# Service difficulty reports: N8960A

A list on [N8960A](https://openairdocs.org/aircraft/N8960A.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 2 · 71 reports

- [SDR REXA2017111301163](https://openairdocs.org/sdr/REXA2017111301163.md): Trim System · disengaged · Nov 13, 2017 · N8960A · Cndair CL6002B19 · Stabilizer Control System
  > STAB TRIM AND MACH TRIM CAUTION MESSAGE, DISENGAED AFTER TAKEOFF RESELECTED STAB TRIM & MACH TRIM BUT DISCONNECTED AGAIN. AUTO PILOT WAS NOT ABLE TO LEVEL THE AIRCRAFT AT 10'000 FT AND VIOLENTLEY DISENGAGED. RAN QRH FOR STAB & MACH TRIM. WERE ABLE TO RE-ENGA
- [SDR REXA2017091601016](https://openairdocs.org/sdr/REXA2017091601016.md): Battery · discharged · Sep 16, 2017 · N8960A · Cndair CL6002B19 · Emergency Equipment
  > FWD FA FLASHLIGHT BATTERY DISCHARGED. REPLACED THE BATTERY.
- [SDR REXA2016111402218](https://openairdocs.org/sdr/REXA2016111402218.md): Oxygen Mask · ruptured · Nov 14, 2016 · N8960A · Cndair CL6002B19 · Crew Oxygen System
  > FO O2 MASK HARNESS RUPTURED DURING TESTING. REMOVED AND REPLACED FO'S OXYGEN MASK IAW AMM 35-11-12. OPS CHECK GOOD.
- [SDR REXA2016060700975](https://openairdocs.org/sdr/REXA2016060700975.md): Oxygen Mask · defective · Jun 7, 2016 · N8960A · Cndair CL6002B19 · Crew Oxygen System
  > OBSERVER O2 MASK IS NOT TESTING CORRECTLY WHEN THE PRESS O2 TO TEST & RESET IS PUSHED. THE O2 DOES NOT STOP FLOWING IT NOT IN THE EMER SETTING. R & R OBSERVERS 02 MASK IAW AMM 35-11-12. OPERATIONS CHECKED GOOD.
- [SDR REXA2016020900134](https://openairdocs.org/sdr/REXA2016020900134.md): Flashlight · inoperative · Feb 9, 2016 · N8960A · Cndair CL6002B19 · Emergency Equipment
  > 1ST OFFICER'S EMER FLASHLIGHT IS INOPERATIVE. R & R 1ST OFFICERS EMER FLASHLIGHT IAW AMM 25-61-02.
- [SDR REXA2016012000050](https://openairdocs.org/sdr/REXA2016012000050.md): Frame · corroded · Jan 20, 2016 · N8960A · Cndair CL6002B19 · Fuselage Main, Frame
  > AFT FUSELAGE BELOW FLOOR FRAME AT FS 605, BETWEEN STRINGERS 24LT & 24RT IS CORRODED. REMOVED CORROSION WITH A LOSS OF.008 WITH.042 REMAINING & IS OUT OF LIMITS IAW SRM 5300-00. REPAIRED FRAME IAW EA NR 253-03910.
- [SDR REXA2016011800058](https://openairdocs.org/sdr/REXA2016011800058.md): Drag Angle · cracked · Jan 18, 2016 · N8960A · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT DRAG ANGLE CRACKED. REMOVED & REINSTALLED NEW AFT DRAG ANGLE IAW REO 601R-52-11-082.
- [SDR REXA2016011800047](https://openairdocs.org/sdr/REXA2016011800047.md): Oxygen Mask · malfunctioned · Jan 18, 2016 · N8960A · Cndair CL6002B19 · Passenger Oxygen System
  > FLIGHT ATTENDANT OXYGEN MASKS FAILED TO DEPLOY DURING OPERATIONAL CHECK. R & R FLIGHT ATTENDANT OXYGEN MASK CATCH MECHANISM IAW AMM 35-21-05-020-803 STEP 3A. OPERATIONS CHECK OF FLIGHT ATTENDANT OXYGEN MASK GOOD IAW AMM 35-20-00-710-803. OPERATIONS CHECKED
- [SDR REXA2016011600059](https://openairdocs.org/sdr/REXA2016011600059.md): Support Fitting · cracked · Jan 16, 2016 · N8960A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL SUPPORT CLIP CRACKED AT FS 621 BH, STRINGER 12L. REMOVED INTERCOSTAL SUPPORT CLIP AT FS 621, STRINGER 12L IAW SRM 51-42-06. REPLACED WITH NEW SUPPORT CLIP IAW SRM 51-42-06.
- [SDR REXA2016011500046](https://openairdocs.org/sdr/REXA2016011500046.md): Glowstrip · debonded · Jan 15, 2016 · N8960A · Cndair CL6002B19 · Emergency Equipment
  > ALL PHOTO LUMINESCENT EMER FLOOR LIGHTS STAINED & DISBONDED. R & R ALL PHOTO LUMINESCENT EMER FLOOR LIGHTS ON PANEL RACK.
- [SDR REXA2016011400057](https://openairdocs.org/sdr/REXA2016011400057.md): Angle · cracked · Jan 14, 2016 · N8960A · Cndair CL6002B19 · Engine Cowling System
  > NUMBER 1 ENG INLET NOSE COWL, CRACKED SPRING ANGLE AT 6 O'CLOCK POSITION AFT OF PDU. R & R DAMAGED SPRING ANGLE ON NR 1 ENG INLET NOSE COWL AT 6 O'CLOCK POSITION IAW CMM 20-42-13.
- [SDR REXA2016011300056](https://openairdocs.org/sdr/REXA2016011300056.md): Bracket · cracked · Jan 13, 2016 · N8960A · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RIGHT WING REFUEL DEFUEL BRACKET IS CRACKED. REMOVED CRACK, FOUND IT TO BE WITHIN LIMITS IAW SRM 57-00-00.
- [SDR REXA2016011300048](https://openairdocs.org/sdr/REXA2016011300048.md): Angle · cracked · Jan 13, 2016 · N8960A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT OBLIQUE ANGLE AT FS 621 BH STRINGER 13L CRACKED. R & R LT OBLIQUE ANGLE AT FS 621 BH. STRINGER 13L IAW SRM 51-42-21. "
- [SDR REXA2016011300045](https://openairdocs.org/sdr/REXA2016011300045.md): Support Fitting · cracked · Jan 13, 2016 · N8960A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL SUPPORT CLIP CRACKED AT FS 621 BH, STRINGER 13L. R & R CRACKED INTERCOSTAL SUPPORT CLIP WITH A SERVICEABLE INTERCOSTAL SUPPORT CLIP IAW SRM 51-42-21.
- [SDR REXA2016011000060](https://openairdocs.org/sdr/REXA2016011000060.md): Floor Support · corroded · Jan 10, 2016 · N8960A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOORBEAM HAS CORROSION AT FASTENER HOLES STATION 574 - 621, LBL 27. R & R FLOORBEAM UPPER CAP FROM FS 574 - 621, LBL 27 IAW SRM 51-42-20 & REO 601R-53-61-3778.
- [SDR REXA2016011000055](https://openairdocs.org/sdr/REXA2016011000055.md): Handle · cracked · Jan 10, 2016 · N8960A · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INNER HANDLE CRACKED. R & R PAX DOOR INNER HANDLE IAW SRM 51-42-02.
- [SDR REXA2016011000049](https://openairdocs.org/sdr/REXA2016011000049.md): Door Sill · corroded · Jan 10, 2016 · N8960A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR STRUCTURE AT PAX DOOR OPENING, HAS CORROSION AT THE LOWER ANGLE, BETWEEN FS 310 & FS 349. R & R SILL PAX DOOR IAW SRM 51-42-21 & 51-42-06.
- [SDR REXA2016010800054](https://openairdocs.org/sdr/REXA2016010800054.md): Fitting · cracked · Jan 8, 2016 · N8960A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT WINDSHIELD SIDE POST, LOWER AFT FITTING CRACKED. R & R RT WINDSHIELD SIDE POST FITTING IAW SRM 51-42-21.
- [SDR REXA2016010800053](https://openairdocs.org/sdr/REXA2016010800053.md): Fitting · cracked · Jan 8, 2016 · N8960A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT WINDSHIELD SIDE POST, LOWER AFT FITTING CRACKED. R & R LT WINDSHIELD SIDE POST FITTING IAW SRM 51-42-21.
- [SDR REXA2016010600052](https://openairdocs.org/sdr/REXA2016010600052.md): Strap · corroded · Jan 6, 2016 · N8960A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR STRAP HAS CORROSION AT FS 559, BETWEEN RBL 27 & THE RT FLOOR SILL IN CABIN. REMOVED CORROSION WITH A LOSS OF.006 & WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-41-45. FABRICATED & INSTALLED NEW FLOOR STRAP IAW SRM 51-42-06.
- [SDR REXA2016010500051](https://openairdocs.org/sdr/REXA2016010500051.md): Door Sill · cracked · Jan 5, 2016 · N8960A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING CORROSION REMOVAL A CRACK WAS NOTED WHILE PERFORMING NDT ON THE AFT CARGO LOWER DOOR SILL AT FS 589. REPAIRED CRACK ON AFT CARGO LOWER DOOR SILL AT FS.589 IAW EO 601R-53-61-433.
- [SDR REXA2015120701174](https://openairdocs.org/sdr/REXA2015120701174.md): Flashlight · inoperative · Dec 7, 2015 · N8960A · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT ATTENDANT FLASHLIGHT IS OUT OF CASE & DEAD. R & R FLIGHT ATTENDANTS FLASHLIGHT IAW AMM 25-61-04.
- [SDR REXA2015120301168](https://openairdocs.org/sdr/REXA2015120301168.md): Landing Gear · defective · Dec 3, 2015 · N8960A · Cndair CL6002B19 · Nose/Tail Landing Gear
  > AFT TAKEOFF, WHEN LG CYCLED UP, WE RECEIVED NOSE DOOR OPEN, GEAR DISAGREE WARNING MSG. DASHED IN LT & RT GEAR & ON INDICATION IN CTR, ALSO RECEIVED STEERING INOPERATIVE. WOW INPUT & WOW INPUT FAILED CAUTION MSG. RAN QRH, WARNING MSG WENT AWAY, WOW INPUT REM
- [SDR REXA2015120101162](https://openairdocs.org/sdr/REXA2015120101162.md): Wire Harness · defective · Dec 1, 2015 · N8960A · Cndair CL6002B19 · Landing Gear System Wiring
  > AFTER TAKEOFF, WHEN LG CYCLED UP, WE GOT NOSE DOOR OPEN, GEAR DISAGREE, STEERING INOPERATIVE, WOW INPUT & WOW INPUT FAIL. RAN QRH & GOT THE GEAR DOWN & LOCKED. WOW INPUT & WOW INPUT FAIL LIGHTS REMAINED ON. LANDED NORMALLY. IAW MOTR GROUP REPLACE NLG WOW N
- [SDR REXA2015052500523](https://openairdocs.org/sdr/REXA2015052500523.md): Seal · leaking · May 25, 2015 · N8960A · Cndair CL6002B19 · Emergency Exits
  > CREW ESCAPE HATCH LEAKING. R & R CREW ESCAPE HATCH SEAL IAW AMM 55-22-07. OPERATIONS & LEAK CHECK GOOD, PN ON & OFF CC670-38022-1.
- [SDR REXA2015040700381](https://openairdocs.org/sdr/REXA2015040700381.md): Bracket · damaged · Apr 7, 2015 · N8960A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE AFTER ROTATION, NOSE GEAR WOULD NOT RETRACT FOR 20 SECONDS, SPEED APPROX 160 KTS. GEAR SELECTED DOWN, 3 GREEN LANDED WITHOUT INCIDENT. R & R CENTERING SWITCH BRACKET & WOW NR 2 CENTERING HARNESS IAW AMM 32-61-25. PERFORMED EXTENSION & RETRACTI
- [SDR REXA2014122101226](https://openairdocs.org/sdr/REXA2014122101226.md): Warning System · false activation · Dec 21, 2014 · N8960A · Cndair CL6002B19 · Landing Gear Position and Warning
  > DURING DEPARTURE, AS GEAR WENT UP RECEIVED A TRIPLE CHIME GEAR DISAGREE NOSE WHEEL WARNINGS. PERFORMED QRH UPON SELECTING HYD 2B PUMP ON GEAR RETRACTED. CYCLED TWICE OK. LANDED WITHOUT PROBLEMS TROUBLESHOT IAW FIM 32-60-07, NLG HARNESS 31-61-25. OPS CHECK
- [SDR REXA2014121901197](https://openairdocs.org/sdr/REXA2014121901197.md): Battery · discharged · Dec 19, 2014 · N8960A · Cndair CL6002B19 · Emergency Equipment
  > FIRST OFFICER`S EMER FLASHLIGHT INOPERATIVE. R & R THE FIRST OFFICER`S EMER FLASHLIGHT BATTERY IAW AMM 25-61-02. NO DEFECTS NOTED. ACFT OK FOR SERVICE.
- [SDR REXA2014101300896](https://openairdocs.org/sdr/REXA2014101300896.md): Skin · dented · Oct 7, 2014 · N8960A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT IN THE FUSELAGE SKIN AT FS 598 AT THE SKIN SPLICE AT STRINGER 20L. THE DENT MEASURES 1 INCH X 0.63 INCH X 0.017 INCHES DEEP. REPAIRED IAW EA CRJ253-02971.
- [SDR REXA2014092200982](https://openairdocs.org/sdr/REXA2014092200982.md): Apu · malfunctioned · Sep 22, 2014 · N8960A · Cndair CL6002B19 · APU Core Engine
  > DURING TAXI AFTER STARTING THE NR 1 ENG THE FIRST OFFICER NOTICED THAT THE APU TEMP SPIKED. TURNED THE APU BLEED OFF & ENG BLEEDS ON. ACFT FILLED WITH SMOKE AT THAT TIME PAX & CREW EVACUATED ACFT. PERFORMED OPERATIONAL CHECKS OF THE APU & LT & RT ENG BLEED
- [SDR REXA2014091600788](https://openairdocs.org/sdr/REXA2014091600788.md): Spar · out of alignment · Sep 7, 2014 · N8960A · Cndair CL6002B19 · Wing, Plate/Skin
  > FOUND 7 FASTENER HOLES COMMON TO THE WINGLET SPAR & SPAR FITTINGS DID NOT PROPERLY ALIGN. REPAIRED IAW EA CRJ257-02898.
- [SDR REXA2014082200840](https://openairdocs.org/sdr/REXA2014082200840.md): Battery Pack · discharged · Aug 22, 2014 · N8960A · Cndair CL6002B19 · Emergency Lighting
  > AFT FACING EXIT SIGN & EXTERIOR EMER LIGHTS WHERE NOT WORKING. R & R NR 3 EMER BATTERY PACK IAW AMM 33-51-04. OK FOR SERVICE.
- [SDR REXA2014060100543](https://openairdocs.org/sdr/REXA2014060100543.md): Battery · discharged · Jun 1, 2014 · N8960A · Cndair CL6002B19 · Emergency Lighting
  > THE FRONT CEILING EMER FLOODLIGHT TURNS ON & FADES TO BLACK AFTER 5 - 10 SECONDS WHEN THE EMERGENCY LIGHTS ARE TURNED ON. DEFERRED OVERHEAD EMER LIGHT IAW MEL 33-51-11. R & R EMER LIGHT BATTERY NR 1 IAW AMM 33-51-04.
- [SDR REXA2014020300166](https://openairdocs.org/sdr/REXA2014020300166.md): Flap · obstructed · Feb 3, 2014 · N8960A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MSG AT GATE. FLIGHT CONTROL SYNOPTIC PAGE SHOWS LT FLAP AT 0 DEGREES & RT FLAP AT 2 DEGREES. PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC DATED JULY 22, 2013 & PA AD 27-052N. CLEANED ICE & SLUSH AWAY FRO
- [SDR REXA2014012400138](https://openairdocs.org/sdr/REXA2014012400138.md): Life Vest · unserviceable · Jan 24, 2014 · N8960A · Cndair CL6002B19 · Life Jacket
  > ONE INFANT LIFE VEST HAS TEAR IN BAG. R & R ONE INFANT LIFE VEST IAW PA 25-096A.
- [SDR REXA2014010400004](https://openairdocs.org/sdr/REXA2014010400004.md): Skin · damaged · Jan 1, 2014 · N8960A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT FS 580.00 BELOW STRINGER 24L HAS LIGHTNING DAMAGE. THE DAMAGE WAS REMOVED BY BLENDING RESULTING IN A BLEND OUT MEASURING 3 INCHES X 1.70 INCHES, ” X 0.017 INCHES DEEP. REPAIRED IAW EA CRJ253-02227.
- [SDR REXA2014010400003](https://openairdocs.org/sdr/REXA2014010400003.md): Skin · damaged · Jan 1, 2014 · N8960A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MAINTENANCE FOUND THE FUSELAGE SKIN AT FS 605, 609, AND 615 JUST BELOW S24L TO HAVE LIGHTNING DAMAGE. REPAIRED IAW EA CRJ253-02226.
- [SDR REXA2014010400002](https://openairdocs.org/sdr/REXA2014010400002.md): Skin · damaged · Jan 1, 2014 · N8960A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MAINTENANCE FOUND THE FUSELAGE SKIN AT FS 640 AND S25L TO HAVE LIGHTNING DAMAGE. REPAIRED IAW EA CRJ253-02225.
- [SDR REXA2014010400001](https://openairdocs.org/sdr/REXA2014010400001.md): Skin · damaged · Jan 1, 2014 · N8960A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MAINTENANCE FOUND A LIGHTNING BURN TO THE LEFT FUSELAGE AT FS 700.00 AT S22L. REPAIRED IAW EA CRJ253-02224.
- [SDR REXA2012122801831](https://openairdocs.org/sdr/REXA2012122801831.md): Battery · discharged · Dec 28, 2012 · N8960A · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT ATTENDANT REPORTS EMERGENCY LIGHTS ACTIVATED AFTER LANDING. CANNOT TURN THEM OFF FROM THE FLIGHT DECK. REPLACED NR 1 EMERGENCY BATTERY AND EMERGENCY BATTERY CHARGER IAW CRJ200 AMM 33-51-00. OPS CHECKS GOOD. OK FOR SERVICE.
- [SDR REXA2012092401367](https://openairdocs.org/sdr/REXA2012092401367.md): Seal · broken · Sep 24, 2012 · N8960A · Cndair CL6002B19 · Emergency Equipment
  > GREEN SEAL ON MEDICAL KIT IS BROKEN. REPLACED GREEN SEAL ON EMK AS REQUIRED. OK FOR SERVICE.
- [SDR REXA2012081701277](https://openairdocs.org/sdr/REXA2012081701277.md): Pump · malfunctioned · Aug 17, 2012 · N8960A · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > FLIGHT 4145, RECEIVED GEAR DISAGREE ON GEAR EXTENSION. QRH COMPLETED FOR GEAR UP DISAGREE AND HYD 3 LOW PRESSURE CAUTION GEAR EXTENDED AND LOCKED WITH MANUAL EXTENSION. HYD 3 SHOWED LESS THAT 5 PERCENT FLUID AND ZERO PRESSURE. EMERGENCY DECLARED AND COMPLE
- [SDR REXA2012080401078](https://openairdocs.org/sdr/REXA2012080401078.md): Angle · damaged · Jul 31, 2012 · N8960A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING THE ACCOMPLISHMENT OF GREO 601R-53-61-1230, IT WAS NOTED THAT THE LEFT LOWER CAP ANGLE AT APPROXIMATE BS 621, WL 106 HAS DRILL START DAMAGE. REPAIRED IAW REO 601R-53-61-4596.
- [SDR REXA2012073101215](https://openairdocs.org/sdr/REXA2012073101215.md): Bulb · inoperative · Jul 31, 2012 · N8960A · Cndair CL6002B19 · Emergency Lighting
  > RIGHT NR 1 EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR REXA2012101601115](https://openairdocs.org/sdr/REXA2012101601115.md): Bulkhead · cracked · Jul 22, 2012 · N8960A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 PRESSURE BULKHEAD CRACKED AT LEFT LINTEL FITTING. REPAIRED IAW BOMBARDIER REO 601R-5361-1230.
- [SDR REXA2012081501085](https://openairdocs.org/sdr/REXA2012081501085.md): Bearing · worn · Jul 15, 2012 · N8960A · Cndair CL6002B19 · Elevator Structure
  > LEFT ELEVATOR INBOARD HINGE BEARING WORN. REPAIRED IAW SRM 51-42-21/51-42-06.
- [SDR REXA201201501086](https://openairdocs.org/sdr/REXA201201501086.md): Angle · cracked · Jul 14, 2012 · N8960A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK IN FS 559 CAP ANGLES RBL 9, RBL18, AND LBL18. REPAIRED IAW REO 601R-53-41-206 AND REO 601R-53-41-609.
- [SDR REXA2012050200601](https://openairdocs.org/sdr/REXA2012050200601.md): Light · out of position · May 2, 2012 · N8960A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT LIGHT IN ROW 1 A+B CAME OFF THE BULKHEAD. LIGHT STILL WORKS. REMOVED AND REPLACED EMERGENCY LT IAW CRJ200 AMM 33-51-13 VERIFIED PARTS EFFECTIVITY.
- [SDR REXA2012042800586](https://openairdocs.org/sdr/REXA2012042800586.md): Battery · discharged · Apr 28, 2012 · N8960A · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT INOP. REMOVED AND REPLACED F/A FLASHLIGHT BATTERY IAW AMM 25-61-00. CHECKS GOOD. OK FOR SERVICE.
- [SDR REXA2012040800479](https://openairdocs.org/sdr/REXA2012040800479.md): Battery · inoperative · Apr 8, 2012 · N8960A · Cndair CL6002B19 · Emergency Lighting
  > NR 4 EMERGENCY LIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY IAW AMM 33-51-04 OPS CHECKED GOOD.

Next page: https://openairdocs.org/aircraft/N8960A/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 = 'N8960A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8960A/reports

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