# Service difficulty reports: N337PQ

A list on [N337PQ](https://openairdocs.org/aircraft/N337PQ.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 · 57 reports

- [SDR REXA2026020500041](https://openairdocs.org/sdr/REXA2026020500041.md): Packing · missing · Jan 24, 2026 · N337PQ · Cndair CL6002D24 · Turbine Engine Oil System
  > DURING CLIMB THRU FL250, RT OIL LEVEL LOW STATUS MESSAGE, 15% OIL LEVEL NO ACTION REQUIRED IAW QRH 0-23, OIL PRESSURE 80 PSI AT FL250, 67 PSI AT FL270, 55 PSI AT FL300, 30 PSI AT FL330, FOLLOWED BY RT ENG LOW WARNING, RAN QRH 1-20, RT ENG OIL PRESS. COMPLE
- [SDR REXA2024103001170](https://openairdocs.org/sdr/REXA2024103001170.md): Doubler · chafed · Oct 29, 2024 · N337PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > "CHAFF MARK F.S. 913-927 STR27 IN DOUBLER REMOVED DAMAGE DOUBLER ON FUSELAGE SKIN AT F.S. 913 - F.S. 927 STGR 27, IAW CRJ 900 SRM 51-42-21-001-001-A01. FABRICATED, LOCATED AND DRILLED NEW SERVICEABLE DOUBLER FROM FUSELAGE SKIN AT F.S. 913 - F.S. 927 STGR 27,
- [SDR REXA2024103101257](https://openairdocs.org/sdr/REXA2024103101257.md): Floorbeam · cracked · Oct 17, 2024 · N337PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RH CENTER COCKPIT FLOOR BEAM @ RBL 12.00 IS CRACKED AT 280 CONNECTION POINT. REPAIRED CONNECTION POINT. AT RBL12.00 AND FS280.00 IAW MHIRJ REO 690-53-11-1873 REV-- DATED 2024-10-17.
- [SDR REXA2024102500961](https://openairdocs.org/sdr/REXA2024102500961.md): Angle · corroded · Oct 17, 2024 · N337PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS280 J-ANGLE BETWEEN LBL12 AND RBL12 IS CORRODED. LOCATED AND DRILLED NEW J-ANGLE P/N CC670-34065-1SB, AT FS280 BETWEEN LBL12 TO RBL12, IAW CRJ-900 SRM 51-40-11-001-001-A01.REMOVED AND REPLACED J-ANGLE P/N CC670-34065-1SB, AT FS280 BETWEEN LBL 12 TO RBL 12
- [SDR REXA2024103101309](https://openairdocs.org/sdr/REXA2024103101309.md): Floorbeam · cracked · Oct 15, 2024 · N337PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RBL 11 COCKPIT FLOOR BEAM IS CRACKED AT F.S.280. REPAIRED CENTER COCKPIT FLOOR BEAM AT RBL12.00 AND FS280.00 IAW MHIRJ REO 690-53-11-1874 REV-- DATED 2024-10-17.
- [SDR REXA2024110601434](https://openairdocs.org/sdr/REXA2024110601434.md): Lug · cracked · Oct 14, 2024 · N337PQ · Cndair CL6002D24 · Emergency Exits
  > LH AFT OVERWING EMERGENCY EXIT DOOR (835) AFT UPPER LUG CRACKED AT BASE. REPAIRED IAW ENDEAVOR AIR ENDEAVOR AIR EA# CRJ952-17565, REV IR, DATED 10/19/2024.
- [SDR REXA2024110601433](https://openairdocs.org/sdr/REXA2024110601433.md): Lug · cracked · Oct 14, 2024 · N337PQ · Cndair CL6002D24 · Emergency Exits
  > RH FWD OVERWING EMERGENCY EXIT DOOR (843) AFT UPPER LUG CRACKED AT BASE. REPAIRED IAW ENDEAVOR AIR EA# CRJ952-17564, REV IR, DATED 10/19/2024.
- [SDR REXA2024110601432](https://openairdocs.org/sdr/REXA2024110601432.md): Door Frame · cracked · Oct 14, 2024 · N337PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > RH AFT OVERWING EMERGENCY EXIT DOOR (845) FWD AND AFT UPPER LUGS CRACKED AT BASE. REPAIRED IAW ENDEAVOR AIR ENDEAVOR AIR EA# CRJ952-17565, REV IR, DATED 10/19/2024.
- [SDR REXA2021062900445](https://openairdocs.org/sdr/REXA2021062900445.md): Retainer · corroded · Jun 20, 2021 · N337PQ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS DOOR SEAL DETERIORATION AND SEAL RETRAINERS CORRODED. REMOVED & REPLACED MAIN AVIONICS BAY DOOR SEAL RETAINERS & SEAL IAW CRJ SRM 51-42-06-001-001-A01 & AMM 52-42-07-400-801-A01.
- [SDR REXA2021062900446](https://openairdocs.org/sdr/REXA2021062900446.md): Retainer · corroded · Jun 20, 2021 · N337PQ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS DOOR SEAL DETERIORATION AND SEAL RETRAINERS CORRODED. REMOVED & REPLACED MAIN AVIONICS BAY DOOR SEAL RETAINERS & SEAL IAW SRM 51-42-06-001-001-A01 & AMM 52-42-07-400-801-A01.
- [SDR REXA2021062900423](https://openairdocs.org/sdr/REXA2021062900423.md): Door Sill · corroded · Jun 19, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER DOOR SILL CORRODED. LOCATED AND DRILLED REPLACEMENT SILL IAW SRM 51-40-11-001-001-A01. LEAK CHECK FAILED.
- [SDR REXA2021062900424](https://openairdocs.org/sdr/REXA2021062900424.md): Skin · gouged · Jun 14, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FUSELAGE OUTER SKIN GOUGED AT STGR 27 BETWEEN FS 897.00 AND FS 913.00. REPAIRED PER ENDEAVOR EA CRJ953-11713, REV. IR DATED 6/8/21. REPAIRED PER EA 953-11713 REV IR DATED 6-8-2021. REMOVED AND RE-INSTALLED BELOW FLOOR DISTRIBUTION DUCT IAW CRJ 900 AMM 21-23
- [SDR REXA2021062900429](https://openairdocs.org/sdr/REXA2021062900429.md): Floor Support · corroded · Jun 14, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOORBEAM AT LBL27 CORRODED IN MULTIPLE SPOTS FROM FS 977.00 TO FS 1098.00. COMPLIED WITH CRJ 900 SRM 53-00-44-201-001-A03 FOR REPLACEMENT OF LBL27 FLOORBEAM.
- [SDR REXA2021062900437](https://openairdocs.org/sdr/REXA2021062900437.md): Floor Support · corroded · Jun 14, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL AT RBL36 HAS 3 AREAS OF CORROSION BETWEEN FS 280.00 AND FS 319.70. REMOVED AND REPLACED R/H FLOOR SILL AND FLOOR SILL DOUBLER BETWEEN FS 280 TO FS 319.70 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. REMOVED AND REPLACED R/H
- [SDR REXA2021062900438](https://openairdocs.org/sdr/REXA2021062900438.md): Floor Support · corroded · Jun 14, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL AT RBL36 HAS 3 AREAS OF CORROSION BETWEEN FS 280.00 AND FS 319.70. REMOVED AND REPLACED R/H FLOOR SILL AND FLOOR SILL DOUBLER BETWEEN FS 280 TO FS 319.70 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. REMOVED AND REPLACED R/H FLO
- [SDR REXA2021062900447](https://openairdocs.org/sdr/REXA2021062900447.md): Longeron · corroded · Jun 14, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON RH LONGERON, AFT OF STRG 25R, BTW FS 333-349. REPAIRED CORROSION ON STR R25 BETWEEN FS 333 TO FS 349 IAW APPROVED REO 690-53-21-1380, REV.(P1).
- [SDR REXA2021062900443](https://openairdocs.org/sdr/REXA2021062900443.md): Bulkhead Web · corroded · Jun 12, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > RH FS280 BULKHEAD LOWER WEB IS CORRODED AT WL72 AND AT RBL 12 AND 42. BLENDED ON FS 280 BULKHEAD LOWER WEB ON R/H SIDE IAW CRJ 900 SRM 51-21-06-001-001-A01. CORROSION GOES THRU ENTIRE THICKNESS OF WEB AND REQUIRES REPLACEMENT. COMPLIED WITH STEPS 5(B)1-10 OF
- [SDR REXA2021062900430](https://openairdocs.org/sdr/REXA2021062900430.md): Handle · cracked · Jun 11, 2021 · N337PQ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS DOOR HANDLE HOUSING HAS INDICATIONS 100% FSH AROUND ENTIRE CIRCUMFERENCE AT THE BADE OF THE SHAFT HOUSING FAILED NDT INSPECTION. REMOVED UNSERVICEABLE MAIN AVIONICS DOOR HANDLE AND INSTALLED SERVICEABLE IAW CRJ900 AMM 52-42-03-000/400-801-A01 AN
- [SDR REXA2021062900441](https://openairdocs.org/sdr/REXA2021062900441.md): Hinge · gouged · Jun 11, 2021 · N337PQ · Cndair CL6002D24 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE DOOR SIDE FROM FRONT TO BACK LUG #17,#19,#22,#23,AND #24 ARE GOUGED. REMOVED & REPLACED PASSENGER DOOR HINGE IAW CRJ 900 SRM 52-11-01-201-02-A01.
- [SDR REXA2021062900420](https://openairdocs.org/sdr/REXA2021062900420.md): Placard · worn · Jun 10, 2021 · N337PQ · Cndair CL6002D24 · Placards and Markings
  > LH FORWARD AND AFT EMERGENCY DOORS EXTERNAL PLACARDS ON FLAPPER DOOR UNREADABLE PANEL 833 PANEL 835. INSTALLED LH FORWARD AND AFT EMERGENCY DOORS EXTERNAL PLACARDS ON FLAP DOOR IAW CRJ 900 AMM 20-60-11-400-801-A01.
- [SDR REXA2021062900421](https://openairdocs.org/sdr/REXA2021062900421.md): Placard · worn · Jun 10, 2021 · N337PQ · Cndair CL6002D24 · Placards and Markings
  > RH FORWARD AND AFT EMERGENCY DOOR EXTERNAL PLACARD ON FLAPPER TORN UNREADABLE PANEL 843 AND PANEL 845. INSTALLED FH FORWARD AND AFT EMERGENCY DOORS EXTERNAL PLACARDS ON FLAP DOOR IAW CRJ 900 AMM 20-60-11-400-801-A01. WVAC EMP # 56399
- [SDR REXA2021062900425](https://openairdocs.org/sdr/REXA2021062900425.md): Angle · cracked · Jun 10, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PANEL #196DR HAS AFT I/B ANGLE CRACKED. REMOVED CRACKED ANGLE, LOCATED AND INSTALLED NEW ANGLE, REMOVED AND REINSTALLED AFT FAIRING CHANNEL ON NEW FABRICATION JOINT STRAP IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 57-42-13- 001-001-A01.
- [SDR REXA2021062900434](https://openairdocs.org/sdr/REXA2021062900434.md): Stringer · corroded · Jun 10, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AVIONICS FLOOR STRUCTURE STR R26 IS CORRODED FROM FS 319.00 TO FS 333.00. REPAIRED AVIONICS BAY FLOOR STRUCTURE IAW APPROVED EA:CRJ953-11682.
- [SDR REXA2021062900448](https://openairdocs.org/sdr/REXA2021062900448.md): Skin · damaged · Jun 10, 2021 · N337PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > WHILE WORKING THE INSPECTION OF THE LH MLG RETRACT BRACKET FOR CORROSION (EO AR181403C) GEAR MADE CONTACT WITH THE WING PLANK, CAUSING DAMAGE TO THE WING PLANK. REPAIRED LH WING PLANK IAW REO 690-57-21-389 REV-. LPI SHOWED NO INDICATIONS AT THIS TIME.
- [SDR REXA2021062900433](https://openairdocs.org/sdr/REXA2021062900433.md): Frame · corroded · Jun 6, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT FS 295.00 IS CORRODED FROM STR L26 TO STR26. REMOVED CORROSION AT FRAME FS 295 FROM STR L26 TO R26 IAW CRJ SRM 53-00-06-201-006-A01. WVAC EMP # 56399
- [SDR REXA2021062900426](https://openairdocs.org/sdr/REXA2021062900426.md): Fitting · corroded · Jun 5, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER FWD FITTING AT FS 310.00 AT WL 72.50 IS CORRECT. REMOVED AND REPLACED SERVICE DOOR LOWER FWD FITTING IAW CRJ 900 SRM 51-42-21-001-001-A01 AT FS 319.00 WL 72.50.
- [SDR REXA2021062900439](https://openairdocs.org/sdr/REXA2021062900439.md): Angle · corroded · Jun 4, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS 280.00 FWD J ANGLE IS CORRODED. REMOVED AND INSTALLED NEW J ANGLE AT FS 280 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 P/N CC670-34095-15B. W
- [SDR REXA2021062900422](https://openairdocs.org/sdr/REXA2021062900422.md): Vane · chafed · Jun 3, 2021 · N337PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > LH INBOARD FLAP VANE IS CHAFED ON LEADING EDGE WS 38.00 INBOARD ACTUATOR ARM. REPLACED PANEL 584ET IAW CRJ 900 SRM 51-40-11-001-001-A01.
- [SDR REXA2021062900431](https://openairdocs.org/sdr/REXA2021062900431.md): Stringer · corroded · Jun 3, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AVIONICS BAY STRINGER R25 IS CORRODED FROM FS 280.00 TO FS 319.00. REMOVED AND INSTALLED NEW STRINGER AND SPLICE IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01 AT FS 280.00 TO FS 319.00 STR R25.
- [SDR REXA2021062900432](https://openairdocs.org/sdr/REXA2021062900432.md): Stringer Splice · corroded · Jun 3, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AVIONICS BAY STRINGER R25 IS CORRODED FROM FS 280.00 TO FS 319.00. REMOVED AND INSTALLED NEW STRINGER AND SPLICE IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01 AT FS 280.00 TO FS 319.00 STR R25.
- [SDR REXA2021062900436](https://openairdocs.org/sdr/REXA2021062900436.md): Attach Bracket · corroded · Jun 2, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > AVIONICS DOOR ANGLE ATTACH BRACKET ATTACHED TO STRINGER R26 CORRODED AT FS 364.00 TO FS 349.00. REMOVED AND INSTALLED NEW AVIONICS DOOR ANGLE ATTACH BRACKET PN SH670-32077-4 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A. 51-42-21-001-001-A01.
- [SDR REXA2021062900444](https://openairdocs.org/sdr/REXA2021062900444.md): Crossbeam · corroded · Jun 2, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > RH FS 280 CROSSBEAM IS CORRODED AT RBL 12 AROUND FASTENER HOLES. REMOVED AND INSTALLED SERVICEABLE RH 280 CROSSBEAM IAW CRJ 900 SRM 57-42-06-001-001-A01 AND 51-42-21-001-001-A01, LOCATED AND DRILLED PART IAW CRJ 900 SRM 51-40-11-001-001-A01 CIC AND PAINTED IA
- [SDR REXA2021062900435](https://openairdocs.org/sdr/REXA2021062900435.md): Stringer Splice · corroded · May 28, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AVIONICS BAY STRINGER R26 FROM FS 340.00 TO FS 364.00 CORRODED. REMOVED STRG 26R AT FS 364 TO 340. LOCATED, DRILLED AND REPLACED STRG 26R AT FS 340-364. REMOVED AND REPLACED SPLICE IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2021062900442](https://openairdocs.org/sdr/REXA2021062900442.md): Seat Track · corroded · May 28, 2021 · N337PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL9 IS CORRODED BETWEEN FS 349 AND FS 364. REMOVED AND REPAIRED SEAT TRACK P/N:SH670-32159-1 AT FS 349 RBL 9 IAW CRJ 900 AMM 53-00-49-000/400-801-A12.
- [SDR REXA2021062900427](https://openairdocs.org/sdr/REXA2021062900427.md): Intercostal · corroded · May 21, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STR R20 FS 310.00 TO FS 319.0 CORRODED. REMOVED, LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE INTERCOSTAL AT STR 20R FS 310-319 IAW CRJ 900 SRM 51-40-11-001-001-A01 51-42-06-001-001-A01. WVAC EMP STAMP # 712 MTC
- [SDR REXA2021062900428](https://openairdocs.org/sdr/REXA2021062900428.md): Cargo Track · corroded · May 21, 2021 · N337PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO BAY AT FS 661.00+16 STR 27 CARGO TIE DOWN PAD HAS SURFACE CORROSION ON TOP. REMOVED, LOCATED, DRILLED AND INSTALLED A NEW SERVICEABLE FWD CARGO BAY TIE DOWN AT FS 661.00+16 STR 27 IAW CRJ 900 SRM 51-42-06-001-001-51-42-06-001-001-A01, AND 51-42-21-0
- [SDR REXA2021062900440](https://openairdocs.org/sdr/REXA2021062900440.md): Seat Track · corroded · May 21, 2021 · N337PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SEAT TRACK AT APPROX. FS 379 LBL 9 IS CORRODED. REMOVED AND REPLACED SEAT TRACK PN:SH670-32249-3 AT FS 379 LBL 9 IAW CRJ 900 AMM 53-00-49-000/400-801-A12.
- [SDR REXA2021062900419](https://openairdocs.org/sdr/REXA2021062900419.md): Bracket · chafed · May 20, 2021 · N337PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD AND AFT HANDRAIL BRACKETS CHAFFED ON OUTER EDGES. LOCATED, DRILLED AND INSTALLED FWD AND AFT PAX DOOR HANDRAIL RETAINING BRACKETS P/N 601R317727-1 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND SRM 57-42-21-001-001-A01.
- [SDR REXA2020091600649](https://openairdocs.org/sdr/REXA2020091600649.md): Clamp · loose · Sep 8, 2020 · N337PQ · Cndair CL6002D24 · Cabin Temperature Control System
  > DETECTED BURNING SMELL WHEN COWL ANTI-ICE SELECTED ON, NO SMOKE, NO SIGN OF FIRE, NO ABNORMAL INDICATIONS. PERFORMED GVI OF AFT EQUIPMENT BAY AND FOUND CLAMP NOT SECURE ON TEMP CONTROL VALVE LT. INSP LT CONTROL VALVE FOR CORRECT INSTALLATION, IAW AMM 21-50-2
- [SDR REXA2018121171228](https://openairdocs.org/sdr/REXA2018121171228.md): Bulb · inoperative · Dec 7, 2018 · N337PQ · Cndair CL6002D24 · Emergency Lighting
  > PASSENGER DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP OKAY TO DEFER IAW MEL 33-51-2C PALCARD INSTALLED MMO2 UPDATED. MOC #95 770 NOTIFIED. CAT C*****RE-CLASSIFIED TO MEL 33-51-2A OKAY TO DEFER IAW MEL 33-51-2A PLACARD INSTALLED. MMO2 UPDATED.
- [SDR REXA2018081540685](https://openairdocs.org/sdr/REXA2018081540685.md): Battery · inoperative · Aug 14, 2018 · N337PQ · Cndair CL6002D24 · Emergency Equipment
  > F.A. SECONDARY FLASHLIGHT NOT WORKING. REPLACED THE BATTERY ASSY IAW CMM 25-60-01, OPS CHECKED GOOD.
- [SDR REXA2017121201251](https://openairdocs.org/sdr/REXA2017121201251.md): Access Panel · dented · Dec 12, 2017 · N337PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > LEFT INBOARD FLAP VANE ACCESS PANEL 584FT IS DENTED. LOCATED AND DRILLED A NEW FLAP ACCESS PANEL IAW SRM 51-40-11.
- [SDR REXA2017121001250](https://openairdocs.org/sdr/REXA2017121001250.md): Door · damaged · Dec 10, 2017 · N337PQ · Cndair CL6002D24 · Emergency Exits
  > REF NEF 25-26-19, CONTROL #3433546-1 OVER WING EXIT DOOR DAMAGE REPAIRED OVER WING EXIT DOOR IAW EA NO:CRJ925-06298 REV:I/R DATE: 12/4/17. WORK ACCOMPLISHED ON RS3E S/N:5899356, W/O:1015121, Z/I:2000-0023.
- [SDR REXA2017121001249](https://openairdocs.org/sdr/REXA2017121001249.md): Floorbeam · corroded · Dec 10, 2017 · N337PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > AFTER REMOVING FWD FLOOR SUPPORT ANGLE FS 280 FOUND LH FLOOR BEAM CORRODED REPAIRED THE LH FLOORBEAM AT FS280.00 IAW CRJ 900 AMM 20-21-00-410-801-A01, SRM 51-12-00-001-001-A01, 53-00
- [SDR REXA2017120901248](https://openairdocs.org/sdr/REXA2017120901248.md): Web · cracked · Dec 9, 2017 · N337PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT WEB HAS MULTIPLE CRACKS AT MID STEP UPPER RADIUS REPAIRED PAX DOOR AFT WEB IAW CRJ 900 SRM 52-11-04 AAR AP 403
- [SDR REXA2017120701247](https://openairdocs.org/sdr/REXA2017120701247.md): Floor Support · corroded · Dec 7, 2017 · N337PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SUPPORT SILL CORRODED FS 280.0 TO FS290.0. (DOT A-293 001) CUT AWAY DAMAGED AREA AND INSTALLED FLOOR SILL REPAIR IAW CRJ 900 SRM 53-21-43-991-806 AAR SM 107
- [SDR REXA2017120601246](https://openairdocs.org/sdr/REXA2017120601246.md): Web · cracked · Dec 6, 2017 · N337PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD WEB HAS MULTIPLE CRACKS AT MID STEP UPPER RADIUS REPAIRED PAX DOOR FWD WEB IAW CRJ 900 SRM 52-11-04 AAR SM 107
- [SDR REXA2017111901183](https://openairdocs.org/sdr/REXA2017111901183.md): Smoke Detector · false activation · Nov 19, 2017 · N337PQ · Cndair CL6002D24 · Smoke Detection
  > SMOKE WARNING IN THE AFT LAVATORY. PERFORMED TROUBLESHOOTING OF WIRES AND CONNECTOR. FOUND NO EVEIDENCE OF FIRE OR SMOKE. REMOVED AND REPLACED THE SMOKE DETECTOR IN THE AFT LAVATORY IAW AMM 26-16-01. OPS CHECKED GOOD.
- [SDR REXA2017092401031](https://openairdocs.org/sdr/REXA2017092401031.md): Pbe · unserviceable · Sep 24, 2017 · N337PQ · Cndair CL6002D24 · Emergency Equipment
  > COCKPIT PBE HAS LOST VACUUM. REMOVED AND REPLACED COCKPIT PBE IAW AMM 35-31-06.
- [SDR REXA2017090500972](https://openairdocs.org/sdr/REXA2017090500972.md): Smoke Detector · no test · Sep 5, 2017 · N337PQ · Cndair CL6002D24 · Smoke Detection
  > FWD LAVATORY SMOKE DETECTOR FAILED STEP 16. INTERRUPT SWITCH FAILED TO SILENCE ALARM. R & R THE SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECKED GOOD.

Next page: https://openairdocs.org/aircraft/N337PQ/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 = 'N337PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N337PQ/reports

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