# Service difficulty reports: N8936A A list on [N8936A](https://openairdocs.org/aircraft/N8936A.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 · 108 reports - [SDR REXA2022062201300](https://openairdocs.org/sdr/REXA2022062201300.md): Connector · loose · Jun 19, 2022 · N8936A · Cndair CL6002B19 · Emergency Lighting > LIGHTED FLOOR LEVEL EXIT SIGN AT LEFT OVERWING EMERG. EXIT INOP. RESEATED ELECTRICAL CONNECTOR. OPS TEST GOOD IAW CRJ 20033-51-00. - [SDR REXA2021122301186](https://openairdocs.org/sdr/REXA2021122301186.md): Light · inoperative · Dec 18, 2021 · N8936A · Cndair CL6002B19 · Emergency Lighting > RH MIDDLE WING EMERGENCY LIGHT INOP. R&R EXTERIOR EMERGENCY LIGHT 6 IAW CRJ 200 CMM 33-52-06. OPS CHECK IS GOOD. PN ON & OFF: 8GH002473-08 - [SDR REXA2021101500881](https://openairdocs.org/sdr/REXA2021101500881.md): Battery · inoperative · Oct 14, 2021 · N8936A · Cndair CL6002B19 · Emergency Lighting > "LEFT HAND OVERWING EXIT LOWER LIGHT APPEARS TO BE INOPERATIVE. FOUND ON PREFLIGHT. "INSPECTED AND VERIFIED LIGHT INOP DEFFERED CABIN EMERGENCY LIGHTS IAW MEL 33-51-1A ENTERED IN MMO2 MOC NOTIFIED 4488***REMOVED & REPLACED ALL EMERGENCY BATTERY PACKS IAW AMM - [SDR REXA2020090200638](https://openairdocs.org/sdr/REXA2020090200638.md): Frame · corroded · Aug 25, 2020 · N8936A · Cndair CL6002B19 · Fuselage Main, Frame > FS 574 FRAME IS CORRODED ON AFT FACE BETWEEN STRINGER 27 & 26R. CONTINUED FROM JOB 8793631, OP 105 FS 574 FRAME IS CORRODED ON AFT FACE BETWEEN STRINGER 27 & 26R. CONTINUATION CARD: YES, OP: 128 REPAIRED FS 574 FRAME BETWEEN STRINGER 27 & 26R IAW RE601R-53- - [SDR REXA2020090200637](https://openairdocs.org/sdr/REXA2020090200637.md): Support · cracked · Aug 24, 2020 · N8936A · Cndair CL6002B19 · Fuselage Miscellaneous Structure > RT SYSTEM #2 HYDRAULIC FILTER MANIFOLD SUPPORT IN AEB IS CRACKED IN LOWER AFT CORNER. REMOVED & REPLACED RT SYSTEM #2 HYDRAULIC FILTER MANIFOLD SUPPORT IN AEB. REMOVED & INSTALLED RETURN & PRESSURE MANIFOLD ASSEMBLY IAW CRJ 200 AMM 29-11-44-000/400-801 & SRM - [SDR REXA2020090200636](https://openairdocs.org/sdr/REXA2020090200636.md): Floor Support · corroded · Aug 24, 2020 · N8936A · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LT CARGO FLOOR SILL CORRODED AROUND FLOOR BOARD FASTENER HOLES BETWEEN FS 574.00 AND FS 621.00. CONTINUATION CARD: YES, OP: 125 REPLACED LT CARGO FLOOR SILL BETWEEN FS 574.00 TO FS 621.00 IAW CRJ 200 SRM 51-42-06, 51-42-13, 51-42-21 AND BOMBARDIER REO# 601R-5 - [SDR REXA2020090200635](https://openairdocs.org/sdr/REXA2020090200635.md): Floor Support · cracked · Aug 24, 2020 · N8936A · Cndair CL6002B19 · Fuselage Miscellaneous Structure > UPON INSTALLATION OF AFT CARGO FLOOR SILL, FOUND ANGLE P.N. 601R35011-15 TO BE CRACKED. REMOVED & DRILL & LOCATED NEW SERVICEABLE ANGLE IAW CRJ 200 SRM 51-40-11 & INSTALLED ANGLE IAW CRJ 200 SRM 51-42-21. - [SDR REXA2020090200629](https://openairdocs.org/sdr/REXA2020090200629.md): Seat Track · corroded · Aug 23, 2020 · N8936A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > CARGO FLOOR SEAT RAIL CORRODED AT RBL 27, BETWEEN FS 559.00+80 AND FS559.00+96. REMOVED & REPLACED SEAT RAIL AT RBL 27 AT FS 559.00+80 TO FS 559.00+96 IAW CRJ 200 AMM 53-01-11-000-802/400-802. REPLACED FITTING PN CDSP1900-15 IAW AMM 25-41-01-400-806. - [SDR REXA2020090200631](https://openairdocs.org/sdr/REXA2020090200631.md): Plate · bent · Aug 22, 2020 · N8936A · Cndair CL6002B19 · Fuselage Main, Structure > FWD & AFT DOOR LANDINGS ON GROUND AIR DOOR BENT. REMOVED & REPLACED AFT DOOR LANDING IAW CRJ 200 SRM 51-40-11, 51-42-0651-25-01 & 51-23-00 & REPAIRED FWD LANDING IAW REO 601R-53-61-6078 REV, DATED 2018-04-06. - [SDR REXA2020090200630](https://openairdocs.org/sdr/REXA2020090200630.md): Floor Support · corroded · Aug 22, 2020 · N8936A · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CARGO LBL 27 FLOOR BEAM CAP HAS CORROSION AROUND NUTPLATE HOLES FROM FS 574.00 TO FS 605.00. REMOVED AND REPLACED FLOORBEAM CAP FROM FS 574 - FS 621 LBL 27 IAW CRJ200 SRM 51-42-06 AND SRM 51-42-21. - [SDR REXA2020090200634](https://openairdocs.org/sdr/REXA2020090200634.md): Seat Track · corroded · Aug 21, 2020 · N8936A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > CARGO FLOOR SEAT RAIL CORRODED AT LBL 27, BETWEEN FS 559.00+80 AND FS559.00+96. REMOVED AND REPLACED SEAT TRACK AT LBL 27 FS 559+80, FS 559+96 IAW CRJ 200 AMM 53-01-11-000/400-802. REMOVED BROKEN FITTING RETAINER IAW CRJ 200 AMM 20-21-00-910-801. - [SDR REXA2020090200633](https://openairdocs.org/sdr/REXA2020090200633.md): Seat Track · corroded · Aug 21, 2020 · N8936A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > CARGO FLOOR SEAT RAIL CORRODED AT LBL 9.0, BETWEEN FS 559.00+112 AND FS 574.00. REMOVED TAPE, REMOVED AND REPLACED CARGO FLOOR SEAT RAIL AT LBL 9.0, BETWEEN FS 559.00+112 AND FS 574 IAW CRJ 200 SRM 51-41-02. - [SDR REXA2020090200632](https://openairdocs.org/sdr/REXA2020090200632.md): Seat Track · corroded · Aug 21, 2020 · N8936A · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CARGO FLOOR SEAT RAIL CORRODED AT RBL 9.0, BETWEEN FS 559.00+112 AND FS 574.00. REMOVED TAPE, REMOVED AND REPLACED CARGO FLOOR SEAT RAIL AT RBL 9.0, BETWEEN FS 559.00+112 AND FS 574.00 IAW CRJ 200 SRM 51-41-02. - [SDR REXA2019122621781](https://openairdocs.org/sdr/REXA2019122621781.md): Light · inoperative · Dec 22, 2019 · N8936A · Cndair CL6002B19 · Emergency Lighting > RIGHT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD - [SDR REXA2018071600617](https://openairdocs.org/sdr/REXA2018071600617.md): Smoke Detector · inoperative · Jul 14, 2018 · N8936A · Cndair CL6002B19 · Smoke Detection > LAV SMOKE DETECTOR WON'T TEST. R&R LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECK GOOD. - [SDR REXA2018070300575](https://openairdocs.org/sdr/REXA2018070300575.md): Angle · cracked · Jun 16, 2018 · N8936A · Cndair CL6002B19 · Wing Miscellaneous Structure > RT WING L/E SUPPORT STRUCTURE UPPER ANGLE AT TRANSITION DUCT SUPPORT ASSY CRACKED, WS149.0. REMOVED AND REPLACED RT WING LE SUPPORT STRUCTURE UPPER ANGLE AT TRANSITION DUCT IAW SRM 51-41-02. - [SDR REXA2018070300584](https://openairdocs.org/sdr/REXA2018070300584.md): Skin · corroded · Jun 15, 2018 · N8936A · Cndair CL6002B19 · Wing, Plate/Skin > LT WING FUEL ACCESS PANEL LAND 540BB HAS FRETTING CORROSION. REPAIRED LEFT WING ACCESS PANEL LAND 540BB IAW REO 601R-57-21-030. - [SDR REXA2018070300583](https://openairdocs.org/sdr/REXA2018070300583.md): Doubler · chafed · Jun 15, 2018 · N8936A · Cndair CL6002B19 · Fuselage Main, Bulkhead > REPAIR DOUBLER ON APB RBL18.25 CHAFED FROM PANEL FASTENERS 36INCHES ABOVE FLOOR. REMOVED DAMAGED REPAIR DOUBLER FABRICATED AND INSTALLED NEW REPAIR DOUBLER ON APB, AT RBL 18.25, 36INCHES ABOVE FLOOR IAW REO 601R-53-61-1285. - [SDR REXA2018070300582](https://openairdocs.org/sdr/REXA2018070300582.md): Doubler · chafed · Jun 15, 2018 · N8936A · Cndair CL6002B19 · Fuselage Main, Bulkhead > REPAIR DOUBLER ON APB RBL35.5 CHAFED FROM PANEL FASTENERS 36 INCHES ABOVE FLOOR. REMOVED DAMAGED REPAIR DOUBLER. FABRICATED AND INSTALLED NEW REPAIR DOUBLER ON APB, REL35.5 36 INCHES ABOVE FLOOR IAW REO 601R-53-61-1285. - [SDR REXA2018070300581](https://openairdocs.org/sdr/REXA2018070300581.md): Doubler · chafed · Jun 15, 2018 · N8936A · Cndair CL6002B19 · Fuselage Main, Bulkhead > REPAIR DOUBLER ON APB RBL27.75 CHAFED FROM PANEL FASTENERS 36 INCHES ABOVE FLOOR. REMOVED DAMAGED REPAIR DOUBLER. FABRICATED AND INSTALLED NEW REPAIR DOUBLER ON APB AT RBL 27.75, 36INCHES ABOVE FLOOR IAW REO 601R-53-61-1285. - [SDR REXA2018070300580](https://openairdocs.org/sdr/REXA2018070300580.md): Access Panel · corroded · Jun 15, 2018 · N8936A · Cndair CL6002B19 · Wing, Plate/Skin > RT WING FUEL ACCESS PANEL LAND 640BB HAS FRETTING CORROSION. REPAIRED RIGHT ACCESS PANEL LAND 640BB IAW REO 601R-57-21-030. - [SDR REXA2018070300579](https://openairdocs.org/sdr/REXA2018070300579.md): Access Panel · corroded · Jun 15, 2018 · N8936A · Cndair CL6002B19 · Wing, Plate/Skin > LT WING FUEL ACCESS PANEL LAND 510AB HAS FRETTING CORROSION. REPAIRED LEFT WING ACCESS PANEL LAND 510AB IAW REO 601R-57-21-030. - [SDR REXA2018070300578](https://openairdocs.org/sdr/REXA2018070300578.md): Panel · damaged · Jun 15, 2018 · N8936A · Cndair CL6002B19 · Wing, Plate/Skin > RT LE PANEL 630BL HAS ELONGATED AND OVER COUNTERSUNK ATTACH FASTENERS HOLES. REMOVED AND REPLACED WITH NEW PANEL 630BL IAW SRM 51-40-11. - [SDR REXA2018070300577](https://openairdocs.org/sdr/REXA2018070300577.md): Rivet · chafed · Jun 15, 2018 · N8936A · Cndair CL6002B19 · Fuselage Main, Bulkhead > APB SKIN AND RIVET HEADS CHAFED FROM LINER FASTENERS 14 INCHES ABOVE FLOOR LBL36 TO RBL35.5. BLENDED CHAFES AND RESTORED FINISH. REMOVED AND REPLACED DAMAGED RIVETS IAW REO GOIR-53-61-2155. - [SDR REXA2018070300574](https://openairdocs.org/sdr/REXA2018070300574.md): Attach Angle · cracked · Jun 15, 2018 · N8936A · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER ENTRY DOOR HOIST MOTOR ATTACH ANGLE IS CRACKED AT LOWER RADIUS. REMOVED AND REPLACED PASSENGER ENTRY DOOR ATTACH ANGLE IAW SRM 51-42-21 & 51-42-06. - [SDR REXA2018070300573](https://openairdocs.org/sdr/REXA2018070300573.md): Drag Angle · cracked · Jun 15, 2018 · N8936A · Cndair CL6002B19 · Fuselage Miscellaneous Structure > RT MLG WHEEL WELL, DRAG ANGLE ADJACENT TO BATT RIB CRACKED. REMOVED AND REPLACED DRAG ANGLE IAW SRM 51-42-21. - [SDR REXA2018070300572](https://openairdocs.org/sdr/REXA2018070300572.md): Attach Bracket · cracked · Jun 15, 2018 · N8936A · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle > LT ENGINE TAIL PIPE FAIRING 436AL FIRE DETECTION LOOP MOUNT BRACKET ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED FIRE DETECTION COOP COVER ATTACH BRACKET IAW CMM 20-41-00. - [SDR REXA2018070300571](https://openairdocs.org/sdr/REXA2018070300571.md): Skin · chafed · Jun 15, 2018 · N8936A · Cndair CL6002B19 · Trailing Edge Flaps > RT INBD FLAP VANE LE SKIN CHAFED AT OTBD BUMP STOP CONTACT POINT. BLENDED CHAFE FOUND TO BE OUT OF LIMITS, REMOVED & REPLACED LE IAW REO601R-57-52-004 & SRM 51-40-11 PG 1413, 51-42-10 PG 10&15. - [SDR REXA2018070300570](https://openairdocs.org/sdr/REXA2018070300570.md): Attach Bracket · cracked · Jun 15, 2018 · N8936A · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle > LT ENGINE TAIL PIPE FAIRING 436AL FIRE DETECTION LOOP MOUNT BRACKET ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED FIRE DETECTION COOP COVER ATTACH BRACKET IAW CMM 20-41-00. - [SDR REXA2018061300569](https://openairdocs.org/sdr/REXA2018061300569.md): Plate · cracked · Jun 13, 2018 · N8936A · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure > PYLON PANEL 412BB DIVIDER PLATES ARE BOTH CRACKED. REMOVE AND REPLACE 2 EACH DIVIDER PLATES ON PANEL 412BB IAW SRM 51-42-06. - [SDR REXA2017112701199](https://openairdocs.org/sdr/REXA2017112701199.md): Light · inoperative · Nov 27, 2017 · N8936A · Cndair CL6002B19 · Emergency Lighting > RT EMERGENCY LIGHT FOUND TO BE INOP DURING ROUTINE 200 JOB CARD INSPECTION OF EMERGENCY LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHT BULB IAW AMM 33-51-21-04 P/N OFF/ON WL-1317. - [SDR REXA2017112201191](https://openairdocs.org/sdr/REXA2017112201191.md): Inverter · inoperative · Nov 22, 2017 · N8936A · Cndair CL6002B19 · Emergency Lighting > FLOOR EMERGENCY LIGHTS ARE INOPERATIVE FROM ROWS 6 THRU 8. REPLACED THE INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD. - [SDR REXA2017100101041](https://openairdocs.org/sdr/REXA2017100101041.md): Light · inoperative · Oct 1, 2017 · N8936A · Cndair CL6002B19 · Emergency Lighting > SEAT 8D EMERGENCY LIGHT OUT. R & R THE EMERGENCY LIGHT IAW AMM 33-51-19. OPS CHECKED GOOD, OK FOR SERVICE. - [SDR REXA2017090400961](https://openairdocs.org/sdr/REXA2017090400961.md): Bulb · inoperative · Sep 4, 2017 · N8936A · Cndair CL6002B19 · Emergency Lighting > FORWARD EMERGENCY LIGHTS NEAR MAIN AND SERVICE DOORS ARE INOPERATIVE. R & R THE BULBS AND OPS CHECKED IAW AMM 38-51-10. - [SDR REXA2017071800798](https://openairdocs.org/sdr/REXA2017071800798.md): Light · inoperative · Jul 18, 2017 · N8936A · Cndair CL6002B19 · Emergency Lighting > FLOOR EMERGENCY LIGHT STRIP IN THE MIDDLE SECTION INOPERATIVE. R & R THE EMERGENCY LIGHT STRIP IAW AMM 33-51-01, OPS CHECKED GOOD. - [SDR REXA2017052300634](https://openairdocs.org/sdr/REXA2017052300634.md): Light · broken · May 23, 2017 · N8936A · Cndair CL6002B19 · Emergency Lighting > ROW 1 & 2 EMERGENCY LIGHTS HAS A WHITE WIRE SHOWING AND LIGHT STRIP NOT BONDED TO THE FLOOR. FOUND ROW 1 & 2 EMERGENCY FLOOR LIGHT SPLICE BROKEN. INSTALLED A NEW SPLICE IAW ESPM 20-16-00. REINSTALLED THE EMERGENCY LIGHTS IAW AMM 33-51-01. OPS CHECKED GOOD. - [SDR REXA2017042900558](https://openairdocs.org/sdr/REXA2017042900558.md): Sign · inoperative · Apr 29, 2017 · N8936A · Cndair CL6002B19 · Emergency Lighting > RT EMERGENCY OVERWING EXIT IDENTIFICATION INOP. REMOVED AND REPLACED RT EMERGENCY EXIT IDENTIFIER P/N 6020-5 IAW AMM 33-51-10. OPS CHECK GOOD. - [SDR REXA2017010800015](https://openairdocs.org/sdr/REXA2017010800015.md): Battery Pack · discharged · Jan 8, 2017 · N8936A · Cndair CL6002B19 · Emergency Equipment > FO'S EMERGENCY FLASHLIGHT DISCHARGED. REMOVED & REPLACED THE BATTERY PACK IAW AMM 25-61-00. - [SDR REXA2016092801821](https://openairdocs.org/sdr/REXA2016092801821.md): Battery · discharged · Sep 28, 2016 · N8936A · Cndair CL6002B19 · Emergency Equipment > CAPTAINS FLASHLIGHT NOT BLINKING. REMOVED AND REPLACED CAPT'S EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-61-04. OPS CHECK GOOD. - [SDR REXA2016080401511](https://openairdocs.org/sdr/REXA2016080401511.md): Light · inoperative · Aug 4, 2016 · N8936A · Cndair CL6002B19 · Emergency Lighting > LOWER EMERGENCY LIGHT AT LT EMERGENCY EXIT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-10. OPS CHECKED GOOD IAW AMM 33-51-00-710-801. - [SDR REXA2016073001488](https://openairdocs.org/sdr/REXA2016073001488.md): Seat Track · corroded · Jul 30, 2016 · N8936A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT CABIN SEAT TRACK RBL 9 HAS CORROSION 8 INCHES AND 39 FROM FWD END. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11. - [SDR REXA2016073001487](https://openairdocs.org/sdr/REXA2016073001487.md): Seat Track · corroded · Jul 30, 2016 · N8936A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT CABIN SEAT TRACK RBL 9 HAS CORROSION AND GOUGES IN SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-41-49 AND AMM 53-01-11. - [SDR REXA2016073001486](https://openairdocs.org/sdr/REXA2016073001486.md): Seat Track · corroded · Jul 30, 2016 · N8936A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT CABIN SEAT TRACK RBL 9 HAS CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11. - [SDR REXA2016072801509](https://openairdocs.org/sdr/REXA2016072801509.md): Riser · cracked · Jul 28, 2016 · N8936A · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR STAIR RISER EDGE MEMBER BELOW UPPER FOLDING STEP CRACKED AT FWD AND AFT ENDS OF RADIUS. AFT END FOUND NOT TO BE CRACKED BY NDT TESTING IAW NDTM 51-20-06 AND REPAIRED FORWARD END IAW REO 601R-52-11-279 AAR SM-39 - [SDR REXA2016072801508](https://openairdocs.org/sdr/REXA2016072801508.md): Attach Angle · cracked · Jul 28, 2016 · N8936A · Cndair CL6002B19 · Fuselage Main, Attach Fittings > AFT PRESSURE BULKHEAD TO SKIN ATTACH ANGLE CRACKED BETWEEN BS 621 - 625 AT STRINGER 13L. REMOVED & REPLACED THE ATTACH ANGLE IAW REO 601R-53-61-5265 & SRM 51-42-21. - [SDR REXA2016072801507](https://openairdocs.org/sdr/REXA2016072801507.md): Attach Fitting · cracked · Jul 28, 2016 · N8936A · Cndair CL6002B19 · Fuselage Main, Attach Fittings > AFT PRESSURE BULKHEAD TO SKIN ATTACH CLIP CRACKED BETWEEN STA 621 AND STA 625 AT STR 15L. R & R UNSERVICEABLE ATTACH CLIP WITH A SERVICEABLE ATTACH CLIP ON AFT PRESSURE BULKHEAD TO SKIN BETWEEN STA 621 & STA 625 AT STR 15L IAW REO 601R-53-61-5265 & SRM 51-42- - [SDR REXA2016072801506](https://openairdocs.org/sdr/REXA2016072801506.md): Attach Angle · cracked · Jul 28, 2016 · N8936A · Cndair CL6002B19 · Fuselage Main, Attach Fittings > AFT PRESSURE BULKHEAD AFT FACE LT SIDE IN LINE WITH STRINGER 14L, BS 625.3 TO INTERCOSTAL ATTACH ANGLE CRACKED. REMOVED & REPLACED THE ATTACH ANGLE IAW SRM 51-42-06, & 51-42-21. - [SDR REXA2016072801505](https://openairdocs.org/sdr/REXA2016072801505.md): Attach Angle · cracked · Jul 28, 2016 · N8936A · Cndair CL6002B19 · Fuselage Main, Attach Fittings > AFT PRESSURE BULKHEAD TO SKIN ATTACH ANGLE CRACKED BETWEEN BS 621 - 625, STRINGER 15L. REMOVED & REPLACED THE ATTACH ANGLE IAW REO 601R-53-61-5265 & SRM 51-42-21. - [SDR REXA2016072701504](https://openairdocs.org/sdr/REXA2016072701504.md): Support Angle · cracked · Jul 27, 2016 · N8936A · Cndair CL6002B19 · Spoilers > RIGHT WING TE INBD GROUND SPOILER SUPPORT ANGLE BENT AND CRACKED AT FREE FLANGE. WS 75.0. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-42-06. - [SDR REXA2016072601503](https://openairdocs.org/sdr/REXA2016072601503.md): Bulkhead Web · damaged · Jul 26, 2016 · N8936A · Cndair CL6002B19 · Fuselage Main, Bulkhead > BS 621 AFT PRESSURE BULKHEAD FWD FACE DAMAGED AT RBL 17 AND WL 102. CUT OUT DAMAGE AND REPAIRED IAW REO 601R-53-61-1285. Next page: https://openairdocs.org/aircraft/N8936A/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 = 'N8936A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N8936A/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.