N467AW
Service difficulty reports · 166
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 = 'N467AW' 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 = 'N467AW' 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 A6WA202401318710Skin · dentedEXTERNAL SKIN ON FUSELAGE HAS 3 DENTS WITH CREASE AT FS 589 TO FS621 BETWEEN STRG21R AND STRG22R. AIRCRAFT HAS BEEN REMOVED FROM SERVICE. REPAIRED FWD AND AFT FUSELAGE SKIN AT FS 589.00 STR17R REF REO 601R-53-61-8146 REV -- DATED 2024-01-25.SDR A6WA202401318709Skin · dentedREF WO 332477 MXWC #4 DAMAGE TO FUSELAGE AT FS587 BETWEEN STR17R-STR18R DENT MEASURES 3" X 3.2" X .045 DEPTH. DAMAGE TO UNDERLYING FRAME SECTOR AT FS589 AND STRINGER 17R ALSO NOTED. TROUBLE SHOOT AND REPAIR AS REQUIRED. AIRCRAFT HAS BEEN REMOVED FROM SERVICE. SDR A6WA202401318708Frame · corrodedCORROSION FOUND ON FRAME AT FS589 R/H BETWEEN STRINGER 22R-24R ***** AIRCRAFT REMOVED FROM SERVICE ***** LOCATED AND DRILLED NEW FRAME SECTION AT FS 589 SEE JOB HN00131220 FOR INSTALLSDR A6WA202304028531Unknown · unknownINFLIGHT RECEIVED DISPLAY COOL CAUTION MESSAGE. MESSAGE BECAME INTERMITTENT. EXTINGUISHED AND REMAINED OUT BELOW FL140. *****AIRCRAFT REMOVED FROM SERVICE******** FOUND DUCT TO DISPAY COOL PLENUM OFF. REATTACEHD DUCT IN REF TO AMM 21-24 OPS CHECK GOOD.SDR A6WA202301298509Doubler · dentedDENT ON AFT FUSELAGE SKIN AT FS589-605 AND BETWEEN S22R -25R. ADDITIONAL DAMAGE TO FS574-589 AND S22R TO 25R. FASTENERS INSTALLED FOUND CLOSE TO RADIUS OF STRINGER & WEAR DAMAGE TO STRINGER FLANGE DUE TO DOOR. LATCH WEAR. PERFORMED TEMPORARY REPAIR TO SKIN, SDR A6WA202301298498Unknown · unknownCOMPLY WITH EO E17/003/453 AFT FUSELAGE MODIFICATION TO FS621.00 PRESSURE BULKHEAD WEB. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH EO E17/003/453 AFT FUSELAGE MODIFICATION TO FS621.00 PRESSURE BULKHEAD WEB. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTESDR A6WA202301298482Angle · corrodedCORROSION ON CABIN FLOOR SUPPORT STRUCTURE AT FS349 AND RBL27 TO RBL 42. *****AIRCRAFT REMOVED FROM SERVICE********* REMOVED AND REPLACED CABIN FLOOR SUPPORT ANGLE PN 601R38783-13 AT FS349 AND RBL27 TO RBL 42. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITSDR A6WA202301298474Seat Track · corrodedCORROSION ON CABIN LH SIDE SEAT TRACK PN 20276-288-0-0 AT FS449.85 TO FS499.0. P7 - L= 0.800Ï¿½ X W= 0.400Ï¿½ X D= 0.023Ï¿½, REMAINING THICKNESS 0.077Ï¿½, CENTER OF SEAT TRACK AT FS449.85+2.0Ï¿½. *****AIRCRAFT REMOVED FROM SERVICE******* REPLACED WITH A NEWSDR A6WA202301298469Skin · chafedRH INBOARD FLAP VANE HAS WEAR MARK AT CENTER OF LEADING EDGE SKIN PN 601R14303-52. WEAR DIMENSIONS FOR P2 ARE - L = 2.300Ï¿½ X W = 0.500Ï¿½ X D = 0.012Ï¿½, WS 97.009+6.5 TO WS 106.352+1.0. *********AIRCRAFT REMOVED FROM SERVICE********** BLENDED DAMAGE OF RH ISDR A6WA202301298470Skin · chafedRH INBOARD FLAP VANE HAS WEAR MARK AT INBD END OF LEADING EDGE SKIN PN 601R14303-54. WEAR DIMENSIONS FOR P1 ARE - L = 2.100Ï¿½ X W = 0.700Ï¿½ X D = 0.018Ï¿½, WS 50.448+5.0 TO WS 54.848+1.5. *******AIRCRAFT REMOVED FROM SERVICE********** BLENDED DAMAGE OF RH INSDR A6WA202301298471None · noneRH HORIZONTAL STABILIZER SHROUD UPPER FLANGE HAS 1 ELONGATED HOLE BETWEEN FSS 110.63 AND FSS 118.63. ****AIRCRAFT REMOVED FROM SERVICE******* TEMPORARY REPAIR DISPOSITION FOR RH HORIZONTAL STABILIZER SHROUD UPPER FLANGE, 1 ELONGATED HOLE BETWEEN FSS 110.63 ANDSDR A6WA202301298468Skin · chafedRH INBOARD FLAP VANE HAS WEAR MARK AT OUTBOARD END OF LEADING EDGE SKIN PN 601R14303-44. WEAR DIMENSIONS FOR P3 ARE - L = 1.800Ï¿½ X W = 0.650Ï¿½ X D = 0.014Ï¿½, WS 135.513+3.5 TO WS 142.512+0.50. ******AIRCRAFT REMOVED FROM SERVICE******** BLENDED DAMAGE OFSDR A6WA202201108059None · noneWHILE CLIMBING OUT OF KHPN AND GOING THROUGH 10,000', THE CABIN ALT CAUTION MESSAGE INDICATED. THE FO LEVELED OFF AND RETURNED TO 10,000' WHICH I COORDINATED WITH DEPARTURE CONTROL. THE CABIN WAS INDICATING AN ALTITUDE OF 9,300 AT THAT TIME. WE RAN THE QRH FOSDR A6WA202110137899Skin · dentedMULTIPLE DENTS ON AFT FUSELAGE SKIN AT FS682.00 - FS700.00 AND RH STR22 TO STR24. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENTS ON AFT FUSELAGE SKIN AT FS682.00 - FS700.00 AND RH STR22 TO STR24 AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION P1- L = 7SDR A6WA202110137898Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS605.00 TO FS621.00 AND STR18L TO STR20L. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON AFT FUSELAGE SKIN AT FS605.00 TO FS621.00 AND STR18L TO STR20L AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 5.300Ï¿½ X W = 0SDR A6WA202110127897None · dentedRIGHT HAND OUTBOARD FLAP CENTER HINGE BOX AT WS220.00 HAS A GOUGE DAMAGE. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE ON RIGHT HAND OUTBOARD FLAP CENTER HINGE BOX AT WS220.00. ROTO PEENED REWORKED AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFASDR A6WA2019091846874Stiffener · crackedFS 409+128 BULKHEAD RBL 18 POST OUTBD SIDE HAS A CRACK INDICATION ON THE LOWER RADIUS. REPLACED.SDR A6WA2019091846873Skin · chafedRT I/B FLAP VANE SKIN OB OF CENTER VANE ACT CHAFED. REMOVED AND REPLACED RT IB FLAP VANE SKIN OUTBOARD INSTALLED NEW FLAP VANE LEADING EDGE IAW SRM 51-42-13.SDR A6WA2019091846872Beam · damagedCARGO DOOR BEAM MEMBER 601R35050-64 HAS CUT MARKS FWD AND AFT FROM CABLE ASSIST. REPLACED DAMAGED BEAM IAW SRM 51-42-06, 51-40-11.SDR A6WA2019091846871Attach Angle · crackedATTACH ANGLE CRACKED ON BOTTOM AFT CARGO DOOR BEAM, FS621.00. REPLACED ANGLE IAW SRM 51-42-06, 51-40-11-00, TR51-42, 51-42-21.SDR A6WA2019091846869Post · cracked409+128 VERTICAL POST @ LBL18 CRACKED. REPLACED VERTICAL POST @ FS409+128, LBL18 IAW REO 601R-53-41889 REV-D.SDR A6WA2019091846870Angle · crackedVERTICAL POST AT FS 409+128, BL0 CRACKED ON BOTH LEFT AND RIGHT AFT ANGLES. REPLACED LEFT AND RIGHT AFT ANGLES IAW SRM 51-42-06, REO601R-53-41-889 REV-D.SDR A6WA2019091746867Panel · crackedPANEL 446AL HAS CRACKED STIFFENER RING. REPLACED STIFFENER RING IAW CMM 20-42-06, 20-40-11.SDR A6WA2019091746868Retainer · corrodedAVIONICS BAY DOOR SEAL RETAINER CORRODED. REPLACED SEAL RETAINER IAW SRM 51-42-06.SDR A6WA2019091146865Doubler · gougedFS 621 BULKHEAD RBL 18 PREVIOUS REPAIR HAS SCREW MARKS. REMOVED AND REPLACED DOUBLER IAW REO# 601R-53-61-1285 REV E.SDR A6WA2019091146862Doubler · gougedFS 621 BULKHEAD RBL 36 PREVIOUS REPAIR HAS SCREW MARKS. REMOVE AND REPLACED DOUBLED IAW REO# 601R-53-61-1285 REV E.SDR A6WA2019091146864Doubler · gougedFS 621 BULKHEAD RBL 27 PREVIOUS REPAIR HAS SCREW MARKS. REMOVED AND REPLACED DOUBLER IAW REO# 601R-53-61-1285 REV E.SDR A6WA2019091146861Landing · crackedLT AFT TRU LAND LATCH IS CRACKED. REPAIRED TRU LAND LATCH AREA IAW SUPPLEMENT 19-016B.SDR A6WA2019091146863Doubler · gougedFS 621 BULKHEAD WL 103.5 AT LBL 18 PREVIOUS REPAIR HAS SCREW MARKS. REMOVED AND REPLACED DOUBLER IAW REO# 601R-53-61-1285 REV E.SDR A6WA2019091046860Support Channel · crackedCARGO DOOR FWD TRACK LOWER SUPPORT CHANNEL IS CRACKED. REPLACED SUPPORT CHANNEL IAW SRM 51-42-06, 51-41-02.SDR A6WA2019090946856Intercostal · crackedAFT PRESSURE BULKHEAD FS621.00 ON THE LEFT SIDE STR13L, INTERCOSTAL IS CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21.SDR A6WA2019090946855Retainer · crackedPASSENGER DOOR LOWER CENTER SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW REO 601R-52-11-915 AND SRM 51-42-13.SDR A6WA2019090946854Divider · chafedPYON PANEL 422DB HAS 2 CHAFED DIVIDER PANELS. REPLACED DIVIDERS IAW SRM 51-42-06.SDR A6WA2019090946853Retainer · crackedPYLON PANEL 422 DB HAD CRACKED SEAL RETAINER. REPLACED SEAL RETAINER IAW SRM 51-42-06.SDR A6WA2019090946852Divider · chafedPYLON PANEL 412DB HAS 2 EACH DIVIDER PANELS KNIFE EDGED. REPLACED DIVIDER PANELS IAW SRM 51-42-06, 51-42-13.SDR A6WA2019073046741Warning System · activatedAFTER SELECTING GEAR DOWN ON FINAL APPROACH, RECIEVED GEAR DIS WRNING AFTER 6 SECONDS FROM DOWN SELECTION. RT MAIN GEAR SHOWED RED BOX UP. HYD TEMPS AND PRESSURE NORMAL NO OTHER ASSOCIATED MSGS DISPLAYED CONDUCTED GO AROUND, BROUGHT FLAPS TO 8 DEGREES LEFT GESDR A6WA201845610Rvdt · failedDURING CRUISE, RECEIVED A STEERING INOPERATIVE MESSAGE, RAN QRH. LANDING WITH NOSE WHEEL STEERING IN OFF POSITION. AFTER LANDING REARMED NOSE WHEEL STEERING, MESSAGE PERSISTED. REMOVED AND REPLACED LEFT RVDT IAW AMM 32-51. OPS CHECKED GOOD.SDR A6WA201745416Proximity Sensor · malfunctionedRECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES AFTER LANDING GEAR HANDLE SELECTED UP. MLG SHOWED UP AND LOCKED AND NLG SHOWED DOWN AND GREEN. MANUALLY LOWERED GEAR, LANDING SMOOTH AND UNEVENTFUL. ADJUSTED NOSE LANDING GEAR OLEO CENTERED/EXTENDED PRSDR A6WA2017102045365Frame · crackedFRAME AT BS 333 ABOVE MAIN ENTRY DOOR IS CRACKED AT EWIS SUPPORT ATTACH POINT.SDR A6WA2017101645362Heat Shield · crackedAPU EXHAUST HEAT SHIELD PREVIOUS REPAIR WELD CRACKED. REPAIRED APU HEAT SHIELD IAW REO 601R-49-81-003 REV-B.SDR A6WA2017101145352Attach Bracket · crackedFWD ATTACH BRACKET FOR VERTICAL STAB ACCESS PANEL 326CR IS CRACKED. REPLACED THE ATTACH BRACKET IAW SRM 51-42-20.SDR A6WA2017101145344Drag Angle · crackedPAX DOOR AFT RISER DRAG ANGLE CRACKED.SDR A6WA201745340Angle · crackedREAR PRESSURE BULKHEAD, STRINGER 14R OBLIQUE ANGLE CRACKED.SDR A6WA2017101145353Fitting · crackedFLIGHT DECK WINDSHIELD CENTER POST LEFT LOWER FITTING IS CRACKED. REPLACED THE FITTING IAW SRM 51-42-21.SDR A6WA2017101145339Angle · crackedREAR PRESSURE BULKHEAD AT STRINGER 14L OBLIQUE ANGLE IS CRACKED.SDR A6WA2017101145347Floor Support · corrodedFLOOR SUPPORT CORRODED AT BS 574 TO 621, LBL 27. REPAIRED THE FLOOR SUPPORT IAW EA 15-2013-442.SDR A6WA2017101145355Angle · crackedANGLE CRACKED AT BS 280, LBL 9 OTBD. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21, AND 51-40-11.SDR A6WA2017101145348Angle · crackedRIGHT WINDSHIELD SIDE POST LOWER OTBD ANGLE IS CRACKED. REPLACED THE IAW SRM 51-42-21.SDR A6WA2017101145342Angle · crackedANGLE CRACKED AT BS 484, LBL 27. REPLACED THE ANGLE IAW REO 601R-53-41-059, REV-B.SDR A6WA2017101145341Angle · crackedANGLE CRACKED AT BS 484, LBL 36 ON INBD SIDE. REPLACED THE ANGLE IAW REO 601R-53-41-059, REV-B.
Back to N467AW