N295PQ

Service difficulty reports · 99

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

Query with SQL
duckdb -csv -c "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 = 'N295PQ' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR REXA2026030900165Channel · crackedCRACK & TOOL MARKS AT LOWER & AFT SUPPORT ANGLES OF EXTERNAL POWER RECEPTACLE. LOWER & AFT SUPPORT ANGLES OF EXTERNAL POWER RECEPTACLE WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND PER CRJ-900 SRM 51-42-10-001-001-A01Dec 20, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026030900164Support Angle · crackedCRACK & TOOL MARKS AT LOWER & AFT SUPPORT ANGLES OF EXTERNAL POWER RECEPTACLE. LOWER & AFT SUPPORT ANGLES OF EXTERNAL POWER RECEPTACLE WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND PER CRJ-900 SRM 51-42-10-001-001-A01Dec 20, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2024012900128Lamp · inoperativeDURING EMERGENCY EXIT LIGHT CHECK FWD EXTERIOR LIGHT BY PAX DOOR FOUND INOP. REMOVED AND REPLACED EMERGENCY FWD EXTERIOR LAMP REF AMM 33-51-15. OPS CHECK GOOD.Jan 28, 2024 · N295PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2022031700262Lamp · inoperativeLH REAR /AFT EXTERNAL EMERGENCY LIGHT IS INOP. R+R LH REAR/AFT EXTERNAL EMERGENCY LIGHT LAMP IAW CRJ-900 AMM 33-51-15.OPS CHECK GOOD. P/N ON/OFF:8GH002473-08Mar 16, 2023 · N295PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2019050300599Plate · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY: LEVEL CORROSION 2; PROTECTION PLATE AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS REPLACED PER SRM 51-41-May 3, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019050300584Frame · corroded[IN REFERENCE NRC 88] INITIAL INSPECTION: CORROSION ON FRAME, FS310 BETWEEN STR25L TO STR25R. (E/E) (TCI: 100-09, 09E4, 09E5) SUMMARY: LEVEL CORROSION 2; FRAME, FS310 BETWEEN STR25L TO STR25R WAS REPAIRED PER EA CRJ953-08842 REV. IR.May 3, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2019050300583Frame · corroded[IN REFERENCE NRC 88] INITIAL INSPECTION: CORROSION ON FRAME, FS319 BETWEEN STR26L TO STR26R. (E/E) (TCI: 100-09, 09E4, 09E5) SUMMARY: LEVEL CORROSION 2; FRAME AT FS319 BETWEEN STR26L TO STR26R WAS REPAIRED PER SRM 53-00-06-201-004-A01, FIG. 53-00-06-995-803.May 3, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2019050300573Skin · dentedINITIAL INSPECTION: SEVERAL DENTS ON LWR EXTERNAL SKIN BTW FLS=75.60 / FLS=84.20 AT LH INBOARD FLAP (AI) (SM) SUMMARY: LWR EXTERNAL SKIN BTW FLS=75.60 / FLS=84.20 AT LT INBOARD FLAP (AI) WAS REPAIRED PER SRM 57-52-01-201-005-A01, FIGURE 57-52-01-995-803 AND FMay 3, 2019 · N295PQ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2019050100581Stringer · corroded[IN REFERENCE NRC 88] INITIAL INSPECTION: CORROSION ON STR 25R BETWEEN FS333 TO FS349. (E/E) (TCI: 100-09, 09E4, 09E5) SUMMARY: LEVEL CORROSION 2. STR 25R BETWEEN FS333 TO FS349 WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR. 6 AND SRM 51-42-21-001-001-A01 PAR.May 1, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019042900582Frame · corroded[IN REFERENCE NRC 88] INITIAL INSPECTION: CORROSION ON FRAME , FS333 BETWEEN STR 27 TO STR 26R. (E/E) (TCI: 100-09, 09E4, 09E5) SUMMARY: LEVEL CORROSION 2; FRAME AT FS333 BETWEEN STR 27 TO STR 26R WAS REPAIRED PER SRM 53-00-06-201-004-A01, FIG. 53-00-06-995-8Apr 29, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2019042900580Frame · corroded[IN REFERENCE NRC 88] INITIAL INSPECTION: CORROSION ON FRAME FS 349 BETWEEN STR 26L TO STR 26R. (E/E) (TCI: 100-09, 09E4, 09E5) SUMMARY: LEVEL CORROSION 2; FRAME FS 349 BETWEEN STR 26L TO STR 26R WAS REPAIRED PER SRM 53-00-06-201-004-A01, FIG. 53-00-06-995-80Apr 29, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2019042600585Stringer · corroded[IN REFERENCE NRC 88] INITIAL INSPECTION: CORROSION ON STR25R BETWEEN FS280 TO FS333. (E/E) (TCI: 100-09, 09E4, 09E5) SUMMARY: LEVEL CORROSION 2; STR25R BETWEEN FS280 TO FS333 WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR. 6.Apr 26, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019042500600Stringer Splice · corroded[ IN REFERENCE NRC 0088 ] INITIAL INSPECTION: CORROSION ON STRINGER SPLICE 26R IN STA. FS= 327 TO FS= 337 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 LEVEL CORROSION 2. STRINGER SPLICE 26R IN STA. FS= Apr 25, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019042500587Door Sill · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON SILLS IN STA. FS= 280 TO FS= 319 BETWEEN 41RBL TO 46RBL AT PAX CABIN FWD WET AREA. (W1) (CPAX) LEVEL CORROSION 2. SILLS IN STA. FS= 280 TO FS= 319 BETWEEN 41RBL TO 46RBL AT PAX CABIN FWD WET AREA WApr 25, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019042400586Support Angle · corrodedINITIAL INSPECTION: CORROSION ON FLOOR PANEL SUPPORT ANGLE OF ACCESS PANEL 221ALF IN STA. FS= 280 BETWEEN 11LBL/RBL AT PAX CABIN FWD WET AREA. (W1) (CPAX) TCI 53-10-219 SUMMARY. FLOOR PANEL SUPPORT ANGLE OF ACCESS PANEL 221ALF IN STA. FS= 280 BETWEEN 11LBL/RBLApr 24, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019042400579Stringer · corroded[IN REFERENCE NRC 88] INITIAL INSPECTION: CORROSION ON STR 26R BETWEEN FS364 TO FS333. (E/E) (TCI: 100-09, 09E4, 09E5) SUMMARY: LEVEL CORROSION 2: STR 26R BETWEEN FS364 TO FS333. (E/E) WAS REPLACED PER SRM 51-42-06-001-001-A01.Apr 24, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019042300601Floor Support · corrodedINITIAL INSPECTION: CORROSION ON FLOORBEAM 27LBL IN STA. FS= 980 TO FS= 1055 AT AFT BAGGAGE BAY. (CCT) (TCI 100-15) LEVEL CORROSION 2. FLOORBEAM 27LBL IN STA. FS= 980 TO FS= 1055 AT AFT BAGGAGE BAY WAS REPAIRED PER SRM 53-00-41-201-001-A03 PAR. 5.B.Apr 23, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019042100595Support · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY: LEVEL CORROSION 2.PROTECTION PLATE SUPPORT IN STA. FS= 339 BETWEApr 21, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019042100588Seat Track · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAIL IN SECTION [ FS= 349 TO FS= 485, 9RBL ] AT PAX CABIN FWD WET AREA. (W1) (CPAX) SUMMARY: LEVEL CORROSION 2. FLOOR SEAT RAIL IN SECTION FS= 349 TO FS= 485, 9RBL PAX CABIN WAS REPLACED Apr 21, 2019 · N295PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019042100578Seat Track · corrodedINITIAL INSPECTION. CORROSION ON SIDE SEAT RAILS STR 15L BTW FS= 785 TO FS= 847+8. (SM)(CPAX)(TCI 100-20). SUMMARY. LEVEL CORROSION 2. SEAT RAILS STR 15L BTW FS= 785 TO FS= 847+8 WAS REPLACED PER AMM 53-00-49-400-801-A07.Apr 21, 2019 · N295PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019042100575Seat Track · corrodedINITIAL INSPECTION. CORROSION ON SIDE SEAT RAILS STR 15L, BTW FS 744 TO FS 761. (SM)(CPAX)(TCI 53-20-243) SUMMARY: LEVEL CORROSION 2. SEAT RAILS STR 15L, BTW FS 744 TO FS 761 WAS REPLACED PER AMM 53-00-49-400-801-A07 PAR 4.Apr 21, 2019 · N295PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019042100574Seat Track · corrodedINITIAL INSPECTION. CORROSION ON FLOOR SEAT RAILS LBL9 BTW FS= 847+16 TO FS= 977. (SM)(CPAX)(TCI 53-20-245). SUMMARY: LEVEL CORROSION 2. FLOOR SEAT RAIL IN SECTION FS= 847+16 TO FS= 977, 9LBL PAX CABIN WAS REPLACED PER AMM 53-00-49-400-801-A07.Apr 21, 2019 · N295PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019041900598Striker · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON LOWER STRIKER IN STA. FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) LEVEL CORROSION 2. LOWER STRIKER IN STA. FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICApr 19, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019041900597Angle · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON SUPPORT MOUNTING ANGLE IN STA. FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) LEVEL CORROSION 2. SUPPORT MOUNTING ANGLE IN STA. FS= 319 TO FS= 349 AND 41RBApr 19, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019041900596Support · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) LEVEL CORROSION 2. PROTECTION PLATE SUPPORT IN STA. FS= 346 BETWEEN 41RBLApr 19, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019041900594Support · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY: LEVEL CORROSION 2. PROTECTION PLATE SUPPORT IN STA. FS= 329 BETWApr 19, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019041900593Support · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) LEVEL CORROSION 2. PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41RBLApr 19, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019041900576Seat Track · corrodedINITIAL INSPECTION. CORROSION ON SIDE SEAT RAILS STR 15R BTW FS= 744 TO FS= 761.(SM)(CPAX)(TCI 53-20-318). SUMMARY: LEVEL CORROSION 2; SIDE SEAT RAILS STR 15R BTW FS= 744 TO FS= 761 WAS REPLACED PER AMM 53-00-49-400-801 PAR 4.Apr 19, 2019 · N295PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019041800577Seat Track · corrodedINITIAL INSPECTION. CORROSION ON SIDE SEAT RAILS STR 15R BTW FS= 785 TO FS= 847+8. (SM)(CPAX)(TCI 53-20-301). SUMMARY: LEVEL CORROSION 2; SIDE SEAT RAILS STR 15R BTW FS= 785 TO FS= 847+8, WAS REPLACED PER AMM 53-00-49-400-801 PAR 4.Apr 18, 2019 · N295PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019041700592Support Angle · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY: LEVEL CORROSION 2; PROTECTION PLATE SUPPORTS ANGLE IN STAApr 17, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019041700591Support Angle · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY: LEVEL CORROSION 2; PROTECTION PLATE SUPPORTS ANGLE IN STAApr 17, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019041700590Support Angle · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY: LEVEL CORROSION 2; PROTECTION PLATE SUPPORTS ANGLE IN STAApr 17, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019041700589Support Angle · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) LEVEL CORROSION 2; PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 322Apr 17, 2019 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2018090700809Battery · dischargedAFT FA FLASHLIGHT FOUND WITH SEAL BROKEN DEAD BATTERY. R&R AFT FLASHLIGHT BATTERY & SEAL IAW AMM 35-61-02, OPS CK GOOD. PN OFF ON P4-01-0021.Sep 6, 2018 · N295PQ · Cndair CL6002D24 · Emergency EquipmentSDR REXA2018062017519Light · missingFLOOR EMERGENCY LIGHTING MISSING IN FRONT OF GALLEY, NEAR THE LAVATORY SIDE. REPLACED THE EMERGENCY LIGHTING IAW AMM 33-51-01.Jun 17, 2018 · N295PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2017112801208Battery · inoperativeAFT FLASHLIGHT STATUS LIGHT DOES NOT BLINK. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-61-02. OPS CHECKED GOOD.Nov 28, 2017 · N295PQ · Cndair CL6002D24 · Emergency EquipmentSDR REXA2016111602222Seal · brokenDURING INSPECTION, NOTED WARDROBE PBE PACKAGE VACUUM SEAL BROKEN. INSTALLED A NEW PBE IAW AMM 35-31-06.Nov 16, 2016 · N295PQ · Cndair CL6002D24 · Emergency EquipmentSDR REXA2016111602221Seal · brokenDURING INSPECTION NOTED AFT FLT ATENDANT PBE PACKAGE VACUUM SEAL BROKEN. INSTALLED A NEW PBE IAW AMM CH 35-31-06.Nov 16, 2016 · N295PQ · Cndair CL6002D24 · Emergency EquipmentSDR REXA2016060400974Power Supply · inoperativeEMERGENCY LIGHTS IN CEILING, PAST ROW 9 ARE INOPERATIVE. LOWER EMER EXIT SIGN IN ROW 13 ARE INOPERATIVE. EMERGENCY EXIT SIGN IN CEILING AT ROW 13 INOPERATIVE. R & R THE NR 4 EMER POWER SUPPLY UNIT BATTERY PACK IAW AMM 33-51-17. OPERATIONS TEST OF EMER LIGHJun 4, 2016 · N295PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2016022900346Plate · corrodedSERVICE DOOR STEP PLATE IS BENT & HAS CORROSION ALONG THE BOTTOM EDGE. LOCATED & DRILLED NEW SERVICEABLE STEP PLATE IAW SRM 51-40-11-001-001-A01, PN SH670-31407-7.Feb 29, 2016 · N295PQ · Cndair CL6002D24 · Service DoorsSDR REXA2016022900345Channel · brokenC CHANNEL FOR 195DL IS BROKEN. R & R CHANNEL, PN CC690-39251-1 IAW EO R53573 REV 1 DATED 29 JAN 16.Feb 29, 2016 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2016022900344Support Channel · corrodedLEFT & RIGHT MLG SUPPORT CHANNEL ASSEMBLY FOR WHEEL BIN DIAPHRAGM, BOLT HOLE IS ELONGATED. REMOVED RED TAPE AS REQUIRED. REMOVED & INSTALLED LT & RT NEW SERVICEABLE SUPPORT CHANNEL ASSEMBLIES, PN CC670-85500-3 & CC670-85500-4 IAW SRM 51-40-11-001-001-A01 & 5Feb 29, 2016 · N295PQ · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR REXA2016022900343Angle · corrodedPASSENGER DOOR UPPER & LOWER SILL ANGLES ARE CORRODED LOWER IN THE RADIUS, UPPER AROUND SCREW HOLES. REPAIRED CORRODED UPPER & LOWER PAX DOOR SILL ANGLES. REFERENCE MWC 81529511 OP 50 FOR DETAIL OF WORK PERFORMED.Feb 29, 2016 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2016022900342Floor Support · corrodedFS 280 CROSSBEAM FLOOR SUPPORT, FWD J ANGLE HAS AREAS OF CORROSION. REMOVED CORROSION IAW SRM 53-00-00-101-001-A01 & 51-21-06-001-001-A01.Feb 29, 2016 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2016022900340Housing · crackedMAIN AVIONICS DOOR HANDLE HOUSING HAS A CRACK INDICATION NOTED ALL THE WAY AROUND THE BASE OF HANDLE SHAFT 100% FSH, FAILED NDT INSPECTION. REMOVED MAIN AVIONICS BAY DOOR IAW 52-42-00-000-801-A01. REMOVED & INSTALLED NEW SERVICEABLE AVI DOOR HANDLE HOUSING AFeb 29, 2016 · N295PQ · Cndair CL6002D24 · Electrical/Electronic Compartment DoorsSDR REXA2016022800341Vane · chafedTHE RIGHT INBD FLAP VANE IS CHAFED AT INBD MOST LOCATION ON PANEL 684ET. R & R RT INBD FLAP VANE AT THE MOST INBD LOCATION ON PANEL 684ET IAW SRM 51-40-11-001-001-A01.Feb 28, 2016 · N295PQ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2016012900119A/C Pack · faultyLEVEL AT 35000 WE WERE CLEARED TO 24000, AS WE STARTED DOWN FLIGHT ATTENDANTS ASKS TO WARM UP THE AFT SECTION, WE INCREASED LT PACK & STARTED TO SMELL FUMES, WE ALSO RECEIVED AFT LAVATORY SMOKE & MASTER CAUTION. FLIGHT CREW WENT ON OXYGEN & FOLLOWED SMOKE AT Jan 29, 2016 · N295PQ · Cndair CL6002D24 · Cabin Cooling SystemSDR REXA2015110601008Flashlight · inoperativeFWD EMER FLASHLIGHT INOPERATIVE. DEFERRED FWD FLASHLIGHT IAW MEL 25-61-4A, ENTERED INTO MM02 & PLACARD INSTALLED. R & R FLASHLIGHT & FLASHLIGHT MOUNTING BRACKETS IAW AMM 25-61-02. OPERATIONS CHECKED GOOD IAW AMM-25-61-00. CLEARED FROM MMO2 & PLACARD REMOVENov 5, 2015 · N295PQ · Cndair CL6002D24 · Emergency EquipmentSDR REXA2015070300634Unknown · odorFLIGHT ATTENDANT REPORTED BURNING SMELL IN FIRST CLASS CABIN. SMELLED LIKE BURNING POPCORN. INSPECTED ACFT, CHECKED FOR BURNING SMELL IN CABIN & COCKPIT, NO EVIDENCE OF BURN OR SMELL NOTED. ALSO SEE MINIMUM WORK SCOPE FOR SMOKE & FUMES IN CABIN, FLIGHT DECKJul 3, 2015 · N295PQ · Cndair CL6002D24 · Air Distribution System
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