# Service difficulty reports: N305PQ

A list on [N305PQ](https://openairdocs.org/aircraft/N305PQ.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 · 92 reports

- [SDR REXA2025071600745](https://openairdocs.org/sdr/REXA2025071600745.md): Lamp · inoperative · Jun 28, 2025 · N305PQ · Cndair CL6002D24 · Emergency Lighting
  > ON WALK-AROUND FOUND RH AFT EMERGENCY LIGHT INOP R/R AFT RIGHT EMERGENCY LIGHT IAW AMM 33-51-15. OPS CHK GOOD.
- [SDR REXA2025022600224](https://openairdocs.org/sdr/REXA2025022600224.md): Module · inoperative · Feb 23, 2025 · N305PQ · Cndair CL6002D24 · Emergency Lighting
  > DURING LINE CHECK FOUND EMERGENCY SIGN LIGHT INOP. (DS158 EMERG EXIT SIGN WARDROBE.) DEFERRED CABIN EMERGENCY LIGHT IAW CRJ 900 MEL 33-51-1A CAT 'A' MOC #103619 NOTIFIED MMO2 UPDATED PLACARD INSTALLED. REMOVED AND REPLACED TM153 IAW ESPM 20-35-00.PERFORME
- [SDR REXA2024120201532](https://openairdocs.org/sdr/REXA2024120201532.md): Charger · inoperative · Nov 25, 2024 · N305PQ · Cndair CL6002D24 · Emergency Lighting
  > EMER LIGHTS ON EICAS MESSAGE NOT APPEARING WHEN PRESSING TEST SWITCH ON THE EPSU BATTERY PACK LOCATED IN THE AVIONICS BAY (PS35) R+R BATTERY CHARGER FOR EPSU BATTERY PACK IAW AMM 33-51-17. OPS CHECK GOOD AT THIS TIME.
- [SDR REXA2024102801065](https://openairdocs.org/sdr/REXA2024102801065.md): Liner · cracked · Feb 20, 2024 · N305PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PANEL 282CRW FOUND TO HAVE CRACK IN PANEL REMOVED AFT CARGO LINER 282CRW IAW CRJ-900 AMM 25-52-01-000-801-A08. REPAIRED COMPOSITE DAMAGE ON AFT CARGO LINER 282CRW. IAW C&D ZODIAC CMM 25-52-06 AND ENDEAVOR AIR EA. NO: CRJ925-16118 EA REV. IR DATE: 2/22/2024. I
- [SDR REXA2024102801064](https://openairdocs.org/sdr/REXA2024102801064.md): Angle · corroded · Feb 20, 2024 · N305PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR FLOOR SILL IS CORRODED BETWEEN F.S.310-349. REMOVED CORRODED FLOOR SILL KICKPLATE ANGLE P/N SH670-31875-7 AND CAP ANGLE P/N SH670-31821-5, INSTALLED NEW SERVICABLE ANGLES IAW CRJ 900 SRM 51-42-06-001-001-A01.
- [SDR REXA2024102801063](https://openairdocs.org/sdr/REXA2024102801063.md): Former · cracked · Feb 20, 2024 · N305PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > R/H AFT OVERWING EMERGENCY EXIT (S/N SB1400) TOP FORMER IS CRACKED AT SWITCH TARGET. REPAIRED RH AFT OVERWING EXIT DOOR IAW CRJ952-16067 REV IR DATED 2/16/24.
- [SDR REXA2024102801061](https://openairdocs.org/sdr/REXA2024102801061.md): Latch · inoperative · Feb 17, 2024 · N305PQ · Cndair CL6002D24 · Emergency Exits
  > WHILE PERFORMING FUNCTIONAL TEST OF CREW ESCAPE HATCH FOUND OUTER HANDLE TO BE STUCK. WILL NOT POP OUT WHEN THE PUSH BUTTON IS PRESSED. REMOVED AND INSTALLED NEW SERVICEABLE CREW ESCAPE LATCH ASSY. (INCLUDING HANDLE HOUSING) P/N H3419-35 IAW CRJ-900 SRM 51-42-
- [SDR REXA2024110601430](https://openairdocs.org/sdr/REXA2024110601430.md): Floorbeam · cracked · Feb 16, 2024 · N305PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > FLIGHT DECK FLOOR BEAM AT RBL 12 IS CRACKED IN AFT RADIUS AT FS 280. REPAIRED FLIGHT DECK FLOOR BEAM AT RBL 12 IAW MHIRJ REO# 690-53-11-1686
- [SDR REXA2024102801058](https://openairdocs.org/sdr/REXA2024102801058.md): Floorbeam · corroded · Feb 15, 2024 · N305PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RH 280 CROSSBEAM IS CORRODED ON FWD FACE. REMOVED AND INSTALLED NEW SERVICEABLE FS 280 CROSSBEAM P/N CC670-34094-2 IAW CRJ 900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01 AND SRM 51-42-22-001-001-A01
- [SDR REXA2024102801057](https://openairdocs.org/sdr/REXA2024102801057.md): Angle · corroded · Feb 14, 2024 · N305PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR FLOOR SILL MID CAP ANGLE IS CORRODED BETWEEN F.S.310 TO F.S.349 REMOVED AND INSTALLED NEW PASSENGER DOOR FLOOR SILL MID CAP ANGLE BETWEEN F.S.310 TO F.S.349 51-41-02-001-001-A01
- [SDR REXA2024102801056](https://openairdocs.org/sdr/REXA2024102801056.md): Floorbeam · corroded · Feb 14, 2024 · N305PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RIGHT HAND FLOOR SILL IS CORRODED AT F.S.280 REMOVED AND INSTALLED NEW RH FLOOR SILL P/N SH670-32172-11 AT FS280-319, IAW CRJ-900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01.
- [SDR REXA2024062000456](https://openairdocs.org/sdr/REXA2024062000456.md): Fitting · corroded · Feb 14, 2024 · N305PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WARDROBE FLOOR FITTING IS CORRODED AT F.S.310 AND LBL18. WARDROBE FLOOR FITTING @ F.S.310 AND LBL18 P/N SH670-31754-1 REQUIRES REPLACEMENT DUE TO MULTIPLE DEEP PITS. LOCATED AND DRILLED NEW WARDROBE FLOOR FITTING P/N SH670-31754-1 IN STGR 18, LBL18 IAW CRJ900
- [SDR REXA2024102801055](https://openairdocs.org/sdr/REXA2024102801055.md): Bulkhead Web · corroded · Feb 10, 2024 · N305PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > R/H LOWER BULKHEAD WEB AT FS 280 IS CORRODED IN SEVERAL PLACES REMOVED AND INSTALLED RH FS 280 LOWER WEB PN: 53-11-10-201-004-A01-2 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, AND 53-11-10-201-004-A01
- [SDR REXA2024102801054](https://openairdocs.org/sdr/REXA2024102801054.md): Access Panel · chafed · Feb 10, 2024 · N305PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > RH FLAP ACCESS PANEL 684EB IS CHAFED. REMOVED AND REPLACED 684EB
- [SDR REXA2024102801053](https://openairdocs.org/sdr/REXA2024102801053.md): Floorbeam · corroded · Feb 10, 2024 · N305PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > F.S.280 J-ANGLE IS CORRODED. REMOVED, LOCATED AND DRILLED NEW SERVICEABLE FWD J ANGLE ASSEMBLY P/N CC670-34095-1 AT FS 280 BETWEEN LBL 11 AND RBL 11 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND INSTALLED NEW SERVICEABLE FWD J ANGLE ASSEMBLY P/N CC670-34095-1 AT F
- [SDR REXA2024102801051](https://openairdocs.org/sdr/REXA2024102801051.md): Drag Angle · cracked · Feb 9, 2024 · N305PQ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > L/H AFT DRAG ANGLE IS CRACKED. REMOVED AND INSTALLED L/H AFT DRAG ANGLE WITH P/N AV670-21186-003 IAW CRJ-900 SRM 51-42-13-001-001-A01, 51-42-22-001-001-A01, 51-42-21-001-001-A01.
- [SDR REXA2024020900168](https://openairdocs.org/sdr/REXA2024020900168.md): Angle · cracked · Feb 8, 2024 · N305PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND STIFFENER ANGLE CRACKED AT FS 280 AND RBL 26 REMOVED DAMAGED STIFFENER ANGLE LOCATED AT FS 280 AND RBL 26 IAW CRJ-900 SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW STIFFENER ANGLE LOCATED AT FS 280 AND RBL 26 IAW CRJ-900 SRM 51-40-11-001-
- [SDR REXA2024020900167](https://openairdocs.org/sdr/REXA2024020900167.md): Angle · cracked · Feb 8, 2024 · N305PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STIFFENING ANGLE AT LBL 33 IS CRACKED. REMOVED DAMAGED STIFFENER ANGLE LOCATED AT RBL 33 AND FS 280 IAW CRJ-900 SRM 51-42-06-001-001-A01. FABRICATED, LOCATED AND DRILLED NEW STIFFENER ANGLE LOCATED AT FS 280 RBL 33 MATERIAL USED P/N S6144-1 IAW CRJ-900 SRM 51
- [SDR REXA2024102801050](https://openairdocs.org/sdr/REXA2024102801050.md): Floorbeam · deformed · Feb 7, 2024 · N305PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > L/H AND R/H RBL 9 FLOOR BEAM ANGLES COMMON TO FS 280 CROSSBEAM HAVE ELONGATED HOLES. LOCATED AND DRILLED NEW SERVICEABLE L/H AND R/H BL 9 FLOOR BEAM ANGLES COMMON TO FS 280 CROSSBEAM.P/N CC670-34269-9 AND CC670-34269-8 IAW CRJ 900 SRM 51-40-11-001-001-A01. IN
- [SDR REXA2024102801045](https://openairdocs.org/sdr/REXA2024102801045.md): Drag Angle · cracked · Feb 7, 2024 · N305PQ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > R/H AFT DRAG ANGLE IS CRACKED. REMOVED AND REPLACED RH AFT VERTICAL STAB DRAG ANGLE PN: AV670-21186-004 IAW CRJ900 SRM TASKS 51-40-11-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, AND 51-23-00-001-001-A01.
- [SDR REXA2024062000455](https://openairdocs.org/sdr/REXA2024062000455.md): Bracket · chafed · Feb 6, 2024 · N305PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > "AFT CARGO DOOR FWD BRACKET AT F.S. 1000.00 STGR 16L IS CHAFED. CHAFE IS APPROX 0.0625 LONG, 0.375 WIDE AND 0.015 DEEP. AFT CARGO DOOR FWD ROLLER GUIDE BRACKET AT F.S. 1000 IS IDENTIFIED AS P/N CC670-38812-1 AND HAS DEEP CHAFING ALONG EDGE AND CORNER. NO DAMAG
- [SDR REXA2024103001248](https://openairdocs.org/sdr/REXA2024103001248.md): Floorbeam · corroded · Feb 5, 2024 · N305PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LH CAP ANGLE AT 280 FLOOR BEAM IS CORRODED. UPON FURTHER INVESTIGATION, FOUND FS 280, LH CAP ANGLE TO BE FREE OF CORROSION. FOUND 2EA RIVETS ON LH CAP ANGLE TO BE CORRODED. REMOVED AND REPLACED 2EA RIVETS IAW CRJ 900 SRM 51-42-13-001-001-A01.
- [SDR REXA2024102801040](https://openairdocs.org/sdr/REXA2024102801040.md): Track · chafed · Feb 4, 2024 · N305PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > AFT CARGO DOOR AFT DOOR TRACK IS CHAFED IN TWO LOCATIONS 0.250 LONG, 0.250 WIDE AND 02.015 DEEP REMOVED DAMAGE IAW GREO 670-53-61-1296 REV-- DATED: 2018-03-28
- [SDR REXA2024102801038](https://openairdocs.org/sdr/REXA2024102801038.md): Access Panel · chafed · Feb 4, 2024 · N305PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > PNL 684HT IS CHAFED. CHAFED AREA ON ACCESS PANEL 684HT EVALUATED AND FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS IAW CRJ-900 SRM 57-52-01-101-001-A01. RECEIVED NEW SERVICEABLE VANE ACCESS PANEL 684HT (P/N CC670-14027-3), LOCATED AND DRILLED NEW PANEL IAW CRJ-90
- [SDR REXA2024022700226](https://openairdocs.org/sdr/REXA2024022700226.md): Skin · chafed · Feb 3, 2024 · N305PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > RH LEADING EDGE PANEL 631AR IS CHAFED. REMOVED THE DAMAGE ON RH LEADING EDGE PANEL 631AR IAW. CRJ900 SRM 51-12-00-001-001-A01. C/W AND ACCOMPLISHED EA# CRJ957-16065 REV IR. DATE 2/6/2024.
- [SDR REXA2022030700249](https://openairdocs.org/sdr/REXA2022030700249.md): Relay · inoperative · Mar 3, 2023 · N305PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > POWER ASSIST MOTOR PREVENTED MAIN CABIN DOOR FROM OPENING. REMOVED POWER TO OPEN DOOR, PULLED ASSIST MOTOR CIRCUIT BREAKER TO PREVENT DOOR FROM CLOSING. REPLACED RELAY K138 PASSENGER DOOR POWER ASSIST MOTOR OPERATIONAL TEST GOOD PER AMM 52-11-08. REF AMM 33-22
- [SDR REXA2020041600471](https://openairdocs.org/sdr/REXA2020041600471.md): Retainer · worn · Mar 11, 2020 · N305PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > LATE FINDING: WEAR ON PRESSURIZATION SEAL LOWER RETAINER AT FWD / CENTRAL BAGGAGE BAY DOOR. (CCD) LOWER SEAL RETAINER AT FWD/CENTRAL BAGGAGE BAY
- [SDR REXA2020041600507](https://openairdocs.org/sdr/REXA2020041600507.md): Hinge Fitting · corroded · Mar 9, 2020 · N305PQ · Cndair CL6002D24 · Ailerons
  > AWR; HIDDEN DAMAGE: [ DURING REMOTION OF FLANGED BUSHINGS IN HINGE FITTING #3 RELATED WITH NRC 00440 ]: CORROSION ON HINGE FITTING #3 STA. WS= 323 ( OUTBD LUG) AT RH AILERON. (AD).
- [SDR REXA2020041600506](https://openairdocs.org/sdr/REXA2020041600506.md): Hinge Fitting · corroded · Mar 9, 2020 · N305PQ · Cndair CL6002D24 · Ailerons
  > AWR; HIDDEN DAMAGE: [ DURING REMOTION OF FLANGED BUSHINGS IN HINGE FITTING #3 RELATED WITH NRC 00440 ]: CORROSION ON HINGE FITTING #3 STA. WS= 323 ( INBD LUG) AT RH AILERON. (AD).
- [SDR REXA2020041600505](https://openairdocs.org/sdr/REXA2020041600505.md): Hinge Fitting · corroded · Mar 9, 2020 · N305PQ · Cndair CL6002D24 · Ailerons
  > AWR; HIDDEN DAMAGE: [ DURING REMOTION OF FLANGED BUSHINGS IN HINGE FITTING #2 RELATED WITH NRC 00439 ]: CORROSION ON HINGE FITTING #2 STA. WS= 319 ( OUTBD LUG) AT RH AILERON. (AD).
- [SDR REXA2020041600504](https://openairdocs.org/sdr/REXA2020041600504.md): Hinge Fitting · corroded · Mar 9, 2020 · N305PQ · Cndair CL6002D24 · Ailerons
  > AWR; HIDDEN DAMAGE: [ DURING REMOTION OF FLANGED BUSHINGS IN HINGE FITTING #2 RELATED WITH NRC 00439 ]: CORROSION ON HINGE FITTING #2 STA. WS= 319 ( INBD LUG) AT RH AILERON. (AD).
- [SDR REXA2020041600503](https://openairdocs.org/sdr/REXA2020041600503.md): Hinge Fitting · corroded · Mar 9, 2020 · N305PQ · Cndair CL6002D24 · Ailerons
  > AWR; HIDDEN DAMAGE: [ DURING REMOTION OF FLANGED BUSHINGS IN HINGE FITTING #2 RELATED WITH NRC 00459 ]: CORROSION ON HINGE FITTING #2 STA. WS= 319 ( OUTBD LUG) AT LH AILERON. (AI)
- [SDR REXA2020041600502](https://openairdocs.org/sdr/REXA2020041600502.md): Hinge Fitting · corroded · Mar 9, 2020 · N305PQ · Cndair CL6002D24 · Ailerons
  > AWR; HIDDEN DAMAGE: [ DURING REMOTION OF FLANGED BUSHINGS IN HINGE FITTING #2 RELATED WITH NRC 00459 ]: CORROSION ON HINGE FITTING #2 STA. WS= 319 ( INBD LUG) AT LH AILERON. (AI)
- [SDR REXA2020041600501](https://openairdocs.org/sdr/REXA2020041600501.md): Hinge Fitting · corroded · Mar 9, 2020 · N305PQ · Cndair CL6002D24 · Ailerons
  > AWR; HIDDEN DAMAGE: [ DURING REMOTION OF FLANGED BUSHINGS IN HINGE FITTING #3 RELATED WITH NRC 00461 ]: CORROSION ON HINGE FITTING #3 STA. WS= 323 ( OUTBD LUG) AT LH AILERON. (AI)
- [SDR REXA2020041600500](https://openairdocs.org/sdr/REXA2020041600500.md): Hinge Fitting · corroded · Mar 9, 2020 · N305PQ · Cndair CL6002D24 · Ailerons
  > AWR; HIDDEN DAMAGE: [ DURING REMOTION OF FLANGED BUSHINGS IN HINGE FITTING #3 RELATED WITH NRC 00461 ]: CORROSION ON HINGE FITTING #3 STA. WS= 323 ( INBD LUG) AT LH AILERON. (AI) HINGE FITTING #3 STA. WS= 323 (
- [SDR REXA2020041600499](https://openairdocs.org/sdr/REXA2020041600499.md): Plate · cracked · Mar 8, 2020 · N305PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR; [ TASK R53520 STEP 7 ] CRACK ON PROTECTION PLATE AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) PROTECTION PLATE AT GALLEY SERVICE DOOR LOWER
- [SDR REXA2020041600498](https://openairdocs.org/sdr/REXA2020041600498.md): Bulkhead · corroded · Mar 8, 2020 · N305PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > AWR; HIDDEN CORROSION: [ DURING REMOTION OF BEAM 280 RELATED WITH NRC 00408 ]: CORROSION ON BULKHEAD WEB IN STA. FS= 280 BETWEEN 11LBL TO 14 LBL AT PAX CABIN FWD WET AREA. (W1) (CPAX) [ TASK R53520 STEP 7 ] TCI 53-10-219
- [SDR REXA2020041600497](https://openairdocs.org/sdr/REXA2020041600497.md): Bulkhead · corroded · Mar 8, 2020 · N305PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > AWR; HIDDEN CORROSION: [ DURING REMOTION OF BEAM 280 RELATED WITH NRC 00343 ]: CORROSION ON BULKHEAD WEB IN STA. FS= 280 BETWEEN 11RBL TO 14 RBL AT PAX CABIN FWD WET AREA. (W1) (CPAX) [ TASK R53520 STEP 7 ] TCI 53-10-219
- [SDR REXA2020041600496](https://openairdocs.org/sdr/REXA2020041600496.md): Fitting · corroded · Mar 8, 2020 · N305PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWRT; HIDDEN CORROSION: [ DURING REPAIR RELATED WITH NRC 00249 ]: CORROSION ON RH CLIP IN STA. FS= 277 TO FS= 280 AND 11RBL IN COCKPIT DOOR CUT-OUT AREA AT PAX CABIN FWD WET AREA. (W1) (CPAX) [ TASK R53520 STEP 7 ] CORROSION LEVEL 2. RH CLIP IN STA. FS= 2
- [SDR REXA2020041600495](https://openairdocs.org/sdr/REXA2020041600495.md): Fitting · corroded · Mar 7, 2020 · N305PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR; HIDDEN CORROSION: [ DURING REPAIR RELATED WITH NRC 00248 ]: CORROSION ON LH CLIP IN STA. FS= 277 TO FS= 280 AND 11LBL IN COCKPIT DOOR CUT-OUT AREA AT PAX CABIN FWD WET AREA. (W1) (CPAX) TASK R53520 STEP 7
- [SDR REXA2020041600494](https://openairdocs.org/sdr/REXA2020041600494.md): Canister · cracked · Mar 7, 2020 · N305PQ · Cndair CL6002D24 · Wing Miscellaneous Structure
  > INITIAL INSPECTION. CRACK ON SLAT TRACK CANISTER 1-3 INSIDE RH WING MAIN FUEL TANK WS 148.(AD). SLAT TRACK CANISTER 1-3 AT RH WING MAIN FUEL T
- [SDR REXA2020041600493](https://openairdocs.org/sdr/REXA2020041600493.md): Canister · cracked · Mar 7, 2020 · N305PQ · Cndair CL6002D24 · Wing Miscellaneous Structure
  > INITIAL INSPECTION: CRACK ON SLAT TRACK CANISTER 1-3 AT LH WING MAIN FUEL TANK WS 148. (SM)(AI). SLAT TRACK CANISTER 1-3 AT LH WING MAIN FUEL
- [SDR REXA2020041600492](https://openairdocs.org/sdr/REXA2020041600492.md): Fitting · corroded · Mar 7, 2020 · N305PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR; HIDDEN CORROSION: [DURING REMOTION OF BUSHING RELATED WITH TASK 900-35-710-902 STEP 5]: CORROSION ON LH/RH FITTINGS (AIRFRAME STRUCTURE) AT AFT NOSE LANDING GEAR CUTOUT. (FYT)
- [SDR REXA2020041600491](https://openairdocs.org/sdr/REXA2020041600491.md): Floor Panel · delaminated · Mar 7, 2020 · N305PQ · Cndair CL6002D24 · Fuselage Floor Panel
  > AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION^: DELAMINATION IN FLOOR PANEL NBR. 221ALF AND 231ALF AT PAX CABIN FWD WET AREA. (W1) (CPAX) FLOOR PANEL NBR. 231ALF AT PAX CABIN FWD WET AREA WAS REPAIRED PER CRJ 900 CMM ATA 53 COMTEK COMCMM-030 REV. T PAR. 10.
- [SDR REXA2020042100486](https://openairdocs.org/sdr/REXA2020042100486.md): Bracket · damaged · Mar 6, 2020 · N305PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: ELONGATED HOLE IN BRACKET SUPPORT BTW FS.319.70 AND FS. 333.00 AND STRINGER 3 LH AT PASSENGER DOOR SURROUND STRUCTURE. (L1) (CPAX) BRACKET SUPPORT BTW FS.319.70 AND FS. 333.00 AND STRINGER 3 LH WAS FABRICATED PER EA CRJ953-10545 REV. IR AN
- [SDR REXA2020041500490](https://openairdocs.org/sdr/REXA2020041500490.md): Crossbeam · corroded · Mar 6, 2020 · N305PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > HIDDEN DISCREPANCY: AFTER FLOOR PANEL SUPPORT ANGLE REMOVAL, CORROSION ON CROSSBEAM FS 280.00 AND LBL 12 WAS FOUND. IN REF NRC S/N 00285. (W1)
- [SDR REXA2020041500489](https://openairdocs.org/sdr/REXA2020041500489.md): Rib · cracked · Mar 6, 2020 · N305PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > INITIAL INSPECTION: CRACK ON RIB LEADING EDGE SS58.41 LH WING (AI). RIB LEADING EDGE SS58.41 LH WING WAS REPIARED PER REO 690-57-41-240 REV.
- [SDR REXA2020041500488](https://openairdocs.org/sdr/REXA2020041500488.md): Baffle · cracked · Mar 6, 2020 · N305PQ · Cndair CL6002D24 · Engine Thrust Reverser
  > INITIAL INSPECTION: CRACK ON BAFFLES 2E/A ON RH ENGINE LOWER THRUST REVERSER CASCADE FITTINGS.(MOT2) BAFFLES 2E/A ON RH ENGINE LOWER THRUST REVERSE
- [SDR REXA2020041500487](https://openairdocs.org/sdr/REXA2020041500487.md): Bracket · scratched · Mar 6, 2020 · N305PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: TOOL MARK IN BRACKET SUPPORT AT FS.319.70 AND STRINGER 7 RH AT GALLEY SERVICE DOOR SURROUND STRUCTURE. (R1) (CPAX) BRACKET SUPPORT AT FS.319.70 AND STRINGER 7 RH AT
- [SDR REXA2020041500485](https://openairdocs.org/sdr/REXA2020041500485.md): Bracket · corroded · Mar 6, 2020 · N305PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON BRACKET´S (2EA´S) IN FS= 533.00 TO 549.00 BTW STGR 26LH/24RH AT FWD BAGGAGE BAY. (CCD). CORROSION LEVEL 2. BRACKET IN FS 557 BTW STGR 26LH/24RH AT FWD BAGGAGE BAY WAS REPAIRE

Next page: https://openairdocs.org/aircraft/N305PQ/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 = 'N305PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N305PQ/reports

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