# Service difficulty reports: N545PB

A list on [N545PB](https://openairdocs.org/aircraft/N545PB.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 · 53 reports

- [SDR 1Q2R2026070400001](https://openairdocs.org/sdr/1Q2R2026070400001.md): Fitting · damaged · Jul 4, 2026 · N545PB · Cndair CL6002C10 · Fuselage Main, Frame
  > TEMPORARY TO PERMANENT REPAIR REQUIRED TO NOSE JACKING PAD. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH MHI RJ REO 670-53-11-1392 AND REO 670-53-11-2336.
- [SDR 1Q2R2026070300001](https://openairdocs.org/sdr/1Q2R2026070300001.md): Floorbeam · corroded · Jul 2, 2026 · N545PB · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > BS 280 ANGLE CORRODED. REPAIRED BY REPLACEMENT IAW REO 670-53-1-2319 REV-.
- [SDR 1Q2R2026070100003](https://openairdocs.org/sdr/1Q2R2026070100003.md): Structure · worn · Jul 1, 2026 · N545PB · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > DURING INSPECTION OF THE L/H AFT CORE COWL, WEAR DAMAGED WAS FOUND ON THE FORWARD FLANGE BEHIND THE P-SEAL AT 9 O'CLOCK POSITION. PERFORMED REPAIR IN ACCORDANCE WITH EA 5413-2026-0653, REV-.
- [SDR 1Q2R2026070100001](https://openairdocs.org/sdr/1Q2R2026070100001.md): Skin · damaged · Jul 1, 2026 · N545PB · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > SCREW HOLE ELONGATED ON FUSELAGE SKIN AT BS 1005.2 BETWEEN S22R AND S23R. PERFORMED PERMANENT REPAIR IAW REO 670-53-61-2722, REV-.
- [SDR 1Q2R2026061200002](https://openairdocs.org/sdr/1Q2R2026061200002.md): Plate · damaged · Jun 9, 2026 · N545PB · Cndair CL6002C10 · Fuselage Main, Structure
  > PSA AIRLINES REQUIRED PERMANENT REPAIR TO NO. 3 PITOT PROBE MOUNTING SCREW ON PLATE TEMPORARILY DISPOSED THROUGH MHI RJ REO 670-53-11-1820 REV. A, DATED OCTOBER 28, 2022. DUE TO ADDITIONAL DAMAGE NOTED DURING REPAIR PROCESS, A TEMPORARY REPAIR WAS PERFORMED IN
- [SDR 1Q2R2026061800001](https://openairdocs.org/sdr/1Q2R2026061800001.md): Skin · gouged · Jun 4, 2026 · N545PB · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TWO (2) RIVETS FOUND PULLED THROUGH SKIN ON PATCH AT AFT LOWER FUSELAGE AREA (FS801.25 TO FS977.00, STR27). PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-128886 REV. 0, AND REO 670-53-00-830 REV. --.
- [SDR 1Q2R2026061500001](https://openairdocs.org/sdr/1Q2R2026061500001.md): Seat Track · damaged · Jun 4, 2026 · N545PB · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > OPERATOR REQUESTS PERMANENT REPAIR FOR MISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO) 670-53-11-210 REV. D, DATED JANUARY 13, 2020.
- [SDR 1Q2R2026070100002](https://openairdocs.org/sdr/1Q2R2026070100002.md): Skin · gouged · May 26, 2026 · N545PB · Cndair CL6002C10 · Leading Edge Devices
  > SLAT SS249.04, DAMAGED DURING OPERATION DUE TO PROTRUDING HARDWARE. PERFORMED REPAIR IAW REO 670-57-41-704 REV --,
- [SDR 1Q2R2026061100003](https://openairdocs.org/sdr/1Q2R2026061100003.md): Arm · gouged · May 26, 2026 · N545PB · Cndair CL6002C10 · Cargo/Baggage Doors
  > 2-OFF AREAS OF BLENDED GOUGE DAMAGE TO FWD BAGGAGE BAY DOOR FWD INNER HINGE ARM (DWG: LE670-39723, AL ALY 7050-T7451, REF). BLEND DIMENSIONS MEASURE: BLEND #1: 0.800" L X 0.150" W1 X 0.100" W2 X 0.083" MAX. DEPTH, REF. BLEND #2: 1.00" L X 0.030" W1 X 0.025"
- [SDR 1Q2R2026061100002](https://openairdocs.org/sdr/1Q2R2026061100002.md): Arm · gouged · May 26, 2026 · N545PB · Cndair CL6002C10 · Cargo/Baggage Doors
  > DURING INSPECTION OF FWD BAGGAGE BAY DOOR GOUGE DAMAGE WAS FOUND IN 3 LOCATIONS. DAMAGE WAS BLENDED ON 3 LOCATIONS. LOCATION #1 ZONE #1 INTO ZONE #2: ONE #1 L=2.00 X FWD FACE=.200 X INBD FACE=.300 ZONE #2 L= 1.00 X FWD FACE=.025 X INBD FACE=.200 LOCATION #
- [SDR 1Q2R2026070100004](https://openairdocs.org/sdr/1Q2R2026070100004.md): Aileron · nicked · May 4, 2026 · N545PB · Cndair CL6002C10 · Ailerons
  > TEMPORARY TO PERMANENT REPAIR (TRFKE00BS7ND) TO LEFT-HAND AILERON ASSEMBLY. REPAIR PERFORMED IAW REO 670-57-61-484 REV--.
- [SDR 1Q2R2026070600001](https://openairdocs.org/sdr/1Q2R2026070600001.md): Skin · cracked · Apr 25, 2026 · N545PB · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TEMPORARY TO PERMANENT REPAIR REQUIRED TO FUSELAGE SKIN BETWEEN FS280 AND FS310, AND STGR 12R TO 15R. PERMANENT REPAIR PERFORMED THROUGH SKIN REPLACEMENT. REPLACEMENT PERFORMED BY MHI RJ MRT (MIS-6317).
- [SDR VNAA2025080711101](https://openairdocs.org/sdr/VNAA2025080711101.md): Control Panel · faulted · Jul 30, 2025 · N545PB · Cndair CL6002C10 · Landing Gear Steering System
  > STEERING INOP IN FLIGHT, SHORTLY AFTER GEAR UP, PLANE CAME IN WITH NWS INOP CAUTION MSG. NWS INOP MESSAGE CAME ON IN FLIGHT WHEN TAKEOFF HAPPENED. WHEN PLANE LANDED NWS INOP WAS CLEARED BY CB RESET BY THE PILOTS PER THE MIPM. PILOTS TAXI PLANE TO GATE AFTER C
- [SDR VNAA202304251111](https://openairdocs.org/sdr/VNAA202304251111.md): Pin · unserviceable · Apr 22, 2023 · N545PB · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > WHILE CLIMBING OUT OF DTW THE FLIGHT CREW ENCOUNTERED AN ENGINE VIBE ISSUE. THEY THEN MADE THE DECISION TO RETURN TO DTW. REMOVED AND REPLACED FAN BLADE PINS IAW CRJ 700 AMM 12-20-72-640-803. VIBE CHECK GOOD.
- [SDR VNAA202205201111](https://openairdocs.org/sdr/VNAA202205201111.md): Handle · binding · May 17, 2022 · N545PB · Cndair CL6002C10 · Passenger/Crew Doors
  > MAIN CABIN DOOR INTERIOR HANDLE BINDS MID-RANGE WHEN OPENING DOOR. PERFORMED LUBRICATION OF PASS DOOR IAW CRJ 700 AMM 12-20-52-640-808/809. OPS CHECK IAW CRJ 700 AMM 52-11-00-PSA. NO FURTHER DEFECTS NOTED."
- [SDR VNAA202203259996](https://openairdocs.org/sdr/VNAA202203259996.md): Angle · cracked · Mar 25, 2022 · N545PB · Bombdr CL6002D15 · Doors
  > (N0304) DURING INSPECTION CRACK WAS FOUND ON AFT. SIDE OF PASSENGER DOOR - LOCATION AT FS 338.963 BETWEEN DOOR DATUM 4 AND 5. REPLACED PASSENGER DOOR AFT DRAG ANGLE AT FS 338.963 BETWEEN DOOR DATUM 4 AND 5 AS PER CRJ 700 SRM 51-42-06. OPS CHECK GOOD.
- [SDR VNAA202203259995](https://openairdocs.org/sdr/VNAA202203259995.md): Bar · cracked · Mar 25, 2022 · N545PB · Cndair CL6002C10 · Doors
  > (N0290) GALLEY SERVICE DOOR, STABILIZER BAR, UPPER PLATE, (REF IPC 52-41-27 ITEM 80, CRACKED AT AFT STABILIZER ARM ATTACHMENT POINT. REMOVED & REPLACED GALLEY SERVICE DOOR UPPER PLATE ASSEMBLY PER CRJ700 SRM51-40-00..
- [SDR VNAA202203259994](https://openairdocs.org/sdr/VNAA202203259994.md): Angle · cracked · Mar 25, 2022 · N545PB · Bombdr CL6002D15 · Empennage Structure
  > (N0071) THE R/H DRAG ANGLE WHERE THE VERTICAL STAB, FUSELAGE, AND APU FIREWALL MEET IS CRACKED. PERFORMED PERM. REPAIR ON R/H AFT DRAG ANGLE PER CRJ700 SRM 55-31-00-201-001-A01
- [SDR VNAA202203259993](https://openairdocs.org/sdr/VNAA202203259993.md): Angle · cracked · Mar 25, 2022 · N545PB · Bombdr CL6002D15 · Fuselage Structure (General)
  > (N0070) THE L/H DRAG ANGLE WHERE THE VERTICAL STAB, FUSELAGE, AND APU FIREWALL MEET IS CRACKED. ACCOMPLISHED REPAIR OF L/H DRAG ANGLE WHERE THE VERTICAL STAB, FUSELAGE AND APU FIREWALL MEET, BOTH FWD & AFT DRAG ANGLE IAW CRJ700 SRM 55-31-00-201-001-A01. TOP C
- [SDR VNAA202203259992](https://openairdocs.org/sdr/VNAA202203259992.md): Door · cracked · Mar 25, 2022 · N545PB · Bombdr CL6002D15 · Passenger/Crew Doors
  > PAX DOOR CRACKS ZONE 2. ACCOMPLISHED TASK CARD 52-11-04 AFT (ZONE 2) PAX DOOR CRACKS ZONE 2 AFT SIDE OF PAX DOOR PERM REPAIR OF ZONE 2 CRACK DAMAGE ON AFT SIDE OF PAX DOOR
- [SDR VNAA202203259991](https://openairdocs.org/sdr/VNAA202203259991.md): Slat · dented · Mar 25, 2022 · N545PB · Bombdr CL6002D15 · Leading Edge Devices
  > MX REPORTS A DENT IN THE LEADING EDGE OF THE LH #2 SLAT. ACCOMPLISHED PERMANENT REPAIR - LH SLAT #2 SKIN DENTED OTBD OF SS 241.75 IAW EA 22-C7-57-0212
- [SDR VNAA202202021111](https://openairdocs.org/sdr/VNAA202202021111.md): Bleed Valve · broken · Jan 31, 2022 · N545PB · Cndair CL6002C10 · Compressor Bleed Valve
  > DIVERSION TO CHO DUE TO FUEL LEAK ENROUTE. FLIGHT WAS ABLE TO LAND SAFELY IN CHO. UPON ARRIVAL INTO CHO, THE CREW NOTICED SMOKE COMING OUT OF THE RIGHT ENG. THEY DECIDED TO DEPLANE ON THE TAXIWAY AND CALL FIRE DEPARTMENT OVER. NO INJURIES WERE REPORTED AND ALL
- [SDR VNAA202107131113](https://openairdocs.org/sdr/VNAA202107131113.md): Spoiler Sys · faulted · Jul 11, 2021 · N545PB · Cndair CL6002C10 · Drag Control System
  > CREW RECEIVED OB SPOILERONS AND OB FLT SPOILERS CAUTIONS MESSAGES ENROUTE INTO DCA. CREW DECIDED TO DIVERT TO IAD DUE TO IAD HAVING LONGER RUNWAYS. FLIGHT ARRIVED INTO IAD WITHOUT FURTHER ISSUES. NO FURTHER INFORMATION AT THIS TIME. / TROUBLESHOT IAW CRJ700 FI
- [SDR VNAA2020102211101](https://openairdocs.org/sdr/VNAA2020102211101.md): Battery Pack · discharged · Oct 20, 2020 · N545PB · Cndair CL6002C10 · Emergency Lighting
  > BOTH EMERGENCY LIGHTS BY OVER WING EXIT WILL NOT STAY ILLUMINATED. EMERGENCY BATTERY CHARGE BY APU FOR 6 HOURS. PERFORM OPERATIONS CHECK OF EMERGENCY LIGHTS SYSTEM. OPERATIONS CHECK GOOD, IAW CRJ 900 AMM 33-51-00-710-802 A01 NO DEFECTS NOTED.
- [SDR VNAA202004139995](https://openairdocs.org/sdr/VNAA202004139995.md): Door Sill · corroded · Apr 13, 2020 · N545PB · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > RH FLOOR SUPPORT SEAL PLATE AT FS280 IS CORRODED. INSTALLED NEW FLOOR SILL AT FS280 RH IAW CRJ 700 SRM 51-42-21-001-001-A01,51-42-06-001-001-A01,51-42-10-001-001-A01, APPLIED TOPCOAT IAW CRJ 700 SRM 51-25-01-001-001-A01.
- [SDR VNAA202004139994](https://openairdocs.org/sdr/VNAA202004139994.md): Beam · cracked · Apr 13, 2020 · N545PB · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > LH FS280 BEAM IS CRACKED. INSTALLED NEW SERVICEABLE LH FS280.00 BEAM P/N:CC670-34094-15 IAW CRJ 700 SRM 51-42-06-001-001-A01,51-42-13-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR VNAA2018031299902](https://openairdocs.org/sdr/VNAA2018031299902.md): Door · cracked · Mar 12, 2018 · N545PB · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LINTEL, STRINGER 3L BETWEEN BS 280 & 295 CRACKED. PERFORMED A MAJOR REPAIR TO THE DOOR LINTEL IAW SB 670BA-53-040, REV C, PART B.
- [SDR VNAA2018031299901](https://openairdocs.org/sdr/VNAA2018031299901.md): Skin · dented · Mar 12, 2018 · N545PB · Cndair CL6002C10 · Trailing Edge Flaps
  > TWO DENTS ON THE LT INBD FLAP BOTTOM SKIN. DENTS ARE OUT OF LIMITS IAW SRM 57-52-01-101-001-A01. PERFORMED A CUTOUT IAW REO:678-57-52-009, REV A, COMPLIED WITH REO 670-57-52-009, REV A FOR THE SKIN REPAIR.
- [SDR VNAA2017080111101](https://openairdocs.org/sdr/VNAA2017080111101.md): Unknown · odor · Aug 1, 2017 · N545PB · Cndair CL6002C10 · Air Distribution System
  > WHEN THE CREW WAS DOING THEIR PREFLIGHT CHECKS THEY SMELLED A SMOKE ODOR COMING FROM THE CABIN. THE CREW REPORTED THE ISSUE TO MAINTENANCE CONTROL AND THEY DISPATCHED LOCAL MAINTENANCE TO THE AIRCRAFT. MAINTENANCE COULD NOT DUPLICATE THE SMOKE ODOR BUT DID GET
- [SDR VNAA20170716111](https://openairdocs.org/sdr/VNAA20170716111.md): Pcu · failed · Jul 16, 2017 · N545PB · Cndair CL6002C10 · Drag Control System
  > CREW HAD A OUTBOARD SPOILERONS AND OUTBOARD FLIGHT SPOILERS CAUTION MESSAGE. THEY DECLARED AN EMERGENCY ON DECENT AND LANDED WITH OUT ANY FURTHER ISSUES. MAINTENANCE REPLACED THE LT INBOARD AND OUTBOARD MULTI FUNCTION SPOILER PCU'S AND EVERYTHING OPS CHECKED G
- [SDR VNAA2017062111101](https://openairdocs.org/sdr/VNAA2017062111101.md): Warning System · false activation · Jun 21, 2017 · N545PB · Cndair CL6002C10 · Bleed Air Indicating System
  > WITH THE RT PACK ON DEFERRAL, HAD A LT BLEED DUCT WARNING MSG IN FLIGHT, CABIN LOST PRESSURE DUE TO WARNING MSG. PAX O2 MASK'S AUTO DEPLOYED AND USED. SMELL OF BURNING IN CABIN, SUSPECT FROM O2 GENERATORS. AIRCRAFT DIVERTED. COMPANY MX CREW INSP BLEED DUCT SYS
- [SDR VNAA2016091400033](https://openairdocs.org/sdr/VNAA2016091400033.md): Crossbeam · cracked · Oct 14, 2016 · N545PB · Cndair CL6002C10 · Fuselage Main, Structure
  > RIGHT SIDE OF CROSSBEAM AT BS 280, RBL 9 - 18 CRACKED. MAINTENANCE REMOVED AND REPLACED THE CROSSBEAM AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016091400034](https://openairdocs.org/sdr/VNAA2016091400034.md): Stringer · cracked · Sep 14, 2016 · N545PB · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > PASSENGER DOOR LINTEL STRINGER 3L AT BS 281 HAS VISUAL INDICATION OF A CRACK. MAINTENANCE PERFORMED A REPAIR IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016091400032](https://openairdocs.org/sdr/VNAA2016091400032.md): Web · corroded · Sep 14, 2016 · N545PB · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 280 LOWER WEB CORRODED ON LEFT HAND SIDE. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND LOWER WEB IAW THE AMM. THE AIRCRAFT WAS RELEASE FOR SERVICE.
- [SDR SIMA20150831009](https://openairdocs.org/sdr/SIMA20150831009.md): Skin · canning · Aug 31, 2015 · N545PB · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR FWD STAIR, SIDE SKIN HAS OIL CANNING. AFTER PERFORMING REPAIR TO PAX DOOR SIDE SKIN IAW ERS CR-52MR-436, NO OIL CANNING WAS FOUND.
- [SDR SIMA20150831007](https://openairdocs.org/sdr/SIMA20150831007.md): Frame · corroded · Aug 31, 2015 · N545PB · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 310.00 FRAME IS CORRODED JUST TO THE LT SIDE OF STRINGER 27. REPAIRED FS 310.00 FRAME JUST TO THE LT SIDE OF STRINGER 27 IAW SRM 53-21-06.
- [SDR SIMA20150301003](https://openairdocs.org/sdr/SIMA20150301003.md): Acm · seized · Mar 1, 2015 · N545PB · Cndair CL6002C10 · Cabin Cooling System
  > SMOKE IN CABIN, PERFORMED OPS CHECK OF LT PACKS IAW AMM 21-51-00. LT PACK CHECKED GOOD, CONFIRMED SMOKE TO BE FROM INOPERATIVE NR 2 PACK.. RT ACM APPEARS TO BE SEIZED & INOPERATIVE. REMOVED AND REPLACED RT ACM IAW AMM 21-51-08. OPS CHECKED GOOD.
- [SDR SIMA20150216002](https://openairdocs.org/sdr/SIMA20150216002.md): Fan · failed · Feb 16, 2015 · N545PB · Cndair CL6002C10 · Central Display
  > DISPLAY COOL FAN CAUTION MESSAGE. PLASTIC BURNING ODOR BEFORE CAUTION ILLUMINATED. REMOVED AND REPLACED NR 2 DISPLAY COOLING FAN IAW AMM 21-24-12. OPS CHECKED GOOD.
- [SDR SIMA20150211001](https://openairdocs.org/sdr/SIMA20150211001.md): Acm · failed · Feb 11, 2015 · N545PB · Cndair CL6002C10 · Cabin Cooling System
  > AFTER STARTING BOTH ENGS WITH THE APU STILL RUNNING SMOKE FILLED THE COCKPIT & CABIN. CABIN EVACUATED ONTO RAMP, EMER DECLARED. PERFORMED TROUBLESHOOTING IAW FIM TASK 21-22-00-810-806-A01 & FOUND THE LT PACK TO BE AT FAULT. R & R ACM IAW AMM 21-51-08. OPERA
- [SDR SIMA20141228005](https://openairdocs.org/sdr/SIMA20141228005.md): Holder · inoperative · Dec 28, 2014 · N545PB · Cndair CL6002C10 · Emergency Equipment
  > FIRST OFFICER`S FLASHLIGHT HOLDER INOPERATIVE. R & R FIRST OFFICER`S FLASHLIGHT ASSEMBLY IAW MM 25-61-02.
- [SDR SIMA20140730002](https://openairdocs.org/sdr/SIMA20140730002.md): Wire Harness · defective · Jul 30, 2014 · N545PB · Cndair CL6002C10 · Landing Gear System Wiring
  > ON TAKEOFF AT 90 KNOTS BRAKE OVERHEAT WARNING. WE ABORTED TAKEOFF & LT OTBD TEMP INDICATOR WAS RED, IT SHOWED NR 2. FIRE RESCUE CAME OUT & SAID TIRE LOOKED LOW BUT NO SIGNS OF FIRE OR MELTING FROM HEAT. TROUBLE SHOT & FOUND LT OTBD BRAKE HARNESS TO BE POSSI
- [SDR SIMA20140412001](https://openairdocs.org/sdr/SIMA20140412001.md): Controller · failed · Apr 12, 2014 · N545PB · Cndair CL6002C10 · Windshield/Door Rain/Ice Removal
  > RIGHT WINDOW HEAT FAILED AFTER TAKEOFF. IAW FIM TASK 30-41-00 INSPECTED RT WINDOW LEADS, S5 FOUND LOOSE. SECURED LEAD S5 IAW MM 56-11-01, NO FIX. R & R RT WINDOW TEMP CONTROLLER IAW MM 30-41-06. OPERATIONS CHECKED GOOD NO FURTHER DEFECTS NOTED AT THIS TIME
- [SDR SIMA20130729002](https://openairdocs.org/sdr/SIMA20130729002.md): Unknown · odor · Jul 28, 2013 · N545PB · Cndair CL6002C10 · Air Distribution System
  > LAVATORY SMOKE ON EICAS, F/A REPORTED SMOKE ODOR THROUGHOUT CABIN. INSPECTED LAVATORY SMOKE DETECTOR AND LIGHT, NO DEFECTS NOTED, PERFORMED OP CHECK OF LAVATORY SMOKE DETECTOR IAW AMM 26-16-00. SYSTEM CHECKED GOOD. OK TO RETURN TO SERVICE.
- [SDR SIMA20130728004](https://openairdocs.org/sdr/SIMA20130728004.md): Unknown · odor · Jul 28, 2013 · N545PB · Cndair CL6002C10 · Air Distribution System
  > LAV SMOKE ON EICAS. F/A REPORTED SMOKE ODOR THROUGHOUT CABIN. INSPECTED LAV SMOKE DETECTOR AND LIGHT. NO DEFECT NOTICED, PERFORMED OPS CHECK OF LAV SMOKE DETECTOR IAW AMM 26-16-00. SYS CHECKED GOOD AT THIS TIME. OK TO RETURN TO SERVICE.
- [SDR SIMA20130723003](https://openairdocs.org/sdr/SIMA20130723003.md): Unknown · unknown · Jul 23, 2013 · N545PB · Cndair CL6002C10 · Emergency Lighting
  > F/A NR 1 EMERGENCY LIGHTS SWITCH WILL NOT TURN EMERGENCY LIGHTS ON. PERFORM OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00, SYS CHECKED OK.
- [SDR SIMA20130401007](https://openairdocs.org/sdr/SIMA20130401007.md): Counterbalance · out of adjust · Apr 1, 2013 · N545PB · Cndair CL6002C10 · Passenger/Crew Doors
  > DURING MAINTENANCE INSPECTION FOUND THAT AFTER PRESSURIZATION CHECK THE PASSENGER DOOR WOULD NOT OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJSUTED THE PASSENGER DOOR’S FORWARD AND AFT COUNTERBALANCE ASSEMBLY IAW CRJ AMM 52-11-00. THE PASSENGER DOOR OPEN
- [SDR SIMA20130117009](https://openairdocs.org/sdr/SIMA20130117009.md): Battery · unserviceable · Jan 17, 2013 · N545PB · Cndair CL6002C10 · Emergency Lighting
  > DURING MAINTENANCE INSPECTION FOUND THE AFT EMERGENCY LIGHTS WOULD NOT SHUT OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE NR 4 BATTERY CHARGER AND BATTERY IAW CRJ 700 AMM 33-51-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETUR
- [SDR SIMA20121015012](https://openairdocs.org/sdr/SIMA20121015012.md): Flashlight · defective · Oct 15, 2012 · N545PB · Cndair CL6002C10 · Emergency Equipment
  > DURING MAINTENANCE INSPECTION FOUND THE AFT FLASHLIGHT HOLDER INOPERABLE. PLACED ON MEL 25-15. REMOVED AND REPLACED THE AFT FLASHLIGHT ASSEMBLY IAW CMM 25-60-11. MEL RESTORED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20121014006](https://openairdocs.org/sdr/SIMA20121014006.md): Flashlight · faulty · Oct 14, 2012 · N545PB · Cndair CL6002C10 · Emergency Equipment
  > ON FLIGHT 3745 THE CREW REPORTED ALL PASSENGER BUTTONS WERE INOPERABLE WITH AN ELECTRICAL ODOR IN CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ELECTRICAL ODOR COMING FROM FLASHLIGHT HOLDER (CHARGER) DEF AFT EMERGENCY FLASHLIGHT HOLDER MEL 25-15. REMO
- [SDR SIMA20120814006](https://openairdocs.org/sdr/SIMA20120814006.md): Flashlight · missing · Aug 15, 2012 · N545PB · Cndair CL6002C10 · Emergency Equipment
  > FLIGHT 4596, FOUND FWD FLIGHT ATTENDANT FLASHLIGHT IS MISSING. REPLACED FLASHLIGHT IAW AMM 21-61-02.

Next page: https://openairdocs.org/aircraft/N545PB/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 = 'N545PB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N545PB/reports

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