N936AX, cancelled Feb 7, 2008
Service difficulty reports · 74
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 = 'N936AX' AND deregistration_id = 'N936AX-2008-02-07' 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 = 'N936AX' AND deregistration_id = 'N936AX-2008-02-07' 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 ABXA040139Keelbeam · crackedLEFT KEELBEAM TO VERTICAL WEB ATTACH FITTING CRACKED AT BOTTOM OF WING ATTACH POINT APPROXIMATELY STA 693 FORWARD OF GEAR DOOR ACTUATOR. REPLACED FITTING IAW DC-9 SRM.SDR ABXA020206Longeron · crackedLONGERON 29 LEFT FORE AND AFT OF SPLICE CRACKED AT FS 408. REPLACED SECTION OF LONGERON IAW DC-9 SRM 53-02.SDR ABXA020205Angle · damagedRIGHT DORSAL FIN ATTACH ANGLE HAD TOOLING DAMAGE IN THE RADIUS. REPLACED DORSAL FIN ATTACH ANGLE IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-5, AND REA D953-44887.SDR ABXA020204Skin · crackedFUSELAGE SKIN CRACKED AT UPPER/AFT STOP. REPAIRED UPPER AFT DOOR CUTOUT IAW DC-9 SRM 53-05.SDR ABXA010041Pan · crackedFORWARD LOWER CARGO DOOR LOWER PAN WAS CRACKED IN THE RADIOUS. MAINTENANCE INSPECTED AND REPAIRED THE CRACKED AREA IAW DC-9 SRM 52-03 FIG 8.SDR ABXA010045Shear Tie · crackedSHEAR TIE AT FUSELAGE STATION 1087, LONGERON 2R WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE SHEAR TIE IAW DC-9 SRM 51-30.SDR ABXA010044Longeron · crackedLONGERON 2R WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE LONGERON IAW DC-9 SRM 53-01, 53-30.SDR ABXA010043Longeron · crackedLONGERON 2L WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE LONGERON IAW DC-9 SRM 53-01, 51-30.SDR ABXA010042Frame · crackedFUSELAGE FRAME AT STATION 617 WAS FOUND TO HAVE TWO CRACKS (1.25 AND .5 INCH LENGTHS). MAINTENANCE INSPECTED AND REPAIRED THE FRAME IAW ABX REA D953-39920-MR.SDR ABXA010136Bearing · wornTHE HORIZONTAL STABILIZER JACKSCREW BEARING FREE PLAY EXCEEDED LIMITATIONS. MAINTENANCE INSPECTED AND REPLACED THE JACKSCREW ASSEMBLY IAW DC-9 MM 27-40-01.SDR ABXA000107Switch · failedON LANDING HAD TO RECYCLE GEAR BECAUSE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE. GEAR WAS SELECTED DOWN AGAIN AND ALL THREE GREEN LIGHTS ILLUMINATED. REPLACED NLG DOWNLOCK POSITION SWITCH IAW DC9 SMM 32-60-00. OPS CHECKED GOOD.SDR ABXA9900433Frame · crackedDURING C-CHECK, FOUND LEFT MAIN FRAME STATION 699 CRACKED. REPLACED LEFT MAIN FRAME IAW DC9 SRM 51-30-2 AND 51-30-1.SDR ABXA9900416Pan · crackedDURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR PAN CRACKED. REPAIRED IAW DC9 SRM 52-03 AND 51-30-1.SDR ABXA9900403Longeron · crackedDURING C-CHECK, FOUND LONGERON 26 LEFT CRACKED AT STATION 945. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2.SDR ABXA9900425Longeron · crackedDURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 980. REPLACED LONGERON 17 LEFT IAW DC9 SRM 51-30-5.SDR ABXA9900424Retainer · crackedDURING C-CHECK, FOUND WINDOW RETAINER CRACKED AT STATION 698, LEFT SIDE. REPAIRED IAW ABX REA D953-31670.SDR ABXA9900423Pan · crackedDURING C-CHECK, FOUND AFT LOWER CARGO DOOR PAN CRACKED. REPLACED DOOR PAN IAW DC9 SRM 51-30-2.SDR ABXA9701706Vane · delaminatedDURING C-CHECK, FOUND THE LEFT WING CENTER FIXED VANE WAS DELAMINATED. REPLACED VANE.SDR ABXA9701705Doubler · crackedDURING C-CHECK, FOUND MAIN ENTRY DOOR CUTOUT INTERNAL UPPER FORWARD DOUBLER CRACKED. REPAIRED IAW DC-9 SRM 53-05.SDR ABXA9701704Angle · crackedDURING C-CHECK, FOUND THE RIGHT PYLON UPPER ATTACH ANGLE WAS CRACKED. REPAIRED IAW DC-9 SRM 54-04.SDR ABXA9701701Vane · delaminatedDURING C-CHECK, FOUND THE LEFT WING INBOARD FIXED VANE WAS DELAMINATED. THE VANE WAS REPLACED IAW DC-9 M/M.SDR ABXA9701702Bulkhead Angle · crackedDURING C-CHECK, FOUND ANGLE ON THE AFT SIDE OF THE AFT PRESSURE BULKHEAD WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW DC-9 SRM.SDR ABXA9701703Angle · corrodedDURING C-CHECK, FOUND ANGLE CORRODED AT FORWARD OUTBOARD CORNER OF RIGHT WHEEL WELL. THE ANGLE WAS REPLACED IAW DC-9 SRM.SDR ABXA9700962Gear Indication · inoperativeNOSE LANDING GEAR INDICATION LIGHT APPEARS TO BE INOPERATIVE. VERIFIED DOWN BY TOWER FLY-BY. INSPECTED NOSE GEAR DOWN LOCK SWITCH AND GEAR HANDLE SWITCH. CYCLED NOSE GEAR 4 TIMES, OPS CHECKED GOOD IAW DC-9 MM 32-30-01. NO DEFECTS NOTED.SDR ABXA9600423Power Supply · inoperativeEMERGENCY LIGHTS INTERMITTENTLY STAY ON WITH POWER OFF. REPLACED EMERGENCY LIGHT POWER SUPPLY.SDR ABXA9600245Power Supply · inoperativeDURING PRE-DEPARTURE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY.SDR ABXA9600244Uplock Switch · defectiveAFTER GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED, RECYCLED GEAR, NO HELP. LIGHT EXTINGUISHED AFTER 2-3 MINUTES UPON ENTERING TURBULENCE. REPLACED LEFT GEAR UPLOCK SWITCH S1-79.SDR ABXA9600404Pressure Panel · defectiveDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE PRESSURE PANEL AT FS 37 HAD A ONE INCH DIAMETER HOLE ON THE RIGHT SIDE BELOW THE RADOME HINGE POINT. REPAIRED PRESSURE PANEL AT FS 37 IAW ABX REA D953-14357-MR.SDR ABXA9600403Floor Panel · damagedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A FLOOR PANEL DAMAGED FROM FS 237 TO 313. REPAIRED FLOOR PANEL IAW ABX REA D953-14339-MR.SDR ABXA9600387Skin · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FUSELAGE SKIN AT FORWARD EDGE OF THE FORWARD CARGO COMPARTMENT DOOR JAMB HAD TWO CRACKS AND EXCESSIVE CORROSION BLENDOUTS. REPAIRED IAW ABX REA D953-13853-MR.SDR ABXA9600400Door Pan · bindingDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND WHILE REPLACING THE LEFT FORWARD ENTRY DOOR, THE NEW DOOR REQUIRED EXCESSIVE TRIM OUT AROUND THE UPPER POCKET OF THE LOWER HINGE CAVITY. REPAIRED LEFT FORWARD ENTRY DOOR IAW REA D952-14205-MR.SDR ABXA9600402Floor Beam · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FLOOR BEAM WEB AT FS 996 AND BL 0 CRACKED AND CORRODED. REPAIRED FLOOR BEAM WEB AT FS 996 IAW ABX REA D953-14261-MR.SDR ABXA9600401Skin · damagedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, AND EXISTING REPAIR ON THE SERVICE DOOR FORWARD JAMB UPPER CORNER INTERFERED WITH THE ACCOMPLISHMENT OF SID INSPECTION PSE 53-09-033A, IAW AD 94-03-1. VERIFIED REPAIR AND PLACED ON CARRYOVER FOR DACO TO PERFORM DTASDR ABXA9600419Te Panel · delaminatedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT WING TRAILING EDGE PANEL AT XRS 91.0 DELAMINATED AND RIVETS SHEARED. REPLACED LEFT WING TRAILING EDGE PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.SDR ABXA9600397Web · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A PREVIOUS REPAIR ON THE AFT PRESSURE BULKHEAD LOWER WEB THAT WAS CORRODED AND HAD DRILL STARTS. REPAIRED AFT PRESSURE BULKHEAD WEB IAW ABX REA D953-14176-MR.SDR ABXA9600399Floor Beam Web · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A FLOOR BEAM WEB CORRODED AT FS 996. REPAIRED FLOOR BEAM WEB AT FS 996 IAW ABX REA D953-14201-MR.SDR ABXA9600374Skin · dentedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT AFT FUSELAGE SKIN HAD TWO DENTS BETWEEN FS 966 AND 987, BETWEEN LONGERONS 16R AND 18R. REPAIRED AFT FUSELAGE SKIN IAW ABX REA D953-13715-MR.SDR ABXA9600398Skin · dentedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND TWO DENTS IN THE RIGHT FORWARD FUSELAGE SKIN BETWEEN FS 351 AND 364 AND LONGERONS 24 AND 25R. REPAIRED FORWARD FUSELAGE SKIN IAW ABX REA D953-14200-MR.SDR ABXA9600381Floor Beam · chafedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FLOOR BEAMS AT FS 389 AND 408 GOUGED AND CHAFED. REPAIRED FLOOR BEAMS IAW ABX REA D953-13826-MR.SDR ABXA9600380Floor Beam · chafedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FLOOR BEAM AT FS 389 AND 408 GOUGED AND CHAFED. REPAIRED FLOOR BEAMS IAW ABX REA D953-13826-MR.SDR ABXA9600395Floor Beam · chafedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FLOOR BEAM AT FS 980 HAD UPPER FLANGE CHAFE DAMAGE AT BL 40.0 AND 50.0. REPAIRED FLOOR BEAM AT FS 980 IAW ABX REA D953-14061-MR.SDR ABXA9600392Frame · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT FUSELAGE FRAME AT FS 658 HAD A PREVIOUS REPAIR THAT WAS CRACKED THROUGH THE STOP DRILL. REPAIRED LEFT FUSELAGE FRAME FS 658 IAW ABX REA D953-13924-MR.SDR ABXA9600391Frame · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT FUSELAGE FRAME AT FS 639 HAD A PREVIOUS REPAIR ON THE AFT SIDE AT LONGERON 18L THAT HAD CRACKED THROUGH THE PREVIOUS STOP DRILL. REPAIRED LEFT FUSELAGE FRAME AT FS 639 IAW ABX REA D953-13924-MR.SDR ABXA9600420Te Panel · delaminatedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT WING TRAILING EDGE PANEL BETWEEN STATION XRS 445.0 AND XRS 509 CORRODED AND DELAMINATED. REPLACED TRAILING EDGE PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.SDR ABXA9600408Frame · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05; SB 53-131 VISUAL INSPECTION OF LEFT AND RIGHT FUSELAGE FRAMES, FOUND THE FRAME AT FS 737L CRACKED IN TWO PLACES. REPLACED FRAME AT FS 737 IAW SB 53-131 AND DC-9 SRM CHAPTERS 51-30-1SDR ABXA9600407Frame · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05; SB 53-131, VISUAL INSPECTION OF LEFT AND RIGHT FUSELAGE FRAMES, FOUND THE LEFT FRAME CRACKED AT FS 718. REPLACED FRAME AT FS 718 IAW SB 53-131 AND DC-9 SRM CHAPTERS 51-30-1, 51-30-2SDR ABXA9600394Skin · chafedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL STABILIZER RIGHT AND LEFT UPPER SKIN PANELS CHAFED AND BLENDED BEYOND THE DC-9 SRM LIMITS. REPAIRED HORIZONTAL STABILIZER LEFT AND RIGHT UPPER SKIN PANELS IAW ABX REA D955-14035-MR.SDR ABXA9600393Skin · chafedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL STABILIZER RIGHT AND LEFT UPPER SKIN PANELS CHAFED AND BLENDED BEYOND THE DC-9 SRM LIMITS. REPAIRED HORIZONTAL STABILIZER LEFT AND RIGHT UPPER SKIN PANELS IAW ABX REA D955-14035-MR.SDR ABXA9600396Service Panel · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT LAVATORY SERVICE PANEL DAMAGED BETWEEN FS 965 AND FS 980 AT LONGERON 19L. REPAIRED LEFT AFT FUSELAGE SKIN PANEL IAW ABX REA D953-14063-MR.SDR ABXA9600389Skin · dentedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT FORWARD FUSELAGE SKIN AT FS 148 AND LONGERON 19R HAD A SHARP DENT THAT EXCEEDED THE DC-9 SRM LIMITS. REPAIRED RIGHT FUSELAGE FORWARD SKIN IAW ABX REA D953-13887-MR.
Back to N936AX, cancelled Feb 7, 2008