# Service difficulty reports: N8886A

A list on [N8886A](https://openairdocs.org/aircraft/N8886A.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 · 112 reports

- [SDR REXA2020121700837](https://openairdocs.org/sdr/REXA2020121700837.md): Battery Pack · inoperative · Dec 15, 2020 · N8886A · Cndair CL6002B19 · Emergency Lighting
  > CEILING MOUNTED "EXIT" SIGN LIGHTS INOPERABLE. REMOVED AND REPLACED BATTERY PACK FOR CEILING MOUNTED EXIT LIGHT SIGN, IAW CRJ-200 AMM 33-51-04. OPERATIONS CHECK GOOD. P/N OFF 2013-1A P/N ON 2013-1ASMI S/N ON 10046 S/N OFF 102558.
- [SDR REXA2020070600573](https://openairdocs.org/sdr/REXA2020070600573.md): Bulb · inoperative · May 5, 2020 · N8886A · Cndair CL6002B19 · Emergency Lighting
  > CABIN CEILING EMERGENCY LIGHT BETWEEN ROWS 4 AND 5 IS INOP. REMOVED AND REPLACED LAMP IAW AMM 33-51-16. OPS CHECK GOOD. PN ON: 1317 PN OFF: 1317.
- [SDR REXA2019110731565](https://openairdocs.org/sdr/REXA2019110731565.md): Battery Pack · inoperative · Nov 3, 2019 · N8886A · Cndair CL6002B19 · Emergency Lighting
  > DURING FIRST FLIGHT PREPARATIONS, FOUND INTERIOR AND EXTERIOR OVER WING AND FLOOR TRACK LIGHTS INOP REMOVED AND REPLACED THE #2 AND #3 EMERGENCY LIGHT BATTERY PACKS IAW AMM 33-51-04. OPS CHECK GOOD
- [SDR REXA2019082211250](https://openairdocs.org/sdr/REXA2019082211250.md): Light · inoperative · Aug 21, 2019 · N8886A · Cndair CL6002B19 · Emergency Lighting
  > FLOOR LEVEL EMERGENCY LIGHT AT THE PASSENGER DOOR IS NOT WORKING. R&R'D FLOOR LEVEL EMERGENCY FLOOD LIGHT ASSY IAW AMM 33-51-19. OPS CHECK GOOD
- [SDR REXA2019061070815](https://openairdocs.org/sdr/REXA2019061070815.md): Wire · broken · Jun 7, 2019 · N8886A · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHTS IN GALLEY WONT ILLUMINATE WHEN TESTED. REPAIRED BROKEN WIRE TO LIGHT ASSEMBLY IAW CRJ200 ESPM 20-16-00. OPS CHECK GOOD.
- [SDR REXA20190130099](https://openairdocs.org/sdr/REXA20190130099.md): Sign · inoperative · Jan 29, 2019 · N8886A · Cndair CL6002B19 · Emergency Lighting
  > FLOOR LEVEL EXIT SIGN INOP. REPLACED EXIT SIGN IAW AMM 33-51-10 OPS CHECK GOOD
- [SDR REXA2018080300661](https://openairdocs.org/sdr/REXA2018080300661.md): Fitting · corroded · Jul 24, 2018 · N8886A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT O/B FLOORBEAM ATTACH TO APB, HAS CORROSION AT FASTENER HOLE. REPAIRED RT O/B FLOORBEAM FITTING IAW EA 253-07317.
- [SDR REXA2018080300660](https://openairdocs.org/sdr/REXA2018080300660.md): Seat Track · corroded · Jul 24, 2018 · N8886A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL27 FLOOR SUPPORT BETWEEN FS574.0 AND FS609.0 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06 FOUND TO BE OUT OF LIMTS IAW SRM 53-00-00. REMOVED AND REPLACED SEAT RAIL BEAM LBL 27 SRM 51-42-21.
- [SDR REXA2018080300658](https://openairdocs.org/sdr/REXA2018080300658.md): Frame · cracked · Jul 24, 2018 · N8886A · Cndair CL6002B19 · Fuselage Main, Frame
  > CARGO BAY AT 605 9L FRAME CRACKED. REPAIRED FRAME 605 IAW REO 601R-53-61-5214.
- [SDR REXA2018080300655](https://openairdocs.org/sdr/REXA2018080300655.md): Retainer · cracked · Jul 24, 2018 · N8886A · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENG PNL 412BT SEAL RETAINER IS CRACKED. REMOVED AND REPLACED SEAL RETANER ON PNL 412BT IAW SRM 51-42-06.
- [SDR REXA2018080300657](https://openairdocs.org/sdr/REXA2018080300657.md): Stringer · cracked · Jul 22, 2018 · N8886A · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STR 3L IS CRACKED JUST BELOW THE UPPER PAX DOOR SILL AT FS 379, IN THE CABIN. R&R STRINGER 3L STATION 379 TO 409 IAW SRM 51-42-06. OPS TEST OF LIGHTING C/W ON W/O.
- [SDR REXA2018080300656](https://openairdocs.org/sdr/REXA2018080300656.md): Fitting · cracked · Jul 19, 2018 · N8886A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLIGHT DECK CENTER WINDSHIELD POST LOWER LEFT FITTING IS CRACKED. (NDT HAS VERIFIED). REMOVED AND REINSTALLED REF ITEMS 1-4-7 IAW REM ITEMS 1-4& 7 OPS TEST OF EFDS 3 & 4 GOOD IAW AMM 31-61-01-710-801 ISI WAS NEVER REMOVED THEREFORE LEAK CHECK OF THE P3 S3 AND
- [SDR REXA2018080300654](https://openairdocs.org/sdr/REXA2018080300654.md): Stiffener · cracked · Jul 19, 2018 · N8886A · Cndair CL6002B19 · APU Cowling/Containment
  > CRACK IN WELD AT APU ENCLOSURE UPPER CENTER STIFFENER AT AFT END. REPAIRED APU ENCLOSURE UPPER CENTER STIFFENER IAW REO 601R-49-11-071.
- [SDR REXA2018080300664](https://openairdocs.org/sdr/REXA2018080300664.md): Fitting · cracked · Jul 13, 2018 · N8886A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BEAM CLIP IS CRACKED AT FS484.00 BL36R. REPAIRED FLOOR SUPPORT BEAM CLIP AT STATION 484 BL36R IAW REV 601 R-53-41-059.
- [SDR REXA2018080300662](https://openairdocs.org/sdr/REXA2018080300662.md): Angle · cracked · Jul 7, 2018 · N8886A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > EVIDENCE OF A CRACK ON AN ANGLE BRACKET OF THE AFT PRESSURE BULKHEAD RT SIDE AROUND STR 14A. REMOVED AND REPLACED ANGLE AT STRINGER 14R IAW SRM 51-42-06.
- [SDR REXA2018061100482](https://openairdocs.org/sdr/REXA2018061100482.md): Post · cracked · Jun 11, 2018 · N8886A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING COMPLIANCE OF TC53-160-604, 10K INSP, VERT POST RBL 27.00 AT FS 409+128 HAS A CRACK ON THE IB CHANNEL. CRACK EXTENDS UP FROM THE BOTTOM EDGE UP TO BUT NOT PAST 2ND RIVET UP. PERMANENTLY REPAIRED VERTICAL POST RBL 27.00 AT FS 409+128 IAW REO 601R-53-41-0
- [SDR REXA2018040600251](https://openairdocs.org/sdr/REXA2018040600251.md): Light · inoperative · Apr 6, 2018 · N8886A · Cndair CL6002B19 · Emergency Lighting
  > EXTERIOR LT AFT EMERGENCY LIGHT OUT. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR REXA2017102801133](https://openairdocs.org/sdr/REXA2017102801133.md): Intercostal · cracked · Oct 28, 2017 · N8886A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT TOP INTERCOSTAL OTBD OF RBL 36.2 BS 621 TO 625.3, STRINGER 14R CRACKED ONE INCH.
- [SDR REXA2017091901014](https://openairdocs.org/sdr/REXA2017091901014.md): Microphone · inoperative · Sep 19, 2017 · N8886A · Cndair CL6002B19 · Audio Integrating System
  > OBSEVER OXYGEN MASK MICROPHONE INOPERATIVE. R & R THE OXYGEN MASK IAW AMM 35-11-12. PERFORMED AN OPS CHECK IAW AMM 23-51-00. CHECKED GOOD.
- [SDR REXA2017082500926](https://openairdocs.org/sdr/REXA2017082500926.md): Light · inoperative · Aug 25, 2017 · N8886A · Cndair CL6002B19 · Emergency Lighting
  > FORWARD FLOOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-51-01. OPERATIONAL CHECKED GOOD IAW AMM 33-51-00.
- [SDR REXA2017041900525](https://openairdocs.org/sdr/REXA2017041900525.md): Sign · inoperative · Apr 19, 2017 · N8886A · Cndair CL6002B19 · Emergency Lighting
  > FOUND LIGHTED EXIT SIGN FLOOR LEVEL AT MAIN ENTRANCE ON LEFT, INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-51-10. OPS CHECKED GOOD.
- [SDR REXA2017041300503](https://openairdocs.org/sdr/REXA2017041300503.md): Control Unit · loose · Apr 13, 2017 · N8886A · Cndair CL6002B19 · Audio Integrating System
  > FIRST OFFICER`S OXYGEN MASK FAILED TO TEST OVER THE SPEAKER. REPLACED THE OXYGEN BOX IAW AMM 35-11-15. DURING OPERATIONAL CHECKS, FOUND THE AECU LOOSE IN THE RACK. SECURED AECU 23-51-00. REPERFORMED OPERATIONAL CHECKS OF THE FO OXYGEN BOX, ALL CHECKS (AUDI
- [SDR REXA2017030600323](https://openairdocs.org/sdr/REXA2017030600323.md): Lamp · inoperative · Mar 6, 2017 · N8886A · Cndair CL6002B19 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-00, OPS TESTED NORMAL.
- [SDR REXA2017020400168](https://openairdocs.org/sdr/REXA2017020400168.md): Elt · inoperative · Feb 4, 2017 · N8886A · Cndair CL6002B19 · Emergency Locator Beacon
  > ELT FAILS OPERATIONAL TEST. REMOVED AND REPLACED ELT IN ACCORDANCE WITH AMM 25-62-01. OPS GOOD AT THIS TIME P/N ON AND OFF 453-5000 S/N ON 04010 S/N OFF 170-14569.
- [SDR REXA2017010200003](https://openairdocs.org/sdr/REXA2017010200003.md): Oxygen Mask · unwanted deploy · Jan 2, 2017 · N8886A · Cndair CL6002B19 · Passenger Oxygen System
  > FOUND OXYGEN MASKS DEPLOYED. STOWED ALL OXYGEN MASKS IAW AMM 35-21-09. PERFORMED OPS TEST IAW AMM 35-20-00. TEST PASS. ACFT OK FOR SERVICE.
- [SDR REXA2016112102257](https://openairdocs.org/sdr/REXA2016112102257.md): Detector · inoperative · Nov 21, 2016 · N8886A · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAPS FAIL MASTER CAUTION FLAPS SELECTED OUT OF ZERO TO 20 FLAPS FAILED AT 0 DEGREES. INSPECTED SDU NOTED FAULTS ON LT AND RT CHANNELS, RESET SDU IAW AMM 27-51-15. PERFORMED OPERATIONAL TEST OF THE FLAP SYS IAW 27-54-00. PLACED FLAP SYSTEM IN MEL DUE TO DUAL
- [SDR REXA2016102502014](https://openairdocs.org/sdr/REXA2016102502014.md): Oxygen Mask · unwanted deploy · Oct 25, 2016 · N8886A · Cndair CL6002B19 · Passenger Oxygen System
  > OXYGEN MASKS DROPPED OVER SEAT 4 CD. REPACKED THE OXYGEN MASK IAW AMM 35-21-09. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR REXA2016091301721](https://openairdocs.org/sdr/REXA2016091301721.md): Acm · out of adjust · Sep 13, 2016 · N8886A · Cndair CL6002B19 · Cabin Cooling System
  > AFTER TAKEOFF AND SWITCHES TO 10TH STAGE BLEEDS THERE WAS A NOTICEABLE ODOR IN FLIGHT DECK AND CABIN. ODOR DISSIPATED IN CABIN BUT PERSISTED IN FLIGHT DECK, MINOR BUT DETECTABLE. PERFORMED ADJUSTMENT TEST OF ACM IAW AMM 21-51-00. NO DEFECTS NOTED.
- [SDR REXA2016070101194](https://openairdocs.org/sdr/REXA2016070101194.md): Light · inoperative · Jul 1, 2016 · N8886A · Cndair CL6002B19 · Emergency Lighting
  > RIGHT FWD EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R LAMP AT RT FWD EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. NO FURTHER DEFECTS NOTED.
- [SDR REXA2016050700783](https://openairdocs.org/sdr/REXA2016050700783.md): Wire · damaged · May 7, 2016 · N8886A · Cndair CL6002B19 · Light System Wiring
  > CABIN DOOR NOT LIGHTING UP, EMER LIGHTS. REPAIRED WIRE AT LIGHT IAW ESPM 20-16-00. OPERATIONS CHECKED GOOD.
- [SDR REXA2016022900317](https://openairdocs.org/sdr/REXA2016022900317.md): Battery Pack · discharged · Feb 29, 2016 · N8886A · Cndair CL6002B19 · Emergency Equipment
  > PILOT & CO-PILOT EMER FLASHLIGHTS ARE INOPERATIVE. REMOVED & INSTALLED NEW SERVICEABLE BATTERY PACK, PN P4-01-0021, IN PILOT & CO-PILOT EMER FLASHLIGHTS IAW AMM 25-61-00-960-801. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR REXA2016022900302](https://openairdocs.org/sdr/REXA2016022900302.md): Landing · damaged · Feb 29, 2016 · N8886A · Cndair CL6002B19 · Wing, Plate/Skin
  > ACCESS HOLE FOR FUEL PANEL 540BB HAS DAMAGE ON THE LANDING. REPAIRED 540BB FUEL ACCESS WING PLANK LANDING. REF STEPS 1 - 4 FOR WORK PERFORMED. REO 601R-57-21-2418 COMPLIED WITH. THIS IS A MAJOR REPAIR.
- [SDR REXA2016022900288](https://openairdocs.org/sdr/REXA2016022900288.md): Step · dented · Feb 29, 2016 · N8886A · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR, MID FIXED STEP IS DENTED, APPROX 2" IN DIAMETER. LOCATED, DRILLED & COUNTERSUNK NEW SERVICEABLE FIXED MID STEP, PN 601R317076-9, IAW SRM CH 51-40-11.
- [SDR REXA2016022800319](https://openairdocs.org/sdr/REXA2016022800319.md): Connector · broken · Feb 28, 2016 · N8886A · Cndair CL6002B19 · Light System Wiring
  > CABIN TRACK LIGHTING, FWD CONNECTION HAS A BROKEN CONNECTOR PLUG. EMER FLOOR TRACK LIGHTING WAS REPAIRED BY REPLACING SPLICE IAW ESPM 20-17-31 & REPLACING NR 4 BATTERY CHARGER IAW AMM 33-51-05-400-801. OPERATIONS CHECKED GOOD.
- [SDR REXA2016022800316](https://openairdocs.org/sdr/REXA2016022800316.md): Flashlight · inoperative · Feb 28, 2016 · N8886A · Cndair CL6002B19 · Emergency Equipment
  > WARDROBE COMPARTMENT EMER FLASHLIGHT INOPERATIVE. R & R WARDROBE COMPARTMENT EMERGENCY FLASHLIGHT IAW AMM 20-21-00-910-801 & BY REMOVING 2 SCREWS, INSTALLING NEW LIGHT & INSTALLING 2 SCREWS.
- [SDR REXA2016022800314](https://openairdocs.org/sdr/REXA2016022800314.md): Rib · corroded · Feb 28, 2016 · N8886A · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > BATTERY RIBS ON LT SIDE AT WING STATION 48.30 & 53.60, HAVE CORROSION. CONTINUATION CARD 8788615 OP 50, 51, 53 & 70. R & R LT WING LOWER SKIN PANEL, PN 601R10213-3, IAW SRM 51-42-21. REPAIRED IAW EA CRJ257-04062. R & R BATTERY RIB, PN 601R10203-27, AT WS 5
- [SDR REXA2016022800289](https://openairdocs.org/sdr/REXA2016022800289.md): Bulkhead · chafed · Feb 28, 2016 · N8886A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD IS CHAFED IN MULTIPLE LOCATIONS, FROM CARGO LINER SCREWS. CONTINUATION CARD 8788611 OP 171 & 187. REPAIRED CHAFE IN 621 BULKHEAD IAW STEPS 1 - 12 FOR WORK PERFORMED. THIS IS A MAJOR REPAIR IAW 601R-53-61-1285 REV D 2155 REV A & - 5648.
- [SDR REXA2016022800279](https://openairdocs.org/sdr/REXA2016022800279.md): Skin · corroded · Feb 28, 2016 · N8886A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN FS 559+64 - 559+112, STRINGER 25L - 25R, HAS CORROSION AROUND LOCK FASTENERS. CONTINUATION CARD 8788611 OP 160 & 223. REPAIRED EXTERIOR SKIN CORROSION AROUND LOCK FASTENERS IAW EA CRJ253-04013. REF JC 8788611 OPS 63, 160, & 223 STEPS 1 - 12 FO
- [SDR REXA2016022700313](https://openairdocs.org/sdr/REXA2016022700313.md): Bulkhead · damaged · Feb 27, 2016 · N8886A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESS BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX.100" IN LENGTH, 50% FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1230 REV F DATED 10 31 11. THIS IS A MAJOR REPAIR.
- [SDR REXA2016022700311](https://openairdocs.org/sdr/REXA2016022700311.md): Landing · damaged · Feb 27, 2016 · N8886A · Cndair CL6002B19 · Wing, Plate/Skin
  > FOUND RT FUEL ACCESS HOLE 650AB LANDING, INBD SIDE HAS MULTIPLE INDICATIONS NOTED APPROX 7.O" INCHES LONG BY.250 WIDE 50% FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-57-21-030 REV L. THIS IS A MAJOR REPAIR.
- [SDR REXA2016022600309](https://openairdocs.org/sdr/REXA2016022600309.md): Panel · damaged · Feb 26, 2016 · N8886A · Cndair CL6002B19 · Vertical Stabilizer
  > PANEL 326BL FOUND TO BE SPLIT ON UPPER RT CORNER OF PANEL. REPAIRED PANEL 326BL IAW REO 601R-55-32-233 REV A DATED 05 05 09 & SRM 51-25-01. REINSTALLED PANEL 326BL IAW AMM 55-32-05-400-805.
- [SDR REXA2016022600308](https://openairdocs.org/sdr/REXA2016022600308.md): Hinge · damaged · Feb 26, 2016 · N8886A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY STEP PLATE FWD HINGE REQUIRES REPLACEMENT DUE TO ELONGATED HOLE, AS WELL AS CTR HINGE. R & R FWD & MIDDLE HINGES, PN 601R35205-69 IAW SRM 51-42-06 & 51-40-11. ALSO PN 601R35205-67.
- [SDR REXA2016022500307](https://openairdocs.org/sdr/REXA2016022500307.md): Hinge · broken · Feb 25, 2016 · N8886A · Cndair CL6002B19 · Wing, Plate/Skin
  > BUTTE DOOR PANEL 694JB HINGE IS BROKEN. R & R BUTTE DOOR PANEL 694JB HINGE IAW SRM 51-25-16, 51-42-06 & 51-25-06.
- [SDR REXA2016022500301](https://openairdocs.org/sdr/REXA2016022500301.md): Landing · damaged · Feb 25, 2016 · N8886A · Cndair CL6002B19 · Wing, Plate/Skin
  > ACCESS HOLE FOR FUEL PANEL 640BB HAS DAMAGE TO THE LANDING. CONTINUATION CARD 8788611 OP 222. REPAIRED FUEL TANK CUT OUT FOR 640BB IAW REO 601R-57-21-030 REV L DATED 02 05 14. LEAK CHECKED GOOD. THIS IS A MAJOR REPAIR.
- [SDR REXA2016022400306](https://openairdocs.org/sdr/REXA2016022400306.md): Fairing · gouged · Feb 24, 2016 · N8886A · Cndair CL6002B19 · Aerodynamic Fairings
  > RIGHT STUB FAIRING HAS GOUGE MEASURING.015" DEEP. RECEIVED NEW SERVICEABLE STUB FAIRING ASSEMBLY PN 601R31199-92. INSTALLED SEAL ONTO STUB FAIRING IAW SRM 51-42-15. REF MWC JOB 8788610 OP 507 FOR INSTALL OF STUB FAIRING.
- [SDR REXA2016022400305](https://openairdocs.org/sdr/REXA2016022400305.md): Retainer · corroded · Feb 24, 2016 · N8886A · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > AVI BAY DOOR SEAL RETAINERS ARE CORRODED FWD EDGE AFT OF SEAL MARKED WITH TAPE. CONTINUATION CARD 8788611 OP 159 & 192. R & R AVI BAY DOOR SEAL RETAINERS IAW SRM 51-42-06 & 51-40-11. REF MWC JOB 8788611 85, 159 & 192 FOR WORK PERFORMED.
- [SDR REXA2016022400297](https://openairdocs.org/sdr/REXA2016022400297.md): Frame · corroded · Feb 24, 2016 · N8886A · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME SECTOR FS 333 IS CORRODED, BETWEEN STRINGER 26R & 26L. CONTINUATION CARD 8788611 OP 166. R & R FS 333 FRAME SECTOR IAW SRM 51-42-06 & 51-42-21.
- [SDR REXA2016022400294](https://openairdocs.org/sdr/REXA2016022400294.md): Frame · corroded · Feb 24, 2016 · N8886A · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME SECTOR FS 605 AT STRINGER 26R IS CORRODED. CONTINUATION CARD 8788611 OP 158, 164, 180, & 211. R & R FS 605 FRAME IAW SRM 51-42-06, 51-42-11 & 51-42-21. REF JC 8788611 OPS 111, 158, 164, 180 & 211 STEPS 1 - 25 FOR WORK PERFORMED.
- [SDR REXA2016022400293](https://openairdocs.org/sdr/REXA2016022400293.md): Frame · corroded · Feb 24, 2016 · N8886A · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME SECTOR FS 585 AT STRINGER 26R IS CORRODED. CONTINUATION CARD 8788611 OP 167 & 172. REPLACED FRAME AT FS 589, DUE TO CORROSION BEING OUT OF LIMITS IAW SRM 51-42-06, 51-42-21. IAW MWC JOB 8788611 110, 167 & 172 FOR WORK PERFORMED. FRAME AT 589 NOT 585 C
- [SDR REXA2016022400280](https://openairdocs.org/sdr/REXA2016022400280.md): Bracket · cracked · Feb 24, 2016 · N8886A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AIRCRAFT GND POWER RECEPTACLE BRACKET IS CRACKED. CONTINUATION CARD 8788611 OP 165 & 178. REPLACED ACFT GND POWER RECEPTACLE BRACKET IAW SRM 51-40-00, 51-42-21, 51-40-11, 51-42-06 & 51-23-00. REF MWC JOB 8788611 65, 165, 178 & 206 FOR WORK PERFORMED.

Next page: https://openairdocs.org/aircraft/N8886A/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 = 'N8886A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8886A/reports

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