N797AX
Service difficulty reports · 155
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 = 'N797AX' 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 = 'N797AX' 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 ABXA2014040867Stringer · corrodedAFT LOWER CARGO STRINGER 36R CORRODED BETWEEN STATION 1395 & 1417. REPAIRED STRINGER 36R FROM FS 1384 TO 1406 IAW SRM 53-00-03 FIG 201 REPAIR 2. PN 146T3003-12, STRINGER, CORRODED, FS 1384 TO FS 1406, STRINGER 36R. ACFT WAS GNDED.SDR ABXA2014040865Fitting · crackedAFT LOWER CARGO LT SIDE STA 1087 OTBD LT ROLLER SUPPORT INTERCOSTAL TIE IS CRACKED AT BOTTOM RIVET. AFT LOWER CARGO LT SIDE STA 1087 OTBD LT ROLLER SUPPORT INTERCOSTAL, R & R CLIP. REINSTALLED INTERCOSTAL SRM 51-40-02. IAW DWG 451T 1302 & AMM 25-53-02. PN 4SDR ABXA2014040768Structure · corrodedTHE BULK CARGO DOOR, INTERIOR AREA, JUST AFT & ABOVE THE INNER HANDLE THERE IS CORROSION AT THE MISSING NUTPLATE. REMOVED 2 CORRODED CHORDS, REPLACED CHORDS WITH NEW FABRICATED CHORDS IAW SRM 51-40-02, DWG 146T6301 & SRM 52-30-01. PN 146T6342-1, 146T6319-5, SDR ABXA2014040362Bracket · crackedBELOW FLOOR PANEL 221A FOUND ANGLE BRACKET ON FLOOR BEAM CRACKED AT COCKPIT ENTRANCE. R & R ANGLE BRACKET IAW 141T5198 & SRM 51-40-02. SDR INFO CRACKED .4 INCHES, PN 141T5198-6, FS & BS LOC FROM STA 266.5 TO LBL 14. ACFT WAS GNDED.SDR ABXA2014032869Skin · corrodedCORROSION FOUND BETWEEN RIBS 1R & 1L LOWER STRINGERS BETWEEN 4 & 5 ON HORZ STAB SKIN. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. .020 INCHES MATERIAL LOSS OUT OF .015 INCHES ALLOWABLE. CUT OUT DAMAGE & REPAIRED IAW SRM 55-10-01 FIG 201 REPAIR 2. SDR CORROSDR ABXA20130724484Warning Message · false activationPASSING FL 260, LT FWD ENTRANCE DOOR MESSAGE ILLUMINATED. CHECKED IAW MM 52-11-00-6, OPS CHECKED NORMAL AND DOOR WARNING SYS OPS IAW 52-71-00-5. OPS CHECKED GOOD, ACFT WAS GROUNDED.SDR ABXA20130501429Actuator · failed27 81 05 00 EICAS MSG L/E SLAT ASYM DISPLAYED, LEADING EDGE LIGHT ILLUM WITH THE FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. UPON WALK AROUND MAINTENANCE FOUND THE NUMBER 8 SLAT INBOARD PORTION EXTENDED AND OUTBOARD PORTION RETRACTED. FURTHER INVESSDR ABXA20120802241Door Frame · corrodedLEFT OVERWING EXIT CUTOUT FRAME CORRODED ALONG THE AFT SIDE MIDWAY UP. CUT OUT CORRODED SECTION AND REPAIRED PER REA B653-59933-MR, ACFT WAS GROUNDED.SDR ABXA20120801242Spar · corrodedCORROSION FOUND IN 2EA PLACES ON RIGHT WING UPPER SURFACE AT REAR SPAR UNDER T/E PANEL AT WS 261 AND WS 236. DEEP EXFOLIATION AT BOTH LOCATIONS. BLENDED AREAS ARE COMPLIED WITH ON REA B657-59956-MR, ACFT WAS GROUNDED.SDR ABXA20120801240Doubler · corrodedWING TRAILING EDGE PANEL FORWARD OF OUTBOARD AILERON HAS RAISED AREAS AT LEADING EDGE STA 927, 936, 981 APPROX ON UPPER SURFACE. REMOVED AND REPLACED DOUBLERS & FILLERS TO COMPLETE MAINTENANCE. INSTALLED ON REA B657-59950-MR, ACFT WAS GROUNDED.SDR ABXA20120730227Rib · crackedNUMBER 5 SLAT OUTBOARD DRIVE ROD CUTOUT OUTBOARD NOSE RIB CRACKED. MANUFACTURED RIB IAW BOEING DWG 114T2511 REMOVED OLD RIB & REPLACED WITH NEW PART. WORKED IAW DWG 114T2511, B767 SRM 51-40-2 PAGE 7D, 51-20-01 METAL PO#0016868. HEAT TREAT IAW BAC 5602, BAC SDR ABXA20120725232Beam · corrodedAREA OF CORROSION ON LOWER T-CAP OF UPPER PANEL ATTACH BEAM INBOARD OF GEAR AT WS 255, 23 INCHES FROM LEADING EDGE. BLENDED CORROSION SIZE:7.25 LONG X 1.00 WIDE LOCATION: WS 255, OUTBOARD HORZ FLANGE OF LWR CHORD. ON LOWER TEE CAP OF ATTACH BEAM AT WS 255. FSDR ABXA20120724243Beam · corrodedWING STA 819 EXFOLIATION CORROSION FOUND ON LOWER SURFACE OF RIGHT WING T/E PANEL SUPPORT BEAM AT WS 257, 22 INCHES AFT OF AFT WING SPAR UNDERNEATH "I" BEAM SUPPORT. BLENDED CORROSION IAW REA B657-59954-MR, ACFT WAS GROUNDED.SDR ABXA20120723231Stringer · crackedSTRINGER 9L HAS A 5 INCH CRACK AT THE UPPER RADIUS AND LOWER RADIUS LOCATED AT THE AFT SPLICE PLATE STA 676. REPLACED STRINGER CLIP AND REPAIRED STRINGER IAW REA B653-59940-MR SRM 51-40-02.SB-44/350771, ACFT WAS GROUNDED.SDR ABXA20120723226Rib · corrodedNUMBER 8 SLAT INBOARD AUX TRACK ATTACH FITTING OUTBOARD LOWER RIB HAS CORROSION AROUND NUT PLATES. LOWER RIB REPLACED UNDER NR 8 SLAT INBOARD AUX TRACK ATTACH FITTING OUTBOARD & NEW NUT PLATES INSTALLED IAW B767 SRM 57-41-09, ACFT WAS GROUNDED.SDR ABXA20120721233Skin · corrodedRIGHT WING LEADING EDGE OF WING TRAILING EDGE UPPER PANEL AT STA 819 APPROX HAS RAISED SPOT. REMOVED PANEL, FOUND CORROSION, BLENDED OUT OF LIMITS PER SRM 57-20-01. COMPLIED WITH B657-59951-MR, ACFT WAS GROUNDED.SDR ABXA20120720234Skin · corrodedLEFT WING UPPER T/E WING SKIN AT STA 466, 505, AND 532 ARE CORRODED. REMOVED CORROSION FROM UPPER T/E WING SKIN IAW B767 SRM 57-20-01. REPAIRED UPPER T/E WING SKIN AT WS 505, 532 IAW AMES REA B657-55943-MR. TREATED & PRIMED AREAS IAW B767 SRM 51-20-01, ACFT SDR ABXA20120719230Stringer · crackedSTRINGER 8L HAS A 4 INCH CRACK AT THE UPPER RADIUS LOCATED AT THE AFT SPLICE PLATE STA 676. REPAIRED STRINGER 8 IAW REA 653-59940-MR, ACFT WAS GROUNDED.SDR ABXA20120718229Cowling · wornNR 1 ENGINE INBOARD CORE COWL TRAILING EDGE WORN TO SHARP EDGE IN SEVERAL PLACES. REPLACED NR 1 INBOARD CORE COWL T/E STRAP IAW 767 SRM 51-40-02 AND CMM 71-11-45. SEE PWA & PWS #30 FOR DETAILS. CORE COWL RE-INSTALLED ON NR 0676, ACFT WAS GROUNDED.SDR ABXA20120714228Rib · crackedNUMBER 4 SLAT OUTBOARD DRIVE ROD CUTOUT INBOARD NOSE RIB CRACKED. REMOVED AND REPLACED NR 4 SLAT I/B DRIVE ROD CUTOUT I/B NOSE RIB IAW B767 SRM 51-40-02 REF DRAWING 114T2512, ACFT WAS GROUNDED.SDR ABXA2011030908Inertia Reel · out of positionSAFETY INERTIAL REEL FELL OUT ON APPROACH. SUPERNUMERARY COMPARTMENT. STOWED DESCENT DEVICE IAW B767 AMM 25-61-03.SDR ABXA201011240160Support Beam · corrodedCORROSION ON BEAM AFT OF LEFT MLG AFT TRUNNION. PANEL SUPPORT BEAM RUNS INBOARD TO OUTBOARD VIEWED FROM 552AB LOOKING UP. OPEN PANEL FOM REMOVED AND REINSTALLED SUPPORT RIB. RE-INSTALLED PANEL IAW BOEING 767 SRM 51-40-2.SDR ABXA201011190159Support · corrodedLEFT, I/B AILERON, I/B AILERON HINGE SUPPORT RIB UPPER NUT PLATE CHANNEL IS CORRODED ON BOTH SIDES OF SUPPORT AND RIB AS MARKED. REMOVED AND REPLACED TEE P/N 113T1510-33AX IAW AMM 51-40-2. LEAK CHECK GOOD IAW B767 AMM 28-11-00.SDR ABXA201011190457Beam · corrodedCORROSION ON BEAM, AFT OF RT MLG AFT TRUNNION - BEAM RUNS INBOARD TO OUTBOARD VIEWED FROM 652 AB LOOKING UP. REMOVED AND REPLACED IAW 767 SRM 51-40-2.SDR ABXA201011190158Support Fitting · corrodedAREA OF CORROSION AT APPROX WS 450 WHERE LT AILERON DROOP MECHANISM - TO AFT SPAR ATTACH ANGLE. REMOVED AND REPLACED VERTICAL SUPPORT FITTING IAW B767 AMM 51-40-02. LEAK CHECK GOOD IAW B767 AMM 28-11-00.SDR ABXA201011240164Support Beam · crackedLEFT ENG PYLON HYD ACCESS BAY OUTBOARD SUPPORT BEAM IS CRACKED THRU NUT PLATE, COMMON TO PANEL 437ELX. INSTALLED NEW LEFT WING ENG PYLON HYD ACCESS BAY SUPPORT BEAM IAW B767 SRM 51-40-2.SDR ABXA201011120150Rib · corrodedCORROSION AROUND PANEL ATTACH NUT PLATES ON NR 3 SLAT I/B AUX TRACK I/B AND O/B RIBS. REMOVED AND REPLACED RIB IAW 767-200 SRM 51-40-02.SDR ABXA201011120149Rib · corrodedNR 2 SLAT I/B AUX TRACK FITTING O/B RIB CORRODED AROUND PANEL ATTACH NUT PLATES AND SHIM PACK FOR FITTING. REMOVED NR 2 SLAT I/B AUX TRACK I/B AND O/B LOWER RIBS. INSTALLED NEW RIBS IAW 767 SRM 51-40-02.SDR ABXA201011120147Rib · corrodedNR 9 SLAT I/B AUX TRACK ATTACH FITTING I/B RIB HAS CORROSION UNDER PANEL ATTACH NUT PLATES. REMOVED AND REPLACED RIB ON NR 9 SLAT I/B AUX TRACK ATTACH FITTING IAW B767 SRM 57-40-02.SDR ABXA201011120146Rib · corrodedWING L/E PANEL ATTACH NUT PLATE HAS CORROSION UNDER IT AT NR 10 SLAT BETWEEN O/B AUX AND MAIN TRACK. REMOVED AND REPLACED DAMAGED RIB AND CLOSE OUT NOSE BEAM WEB ON LT WING SLAT O/B AUX TRACK O/RIB IAW B767-200 SRM 51-40-02.SDR ABXA201011240161Rib · corrodedNR 9 SLAT STRUT RIB IS CORRODED (LOCATED I/B OF THE O/B AUX TRACK). REMOVED AND REPLACED NR 9 SLAT STRUT RIB I/B OF THE O/B AUX TRACK IAW B767 SRM 51-40-02.SDR ABXA20101124163Attach Angle · corrodedPANEL ATTACH ANGLE AT STA 913 BETWEEN LT AND RT KEEL BEAM IS CORRODED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02.SDR ABXA201011240162Attach Angle · corrodedPANEL ATTACH ANGLE AT STA 958 BETWEEN LT AND RT KEEL BEAM IS CORRODED. REMOVED AND REPLACED IAW BOEING 767 SRM 51-40-2.SDR ABXA201011170155Panel · crackedNR 4 SLAT I/B DRIVE ROD CUTOUT I/B NOSE RIB CLOSING PANEL CRACKED. REMOVED, FABRICATED NR 4 SLAT I/B DRIVE ROD CUTOUT I/B NOSE RIB CLOSING PANEL IAW DWG 114T25-12. INSTALLED RIB IAW B767 SRM 51-40-02 REMOVED AND REPLACED SLAT TRACK CURTAIN FOR NR 4 SLAT I/B SDR ABXA201011120145Plate · corrodedFWD INBOARD CORNER OF BULK CARGO DOOR LOWER SILL UPPER SURFACE CORRODED. FOUND CORROSION BEYOND LIMITS. REPLACED BULK CARGO DOOR LOWER SILL FLOOR PLATE AND RE-SEALED IAW BOEING 767 DWG 146T8211 AND SRM 51-40-02.SDR ABXA201011090142Skin · damagedFOUND FWD SKIN AT LT STAB HORSE COLLAR DAMAGED. REMOVED DAMAGED SKIN FROM AIRCRAFT MANUFACTURED NEW SKIN IAW 767 SRM 53-80 SECTION 48 PAGE 1 DETAIL 1 PO 407827176. INSTALLED NEW SKIN IAW 767 SRM 51-40-2. RE-INSTALLED I/B LOWER SEAL PANEL IAW SRM 51-40-2.SDR ABXA201011090140Stiffener · gougedNR 1 PYLON AFT FAIRING (STRINGER) 437DB INNER STIFFENER OUTBOARD SIDE IS GOUGED. FABRICATED NEW INNER STIFFENER FOR NR 1 PYLON AFT FAIRING AND INSTALLED FABRICATED STIFFENER IAW B767-200 SRM 54-51-71.SDR ABXA201011090141Skin · chafedSKIN CHAFED THRU ON LEFT SIDE FUSELAGE WHOLE LOWER HORSE COLLAR OPERATES. REPAIRED AREA IAW 767 SRM 53-80-01.SDR ABXA201008200104Warning System · false activationLEFT FWD ENTRY DOOR LIGHT ILLUMINATED INFLIGHT DOOR HANDLE RAISED OUT OF POSITION. INSPECTED BOTH OUTER AND INNER DOOR HANDLES FOR OPERATION PER MM 52-11-2-5-5 BOTH WERE GOOD. COMPARED TO L1 AND R1 DOOR HANDLES AND OPERATION BOTH WERE THE SAME. CHECKED RIG SDR ABXA201006120089Handle · poppedEICAS MSG FWD ENTRY DOOR ILLUMINATED INFLIGHT 3 TIMES DOOR HANDLE POPPED SLIGHTLY OPEN EACH TIME, BUT WOULD NOT REMAIN IN FULL LOCKED POSITION. INSPECTED DOOR HANDLE & MECHANISM FOR WEAR. ALL WAS GOOD. INSPECTED DOOR PROX SW 194 & 195. BOTH WERE 52-11-25-5SDR ABXA200903130015Fitting · crackedDURING C-CHECK AT ILN, MAINTENANCE FOUND A CRACK INDICATION DURING AFTER MODIFICATION INSPECTION OF THE RIGHT FORWARD OUTER CHORD AND TENSION FITTING PER A/B 767-53A0078, AS MANDATED BY AD 2005-11-02. THREE DISCREPANT FASTENER HOLE LOCATIONS WERE OVERSIZED TOSDR ABXA200903130014Bulkhead · crackedDURING C-CHECK INSPECTION, FOUND LWW BULKHEAD STA 1065 HAD BULGE AT LOWER HYDRAULIC FITTING LBL 70. FOUND CRACK ON STRUCTURE UNDER FITTING. BULKHEAD REPAIRED IAW B767 SRM 51-70-13 FIG 1. CRACK REQUIRED CUTOUT AND DOUBLER. CUT OUT CRACK AND FABRICATED DOUBLSDR ABXA070236Wire · detachedR1 EMERGENCY EXIT LIGHT DID NOT ILLUMINATE WHEN EMERGENCY TEST SWITCH WAS DEPRESSED. FOUND WIRES TO EXIT LIGHT NOT ATTACHED. CHECKED AND ATTACHED WIRES, OPS CHECKED GOOD IAW BOEING MM.SDR ABXA070235Wire · out of positionEMERGENCY 02 TEST LIGHT WOULD NOT PRESS TO TEST (INOPERATIVE) SUPERNUMERARY AREA. REPOSITIONED WIRING AT DEPRESS LIGHT L9003 IAW WDM 33-24-11. OPS CHECKED GOOD IAW BOEING MM.SDR ABXA070216Skin · debondedLEFT ELEVATOR OUTBOARD HAD INTERPLY DISBOND AT EACH ACTUATOR FITTING AREA ON LOWER LEADING EDGE. REPLACED LEFT ELEVATOR ON NON ROUTINE 0395 IAW BOEING SRM.SDR ABXA070215Rib · corrodedCORROSION WS 564, RIGHT WING LEADING EDGE PANEL SUPPORT/RIB. REPLACED STRUT RIB IAW B767 SRM 51-40-02.SDR ABXA070214Rib · corrodedCORROSION WS 720, RIGHT WING LEADING EDGE LOWER PANEL SUPPORT/RIB. REPLACED STRUT RIB IAW B767 SRM 51-40-02.SDR ABXA070213Pin · corrodedRIGHT HORIZONTAL STABILIZER PIVOT PIN HAD CORRODED PITTING IN THREADS. REPLACED PIVOT PIN IAW JOB CARD 7302001.SDR ABXA070212Doubler · crackedL1 DOOR CUTOUT LOWER CORNER INTERNAL DOUBLER AFT CORNER HAD CRACK INDICATION. TWO CRACKS, ONE .275 INCH AND ONE .210 INCH. REPAIRED AREA IAW REA B653-55867-MR.SDR ABXA070211Pin · crackedLEFT OUTER HORIZONTAL STABILIZER PIVOT PIN CRACKED. REPLACED PIVET PIN AND OUTBOARD PIVOT SPACER IAW B767 JOB CARD 7302001.
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