · N825BX · Doug DC871F · Hydraulic Pressure IndicatorSDR IXXA060451OAdi · faultyDURING CRUISE FROM KMIA THE CAPTAINS ADI DISPLAYED BOTH FLIGHT DIRECTOR AND GYRO FLAGS, FLAGS STAYED IN VIEW FOR APPROXIMATELY 1-2 MINUTES THEN WENT AWAY FOR APPROXIMATELY 5 MINUTES, THEN INTERMITTENTLY DISPLAYED AFTER THAT. THE CREW RETURNED TO KMIA AND LANDJun 21, 2006 · N825BX · Doug DC871F · Integrated Flight System
Back to N825BX, cancelled May 1, 2014