# Service difficulty reports: N8412F, cancelled Apr 10, 2019

A list on [N8412F, cancelled Apr 10, 2019](https://openairdocs.org/deregistered/N8412F-2019-04-10.md).

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

- [SDR REXA2015010900012](https://openairdocs.org/sdr/REXA2015010900012.md): Bulb · wrong part · Jan 9, 2015 · N8412F · Cndair CL6002B19 · Emergency Lighting
  > PA & EMERGENCY LIGHTS, LIGHT SWITCHES INOPERATIVE ON LOWER PEDESTAL, R & R PA & EMERGENCY LIGHT SWITCH BULBS WITH CORRECT BULBS IAW CMM 23-31-07 & AMM 31-11-00. OPS CHECKED GOOD.
- [SDR REXA2014111801140](https://openairdocs.org/sdr/REXA2014111801140.md): Packing · damaged · Nov 18, 2014 · N8412F · Cndair CL6002B19 · Hydraulic System, Main
  > TASK CARD 900-53-900-504 2 LT, 4 RT, 6 TOTAL RUBBER DECOMPRESSION PANEL BETWEEN FS 280.00 & FS 477.40 ARE TORN. UPON GEAR RETRACTION RECEIVED NR 3 HYD CAUTION FOLLOWED BY GEAR DISAGREE WARNING HYD NR 3 WAS SHOWING BOTH PUMPS OFF, YELLOW FLOW LINES & 100% CAPA
- [SDR REXA2014100301014](https://openairdocs.org/sdr/REXA2014100301014.md): Inverter · inoperative · Oct 3, 2014 · N8412F · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR LIGHTS MID CABIN INOPERATIVE. WALL EMER EXIT LIGHT AT 8D INOPERATIVE. REPLACED EMER LIGHTING INVERTER NR 3 IAW AMM 33-51-07. OPERATIONS CHECKED GOOD. REFERENCE WORK CARD 54556 FOR DETAILS.
- [SDR REXA2014091300951](https://openairdocs.org/sdr/REXA2014091300951.md): Connector · disconnected · Sep 13, 2014 · N8412F · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY FLOOR LIGHTING IN CTR OF ACFT INOPERATIVE. TROUBLESHOOTING REVEALED AFT CONNECTION OF RT OVERWING EMER FLOOR TRACK LIGHTS DISCONNECTED. RESTORED CONNECTION & OPERATIONS CHECKED IAW AMM 33-51-01. OPERATIONS CHECKED GOOD, ACFT OK FOR SERVICE.
- [SDR REXA2014090300861](https://openairdocs.org/sdr/REXA2014090300861.md): Light · inoperative · Sep 3, 2014 · N8412F · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT ON PA PANEL INT. RELAMPED & OPERATIONS CHECKED GOOD IAW AMM 31-11-00.
- [SDR REXA2014060500570](https://openairdocs.org/sdr/REXA2014060500570.md): Smoke Goggles · broken · Jun 5, 2014 · N8412F · Cndair CL6002B19 · Emergency Equipment
  > CAPTAIN`S SMOKE GOGGLES BROKEN. R & R CAPTAIN'S SMOKE GOGGLES IAW AMM 35-11-12. OK FOR SERVICE.
- [SDR REXA2014032100320](https://openairdocs.org/sdr/REXA2014032100320.md): Check Valve · faulty · Mar 21, 2014 · N8412F · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE WARNING MSG ON RETRACTION NOSE GEAR NOT RETRACTING. PERFORMED SERVICING OG NLG SHOCK STRUT IAW 12-12-610-803 WITH FLUSHING OUT SHOCK STRUT. R & R CHECK VLV ON NOSE STRUT IAW AMM 32-21-01. PERFORMED LG EXT & RETRACTION SEVERAL TIMES IAW AMM 32-
- [SDR REXA2014022100231](https://openairdocs.org/sdr/REXA2014022100231.md): Bulb · inoperative · Feb 21, 2014 · N8412F · Cndair CL6002B19 · Passenger Compartment Lighting
  > PASSENGER CALL LIGHT IN THE OVERHEAD EMERGENCY EXIT SIGN OVER ROW 8 IS INOPERATIVE. THE REAR LIGHT IS INOPERATIVE, THE FWD LIGHT IS FUNCTIONING PROPERLY. REPLACED BULB. OPS TESTED OK IAW AMM 33-22-03.
- [SDR REXA2013082901619](https://openairdocs.org/sdr/REXA2013082901619.md): Proximity Switch · out of adjust · Aug 29, 2013 · N8412F · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE ON RETRACTION AFTER TAKEOFF. RT MLG WOULD NOT LOCK UP. C/W PA 05-018K SCENARIO 1. ADJUSTED RT MLG UPLOCK PROXIMITY SWITCH IAW AMM 32-61-05. VERIFIED CORRECT RIG OF LT MLG UPLOCK PROXIMITY SWITCH IAW AMM 32-61-05. PERFORMED EXT/RETRACTION. OP
- [SDR REXA2013082201606](https://openairdocs.org/sdr/REXA2013082201606.md): Transponder · inoperative · Aug 22, 2013 · N8412F · Cndair CL6002B19 · Dependent Position Determining System
  > NR 2 TRANSPONDER IS INOPERATIVE.
- [SDR REXA2013070301084](https://openairdocs.org/sdr/REXA2013070301084.md): Frame · corroded · Jul 2, 2013 · N8412F · Cndair CL6002B19 · Fuselage Main, Frame
  > MX FOUND CORROSION TO THE LOWER SECTOR OF THE FRAME AT FS 319.7 BETWEEN S26R AND S26L. REPAIRED IAW EA CRJ253-01691.
- [SDR REXA2013062401077](https://openairdocs.org/sdr/REXA2013062401077.md): Skin · gouged · Jun 21, 2013 · N8412F · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MX FOUND A GOUGE IN THE FUSELAGE SKIN AT FS 633 S20L. GOUGE BLENDED.
- [SDR REXA2013061101178](https://openairdocs.org/sdr/REXA2013061101178.md): Smoke Goggles · cracked · Jun 11, 2013 · N8412F · Cndair CL6002B19 · Emergency Equipment
  > F/O'S SMOKE GOGGLES CRACKED. R & R F/O'S SMOKE GOGGLES IAW AMM 25-20-01.
- [SDR REXA2013052700920](https://openairdocs.org/sdr/REXA2013052700920.md): Oxygen Mask · inoperative · May 27, 2013 · N8412F · Cndair CL6002B19 · Crew Oxygen System
  > OBSERVER O2 MASK, INOPERABLE.
- [SDR REXA2013052500913](https://openairdocs.org/sdr/REXA2013052500913.md): Oxygen Mask · defective · May 25, 2013 · N8412F · Cndair CL6002B19 · Crew Oxygen System
  > OBSERVER O2 MASK DOES NOT INFLATE, TEST PROPERLY.
- [SDR REXA2013052300908](https://openairdocs.org/sdr/REXA2013052300908.md): Smoke Goggles · broken · May 23, 2013 · N8412F · Cndair CL6002B19 · Emergency Equipment
  > CAPTAIN SMOKE GOGGLE BROKEN. REMOVED & REPLACED CAPTAIN SMOKE GOGGLES IAW CRJ200 AMM 35-11-12. OK FOR SERVICE.
- [SDR REXA2013050400869](https://openairdocs.org/sdr/REXA2013050400869.md): Flap · malfunctioned · May 4, 2013 · N8412F · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 45 UPON RETRACTION AFTER LANDING, FLAP LEVER POSTION AT 45 AT FAILURE. AIRSPEED=0KTS OAT= 22. PERFORMED OPERATIONS CHECK OF FECU IAW AMM 27-51-05 & SKEW DETECTION SYS IAW AMM 27-51-15. OPERATIONS CHECK GOOD. CYCLED FLAPS MESSAGE CLEARED. OPE
- [SDR REXA2013050200865](https://openairdocs.org/sdr/REXA2013050200865.md): Flap · failed · May 2, 2013 · N8412F · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL UPON LANDING. CREW REPORTED FLAPS FAIL AT 4S DEGREES UPON RETRACTION AFTER LANDING FLAP LEVER POSITION AT 45 AT FAILURE AIRSPEED=0KTS OAT=22 DEGREES C. CREW DID NOT DECLARE EMERGENCY. "
- [SDR REXA2013032100581](https://openairdocs.org/sdr/REXA2013032100581.md): Wire · broken · Mar 21, 2013 · N8412F · Cndair CL6002B19 · Light System Wiring
  > BOTH EMERGENCY LIGHTS INOP. FOUND GROUND WIRES DISCONNECTED AND BROKEN WIRE. REPAIRED BROKEN WIRE TO SPLICE IAW ESPM 20-16-00. RE-INSTALLED GROUND WIRES TO TERMINAL LUG IAW ESPM 20-20-00. OPS CHECK GOOD.
- [SDR REXA2013010700118](https://openairdocs.org/sdr/REXA2013010700118.md): Light · inoperative · Jan 7, 2013 · N8412F · Cndair CL6002B19 · Emergency Lighting
  > 3RD EMERGENCY FLOOD LIGHT IN CABIN INOPERABLE. REMOVED AND REPLACED 3RD EMERGENCY FLOOD LIGHT BULB. OPS CHECK GOOD.
- [SDR REXA2012081401262](https://openairdocs.org/sdr/REXA2012081401262.md): Flap System · malfunctioned · Aug 14, 2012 · N8412F · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 4239, HAD A FLAPS FAIL ON APPROACH WHEN THE FLAPS REACHED 45 DEGREES. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H) (6) (1) AMOC DATED MARCH 27TH 2009 TR NR 12-012 PER AMOC DATED DECEMBER 18 2009 AND PAAD27-052G.
- [SDR REXA20120500668](https://openairdocs.org/sdr/REXA20120500668.md): Track · cracked · May 19, 2012 · N8412F · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK FOUND AT TOP OF AFT CARGO DOOR TRACK, MEASURING 1.5" LONG. REPAIRED IAW BOMBARDIER REO 601R-53-61-1541.
- [SDR REXA2012051100704](https://openairdocs.org/sdr/REXA2012051100704.md): Light · disconnected · May 11, 2012 · N8412F · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS FLOOR STRIPS OUT AFT OF EMERGENCY EXIT. RECONNECTED FLOOR EMERGENCY LIGHTS IAW CRJ 200 AMM CH 33-51-01.
- [SDR REXA2012031900393](https://openairdocs.org/sdr/REXA2012031900393.md): Connector · disconnected · Mar 16, 2012 · N8412F · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHTS INOP FROM ROW 8 AFT. RECONNECTED FLOOR LIGHT CONNECTOR AT LAV AND OPS CHECK IAW AMM 33-51-01, NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR REXA2012030400329](https://openairdocs.org/sdr/REXA2012030400329.md): Unknown · malfunctioned · Mar 4, 2012 · N8412F · Cndair CL6002B19 · Aileron Control System
  > AILERON TRIM FUNCTIONS IN ONE DIRECTION ONLY, CENTERED. OPS CHECKED GOOD IAW AMM.
- [SDR REXA2012022900295](https://openairdocs.org/sdr/REXA2012022900295.md): Connector · defective · Feb 29, 2012 · N8412F · Cndair CL6002B19 · Light System Wiring
  > CENTER EMERGENCY FLOOR LIGHTING INOP. REPLACED CENTER EMERGENCY FLOOR LIGHT STRIP CONNECTOR IAW CRJ200 AMM 33-51-01. OPS CHECK GOOD.
- [SDR REXA201100891](https://openairdocs.org/sdr/REXA201100891.md): Bracket · bent · Nov 30, 2011 · N8412F · Cndair CL6002B19 · Landing Gear Position and Warning
  > NOSE GEAR DISAGREE UPON GEAR RETRACTION. NOSE INDICATION STAYED GREEN DURING ENTIRE EVENT. FOUND NLG OLEO EXTENSION PROX SWITCH BRACKET BENT, SWITCH TO TARGET CLEARANCE OUT OF LIMITS. REMOVED AND REPLACED SWITCH BRACKET IAW CMM 32-20-04. SEE AML 2152304 FO
- [SDR REXA201100626](https://openairdocs.org/sdr/REXA201100626.md): Spoiler · deployed · Sep 27, 2011 · N8412F · Cndair CL6002B19 · Drag Control System
  > GROUND SPOILER DEPLOYED. PERFORMED OPS CHECK OF SPOILERS IAW 27-61-00. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR REXA201100524](https://openairdocs.org/sdr/REXA201100524.md): Crossbeam · corroded · Jul 17, 2011 · N8412F · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT END OF FS 349 CROSSBEAM CORRODED ON O/B END AT SERVICE DOOR ENTRANCE. REPAIRED IAW BOMBARDIER REO 601R-53-21-1320.
- [SDR REXA201100461](https://openairdocs.org/sdr/REXA201100461.md): Sill · corroded · Jul 16, 2011 · N8412F · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT CABIN PRESSURE FLOOR SILL ASSY HAS AREAS OF CORROSION BETWEEN FS 409+128 AND FS 559. REPAIRED IAW REO 601R-53-41-666.
- [SDR REXA201100452](https://openairdocs.org/sdr/REXA201100452.md): Skin · dented · Jul 13, 2011 · N8412F · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT I/B FLAP UPPER SKIN DENTED. REPAIRED IAW SRM 57-52-00 REPAIR 3.
- [SDR REXA201100459](https://openairdocs.org/sdr/REXA201100459.md): Skin · corroded · Jul 11, 2011 · N8412F · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER PLANK FUEL ACCESS HOLE AT WS 54.897 HOLE NR 1 HAS PITTING CORROSION ON O/B EDGE OF CUTOUT MEASURING APPROX.022L,.021W,.003 DEEP IN A NON CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100458](https://openairdocs.org/sdr/REXA201100458.md): Skin · corroded · Jul 11, 2011 · N8412F · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER PLANK FUEL ACCESS HOLE AT WS 188.040 HOLE NR 10 HAS PITTING CORROSION ON I/B EDGE OF CUTOUT MEASURING APPROX.018L,.020W,.002 DEEP IN A NON CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100457](https://openairdocs.org/sdr/REXA201100457.md): Skin · corroded · Jul 11, 2011 · N8412F · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER PLANK FUEL ACCESS HOLE AT WS 230.415 HOLE NR 12 HAS PITTING CORROSION ON O/B EDGE OF CUTOUT MEASURING APPROX.028L,.030W,.002 DEEP IN A NON CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100456](https://openairdocs.org/sdr/REXA201100456.md): Skin · corroded · Jul 11, 2011 · N8412F · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER PLANK FUEL ACCESS HOLE AT WS 95.950 HOLE NR 6 HAS PITTING CORROSION ON I/B EDGE OF CUTOUT MEASURING APPROX.041L,.018W,.002 DEEP IN A NON CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100455](https://openairdocs.org/sdr/REXA201100455.md): Skin · corroded · Jul 11, 2011 · N8412F · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER PLANK FUEL ACCESS HOLE AT WS 54.897 HOLE NR 1 HAS PITTING CORROSION ON I/B EDGE OF CUTOUT IN SEVERAL AREAS MEASURING APPROX.035L,.035W,.002 DEEP IN A NON CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100454](https://openairdocs.org/sdr/REXA201100454.md): Skin · corroded · Jul 11, 2011 · N8412F · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER PLANK FUEL ACCESS HOLE AT WS 249.048 HOLE NR 15 HAS PITTING CORROSION ON I/B EDGE OF CUTOUT MEASURING APPROX.065L,.050W,.002 DEEP IN A NON CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100453](https://openairdocs.org/sdr/REXA201100453.md): Bulkhead · chafed · Jul 11, 2011 · N8412F · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 PRESSURE BULKHEAD FWD FACE IS CHAFED IN 5 PLACES APPROX 3FT ABOVE THE FLOOR, SOME HAVE BEEN PREVIOUSLY BLENDED. REPAIRED IAW BOMBARDIER REO REO 601R-53-61-2155.
- [SDR REXA201100403](https://openairdocs.org/sdr/REXA201100403.md): Unknown · malfunctioned · Jun 19, 2011 · N8412F · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > REF DM 45662, MLG EXTENSION / RETRACTION PERFORMED GEAR SWING AND PA 05-018A, CHECKS GOOD. THIS CLEARS DM 45662 PLACARD REMOVED.
- [SDR REXA201100231](https://openairdocs.org/sdr/REXA201100231.md): A/C Pack · malfunctioned · Apr 13, 2011 · N8412F · Cndair CL6002B19 · Cabin Cooling System
  > CREW REPORTED LT PACK HI TEMP - SMOKE SMELL DEFERRED LT PACK PER MEL 21-51-11. VERIFIED WITH MX THE LT PACK WAS THE SOURCE OF THE SMOKE SMELL.
- [SDR REXA201100229](https://openairdocs.org/sdr/REXA201100229.md): Landing Gear · malfunctioned · Apr 11, 2011 · N8412F · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE MSG WHEN GEAR SELECTED DOWN GEAR CYCLED 3 TIMES COULD NOT GET DOWN & LOCKED. MANUALLY EXTENDED LANDING GEAR AND GOT DOWN & LOCKED WITH 3 GEAR WO 308909 ON APPROACH INTO DTW. C/W PA 05-018A FOUND PSEU CODE TO BE DI 20 DOWN NEAR, S35 DOWN NEAR S2
- [SDR REXA201000177](https://openairdocs.org/sdr/REXA201000177.md): Bulkhead · cracked · Oct 3, 2010 · N8412F · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 559.0 SEMI PRESSURE BULKHEAD HAS INDICATION OF CRACKS AT RBL 9.0 AND RBL 16.0. REPAIRED FS 559.0 BULKHEAD WEB LAW BOMBARDIER REO 601R-53-41-260 REV E, REO 601R-53-41-609 REV B, DEVIATION "C", BSC EO 601R-53-19687 AND BSC EO 601 R-53-19670.
- [SDR REXA201000049](https://openairdocs.org/sdr/REXA201000049.md): Bearing · cracked · Mar 23, 2010 · N8412F · Cndair CL6002B19 · Engine Mount Section
  > DURING ENGINE REMOVAL FOR 18K LLP SHOP VISIT, MAINTENANCE DISCOVERED WHAT APPEARED TO BE A CRACK IN A FORWARD ENGINE MOUNT YOKE BEARING. THE MOUNT YOKE WAS REMOVED FROM SERVICE AND SENT OUT FOR REPAIR. THE REPAIR VENDOR CONFIRMED THE BEARING RACE TO BE CRACK
- [SDR REXA200900116](https://openairdocs.org/sdr/REXA200900116.md): Bpsu · inoperative · Oct 10, 2009 · N8412F · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLIGHT 4106 MSP/MOT - ON APPROACH TO MOT, CREW RECEIVED A "FLAP FAILURE" MESSAGE. QRH FOLLOWED AND AIR RETUNED TO MSP. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE BRAKE POSITION SENSING UNIT (BPSU) FAILED. BPSU REMOVED AND REPLACED AND FLAPS RIGGED PER AMM
- [SDR REXA200900113](https://openairdocs.org/sdr/REXA200900113.md): Bpsu · failed · Aug 28, 2009 · N8412F · Cndair CL6002B19 · Trailing Edge Flap Control System
  > DTW/MEM FLAP FAILURE IN CRUISE QRH FOLLOWED DIVERTED WITH AN UNEVENTFUL LANDING. AIRCRAFT INSPECT AND FOUND THE RIGHT BPSU (BRAKE POSITION SENSING UNIT) FAILED. REMOVED AND REPLACED BPSU PER BOMBARDIER AMM.
- [SDR REXA200600070](https://openairdocs.org/sdr/REXA200600070.md): Clip · corroded · Jun 17, 2006 · N8412F · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION AT FS 319.70 FRAME TO FLOOR ATTACH CLIP. REMOVED AND REPLACED CORRODED CLIP IAW STRUCTURAL REPAIR MANUAL(SRM) 51-42-06, SRM 51-42-10, SRM 51-42-20, AND REPAIR ENGINEERING ORDER (REO)601R-53-21-682.
- [SDR REXA200600052](https://openairdocs.org/sdr/REXA200600052.md): Engine · bird ingestion · Apr 15, 2006 · N8412F · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF AIRCRAFT SUSTAINED BIRD STRIKES LEFT SIDE. LEFT ENGINE SHOWED N1, ITT & VIBRATION FLUCTUATIONS. AN EMERGENCY DECLARED. VECTORS RECEIVED FOR RETURN TO DTW. FLIGHT CREW REQUESTED CFR BE STANDING BY. ENGINE WAS STILL PRODUCING SOME THRUST, FLIG
- [SDR REXA04034](https://openairdocs.org/sdr/REXA04034.md): Flap · out of rig · Nov 18, 2004 · N8412F · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL ON LANDING. SYSTEM RE-RIGGED IAW AMM 27-54-00, OPERATIONALLY CHECKED GOOD.
- [SDR REXA04028](https://openairdocs.org/sdr/REXA04028.md): Potentiometer · out of rig · Nov 5, 2004 · N8412F · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAILURE ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. PERFORMED RIGGING OF FLAP POTENTIOMETERS AND BPSU IAW AMM 27.
- [SDR REXA00006](https://openairdocs.org/sdr/REXA00006.md): Pump · malfunctioned · Jul 27, 2000 · N8412F · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > DURING CRUISE AT FL270, CREW RECEIVED A NR 2 HYDRAULIC HI TEMP CAUTION ON EICAS. SECONDARY INDICATIONS ON THE SYNOPTIC PAGE REVEALED NR 2 SYSTEM PRESSURE WAS A 3600 PSI AND THE TEMPERATURE OF THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP WAS RAPIDLY CLIMBING. RETARD

## 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 = 'N8412F' AND deregistration_id = 'N8412F-2019-04-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8412F-2019-04-10/reports

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