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 ABXA20150710121Longeron · crackedNUMBER 2 ENG OTBD CORE COWL LOWER FRAME CRACKED BY NR 3 LATCH. REMOVED & REINSTALLED NR 3 LATCH & LOWER FRAME IAW SRM 51-40-02 D. WELD REPAIR LOWER FRAME IAW PROCESS STANDARDS MANUAL CH 900-7-2-1. PRIMED & PAINTED LOWER FRAME IAW AMM 51-21-02 & 51-21-10. CSDR ABXA20150703140Bushing · crackedNUMBER 2 FLAP SUPPORT 1 - 3, BEAM HAS A WORN BUSHING AT JOINT 1. REPLACED NR 1 JOINT BUSHING ON THE NR 2 FLAP SUPPORT 1B BEAM IAW REA C057-61596-MR ITEM 18. CRACK UNKNOWN LENGTH, PN BACBZBAP, PART NAME BUSHING, SN NSN, LT WING. ACFT WAS GNDED.SDR ABXA20150703139Support Beam · crackedNUMBER 2 FLAP SUPPORT 1 - 3, BEAM HAS 5 HOLES WITH DEFECT INDICATIONS & 1 HOLE WITH DEFECT INDICATION & CORROSION AROUND OUTSIDE OF HOLE, FOUND WITH HFEC ROTARY SCAN. REMOVED DEFECTS FROM NR 2 FLAP SUPPORT 1 - 3, BEAM IN 5 LOCATIONS HFEC ROTARY SCAN FOUND NO SDR ABXA20150703137Support Beam · crackedNUMBER 8 FLAP SUPPORT, 1 - 3 BEAM HAS 4 HOLES WITH DEFECT INDICATION WITH ROTARY SCAN. REMOVED DAMAGE TO 4 HOLES ON NR 8 FLAP SUPPORT, 1 - 3 BEAM. HFEC ROTARY SCANNED HOLES & FOUND NO DEFECTS IAW NDT MAN PART 6 51-00-16. COMPLIED WITH C057-61597-MR. SDR INSDR ABXA20150629129Skin Panel · crackedAFT FUSELAGE EXTERNAL SKIN IS CRACKED, AT STATION 1735 FWD OF LT LOWER STAB FAIRING, SEEN FROM INSIDE. REMOVED SKIN PANELS 148T7321-1 & 148T7320-17. INSTALLED NEW SKIN PIECES. SDR INFO, CRACKED 1.5", PN 148T7321-1, SN N/A, PART NAME SKIN PANEL, FS LOCATION SDR ABXA20150624132Stringer · crackedSTRINGER 7L LOWER LEG, IS CRACKED APPROX. 2.5" AT APPROX FS 680. STRINGER WAS R & R IAW SRM 53-00-03 & SKETCH ES02821, MATERIAL PO 0064680 & PO 0037419. APPLIED PROTECTIVE COATINGS IAW SRM 51-20-01. SDR INFO, CRACKED 3", PN BAC1498-207, SN NONE, PART NAME SSDR ABXA20150617128Rib · corrodedLEFT WING LE RIB, CORRODED ON OTBD SIDE AT LES 454, IN SEVERAL PLACES. R & R LT WING LE AT LES 454 IAW SRM 51-40-02. SDR INFO, CORRODED L2, PN 114T2202-23, SN NSN, PART NAME RIB, STRINGER & WS LOCATION ON ACFT, FROM LT WING STATION WS 454. ACFT WAS GNDED.SDR ABXA20150610134Skin · crackedSKIN ON THE FWD OF THE ANTENNA AT STATION 392, STRINGER 39R HAS .125" CRACK, VERIFIED WITH HFEC. REPAIRED SMALL CRACK IAW SRM 53-00-01 REPAIR 8 FIG 201 SECTION I STEPS 1 - 3. REPAIR RECORD SUBMITTED. SDR INFO CRACKED .125, PN 141T0118, SN NSN, PART NAME FUSSDR ABXA20150606126Rib · corrodedRIGHT WING OTBD INTERNAL LE AIR LOAD STRUT HAS CORROSION, AT FWD END & ON WIRE CLAMP STANDOFF, AT APPROX LES 612, INBD OF NR 9 SLAT, OTBD AUXILIARY TRACK. R & R AIR LOAD STRUT IAW SRM 51-40-02. SDR CORRODED, LEVEL 2, PN 114T2210-16, PART NAME RIB, SN NSN, EXSDR ABXA20140710237Dcu · faultyDEFECT FIRST OFFICER'S PRIMARY FLIGHT DISPLAY & NAVIGATION DISPLAY BLANKED OUT. REPLACED DATA CONCENTRATOR UNIT. NO OTHER ACTION TAKEN & NO FURTHER FAULTS OCCURRED REGARDING THE BLANKING OF THE FIRST OFFICER'S PRIMARY FLIGHT DISPLAY & NAVIGATION DISPLAY.SDR ABXA20140212001Structure · crackedRIGHT HAND STATION 1809 FWD CHORD AT STRINGER 12R HAS AN ELONGATED HOLE. IAW NEA53800003-001 S. CHORD REPAIRED IAW EA53800002-002 & 003. REMOVED TWO EACH FASTENERS, FOUND ELONGATED HOLE, CRACK INDICATION FOUND. REAMED HOLE TO 310, REPLACED FASTENERS, TREATSDR ABXA2014021114Case · corrodedFAN EXIT CASE INNER SKIN CORRODED AT NR 7 FAN FRAME STRUT. BLENDED AREA IAW GECF6-80A ESM 70-42-00. REPAIRED AREA IAW ABX AIR REA-C072- 60864 RFTS NR E-46177 REVISION DATE 2-11-14. SDR INFO PN 9295M34G15, SN 3HY20080, AFT FAN CASE, CORRODED, RT, NAC 160.0. SDR ABXA20131014619Seal Depressor · crackedFORWARD LOWER CARGO DOOR FWD LOWER SEAL DEPRESSOR IS CRACKED. R & R SEAL DEPRESSOR IAW DWG 143T6201, 51-40-2, SEE PARTIAL WORK ACCOMPLISHED FOR WORK COMPLETED. CRACK LENGTH: .250", PN: 143T6201-27, PART NAME SEAL DEPRESSOR, LOC: 550 TO 550.SDR ABXA20131013618Intercostal · corrodedAFT LOWER CARGO CEILING PANEL ATTACH INTERCOSTAL CORRODED AT NUTPLATE BS 1410. R & R ATTACH INTERCOSTAL IAW SRM 51-40-02,SDR ABXA20131011589Keelbeam · corrodedCORROSION ON TOP SURFACE OF KEEL BEAM, FROM BL 0 TO LBL 11, BS 977 TO 1080. BLENDED CORRODED AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-50-12, FIG 101. REPAIRED IAW REA B653-60727-MR, PN: 145T8612-1, KEEL BEAM HORIZONTAL WEB CORRODED, 999 TO 1065 BLO TO LBLSDR ABXA20131009612Cargo Track · corrodedUPPER DECK CARGO TRACK AT LBL 33 BETWEEN BS 1461-1605 IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R CARGO TRACK IAW SRM 51-40-02. ACFT WAS GROUNDED.SDR ABXA20131009611Cargo Track · corrodedUPPER DECK CARGO TRACK IS CORRODED AT LBL 11, BETWEEN BS 1461- 1605. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R CARGO TRACK IAW SRM 51-40-02. ACFT WAS GROUNDED.SDR ABXA20131009610Floor Support · corrodedUPPER CARGO AFT WALL FLOOR DRAIN STRUCTURE BELOW FLOOR PANELS BS 1605 , S88L-S88R HAS CORROSION ON UPPER SURFACE. REMOVED DRAIN AND DRAIN LINES AT STA 1605, REMOVED LT AFT WALL. R & R LT AND RT OTBD FLOOR BRACES AT STA 1580 TO 1605, PICKED UP FLOOR PANEL HOLSDR ABXA20131009609Seat Track · corrodedUPPER CARGO BELOW FLOOR PANELS BETWEEN BS-1197 & BS-1605 , S88L-S88R CORROSION ON NUMEROUS CLIP NUTS AT UPPER CHORDS. FLOOR LOCK PLATES, FLOOR PANEL FASTENER LOCATIONS. R & R CORRODED CLIP NUTS IAW SRM 51-40-02. R & R CORRODED FLOOR LOCK PLATES AND SEAT TRACSDR ABXA20131009605Panel · corrodedNR 2 NACELLE PANEL AFT OF THE NR 2 HYD BAY DOOR, OTBD, HAS SEVERAL SMALL AREAS OF CORROSION, REPLACED PANEL WITH NEW PN 313T3381-84 REINSTALLED IAW AMM 20-11-00-2 AND SRM 51-40-02, PART 7. SDR: PN: 313T3381 PYLON PANEL ASSY AFT RT CORRODED, LEVEL 2 LOC: NAC SSDR ABXA20131009583Skin · corrodedLEFT WING UPPER T/E SURFACE HAS CORROSION AT LWS 1018. REMOVED CORROSION IAW SRM 57-20-01, FIG 101. REPAIRED IAW REA B657-60708. ACFT WAS GROUNDED.SDR ABXA20131009582Skin · corrodedRT WING UPPER T/E SKIN HAS CORROSION AT APPROXIMATELY RT WING STA 746.2. REPAIRED RT WING UPPER T/E SKIN AT APPROX RT WING STA 746.2 IAW REA B657-60709-MR. ACFT WAS GROUNDED.SDR ABXA20131009581Skin · corrodedRT WING UPPER T/E SKIN HAS CORROSION AT APPROX 772.2. REPAIRED RT WING UPPER T/E SKIN AT APPROXIMATELY RT WING 772.2 IAW REA B657-60709-MR. ACFT WAS GROUNDED.SDR ABXA20131009579Skin · corrodedRIGHT WING UPPER L/E SKIN AT APPROXIMATELY RWS 837 HAS HEAVY CORROSION. REPAIRED IAW REA B657-60709 MR. AFT WAS GROUNDED.SDR ABXA20131008617Channel · crackedNR 2 PYLON AFT "V" WEB IN FRONT OF THE STINGER INTERNALLY IS CRACKED. R & R CRACKED CHANNEL IAW SRM 51-40-02. PN 313T3380-244, CHANNEL, CRACKED, LENGTH 1.5" FS /BS LOC ON ACFT: NAC 410.59. ACFT WAS ON GROUND.SDR ABXA20131008615Shear Tie · corrodedSHEAR TIE AT FS 1329 BETWEEN STRINGER 39 LT AND 39 RT AFT LOWER CARGO HAS SURFACE CORROSION, MARKED. R & R SHEAR TIE AS REQUIRED IAW DWG 146T1212 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. FABRICATED PART IAW DWG 146T1212 & SRM 51-20, 51-40-02. ACFT WSDR ABXA20131008602Floorbeam · corrodedCORRODED FLOORBEAM AT DOOR CUTOUT AT BS 1329. R & R FLOORBEAM IAW DWG 146T1212.SDR ABXA20131008584Skin · corrodedREMOVED CORROSION ON LT WING UPPER T/E WS 1006 IAW SRM 57-20-01, FIG 101. REPAIRED AREA IAW REA B657-60708-MR. ACFT WAS GROUNDED.SDR ABXA20131007595Skin · corrodedWHERE THE LOWER TCAS OMNI DIRECTIONAL ANTENNA MOUNTS IT HAS LIGHT CORROSION ON SKIN. R & R EXTERNAL TCAS DOUBLER IAW SRM 51-40-02 AND SB 767-34-0087, REV 4, DATED AUG 5 1993. PN 141T0112U31, PARTNAME: ANTENNA DOUBLE CORRODED LEVEL 2 FS/BS 399 STR/WS 538. ACSDR ABXA20131004616Support · corrodedLEFT WING LOWER T/E PANEL SUPPORT BEAM FOR PANEL 551XBX IS CORRODED. REMOVED CORROSION FOUND LOWER CHORD TO BE OUT OF LIMITS. REPAIRED AREA IAW SRM 57-51-02 REPAIR 2. ACFT WAS GROUNDED.SDR ABXA20131004590Keelbeam · corrodedCORROSION ON ANGLE ON KEEL BEAM TO UPRIGHT AT BS 1043, BL0 TO LBL 11. R & R ANGLE IAW DWG 145T8610,SDR ABXA20131003614Skin · crackedANTENNA BLANKING PLATE AT BS 731 S34-35R CRACKED. REPAIRED WITH SRM REPAIR IAW SRM 53-00-01, FIG 101. ACFT GROUNDED.SDR ABXA20131003613Skin · crackedANTENNA BLANKING PLATE AT BS 731 S34-35L CRACKED. REPAIRED IAW SRM 53-00-01, FIG 101ACFT WAS GROUNDED.SDR ABXA20131001585Skin · crackedFUSELAGE SKIN COMMON TO RT LOWER HORSE COLLAR PANEL 314CRX IS CRACKED AT APPROX STA 1746. R & R SKIN SECTION 148T7321-4 IAW SRM 51-40-02 PAR 4 PG 2. REAR SDR INFORMATION: CRACKED PN 148T7321-4. PARTNAME SKIN PANEL-STAB FAIRING EXACT FS/BS LOCATION ON ACFT FSDR ABXA20130930596Floor Support · crackedBULK CARGO, BS 1461, FLOOR SUPPORT CRACKED. R & R FLOOR SUPPORT BS 1420-1540. INSTALLED IAW SRM 51-40-02. ACFT WAS GROUNDED.SDR ABXA20130930594Stringer · corrodedAFT LOWER CARGO BULK CARGO FLOOR AREA,BETWEEN BS 1417 & 1439, STRINGER 39L IS CORRODED. REMOVED 8.1 INCH SECTION OF STRINGER. LOCATED, DRILLED, AND INSTALLED REPAIR SHIM, CHANNEL, ANGLES, AND STRINGER FILLER ALONG WITH FAYE SEALING IAW SRM 53-00-03, FOG 201 SDR ABXA20130925598Floorbeam · corrodedFLOORBEAM AT BS 1087 HAS SEVERAL CORRODED NUTPLATES. REMOVED CORROSION IAW SRM 53-00-07. ACFT WAS GROUNDED.SDR ABXA20130925597Floorbeam · corrodedAFT LOWER CARGO BS 1100 LT FLOORBEAM HAS CORROSION UNDER ROLLER ASSY. INSTALLED LT AND RT OTBD ROLLER TRAYS IAW CMM 25-50-25. ACFT WAS GROUNDED.SDR ABXA20130925586Stringer Splice · crackedFORWARD LOWER CARGO BS 434 , STRINGER SPLICE 30L CRACKED. SPLICE REMOVED AND INSTALLED NEW SPLICE IAW SRM 51-40-02. SDR CRACKED 1" PN 140T0115-14, STRINGER SPLICE EXACT FS/BS LOCATION ON AC 434 TO 438 AND 30L TO 30L. ACFT WAS GROUNDED.SDR ABXA20130925580Skin · corrodedRT WING UPPER T/E SKIN HAS HEAVY CORROSION AT RWS 790. REMOVED CORROSION, ROTO PEENED REINSTALLED FASTENERS AND RESTORED FINISH IAW EA B657-60709 MR. ACFT WAS GROUNDED.SDR ABXA20130920588Splice · corrodedKEEL BEAM PANEL ATTACH CROSSMEMBER AT STA. 1013 CORRODED AROUND NUTPLATE ON UPPER SURFACE. REMOVED AND REPLACED CROSSMEMBER IAW B767-200 SRM 51-40-02. PART NUMBER: 145T8629-3, PARTNAME: SPLICE TEE, FS/BS LOC: 1008 TO 1008, STR/WS: B/L9L TO B/L9R, CORRODED, LESDR ABXA20130919603Bracket · crackedCRACKED BRACKET ON LOWER FWD END OF THE E6 RACK. R & R AND INSTALLED BRACKET ON LOWER FWD END OF E6 RACK IAW DWG 453T12B2 FOR WORK COMPLETED. ACCOMPLISHED. ACFT WAS GROUNDED.SDR ABXA20130918604Angle · crackedNR 1 NACELLE ANGLE BRACKET JUST FWD OF THE OTBD ARROW HEAD PANEL, ABOVE THE EXHAUST SEAL IS CRACKED. REPAIRED CRACKED ANGLE IAW SRM 51-40-02 AND ABX PROCESS STANDARDS MANUAL. ACFT WAS GROUNDED.SDR ABXA20130918591Attach Fitting · crackedATTACH PLATE FOR AFT END OF NR 1 CORE COWL OTBD SKIRT FAIRING IS CRACKED. REPAIRED CRACKED PLATE, INSTALLED NEW NUTPLATE AND INSTALLED PLATE ONTO PYLON IAW DWG 311T1570 AND SRM 51-40-02, PN: 311T1570-55 NAME: RIB, NACELLE 269.5. ACFT WAS GROUNDED.SDR ABXA20130918587Splice · corrodedKEEL PANEL 194AL FORWARD ATTACH CROSSMEMBER CORRODED AROUND NUTPLATE ON UPPER SURFACE. R & R CROSSMEMBER IAW SRM 51-40-02. SDR INFO - PN: 145T8629-3, SPLICE TEE FS/BS LOC: 962 TO 962, STR/WS LOC: B/L9L TO B/L9R, CORRODED, LEVEL 2. ACFT WAS GROUNDED.SDR ABXA20130917599Support Angle · corrodedCORROSION ON UNDER SIDE OF ANGLES FOR ROLLER TRAY MOUNT AT LT SIDE AT STA 1417. REMOVED ROLLER TRAY MOUNT ANGLE SUPPORTS AND REPLACED WITH NEW PARTS INSTALLED IAW SRM 51-40-02. ACFT WAS GROUNDED.SDR ABXA20130916608Cargo Track · crackedUPPER CARGO LOADING SYSTEM, LT SIDE AFT WALL CARGO TRACK CRACKED. REMOVED UPPER CARGO LOADING SYS CRACKED WALL RAIL AND REPLACED WITH A NEW CARGO TRACK IAW CMM 25-50-0288. ACFT WAS GROUNDED.SDR ABXA20130916607Seat Track · corrodedUPPER CARGO BS 1065-1197, UNDER FLOOR PANELS, SEAT TRACK CORRODED ON AND AROUND SEVERAL NUT CLIPS. CLEANED AREAS UNDER FLOOR PANELS, AND FOUND AREA BS 1145, LBL34 TO BE OUT OF LIMITS IAW SRM 53-00-52. REPAIR FABRICATED AND INSTALLED IAW REA B653-60704-MR. SDR ABXA2013110400606Angle · crackedNR 2 NACELLE ANGLE BRACE CRACKED AT OTBD AREA JUST FORWARD OF THE ARROWHEAD PANEL. R & R AFT FIRE SEAL IAW SRM 51-40-02. ACFT WAS GROUNDED.SDR ABXA20130913593Stiffener · crackedAFT LOWER CARGO, BULK CARGO FLOOR AREA BS 1439 ABOVE STRINGER 38R FLOOR SUPPORT VERTICLE STIFFENER IS CRACKED IN TWO PLACES. REMOVED, LOCATED, DRILLED AND INSTALLED REPLACEMENT STIFFNER IAW DWG 146T1217. ACFT WAS GROUNDED.
Back to N745AX