# Service difficulty reports: N8982A

A list on [N8982A](https://openairdocs.org/aircraft/N8982A.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR SWIA2018091245048](https://openairdocs.org/sdr/SWIA2018091245048.md): Control Panel · deployed · Sep 12, 2018 · N8982A · Cndair CL6002B19 · Hydraulic System, Main
  > ON DESCENT THROUGH 9000 FEET LARGE VIBRATIONS BEGAN. NO CAS MESSAGES AND NO MAJOR HYDRAULIC OR MECHANICAL IRREGULARITIES NOTED. (FLT 4970) CLOSED UPON ARRIVAL, FOUND ADG DEPLOYED. PERFORMED ADG DEPLOYMENT CHECK IAW AMM. NO DEFECTS NOTED. RE-STOWED ADG IAW AMM
- [SDR SWIA2017120544009](https://openairdocs.org/sdr/SWIA2017120544009.md): Selector Valve · failed · Nov 27, 2017 · N8982A · Cndair CL6002B19 · Landing Gear Selector
  > GEAR DISAGREE WARNING MSG WHEN EXTENDING THE GEAR. EMERGENCY WAS DECLARED & A/C LANDED WITHOUT INCIDENT. (FLT 4975) CLOSED REMOVED AND REPLACED NLG SELECTOR VALVE ASSY IAW AMM. OPS CHECK GOOD.
- [SDR SWIA201743009](https://openairdocs.org/sdr/SWIA201743009.md): Warning Message · illuminated · Jan 24, 2017 · N8982A · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > RIGHT COWL ANTI-ICE CAUTION IN FLIGHT. EMERGENCY DECLARED. REPLACED BOTH PRESSURE SWITCH AND VALVE. OPS CHECKED GOOD.
- [SDR SWIA201642099](https://openairdocs.org/sdr/SWIA201642099.md): Vane · chafed · Apr 10, 2016 · N8982A · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE CENTER L/E CAP AT WS 97.0 CHAFED OUT OF LIMITS. INSTALLED NEW RT INBD FLAP VANE CENTER L/E SKIN CAP IAW SRM.
- [SDR SWIA201642098](https://openairdocs.org/sdr/SWIA201642098.md): Vane · chafed · Apr 9, 2016 · N8982A · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING, INBD FLAP VANE CHAFED OUT OF LIMITS AT WS97.0. WET INSTALLED NEW LT INBD FLAP VANE CENTER L/E SKIN, IAW SRM.
- [SDR SWIA201642102](https://openairdocs.org/sdr/SWIA201642102.md): Bulkhead · gouged · Apr 8, 2016 · N8982A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD HAS 15 AREAS WITH SMALL CIRCULAR GOUGES. REPAIRED IAW REO. LEAK CHECKED GOOD, NO LEAKS NOTED.
- [SDR SWIA201642101](https://openairdocs.org/sdr/SWIA201642101.md): Rub Strip · chafed · Apr 6, 2016 · N8982A · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING, INBD FLAP OTBD HINGE ARM RUB STRIP CHAFED. R & R LT WING, INBD FLAP OTBD HINGE ARM, INBD RUB STRIP IAW SRM.
- [SDR SWIA201642100](https://openairdocs.org/sdr/SWIA201642100.md): Threshold · corroded · Apr 6, 2016 · N8982A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR THRESHOLD PLATE HAS SOME CORROSION AROUND FASTENER HOLES. SERVICE DOOR THRESHOLD PLATE REPLACED WITH A NEW THRESHOLD PLATE, PN 601R38957-31 IAW SRM.
- [SDR SWIA201440391](https://openairdocs.org/sdr/SWIA201440391.md): Diode · failed · Dec 10, 2014 · N8982A · Cndair CL6002B19 · Engine Thrust Reverser
  > RT THRUST REVERSER UNLOCK MESSAGE. RETURNED TO FIELD. REMOVED AND REPLACED TB207-7 ASSY FOR DIODE 2CR7KE IAW ESPM.
- [SDR REXA2014082600782](https://openairdocs.org/sdr/REXA2014082600782.md): Skin · dented · Aug 26, 2014 · N8982A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MAINTENANCE FOUND THE FUSELAGE SKIN FROM FS 625 TO FS 640 JUST BELOW STRINGER 20L TO BE DENTED, MEASURING 13.5” X 1.38” X 0.008” DEEP. REPAIRED IAW EA CRJ253-02680.
- [SDR REXA2014040100346](https://openairdocs.org/sdr/REXA2014040100346.md): Safety Wire · broken · Apr 1, 2014 · N8982A · Cndair CL6002B19 · Emergency Equipment
  > SAFETY WIRE ON FIRST AID KIT BROKEN. R & R FIRST AID KIT IAW AMM 25-61-00.
- [SDR REXA2014030700027](https://openairdocs.org/sdr/REXA2014030700027.md): Intercostal · cracked · Mar 5, 2014 · N8982A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN FS 621 & FS 625.3, BETWEEN STRINGER 14L & STRINGER 13L CRACKED. REPLACED IAW SRM 51-40-11, 51-42-21 & 51-42-22.
- [SDR REXA2014030700026](https://openairdocs.org/sdr/REXA2014030700026.md): Intercostal · cracked · Mar 5, 2014 · N8982A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BULKHEAD INTERCOSTAL CRACKED 0.5 INCHES ON OTBD FWD SIDE OF FS 625 AT STRINGER 14L. REPLACED IAW SRM 51-42-06 & 51-42-2151-42-22.
- [SDR REXA2014030700025](https://openairdocs.org/sdr/REXA2014030700025.md): Intercostal · cracked · Mar 5, 2014 · N8982A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BULKHEAD INTERCOSTAL CRACKED ON OTBD FWD SIDE OF FS 625 AT STRINGER 15L. REPLACED IAW SRM 51-42-0651-42-2151-42-22.
- [SDR REXA2014030300019](https://openairdocs.org/sdr/REXA2014030300019.md): Skin · chafed · Feb 28, 2014 · N8982A · Cndair CL6002B19 · Wing, Plate/Skin
  > FUEL ACCESS PANEL CUTOUT ON LT WING AT WS 12.245 CHAFED ON LANDING FOR DOOR 0.007 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2013061201184](https://openairdocs.org/sdr/REXA2013061201184.md): Container · torn · Jun 12, 2013 · N8982A · Cndair CL6002B19 · Life Jacket
  > OBSERVER`S LIFE VEST BAG TORN. R & R LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013050600648](https://openairdocs.org/sdr/REXA2013050600648.md): Angle · cracked · May 6, 2013 · N8982A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 559 SEMI-PRESSURE BULKHEAD CAP ANGLE AT RBL 9 AND LBL 9 FOUND CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-41-260/601R-53-41-609 AND PA 53-025.
- [SDR REXA2013032800601](https://openairdocs.org/sdr/REXA2013032800601.md): Life Vest · unserviceable · Mar 28, 2013 · N8982A · Cndair CL6002B19 · Life Jacket
  > ONE INFANT LIFE VEST BAG TORN. COMPLIED WITH PA 25-096A BY INSTALLING INFANT LIFE VEST.
- [SDR REXA2012122201815](https://openairdocs.org/sdr/REXA2012122201815.md): Wire Harness · faulty · Dec 22, 2012 · N8982A · Cndair CL6002B19 · Landing Gear System Wiring
  > AFTER TAKEOFF ON FLIGHT 4232 FROM DTW ONE SECOND AFTER THE GEAR COMMANDED UP, THE MASTER WARNING FOR GEAR DISAGREE AND NOSE DOOR OPEN CAME ON. QRH COMPLETED GEAR OPERATED NORMALLY DOWN. THE CREW PERFORMED AN AIR RETURN TO DTW. REMOVED AND REPLACED NLG SNSR
- [SDR REXA2012112901720](https://openairdocs.org/sdr/REXA2012112901720.md): Sign · unsecure · Nov 29, 2012 · N8982A · Cndair CL6002B19 · Emergency Lighting
  > EXIT SIGN BESIDE PASSENGER DOOR IS FALLING OFF. REMOVED AND REPLACED EMERGENCY FLOOD LIGHT IAW AMM 33-51-19. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR REXA2012112601711](https://openairdocs.org/sdr/REXA2012112601711.md): Bpsu · faulty · Nov 26, 2012 · N8982A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON FLIGHT 3663 (LGA - GRR) WHILE AT CRUISE RECEIVED A FLAPS FAIL CAUTION MESSAGE WHILE FLAPS AT 0. AIRCRAFT LANDED SAFELY. FLAP SYSTEM FAULT WAS CLEARED WITH CREW AND MOC. PER MOC CYCLE CB'S FROM CRJ FIM MESSAGE CLEARED OK FOR SERVICE MESSAGE CLEARED OK FOR
- [SDR REXA2012112501710](https://openairdocs.org/sdr/REXA2012112501710.md): Life Vest · unserviceable · Nov 25, 2012 · N8982A · Cndair CL6002D24 · Life Jacket
  > OBSERVERS LIFE VEST BAG TORN. REMOVED AND REPLACED OBSERVERSE LIFE VEST IN ACCORDANCE WITH AMM 25-61-03.
- [SDR REXA2012102001128](https://openairdocs.org/sdr/REXA2012102001128.md): Bulkhead · gouged · Oct 9, 2012 · N8982A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FORWARD SIDE OF FS 621 BULKHEAD HAS MULTIPLE GOUGES ON SKIN. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.
- [SDR REXA2012102201129](https://openairdocs.org/sdr/REXA2012102201129.md): Sill · corroded · Oct 8, 2012 · N8982A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SILL IS CORRODED AT FS 439 AND FS 484. RIGHT FLOOR SILL IS CORRODED AT FS 488 AND FS 499. REMOVED 0.005" OF MATERIAL. REPAIRED IAW BOMBARDIER REO 601R-53-41-666.
- [SDR REXA2012102201130](https://openairdocs.org/sdr/REXA2012102201130.md): Angle · cracked · Oct 7, 2012 · N8982A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT AND RIGHT LOWER WEB ANGLE CRACKED AT FS 280 OUTBOARD OF LBL 9 AND RBL 9. LEFT FS 280 FLOORBOARD UPPER FLANGE CRACKED AT LBL 9 OUTBOARD CLIP CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-171/601R-53-11-136.
- [SDR REXA2012052600792](https://openairdocs.org/sdr/REXA2012052600792.md): Light · inoperative · May 26, 2012 · N8982A · Cndair CL6002B19 · Emergency Lighting
  > LEFT NR 2 EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT NR 2 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR REXA2012043000596](https://openairdocs.org/sdr/REXA2012043000596.md): Bulb · inoperative · Apr 30, 2012 · N8982A · Cndair CL6002B19 · Emergency Lighting
  > FLT 4281, FWD CABIN EMERG OVERHEAD CEILING FLOOD LIGHT INOPERATIVE. REMOVED AND REPLACED FWD BULB, OPS CHECKED GOOD.
- [SDR REXA201200147](https://openairdocs.org/sdr/REXA201200147.md): Dcu · faulty · Jan 27, 2012 · N8982A · Cndair CL6002B19 · Central Computers
  > FLIGHT DIVERTED FOR: AFTER TAKEOFF NUMEROUS INDICATIONS AS FOLLOWS - WING ANTI-ICE SHOWN ON WHEN OFF; APU GEN SHOWED OFF WHEN ON; OVER SPEED AURAL WARNING ON AT ANY SPEED. REMOVED AND REPLACED NR 1 DCU IAW AMM 31-41-04 OP/C GOOD ALL FAULTS AND CAUTION MESSAGE
- [SDR REXA201100964](https://openairdocs.org/sdr/REXA201100964.md): Gearbox · out of rig · Dec 11, 2011 · N8982A · Cndair CL6002B19 · Power Lever
  > LEFT THRUST LEVER WILL NOT ADVANCE PAST 94 PERCENT AT FLIGHT LEVEL 170 IT APPEAR TO HIT STOPS 4 PERCENT PRIOR BEFORE READING MAX. FOUND LT ENG THROTTLE GEARBOX SPLINE TO BE OUT OF RIG. RIGGED PER AMM 76-11-17 AND PERFORMED ENGINE RUNS PER AMM 71-00-00. OP/C
- [SDR REXA201100795](https://openairdocs.org/sdr/REXA201100795.md): Life Vest · torn · Oct 30, 2011 · N8982A · Cndair CL6002B19 · Life Jacket
  > OBSERVER'S LIFE VEST TORN. REMOVED AND REPLACED OBSERVERS LIFE VEST IAW AMM 25-61-03. VERIFIED PART EFFECTIVITY.
- [SDR REXA201100727](https://openairdocs.org/sdr/REXA201100727.md): Gearbox · out of adjust · Oct 14, 2011 · N8982A · Cndair CL6002B19 · Power Lever
  > LT THRUST LEVER STOPS AT APPROX 94 PERCENT N1 FULL FWD. ADJUSTED THROTTLE GEARBOX AND THROTTLE CONTROL CABLE IAW AMM 76-10-00 OP CHECK AND FUNCTIONAL CHECK GOOD.
- [SDR REXA201100051](https://openairdocs.org/sdr/REXA201100051.md): Sill · corroded · Jan 17, 2011 · N8982A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DEEP CORROSION, PITTING, FLAKING OF METAL, ON SERVICE DOOR LOWER SILL PLATE ASSY. REMOVED AND REPLACED LOWER SILL PLATE ASSY IAW NDT PART 9, 53-21-08.
- [SDR REXA201100010](https://openairdocs.org/sdr/REXA201100010.md): Skin · dented · Jan 3, 2011 · N8982A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TWO DENTS 0.031" DEEP X 0.80" LONG X 0.50" WIDE AND 0.062" DEEP X 1.10" LONG X 0.50" WIDE ON FUSELAGE SKIN (DWG NUMBER 601R31062 REF.) LOCATED ON PAX DOOR CUTOUT FWD EDGE FS 310 AND BETWEEN STRINGER 15L AND 16 L. TEMPORARY REPAIR IAW BOMBARDIER REO 601R-53-2

## 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 = 'N8982A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8982A/reports

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