# Service difficulty reports: N348PQ A list on [N348PQ](https://openairdocs.org/aircraft/N348PQ.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 · 64 reports - [SDR REXA2026031300237](https://openairdocs.org/sdr/REXA2026031300237.md): Seal · leaking · Feb 20, 2026 · N348PQ · Cndair CL6002D24 · Turbine Engine Oil System > WHILE AT FL 310 I NOTICED L OIL LOW. BEGAN MONITORING OIL INIDCATIONS. EVENTUALLY RECEIVED A L ENG OIL PRESS WARNING MESSAGE. FOLLOWED CRJ 900 QRH 1-20 AND 1-22 AS DIRECTED. SHUTDOWN LEFT ENGINE IN FLIGHT AS DIRECTED BY QRH. REPLACEED OF LT ENGINE C SUMP IN - [SDR REXA2025082500832](https://openairdocs.org/sdr/REXA2025082500832.md): Lamp · inoperative · Aug 21, 2025 · N348PQ · Cndair CL6002D24 · Emergency Lighting > RIGHT SIDE AFT EXTERIOR EMERGENCY LIGHT IS INOP REPLACED LAMP WITH NEW LAMP IAW AMM 33-51-15, OPS CHECK GOOD. P/N OFF/ON 8GH002473-08 - [SDR REXA2026072701189](https://openairdocs.org/sdr/REXA2026072701189.md): Handle · cracked · Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Passenger/Crew Doors > CRACK ON OUTER HANDLE OF PASSENGER DOOR LATCH MECHANISM OUTER HANDLE OF PASSENGER DOOR LATCH MECHANISM WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 - [SDR REXA2025031300318](https://openairdocs.org/sdr/REXA2025031300318.md): Attach Angle · cracked · Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DA - [SDR REXA2025031300316](https://openairdocs.org/sdr/REXA2025031300316.md): Attach Angle · cracked · Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND ON FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR S - [SDR REXA2025031300315](https://openairdocs.org/sdr/REXA2025031300315.md): Seat Track · corroded · Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON SEAT TRACK LOCATED BTW FS364.00 TO FS394.00 AND LBL9.00 DUE TO EXCESIVE CORROSION AT SEAT TRACK LOCATED BTW FS364.00 TO FS394.00 AND LBL9.00 FUSELAGE STRUCTURE PASSENGER CABIN WAS REPLACED PER CRJ-900 SRM 53-21-49-101-001-A01 AND CRJ-900 AMM 53 - [SDR REXA2025031300314](https://openairdocs.org/sdr/REXA2025031300314.md): Floor Support · corroded · Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON FLOOR SILL LOCATED BTWN FS 280.00/FS 295.00 AND RBL 43 DUE EXCESIVE DAMAGE ON FLOOR SILL LOCATED BTWN FS 280.00/FS 295.00 AND RBL 43 WAS REPAIRED PER CRJ-900 SRM 53-21-43-201-002-A01 - [SDR REXA2025031300313](https://openairdocs.org/sdr/REXA2025031300313.md): Support Plate · chafed · Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Wing Miscellaneous Structure > "WEAR ON PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH WING TRAILING EDGE (ROOT WING). PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH WING TRAILING EDGE (ROOT WING) WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42 - [SDR REXA2025031300312](https://openairdocs.org/sdr/REXA2025031300312.md): Fitting · chafed · Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Trailing Edge Flaps > "WEAR ON FLAP FITTING OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH WING TRAILING EDGE (ROOT WING). FLAP FITTING OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH WING TRAILING EDGE (ROOT WING) WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42-2 - [SDR REXA2025031300311](https://openairdocs.org/sdr/REXA2025031300311.md): Fitting · chafed · Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Trailing Edge Flaps > "WEAR ON FLAP FITTING OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH WING TRAILING EDGE (ROOT WING). FLAP FITTING OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH WING TRAILING EDGE (ROOT WING) WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42-2 - [SDR REXA2025031300310](https://openairdocs.org/sdr/REXA2025031300310.md): Support Plate · chafed · Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Wing Miscellaneous Structure > "WEAR ON PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH WING TRAILING EDGE (ROOT WING). PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH WING TRAILING EDGE (ROOT WING) WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42 - [SDR REXA2026072701173](https://openairdocs.org/sdr/REXA2026072701173.md): Hinge · cracked · Feb 17, 2025 · N348PQ · Cndair CL6002D24 · Cargo/Baggage Doors > FWD HINGE WAS FOUND CRACKED OF AFT BAGGAGE DOOR STEP PLATE ASSY. FWD HINGE OF AFT BAGGAGE DOOR STEP PLATE ASSY WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 - [SDR REXA2026072701188](https://openairdocs.org/sdr/REXA2026072701188.md): Bracket · corroded · Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION AT AFT LAVATORY WASTE LEVEL INDICATOR LIGHT SUPPORT OF AFT WASTE TANK (BTW STGR 24RH AND STGR 23RH, FS 927.00). CORROSION AT AFT LAVATORY WASTE LEVEL INDICATOR LIGHT SUPPORT OF AFT WASTE TANK (BTW STGR 24RH AND STGR 23RH, FS 927.00) WAS REMOVED PER C - [SDR REXA2026072701179](https://openairdocs.org/sdr/REXA2026072701179.md): Hinge · corroded · Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Fuselage, Door Hinge > CORROSION ON BOTH FITTINGS AT ACCESS PANEL 196ER. BOTH FITTINGS AT ACCESS PANEL 196ER WERE REPLACED PER CRJ900 AMM 52-45-01 (CONFIG A01) AND CRJ900 SRM 51-41-02-001-001-A01 - [SDR REXA2026072701178](https://openairdocs.org/sdr/REXA2026072701178.md): Hinge · corroded · Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Fuselage, Door Hinge > CORROSION ON BOTH FITTINGS AT ACCESS PANEL 196ER. BOTH FITTINGS AT ACCESS PANEL 196ER WERE REPLACED PER CRJ900 AMM 52-45-01 (CONFIG A01) AND CRJ900 SRM 51-41-02-001-001-A01 - [SDR REXA2026072701177](https://openairdocs.org/sdr/REXA2026072701177.md): Hinge · corroded · Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Fuselage, Door Hinge > CORROSION ON BOTH FITTINGS AT ACCESS PANEL 196ER. BOTH FITTINGS AT ACCESS PANEL 196ER WERE REPLACED PER CRJ900 AMM 52-45-01 (CONFIG A01) AND CRJ900 SRM 51-41-02-001-001-A01 - [SDR REXA2026072701176](https://openairdocs.org/sdr/REXA2026072701176.md): Access Panel · corroded · Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Service Doors > CORROSION ON BOTH FITTINGS AT ACCESS PANEL 196ER. BOTH FITTINGS AT ACCESS PANEL 196ER WERE REPLACED PER CRJ900 AMM 52-45-01 (CONFIG A01) AND CRJ900 SRM 51-41-02-001-001-A01 - [SDR REXA2025031300308](https://openairdocs.org/sdr/REXA2025031300308.md): Rib · cracked · Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACK ON MACHINED RIB LEADING EDGE SS57.16 AT RIGHT WING. MACHINED RIB LEADING EDGE SS57.16 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-468 REV. -- - [SDR REXA2025031300307](https://openairdocs.org/sdr/REXA2025031300307.md): Rib · cracked · Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING WAS REPAIRED PER REO 690-57-51-408 REV. -- - [SDR REXA2025031300306](https://openairdocs.org/sdr/REXA2025031300306.md): Rib · cracked · Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-407 REV. -- - [SDR REXA2025031300305](https://openairdocs.org/sdr/REXA2025031300305.md): Valve · chafed · Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > WEAR ON FLOTATION VALVE ALSO MISSING ITS RUBBER PAD LOCATED AT FS1098.20. FLOTATION VALVE WAS REPLACED PER CRJ-900 AMM 21-32-02-000-801-A01, AMM 21-32-02-400-801-A01 AND RUBBER PAD LOCATED AT FS1098.20 WAS INSTALLED PER CRJ-900 SRM 51-22-00-001-001-A01 - [SDR REXA2025020400118](https://openairdocs.org/sdr/REXA2025020400118.md): Relay · inoperative · Feb 2, 2025 · N348PQ · Cndair CL6002D24 · Emergency Lighting > DURING FIRST FLIGHT OF DAY CHECKS, EMERGENCY LIGHTS DID NOT TURN ON. R/R RELAY K198 IAW AMM 33-51-19. OPS CHECK GOOD. A/C OK FOR SVC - [SDR REXA2022050200309](https://openairdocs.org/sdr/REXA2022050200309.md): Unknown · inoperative · Apr 23, 2023 · N348PQ · Cndair CL6002D24 · Passenger/Crew Doors > UNABLE TO OPEN MAIN CABIN DOOR. CLEANED MEETING POINT LATCH ASSY AND VERIFIED GOOD OPERATION OF PASSENGER DOOR IAW CRJ 900 AMM 52-11-00. - [SDR REXA2022011000101](https://openairdocs.org/sdr/REXA2022011000101.md): Battery Pack · inoperative · Jan 3, 2023 · N348PQ · Cndair CL6002D24 · Emergency Lighting > FOUND GALLEY CEILING, PAX DOOR INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACK AT PS 35 IAW AMM 33-51-17 OPS CHECK GOOD. - [SDR REXA2021091000728](https://openairdocs.org/sdr/REXA2021091000728.md): Pivot · corroded · Sep 1, 2021 · N348PQ · Cndair CL6002D24 · Passenger/Crew Doors > "PAX DOOR UPPER AND LOWER HAND RAIL ATTACH POINTS CORRODED. " "BLENDED CORROSION ON UPPER AND LOWER HANDRAIL ATTACH POINTS AND AFTER FURTHER EVALUATION. NO DAMAGE ALLOWED IN AREA PER BOMBARDIER CMM 52-11-00-06. LOCATED AND INSTALLED 4EA NEW POST PIVO - [SDR REXA2021091000704](https://openairdocs.org/sdr/REXA2021091000704.md): Retainer · corroded · Aug 31, 2021 · N348PQ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors > "AVI DOOR AFT SEAL RETAINER IS CORRODED. " "REMOVED AND REPLACED SEAL RETAINER IAW CRJ 900 SRM 51-42-06-001- 001-A01. NO DEFECTS NOTED. - [SDR REXA2021091000726](https://openairdocs.org/sdr/REXA2021091000726.md): Lever · cracked · Aug 30, 2021 · N348PQ · Cndair CL6002D24 · Passenger/Crew Doors > "PAX DOOR ICE BREAK VENT LEVER CRACKED. " "REMOVED AND REPLACED ICE BREAK LEVER IAW MHIRJ SNIEO 601R31814 IDENTIFIER 501. OPS CHECK GOOD. ALSO USED SNIEO 601R31703-501 FOR INSTALL. WVAC EMP STAMP - [SDR REXA2021091000730](https://openairdocs.org/sdr/REXA2021091000730.md): Lever · damaged · Aug 29, 2021 · N348PQ · Cndair CL6002D24 · Passenger/Crew Doors > "FOUND HANDLE LEVER MOUNT HOLES DAMAGED. " "REMOVED AND REPLACED HANDLE CRJ 900 AMM 52-11-62-400-809-A02 NO DEFECTS NOTED. - [SDR REXA2021091000713](https://openairdocs.org/sdr/REXA2021091000713.md): Seat Track · corroded · Aug 29, 2021 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > RIGHT SIDE SEAT TRACK SEGMENT BETWEEN FS 785 TO FS 853.5 IS CORRODED. FABRICATED SEAT TRACKS @ FS 847-847+16 AND 847+16 TO 897 IAW REO 670-53-00-074 & INSTALLED SEAT TRACKS FS 785-897 IAW AMM 53-00-49-400-801-A12. - [SDR REXA2021091000711](https://openairdocs.org/sdr/REXA2021091000711.md): Crossbeam · corroded · Aug 29, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Main, Structure > "F.S. 280.00 CROSSBEAM IS CORRODED BETWEEN CROSSBEAM AND J-ANGLE. REMOVED L/H AND R/H CORRODED CROSSBEAM AT FS 280 IAW CRJ SRM 51-40-11-001-001-A01. INSTALLED NEW L/H AND R/H CROSSBEAM AT FS 280 IAW CRJ 900 SRM 51-42-20-001-001-A01 AND 51-42-22-001-001-A01 - [SDR REXA2021091000729](https://openairdocs.org/sdr/REXA2021091000729.md): Stringer · corroded · Aug 28, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > "STRINGER 25R IS CORRODED BETWEEN FS 310 AND FS 319.70. " "REMOVED CORROSION ON STR 25R BETWEEN FS 310 AND 319.70 IAW CRJ900 SRM 51-21-06-001-001-A01. REMOVED 0.042"", ORIGINAL MATERIAL THICKNESS IS 0.063"", REMAINING THICKNESS IS 0.021"". OUT OF LIMI - [SDR REXA2021091000722](https://openairdocs.org/sdr/REXA2021091000722.md): Angle · corroded · Aug 28, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > "PAX DOR UPPER SILL ANGLE IS CORRODED AT F.S. 319.70 BELOW THE FLANGE. " "BLENDED CAP SEAL FOUND OUT OF LIMITS REPLACED IAW SRM 51-42-06-001- 001-A01 AND 51-42-13-001-001-A01, 51-42-11-001-001-A01. FOUND SEALANT TO BE CURED AND PULLED FOD. WVAC - [SDR REXA2021091000721](https://openairdocs.org/sdr/REXA2021091000721.md): Frame · corroded · Aug 28, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Main, Frame > "RIB AT F.S. 295.00 IS CORRODED ON BOTH FWD & AFT SIDES BETWEEN STR STR 25R STR 25L. " "REPAIRED DAMAGED (CORRODED) AREA OF RIB AT FS 295 FWD AND AFT SIDES BETWEEN STR 25R AND STR 25L IAW CRJ 900 SRM 53-00- - [SDR REXA2021091000717](https://openairdocs.org/sdr/REXA2021091000717.md): Intercostal · corroded · Aug 28, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > "INTERCOSTAL FWD OF AVIONICS DOOR BETWEEN FS 364-FS 349 AT STRINGER 27L IS CORRODED. " "REMOVED AND REPLACED INTERCOSTAL AT 27L BETWEEN F.S. 349 AND F.S. 364 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-00 - [SDR REXA2021091000712](https://openairdocs.org/sdr/REXA2021091000712.md): Bulkhead Web · corroded · Aug 28, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead > "F.S. 280.00 BULKHEAD IS CORRODED ON AFT SIDE AT RH FLOOR SILL. REMOVED/FABRICATED/INSTALLED RH FS 280 WEB IAW SRM 53-11-10-201-004-A01. - [SDR REXA2021090900710](https://openairdocs.org/sdr/REXA2021090900710.md): Floorbeam · corroded · Aug 28, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam > "FS 280.00 CROSSBEAM 5 ANGLE IS CORRODED. " "REMOVED AND REPLACED 280 J ANGLE PN CC690-34095-1 IAW SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01. CORRECT PN CC670-34095-1. WVAC EMP STAMP # 703 MTC. - [SDR REXA2021090900708](https://openairdocs.org/sdr/REXA2021090900708.md): Skin · chafed · Aug 28, 2021 · N348PQ · Cndair CL6002D24 · Wing, Plate/Skin > PANEL 684EB HAS EXCESSIVE CHAFFING. LOCATED AND DRILLED NEW SERVICEABLE PANEL 684EB P/N CC670-14177-2 IAW CRJ 900 SRM 51-40-11-001-001-A01 REF M-212 FOR INSTALL. MASTER PANEL BOOK PAGE 110 OF 124. - [SDR REXA2021091000725](https://openairdocs.org/sdr/REXA2021091000725.md): Stringer · corroded · Aug 26, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > " STR 26L BTWN F.S. 310 AND F.S. 319 IS CORRODED THROUGH (100% HOLE) AROUND HYD LINE STAND OFFS. " " REMOVED, LOCATED, DRILLED AND INSTALLED A NEW SERVICEABLE STRINGER @ FS 280 - FS 333 26L IAW CRJ900 SRM 51-40-11- - [SDR REXA2021091000720](https://openairdocs.org/sdr/REXA2021091000720.md): Skin · corroded · Aug 26, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin > "A/C SKIN IS CORRODED IN MAIN AVIONICS BAY BETWEEN F.S. 280.00 & F.S. 295.00 AND BETWEEN STR 25R & STR 26R. " "REPAIRED A/C SKIN IN AVI BAY BETWEEN F.S 280-295 BETWEEN STR 25R & 26R IAW ENDEAVOR AIR, EA# CRJ 953-11928 REV IR D - [SDR REXA2021091000714](https://openairdocs.org/sdr/REXA2021091000714.md): Seat Track · corroded · Aug 19, 2021 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > "LEFT SIDE SEAT TRACK SEGMENT BETWEEN F.S. 744 TO F.S. 761 IS CORRODED. " "REMOVED, FABRICATED AND INSTALLED NEW L/H SIDE SEAT TRACK BETWEEN FS 744 TO FS 761 IAW CRJ 900 AMM 53-00-49-100-801-A12, SRM 53-41-49-101- 001-A02, AND 51-40-11-001-001-A01, 51-24-3 - [SDR REXA2021091000718](https://openairdocs.org/sdr/REXA2021091000718.md): Intercostal · corroded · Aug 19, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > "INTERCOSTAL FWD OF AVIONICS DOOR BETWEEN FS 364-FS 349 AT STRINGER 27R IS CORRODED. " "INSTALL INTERCOSTAL AND GUSSET ON 27R BETWEEN FS 349 AND FS 364 IAW CRJ900 SRM 51-40-11-001-001-A01, SRM 51-42-2 - [SDR REXA2021091000716](https://openairdocs.org/sdr/REXA2021091000716.md): Seat Track · corroded · Aug 16, 2021 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > "LEFT SIDE SEAT TRACK SEGMENT BETWEEN F.S. 672 - F.S. 720 IS CORRODED. " "REMOVED & REPLACED LH SEAT TRACK SEGMENT COMMOM TO FS 672-FS 720 IAW CRJ 900 AMM TASK 53-00-49-000-801-A12 AND 53-00-49-400-801-A12. - [SDR REXA2021091000715](https://openairdocs.org/sdr/REXA2021091000715.md): Seat Track · corroded · Aug 11, 2021 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > "RIGHT SIDE SEAT TRACK SEGMENT BETWEEN F.S. 744 TO F.S. 761 IS CORRODED. " "REMOVED FABRICATED AND INSTALLED SEAT TRACK IAW BOMBARDIER GRFO 670-53-00-074 AND AMM 53-00-49-400-801-A12 - [SDR REXA2021091000727](https://openairdocs.org/sdr/REXA2021091000727.md): Retainer · corroded · Aug 11, 2021 · N348PQ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors > "AVIONICS DOOR AFT RH SEAL RETAINER IS CORRODED " "REMOVED AND REPLACED WITH A NEW PART P/N CC670-38675-3$. AVIONICS DOOR SEAL RETAINER AFT R/H IAW CRJ SRM 51-42-06-001-001-A01. WVAC EMP STAMP # 738 MTC " - [SDR REXA2021091000724](https://openairdocs.org/sdr/REXA2021091000724.md): Seat Track · corroded · Aug 11, 2021 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > "CABIN SEAT TRACK AT LBL 9.0 IS CORRODED FS 374 TO 440 " "INSTALLED NEW TRACK LBL9 PN SH670-32249-3 IAW CRJ900 AMM 53-00-49-400- 801-A12 WVAC EMP STAMP # 769 MTC " - [SDR REXA2021091000723](https://openairdocs.org/sdr/REXA2021091000723.md): Seat Track · corroded · Aug 11, 2021 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > "CABIN SEAT TRACK AT RBL9.0 IS CORRODED FS 349 TO 388 TO INCLUDE FWD LAV MOUNTS. " "INSTALLED NEW SEAT TRACK AT RBL 9.0 PN SH670-32159-1 IAW CRJ900 AMM 53-00-49-400-801-A12. STA 349-485 RBL 9 WVAC EMP - [SDR REXA2021091000719](https://openairdocs.org/sdr/REXA2021091000719.md): Seat Track · gouged · Aug 11, 2021 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > "R/H OUTBD SEAT TRACK GOUGED IN 2 PLACES AT F.S. 549 & 565, RBL9. " "REMOVED SEAT TRACK IAW CRJ900 SRM 53-00-49-000-801-A12 AND INSTALLED NEW P/N SH690-33407-1 IAW CRJ900 SRM 53-00-49-400-801-A12, STA485-581 485-581 RBL9 WVAC EMP STAMP # 769 MTC - [SDR REXA2021090900706](https://openairdocs.org/sdr/REXA2021090900706.md): Drag Angle · cracked · Aug 10, 2021 · N348PQ · Cndair CL6002D24 · Vertical Stabilizer > L/H VERTICAL STABILIZER AFT DRAG ANGLE IS CRACKED. REMOVED LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01 AND 51-42-22-001-001-A01. LOCATED, DRILLED AND INSTALLED LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-13-0 - [SDR REXA2021090900705](https://openairdocs.org/sdr/REXA2021090900705.md): Drag Angle · cracked · Aug 10, 2021 · N348PQ · Cndair CL6002D24 · Vertical Stabilizer > "R/H VERTICAL STABILIZER AFT DRAG ANGLE IS CRACKED. REMOVED R/H AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01 AND 51-42-22-001-001-A01. LOCATED, DRILLED AND INSTALLED RH AFT DRAG ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-1 - [SDR REXA2020909100709](https://openairdocs.org/sdr/REXA2020909100709.md): Plate · chafed · Aug 9, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > "LH LOWER BLOW-OUT DOOR REINFORCING PLATE FOR LATCH CHAFED " "INSTALLED NEW SERVICEABLE REINFORCING PLATE FOR LH LOWER BLOW- OUT DOOR LATCH IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-40-11-001- 001-A01. WVAC EMP # 56392 Next page: https://openairdocs.org/aircraft/N348PQ/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 = 'N348PQ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N348PQ/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.