# Service difficulty reports: N8969A

A list on [N8969A](https://openairdocs.org/aircraft/N8969A.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 · 101 reports

- [SDR REXA2021111100940](https://openairdocs.org/sdr/REXA2021111100940.md): Intercostal · corroded · Oct 28, 2021 · N8969A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > "LBL9 SEAT RAIL BEAM REQUIRES REPLACEMENT PN 601R35031-263 " "REMOVED AND REPLACED LBL9 SEAT RAIL BEAM P/N 601R35031-263, IAW SRM 53-61-43, 51-42-21 " ADDITIONAL PART REPLACED: 601R35031-263
- [SDR REXA2021111100938](https://openairdocs.org/sdr/REXA2021111100938.md): Floorbeam · corroded · Oct 28, 2021 · N8969A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > "LBL 27 SEAT RAIL BEAM REQUIRES REPLACEMENT PN 601R35031-263 "
- [SDR REXA2021111100939](https://openairdocs.org/sdr/REXA2021111100939.md): Floorbeam · corroded · Oct 27, 2021 · N8969A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > "I/B FLANGE OF CARGO FLOOR SUPPORT BEAM AT LBL27, FS 614.5 HAS CORROSIO N AT NUTPLATE. " "REPAIRED CORROSION AT NUTPLATE IAW EA CRJ253-12328. SEE EA FOR DETAILS " ADDITIONAL PART REPLACED: 601R35031-2
- [SDR REXA2020011760047](https://openairdocs.org/sdr/REXA2020011760047.md): Light · inoperative · Jan 16, 2020 · N8969A · Cndair CL6002B19 · Emergency Lighting
  > UPON INSPECTION FOUND RH OVERWING EXTERIOR EMERGENCY LIGHT 6 BELOW AND BETWEEN THE PASSENGER WINDOWS AT FS416.50R INOP RELAMPED RH OVER WING EXTERIOR EMERGENCY LIGHT 6 IAW AMM 33-51-21, OPERATIONAL TEST GOOD, NO DEFECTS NOTED AT THIS TIME. P/N 1317
- [SDR REXA2019071101091](https://openairdocs.org/sdr/REXA2019071101091.md): Actuator · inoperative · Jul 11, 2019 · N8969A · Cndair CL6002B19 · Landing Gear Actuator
  > GEAR DISAGREE ON TAKEOFF (NOSEWHEEL) RESEATED LG MANUAL EXTENSION HANDLE,FULLY SEATED DEFERRING GEAR RETRACTION SYSTEM IAW MEL 32-30-1. MX PROCEDURES C/W. GEAR PINS INSTALLED AND SAFTIED. MMO2 UPDATED. PLACARD INSTALLED MOC#96164 NOTIFIED. REMOVED & REPLACED
- [SDR REXA2019022540172](https://openairdocs.org/sdr/REXA2019022540172.md): Lamp · inoperative · Feb 24, 2019 · N8969A · Cndair CL6002B19 · Emergency Lighting
  > RIGHT HAND EMERGENCY LIGHT INOP (OUTSIDE). RE-LAMPED EXTERIOR EMERGENCY LIGHT #6 IAW CRJ 200 CMM 33-52-07. ERFORMED OPS TEST. OS TEST PASSED. A/C OK FOR SVC. MMO2 UPDATED, PLACARD REMOVED. MOC NOTIFIED# 93942 MEL CLEARED.
- [SDR REXA2018123101359](https://openairdocs.org/sdr/REXA2018123101359.md): Bpsu · inoperative · Dec 31, 2018 · N8969A · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > SUPPLEMENTAL INFORMATION. FLAP FAIL CAUTION AT APPEX 1000FT 180KTS WHEN SELECTED FLAPS UP THEY MOVED TO 0 THEN RECIEVED MESSAGE OAT 10 JUST AFTER T/O. R&R RIGHT HAND BPSU IAW AMM 27-51-10 OPS CHECK GOOD SEE NRWC 634863 FOR DETAILS. PERFORMED TROUBLESHOOTING PE
- [SDR REXA2018123001358](https://openairdocs.org/sdr/REXA2018123001358.md): Bpsu · inoperative · Dec 30, 2018 · N8969A · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAP FAIL CAUTION AT 20 WITH LEVER AT 20 IN FLIGHT DURING EXTENSION AT APOX 1 HOUR IN FLIGHT AIRSPEED 200 OAT 7 PERFORMED FLAP RESET AND 5 CONSECUTIVE CYCLES AND DEFERRED FLAPS AND FLAP FAIL MESSAGE IN ACCORDANCE WITH MEL 27-50-1 NOTIFIED MOC 98628 ENTERED IN
- [SDR REXA2018110521038](https://openairdocs.org/sdr/REXA2018110521038.md): Vertical Beam · cracked · Nov 2, 2018 · N8969A · Cndair CL6002B19 · Fuselage Main, Structure
  > CRACK FOUND AT VERTICAL BEAM FS 409+128 LBL 18 ON THE OB ANGLE FLANGE REPAIRED CRACK IN VERTIVAL BEAM FS 409+128 LBL 18 OB IAW BOMBARDIER REO 601R-53-41-0056. THIS IS A MAJOR REPAIR.
- [SDR REXA2018100900939](https://openairdocs.org/sdr/REXA2018100900939.md): Floorbeam · corroded · Oct 3, 2018 · N8969A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT BEAM ATTACHMENT FITTING LBL27 FS 621.0 FLOOR ATTACHMENT NUTPLATE HOLES HAVE CORROSION. REPAIRED LBL 27 FLOOR BEAM FITTING IAW EA 253-07723.
- [SDR REXA2018100900952](https://openairdocs.org/sdr/REXA2018100900952.md): Bulkhead · gouged · Sep 28, 2018 · N8969A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > APB HAS HARDWARE GOUGE AT REPAIR. REMOVED/REPLACED REPAIR IAW REO 601R-53-61-1285.
- [SDR REXA2018100900951](https://openairdocs.org/sdr/REXA2018100900951.md): Bulkhead · gouged · Sep 28, 2018 · N8969A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD GOUGED IN SEVERAL LOCATIONS BY HARDWARE. REPAIRS TO AFT PRESSURE BULKHEAD MADE IAW REO 601R-53-61-2155.
- [SDR REXA2018092600954](https://openairdocs.org/sdr/REXA2018092600954.md): Seat Track · corroded · Sep 26, 2018 · N8969A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT AISLE SEAT TRACK STICK 4 HAS CORROSION, IN THE CABIN. REMOVED AND REPLACED RT AISLE SEAT TRACK STICK 4 IAW AMM 53-01-11.
- [SDR REXA2018092600950](https://openairdocs.org/sdr/REXA2018092600950.md): Housing · cracked · Sep 26, 2018 · N8969A · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > AVIONICS DOOR HANDLE HOUSING IS CRACKED, VERIFIED BY HFEC. REMOVED/REPLACED AVIONICS DOOR HANDLE ASSY WITH NEW HANDLE ASSY IAW AMM 52-42-03-400-801 AND SRM 51-42-21.
- [SDR REXA2018100900949](https://openairdocs.org/sdr/REXA2018100900949.md): Intercostal · cracked · Sep 24, 2018 · N8969A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN LBL27 AND LT SILL AT FS484.0 IS CRACKED ON INBD CLIP. REMOVED/REPLACED CLIP AT INTERCOSTAL BETWEEN LBL27 AND LT SILL AT FS484.0 IAW SRM 51-42-21.
- [SDR REXA2018100900948](https://openairdocs.org/sdr/REXA2018100900948.md): Bracket · cracked · Sep 24, 2018 · N8969A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR UPPER SILL HAS A CRACK ON L BRAKET AT FS280 BY STR3. FABRICATED/LOCATED/DRILLED/INSTALLED NEW L ANGLE AT FS280 STGR 3L IAW SRM 51-42-06 SRM 51-42-21 SRM 51-40-11 SRM 51-24-36 AND SRM 51-24-21.
- [SDR REXA2018100900941](https://openairdocs.org/sdr/REXA2018100900941.md): Attach Bracket · cracked · Sep 22, 2018 · N8969A · Cndair CL6002B19 · Wing, Attach Fittings
  > RT WING L/E PNL630JL INBD ATTACH BRACKET CRACKED AT SPAR TRANSITION AREA. REMOVED AND REPLACED RT WING L/E PNL 630JL INBD ATTACH BRACKET AT SPAR TRANSITION AREA IAW SRM 51-41-02.
- [SDR REXA2018100900940](https://openairdocs.org/sdr/REXA2018100900940.md): Support Bracket · cracked · Sep 22, 2018 · N8969A · Cndair CL6002B19 · Wing, Attach Fittings
  > RT WING INBD L/E, SPR VALVE SUPPORT BRACKET CRACKED. REMOVED AND REPLACED RT WING INBD L/E, SPR VALVE SUPPORT BRACKET IA SRM 51-42-06, 51-41-02, ESPM 20-20-00.
- [SDR REXA2018100900947](https://openairdocs.org/sdr/REXA2018100900947.md): Skin · chafed · Sep 21, 2018 · N8969A · Cndair CL6002B19 · Wing, Plate/Skin
  > LT LWR WING PLANK CHAFED BY CONTACT WITH AERODYNAMIC FAIRING PNL 193AB AT WS45.00. REPAIRED CHAFE IAW REO 601R-57-21-880.
- [SDR REXA2018100900946](https://openairdocs.org/sdr/REXA2018100900946.md): Skin · chafed · Sep 21, 2018 · N8969A · Cndair CL6002B19 · Wing, Plate/Skin
  > RT LWR WING PLANK CHAFED BY CONTACT WITH AERODYNAMIC FAIRING PNL 193AB AT WS45.00. REPAIRED CHAFE IAW REO 601R-57-21-880.
- [SDR REXA2018100900942](https://openairdocs.org/sdr/REXA2018100900942.md): Angle · bent · Sep 21, 2018 · N8969A · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN ENTRY DOOR STEP STRUCTURE STIFFENER ANGLE BENT. AFT STEP SUPPORT WALL BETWEEN TWO UPPER INSPECTION HOLES INSIDE. BENT STIFFENER IS OUT OF LIMITS REMOVED/LOCATED/DRILLED/INSTALLED NEW STIFFENER IAW SRM 52-00-00 AND SRM 51-42-06.
- [SDR REXA2018100900944](https://openairdocs.org/sdr/REXA2018100900944.md): Seat Track · corroded · Sep 20, 2018 · N8969A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT AISLE SEAT TRACK STICK 2 HAS CORROSION, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2018100900943](https://openairdocs.org/sdr/REXA2018100900943.md): Seat Track · corroded · Sep 20, 2018 · N8969A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT AISLE SEAT TRACK STICK 3 HAS CORROSION, IN THE CABIN. REMOVED/REPLACED NEW RT AISLE SEAT TRACK IAW SRM 53-01-11.
- [SDR REXA2018100900938](https://openairdocs.org/sdr/REXA2018100900938.md): Seat Track · corroded · Sep 18, 2018 · N8969A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDEWALL SEAT TRACK STICK 2 HAS CORROSION, IN THE CABIN. REMOVED OLD SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2018100900937](https://openairdocs.org/sdr/REXA2018100900937.md): Seat Track · corroded · Sep 18, 2018 · N8969A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDEWALL SEAT TRACK STICK 3 HAS CORROSION, IN THE CABIN. REMOVED OLD SEAT TRACK IAW AMM 53-01-11. REINSTALLED NEW SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2018100900936](https://openairdocs.org/sdr/REXA2018100900936.md): Seat Track · corroded · Sep 18, 2018 · N8969A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDEWALL SEAT TRACK STICK 7 HAS CORROSION, IN THE CABIN. REMOVED AND REPLACED LT SIDEWALL SEAT TRACK STICK 7 IAW AMM 53-01-11.
- [SDR REXA2018100900935](https://openairdocs.org/sdr/REXA2018100900935.md): Seat Track · corroded · Sep 13, 2018 · N8969A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT AISLE SEAT TRACK STICK 2 HAS CORROSION, IN THE CABIN. REMOVED/REPLACED SEAT TRACK IAW AMM 53-00-49.
- [SDR REXA2018100900934](https://openairdocs.org/sdr/REXA2018100900934.md): Seat Track · corroded · Sep 13, 2018 · N8969A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT AISLE SEAT TRACK STICK 1 HAS CORROSION, IN THE CABIN. REMOVED/REPLACED SEAT TRACK IAW AMM 53-00-49.
- [SDR REXA2018100900933](https://openairdocs.org/sdr/REXA2018100900933.md): Seat Track · corroded · Sep 13, 2018 · N8969A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDEWALL SEAT TRACK STICK 5 HAS CORROSION, IN THE CABIN. REMOVED/REPLACED SIDE SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2018070600600](https://openairdocs.org/sdr/REXA2018070600600.md): Oxygen Mask · leaking · Jul 6, 2018 · N8969A · Cndair CL6002B19 · Crew Oxygen System
  > FO OXYGEN MASK LEAKING. REPLACED MASK IAW AMM 35-10-01 OS CHECK GOOD. SERVICED CREW O2 IAW AMM 12-16-35 10 1900 PSI. CAP ON DOOR CLOSED.
- [SDR REXA2018062740540](https://openairdocs.org/sdr/REXA2018062740540.md): Angle · cracked · Jun 24, 2018 · N8969A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING COMPLIANCE OF TC 53-160-604, THE BS 409+128 INBD ANGLE AT LBL 9 HAD A CRACK EXTENDING UP FROM BOTTOM EDGE IN THE RADIUS OF LBL 9, THEN TRAILING INTO THE RIVETED FLANGE AREA SLIGHTLY. TOTAL LENGTH APPROX.718 INCH. REPAIRED THE ANGLE OF LBL 9.0 VERTI
- [SDR REXA2018062620539](https://openairdocs.org/sdr/REXA2018062620539.md): Angle · cracked · Jun 22, 2018 · N8969A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING COMPLIANCE OF JC 53-160-604, THE BS 409+128 INBD ANGLE, LBL 27 HAD A CRACK, EXTENDING UP FROM BOTTOM FLANGE, UP TO AND PAST THE FIRST RIVET, ENDING APPROX MID POINT BETWEEN FIRST AND SECOND RIVETS. REPAIRED THE ANGLE IAW REO 601R-53-41-056. MAJOR R
- [SDR REXA2018061870493](https://openairdocs.org/sdr/REXA2018061870493.md): Light · burned out · Jun 17, 2018 · N8969A · Cndair CL6002B19 · Emergency Lighting
  > LOWER MAIN CABIN ENTRY EMERGENCY FLOOD LIGHT WAS BURNED OUT. REMOVED & REPLACED THE FLOOD LIGHT IAW AMM 33-51-19-000. OPS CHECKED GOOD.
- [SDR REXA2018052800425](https://openairdocs.org/sdr/REXA2018052800425.md): Battery Pack · discharged · May 28, 2018 · N8969A · Cndair CL6002B19 · Emergency Equipment
  > COPILOT FLASHLIGHT INOP (LIGHT NOT BLINKING). REMOVED AND REPLACED COPILOT FLASH LIGHT BATTERY PACK IAW AMM 25-61-00. OPS CHECK GOOD.
- [SDR REXA2017111301161](https://openairdocs.org/sdr/REXA2017111301161.md): Oxygen Mask · inoperative · Nov 10, 2017 · N8969A · Cndair CL6002B19 · Crew Oxygen System
  > HARNESS ON THE CAPTAIN`S OXYGEN MASK WON'T FUNCTION PROPERLY. SWAPPED CAPTAIN`S AND OBSERVER`S OXYGEN MASK. REPLACED THE OBSERVER`S OXYGEN MASK IAW AMM 35-11-12 & OPS TESTED GOOD IAW 35-10-00-710-802.
- [SDR REXA2017101001074](https://openairdocs.org/sdr/REXA2017101001074.md): G Switch · failed · Oct 10, 2017 · N8969A · Cndair CL6002B19 · Emergency Locator Beacon
  > G-SWITCH TEST FOR ELT, FAILED TO OPERATE. REMOVED AND REPLACED ELT ASSY IAW AMM 25-62-01-400-801. ELT RAMP TESTED GOOD.
- [SDR REXA2017070700773](https://openairdocs.org/sdr/REXA2017070700773.md): Tube · broken · Jul 7, 2017 · N8969A · Cndair CL6002B19 · Crew Oxygen System
  > FIRST OFFICER`S OXYGEN MASK TUBING IS BROKEN. REMOVED AND REPLACED OXYGEN MASK IAW AMM 35-11-12. OPS CHECKED GOOD.
- [SDR REXA2017021600245](https://openairdocs.org/sdr/REXA2017021600245.md): Battery Pack · discharged · Feb 16, 2017 · N8969A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT TURN ON. TRIED FROM FLIGHT DECK AND FA STATION. CHARGED THE BATTERY PACKS, AND OPS CHECKED GOOD IAW AMM 33-51-00.
- [SDR REXA2016090801817](https://openairdocs.org/sdr/REXA2016090801817.md): Bpsu · inoperative · Sep 8, 2016 · N8969A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MESSAGE ON CLIMB THROUGH 11000 FT. NO CONFIG OR POWER CHANGES AT THAT TIME. FLAPS FAILED AT ZERO WITH LEVER AT ZERO. PERFORMED WIRING AND MEG CHECKS OF LT BPSU HARNESS TO FECU. ALL CHECKS GOOD. REMOVED RT BPSU AND INSTALLED ON LT SIDE. INS
- [SDR REXA2016072601815](https://openairdocs.org/sdr/REXA2016072601815.md): Bpsu · inoperative · Jul 26, 2016 · N8969A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED CAUTION CAME ON AT FL 260, 290 KNOTS. FLAPS ZERO NO FLAP HANDLE MOVEMENT. REMAINED ON LANDED AT 200 FT/MIN. PERFORMED TROUBLESHOOTING IAW FIM 27-50-00 REV 51 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AMOC LOG 16-26 DATED 05-27-20 16, AND TS 001100
- [SDR REXA2016062201146](https://openairdocs.org/sdr/REXA2016062201146.md): Oxygen Mask · failed · Jun 22, 2016 · N8969A · Cndair CL6002B19 · Crew Oxygen System
  > OBSERVERS MASK FAILS TO TEST, DEFERRING OBSERVERS O2 MASK IAW MEL 35-10-01, MM02 UPDATED. PLACARD INSTALLED. MAINTENANCE NOTIFIED. R & R OBSERVERS OXYGEN MASK IAW AMM 35-11-12. OPS/CHECKS GOOD. REMOVED PLACARD, CLEARED, FROM MM02.
- [SDR REXA2016031300410](https://openairdocs.org/sdr/REXA2016031300410.md): Light · inoperative · Mar 13, 2016 · N8969A · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT ATTENDANT REPORTS EMER SIGN LIGHT BULB BURNT OUT BY ROW 8 C & D. OK TO DEFER IAW MEL 33-51-16 CAT C MM02 ENTRY, PLACARD MOC 96211 NOTIFIED. R & R BULBS IN EMER SIGN AT 8 C & D IAW AMM 33-51-10. OPERATIONS CHECKED GOOD MMO2 UPDATED, PLACARD REMOVED,
- [SDR REXA2016021200200](https://openairdocs.org/sdr/REXA2016021200200.md): Door Sill · corroded · Feb 12, 2016 · N8969A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT SILL FS 559.0+112 - 621.0 HAS CORROSION. R & R LT FLOOR SILL FS 559+112 - 621 IAW SRM 51-42-06 & SRM 51-42-20.
- [SDR REXA2016021100198](https://openairdocs.org/sdr/REXA2016021100198.md): Bulkhead · cracked · Feb 11, 2016 · N8969A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESS BULKHEAD CRACKED AT LINTEL FITTING. REPAIRED IAW REO 601R-53-61-1230. REQUIRES DETAILED VISUAL INSPECTION IAW NDTM 51-20-09 PART 1. THRESHOLD 18160 FLIGHT CYCLES REPEAT INSPECTION 6215 FLIGHT CYCLES DUE AT 39435 FLIGHT CYCLES. NO FURTHER ACTION A
- [SDR REXA2016021000197](https://openairdocs.org/sdr/REXA2016021000197.md): Door · chafed · Feb 10, 2016 · N8969A · Cndair CL6002B19 · Landing Gear Doors
  > MIDDLE LE OF LT MLG DOOR IS CHAFED. REPAIRED LT MLG DOOR LE IAW REO 601R-52-82-102.
- [SDR REXA2016021000196](https://openairdocs.org/sdr/REXA2016021000196.md): Door · chafed · Feb 10, 2016 · N8969A · Cndair CL6002B19 · Landing Gear Doors
  > LOWER LE OF LT MLG DOOR IS CHAFED. REPAIRED LT MLG DOOR LE IAW REO 601R-52-82-016.
- [SDR REXA2016021000195](https://openairdocs.org/sdr/REXA2016021000195.md): Door · chafed · Feb 10, 2016 · N8969A · Cndair CL6002B19 · Landing Gear Doors
  > LOWER LE OF RT MLG DOOR IS CHAFED. REPAIRED RT MLG DOOR LE IAW REO 601R-52-82-016.
- [SDR REXA2016021000194](https://openairdocs.org/sdr/REXA2016021000194.md): Door · chafed · Feb 10, 2016 · N8969A · Cndair CL6002B19 · Landing Gear Doors
  > LOWER TE OF RT MLG DOOR IS CHAFED. REPAIRED LOWER TE OF RT MLG IAW REO 601R-52-82-407.
- [SDR REXA2016021000193](https://openairdocs.org/sdr/REXA2016021000193.md): Seal · cracked · Feb 10, 2016 · N8969A · Cndair CL6002B19 · Engine Thrust Reverser
  > LOWER EDGE OF LOWER FWD OTBD SEAL ON NR 1 ENG THRUST REVERSER TORQUE BOX IS CRACKED. R & R LOWER EDGE SEAL IAW CMM 78-30-00.
- [SDR REXA2016021000191](https://openairdocs.org/sdr/REXA2016021000191.md): Fitting · broken · Feb 10, 2016 · N8969A · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 2 ENG HAS A BROKEN ANGLE ON REAR OF FRONT FRAME, LOWER INBD SIDE. R & R UNSERVICEABLE FITTING WITH SERVICEABLE FITTING IAW CMM 20-42-14.

Next page: https://openairdocs.org/aircraft/N8969A/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 = 'N8969A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8969A/reports

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