N606AL, cancelled Oct 6, 2014
Service difficulty reports · 446
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 = 'N606AL' AND deregistration_id = 'N606AL-2014-10-06' 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 = 'N606AL' AND deregistration_id = 'N606AL-2014-10-06' 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 IXXA20121127032OConnector · looseON APPROACH, RT MLG DOWN GREEN LIGHT DID NOT ILLUMINATE, NO RED LIGHTS ILLUMINATED. CYCLED LANDING GEAR AND GREEN LIGHT ILLUMINATED. RESEATED CONNECTOR PLUG ON RT MLG DOWNLOCK SWITCH IAW MM 32-60-0. OPS CHECKS GOOD.SDR IXXA110048OConnector · dirtyON FINAL APPROACH WITH LANDING GEAR LEVER DOWN, RT LANDING LIGHT DID NOT ILLUMINATE. THE CREW CYCLED THE GEAR AND GEAR LIGHT ILLUMINATED 10 SECONDS AFTER GEAR CYCLE. THEY LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND CLEANED THE CONNECTOR PLUG ON THE DOWNSDR IXXA110027OMec · defectiveAT THE TOP OF CLIMB OUT AT FLIGHT LEVEL 36,000 FT WHEN THROTTLES WERE PULLED BACK FROM CLIMB POWER TO CRUISE POWER NR 3 ENG MOMENTARILY COMPRESSOR STALLED. ALL OTHER ENGINES PARAMETERS WERE NORMAL AND NR 3 COMPRESSOR STALLED AGAIN 10 MINUTES LATER AT CRUISE WSDR IXXA110026OSensor · defectiveDURING CRUISE NR 3 ENG COMPRESSOR STALLED. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED (CIT) SENSOR. OPS CHECK GOOD IAW CFM MM 73-21-20. ACFT WAS RETURNED TO SERVICE.SDR IXXA110021OEngine · flamed outAFTER TAKEOFF, WHEN THROTTLES WERE RETARDED AT FL 37.0 NR 3 ENGINE FLAMED OUT. BEFORE THE CREW COULD ACCOMPLISH FLAME OUT CHECK LIST, THE ENG RELIT WITH NO PROBLEMS THE REMAINDER OF THE FLIGHT, LANDED WITHOUT FURTHER INCIDENT. MX ACCOMPLSHED TREE FAULT 51 WITHSDR IXXA110006OUnknown · unknownDURING TAKEOFF ROLL, ACFT PULLED HARD LEFT. CREW WAS UNABLE TO MAINTAIN DIRECTIONAL CONTROL WITH FULL RT RUDDER. THEY ABORTED TAKEOFF AND RETURNED TO BLOCKS WITH OUT FURTHER INCIDENT. MX INSPECTED THE NOSE GEAR, WHEELS, BRAKES, NOSE WHEEL STEERING, NOSE STEESDR IXXA10SMN095SSpar Cap · crackedDURING ROUTINE C-CHECK INSP FOUND RT WING T/E SPAR CAP UPPER PART CRACKED AT STA XRS 74.000. REMOVED CRACKED UPPER SPAR CAP. FABRICATED NEW UPPER SPAR CAP. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED NEW UPPER SPAR CAP IAW DWG 5611440, 5616128, SDR IXXA10SMN094SSkin · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING OUTER WING OTBD L/E LOWER SKIN CRACKED AT STA XFS 847.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. FABRICATED NEW SKIN, FILLERS AND DOUBSDR IXXA10SMN093SSupport Angle · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT WING UPPER PANEL SUPPORT ANGLE CORRODED AT STA XW 5.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED ANGLE. FABRICATED NEW ANGLE. CLEANED, TERATED, AND PRIMED AREA. ISDR IXXA10SMN092SSkin · damagedDURING ROUTINE C-CHECK INSP, FOUND LT WING NR 2 STUB WING LOWER SKIN ELONGATED HOLES AT STA XFS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED SPLICE DOUBLER AND NEW SKIN. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTSDR IXXA10SMN091SSkin · crackedDURING ROUTINE C-CHECK INSP FOUND LT WING NR 2 STUB WING LOWER SKIN CRACKED AT STA XFS 200.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED SPLICE DOUBLER AND NEW SKIN. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. SDR IXXA10SMN090SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND AFT CARGO COMPARTMENT SPLICE FITTING CRACKED AT STA 1390.000 LONGERON 30 LT. REMOVED CRACKED FITTING. FABRICATED NEW SPLICE FITTING. CLEANED, TREATED, PRIMED AREA AND SPLICE FITTING. INSTALLED NEW SPLICE FITTING IAW SRM 53-SDR IXXA10SMN089SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND AFT CARGO COMPARTMENT SPLICE FITTING CRACKED AT STA 1370.000, LONGERON 31 LT. R & R SPLICE FITTING IAW SRM 51-1-20D AND SRM 51-3-1.SDR IXXA10SMN088SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING T/E UPPER FITTING CRACKED AT STATION XRS 409.000. R & R CRACKED FITTING IAW SRM 51-1-21.SDR IXXA10SMN086SDoubler · crackedDURING ROUTINE C-CHECK INSP FOUND LT WING NR 2 STUB WING EXTERNAL LOWER REPAIR DOUBLER CRACKED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED DOUBLER. FABRICATED EXTERNAL AND INTERNAL DOUBLERS. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMESDR IXXA10SMN087SSkin · crackedDURING ROUTINE C-CHECK INSP, FOUND LT OTBD AILERON LOWER SKIN CRACKED AT STA 761.695. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND DOUBLERS BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, AND PRIMED AREA ASDR IXXA10SMN085SFrame · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FRAME FLANGE CRACKED AT STA 1580.000 LONGERON20-21 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED FRAME. FABRICATED FRAME SEGMENT. PERFORMED HEAT TREATMENT. CLEANED,TREATED, AND PSDR IXXA10SMN084SSupport Fitting · crackedDURING ROUTINE C-CHECK INSP FOUND RT WING MLG SUPPORT FITTING EXTERNAL FACE CRACKED. R & R RT MLG SUPPORT FITTING IAW AD 89-10-04, DACO S/B, DC8-57-094, REV 04 DATED 03-24-2000, DWG 5611021, 5611440, 5611425, 5616128, 5641112, 5893930, AND EO NR 2010556.SDR IXXA10SMN083SWeb · crackedDURING ROUTINE C-CHECK INSP FOUND NR 4 PYLON TEE DOUBLER HORIZ FLANGE CRACKED IN UPPER INTERNAL PART AT STA YN 335.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. FABRICATED SPACER.SDR IXXA10SMN082SSkin · wornDURING ROUTINE C-CHECK INSP FOUND LT WING INBD FLAP UPPER EXTERNAL SKIN WORN AT STA XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATEDSDR IXXA10SMN081SSkin · dentedDURING ROUTINE C-CHECK INSP, FOUND LT WING INBD FLAP UPPER EXTERNAL SKIN DENTED AT STATION XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEWSDR IXXA10SMN080SSkin · crackedDURING ROUTINE C-CHECK INSP FOUND LT WING INBD FLAP LOWER EXTERNAL SKIN CRACKED AT STATION XCW 64.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATSDR IXXA10SMN078SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND RT OTBD FLAP UPPER SKIN CORRODED AT STATION XF 304.000 - 333.0000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORRODED SKIN. FABRICATED NEW SKIN AND DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATEDSDR IXXA10SMN076SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND EXTERNAL FUSELAGE LOWER PART BUTT JOINT SKIN CORRODED AT STA 1690.000 BETWEEN LONGERON 34 RT- LONGERON 34 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, DOUBLERS, FINGER DOUBLERS AND FISDR IXXA10SMN077SSkin · wornDURING ROUTINE C-CHECK INSP, FOUND RT INBD FLAP SKIN WORN AT STA XW 104.000 - 115.0000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND RESDR IXXA10SMN075SDoubler · misrepairedDURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT STATION FS 1560, LONGERON 20.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS AND FILLER. CLEANED, TREATED, PRIMED SDR IXXA100044OSwitch · brokenDURING CLIMBOUT, AFTER GEAR RETRACTION, THE "DOOR NOT LATCH" LIGHT REMAINED ON. CREW CYCLED THE GEARS AND WAS UNABLE TO DETERMINE CONDITION OF MAIN GEAR DOORS. THEY CONTINUED FLIGHT AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED THE MAIN GEAR DOOR WARNINGSDR IXXA090075OGenerator · failedDURING CLIMB OUT FROM DEPARTURE NR 3 GENERATOR BUSS FAILURE, VOLTS AND FREQUENCIES AT ZERO. THE CREW ACCOMPLISHED COM PROCEDURES AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX RESET NR 3 GENERATOR BUS FAULT RESET SWITCH. OPS CHECK GOOD IAW MM 24-20-0. SDR IXXA090040STee Fitting · crackedDURING INSP IAW AD2007-21-18 AND SB DC8-53A081 FOUND AFT PRESSURE BULKHEAD TEE FITTING CRACKED AT LONGERON 9 RT TO LONGERON 10 RT. STOP DRILLED CRACK IAW SRM 53-2-5.SDR IXXA090039STee Fitting · crackedDURING INSP IAW AD2007-21-18 AND SB DC8-53A081 FOUND AFT PRESSURE BULKHEAD TEE FITTING CRACKED AT LONGERON 11 LT TO LONGERON 13 LT. STOP DRILLED CRACK IAW DACO DC8 SRM 53-2-5.SDR IXXA090028OCable · defectiveDURING CLIMB-OUT FROM KTOL NUMBER TWO ENGINE EGT WENT TO 914 DEGREE FOR TWO TO FIVE SECONDS. THE CREW RETARDED THE THROTTLE AND EGT INDICATOR DECREASED AND ALL OTHER ENGINES PARAMETER WERE NORMAL. THE CREW RETURNED TO KTOL AND LANDED WITHOUT FURTHER INCIDENTSDR IXXA090005OTube · cloggedDURING DESCENT INTO ETAR NUMBER 2 ENGINE FLAME OUT. WITH THROTTLE REDUCTION, MILD VIBRATION, AND FUEL FLUCTUATION. THE CREW LANDED IN ETAR WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED CFM TROUBLESHOOTING TREE FAULT 51 AND FOUND CDP TUBES CLOGGED. MAISDR IXXA080016OFire Loop · shortedDURING CRUISE FROM KTOL, NUMBER THREE ENGINE FIRE WARNING LIGHT AND BELL CAME ON INTERMITTENTLY. THE CREW ACCOMPLISHED THE ENGINE FIRE CHECKLIST AND DISCHARGED BOTH BOTTLES. AFTER BOTH BOTTLES WERE DISCHARGED THE FIRE WARNING CAME ON STEADY AND STAYED ON JUSSDR IXXA080004OSwitch · defectiveDURING CLIMB FROM KTOL, AFTER GEAR WAS RETRACTED DOOR NOT LATCH LIGHT CAME ON, THE CREW CYCLED THE GEAR THE LIGHT STAYED ON. THE CREW ACCOMPLISHED UPLATCH CHECK AND CYCLED THE GEAR A SECOND TIME THE LIGHT STAYED ON. THE CREW CLIMB TO 32,000 FEET CYCLED THE GSDR IXXA07SMN224SStructure · misrepairedDURING ROUTINE C CHECK INSPECTION, FS 1345, LONGERON 30.5 LEFT. DOUBLER BELOW AND AFT OF AFT EMERGENCY EXIT DOOR. REPAIR NUMBER 606 AL-R36. PROBLEM: SIDE 2, 2ND ROW EXCEEDS MAS RIVET SPACING. DISPOSITION: ADD RIVETS TO BRING INTO LIMITS OR UPGRADE.SDR IXXA07SMN223SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO LT CUSP EXTRUSION, FITTING WITH CORROSION AT STA 80.000, L-21L.SDR IXXA07SMN225SLongeron · misrepairedDURING ROUTINE C CHECK INSPECTION, FS 1367, LONGERON 30.5 LEFT, DOUBLER BELOW AND AFT OF AFT EMERGENCY EXIT DOOR. REPAIR NUMBER 606AL-R37. PROBLEM: SIDE 2 ENDS ON LONGERON WITHOUT FINGER DOUBLER. DISPOSITION: UPGRADE IAW SRM.SDR IXXA07SMN217SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT AFT FITTING SHOWS CRACK 2" BETWEEN STA 1220.000 AND L-19R. REPLACED CRACKED FITTING WITH NEW FITTING IAW DC8 SRM 51-1-20D.SDR IXXA07SMN222SSpar · crackedDURING ROUTINE C CHECK INSPECTION, NR 2 MAIN TANK WEB OF CENTRAL SPAR (LWR SIDE) CRACKED 2 1/2" AT STA XRS 172.000 BETWEEN S-61 AND S-62.SDR IXXA07SMN212SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING INBD FLAP UPPER SKIN SHOWS DENT AT XW 88.000.SDR IXXA07SMN211SLongeron Splice · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT LONGERON SPLICE FITTING CRACKED AT STA 1690.000 L-36.SDR IXXA07SMN221SSpar Cap · crackedDURING ROUTINE C CHECK INSPECTION, NR 2 MAIN TANK LOWER CAP OF CENTER SPAR 3" CRACKED AT STA ZRS 172.000 BETWEEN S-61 AND S-62.SDR IXXA07SMN214SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, LT HORIZONTAL STABILIZER, POINTS OF CORROSION ON UPPER SKIN FROM STA XE 28.843 TO STA XE 30.000.SDR IXXA07SMN216SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT FWD FITTING SHOWS CRACK 1" BETWEEN STA 1152.000 AND L-20R.SDR IXXA07SMN218SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT AFT FITTING SHOWS CRACK 2" AT STA 759.000 AND L-18.8L.SDR IXXA07SMN215SFitting · crackedDURING ROUTINE C CHECK INSPECTION, RT HORIZ STABILIZER FITTING SHOWS CRACK 2" FRONT PART AT STA NFS 60.000.SDR IXXA07SMN220SSpar · crackedDURING ROUTINE C CHECK INSPECTION, NR 1 MAIN TANK CTR SPAR WEB LWR SIDE, CRACK 4" AT STA XRS 255.000 BETWEEN S-61 AND S-62.SDR IXXA07SMN219SSpar · crackedDURING ROUTINE C CHECK INSPECTION, NR 1 MAIN TANK, CTR SPAR LWR CAP, CRACKED 3" AT STA XRS 255.000 BETWEEN S-61 AND S-62.SDR IXXA07SMN213SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING INNER FLAP, UPPER SKIN SHOWS DENT BETWEEN STA XF 112.000 TO STA XF 120.000.SDR IXXA07SMN209SSkin · dentedDURING ROUTINE C CHECK INSPECTION, RT ELEVATOR OIL CANNING LOWER PANEL, PLATING AT STA XE 279.000 STA XE 306.000.
Back to N606AL, cancelled Oct 6, 2014