# Service difficulty reports: N8836A

A list on [N8836A](https://openairdocs.org/aircraft/N8836A.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 · 111 reports

- [SDR REXA2021121601129](https://openairdocs.org/sdr/REXA2021121601129.md): Bulb · inoperative · Dec 12, 2021 · N8836A · Cndair CL6002B19 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS ON FFOD TEST NOT STAYING LIT.OVERHEAD WING EXIT LIGHT(FWD),OVERHEAD PASSENGER DOOR LIGHT AND LEFT EXTERIOR WING LIGHT OBSERVED TO BRIFELY ILLUMINATE AND THE EXTINGUISH WHEN COMMANDED ON.
- [SDR REXA2020030400320](https://openairdocs.org/sdr/REXA2020030400320.md): Skin · dented · Feb 26, 2020 · N8836A · Cndair CL6002B19 · Spoilers
  > L/WING O/B GRD SPOILER BOTTOM SKIN DENTED APPX.5 X.5 X.020. REPAIRED LH WING O/B GROUND SPOILER DENT ON BOTTOM SKIN IAW EA CRJ257-1045. WVAC STAMP
- [SDR REXA2020030400318](https://openairdocs.org/sdr/REXA2020030400318.md): Bulkhead · damaged · Feb 26, 2020 · N8836A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LH, RH AND CENTER 9G BULKHEAD HAVE TOOLING MARKS AT CARGO PANEL ATTACHEMNT PANELS. REPAIRED 9G BULKHEADS IAW EO'S CL-600-2B19-53-L06370, CL-600-2B19-53-L06371 AND EO CL-600-2B19-53-L06372. WVAC STAMP
- [SDR REXA2020030400317](https://openairdocs.org/sdr/REXA2020030400317.md): Bulkhead · damaged · Feb 26, 2020 · N8836A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LH, RH AND CENTER 9G BULKHEAD HAVE TOOLING MARKS AT CARGO PANEL ATTACHEMNT PANELS. REPAIRED 9G BULKHEADS IAW EO'S CL-600-2B19-53-L06370, CL-600-2B19-53-L06371 AND EO CL-600-2B19-53-L06372. WVAC STAMP
- [SDR REXA2020030400316](https://openairdocs.org/sdr/REXA2020030400316.md): Bulkhead · cracked · Feb 22, 2020 · N8836A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS 4 INDICATIONS NOTED: 1) BL 0.0 WL 134-127 4 INCHES LONG 50% FSH, 2) RBL 36.20 WL91-90 1 INCH LONG 100% FSH, 3) RBL 27.50 WL85-84 1 INCH LONG 100% FSH AND 4) BL 0.0 WL114-1104 INCHES LONG 80% FSH FAILED NDT INSPECTION.
- [SDR REXA2020030400321](https://openairdocs.org/sdr/REXA2020030400321.md): Bulkhead · dented · Feb 21, 2020 · N8836A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS DENT ON FWD SIDE BETWEEN LBL 9.50 AND LBL 18.00 WL 79.400 BY.400.010 DEEP. REPAIRED DENT ON REAR PRESSURE BULKHEAD FWD SIDE IAW REO 601R-53-61-7312 REV--. WEIGHT ADDED.7 LBS. WVAC STAMP
- [SDR REXA2020030400319](https://openairdocs.org/sdr/REXA2020030400319.md): Panel · corroded · Feb 19, 2020 · N8836A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LIGHTNING DIVERTER PANEL CLIP LBL 27 JUST FWD OF F.S. 333.00 IS CORRODED LOCATED, DRILLED & INSTALLED NEW SERVICEABLE LIGHTNING DIVERTER PANEL CLIP PN# 601R52219-117 AT LBL 27 F.S. 333.00 IAW CRJ 200 SRM 51-42-13.
- [SDR REXA2019060300770](https://openairdocs.org/sdr/REXA2019060300770.md): Light · inoperative · May 30, 2019 · N8836A · Cndair CL6002B19 · Emergency Lighting
  > DURING INSPECTION FOUND R/H MID AND AFT EMERGENCY LIGHTS OUT. R/R R/H EMERGENCY LIGHTS IAW AMM 35-51-21. OPS CHECKS GOOD. P/N ON/OFF 1317 NSN ON OR OFF.
- [SDR REXA2019050600616](https://openairdocs.org/sdr/REXA2019050600616.md): Bulkhead Web · damaged · May 6, 2019 · N8836A · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > FS 621 PRESSURE BULKHEAD WEB FWD FACE HAS 7 TOOLING MARKS APPROX.1" ROUND X.001" DEEP AT WL 103, LBL 9,18,27 AND RBL 9,18,27,36. REPAIRED BULKHEAD IAW BOMBARDIER GREO 601R-53-61-2155 REV A DATED 2013-06-13.
- [SDR REXA2019050600620](https://openairdocs.org/sdr/REXA2019050600620.md): Skin · damaged · May 6, 2019 · N8836A · Cndair CL6002B19 · Wing, Plate/Skin
  > DURING REINSPECT OF THE LH WING PLANK ACCESS HOLE 550CB NOTED INDICATIONS AROUND THE CIRCUMFERENCE OF THE ACCESS HOLE LANDING 75% FULL SCREEN HEIGHT. FAILING NDT AREAS MARKED ON A/C. REPAIRED FUEL PANEL WING PLANK ACCESS HOLE 550CB IAW REO 601RX57-21-3020 DATE
- [SDR REXA2019042500621](https://openairdocs.org/sdr/REXA2019042500621.md): Plate · corroded · Apr 25, 2019 · N8836A · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > RT PYLOIN TOP INBD TRAILING EDGE BOND PLATE CORRODED. REMOVED AND REPLACED RT PYLON TOP IB BOND PLATE IAW SRM 51-42-12, BOND TEST GOOD.
- [SDR REXA2019042500619](https://openairdocs.org/sdr/REXA2019042500619.md): Angle · corroded · Apr 25, 2019 · N8836A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL LOWER ANGLE CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE SILL LOWER ANGLE IAW SRM 51-42-13, 51-42-06, AND 51-42-21.
- [SDR REXA2019042400617](https://openairdocs.org/sdr/REXA2019042400617.md): Angle · corroded · Apr 24, 2019 · N8836A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR CUTOUT BOTTOM SILL ANGLE CORRODED BETWEEN FS319 AND FS349. REMOVED & REPLACED SVC DOOR BOTTOM SIL ANGLE IAW 51-42-21, 51-40-11, 51-42-13 & 51-25-00.
- [SDR REXA2019042300618](https://openairdocs.org/sdr/REXA2019042300618.md): Angle · cracked · Apr 23, 2019 · N8836A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT EQUIPMENT COMPARTMENT FS 621.00 TO 625.00 OBLIQUE ANGLE AT STR 14L IN CRACKED. REMOVED AND REPLACED OBLIUQUE ANGLE AT STR14L IAW SRM 51-42-21 P/N 601-35012-51.
- [SDR REXA2018052980415](https://openairdocs.org/sdr/REXA2018052980415.md): Bulkhead · chafed · May 28, 2018 · N8836A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD HAS MULTIPLE SUPERFICIAL HARDWARE HITS & A LIGHT SUPERFICIAL SCRATCH, HITS LOCATED AT RBL 36.20, 27.50, 18.00 ON RIVET CL ONE 1.75" I/B OF RBL 9.50 CL OUTSIDE OF TOE ZONE ANOTHER 1.75" I/B OF LBL 9.50 CL OUTSIDE OF TOE ZONE SUPERFICIAL S
- [SDR REXA2018052980414](https://openairdocs.org/sdr/REXA2018052980414.md): Post · cracked · May 28, 2018 · N8836A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL POST AT RBL 27, BS 409 +128 HAD A CRACK ORIGINATING AT BOTTOM OF THE INBD FLANGE & EXTENDING UP TO & PAST 1ST RIVET, ENDING APPROX BETWEEN 1ST & 2ND RIVETS. REPAIRED IAW REO 601R-53-41-056. MAJOR REPAIR.
- [SDR REXA2018030200172](https://openairdocs.org/sdr/REXA2018030200172.md): Lamp · inoperative · Mar 2, 2018 · N8836A · Cndair CL6002B19 · Emergency Lighting
  > RIGHT FWD CENTER EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW CMM 33-52-07. OPS CHECKED GOOD.
- [SDR REXA2018012100036](https://openairdocs.org/sdr/REXA2018012100036.md): Oxygen Mask · defective · Jan 21, 2018 · N8836A · Cndair CL6002B19 · Crew Oxygen System
  > CAPTAIN`S OXYGEN MASK HARNESS WILL NOT INFLATE. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12, OPS CHECKED GOOD.
- [SDR REXA2017100201042](https://openairdocs.org/sdr/REXA2017100201042.md): Light · inoperative · Oct 2, 2017 · N8836A · Cndair CL6002B19 · Emergency Lighting
  > LEFT FWD AND AFT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FWD AND AFT EMERGENC LIGHTS IAW 33-50
- [SDR REXA2017081300880](https://openairdocs.org/sdr/REXA2017081300880.md): Battery Pack · inoperative · Aug 13, 2017 · N8836A · Cndair CL6002B19 · Emergency Equipment
  > CAPTAIN'S EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-61-00.
- [SDR REXA2017080600858](https://openairdocs.org/sdr/REXA2017080600858.md): Light · inoperative · Aug 6, 2017 · N8836A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT SECTION JUST AFT OF EXIT ROW NOT ILLUMINATING. REMOVED AND REPLACED THE EMERGENCY LIGHT SECTION IAW AMM 33-51-01.
- [SDR REXA2017072800838](https://openairdocs.org/sdr/REXA2017072800838.md): Connector · disconnected · Jul 28, 2017 · N8836A · Cndair CL6002B19 · Light System Wiring
  > FLOOR LIGHTING IS OUT ROW 8-10. PERFORMED VISUAL INSPECTION OF EMERGENCY LIGHT STRIP AT 9-10 C/D, FOUND STRIP CONNECTOR DISCONNECTED. ATTACHED, OPS CHECKED IAW AMM 33-51-00. OK FOR SERVICE.
- [SDR REXA2017071800799](https://openairdocs.org/sdr/REXA2017071800799.md): Light · malfunctioned · Jul 18, 2017 · N8836A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS CAME ON BRIEFLY, THEN TURNED OFF. PERFORMED OPS TEST OF THE EMERGENCY LIGHTS OPS TESTED GOOD.
- [SDR REXA2017071200782](https://openairdocs.org/sdr/REXA2017071200782.md): Wire Splice · damaged · Jul 12, 2017 · N8836A · Cndair CL6002B19 · Light System Wiring
  > FLOOR EMERGENCY LIGHTS NOT ILLUMINATED AT ROWS 9CD TO 12CD. REMOVED AND REPLACED THE CABLE SPLICE CONNECTOR IAW ESPM 20-17-10.
- [SDR REXA2017032000389](https://openairdocs.org/sdr/REXA2017032000389.md): Flashlight · inoperative · Mar 20, 2017 · N8836A · Cndair CL6002B19 · Emergency Equipment
  > FO'S EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FO'S EMERG FLASHLIGHT PN ON/OFF P2-07-0001-214 IAW AMM 25-61-04. OPS CHECK GOOD.
- [SDR REXA2017030700324](https://openairdocs.org/sdr/REXA2017030700324.md): G Switch · inoperative · Mar 7, 2017 · N8836A · Cndair CL6002B19 · Emergency Locator Beacon
  > ELT G SWITCH INOPERATIVE. R & R THE ELT IAW AMM TASK 25-62-01-000-801. OPS CHECKED NORMAL.
- [SDR REXA2017021200199](https://openairdocs.org/sdr/REXA2017021200199.md): Light · inoperative · Feb 12, 2017 · N8836A · Cndair CL6002B19 · Emergency Lighting
  > DURING A ROUTINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. R & R THE LIGHT IAW AMM 33-51-01, OPS CHECKED OK.
- [SDR REXA2016051400786](https://openairdocs.org/sdr/REXA2016051400786.md): Light · inoperative · May 14, 2016 · N8836A · Cndair CL6002B19 · Passenger Compartment Lighting
  > EMERGENCY CALL LIGHT ON MID CABIN EMER EXIT LIGHT OUT, BACKSIDE ONLY. R & R CALL LIGHT MID CABIN EMER EXIT LIGHT IAW AMM 33-50-00. OPERATIONS CHECKED GOOD.
- [SDR REXA2016041100580](https://openairdocs.org/sdr/REXA2016041100580.md): Frame · corroded · Apr 11, 2016 · N8836A · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME SECTOR FS 333 IS CORRODED AT STRINGER 27. CONTINUATION CARD 8783611 OPERATIONS 302 & 311. REPLACED FRAME AT FS 333 IAW SRM 51-40-11, 51-42-06 7 51-42-21.
- [SDR REXA2016040900572](https://openairdocs.org/sdr/REXA2016040900572.md): Door Sill · corroded · Apr 9, 2016 · N8836A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL HAS SURFACE CORROSION AROUND SEVERAL FASTENER HOLES, AT APPROX FS 559+106 & ONE EACH NUTPLATE IS MISSING AT FS 559+92. CONTINUATION CARD 8783611 OPERATIONS 356. REPAIRED RT FLOOR SILL IAW REO 601R-53-00-526 REV DATED 05 22 13 & EA CRJ253-04
- [SDR REXA2016040900567](https://openairdocs.org/sdr/REXA2016040900567.md): Frame · corroded · Apr 9, 2016 · N8836A · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME SECTOR CORRODED AT FS 574, BETWEEN STRINGER 2GR & 2GL. CONTINUATION CARD 8783611 OPERATIONS 327 & 345. REMOVED FRAME SECTOR & REINSTALLED NEW SERVICEABLE FRAME SECTOR IAW SRM 51-42-06, 51-42-21, 51-42-22 & EA CRJ 253-04189 & REINFORCEMENT ANGLE, REPAIR
- [SDR REXA2016040800600](https://openairdocs.org/sdr/REXA2016040800600.md): Bulkhead · damaged · Apr 8, 2016 · N8836A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESS BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED AT INBD LOWER CORNER, APPROX.200" IN LENGTH 90% FSH. FAILED NDT INSPECTION. CONTINUATION CARD 8783615 OP 76. REPAIRED REAR PRESS BULKHEAD AT THE LINTEL ATTACHME
- [SDR REXA2016040800597](https://openairdocs.org/sdr/REXA2016040800597.md): Inverter · inoperative · Apr 8, 2016 · N8836A · Cndair CL6002B19 · Emergency Lighting
  > 48 MONTH. NR 4 EMER LIGHT BATTERY PACK INVERTER INOPERATIVE. R & R NR 4 EMER LIGHT BATTERY PACK INVERTER IAW AMM 33-51-07-400-801. OPERATIONS TESTED GOOD.
- [SDR REXA2016040800594](https://openairdocs.org/sdr/REXA2016040800594.md): Drag Angle · cracked · Apr 8, 2016 · N8836A · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT DRAG ANGLE CRACKED ABOVE PULLEY SUPPORT BRACKET. CONTINUATION CARD 8783611 OP 310. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO:601R-52-11-513 REV B DATED 2015 07 05, TYPE I REPAIR. OPERATIONS CHECKED GOOD.
- [SDR REXA2016040700579](https://openairdocs.org/sdr/REXA2016040700579.md): Vane · chafed · Apr 7, 2016 · N8836A · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING INBD FLAP VANE LE CHAFED IN 3 PLACES. INBD 1.0 X 1.0 X.006 DEEP, MID 1.0 X.750 X.005 DEEP, OTBD 1.0 X.300 X.002 DEEP. CONTINUATION CARD 8783611 OPERATIONS 324. REPAIRED LT INBD FLAP VANE LE CHAFES IAW REO 601R-57-52-004 REV D DATED 2012 12 19
- [SDR REXA2016040700569](https://openairdocs.org/sdr/REXA2016040700569.md): Frame · corroded · Apr 7, 2016 · N8836A · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME CORRODED AT FS 605 & STRINGER 27. CONTINUATION CARD 8783611 OPERATIONS 297, 298, 301, 303, & 338. REMOVED FRAME & INSTALLED NEW FRAMES IAW SRM 53-00-00, 51-40-11, 51-42-06, 51-42-20 & 51-42-21. OPERATIONS CHECKED GOOD.
- [SDR REXA2016040700564](https://openairdocs.org/sdr/REXA2016040700564.md): Bracket · cracked · Apr 7, 2016 · N8836A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AIRCRAFT GND POWER RECEPTACLE STRUCTURE CRACKED. CONTINUATION CARD 8783611 OPERATION 322 & 346. R & R POWER RECEPTACLE BRACKET IAW SRMS 51-42-06, 51-42-21, 51-40-11 & EA CRJ253-04187.
- [SDR REXA2016040600601](https://openairdocs.org/sdr/REXA2016040600601.md): Bulkhead · damaged · Apr 6, 2016 · N8836A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND FS 202.75 PRESS BULKHEAD WEB AT BL 23.71 HAS INDICATION NOTED, APPROX.500 IN LENGTH 50% FSH, FAILED NDT. CONTINUATION CARD 8783615 OP 66 & 82. REPAIRED FS 202.75 PRESS BULKHEAD IAW REO 601R-53-11-563 REV C. THIS IS A MAJOR REPAIR.
- [SDR REXA2016040500570](https://openairdocs.org/sdr/REXA2016040500570.md): Door Sill · corroded · Apr 5, 2016 · N8836A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR FLOOR SILL IS CORRODED AROUND MULTIPLE FASTENER HOLES. R & R CORRODED FLOOR SILL IAW REO 601R-53-61-1574 & SRM 51-40-11.
- [SDR REXA2016040400581](https://openairdocs.org/sdr/REXA2016040400581.md): Fitting · cracked · Apr 4, 2016 · N8836A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OUTBOARD CLIP 1 EACH IS CRACKED ATTACHING TO FLOORBEAM AT FS 280 AT RBL 9 & LBL 9. CONTINUATION CARD 8783611 OPERATIONS 333. FABRICATED, R & R FS 280 CLIPS IAW REO 601R-53-11-926 & SRM 51-42-21.
- [SDR REXA2016040100586](https://openairdocs.org/sdr/REXA2016040100586.md): Skin · chafed · Apr 1, 2016 · N8836A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING INBD LOWER SKIN, WING PLANK, CHAFED FROM FAIRING APPROX 3.0 X.400 X.003 DEEP. REPAIRED IAW REO 601R-57-21-880 REV C DATED 2011 07 18. THIS IS A MAJOR REPAIR. REPAIR PERFORMED TO ZONE A,.010" MATERIAL REMOVED.
- [SDR REXA2016033100593](https://openairdocs.org/sdr/REXA2016033100593.md): Skin · damaged · Mar 31, 2016 · N8836A · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK CUT OUT FOR FUEL PANEL 540FB, HAS FRETTING DAMAGE ON INBD & OTBD ENDS, NON-CRITICAL REGION. REPAIRED FUEL PANEL 540FB WING PLANK CUT OUT IAW REO 601R-57-21-030 REV L DATED 02 05 14. THIS IS A MAJOR REPAIR.
- [SDR REXA2016033100592](https://openairdocs.org/sdr/REXA2016033100592.md): Skin · damaged · Mar 31, 2016 · N8836A · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK CUT OUT FOR FUEL PANEL 550HB, INBD SIDE HAS FRETTING DAMAGE, NON-CRITICAL REGION. REPAIRED FUEL PANEL 550HB WING PLANK CUT OUT IAW REO 601R-57-21-030 REV L DATED 02 05 14. THIS IS A MAJOR REPAIR.
- [SDR REXA2016033100591](https://openairdocs.org/sdr/REXA2016033100591.md): Skin · damaged · Mar 31, 2016 · N8836A · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK CUT OUT FOR FUEL PANEL 540BB, HAS FRETTING DAMAGE ON INBD SIDE, NON-CRITICAL REGION. REPAIRED FUEL PANEL 540BB WING PLANK CUT OUT IAW REO 601R-57-21-030 REV L DATED 02 05 14. THIS IS A MAJOR REPAIR.
- [SDR REXA2016033100585](https://openairdocs.org/sdr/REXA2016033100585.md): Panel · chafed · Mar 31, 2016 · N8836A · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT INBD WING, BOTTOM WING PANEL CHAFED FROM FAIRING, APPROX 1.5 X.300 X.004 DEEP. REPAIRED IAW REO 601R-57-21-880 REV C DATED 07 18 11. THIS IS A MAJOR REPAIR. REPAIR PERFORMED TO ZONE A,.030" MATERIAL REMOVED.
- [SDR REXA2016032900563](https://openairdocs.org/sdr/REXA2016032900563.md): Stringer · cracked · Mar 29, 2016 · N8836A · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L AT FS 379 IS CRACKED APPROX.25". REPAIRED DAMAGE IAW SRM 51-42-06, 51-42-21 & 53-00-03.
- [SDR REXA2016032600590](https://openairdocs.org/sdr/REXA2016032600590.md): Skin · damaged · Mar 26, 2016 · N8836A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING PLANK CUT OUT FOR FUEL PANEL 650HB, HAS FRETTING DAMAGE ON INBD SIDE, NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030 REV L DATED 2014 02 05. REFER TO ATTACHED REO FOR WORK PERFORMED. THIS IS A MAJOR REPAIR.
- [SDR REXA2016032600589](https://openairdocs.org/sdr/REXA2016032600589.md): Skin · damaged · Mar 26, 2016 · N8836A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING PLANK CUT OUT FOR FUEL PANEL 640BB, HAS FRETTING DAMAGE ON INBD & OTBD ENDS, NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030 REV L DATED 2014 02 05. REFER TO ATTACHED REO FOR WORK PERFORMED. THIS IS A MAJOR REPAIR.
- [SDR REXA2016032600588](https://openairdocs.org/sdr/REXA2016032600588.md): Skin · damaged · Mar 26, 2016 · N8836A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING PLANK FUEL PANEL CUT OUT FOR FUEL PANEL 640DB, HAS FRETTING DAMAGE ON INBD, OTBD & FWD EDGES. BOTH CRITICAL & NON-CRITICAL REGIONS. REPAIRED IAW REO 601R-57-21-030 REV L DATED 2014 02 05. THIS IS A MAJOR REPAIR. REFERENCE ATTACHED REO FOR
- [SDR REXA2016032600577](https://openairdocs.org/sdr/REXA2016032600577.md): Cup · corroded · Mar 26, 2016 · N8836A · Cndair CL6002B19 · Passenger/Crew Doors
  > FORWARD & AFT PAX DOOR HANDRAIL CUPS ARE CORRODED AROUND FASTENER HOLES, FS 310 & 349. REPLACED FWD & AFT PAX DOOR HANDRAIL CUPS WITH NEW SERVICEABLE CUPS IAW SRM 51-40-11, 51-42-06, 51-42-21, 51-42-13 & 51-12-00. PN REPLACED 601R31527-137 149.

Next page: https://openairdocs.org/aircraft/N8836A/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 = 'N8836A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8836A/reports

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