# Service difficulty reports: N932XJ A list on [N932XJ](https://openairdocs.org/aircraft/N932XJ.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 125 reports - [SDR REXA2024101400875](https://openairdocs.org/sdr/REXA2024101400875.md): Lamp · inoperative · Oct 11, 2024 · N932XJ · Cndair CL6002D24 · Emergency Lighting > THE EMERGENCY LIGHT IMMENDIATELY AFT OF PASSENGER DOOR IS INOP REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-51-15 OPS CHECK GOOD PN ON OFF:8GH002473-08 - [SDR REXA2022070501469](https://openairdocs.org/sdr/REXA2022070501469.md): Battery · inoperative · Jun 28, 2022 · N932XJ · Cndair CL6002D24 · Emergency Lighting > FWD LH +RH E-LIGHT INOP R+R PS35 BATTERY ASSY IAW 33-51-17-400-801 P/N ON/OFF 2013-1ASMI S/N OFF 1355 S/N ON 14558 - [SDR REXA2021122101181](https://openairdocs.org/sdr/REXA2021122101181.md): Light · missing · Dec 20, 2021 · N932XJ · Cndair CL6002D24 · Emergency Lighting > FLOOR PROXIMITY LIGHTS MISSING BOTH SIDES AT EXITS AND AFT INSTALLED PROX LTS P/N'S PL1100LH07 & PL1600LH07 IAW AMM 33-51-01 - [SDR REXA2021111601020](https://openairdocs.org/sdr/REXA2021111601020.md): Stringer · corroded · Oct 29, 2021 · N932XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > FOUND STR 27R CORRODED AT FS250-FS265. 2.0" X 1.0" X.021" DEEP. REPAIRED PER EA# CRJ953-12410 - [SDR REXA2021111601019](https://openairdocs.org/sdr/REXA2021111601019.md): Cascade · gouged · Oct 3, 2021 · N932XJ · Cndair CL6002D24 · Engine Thrust Reverser > FOUND RH ENGINE LOWER CASCADE GOUGED.022" DEEP. AFTER EVALUATION, ORGINAL PART FOUND TO BE OUT OF LIMITS. REPLACED WITH NEW PART IAW CRJ900 SRM 78-34-01 - [SDR REXA2021111601021](https://openairdocs.org/sdr/REXA2021111601021.md): Seat Track · corroded · Sep 30, 2021 · N932XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > R/H SIDE SEAT RAIL TRACK APPROX 3 FT AFT OF AFT E DOOR HAS A CLIP WITH A BROKEN SCREW IN IT AND CORROSION AROUND THE SCREW. REMOVED AND REPLACED R/H SIDE SEAT RAIL IAW CRJ900 SRM 51-41-02 - [SDR REXA2021111601018](https://openairdocs.org/sdr/REXA2021111601018.md): Panel · damaged · Sep 30, 2021 · N932XJ · Cndair CL6002D24 · Wing, Control Surfaces > R/H I/B FLAP VANE L/E PANEL 684 FT HAS A ELONGATED HOLE PANEL 684FT OUT OF LIMITS DUE TO DAMAGE NEAR FASTENER HOLE IAW CRJ900 57-52-01-001-A01. LOCATED AND DRILED NEW PANEL IAW CRJ900 SRM 51-40-11 RESTORED FINISH IAW CRJ900 SRM 51-21-11, 51-25-06 AND 51-25-16. - [SDR REXA2021111601017](https://openairdocs.org/sdr/REXA2021111601017.md): Bulkhead · damaged · Sep 27, 2021 · N932XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin > AFT FACE OF PRESSURE BULKHEAD FS 1098, 20, AT LT LOWER O/B AIR DUCT FLANGE AT 5:00 POSITION HAS A BOLT WORKING LOOSE AND CUTTING INTO THE FLANGE AND MAYBE HE BULKHEAD. REPAIRED IAW EA CRJ953-12316 REMOVED AND REPLACED LOWER O/B L/H BLEED AIR DUCT IAW CRJ900 AM - [SDR REXA2021111601016](https://openairdocs.org/sdr/REXA2021111601016.md): Panel · chafed · Sep 21, 2021 · N932XJ · Cndair CL6002D24 · Wing, Control Surfaces > L/H WING ACCESS PANEL #584ET HAS CHAFING. CHAFING ON ACCESS PANEL 584ET WAS FOUND TO BE OUT OF LIMITS IAW CRJ900 SRM 57-52-01 LOCATED AND DRILLED ACCESS PANEL 584ET IAW CRJ900 SRM 51-40-11. RESTORED PAINT FINISH IAW CRJ 900 SRM 51-21-11, 51-25-06 AND 51-25-16. - [SDR REXA2021111601014](https://openairdocs.org/sdr/REXA2021111601014.md): Channel · corroded · Sep 19, 2021 · N932XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > FS 295-FS310 BTW STGR 26L TO ATGR 26R CHANNEL TCAS LOWER CORROSION. REMOVED AND REPLACED LWR TCAS ANTENNA CHANNEL IAW CRJ900 SRM 51-42-06, REMOVED AND REPLACED LWR TCAS ANTENNA IAW CRJ900 AMM 34-43-07 - [SDR REXA2021111601015](https://openairdocs.org/sdr/REXA2021111601015.md): Diaphragm · corroded · Sep 15, 2021 · N932XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > FOUND DIAPHRAGM FOR FWD LAV SERVICE DOOR CORRODED. CORROSION IS 4.0" X 1.0" X.050" DEEP. REMOVED AND REPLACED 2 (EA) ANGLES AND 1 (EA) LOWER DIAPHRAM IAW CRJ900 SRM 51-42-06 " - [SDR REXA2020080500609](https://openairdocs.org/sdr/REXA2020080500609.md): Battery · inoperative · Aug 1, 2020 · N932XJ · Cndair CL6002B19 · Emergency Lighting > EXIT LIGHT OUT AT ROW 5 FOUND DURING FA PREFLIGHT. R & R THE BATTERY ASSY PS36 IAW AMM 33-51-17. ALL CHECKED GOOD. - [SDR REXA2020072400605](https://openairdocs.org/sdr/REXA2020072400605.md): Light · inoperative · Jul 21, 2020 · N932XJ · Cndair CL6002D24 · Emergency Lighting > EXTERIOR EMERGENCY LIGHT RH FWD IS INOPERATIVE. REMOVED AND REPLACED LIGHT BULB IAW AMM 33-51-15 - [SDR REXA2020072000603](https://openairdocs.org/sdr/REXA2020072000603.md): Battery · inoperative · Jul 16, 2020 · N932XJ · Cndair CL6002D24 · Emergency Lighting > FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-15, OPS FAILED. R & R THE PS35 BATTERY ASSY AND BATTERY CHARGER ASSY IAW AMM 33-51-17, OPS TESTED GOOD. - [SDR REXA2018110501039](https://openairdocs.org/sdr/REXA2018110501039.md): Sign · missing · Nov 1, 2018 · N932XJ · Cndair CL6002D24 · Emergency Lighting > ROW 13 REARWARDS FACING 'EMERGENCY EXIT' SIGN MISSING. ROW 13 REARWARDS FACING EMERGENCY EXIT SIGN INSTALLED IAW CRJ900 AMM 3 3-51-07. NO FURTHER ACTION REQUIRED. - [SDR REXA2018060138484](https://openairdocs.org/sdr/REXA2018060138484.md): Oven · odor · Jun 8, 2018 · N932XJ · Cndair CL6002D24 · Buffet/Galleys > OVEN EMITTED A BURNING ODOR. R & R THE GALLEY OVEN IAW AMM 25-32-01, OPS CHECKED GOOD. - [SDR REXA201806010432](https://openairdocs.org/sdr/REXA201806010432.md): Flashlight · inoperative · May 31, 2018 · N932XJ · Cndair CL6002D24 · Emergency Equipment > EMERGENCY FLASHLIGHT IN THE GALLEY WAS NOT CHARGING. REPLACED THE FLASHLIGHT IAW AMM 25-61-02, OPS CHECKED GOOD. - [SDR REXA2018052100401](https://openairdocs.org/sdr/REXA2018052100401.md): Seal · broken · May 21, 2018 · N932XJ · Cndair CL6002D24 · Emergency Equipment > FWD F/A FLASHLIGHT NEXT TO JUMPSEAT HAS A BROKEN SEAL & DOES NOT WORK. REPLACED THE FWD FLASHLIGHT SEAL IAW AMM 25-60-00. - [SDR REXA2018040200241](https://openairdocs.org/sdr/REXA2018040200241.md): Light · inoperative · Apr 2, 2018 · N932XJ · Cndair CL6002D24 · Emergency Lighting > FWD OVERWING EMERGENCY LIGHT OUT DEFERRED LT OVERWING EMERGENCY LIGHT (FWD) IAW MEL 33-51-2C. RELAMPED LT FWD OVERWING EMER LIGHT IAW AMM 33-51-15, OPS CHECK GOOD. - [SDR REXA2018012300044](https://openairdocs.org/sdr/REXA2018012300044.md): Smoke Warning · false activation · Jan 23, 2018 · N932XJ · Cndair CL6002D24 · Smoke Detection > FORWARD LAVATORY SMOKE MASTER WARNING ILLUMINATED IN FLIGHT FOR FIVE SECONDS, AND THEN DISSAPEARED. NO SMOKE WAS DETECTED. REMOVED & REPLACED FWD LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECKED GOOD. ACFT OK FOR SERVICE. - [SDR REXA2017122301287](https://openairdocs.org/sdr/REXA2017122301287.md): Heater · odor · Dec 23, 2017 · N932XJ · Cndair CL6002D24 · Heating System > VERY STRONG ODOR OF BURNING ELECTRICAL WIRES NOTED AT THE FORWARD FLIGHT ATTENDANT STATION NEAR PHONE & PA. ODOR ALSO NOTED IN COCKPIT. COMPLIED WITH FIM 21-22-00, FOUND ODOR TO BE FROM DUCT BEHIND PANEL 231AL. ODOR GOES AWAY WITH PACKS AND RECIRCULATION FA - [SDR REXA2017102201127](https://openairdocs.org/sdr/REXA2017102201127.md): Feeder Cable · broken · Oct 22, 2017 · N932XJ · Cndair CL6002D24 · Light System Wiring > OVERWING FWD EMERGENCY LIGHT HAS A BROKEN POWER LEAD. REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51-15-400-801. SYSTEM OPS CHECKED GOOD IAW AMM 33-51-00-710-802. - [SDR REXA2017102201121](https://openairdocs.org/sdr/REXA2017102201121.md): Housing · cracked · Oct 22, 2017 · N932XJ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors > MAIN AVIONICS COMPARTMENT DOOR HANDLE HOUSING IS CRACKED AT THE BASE OF THE HANDLE. REMOVED AND REPLACED MAIN AVIONICS COMPARTMENT DOOR HANDLE HOUSING IAW SRM 51-42-21. PERFORMED OPS TEST IAW AMM 52-42-00-710-801 STEP 4 A, OPS CHECKED GOOD. - [SDR REXA2017101101118](https://openairdocs.org/sdr/REXA2017101101118.md): Longeron · cracked · Oct 11, 2017 · N932XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > LONGERON 3L, BS 280 IS CRACKED. REPAIRED THE LONGERON IAW REO 670-53-21-493, AND EOR53568 REV ONE. - [SDR REXA2017101001119](https://openairdocs.org/sdr/REXA2017101001119.md): Web · cracked · Oct 10, 2017 · N932XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR AFT WEB IS CRACKED AT BOTTOM STEP RISER. REPAIRED PAX DOOR WEB IAW SRM 52-11-04. - [SDR REXA2017100701124](https://openairdocs.org/sdr/REXA2017100701124.md): Seat Track · corroded · Oct 7, 2017 · N932XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > MAIN CABIN SEAT TRACK IS CORRODED AND GOUGED, RBL 15, BS 693 - 977. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, SRM 51-40-11, SRM 51-21-11, AND REO 670-53-00-343, REV M. - [SDR REXA2017100701123](https://openairdocs.org/sdr/REXA2017100701123.md): Seat Track · corroded · Oct 7, 2017 · N932XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > MAIN CABIN SEAT TRACK IS CORRODED AND GOUGED, LBL 15, BS 693 - 977. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, AND REO 670-53-00-343, REV M. - [SDR REXA2017100601122](https://openairdocs.org/sdr/REXA2017100601122.md): Seat Track · damaged · Oct 6, 2017 · N932XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > RIGHT SIDE SEAT TRACK 9 HAS A MISSING FASTENER. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, AND REO 670-53-00-343. - [SDR REXA2017100501125](https://openairdocs.org/sdr/REXA2017100501125.md): Stringer · corroded · Oct 5, 2017 · N932XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > AFTER REMOVING WET INSULATION FOUND A STRINGER 27 CORRODED AT BS 310. REMOVED AND REPLACED THE STRINGER BETWEEN BS 305 TO 339 IAW SRM 51-42-06, AND 51-42-21. - [SDR REXA2017100401126](https://openairdocs.org/sdr/REXA2017100401126.md): Seat Track · gouged · Oct 4, 2017 · N932XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > RIGHT SEAT TRACK 3 GOUGED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, AND REO 670-53-00-343, REV M. - [SDR REXA2017071500791](https://openairdocs.org/sdr/REXA2017071500791.md): Battery · discharged · Jul 15, 2017 · N932XJ · Cndair CL6002D24 · Emergency Lighting > DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTS WERE NOT COMING ON AND THE EMERGENCY SWITCH ON THE FA'S PANEL WAS FOUND IN THE ON POSITION. SUSPECT THE BATTERIES ARE DEAD. PERFORMED AN OPS TEST OF THE EMERGENCY POWER UNIT IAW AMM 33-51-7. OPS CHECK PASSED. - [SDR REXA2017051500604](https://openairdocs.org/sdr/REXA2017051500604.md): Bulb · burned out · May 15, 2017 · N932XJ · Cndair CL6002D24 · Emergency Lighting > FWD ENTRANCE EMERGENCY LIGHT BULBS BURNED OUT. REPLACED THE BULBS IAW AMM 33-51-05, OPS CHECKED GOOD. - [SDR REXA2016112502305](https://openairdocs.org/sdr/REXA2016112502305.md): Glowstrip · missing · Nov 25, 2016 · N932XJ · Cndair CL6002D24 · Emergency Equipment > ON CENTER CARPET R+R NOTED. RT AFT EMERGENCY EXIT FWD GLOW STRIP MISSING. REPLACED FWD GLOW STRIP AS REQUIRED IAW AMM 33-52-01. - [SDR REXA2016112002334](https://openairdocs.org/sdr/REXA2016112002334.md): Flashlight · inoperative · Nov 20, 2016 · N932XJ · Cndair CL6002D24 · Emergency Equipment > FWD FA FLASHLIGHT DOES NOT SHOW THAT IT IS CHARGING. REMOVED & REPLACED FLASHLIGHT IAW AMM 25-61-02. - [SDR REXA2016101601932](https://openairdocs.org/sdr/REXA2016101601932.md): Light · missing · Oct 16, 2016 · N932XJ · Cndair CL6002D24 · Emergency Lighting > EMERGENCY LIGHT MISSING AT ROW 13CD FORWARD. REPLACED THE LIGHT STRIP IAW AMM 31-51-11. ACFT OK FOR SERVICE. - [SDR REXA2016091901756](https://openairdocs.org/sdr/REXA2016091901756.md): Strap · broken · Sep 19, 2016 · N932XJ · Cndair CL6002D24 · Emergency Equipment > FWD FA REPORTS SEAL ON FWD FLASHLIGHT IS BROKEN. R & R THE FLASHLIGHT STRAP IAW AMM 25-61-02. ACFT GOOD FOR SERVICE AT THIS TIME. - [SDR REXA2016082701615](https://openairdocs.org/sdr/REXA2016082701615.md): Battery · discharged · Aug 27, 2016 · N932XJ · Cndair CL6002D24 · Emergency Equipment > CUSTOMER WALK AROUND; FLIGHT DECK FLASHLIGHTS, 2, RED LIGHT IS NOT ON. REMOVED AND REINSTALLED NEW SERVICEABLE BATTERIES ON LT & RT COCKPIT, FLIGHT DECK FLASHLIGHTS IAW AMM 25-61-02-000-801-A10 & 25-61-02-400-801 A10 AND CMM 25-60-11. - [SDR REXA2016082701611](https://openairdocs.org/sdr/REXA2016082701611.md): Light · inoperative · Aug 27, 2016 · N932XJ · Cndair CL6002D24 · Emergency Lighting > 2 FORWARD OVERWING EMERGENCY LIGHTS ON LT WING AND 2 AFT OVERWING EMERGENCY LIGHTS ON THE WING INOPERATIVE. CONTINUATION CARD 81519411, OP 255. REMOVED PANEL 251NLW AND REINSTALLED PANEL AFTER CONNECTING P377 CONNECTOR IAW ESPM 20-26-00 AND AMM 25-26-01-400- - [SDR REXA2016082601654](https://openairdocs.org/sdr/REXA2016082601654.md): Retainer · damaged · Aug 26, 2016 · N932XJ · Cndair CL6002D24 · Passenger/Crew Doors > DURING ENTRY OF CABIN IT WAS NOTICED THAT THE PAX DOOR SEAL RETAINER WAS DAMAGED BY PROXIMITY SENSOR CONDUIT CLAMP GETTING CAUGHT IN WAY DURING DOOR CLOSE. REMOVED AND REPLACED THE SEAL RETAINER IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND REO:670-5 - [SDR REXA2016082601653](https://openairdocs.org/sdr/REXA2016082601653.md): Panel · damaged · Aug 26, 2016 · N932XJ · Cndair CL6002D24 · Passenger/Crew Doors > ON INSTALLATION, FOUND HINGE ON UPPER STAIR PANEL ASSEMBLY BROKEN. LOCATED AND DRILLED HINGE ON UPPER STAIR PANEL ASSEMBLY IAW SRM 51-40-11-001-001-A01. ATTACHED HINGE ASSEMBLY TO THE UPPER STAIR PANEL IAW AMM 51-11-04-400-801-A01 STEPS A.2. - [SDR REXA2016082601636](https://openairdocs.org/sdr/REXA2016082601636.md): Bearing · cracked · Aug 26, 2016 · N932XJ · Cndair CL6002D24 · Wing Main, Frame Structure > RIGHT WING AFT LINK AT WS 797, LOWER BEARING HAS A CRACK AND LINK IS MAKING CONTACT WITH ATTACHMENT FITTING. COMPLIED WITH EO R57200, R57189 AND R57190 FOR INSPECTION AND REPLACEMENT. - [SDR REXA2016082501625](https://openairdocs.org/sdr/REXA2016082501625.md): Intercostal · corroded · Aug 25, 2016 · N932XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > LEFT AND RT JACK FITTING SUPPORT INTERCOSTALS BETWEEN FS 280 TO FS 265 ARE CORRODED. CONTINUATION CARD 81519411 OP 233. REPLACED LT/RT JACK FITTING SUPPORT INTERCOSTALS BETWEEN FS 280 AND FS 265 IAW EA CRJ953-04677. - [SDR REXA2016082301645](https://openairdocs.org/sdr/REXA2016082301645.md): Door Sill · corroded · Aug 23, 2016 · N932XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > AFT CARGO DOOR SILL IS CORRODED FROM BS 1000 TO 1047. REPLACED THE AFT CARGO DOOR SILL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-41-02-001-001-A01, & 51-42-13-001-001-A01. - [SDR REXA2016082301626](https://openairdocs.org/sdr/REXA2016082301626.md): Frame · corroded · Aug 23, 2016 · N932XJ · Cndair CL6002D24 · Fuselage Main, Frame > FRAME IS CORRODED AT FS 265 BETWEEN STR 26R TO 26L. UPON INVESTIGATION, FOUND NO CORROSION TO FS 265 FRAME, CORROSION LIMITED TO STIFFENING ANGLE. R & R STIFFENING ANGLE IAW SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01. - [SDR REXA2016082301620](https://openairdocs.org/sdr/REXA2016082301620.md): Frame · corroded · Aug 23, 2016 · N932XJ · Cndair CL6002D24 · Fuselage Main, Frame > FRAME IS CORRODED AT FS 310 BETWEEN STR 26L TO STR 25R. CONTINUATION CARD 81519411, OP 228. REPAIRED FS 310 FRAME BETWEEN STR 26L TO STR 25R IAW REO 670-53-21-799. - [SDR REXA2016082201635](https://openairdocs.org/sdr/REXA2016082201635.md): Intercostal · corroded · Aug 22, 2016 · N932XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > INTERCOSTAL AT STRINGER 20R, BS 349 CORRODED. REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01. - [SDR REXA2016082201627](https://openairdocs.org/sdr/REXA2016082201627.md): Door Sill · corroded · Aug 22, 2016 · N932XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > SERVICE DOOR LOWER SILL ANGLE CORRODED BETWEEN FS 310 AND FS 349. CONTINUATION CARD 81519411, OPS 190 & 195. REPAIRED SERVICE DOOR LOWER SILL ANGLE BETWEEN FS 310 AND FS 349 BY REMOVING AND REINSTALLING SCUFF PLATE IAW AMM 53-21-23-000-801-A01 AND AMM 53-21- - [SDR REXA2016082201619](https://openairdocs.org/sdr/REXA2016082201619.md): Frame · corroded · Aug 22, 2016 · N932XJ · Cndair CL6002D24 · Fuselage Main, Frame > FRAME IS CORRODED AT FS 319 BETWEEN STR 27 TO 26L. REPAIRED FRAME FS 319 BETWEEN STR 27 TO 26L IAW SRM 51-42-06-001-001-A01 AND REO 670-53-21-799. - [SDR REXA2016082201618](https://openairdocs.org/sdr/REXA2016082201618.md): Frame · corroded · Aug 22, 2016 · N932XJ · Cndair CL6002D24 · Fuselage Main, Frame > FRAME IS CORRODED AT FS 349 BETWEEN STR 26R TO 26L. CONTINUATION CARD 81519411, OP 191. REMOVED CORRODED FRAME AT FS 349 STR 26R TO 26L IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-42-21-001-001-A01. - [SDR REXA2016082101649](https://openairdocs.org/sdr/REXA2016082101649.md): Web · cracked · Aug 21, 2016 · N932XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK ON FLOOR WEB CORNER FWD OF BS 202 BULKHEAD AT BOTTOM OF LT CAP ANGLE. REPAIRED THE WEB IAW REO 670-53-11-509 REV D. Next page: https://openairdocs.org/aircraft/N932XJ/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N932XJ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N932XJ/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.