# Service difficulty reports: N8972E, cancelled Jul 7, 2023

A list on [N8972E, cancelled Jul 7, 2023](https://openairdocs.org/deregistered/N8972E-2023-07-07.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 · 58 reports

- [SDR REXA2016033000443](https://openairdocs.org/sdr/REXA2016033000443.md): Battery Pack · discharged · Mar 30, 2016 · N8972E · Cndair CL6002B19 · Emergency Lighting
  > UPPER EMER EXIT LIGHTED SIGN ON FWD WARDROBE INOPERATIVE. R & R BATTERY PACK AT LOCATION STATION 309L IAW AMM 33-51-04. OPERATIONS CHECKED GOOD.
- [SDR REXA2016012100081](https://openairdocs.org/sdr/REXA2016012100081.md): Mount Bracket · broken · Jan 21, 2016 · N8972E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT WW CONNECTOR MOUNTING BRACKET FOR J110 J112 IS BROKEN. REMOVED & INSTALLED SERVICEABLE CONNECTOR MOUNTING BRACKET FOR J110 J112 IAW SRM 51-42-21, ESPM 20-17-10 & EA CRJ253-03946.
- [SDR REXA2016012000073](https://openairdocs.org/sdr/REXA2016012000073.md): Support · cracked · Jan 20, 2016 · N8972E · Cndair CL6002B19 · Service Doors
  > AIRCRAFT GND POWER RECEPTACLE SUPPORT IS CRACKED AT INBD AFT SIDE. THE EXTERNAL GND POWER RECEPTACLE SUPPORT WAS REPLACED IAW SRM 51-42-06 & 51-42-21. RT DOOR WAS DISCONNECTED AT CONTROL ROD. RECONNECTED & CHECKED GOOD IAW AMM 32-22-15-400-801. PERFORMED
- [SDR REXA2016012000069](https://openairdocs.org/sdr/REXA2016012000069.md): Door Sill · corroded · Jan 20, 2016 · N8972E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT SIDE SILL FS 574.00 - 621 HAS MINOR CORROSION AROUND NUTPLATES. MINOR CORROSION WAS REPAIRED ON LT SIDE SILL BY PERFORMING REO 601R-53-61-1574, REV B. REMOVING LOWER COAMING SECTION THEN REINSTALLING AFTER REPAIRS IAW SRM 51-42-06 & 51-42-21. A LEAK CH
- [SDR REXA2016012000068](https://openairdocs.org/sdr/REXA2016012000068.md): Structure · damaged · Jan 20, 2016 · N8972E · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RIGHT FUEL BOOST PUMP CUT OUT LAND SURFACE HAS AN INDICATION.1"" LONG BY 50% FSH. FAILED NDT INSPECTION. RT FUEL & BOOST PUMP WAS REMOVED, REINSTALLED & OPERATIONS & LEAK CHECKED IAW AMM 28-23-01-400-801. BOOST PUMP CUT OUT WAS REPAIRED IAW REO:601R-57-21-
- [SDR REXA2016011900071](https://openairdocs.org/sdr/REXA2016011900071.md): Glowstrip · delaminated · Jan 19, 2016 · N8972E · Cndair CL6002B19 · Emergency Equipment
  > EMERGENCY LIGHT TRACK HAS 5 PIECES THAT ARE DELAMINATED. THE TWO FWD PIECES LT & RT PIECES AFT & PIECE JUST FWD OF THE AFT & LT. INSTALLED NEW PHOTO LUMINESCENT LIGHT TRACK TOTAL OF 5 PIECES ON THE LT & RT SIDES IAW AMM 33-51-01-400-806.
- [SDR REXA2016011800074](https://openairdocs.org/sdr/REXA2016011800074.md): Handle · damaged · Jan 18, 2016 · N8972E · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > AVIONICS DOOR HANDLE HOUSING HAS INDICATION ALL AROUND THE BASE OF HANDLE SHAFT, APPROX 90% FSH FAILED NDT. AVIONICS DOOR HANDLE WAS REPAIRED BY REMOVING & REINSTALLING DOOR IAW AMM 52-42-00-400-803, REMOVING & INSTALLING NEW HANDLE ASSEMBLY IAW AMM 52-42-03-
- [SDR REXA2016011700086](https://openairdocs.org/sdr/REXA2016011700086.md): Post · damaged · Jan 17, 2016 · N8972E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409.0+128, VERTICAL POST, BL 0.0 AT WL 69, HAS AN INDICATION IN THE AFT FLANGE RADIUS OF BOTH LT POST.265"" LONG BY 70% FSH & RT POST.260"" BY 65% FSH. FAILED NDT INSPECTION. R & R FS 409+128, BL 0 LT & RT VERTICAL POST IAW SRM 51-42-06, 51-40-11 & REO
- [SDR REXA2016011700080](https://openairdocs.org/sdr/REXA2016011700080.md): Seat Track · eroded · Jan 17, 2016 · N8972E · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT FLOOR SEAT RAILS NR 1, 2 & 5 ERODED. REPLACED RT FLOOR SEAT RAIL SECTIONS NR 1 & 2 WITH SERVICEABLE SEAT RAILS. FABRICATED SEAT RAIL SECTION NR 5 & INSTALLED IAW AMM 53-01-11-400-802 & REO 601R-53-00-485.
- [SDR REXA2016011600125](https://openairdocs.org/sdr/REXA2016011600125.md): Post · damaged · Jan 16, 2016 · N8972E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409.0+128, VERTICAL POST RBL 18 AT WL 69, HAS AN INDICATION IN THE AFT FLANGE RADIUS OF BOTH THE INBD POST.250" LONG BY 57% FSH & OTBD POST.250" LONG BY 50% FSH. FAILED NDT INSPECTION. REMOVED & INSTALLED SERVICEABLE LT & RT FS 409+128, RBL 18 VERTICAL
- [SDR REXA2016011600085](https://openairdocs.org/sdr/REXA2016011600085.md): Post · damaged · Jan 16, 2016 · N8972E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409.0+128, VERTICAL POSTS, LBL 18 AT WL 69, HAS AN INDICATION IN THE AFT FLANGE RADIUS OF BOTH THE OTBD POST.250"" LONG X 60% FSH & INBD POST.247"" LONG BY 53% FSH. FAILED NDT INSPECTION. R & R LT & RT FS 409+128, LBL 18 VERTICAL POSTS IAW SRM 51-42-06,
- [SDR REXA2016011600082](https://openairdocs.org/sdr/REXA2016011600082.md): Angle · corroded · Jan 16, 2016 · N8972E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR LOWER SILL, SILL MOUNT ANGLE PN 601R31527-221 IS CORRODED AROUND PROX SENSOR. R & R PAX DOOR LOWER SILL MOUNT ANGLE PN 601R31527-221 IAW SRM 51-42-06, 51-42-21, 51-42-13.
- [SDR REXA2016011600067](https://openairdocs.org/sdr/REXA2016011600067.md): Skin · corroded · Jan 16, 2016 · N8972E · Cndair CL6002B19 · Wing, Plate/Skin
  > LOWER LT WING ACCESS HOLE NR 1, PANEL 540BB, HAS CORROSION ON CUT OUT, IN CRITICAL & NON-CRITICAL AREA. PERFORMED REPAIR ON LOWER LT WING ACCESS HOLE NR 1 PANEL 540BB IAW REO 601R-57-21-030 REV L.
- [SDR REXA2016011400078](https://openairdocs.org/sdr/REXA2016011400078.md): Seat Track · eroded · Jan 14, 2016 · N8972E · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT RAIL NR 5 ERODED FS 409.0+128 - FS 439. REPAIRED LT SIDE SEAT RAIL NR 5 CORROSION FS 409.0+128 - FS 439 IAW EA 253-03929 & SRM 51-40-11.
- [SDR REXA2016011200079](https://openairdocs.org/sdr/REXA2016011200079.md): Seat Track · eroded · Jan 12, 2016 · N8972E · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FLOOR SEAT RAILS NR 1, 2, 4 & 5 ERODED. REMOVED CORRODED SEAT RAILS NR 2, FS 364 - 394.00 & INSTALLED NEW SEAT RAIL PN 601R31032-15 IAW AMM 53-01-11-400-802. REMOVED CORRODED SEAT RAIL NR 2. FABRICATED & INSTALLED NEW NR 2 SEAT RAIL IAW 601R-53-00-485
- [SDR REXA2016011200070](https://openairdocs.org/sdr/REXA2016011200070.md): Support · damaged · Jan 12, 2016 · N8972E · Cndair CL6002B19 · Cargo/Baggage Doors
  > REAR CARGO DOOR TRACK SUPPORT STRUCTURE PN 601R35050-64 IS CUT & CHAFED FROM FWD BALANCE SPRING CABLE. REPAIRED REAR CARGO DOOR TRACK SUPPORT STRUCTURE PN 601R35050-64 IAW A253-03909 THIS IS A MAJOR REPAIR. SEE JOB CARD 8797211 OP 8 FOR STEPS
- [SDR REXA2016011100084](https://openairdocs.org/sdr/REXA2016011100084.md): Angle · cracked · Jan 11, 2016 · N8972E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT EQUIPMENT BAY RT SIDE, FS 621 - 625 OBLIQUE ANGLE CRACKED. REMOVED CRACKED OBLIQUE ANGLE & REPLACED WITH SERVICEABLE OBLIQUE ANGLE, PN 601-35012-52, IAW SRM 51-42-21.
- [SDR REXA2016011100083](https://openairdocs.org/sdr/REXA2016011100083.md): Angle · cracked · Jan 11, 2016 · N8972E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT EQUIPMENT BAY LT SIDE FS 621 - 625 OBLIQUE ANGLE CRACKED. REMOVED CRACKED OBLIQUE ANGLE & REPLACED WITH SERVICEABLE OBLIQUE ANGLE PN 601-35012-51 IAW SRM 51-42-21.
- [SDR REXA2016011100077](https://openairdocs.org/sdr/REXA2016011100077.md): Floor Support · corroded · Jan 11, 2016 · N8972E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO BAY, FLOOR SUPPORT RAIL AT LBL 24.0, FS 590 - 621 HAS MINOR CORROSION AROUND THE NUTPLATES. REPLACED FLOOR CAP PN 601R35031-263. REINSTALLED FILLER STRIP AS DETAILED IN STEPS 1-4.
- [SDR REXA2016011000076](https://openairdocs.org/sdr/REXA2016011000076.md): Attach Fitting · cracked · Jan 10, 2016 · N8972E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280, RBL 9 INBD ATTACH CLIP IS CRACKED. R & R FS 280.00, RBL 9 CLIP PN 601R31113-58 IAW SRM 51-40-11 & 51-42-21.
- [SDR REXA2016011000075](https://openairdocs.org/sdr/REXA2016011000075.md): Angle · corroded · Jan 10, 2016 · N8972E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280, FWD J ANGLE IS CORRODED AROUND FASTENER HOLES. LOCATED, DRILLED & INSTALLED NEW FS 280 FWD J ANGLE IN PLACE OF DAMAGED FWD J ANGLE PN 600-34017-351 IAW 51-40-11, 51-42-06 & 51-42-21
- [SDR REXA2016010800072](https://openairdocs.org/sdr/REXA2016010800072.md): Channel · cracked · Jan 8, 2016 · N8972E · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD TRACK LOWER AFT C CHANNEL IS CRACKED. R & R CHANNEL 601R35050-25 IAW SRM 51-42-06.
- [SDR REXA2015111701067](https://openairdocs.org/sdr/REXA2015111701067.md): Life Vest · unserviceable · Nov 17, 2015 · N8972E · Cndair CL6002B19 · Life Jacket
  > INFANT LIFE VEST SEAL BROKEN. R & R INFANT LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2015110901056](https://openairdocs.org/sdr/REXA2015110901056.md): Bracket · bent · Nov 9, 2015 · N8972E · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE ON TAKEOFF. NOSE GEAR REMAINED IN DOWN POSITION. RAN QRH & DID NOT FIX ISSUE. NOSE DOOR MSG ALSO DISPLAYED. DEFERRED LG RETRACTION SYS IAW MEL 32-30-01. ALL MX REQUIREMENT COMPLIED WITH. PLACARDED IAW MEL, ENTERED INTO MM02. ACFT OK FOR SE
- [SDR REXA2015091200857](https://openairdocs.org/sdr/REXA2015091200857.md): Battery Pack · discharged · Sep 12, 2015 · N8972E · Cndair CL6002B19 · Emergency Lighting
  > ALL EMER LIGHTS INOPERATIVE DURING TEST. R & R EMER BATTERY PACKS 1, 2, 3 & 4 IAW AMM 33-51-04. OPERATIONS CHECKED GOOD.
- [SDR REXA2015072400737](https://openairdocs.org/sdr/REXA2015072400737.md): Control Unit · failed · Jul 24, 2015 · N8972E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MESSAGE RECEIVED AT CRUISE ALTITUDE OF 30,000 FEET. THE EVENT OCCURRED WITH THE FLAPS FULLY RETRACTED AT 0* INFLIGHT WITH AN EICAS POSITION OF 0*. AIRSPEED AT THE TIME OF FAILURE WAS 290 KTS AT APPROX 1 HOUR INTO THE FLIGHT. PERFORMED TRO
- [SDR REXA2015072000127](https://openairdocs.org/sdr/REXA2015072000127.md): Skin · dented · Jul 17, 2015 · N8972E · Cndair CL6002B19 · Rudder, Plate/Skin
  > DURING PAINT, FOUND A DENT IN THE LT RUDDER SKIN. THE DENT MEASURE 7.00” X 2.00” X 0.038” DEEP. REPAIRED IAW EA CRJ255-03564.
- [SDR REXA2015071700720](https://openairdocs.org/sdr/REXA2015071700720.md): Skin · damaged · Jul 17, 2015 · N8972E · Cndair CL6002B19 · Rudder, Plate/Skin
  > DURING PAINT, MX FOUND A DENT, CREASE IN LT SIDE OF RUDDER SKIN BETWEEN RS 136.9 & 142.63, MEASURING 1" LONG & 2" WIDE X.038 DEEP, DEFERRED IAW EA CRJ253-03563, SECTION I, PERMANENT REPAIR AFTER FERRY FLIGHT. PERMANENTLY REPAIRED DENT ON LT SIDE OF RUDDER IA
- [SDR REXA2015070200654](https://openairdocs.org/sdr/REXA2015070200654.md): Bracket · defective · Jul 2, 2015 · N8972E · Cndair CL6002B19 · Landing Gear Position and Warning
  > NOSE DOOR & NOSE GEAR ON GEAR UP DISAGREE MASTER WARNING, NOSE GEAR STAYED DOWN & LOCKED, MAIN GEAR WAS NORMAL. REPLACED NLG SENSOR BRACKET. REPLACED TARGET BRACKET & ADJUSTED SENSOR IAW 32-61-05. REINSTALLED TOW COLLAR IAW PA 32-066C STEPS 1 -12. COMPLET
- [SDR REXA2015050700469](https://openairdocs.org/sdr/REXA2015050700469.md): Clamp · missing · May 7, 2015 · N8972E · Cndair CL6002B19 · Emergency Equipment
  > LEFT OVERWING EMER ROPE MISSING C CLAMP. REPLACED LT D CLIP ON EMER ROPE IAW AMM 25-63-04. OK FOR SERVICE.
- [SDR REXA2015050100456](https://openairdocs.org/sdr/REXA2015050100456.md): Glowstrip · degraded · May 1, 2015 · N8972E · Cndair CL6002B19 · Emergency Equipment
  > CABIN EMER FLOOR PHOTO LUMINESCENT STRIP DEGRADED AT SEAT 3 - 5C. R & R PHOTO LUMINESCENT STRIP IAW AMM 33-51-01.
- [SDR REXA2015020900191](https://openairdocs.org/sdr/REXA2015020900191.md): Oxygen Mask · inoperative · Feb 9, 2015 · N8972E · Cndair CL6002B19 · Crew Oxygen System
  > OBSERVERS OXYGEN MASK IS INOPERATIVE. DEFERRED OBSERVERS OXYGEN SYS IAW MEL 35-10-01 PLACARD INSTALLED. R & R WITH SERVICEABLE OXY MASK IAW AMM 35-11-12. LEAK & OPERATIONS CHECKED GOOD. REMOVED FROM MM02, REMOVED PLACARD, THIS CLEARS DM 000506.
- [SDR REXA2015020300173](https://openairdocs.org/sdr/REXA2015020300173.md): Battery · weak · Feb 3, 2015 · N8972E · Cndair CL6002B19 · Emergency Lighting
  > NUMBER 4 EMER LIGHT BATTERY WEAK. R & R NR 4 EMER LIGHT BATTERY. OPERATIONS CHECKED GOOD IAW AMM 33-51-04.
- [SDR REXA2015020300172](https://openairdocs.org/sdr/REXA2015020300172.md): Lens · missing · Feb 3, 2015 · N8972E · Cndair CL6002B19 · Emergency Lighting
  > AFT CEILING EMER EXIT SIGN BLUE LENS COVER MISSING. INSTALLED BLUE LENS COVER ON CEILING EMER EXIT SIGN AFT SIDE IAW AMM 33-51-14.
- [SDR REXA2014092500997](https://openairdocs.org/sdr/REXA2014092500997.md): Cable · frayed · Sep 25, 2014 · N8972E · Cndair CL6002B19 · Passenger/Crew Doors
  > DURING PA52-059 FOUND PAX DOOR MOTOR CABLE FRAYED & WORN BEYOND LIMITS. R & R THE PAX DOOR MOTOR CABLE IAW AMM 52-11-08-04 & AMM 52-11-09-04. OPERATIONS CHECKED GOOD.
- [SDR REXA2014072800745](https://openairdocs.org/sdr/REXA2014072800745.md): Engine · malfunctioned · Jul 28, 2014 · N8972E · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ACFT EXPERIENCED INFLIGHT SHUTDOWN OF THE RT ENG. RT ENG OIL PRESS WARNING MSG & RT ENG OIL PRESS INDICATIONS WERE <30 PSI & DECREASING, FLUCTUATING. REDUCED RT ENG THRUST TO IDLE ALMOST IMMEDIATELY THEN COMPLETED QRH WITH INFLIGHT SHUTDOWN. R & R RT ENG IA
- [SDR REXA2014052700525](https://openairdocs.org/sdr/REXA2014052700525.md): Pseu · faulty · May 27, 2014 · N8972E · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MSG CLIMBING THROUGH FL 210. FOUND CODE A02 FAIL ON PSEU ON LEG NR 1. PERFORMED OPERATIONS CHECK AFTER REMOVAL & REPLACEMENT OF PSEU IAW AMM 32-61-01. OPERATIONS CHECKED GOOD. PSEU PANEL RELIGHT LIGHT FAILED. A02 CODE IS FOR FAULT ON
- [SDR REXA2011012300010](https://openairdocs.org/sdr/REXA2011012300010.md): Bulkhead · cracked · Jan 21, 2014 · N8972E · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FUSELAGE STATION 621 BULKHEAD CRACKED AT LINTEL FITTING UPPER SIDE. REPAIRED IAW REO 601R-53-61-1230.
- [SDR REXA2013121302402](https://openairdocs.org/sdr/REXA2013121302402.md): Flap · failed · Dec 13, 2013 · N8972E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MESSAGE. DEFERRED, PERFORMED TROUBLESHOOTING IAW FIM REV 45, IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC DATED JULY 22, 2013 & PA AD 27-052N. SEE CORRECTIVE ACTION FOR LOG PAGE 2537736-2. THIS CLEARS DMI 020289 PLACARD REMOVED.
- [SDR REXA2013121002295](https://openairdocs.org/sdr/REXA2013121002295.md): Life Vest · unserviceable · Dec 10, 2013 · N8972E · Cndair CL6002B19 · Life Jacket
  > FIRST OFFICER`S LIFE VEST BAG TORN. R & R FIRST OFFICER'S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013121002294](https://openairdocs.org/sdr/REXA2013121002294.md): Life Vest · unserviceable · Dec 10, 2013 · N8972E · Cndair CL6002B19 · Life Jacket
  > FLIGHT ATTENDANT'S LIFE VEST BAG TORN. R & R FLIGHT ATTENDANT’S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013080601562](https://openairdocs.org/sdr/REXA2013080601562.md): Flashlight · inoperative · Aug 6, 2013 · N8972E · Cndair CL6002B19 · Emergency Equipment
  > F/O EMERGENCY FLASHLIGHT INOPERATIVE.
- [SDR REXA2013042900644](https://openairdocs.org/sdr/REXA2013042900644.md): Angle · cracked · Apr 28, 2013 · N8972E · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 559 SEMI PRESSURE BULKHEAD CAP ANGLE FOUND CRACKED AT LBL 18 AND RBL 18. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 AND 601R-53-41-609 AND PA 53-025.
- [SDR REXA2012091901353](https://openairdocs.org/sdr/REXA2012091901353.md): Bpsu · failed · Sep 19, 2012 · N8972E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > WHEN CREW ATTEMPTED TO EXTEND FLAPS AT 162 KIAS A FLAPS FAIL MESSAGE WAS RECEIVED AND THE FLAPS WERE STUCK AT ZERO DEGREES. THE FLIGHT THEN DIVERTED TO EWR FOR RUNWAY LENGTH REQUIREMENT. FERRIED AIRCRAFT TO DTW ON 9/21/2012 WHERE PERFORMED TROUBLESHOOTING PE
- [SDR REXA2012091101336](https://openairdocs.org/sdr/REXA2012091101336.md): Door · out of position · Sep 11, 2012 · N8972E · Cndair CL6002B19 · Emergency Exits
  > RIGHT EMERGENCY EXIT DOOR CAUTION MESSAGE INTERMITTENTLY ON IN FLIGHT. INSTALLED EMERGENCY EXIT DOORS INTO THEIR CORRECT RESPECTIVE POSITION. OPS CHECKED GOOD, OK FOR SERVICE. CLEARED DM.
- [SDR REXA2012091201093](https://openairdocs.org/sdr/REXA2012091201093.md): Bulkhead · chafed · Sep 5, 2012 · N8972E · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD CHAFED AT WL120.43 AND LBL40. REPAIRED IAW REO 601R-53-61-2155 AND 601R-53-61-4633.
- [SDR REXA2012051800755](https://openairdocs.org/sdr/REXA2012051800755.md): Bpsu · malfunctioned · May 18, 2012 · N8972E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MSG ON CLIMB AT 0. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H) (6) (I). AMOC DATED MARCH 27, 2009 TR# 27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD 27-052G. REMOVED AND REPLACED LEFT BPSU IAW AM
- [SDR REXA2012042200558](https://openairdocs.org/sdr/REXA2012042200558.md): Ecu · malfunctioned · Apr 22, 2012 · N8972E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 0 IN CRUISE (RESET GOOD). REPLACED LT FECU. ALL OPS CHECKS GOOD. NO JAM CODES.
- [SDR REXA2012042000542](https://openairdocs.org/sdr/REXA2012042000542.md): Light · broken · Apr 20, 2012 · N8972E · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT NEAR THE FLOOR BY THE MAIN CABIN DOOR BROKEN. REPLACED LIGHT ASSY W/SERVICEABLE. ALL CHECKS GOOD.
- [SDR REXA2012040100455](https://openairdocs.org/sdr/REXA2012040100455.md): Trim System · malfunctioned · Apr 1, 2012 · N8972E · Cndair CL6002B19 · Aileron Tab Control System
  > AILERON TRIM WILL NOT TRIM LEFT. CYCLED AILERON CIRCUIT BREAKER IAW AMM 27-12-01. OP CHECKED GOOD, OK FOR SERVICE.

Next page: https://openairdocs.org/deregistered/N8972E-2023-07-07/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 = 'N8972E' AND deregistration_id = 'N8972E-2023-07-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8972E-2023-07-07/reports

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