# Service difficulty reports: N299PQ

A list on [N299PQ](https://openairdocs.org/aircraft/N299PQ.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 · 91 reports

- [SDR REXA2024021900202](https://openairdocs.org/sdr/REXA2024021900202.md): Electrical Box · cracked · Feb 7, 2024 · N299PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > FOUND EXTERIOR POWER PLUG BOX SURROUND TO BE CRACKED. REMOVED EXTERNAL POWER PROVISIONS BOX (CC670-33401-3) IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. INSTALLED NEW EXTERNAL POWER PROVISIONS BOX (CC670-33401-3) IAW CRJ 900 SRM 51-42-06-001-
- [SDR REXA2024102901159](https://openairdocs.org/sdr/REXA2024102901159.md): Frame · deformed · Feb 2, 2024 · N299PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > FOUND 2EA ELONGATED HOLES ON FS 193 FOR EXTERIOR POWER PLUG BOX REPAIRED LOWER FRAME SECTOR, F.S.193 IAW ENDEAVOR AIR EA# CRJ953-16057 REV IR DATED 1/29/2024
- [SDR REXA2024102901158](https://openairdocs.org/sdr/REXA2024102901158.md): Vane · chafed · Feb 1, 2024 · N299PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > "R/H I/B FLAP VANE IS CHAFED ON THE LEADING EDGE APPROX 8 INCHES FROM O/B EDGE. BLENDED DAMAGE IAW CRJ900 SRM 57-52-01-101-001-A01 TABLE 1 AND CRJ900 SRM 51-12-00-001-001-A01 PARAGRAPH 7, EVALUATED AND FOUND TO BE OUT OF LIMITS IAW CRJ-900 SRM 57-52-01-101-001
- [SDR REXA2024102901157](https://openairdocs.org/sdr/REXA2024102901157.md): Skin · chafed · Feb 1, 2024 · N299PQ · Cndair CL6002D24 · Leading Edge Devices
  > R/H I/B SLAT HAS 2 AREAS OF CHAFFING ON AFT SIDE BY TELESCOPPING ANTI ICE DUCT. REPAIRED IAW ENDEAVOR AIR EA CRJ957-15996 REV IR DATE 1/16/2024.
- [SDR REXA2024102901156](https://openairdocs.org/sdr/REXA2024102901156.md): Floorbeam · corroded · Jan 25, 2024 · N299PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > F.S.280 CROSSBEAM J ANGLE IS CORRODED BETWEEN LBL12 AND RBL12 REMOVED AND INSTALLED NEW J ANGLE AT FS280 WITH P/N CC670-34095-3S IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2024102901155](https://openairdocs.org/sdr/REXA2024102901155.md): Panel · chafed · Jan 25, 2024 · N299PQ · Cndair CL6002D24 · Wing Structure
  > PANEL 684EB IS CHAFED REMOVED AND REPLACED NEW SERVICEABLE PANEL 684EB (PN CC670-1477-2) IAW CRJ900 SRM 51-40-11-001-001-A01
- [SDR REXA2024012400119](https://openairdocs.org/sdr/REXA2024012400119.md): Retainer · damaged · Jan 21, 2024 · N299PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PERM REPAIR PAX DOOR RETAINER. INSTALLED NEW PAX DOOR SEAL RETAINER P/N 601R318722-1 IAW CRJ-900 SRM 52-11-07-201-001-A01.
- [SDR REXA2024020500147](https://openairdocs.org/sdr/REXA2024020500147.md): Bracket · cracked · Jan 18, 2024 · N299PQ · Cndair CL6002D24 · Emergency Exits
  > R/H FWD OVERWING EMERGENCY EXIT DOOR TOP ALIGNMENT BRACKET IS CRACKED. REPAIRED RH FWD EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA#: CRJ952-16044 REV. IR DATED 1/27/2024.
- [SDR REXA2024020500146](https://openairdocs.org/sdr/REXA2024020500146.md): Bracket · cracked · Jan 18, 2024 · N299PQ · Cndair CL6002D24 · Emergency Exits
  > R/H AFT OVERWING EMERGENCY EXIT DOOR TOP ALIGNMENT BRACKET IS CRACKED. REPAIRED RH AFT EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA#: CRJ952-16043 REV. IR DATED 1/27/2024.
- [SDR REXA2024020500145](https://openairdocs.org/sdr/REXA2024020500145.md): Frame · cracked · Jan 18, 2024 · N299PQ · Cndair CL6002D24 · Emergency Exits
  > L/H FWD OVERWING EMERGENCY EXIT DOOR TOP ALIGNMENT BRACKET IS CRACKED. REPAIRED LH FWD EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA#: CRJ952-16042 REV. IR DATED 1/27/2024.
- [SDR REXA2024020500144](https://openairdocs.org/sdr/REXA2024020500144.md): Bracket · cracked · Jan 18, 2024 · N299PQ · Cndair CL6002D24 · Emergency Exits
  > LH AFT OVERWING EMERGENCY EXIT DOOR TOP ALIGNMENT BRACKET IS CRACKED. REPAIRED LH AFT EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA#: CRJ952-16041 REV. IR DATED 1/27/2024.
- [SDR REXA2024012500124](https://openairdocs.org/sdr/REXA2024012500124.md): Door Sill · corroded · Jan 18, 2024 · N299PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER SILL HAS MULIPLE AREAS OF CORROSION. INSTALLED A NEW LOWER SILL (P/N: MM670-35655-003). IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01 AND RESTORED SURFACE FINISH IAW CRJ 900 SRM (TR51-0068) 51-21-16-001-001-A01.
- [SDR REXA2024102901152](https://openairdocs.org/sdr/REXA2024102901152.md): Drag Angle · cracked · Jan 17, 2024 · N299PQ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > RH FWD VERTICAL STAB DRAG ANGLE IS CRACKED COMPLIED WITH REPAIR OF RH FWD DRAG ANGLE IAW CRJ900 SRM 55-31-00-201-001-A01
- [SDR REXA2024102901151](https://openairdocs.org/sdr/REXA2024102901151.md): Drag Angle · cracked · Jan 17, 2024 · N299PQ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > LH AFT VERTICAL STAB DRAG ANGLE IS CRACKED INSTALLED SERVICEABLE DRAG ANGLE AFT, LH SIDE WITH PN AV670-21186-003 IAW CRJ900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.
- [SDR REXA2024102901150](https://openairdocs.org/sdr/REXA2024102901150.md): Drag Angle · cracked · Jan 17, 2024 · N299PQ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > LH FWD VERTICAL STAB DRAG ANGLE IS CRACKED COMPLIED WITH REPAIR OF LH FWD DRAG ANGLE IAW CRJ900 SRM 55-31-00-201-001-A01
- [SDR REXA2024102901149](https://openairdocs.org/sdr/REXA2024102901149.md): Seal · torn · Jan 17, 2024 · N299PQ · Cndair CL6002D24 · APU Exhaust System
  > APU EXHAUST AFT B SEAL TORN AWAY FROM ATTACH FASTENERS LOWER SIDE BETWEEN 5:00 AND 7:00 POSITION. REMOVED AND REINSTALLED APU EXHAUST TAILCONE ASSEMBLY AS REQUIRED IAW CRJ 900 AMM TASK 53-85-00-000/400-801-A01. REMOVED AND REPLACED AFT APU EXHAUST BAND CLAMP,
- [SDR REXA2024102901096](https://openairdocs.org/sdr/REXA2024102901096.md): Panel · chafed · Jan 16, 2024 · N299PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > "L/H WING FLAP PANELS 584HT AND 584ET HAVE CHAFFING AND PAINT DAMAGE. BLENDED AND GRID CHAFFED AREA ON L/H WING FLAP PANELS 584HT AND 584ET ALLOWABLE DAMAGE 0.015"" IAW CRJ900 SRM 57-53-01-101-001-A02. PANEL 584HT FOUND TO BE IN LIMITS ORG..050"", REMAINING.
- [SDR REXA2024020900166](https://openairdocs.org/sdr/REXA2024020900166.md): Angle · corroded · Jan 16, 2024 · N299PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR SURROUND STRUCTURE, LOWER SILL MID CAP ANGLE IS CORRODED. REMOVED MID CAP ANGLE AS REQUIRED FOR REPLACEMENT IAW CRJ 900 SRM TASK 51-41-02-001-001-A01. INSTALLED NEW SERVICEABLE LOWER SILL MID CAP ANGLE (PN# SH670-31825-9S) IAW CRJ900 SRM 51-41
- [SDR REXA2024012500122](https://openairdocs.org/sdr/REXA2024012500122.md): Angle · cracked · Jan 16, 2024 · N299PQ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > RH AFT VERTICAL STAB DRAG ANGLE IS CRACKED. REPLACED RH AFT DRAG ANGLE USING P/N AV670-21186-004 IAW CRJ 900 SRM 51-42-13-001-001-A01, CRJ 900 SRM 51-42-21-001-001-A01, CRJ 900 SRM 51-42-22-001-001-A01.
- [SDR REXA2024020700159](https://openairdocs.org/sdr/REXA2024020700159.md): Stop Fitting · corroded · Jan 13, 2024 · N299PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > AFT CARGO DOOR UPPER AND LOWER STOP FITTING HAVE LIGHT SURFACE CORROSION. REMOVED DAMAGE FROM AFT CARGO DOOR FWD UPPER AND LOWER STOP FITTINGS BY COMPLYING WITH ALL STEPS OF ENDEAVOR AIR EA CRJ953-16015 REV IR DATED 1/24/2024 AND EA CRJ953-16016 REV IR DATED 1
- [SDR REXA2024102901095](https://openairdocs.org/sdr/REXA2024102901095.md): Panel · chafed · Jan 12, 2024 · N299PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > "L/H WING FLAP PANELS 584LB, 584JB, 584EB, AND 584GB HAVE CHAFFING AND PAINT DAMAGE. BLENDED AND GRIDDED CHAFED AREA ON 4EA L/H WING FLAP ACCESS PANELS 584LB, 584JB, 584EB, AND 584GB IAW CRJ900SRM 51-12-00-001-001-A01. PANELS 584LB, 584EB AND 584GB FOUND TO BE
- [SDR REXA2022122802728](https://openairdocs.org/sdr/REXA2022122802728.md): Light · inoperative · Dec 23, 2022 · N299PQ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHT ON LH SIDE 19TH PAX WINDOW INOPERATIVE. R & R EMERGENCY LIGHT LH SIDE IAW 33-51-15. OPS TESTED GOOD.
- [SDR REXA2022110102345](https://openairdocs.org/sdr/REXA2022110102345.md): None · inoperative · Oct 24, 2022 · N299PQ · Cndair CL6002D24 · Emergency Lighting
  > 14962
- [SDR REXA2020070600586](https://openairdocs.org/sdr/REXA2020070600586.md): Battery Pack · discharged · Jun 24, 2020 · N299PQ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHTS IN THE REAR OF THE AIRCRAFT INOP. R/R'D NR 2 & NR 3 EMER LIGHT BATTERY PACKS IAW AMM 33-51-17. ALL CHECKS GOOD. ACFT OK FOR SVC.
- [SDR REXA2020070600585](https://openairdocs.org/sdr/REXA2020070600585.md): Light · inoperative · Jun 19, 2020 · N299PQ · Cndair CL6002D24 · Emergency Lighting
  > FOUND EMERGENCY LIGHT EXTERIOR BY PAX DOOR INOP. REMOVED AND RELAMPED LIGHT BULB IAW AMM 33-51-15 OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.
- [SDR REXA2020030200233](https://openairdocs.org/sdr/REXA2020030200233.md): Frame · corroded · Feb 26, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > "INITIAL INSPECTION: CORROSION ON FRAME FS310 BTW STGR 26L TO 26R. (E/E)(TCI: 53-20-304). " "FRAME FS310 BTW STGR 26L TO 26R WAS REPAIRED PER EA CRJ953-10298 REV IR
- [SDR REXA2020030200257](https://openairdocs.org/sdr/REXA2020030200257.md): Access Panel · worn · Feb 25, 2020 · N299PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > "PART RACKS: WEAR ACCESS PANEL NBR 584EB AT LH INBD FLAP (SM). ""ACCESS PANEL 584EB WAS REPLACED FOR A ONE NEW P/N CC670-14177-1 PER CRJ900 SRM 57-52-01-001-001-A01 ITEM.10 "
- [SDR REXA2020030200253](https://openairdocs.org/sdr/REXA2020030200253.md): Cargo Track · corroded · Feb 25, 2020 · N299PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "PART RACKS: CORROSION ON RAILS (3EA) PN: BA690-30002-41, BA690-30002-43 AND BA690-30002-45 OF FWD CARGO COMPARTMENT.(SM)(CCD) " "CORROSION ON RAILS WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND REWORKED AREA ON RAIL PN: BA690-30002-45
- [SDR REXA2020030200252](https://openairdocs.org/sdr/REXA2020030200252.md): Cargo Track · corroded · Feb 25, 2020 · N299PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "PART RACKS: CORROSION ON RAILS (3EA) PN: BA690-30002-41, BA690-30002-43 AND BA690-30002-45 OF FWD CARGO COMPARTMENT.(SM)(CCD) ""CORROSION ON RAILS WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND REWORKED AREA ON RAIL PN: BA690-30002-45 IT
- [SDR REXA2020030200244](https://openairdocs.org/sdr/REXA2020030200244.md): Beam · cracked · Feb 25, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION: CRACKED LONGITUDINAL BEAM RBL 12 AT UNION WITH XBEAM 280-. " "LONGITUDINAL BEAM RBL 12 AT UNION WITH XBEAM 280 WAS REPAIRED PER REO 690-53-11-1221 REV. -- AFTER IMPLEMENTATION
- [SDR REXA2020030200243](https://openairdocs.org/sdr/REXA2020030200243.md): Beam · cracked · Feb 25, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION: CRACKED LONGITUDINAL BEAM LBL 12 AT UNION WITH XBEAM 280-. " "LONGITUDINAL BEAM LBL 12 AT UNION WITH XBEAM 280 WAS REPAIRED PER REO 690-53-11-1221 REV. -- AFTER IMPLEMENTATION
- [SDR REXA2020030200222](https://openairdocs.org/sdr/REXA2020030200222.md): Retainer · worn · Feb 25, 2020 · N299PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > "INITIAL INSPECTION: BENT AND WEAR ON FWD/AFT LOWER CORNERS ON INNER/OUTER SEAL RETAINER AT FWD BAGGAGE BAY DOOR. (C1). ""SEAL RETAINER ON FWD BAGGAGE BAY DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2020030200221](https://openairdocs.org/sdr/REXA2020030200221.md): Retainer · worn · Feb 25, 2020 · N299PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > "INITIAL INSPECTION: BENT AND WEAR ON AFT CENTER SEAL RETAINER AT CENTER BAGGAGE BAY DOOR. (C1). ""SEAL RETAINER AT CENTER BAGGAGE BAY DOOR WAS REPLACED PER CRJ-900 SRM51-42-06-001-001-A01.
- [SDR REXA2020030200220](https://openairdocs.org/sdr/REXA2020030200220.md): Retainer · worn · Feb 25, 2020 · N299PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > "INITIAL INSPECTION: BENT AND WEAR ON FWD/AFT LOWER CORNERS ON INNER/OUTER SEAL RETAINER AT CENTER BAGGAGE BAY DOOR. (C1). ""SEAL RETAINER ON CENTER BAGGAGE BAY DOOR WAS REPLACED PER CRJ-900 SRM51-42-06-001-001-A01
- [SDR REXA2020030200261](https://openairdocs.org/sdr/REXA2020030200261.md): Support Fitting · corroded · Feb 24, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "AWR; [ TASK R53520 STEP 7 ]; CORROSION ON SUPPORT FITTING BETWEEN FS 285 AND 17RBL AT PAX CABIN FWD WET AREA. (W1) (CPAX). ""SUPPORT FITTING WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-21-001-001-A01.
- [SDR REXA2020030200259](https://openairdocs.org/sdr/REXA2020030200259.md): Stringer · corroded · Feb 24, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "INITIAL INSPECTION: CORROSION ON STGR 24R BTW FS319 TO FS333. (E/E)(TCI: TCI: 53-20-304). " "STRINGER 24R BTW FS280 TO FS333 WAS REPLACED FOR A NEW ONE PER CRJ900SRM 51-42-06-001-001-A0
- [SDR REXA2020030200258](https://openairdocs.org/sdr/REXA2020030200258.md): Floor Panel · delaminated · Feb 24, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Floor Panel
  > "PART RACKS: DELAMINATION ON FLOOR PANELS 282JRF, 282KRF, 282FRF, 282GRF, 281BLF, 281CLF, 281DLF, 281GLF, AND 281JLF(ALSO HAS A CORRODED INSERT) AFT CARGO COMPARTMENT C-2 " "SUMMARY: FLOOR PANELS 282KRF, 281JLF, 281DL
- [SDR REXA2020030200235](https://openairdocs.org/sdr/REXA2020030200235.md): Frame · corroded · Feb 24, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > "INITIAL INSPECTION: CORROSION ON FRAME FS319 BTW STGR 26L TO 26R. (E/E)(TCI: 53-20-304). ""FRAME FS319 BTW STGR 26L TO 26R WAS REPAIRED PER EA N°: CRJ953-10299 REV IR.
- [SDR REXA2020030200234](https://openairdocs.org/sdr/REXA2020030200234.md): Stringer · corroded · Feb 24, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "INITIAL INSPECTION: CORROSION ON STGR 25R BTW FS310 TO FS319. (E/E)(TCI: 53-20-304). " "STRINGER 25R BTW FS 280 TO FS 333 WAS REPLACED FOR A NEW ONE PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20
- [SDR REXA2020030200231](https://openairdocs.org/sdr/REXA2020030200231.md): Doubler · corroded · Feb 24, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > "INITIAL INSPECTION: CORROSION ON DOUBLER OF FWD TCAS ANTENNA BTW FS 295 TO FS310, STGR 26L TO 26R. (E/E)(TCI:53-20-304). ""DOUBLER OF FWD TCAS ANTENNA BTW FS 295 TO FS310 WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2020030200228](https://openairdocs.org/sdr/REXA2020030200228.md): Intercostal · corroded · Feb 24, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION. CORROSION ON INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R. (TCI 53-20-313)(E/E). ""INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R WERE REPLACED FOR A NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2020030200227](https://openairdocs.org/sdr/REXA2020030200227.md): Intercostal · corroded · Feb 24, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION. CORROSION ON INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R. (TCI 53-20-313)(E/E). " "INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R WERE REPLACED FOR A NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A0
- [SDR REXA2020030200226](https://openairdocs.org/sdr/REXA2020030200226.md): Intercostal · corroded · Feb 24, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION. CORROSION ON INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R. (TCI 53-20-313)(E/E). ""INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R WERE REPLACED FOR A NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2020030200225](https://openairdocs.org/sdr/REXA2020030200225.md): Intercostal · corroded · Feb 24, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION. CORROSION ON INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R. (TCI 53-20-313)(E/E). " "INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R WERE REPLACED FOR A NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A0
- [SDR REXA2020030200224](https://openairdocs.org/sdr/REXA2020030200224.md): Strap · corroded · Feb 24, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PART RACKS: CORROSION ON FWD STRAPS AT ACCESS PANEL 193AB. (FUS). "STRAPS (2EA, P/N:CC670-39052-3S AND CC670-39052-4S) ON ACCESS PANEL 193AB WERE REPLACED FOR A NEW ONES PER CRJ900 SRM 51-42-10-001-001-A01. "
- [SDR REXA2020030200223](https://openairdocs.org/sdr/REXA2020030200223.md): Scuff Plate · dented · Feb 24, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "PART RACKS: SEVERAL DENTS ON SCUFF PLATE OF SOURROUND STRUCTURE AT THE FWD/CENTER BAGGAGE BAY DOORS (CCD). " "SCUFF PLATES (151MLW AND 151ZLW) OF SOURROUND STRUCTURE AT THE FWD/CENTER BAGGAGE BAY DOORS WERE REPLACED FOR A N
- [SDR REXA2020030200229](https://openairdocs.org/sdr/REXA2020030200229.md): Frame · corroded · Feb 23, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > "INITIAL INSPECTION: CORROSION ON FRAME FS295 BTW STGR 26L TO 26R. (E/E)(TCI:53-20-304). " "FRAME FS295 BTW STGR 26L TO 26R WAS REPAIRED PER EA N°: CRJ953-10297 REV IR.
- [SDR REXA2020030200246](https://openairdocs.org/sdr/REXA2020030200246.md): Frame · corroded · Feb 22, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > "INITIAL INSPECTION: CORROSION ON FRAME FS349 BTW STGR 26L TO 26R. (E/E)(TCI: 53-20-304). ""FRAME STA 349 BTW S23L TO S24R WAS REPLACED FOR A NEW ONE PER CRJ-900SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-
- [SDR REXA2020030200232](https://openairdocs.org/sdr/REXA2020030200232.md): Stringer · corroded · Feb 22, 2020 · N299PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "INITIAL INSPECTION: CORROSION ON STGR 26R BTW FS295 TO FS310. (E/E)(TCI: TCI: 53-20-304). " "STRINGER 26R BTW FS280 TO FS330 WAS REPLACED FOR A NEW ONE PER CRJ900SRM 51-42-06-001-001-A01 AND SRM 51-42-20-00
- [SDR REXA2020030200265](https://openairdocs.org/sdr/REXA2020030200265.md): Seal · worn · Feb 21, 2020 · N299PQ · Cndair CL6002D24 · Vertical Stabilizer, Plate/Skin
  > "POST-PATR RACKS: WORN AND LOOSE TEFLON SEAL AT VERTICAL STABILIZER ACCESS PANEL NBR 326DR ( EHV) " "SEAL AT VERTICAL STABILIZER ACCESS PANEL NBR 326DR WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A0

Next page: https://openairdocs.org/aircraft/N299PQ/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 = 'N299PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N299PQ/reports

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