# Service difficulty reports: N8907A, cancelled Feb 24, 2023

A list on [N8907A, cancelled Feb 24, 2023](https://openairdocs.org/deregistered/N8907A-2023-02-24.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 · 69 reports

- [SDR REXA2017111401174](https://openairdocs.org/sdr/REXA2017111401174.md): Wire · broken · Nov 14, 2017 · N8907A · Cndair CL6002B19 · Light System Wiring
  > PAX DOOR EMERGENCY EXIT SIGN INOPERATIVE. FOUND A BROKEN WIRE. REPAIRED THE WIRE IAW ESPM 20-16-00. OPS TESTED GOOD.
- [SDR REXA2017101501099](https://openairdocs.org/sdr/REXA2017101501099.md): Element · malfunctioned · Oct 15, 2017 · N8907A · Cndair CL6002B19 · Pneumatic Indicating System
  > RT 14TH STAGE DUCT WARNING MESSAGE WITH AURAL AND CHIME WARNINGS. COMPLIED WITH QRH BY CLOSING THE 14TH STAGE SOV AND SELECTING 14TH STAGE ISOLATION VALVE TO OPEN. WARNING CLEARED PRIOR TO 40 SECONDS. WARNING REAPPERED WITHIN 2 MINUTES LATER, WITH THE RT 1
- [SDR REXA2017083000950](https://openairdocs.org/sdr/REXA2017083000950.md): Wheel · inoperative · Aug 30, 2017 · N8907A · Cndair CL6002B19 · Wheel/Ski/Float
  > ABORTED TAKEOFF, DUE TO UNABLE TO MAINTAIN DIRECTIONAL CONTROL. ABORTED AT LESS THAN 60 KTS NOSE WHEEL NEVER LEFT THE GROUND. CHECKED LT & RT NWS IAW AMM 32-51-20.FOUND LT RVDT AT - 1.788, RT RVDT +1.788 WITHIN AMM LIMITS. NLG WHEEL ASSY LT & RT REMOVED AND
- [SDR REXA2017040500429](https://openairdocs.org/sdr/REXA2017040500429.md): Connector · not seated · Apr 5, 2017 · N8907A · Cndair CL6002B19 · Light System Wiring
  > CABIN EMERGENCY LIGHTS ROWS 9 CD - 12 CD INOPERATIVE. SEATED THE CONNECTOR IAW AMM 33-51-01. OPS CHECKED GOOD.
- [SDR REXA2016090301676](https://openairdocs.org/sdr/REXA2016090301676.md): Pump · malfunctioned · Sep 3, 2016 · N8907A · Cndair CL6002B19 · Engine Fuel Pump
  > LEFT ENGINE ROLLED BACK TO IDLE AT 1000 FT. N1 & ITT NORMAL FOR IDLE N2 70% ACCOMPLISHED QRH ENGINE SHUTDOWN. R & R THE ENGINE FUEL PUMP IAW AMM 73-11-01, R & R THE ENGINE MAIN FUEL CONTROLLER IAW AMM 73-21-01. OPS CHECKED GOOD IAW AMM 71-00-00
- [SDR REXA2016061001011](https://openairdocs.org/sdr/REXA2016061001011.md): Cap · broken · Jun 10, 2016 · N8907A · Cndair CL6002B19 · Emergency Lighting
  > AT SEAT 12D CONNECTION FOR FLOOR TRACK EMERGENCY LIGHTING BROKEN. R & R THE EMERGENCY FLOOR LIGHT END CAP, P40LY, IAW AMM 33-51-01, OPS CHECK GOOD.
- [SDR REXA2016052800956](https://openairdocs.org/sdr/REXA2016052800956.md): Cover · unsecure · May 28, 2016 · N8907A · Cndair CL6002B19 · Emergency Lighting
  > PLASTIC COVER OVER FLOOR EMERGENCY LIGHT NEAR 1CD, 2CD & 3CD ARE LOOSE & COMING UP. SECURED PLASTIC COVER AS REQUIRED.
- [SDR REXA2016051900843](https://openairdocs.org/sdr/REXA2016051900843.md): Cover · unsecure · May 19, 2016 · N8907A · Cndair CL6002B19 · Emergency Lighting
  > RIGHT REAR FLOOR COVERING FOR EMER LIGHTS CAME OFF. SECURED EMER LIGHT FLOOR COVER IAW AMM 33-51-01. OK FOR SERVICE.
- [SDR REXA2016051600787](https://openairdocs.org/sdr/REXA2016051600787.md): Cover · loose · May 16, 2016 · N8907A · Cndair CL6002B19 · Emergency Lighting
  > FLOOR EMER LIGHT STRIP LOOSE. REINSTALLED PLASTIC COVER ON EMER FLOOR TRACK LIGHTING.
- [SDR REXA2016050900711](https://openairdocs.org/sdr/REXA2016050900711.md): Cover · loose · May 9, 2016 · N8907A · Cndair CL6002B19 · Emergency Lighting
  > PLASTIC COVER OVER FLOOR EMER LIGHTING STRIP LOOSE NEXT TO FIRST TWO ROWS ON FIRST OFFICERS SIDE OF PLANE. SECURED EMER LIGHTING STRIP AS REQUIRED.
- [SDR REXA2016042600657](https://openairdocs.org/sdr/REXA2016042600657.md): Pbe · unserviceable · Apr 26, 2016 · N8907A · Cndair CL6002B19 · Emergency Equipment
  > COCKPIT PBE BAG TORN. REPLACED COCKPIT PBE AS REQUIRED IAW AMM 35-30-00 & SUBTASK 35-30-00-941-007, PN ON & OFF MR-10047N.
- [SDR REXA2016021000149](https://openairdocs.org/sdr/REXA2016021000149.md): Flashlight · inoperative · Feb 10, 2016 · N8907A · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT ATTENDANT EMER FLASHLIGHT INOPERATIVE. OPENED DEFERRAL IAW MEL 25-61-04. ENTERED IN MM02 & PLACARD INSTALLED, OK FOR SERVICE. TEMP FLASHLIGHT PROVIDED IAW MEL & MOC 96211. REPLACED FLASHLIGHT ASSEMBLY WITH A SERVICEABLE FLASHLIGHT ASSEMBLY IAW CMM 2
- [SDR REXA2016020400146](https://openairdocs.org/sdr/REXA2016020400146.md): Cowling · chafed · Feb 4, 2016 · N8907A · Cndair CL6002B19 · Engine Cowling System
  > OUTBOARD LE OF COWL 445AT, NEAR LATCH IS CHAFED. REPAIRED CHAFE IAW CMM 71-12-01 REPAIR SRS104.
- [SDR REXA2016020300145](https://openairdocs.org/sdr/REXA2016020300145.md): Post · cracked · Feb 3, 2016 · N8907A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT LOWER FITTING ON WINDSHIELD CENTER POST, AT FS 202.75 IS CRACKED. REMOVED LT LOWER FITTING & REPLACED WITH NEW FITTING IAW SRM 51-42-20.
- [SDR REXA2016020200144](https://openairdocs.org/sdr/REXA2016020200144.md): Support Angle · broken · Feb 2, 2016 · N8907A · Cndair CL6002B19 · Engine Thrust Reverser
  > RIGHT UPPER THRUST REVERSER TRACK STAND FAIRING, SUPPORT Z ANGLE BROKEN. R & R SUPPORT Z ANGLE IAW MM 20-42-06.
- [SDR REXA2016012900148](https://openairdocs.org/sdr/REXA2016012900148.md): Bracket · cracked · Jan 29, 2016 · N8907A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > IN RIGHT WW THE BRAKE PRESS TRANSDUCER BRACKET IS CRACKED. R & R BRAKE PRESS TRANSDUCER BRACKET IN RT MLG WW IAW SRM 51-42-22 & SRM 51-41-02.
- [SDR REXA2016012600142](https://openairdocs.org/sdr/REXA2016012600142.md): Attach Angle · cracked · Jan 26, 2016 · N8907A · Cndair CL6002B19 · Wing, Attach Fittings
  > LEFT WING INBD LE FUEL MANIFOLD, ATTACH ANGLE CRACKED AT OTBD LOWER RADIUS. REMOVED CRACK BY EDGE BLENDING IAW SRM 57-00-00.
- [SDR REXA2016012500143](https://openairdocs.org/sdr/REXA2016012500143.md): Skin · chafed · Jan 25, 2016 · N8907A · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING INBD FLAP VANE LE IS CHAFED IN 3 AREAS. REMOVED & INSTALLED 3 EA LE SKINS IAW SRM 51-42-11.
- [SDR REXA2016012300139](https://openairdocs.org/sdr/REXA2016012300139.md): Drag Angle · cracked · Jan 23, 2016 · N8907A · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT DRAG ANGLE CRACKED. REMOVED DAMAGED AREA, FABRICATED, LOCATED & INSTALLED REPAIR PARTS IAW REO 601R-52-11-513 REV B. RESTORED TO ORIGINAL FINISH.
- [SDR REXA2016012100140](https://openairdocs.org/sdr/REXA2016012100140.md): Plate · cracked · Jan 21, 2016 · N8907A · Cndair CL6002B19 · Trailing Edge Flaps
  > INBOARD FLAP LE PANEL 684JB, MOUNTING PLATE CRACKED. FABRICATED 2 EACH INBD FLAP LE PANEL 684JB MOUNTING PLATES IAW SRM 51-40-11.
- [SDR REXA2016012000138](https://openairdocs.org/sdr/REXA2016012000138.md): Drag Angle · cracked · Jan 20, 2016 · N8907A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT WW DRAG ANGLE ADJACENT TO BATT RIB CRACKED. REMOVED RT WW DRAG ANGLE & INSTALLED NEW DRAG ANGLE IAW SRM 51-42-21.
- [SDR REXA2016011900141](https://openairdocs.org/sdr/REXA2016011900141.md): Angle · cracked · Jan 19, 2016 · N8907A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT ACCESSORY COMPARTMENT, AFT BULKHEAD, OTBD LBL 36, ANGLE IS CRACKED. R & R CRACKED ANGLE WITH A SERVICEABLE FABRICATED REPAIR ANGLE IAW SRM 51-42-21.
- [SDR REXA2016011900135](https://openairdocs.org/sdr/REXA2016011900135.md): Fitting · corroded · Jan 19, 2016 · N8907A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BATHTUB FITTING AT FS 461.0 & OTBD OF RBL 9 IS CRACKED. REMOVED FITTING, LOCATED & INSTALLED NEW FITTING IAW SRM 51-40-11, 51-42-06 & 53-41-43.
- [SDR REXA2016011800137](https://openairdocs.org/sdr/REXA2016011800137.md): Fitting · cracked · Jan 18, 2016 · N8907A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP UNDER CARGO DOOR SILL AT FS 589.00 IS CRACKED. REMOVED CLIP UNDER CARGO DOOR SILL & REPLACED WITH NEW CLIP IAW SRM 51-42-20.
- [SDR REXA2016011800136](https://openairdocs.org/sdr/REXA2016011800136.md): Seat Track · corroded · Jan 18, 2016 · N8907A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL BEAM, LBL 27, OTBD FLANGE, FS 574.00 TO FS 608.00, IS CORRODED AT FASTENER HOLES. R & R SEAT RAIL BEAM WITH NEW BEAM IAW SRM REO 601R-53-61-3778.
- [SDR REXA2015102700994](https://openairdocs.org/sdr/REXA2015102700994.md): Life Vest · unserviceable · Oct 27, 2015 · N8907A · Cndair CL6002B19 · Life Jacket
  > THREE INFANT LIFE VESTS HAVE DAMAGED PACKAGES. R & R ALL THREE INFANT LIFE VEST IAW PA 25-096A.
- [SDR REXA2015102700993](https://openairdocs.org/sdr/REXA2015102700993.md): Flashlight · inoperative · Oct 27, 2015 · N8907A · Cndair CL6002B19 · Emergency Equipment
  > FIRST OFFICERS EMER FLASHLIGHT DOES NOT SHOW A CHARGE. DEFERRED FLASHLIGHT IAW MEL 25-61-04, CAT C. UPDATED PLACARD INSTALLED. R & R FIRST OFFICERS FLASHLIGHT IAW AMM 25-61-04, CLEARED MM02, CLEARED DM 002511 & PLACARD REMOVED.
- [SDR REXA2015091300859](https://openairdocs.org/sdr/REXA2015091300859.md): Warning System · false activation · Sep 13, 2015 · N8907A · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE AFTER ROTATION, WHEN GEAR LEVER WAS SELECTED TO UP, RETRACTION, WITHIN 6 SECONDS OF HANDLE MOVEMENT, MANUAL RELEASE WAS PULLED. ALSO STEERING INOPERATIVE CAUTION MSG CAME ON NUMEROUS TIMES DURING TAXI IN. PERFORMED GEAR SWINGS IAW AMM 32--30-00
- [SDR REXA2015071900722](https://openairdocs.org/sdr/REXA2015071900722.md): Unknown · smoke · Jul 19, 2015 · N8907A · Cndair CL6002B19 · Landing Gear Brake System
  > LEFT INNER BRAKE, TIRE WHEEL ASSEMBLY, SMOKE COMING FROM BRAKE AREA AFTER LANDING. BTMS WAS 7, 8, 3 & 3 IN GATE, AFTER 5 MINUTES AFTER LANDING. PERFORMED VISUAL INSPECTION OF LT INBD BRAKE ASSEMBLY IAW AMM 32-43-26. NO FAULTS FOUND.
- [SDR REXA2015063000630](https://openairdocs.org/sdr/REXA2015063000630.md): Hose · leaking · Jun 30, 2015 · N8907A · Cndair CL6002B19 · Crew Oxygen System
  > OXYGEN HOSE FOUND LEAKING DURING INSTALLATION & LEAK CHECKS OF CREW OXYGEN STOWAGE BOX. R & R OXYGEN HOSE IAW AMM 35-11-15. OPERATIONS & LEAK CHECKED GOOD. OK FOR SERVICE.
- [SDR REXA2015032900350](https://openairdocs.org/sdr/REXA2015032900350.md): Warning System · false activation · Mar 29, 2015 · N8907A · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAP FAIL MASTER CAUTION MSG AFTER LANDING, ON TAXI IN ON GND WHILE RETRACTING, FAILED AT 27' TEMP OAT 1C. REFER TO AML PAGE 3177544 DISC 1, FLAP FAIL MSG AFTER LANDING ON GND DURING FLAP RETRACTION, TROUBLE SHOT FLAP FAIL EVENT IAW FIM CHAPTER 27-50-00 REV 4
- [SDR REXA2014121001177](https://openairdocs.org/sdr/REXA2014121001177.md): Light · inoperative · Dec 10, 2014 · N8907A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE AT SEAT 1C. REPAIRED EMER FLOOR TRACK LIGHTING IAW MM CH 33-51-01. SEE NON-ROUTINE N61000 FOR WORK COMPLETED.
- [SDR REXA2014083100852](https://openairdocs.org/sdr/REXA2014083100852.md): Cage · damaged · Aug 31, 2014 · N8907A · Cndair CL6002B19 · Smoke Detection
  > CARGO COMPARTMENT FWD SMOKE DETECTOR CAGE IS DAMAGED. R & R CARGO SMOKE DETECTOR NR 1 CAGE ASSEMBLY IAW AMM 26-15-01. OPERATIONS CHECKED OK.
- [SDR REXA2014041900072](https://openairdocs.org/sdr/REXA2014041900072.md): Bulkhead · cracked · Apr 18, 2014 · N8907A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 280 BULKHEAD WEB OTBD OF RBL 9 & LBL 9 IS CRACKED. REPAIRED IAW REO 601R-53-11-171 & 601R-53-11-136.
- [SDR REXA2014041800070](https://openairdocs.org/sdr/REXA2014041800070.md): Stiffener · chafed · Apr 17, 2014 · N8907A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > STIFFENER ON AFT SIDE OF FS 621 BULKHEAD AT BL 0 BEHIND ISOLATION VLV IS CHAFED. REPAIRED IAW REO 601R-53-61-1523.
- [SDR REXA2014041500066](https://openairdocs.org/sdr/REXA2014041500066.md): Skin · dented · Apr 15, 2014 · N8907A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THE DAMAGE CONSISTS OF A DENT TO THE FUSELAGE SKIN MEASURING 3.9” X 3.2” X 0.085” DEEP AFT OF THE PRODUCTION SKIN SPLICE AT FS 333 & BETWEEN STRINGER 20R & STRINGER 21R. REPAIRED IAW EA 253-02443A.
- [SDR REXA2014041500065](https://openairdocs.org/sdr/REXA2014041500065.md): Frame · corroded · Apr 15, 2014 · N8907A · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND CORROSION TO THE FRAME AT FS 605. CORROSION WAS BLENDED FROM THE VERTICAL WEB RESULTING 3” X 2” X 0.007” DEEP MATERIAL REMOVAL. CORROSION WAS ALSO NOTED BETWEEN THE SKIN & LOWER FLANGE. REPAIRED IAW EA 253-02457.
- [SDR REXA2014013100156](https://openairdocs.org/sdr/REXA2014013100156.md): Life Vest · unserviceable · Jan 31, 2014 · N8907A · Cndair CL6002B19 · Life Jacket
  > FLIGHT ATTENDANT`S LIFE VEST BAG TORN. R & R LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013082501607](https://openairdocs.org/sdr/REXA2013082501607.md): Autopilot Sys · malfunctioned · Aug 25, 2013 · N8907A · Cndair CL6002B19 · Autopilot System
  > AT FL 290, AUTOPILOT HAD AN UNCOMMANNDED PITCH UP THAT CAUSED THE ACFT TO CLIMB APPROX 200 FT.
- [SDR REXA2013072501106](https://openairdocs.org/sdr/REXA2013072501106.md): Skin · dented · Jul 21, 2013 · N8907A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN DENTED MEASURING 2.710" X 1.5" X.0655" DEEP WITH MATERIAL LOSS FROM BLENDING MEASURING.007" MAXIMUM DEPTH OVER AND SURROUNDING THE DAMAGED AREA. REPAIRED IAW EA CRJ253-01771 AND ASSOCIATED 8110-3.
- [SDR REXA2013061201183](https://openairdocs.org/sdr/REXA2013061201183.md): Container · torn · Jun 12, 2013 · N8907A · Cndair CL6002B19 · Life Jacket
  > CAPTAIN'S LIFE VEST BAG TORN. R & R LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013010600115](https://openairdocs.org/sdr/REXA2013010600115.md): Sign · loose · Jan 6, 2013 · N8907A · Cndair CL6002B19 · Emergency Lighting
  > EXIT SIGN OVER GALLEY SERVICE DOOR LOOSE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY EXIT SIGN IAW AMM 33-51-13. OPS CHECKS GOOD. OK FOR SERVICE.
- [SDR REXA2012121401775](https://openairdocs.org/sdr/REXA2012121401775.md): Battery · discharged · Dec 14, 2012 · N8907A · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING. REPLACED FLIGHT ATTENDANT'S FLASHLIGHT BATTERY IAW 25-60-00. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.
- [SDR REXA2012121201766](https://openairdocs.org/sdr/REXA2012121201766.md): Sign · broken · Dec 12, 2012 · N8907A · Cndair CL6002B19 · Emergency Lighting
  > GALLEY EMERGENCY EXIT SIGN BROKEN. RE-ATTACHED EMERGENCY LIGHT IAW AMM 33-51-09.
- [SDR REXA2012070701057](https://openairdocs.org/sdr/REXA2012070701057.md): Switch · inoperative · Jul 7, 2012 · N8907A · Cndair CL6002B19 · Speed-Attitude Correction System
  > MACH TRIM WILL NOT ENGAGE. REMOVED AND REPLACED MACH TRIM ENGAGE SWITCH AND OPS CHECKS GOOD IAW AMM 22-21-00.
- [SDR REXA2012051300729](https://openairdocs.org/sdr/REXA2012051300729.md): Switch · dirty · May 13, 2012 · N8907A · Cndair CL6002B19 · Aileron Tab Control System
  > AILERON TRIM IS DIFFICULT TO MOVE TO THE LEFT. REMOVED DEBRIS FROM AILERON TRIM SWITCH, CHECKS NORMAL IAW AMM 27-11-00. OK FOR SERVICE.
- [SDR REXA2012041700526](https://openairdocs.org/sdr/REXA2012041700526.md): Landing Gear · malfunctioned · Apr 17, 2012 · N8907A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > NLG GEAR DISAGREE. PROBLEM OCCURRED ON TAKEOFF NOSE GEAR WOULD NOT RETRACT. NOSE GEAR NEVER MOVED FROM THE DOWN AND LOCKED POSITION AS VERIFIED BY CODES. S35 SHOWED DOWN AND NEAR AND S21 SHOWED DOWN AND NEAR. CODE 23 SHOWED DOWN AND FAR WHICH IS FOR THE OLE
- [SDR REXA2012032100404](https://openairdocs.org/sdr/REXA2012032100404.md): Proximity Switch · out of adjust · Mar 21, 2012 · N8907A · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE ON LANDING (GEAR EXTENSION). FOUND NOSE GEAR UPLOCK PIN STICKING AND FOUND SEVERAL PROX SWITCHES OUT OF ADJUSTMENT. ADJUSTED SWITCHES, LUBED ROLLER, AND OPS CHECK GOOD.
- [SDR REXA2012021800264](https://openairdocs.org/sdr/REXA2012021800264.md): Unknown · odor · Feb 18, 2012 · N8907A · Cndair CL6002B19 · Air Distribution System
  > ON APPROACH AT 7000 FT, FLIGHT ATTENDANT INDICATED A STRONG GASOLINE ODOR IN REAR OF AIRCRAFT AROUND LAVATORY. RAN PACKS WITH ENGINES, AND APU IAW AMM'S 72-20-00 & 49-10-00, COULD NOT FIND LEAK OR FIND ANY EVIDENCE OF FUEL ODOR. ACFT OK FOR SERVICE.
- [SDR REXA201200125](https://openairdocs.org/sdr/REXA201200125.md): Light · inoperative · Jan 15, 2012 · N8907A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT FLOOR STRIP AT SEAT 6CD IS INOP. REMOVED AND REPLACED THE 6CD POSITION EMERGENCY FLOOR LIGHT STRIP IAW AMM 33-51-01. OPS CHECKS GOOD. THIS CLEARS DM 57676. A/C READY FOR SERVICE.

Next page: https://openairdocs.org/deregistered/N8907A-2023-02-24/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 = 'N8907A' AND deregistration_id = 'N8907A-2023-02-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8907A-2023-02-24/reports

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