N829BX, cancelled Apr 14, 2014
Service difficulty reports · 229
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 = 'N829BX' AND deregistration_id = 'N829BX-2014-04-14' 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.
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 = 'N829BX' AND deregistration_id = 'N829BX-2014-04-14' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IXXA070066OWire · out of positionDURING CLIMB FROM KTOL GEAR DOOR WARNING LIGHT CAME ON WOULD NOT GO OUT. THE CREW RETURNED TO KTOL, AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED GEAR DOOR AND REPOSITONED WIRING AT DOOR WARNING LIGHT SOCKET OPERATIONAL CHECK WAS GOOD IAW DC8 MAINTENANCESDR IXXA070059OMechanism · out of adjustDURING CLIMB-OUT FROM KTOL, MAIN LANDING GEAR DOOR LIGHT STAYED ILLUMINATED. THE CREW CYCLED THE GEAR AND THE LIGHT STAYED ON. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED RIGHT MAIN GEAR DOOR AND ADJUSTED RIGHT GEAR DOOR FOLSDR IXXA070057OStriker · out of adjustDURING CLIMB-OUT FROM KPHL TO KTOL, AFTER GEAR RETRACTION THE DOOR LIGHT REMAIN ON. THE CREW CYCLED THE GEAR AND THE LIGHT REMAINED ON. THE CREW CONTINUED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED UPLATCH SWITCHES AND ADJUSTED DSDR IXXA070056OUplock Switch · dirtyDURING CLIMB-OUT FROM KTOL TO KPHL, GEAR LANDING DOOR LIGHT REMAINED ON AFTER GEAR WAS RETRACTED, THE CREW CYCLED THE GEAR AND THE LIGHT REMAINED ON. THE CREW CONTINUED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE SYSTEM AND CLEANED GLYCOL SDR IXXA070055OStriker · wornDURING CLIMB FROM KRFD TO KTOL, THE LANDING GEAR DOORS LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED. THE CREW CYCLED THE GEAR AND THE LIGHT REMAINED ON. THE CREW CONTINUED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE SYSTEM AND REPLSDR IXXA070039OWire · damagedDURING CLIMB FROM KEWR, THE GEAR DOOR LIGHT ILLUMINATED DURING THE UPLATCH CHECK. THE CREW CYCLED THE GEAR. THE DOOR LIGHT REMAINED ON DURING AND AFTER THE UPLATCH CHECK. THE CREW CONTINUED THE FLIGHT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECSDR IXXA070013OUnknown · malfunctionedDURING CLIMB-OUT OF KTOL, THE GEAR DOOR WARNING LIGHT ILLUMINATED AFTER A SATISFACTORY GEAR UP-LATCH CHECK. THE CREW RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE MAIN LANDING GEAR DOOR SYSTEM AND REPLACED THE DOOR ACTUATORS, CONTROL VALVESSDR IXXA070008OLimit Switch · damagedDURING CLIMB-OUT OF KTOL, AFTER SATISFACTORY UPLATCH CHECK, THE MAIN LANDING DOOR LIGHT REMAINED ILLUMINATED. THE CREW COMPLIED WITH THE ABNORMAL PROCEDURES AND CONTINUED THE FLIGHT TO KSJC AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED WIRING OF THE RIGSDR IXXA070007OSwitch · contaminatedDURING TAKEOFF FROM KTOL, THE DOORS NOT LATCHED LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. THE CREW ACCOMPLISHED THE UNSATISFACTORY UP-LATCH PROCEDURE AND THE DOORS NOT LATCHED LIGHT REMAINED ON. THE CREW CONTINUED THE FLIGHT TO KLAX AND LANDED WITHOUT INCISDR IXXA060612OLanding Gear · out of adjustAFTER TAKEOFF FROM KRFD, THE LANDING GEAR DOOR LIGHT REMAINED ON AFTER GEAR UPLATCH CHECK. THE CREW CYCLED THE GEAR AND THE LIGHT STAYED ON. THE CREW PERFORMED THE UNSAFE GEAR-UP OR DOOR INDICATION ABNORMAL PROCEDURE, AND CONTINUED THE FLIGHT TO KTOL AND LANSDR IXXA060611OConnector · dirtyAFTER TAKEOFF FROM KSJC, THE GEAR DOOR LIGHT CAME ON WITH GEAR UP AND LOCKED. THE CREW RECYCLED THE LANDING GEAR AND THE LIGHT CAME BACK ON SEVERAL SECONDS AFTER GEAR WAS UP AND LOCKED. LIGHT FLASHED ON AND OFF DURING GEAR UPLATCH CHECK, THEN CAME ON STEADYSDR IXXA060456SSkin · damagedDURING PREFLIGHT INSPECTION FOUND AIRCRAFT SKIN DAMAGED ON THE RIGHT HAND SIDE BELOW THE LAV SERVICE DOOR. REPAIRED SKIN PER DC8 SRM 53-2-1.SDR IXXA060454OLanding Gear · lack of lubeDURING TAKEOFF FROM KDFW THE AIRCRAFT FAILED THE GEAR UPLATCH CHECK. THE CREW PERFORMED THE UNSATISFACTORY UPLATCH CHECKLIST AND RECYCLED THE GEAR, AGAIN FAILING THE UPLATCH CHECK. THE CREW ELECTED TO RECYCLE THE GEAR AGAIN AND THE UPLATCH CHECK WAS SUCCESSFSDR IXXA060186OActuator · malfunctionedON TAKEOFF UNABLE TO KEEP AIRCRAFT ON CENTERLINE WITH RUDDER PEDALS. REJECTED TAKEOFF AT 90 KTS IN NOSE WHEEL STEERING RUDDER PEDALS VERY SLOW TO REACT. MAINTENANCE REMOVED AND REPLACED BOTH LT AND RT STEERING ACTUATORS RE-RIGGED SYSTEM AND OP CHECK OK. AIRSDR IXXA0600002OO-Ring · failedDURING FLIGHT 817 FROM KMCO TO RATL AFTER TAKEOFF A LOSS OF HYDRAULICS OCCURED. RAN LOSS OF HYDRAULIC EMERGENCY CHECK LIST. DUE TO INTENDED FLIGHT PLAN, CREW ELECTED TO RETURN TO DEPARTURE STATION KMCO AND LANDED WITHOUT INCIDENT. FOUND RIGHT AILERON CYLINDSDR IXXA0500121OUplock · lack of lubeDURING CLIMB OUT, UNSATISFACTORY UPLATCH CHECK, NOSE GEAR IS EXTENDING DURING UPLATCH CHECK. CREW RETURNED AIRCRAFT TO DEPARTURE AND LANDED WITH NO INCIDENT. MAINTENANCE LUBED THE UPLATCH MECHANSIM AND CHECKED OPERATION OF UPLATCH BY GEAR RETRACTION. AN UPLATSDR IXXA0500120OHsi · inoperativeON CLIMB-OUT FROM KTOL, FO'S ADI/HSI WAS INOP. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET C/B AND GYRO PER ALL APPLICABLE MANUALS AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR IXXA05SMN267SSkin · elongatedDURING C CHECK INSPECTION, NR 4 PYLON UPPER PLATING HAS ELONGATED HOLES AT STA YN 254 S. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05471 DATED 10-18-05, SEMAN DWG # ED-4084 DATED 10-11-05 AND EO SEMAN # 20051341 DATED 10-18-05. REMOVED FASTENERS IAW DC8 SDR IXXA05SMN266SSkin · crackedDURING C CHECK INSPECT, LT HORIZ STAB ELEVATOR UPPER SKIN CRACKED ½, XE 200.2379. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3. REMOVED FASTENERS IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4085. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPSDR IXXA05SMN265SFitting · crackedDURING ROUTINE C CHECK INSPECTION, RT FLAP SUPPORT FITTING CRACKED AT STA. XW 410.000. REMOVED AND REPLACED RT FLAP LINK SUPPORT AT STA XW 410.000 IAW DC8 MM 27-51-12 PAGES 201-204. REFER TO N/R FOR OPS CHECK.SDR IXXA05SMN264SSkin · unbondedDURING ROUTINE C CHECK INSPECTION, LT RUDDER TAB SKIN UNBONDED 2 AT STA ZRT 98. REMOVED DAMAGED SKIN, CORE SECTION IAW DC8 SRM 55-2-2 PART 2 PAGE 1. FAB`D REPAIR CORE PLUG (AL. HONEY COMB CORE), REPAIR DOUBLER (ALCLAD 2024 T3 0.012) IAW DC8 SRM 55-2-2 PAR 2 PSDR IXXA05SMN261SDoubler · corrodedDURING ROUTINE C CHECK INSPECTION, LT OUTER WING, OTBD L/E ACCESS DOOR INTERNAL DOUBLER CORRODED, XFS 847.500. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PG 16. REMOVED CORRODED INTERNAL DOUBLER IAW DC8 SRM 51-1-21SDR IXXA05SMN263SSkin Panel · misrepairedDURING C CHECK INSPECTION, EXT FS NON STANDARD REPAIR, STA 8.000 STA 17.000 BTWN L-15 AND L-16L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05447 DATED 10-05-05, SEMAN DWG # ED-4077 DATED 10-01-05 AND EO SEMAN # 20051295 DATED 10-05-05. REMOVED EXISTING DSDR IXXA05SMN262SSkin · improperDURING ROUTINE C CHECK INSPECTION, FWD FUSELAGE CTR LWR PLATING AFT OF FWD BASKET DOOR EXISTING REPAIR ALL SIDES EXCEED MAXIMUM RIVETS SPACING AT STA FS 360.000 L-36. INSTALLED HILOKS IAW FAA FORM 8110-3 # 05448 DATE 10-05-05, SEMAN DWG ED 4080 DATE 10-03-05 SDR IXXA05SMN260SDoubler · corrodedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT MLG W/W PRESSURE PANEL DOUBLER CORRODED, STA 880.000 RBL 2’. REMOVED CORROSION FROM DOUBLER IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PG 2P. REMOVED CORRODED DOUBLER IAW DC8 SRM 51SDR IXXA05SMN259SDoor · crackedDURING C CHECK INSPECT, LT FUSE NOSE SECTION PLATING FREON SYS EXHAUST DOOR UPPER AFT JAMB CORNER CRACK DAMAGE AT STA FS 54.000, L-28L TO L-29L. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 13. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-3-0. REMOVED DASDR IXXA05SMN258SFastener · improperDURING C CHECK INSPECT, EXTERNAL FS REPAIR FASTENERS IMPROPER AND RIVETS EXCEED ALLOWABLE LIMITS, STA 180.000 L-19R. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN 20051309 DATED 09-29-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SDR IXXA05SMN257SDoubler · unknownDURING C CHECK INSPECT, LT FUS AFT CTR SECTION LWR PLATING DOUBLER UPGRADE THICKNESS AT STA FS 1356.00 L-29 RT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN NR 20051303 DATED 09-29-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. REMOVESDR IXXA05SMN256SRepair · improperDURING ROUTINE C CHECK INSPECTION, LT FUSELAGE AFT CENTER SECTION WINDOW BELT EVALUATE CONFORMITY PER SRM AT STA FS 1250.00 L-15.5 LT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 22A, TR # 53-170, EO SEMAN # 20051302 DATED 09-28-05. REMOVED EXISTING REPAIRSDR IXXA05SMN255SRepair · improperDURING C CHECK INSPECTION, LT FUSELAGE FWD CENTER SECTION WINDOW BELT EVALUATE CONFORMITY PER SRM AT STA FS 245.00 L-15.5 LT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 22A, TR # 53-170, EO SEMAN # 20051301 DATED 09-28-05. REMOVED EXISTING REPAIR DOUBLER SDR IXXA05SMN254SRepair · improperDURING C CHECK INSPECT, RT FUSELAGE AFT CENTER SECTION FWD OF R-2 DOOR OPENING EVALUATE CONFORMITY PER SRM AT STA FS 1550.00 L-15.5 RT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 22A, EO SEMAN NR 20051300 DATED 09-28-05. REMOVED EXISTING REPAIR DOUBLER IASDR IXXA05SMN253SDoubler · improperDURING C CHECK INSPECT, LT FUS FWD CTR SECTION LWR PLATING BASKET DOOR FWD JAMB EXISTING REPAIR DBLR NOT ACCOMP 3 ROWS FASTENERS PAST CUT OUT STA FS 279.000 L-35.5L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05461. REMOVED EXISTING REPAIR DOUBLER IAW DCSDR IXXA05SMN244SVane · damagedDURING C CHECK INSPECT, RT WING INNER L/E SLOT VANE HAS ELONGATED HOLES AT STA XOLDO 67.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PARSDR IXXA05SMN252SRepair · misinstalledDURING C-CHECK INSPECT, RT FUSE FWD CTR SECTION LWR PLATING FWD OF A PIT DOOR EXISTING DBLR EXCEED MAX RIVETS SPACING AT BS 272.00 L-31R. PERFORMED MAJOR REPAIR IAW FORM 8110-3 NR 05451, SEMAN DWG NR ED-4078, EO SEMAN 20051296. REMOVED REPAIR DOUBLER IAW DC8SDR IXXA05SMN251SSkin Panel · brokenDURING C CHECK INSPECTION, LT FUSELAGE NOSE SECTION LWR PLATING UPPER AFT CORNER BROKEN OFF AT BS 70 L-33. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-2 FIG 8C-2, TR NR 53-176, EO SEMAN NR 20051299 DATED 09-29-05. PERFORMED DETAIL VISUAL INSPECT. NEITHER CRACK SDR IXXA05SMN249SRepair · misinstalledDURING C-CHECK INSPECT, LT NOSE SKIN FWD PAX DOOR JAMB EXISTING DBLR EXCEED OVERAGE RIVETS SPACING AND CHERRY MAX AT STA FS 24 L-36 LT. PERFORMED MAJOR REPAIR IAW FORM 8110-3, SEMAN DWG ED-4077 DATED 10-01-05 AND EO SEMAN 20051295 DATED 10-05-05. REMOVED EXISDR IXXA05SMN248SRivet · out of toleranceDURING C CHECK INSPECT, LT FUSELAGE NOSE SECTION PLATING DOUBLER REPAIR EXCEED MAX RIVETS SPACING STA FS 10 L-22 LT. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05448 DATED 10-05-05, SEMAN DWG # ED 4076 DATED 10-03-05, EO SEMAN # 20051294 DATED 10-05-05. RESDR IXXA05SMN247SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, LEFT WING NR 2 MAIN TANK FITTING CRACKED, FS 74.000 S.51 (FWD INTERNAL PART). REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP COATING YELLOW IAW DC8 SRM 51-1-12 PAGES 7-25. INSTALLED NEW SDR IXXA05SMN246SFitting · crackedDURING ROUTINE C CHECK INSPECTION, LT WING NR 2 MAIN TANK FITTING CRACKED, FS 74.000 S.51 (FWD EXTERNAL PART). REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP COATING YELLOW IAW DC8 SRM 51-1-12 PAGES 7-25. INSTALLED NEW FISDR IXXA05SMN245SFitting · improperDURING ROUTINE C-CHECK INSPECTION, RIGHT MLG W/W - L-24R FITTING HAS NO STANDARD REPAIR AT STA 879.375. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 8. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-20D. FABIRCATED (4) REPAIR FITTING (P/N 5802677-4) FROM AL7SDR IXXA05SMN243SVane · elongatedDURING ROUTINE C CHECK INSPECTION, RT WING CTR L/E SLOT VANE HAS ELONGATED HOLES AT STA XILD 7095. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05461 DATED 10-10-05, SEMAN DWG NR ED-4081 DATED 10-08-05, EO SEMAN NR 20051290 DATED 10-10-05. REMOVED FASTENERSSDR IXXA05SMN242SSkin Panel · improperDURING C CHECK INSPECT, LT MLG W/W - L-24L HAS NO STANDARD REPAIR BETWEEN BS 960.000 & 980.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-2 FIG 5, TR NR 53-123, EO SEMAN NR 20051282 DATED 09-27-05. REMOVED EXISTING REPAIR IAW DC8 SRM 51-1-20D. STOP DRILLED CRSDR IXXA05SMN241SDoubler · crackedDURING ROUTINE C CHECK INSPECTION, RT INNER WING CTR L/E INTERNAL DOUBLER CRACK 3 AT STA XFS 250.000. REMOVED CRACKED INTERNAL DOUBLER IAW DC8 SRM 51-1-21. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.063”) IAW DC8 SRM 57-3-1 FIG 3. CLEANED, TREATED, PRIMED SDR IXXA05SMN240SPan · crackedDURING ROUTINE C CHECK INSPECTION, RT INNER WING OUTBD L/E ZEE PAN CRACK 2” AT STA XS 250.089. REMOVED CRACKED SPLICE PAN IAW DC8 SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE PAN IAW DC8 SRM 51-1-21, DC8 SRM 51-1-2SDR IXXA05SMN239SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT HORIZONTAL STABILIZER L/E UPPER SKIN DENTED, XFS 78.750 XFS 85.00. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-2-1 FIG 4, EO SEMAN # 20051292 DATED 09-27-05. REMOVED EXISTING REPAIR DOUBLER NEXT DENT IAW DC8 SRM 51-1-21. REMOSDR IXXA05SMN238SDoubler · crackedDURING ROUTINE C-CHECK INSPECTION, LEFT WING CTR L/E LWR INTERNAL DOUBLER CRACK 2 AT STA XFS 342.500. REMOVED CRACKED INTERNAL DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.090”) IAW DC8 SRM 57-3-1 FIG 4. CLEANEDSDR IXXA05SMN237SDoubler · crackedDURING C CHECK INSPECTION, LT WING CTR L/E LWR PART INTERNAL DOUBLER CRACKED 7, XFS 341.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463 DATED 10-11-05, SEMAN DWG # ED-4083 DATED 10-10-05, EO SEMAN # 20051312 DATED 10-11-05. REMOVED EXISTING REPAIR DSDR IXXA05SMN236SSkin · improperDURING C CHECK INSPECTION, RT OTBD FLAP UPPER SKIN HAS NON STANDARD REPAIR, STA XF 210.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4, TR#57-94, EO SEMAN # 20051288 DATED 09-28-05. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0, DC8 SRM 51-1SDR IXXA05SMN235SSkin · improperDURING C CHECK INSPECTION, RT OTBD FLAP UPPER SKIN HAS NON STANDARD REPAIR, STA XF 230.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05447 DATED 10-05-05, SEMAN DWG # ED 4072 DATED 10-01-05, EO SEMAN # 20051298 DATED 10-05-05. REMOVED EXISTING NON STANDARSDR IXXA05SMN234SSkin · improperDURING C CHECK INSPECTION, RT WING INBD FLAP UPPER SKIN HAS NON STANDARD REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 1, EO SEMAN NR 20051279 DATED 09-26-05. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 51-1-21. FABRICATED NEW PLATING (
Back to N829BX, cancelled Apr 14, 2014