N745AX
Service difficulty reports · 269
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 = 'N745AX' AND registry_match = 'registration' 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 = 'N745AX' AND registry_match = 'registration' 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 ABXA20130906592Mount · corrodedNR 2 ENGINE LT SIDE OF AFT MOUNT HAS MINOR CORROSION AND LT SIDE LINK HAS PITTING. R & R NR 2 ENGINE AFT MOUNT AS REQUIRED, WITH A NEW ENGINE MOUNT, IAW AMM 71-21-02-4. CORROSION, PN: 310T1020-3, MOUNT, AFT ENG, SN: 48. NAC 308.50. ACFT WAS GROUNDED.SDR ABXA20130905601Angle · corrodedCEILING PANEL ATTACH ANGLE CORROSION AT BS 1351. R & R CEILING SUPPORT ANGLES IAW SRM 51-40-02. ACFT WAS GROUNDED.SDR ABXA20130905600Angle · corrodedCEILING PANEL ATTACH ANGLES CORRODED AT STA 1263. R & R ANGLES LBL27-RBL40 IAW SRM 51-40-02 CLEANED TREATED AND PRIMED CORROSION ON ANGLE RBL 40 & RBL 66 IAW SRM 53-00-51, FIG 101. FOUND TO BE WITHIN LIMITS. ACFT WAS GROUNDED.SDR ABXA20130703477Fire Detector · false indicationPASSING 5500 FT, WHEEL WELL FIRE WARNING INDICATED. PERFORMED WW AREA INSPECTION ACC FIM 26-17-09-00 FOR DAMAGE. NO PNEUMATIC LEAK EVIDENCE. NO OBVIOUS DAMAGE AND NO SENSOR DEFECTS NOTED. APPLIED FIM 26-17-09-1 FIRE WARNING TEST. ALL STEPS WERE VERIFIESDR ABXA20130511431Duct · blownON TAKEOFF ROLL LOUD POP HEARD, AFTER TAKEOFF SEVERAL STATUS MESSAGE CAME ON; BODY OVERHEAT ON, ADP PRESSURE LIGHT ON, AND CABIN ALT AUTO ON. DUCT LEAK NOTICED. FOUND PNEUMATIC DUCT BLOWN AT STA 1249, ALONG WITH SMOKE DETECTOR TUBING DAMAGED, BODY OVERHEAT DSDR ABXA20130424427Fire Warning · false activationWHEEL WELL FIRE EICAS INDICATION DURING CLIMBOUT. RAN NON-NORMAL, EICAS WARNING EXTINGUISHED. FOLLOWED FIM PROCEDURE 26-17-00-1 AND ALL CHECKS AND REQUIREMENTS ACCOMPLISHED. ALSO INTERROGATED BRAKE TEMPERATURE MONITOR AND PHYSICALLY CHECKED BRAKE UNITS FOR SDR ABXA20121209343Mechanism · out of positionLEFT OVERWING ESCAPE SLIDE DOOR OPEN. UPON INSPECTION FOUND THAT THE INTERLOCK CONTROL ROD LATCH MECHANISM WAS IN THE DOWN POSITON (OPEN). LOCKED THE ROD LATCH MECHANISM BACK INTO THE CLOSED POSITION IAW AMM 25-65-09-4. ACFT WAS GROUNDED.SDR ABXA20120216161Stringer · crackedSTRINGER 22 LT CRACKED JUST AFT OF BS 676, AIRCRAFT GROUNDED. REPAIRED IAW REA B653-59624-MR.SDR ABXA20120215296Web · corrodedWEB PANEL (FLOOR) CORRODED AT SCREWS STA 527 RBL 22. FABRICATED NEW FLOOR WEB PER SAMPLE IAW B767 SRM 53-30-53 FIG 1. AIRCRAFT WAS GROUNDED.SDR ABXA20120215283Stringer Clip · crackedSTRINGER CLIP IS CRACK AT STA 720 STR 39L. INSTALLED NEW STRINGER CLIP PN 140T2101-413 AT STA 720 STR 39L IAW THE BOEING 767-200 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA20120215282Stringer Clip · crackedSTRINGER CLIP IS CRACK AT STA 720 STR 37L. INSTALLED NEW STRINGER CLIP P/N 140T2101-413 AT STA 720 STR 37L IAW THE B767-200 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA20120215205Skin · crackedFUSELAGE SKIN HAS 2.5 IN CRACK, STA 785 S35L. INSTALLED PNL 193FL IAW B767 AMM 20-11-00. REPAIRED FUSELAGE SKIN IAW B767 SRM 53-00-01, FIG 201.SDR ABXA20120214242Web · tornWEB STA 588 TO 566 HAS TORN FASTENER HOLES. REPLACED FLC FLOOR WEB AT STA 566 TO 588 WITH NEWLY FABRICATED ONE PER SAMPLE IAW B767 SRM 51-40-02 AND BOEING DWG 143T500. AIRCRAFT WAS GROUNDED.SDR ABXA20120214226Stringer · corrodedSTRINGER 34L HAS EXFOLIATION CORROSION BETWEEN FS 522 AND 544.0. REPLACED CORRODED SECTION OF STRINGER 34L IAW B767-200 SRM 53-00-03 FIG 201. AIRCRAFT WAS GROUNDED.SDR ABXA20120214168Doubler · corrodedCORROSION FS 742 UPPER SIDE OF STRINGER 35L ON SKIN DOUBLER. REMOVED AND REPLACED TEAR STRAP PN 143T3222-11 IAW DWG 143T3220 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA20120213302Support Bracket · corrodedFLOOR PANEL SUPPORT BRACKET ON WEB AT STA 522-544 RT BL 22 CORRODED. FABRICATED ANGLE PER SAMPLE AND INSTALLED THEM TO WEB PANEL IAW B767 SRM 51-04-02 AND BOEING DWG 143T5000. AIRCRAFT WAS GROUNDED.SDR ABXA20120213297Intercostal · corrodedFLOOR WEB ATTACH "Z" INTERCOSTAL CORRODED AT STA 610 RBL 22. REMOVED AND REPLACED INTERCOSTAL P/N 143T5000-36 IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA20120212238Fitting · corrodedBOX BEAM UPPER CAP FITTING CORRODED BETWEEN STA. 522 AND 544 AT LBL 38. REMOVED AND REPLACED BOX BEAM UPPER CAP FITTING P/N 143T5000-18 BETWEEN STA 522 TO 544 AT LBL 38 IAW B767-200 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA20120212235Angle · corrodedBOX BEAM PANEL STA 610-632 FLC HAS CORRODED L ANGLE AND SKIN PANEL. WEB AND L ANGLE FABRICATED IAW BOEING DWG 143T5000. AIRCRAFT WAS GROUNDED.SDR ABXA20120212234Web · corrodedBOX BEAM PANEL STA 610-632 FLC HAS CORRODED L ANGLE AND SKIN PANEL. WEB AND L ANGLE FABRICATED IAW BOEING DWG 143T5000. AIRCRAFT WAS GROUNDED.SDR ABXA20120211243Skin · corrodedLOWER FUSELAGE SKIN NEEDS REMOVED FROM BS 434 TO BS 786 DUE TO INTERNAL CORROSION. REMOVED AND RE-INSTALLED CENTER BELLY SKIN STA 434-785.9 S36L - 36R IAW BOEING DWG 143T3220 AND B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA20120211287Tear Strap · corrodedTEAR STRAP AT STA 632 S-36L CORRODED. FABRICATED PER SAMPLE AND INSTALLED NEW TEAR STRAP P/N 143T3222-8 IAW B767 SRM 51-40-02 AND BOEING DWG 14332220. AIRCRAFT WAS GROUNDED.SDR ABXA20120211265Tear Strap · corrodedSTA 544 TEAR STRAP HAS CORROSION. FABRICATED SAMPLE AND INSTALLED NEW TEAR STRAP P/N 143T3222-5 IAW B767 SRM 51-40-02 AND BOEING DWG 143T3220. AIRCRAFT WAS GROUNDED.SDR ABXA20120211264Tear Strap · corrodedSTA 566 BELLY TEAR STRAP HAS CORROSION. FABRICATED PER SAMPLE AND INSTALLED NEW TEAR STRAP P/N 143T3222-6 IAW B767 SRM 51-40-02 AND BOEING DWG 14332220. AIRCRAFT WAS GROUNDED.SDR ABXA20120211263Tear Strap · corrodedSTA 610 TEAR STRAP HAS CORROSION. FABRICATED PER SAMPLE AND INSTALLED NEW TEAR STRAP P/N 143T3222-5 IAW B767 SRM 51-40-02 AND BOEING DWG 14332220. AIRCRAFT WAS GROUNDED.SDR ABXA20120210298Terminal Block · corrodedTERMINAL BLOCK HEAVILY CORRODED AT STA 588-610 - S32L. REMOVED AND INSTALLED NEW GROUND BLOCK TO STRINGER IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.SDR ABXA20120210269Tear Strap · corrodedSTA 456 TEAR STRAP HAS CORROSION. REMOVED, FABRICATED NEW AND INSTALLED TEAR STRAP IAW B767 SRM51-40-02 AND DWG 143T3220. AIRCRAFT WAS GROUNDED.SDR ABXA20120210268Tear Strap · corrodedSTA 478 S36-37L TEAR STRAP HAS CORROSION. REMOVED, FABRICATED NEW AND INSTALLED TEAR STRAP IAW B767 SRM 51-40-02 AND DWG 143T3220. AIRCRAFT WAS GROUNDED.SDR ABXA20120210267Tear Strap · corrodedSTA 500 TEAR STRAP HAS CORROSION. REMOVED, FABRICATED NEW AND INSTALLED TEAR STRAP IAW B767 SRM51-40-02 AND DWG 143T3220. AIRCRAFT WAS GROUNDED.SDR ABXA20120210266Tear Strap · corrodedSTA 522 TEAR STRAP HAS CORROSION. SEE PARTIAL WORK ON BACK. REMOVED, FABRICATED NEW AND INSTALLED TEAR STRAP IAW B767 SRM51-40-02 AND DWG 143T3220. AIRCRAFT WAS GROUNDED.SDR ABXA20120210262Tear Strap · corrodedSTA 676 TEAR STRAP HAS CORROSION. FABRICATED PER SAMPLE AND INSTALLED NEW TEAR STRAP P/N 143T3222-1 IAW B767 SRM 51-40-02 AND BOEING DRAWING 143T3220. AIRCRAFT WAS GROUNDED.SDR ABXA20120210261Tear Strap · corrodedSTA 786 CTR DOUBLER TEAR STRAP HAS CORROSION. FABRICATED AND INSTALLED NEW CENTER TEAR STRAP, IAW B767 SRM 51-40-02, BOEING DWG 143T3220. AIRCRAFT WAS GROUNDED.SDR ABXA20120210248Tear Strap · corrodedTEAR STRAP AT STA 434 BETWEEN S-39L AND S-38L HAS CORROSION. FABRICATED NEW AND INSTALLED TEAR STRAP IAW B767 SRM51-40-02 AND DWG 143T3220. AIRCRAFT WAS GROUNDED.SDR ABXA20120210197Skin · corrodedFUSELAGE SKIN CORRODED FS 620 UPPER SIDE OF STRINGER 36L. REPAIRED DAMAGED AREA OF SKIN P/N 143T3210 IAW ABX REA B653-59660-MR, ACFT WAS GROUNDED.SDR ABXA20120210187Tear Strap · corrodedTEAR STRAP AT FS 654 BETWEEN STRINGERS 35L AND 36L CORRODED. REMOVED, FABRICATED NEW, AND INSTALLED TEAR STRAP IAW B767 SRM 51-40-02 AND DWG 143T3220, ACFT WAS GROUNDED.SDR ABXA20120210184Tear Strap · corrodedCORROSION AT FS 742 UPPER SIDE OF STRINGER 34L ON TEAR STRAP. REMOVED TEAR STAP, FABRICATED AND INSTALLED NEW TEAR STRAP IAW B767 SRM 51-40-02 AND BOEING DWG, AWG.SDR ABXA20120210181Doubler · corrodedFUSELAGE SKIN DOUBLER CORRODED. REMOVED FUSELAGE SKIN DOUBLER FABRICATED NEW AND INSTALLED IAW B767 SRM 51-40-02 AND DWG 143T3220, AWG.SDR ABXA20120210178Tear Strap · corrodedSKIN TEAR STRAP CORRODED. REPLACED TEAR STRAP IAW B767 SRM 51-40-02 AND DWG 143T3220.SDR ABXA20120210177Attach Fitting · corrodedWEB ATTACHMENT FITTING TO STRINGER 38L IS CORRODED. INSTALLED NEW ATTACH ANGLE IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA20120210169Doubler · corrodedCORROSION FS 742 UPPER SIDE OF STRINGER 36L ON SKIN DOUBLER. INSTALLED NEW TEAR STRAP IAW B767 SRM 51-40-02 AND BOEING DWG 143T32220. AIRCRAFT WAS GROUNDED.SDR ABXA20120210203Rib · corrodedRT WING L/E EDGE RIB WS 433.1 INBD OF THE TAI DUCT IS CORRODED ON THE OUTBD SIDE. REPLACED RIB AT STA 433.1 IAW B767-200 SRM 51-40-02. REPLACED RIB AT STA 433.11. CORROSION REMOVED & REPLACED RIB AT STA 433.11.SDR ABXA20120210162Rib · corrodedINBOARD RIB, ADJACENT TO NR 5 SLAT OUTBOARD AUXILARY TRACK CORRODED AROUND NUT PLATE, AIRCRAFT GROUNDED. REMOVED & REPLACED RIB IAW REA B767-59641.SDR ABXA20120209191Support · corrodedDRAIN MAST SUPPORT STRUCTURE BETWEEN STRINGERS 34L AND 35L & FS 632 AND 654 CORRODED. REMOVED & REPLACED DRAIN MAST SUPPORT STRUCTURE IAW B767-200 SRM 51-40-02, ACFT WAS GROUNDED.SDR ABXA20120209190Support · corrodedDRAIN MAST SUPPORT STRUCTURE BETWEEN STRINGERS 34L AND 35L & FS 632AND 654 CORRODED. REMOVED & REPLACED DRAIN MAST SUPPORT STRUCTURE IAW B767-200 SRM 51-40-02.SDR ABXA20120209189Support · corrodedDRAIN MAST SUPPORT STRUCTURE BETWEEN STRINGERS 34L AND 35L & FS 632 AND 654 CORRODED. REMOVED & REPLACED DRAIN MAST SUPPORT STRUCTURE IAW B767-200 SRM 51-40-02, ACFT WAS GROUNDED.SDR ABXA20120208275Skin · damagedBELLY SKIN INT CORRODED FS 676-698, 36L. REPAIRED DAMAGE SKIN AREA AT STA 676 S36L LOWER SKIN P/N 143T3220 IAW B767-200 SRM 53-00-01 FIG 201 REPAIR 12. REPAIR IS A CAT B REPAIR SEE 53-00-01 FIG 201 REPAIR 12 TABLE III FOR REINSP REQUIREMENTS. AIRCRAFT WAS GSDR ABXA20120207204Flange · chafedNR 1 PYLON PNL 437ELX LWR ATTACH FLANGE INSIDE PYLON STRUCTURE CHAFED THROUGH. REMOVED AND REPLACED ATTACH FLANGE IAW B767-200 SRM 51-40-02 & B. DWG #311T1380. #3 FITTING TO BE INSTALLED ON NR 0961.SDR ABXA20120205 303Shear Tie · corrodedSHEAR TIE AT STA 610 S36-37R CORRODED. REPLACED SHEAR TIE AT STA 610 S36R-S37R IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA20120205301Stringer · corrodedSTRINGER 35L CORRODED STA 598 TO 610. INSTALLED NEW SECTION OF STRINGER IAW B767 SRM 51-40-02 AND 53-00-03. AIRCRAFT WAS GROUNDED.SDR ABXA20120205300Stringer · corrodedSTRINGER 35L CORRODED STA 598 TO 578. INSTALLED NEW SECTION OF STRINGER IAW B767 SRM 51-40-02 AND 53-00-03. AIRCRAFT WAS GROUNDED.
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