# Service difficulty reports: N8674A

A list on [N8674A](https://openairdocs.org/aircraft/N8674A.md).

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

- [SDR REXA2014071300697](https://openairdocs.org/sdr/REXA2014071300697.md): Light · inoperative · Jul 13, 2014 · N8674A · Cndair CL6002B19 · Emergency Lighting
  > SERVICE DOOR INTERIOR WHITE EMER LIGHTS, 2 OF 5 INOPERATIVE. R & R EMER EXIT LIGHT BULBS IAW 33-51-13. OPERATIONS CHECKED GOOD.
- [SDR REXA2014031200031](https://openairdocs.org/sdr/REXA2014031200031.md): Stiffener · chafed · Mar 8, 2014 · N8674A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ISOLATION VLV IN AEB IS CHAFING ON VERTICAL STIFFENER ON REAR FS 621. REPAIRED IAW REO 601R-53-61-1523.
- [SDR REXA2014031100030](https://openairdocs.org/sdr/REXA2014031100030.md): Frame · corroded · Mar 8, 2014 · N8674A · Cndair CL6002B19 · Fuselage Main, Frame
  > MAINTENANCE FOUND THE FRAME AT FS 349 TO BE CORRODED IN THE WEB & LOWER FLANGE AT STRINGER 25L. THE FRAME WAS SPLICED IAW EA CRJ253-02345 & ASSOCIATED 8110-3.
- [SDR REXA2014031100029](https://openairdocs.org/sdr/REXA2014031100029.md): Floorbeam · corroded · Mar 8, 2014 · N8674A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > MAINTENANCE FOUND THE UPPER FLANGE OF THE FLOOR BEAM AT FS 349 TO BE CORRODED FROM RBL 33.20 TO RBL 42.50. THE CORROSION MEASURES 4.25 INCHES X 1.00 INCH X.034 INCH DEEP. REPAIRED IAW EA CRJ253-02335 & ASSOCIATED 8110-3.
- [SDR REXA2014031100028](https://openairdocs.org/sdr/REXA2014031100028.md): Floorbeam · corroded · Mar 8, 2014 · N8674A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > MAINTENANCE FOUND THE UPPER FLANGE OF THE FLOOR BEAM AT FS 349 TO BE CORRODED SURROUNDING TWO NUTPLATE FASTENER HOLES BETWEEN RBL 9.00 & LBL 45.00. REPAIRED IAW EA CRJ253-02333 & ASSOCIATED 8110-3.
- [SDR REXA2014030500024](https://openairdocs.org/sdr/REXA2014030500024.md): Skin · worn · Mar 4, 2014 · N8674A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT FUEL ACCESS HOLE FOR PANEL 640BB AT WS 54.897 IS WORN AROUND ENTIRE CIRCUMFERENCE 0.003 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014030300021](https://openairdocs.org/sdr/REXA2014030300021.md): Fitting · cracked · Feb 28, 2014 · N8674A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INBOARD & OTBD CLIPS ON FLOOR SUPPORT BEAM CRACKED AT FS 280, RBL9. REPAIRED IAW SRM 51-11-20, 51-42-21, 51-31-59, 51-24-36, 51-21-11, 51-25-16 & 51-41-02.
- [SDR REXA2014030300020](https://openairdocs.org/sdr/REXA2014030300020.md): Fitting · cracked · Feb 28, 2014 · N8674A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OUTBOARD CLIP CRACKED ON FLOOR SUPPORT BEAM AT FS 280, LBL 9. REPAIRED IAW SRM 51-11-20, 51-42-21, 51-31-59, 51-24-36, 51-21-11, 51-25-16 & 51-41-02.
- [SDR REXA2014020600184](https://openairdocs.org/sdr/REXA2014020600184.md): Mechanism · obstructed · Feb 6, 2014 · N8674A · Cndair CL6002B19 · Passenger/Crew Doors
  > BOARDING DOOR HANDLE IS VERY DIFFICULT TO MOVE TO OPEN DOOR. CLEARED ICE FROM DOOR LATCH MECHANISM. OPERATIONS CHECKED DOOR IAW AMM 52-11-00, HANDLE MOVES OK.
- [SDR REXA2013021900356](https://openairdocs.org/sdr/REXA2013021900356.md): Structure · contaminated · Feb 19, 2013 · N8674A · Cndair CL6002B19 · APU Cowling/Containment
  > ON FLIGHT 4096 (DTW TO TYS) STRONG ODOR OF FUEL EACH TIME TRANSFER PACKS TO APU BOTH WHILE ON THE GROUND AND AIRBORNE. FOUND RESIDUAL FUEL IN APU COMPARTMENT. CLEANED COMPARTMENT. LEAK CHECKED APU-NO LEAKS NOTED. RUN LEFT & RIGHT PACKS FROM ENGINES AND APU
- [SDR REXA2012111101514](https://openairdocs.org/sdr/REXA2012111101514.md): Bulkhead · damaged · Nov 7, 2012 · N8674A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FORWARD SIDE OF FS 621 BULKHEAD HAS 4 EACH SCREW MARKS IN A LINE APPROX 30 INCHES ABOVE THE FLOOR. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.
- [SDR REXA2012083101306](https://openairdocs.org/sdr/REXA2012083101306.md): Drain Line · disconnected · Aug 31, 2012 · N8674A · Cndair CL6002B19 · Humidity Control System
  > LEFT PACK IS BLOWING HEAVY CONDENSATION OBSCURING COCKPIT SIDE WINDOWS. FOG ALSO OBSCURING FLOOR PATH IN CABIN, UNABLE TO SEE FLOOR OR EGRESS PATH LIGHTS. FOUND DRAIN LINE ON WATER SEPARATOR DISCONNECTED, RECONNECTED IAW AMM 21-50-00. OPS CHECKS GOOD.
- [SDR REXA2012071601163](https://openairdocs.org/sdr/REXA2012071601163.md): Battery Pack · discharged · Jul 16, 2012 · N8674A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS ON FLOOR ARE INOPERATIVE. ALLOWED SYSTEM TO CHARGE. OPS SYSTEM NORMAL. OK FOR SERVICE PER FIM.
- [SDR REXA2012041600521](https://openairdocs.org/sdr/REXA2012041600521.md): Manifold · cracked · Apr 16, 2012 · N8674A · Cndair CL6002B19 · Air Distribution System
  > FOUND CRACK MANIFOLD MAINFEED UNDER CARGO FLOOR. C/W REO 601R-21-22-003 IAW WORK INSTRUCTION PROVIDED BY ENGINEERING, A/C OK FOR SERVICE.
- [SDR REXA2012040900419](https://openairdocs.org/sdr/REXA2012040900419.md): Intercostal · cracked · Apr 6, 2012 · N8674A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 621 TO 625 S14L CRACKED. REPAIRED IAW REO 601R-53-61-100.
- [SDR REXA2012040300418](https://openairdocs.org/sdr/REXA2012040300418.md): Floor Support · corroded · Apr 2, 2012 · N8674A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 27 FLOOR SUPPORT CORRODED AROUND NUT PLATES BETWEEN FS 574 AND FS 589. REPAIRED IAW REO 601R-53-00-005 AND REO 601R-53-61-3778.
- [SDR REXA2012040300417](https://openairdocs.org/sdr/REXA2012040300417.md): Floorbeam · corroded · Apr 2, 2012 · N8674A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL 9 FLOORBEAM TEE CAP CORRODED AROUND NUT PLATES AT FS 615 WITH 0.004" REMOVED. REPAIRED IAW REO 601R-53-00-005.
- [SDR REXA2012040300416](https://openairdocs.org/sdr/REXA2012040300416.md): Vane · worn · Apr 2, 2012 · N8674A · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE SLIDING BEAM HAS WEAR DAMAGE 0.4" X 0.08" X 0.002" DEEP AND 0.003" DEEP AT WS 59.5. REPAIRED IAW BOMBARDIER REO 601R-57-52-1891.
- [SDR REXA201100063](https://openairdocs.org/sdr/REXA201100063.md): Tape · missing · Jan 27, 2011 · N8674A · Cndair CL6002B19 · Smoke Detection
  > THE CREW REPORTED A SMOKE TOILET MESSAGE ON APPROACH. MAINTENANCE COMPLIED WITH PINNACLE AIRLINES MINIMUM WORK SCOPE FOR SMOKE VISUAL OR INDICATION. MAINTENANCE FOUND SPEED TAPE FOR LAV VENT MISSING, RE-APPLIED TAPE IAW PA 21-009. MAINTENANCE PERFORMED MAX
- [SDR REXA201000191](https://openairdocs.org/sdr/REXA201000191.md): Landing Gear · malfunctioned · Oct 4, 2010 · N8674A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE IN FLIGHT NOSE GEAR DID NOT COME UP WHEN SELECTED. RAN QRH GEAR CAME UP WITH PUMPS ON, GEAR CAME DOWN NORMALLY. FLT--3677 STA--MBS EMP--1 C/W PA 05-018A. FOUND NO DEFECT. FOUND PSEU CODES S22 DOWN FAR, S30 DOWN FAR, S31 DOWN FAR, S32 DOWN FAR,
- [SDR REXA201000184](https://openairdocs.org/sdr/REXA201000184.md): Warning System · malfunctioned · Oct 4, 2010 · N8674A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > OPERATING UNDER AN MEL FOR THE MAIN LANDING GEAR BAY OVERHEAT SYSTEM BEING DEFERRED. THIS MEL REQUIRED THE GEAR TO REMAIN DOWN FOR 10 MINUTES AFTER TAKEOFF. AFTER 10 MINUTES OF FLIGHT, RETRACTED THE GEAR AND THE NOSE GEAR FLAGGED RED DURING TRANSIT AND THE T
- [SDR REXA201000028](https://openairdocs.org/sdr/REXA201000028.md): Priority Valve · malfunctioned · Feb 27, 2010 · N8674A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING ON GEAR DOWN, NOSE GEAR INDICATED AMBER. DISCONTINUED APPROACH. RAN QRH. THREE GREEN, DOWN AND LOCKED INDICATION. NOTIFIED F/A, PAX, ATC, SOC/MOC. LANDED WITHOUT INCIDENT. NOSE GEAR PRIORITY VALVE MALFUNCTION, COMPUTER POSTED A NOSE
- [SDR REXA201000014](https://openairdocs.org/sdr/REXA201000014.md): Compressor · damaged · Jan 26, 2010 · N8674A · Cndair CL6002B19 · Turbine Engine Compressor Section
  > ON CLIMBOUT OF KDTW, THE RIGHT ENGINE WOULD NOT REACH TARGET POWER SETTING WITHOUT OVER TEMPING. THE FLIGHT CREW ELECTED TO RETURN TO KDTW. CENTER WAS NOTIFIED AND THE AIRCRAFT WAS VECTORED FOR A RETURN APPROACH. ON THE APPROACH THE RIGHT ENGINE WAS MAKING
- [SDR REXA200700057](https://openairdocs.org/sdr/REXA200700057.md): Connector · damaged · Jul 16, 2007 · N8674A · Cndair CL6002B19 · Light System Wiring
  > FOUND FORWARD FLOOR EMERGENCY LIGHTS INOP. REPLACED CONNECTOR OF EMERGENCY LIGHT STRIP.
- [SDR REXA200700040](https://openairdocs.org/sdr/REXA200700040.md): Flap System · unknown · Feb 4, 2007 · N8674A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL, SECOND OCCURRENCE WITHIN 72 HOURS.
- [SDR REXA200700028](https://openairdocs.org/sdr/REXA200700028.md): Flap System · unknown · Feb 3, 2007 · N8674A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 20 DEGREES. RESET PER AD 2006-12-21.
- [SDR REXA05002](https://openairdocs.org/sdr/REXA05002.md): Bpsu · failed · Jan 1, 2005 · N8674A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT ZERO AT FLIGHT LEVEL 310. QRH FOLLOWED, DECLARED EMERGENCY, UNEVENTFUL ZERO FLAPS LANDING MADE. SYSTEM WOULD NOT RESET. REPLACED RT BPSU (BRAKE POSITION SENSING UNIT) IAW AMM. OPERATIONALLY TESTED GOOD. (K)
- [SDR REXA04041](https://openairdocs.org/sdr/REXA04041.md): Control Unit · failed · Dec 4, 2004 · N8674A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT ZERO WHEN SELECTED TO 20 ON APPROACH. QRH FOLLOWED, DECLARED EMERGENCY WITH UNEVENTFUL LANDING. RESET SYSTEM AND PLACED FLAPS ON 72 HOUR MONITORING IAW AD98-20-01.
- [SDR REXA04037](https://openairdocs.org/sdr/REXA04037.md): Control System · failed · Nov 24, 2004 · N8674A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01.
- [SDR REXA04030](https://openairdocs.org/sdr/REXA04030.md): Flap · malfunctioned · Nov 9, 2004 · N8674A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. (NE02200500600)

## 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 = 'N8674A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8674A/reports

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