# Service difficulty reports: N272PQ

A list on [N272PQ](https://openairdocs.org/aircraft/N272PQ.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 · 81 reports

- [SDR REXA2026030900222](https://openairdocs.org/sdr/REXA2026030900222.md): Door Sill · corroded · Feb 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON LOWER SILL ALSO ON SETTLEMENT AREA OF CARGO FLOOR 281JLF AT AFT BAGGAGE BAY DOOR CUT-OUT SURROUND STRUCTURE. DUE TO EXCESSIVE DAMAGE LOWER SILL OF AFT CARGO MUST BE REPLACE PER CRJ900 SRM 51-10-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-1
- [SDR REXA2026030900221](https://openairdocs.org/sdr/REXA2026030900221.md): Stringer · corroded · Feb 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 25RH IN STA. FS=295.00 TO FS= 310.00 AT MAIN AVIONICS COMPARTMENT DUE TO EXCESSIVE CORROSION ON STRINGER 25RH IN STA. FS=295.00 TO FS= 310.00 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-
- [SDR REXA2026030900216](https://openairdocs.org/sdr/REXA2026030900216.md): Hinge · excess play · Feb 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FREE PLAY ON HINGE & WEAR ON AFT FACE OF FLOATATION VALVE ON AFT ACCESSORIES COMPARTMENT HINGE OF FLOATATION VALVE ON AFT ACCESSORIES COMPARTMENT WAS REPLACED AND WEAR ON AFT FACE OF FLOATATION VALVE ON AFT ACCESSORIES COMPARTMENT WAS BLENDED OUT AND EVALUATE
- [SDR REXA2026030900214](https://openairdocs.org/sdr/REXA2026030900214.md): Attach Angle · cracked · Feb 19, 2026 · N272PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > CRACK ON ATTACHMENT ANGLE INNER SKIN TO AFT SIDE PANEL AT PASSENGER DOOR EXTERNAL STRUCTURE (NEX TO MOTOR ASSIST PULLEY BRACKET) ANGLE INNER SKIN TO AFT SIDE PANEL AT PASSENGER DOOR EXTERNAL STRUCTURE (NEX TO MOTOR ASSIST PULLEY BRACKET) WAS REPLACED PER CRJ 9
- [SDR REXA2026030900206](https://openairdocs.org/sdr/REXA2026030900206.md): Rib · cracked · Feb 19, 2026 · N272PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT LEFT WING. CRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT LEFT WING WAS REPAIRED PER REO 690-57-41-240 REV - -
- [SDR REXA2026030900230](https://openairdocs.org/sdr/REXA2026030900230.md): Support · cracked · Jan 27, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON BRACKET SUPPORT OF JB6 AT FORWARD EQUIPMENT COMPARTMENT. BRACKET SUPPORT OF JB6 AT FORWARD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2026030900158](https://openairdocs.org/sdr/REXA2026030900158.md): Skin · corroded · Jan 20, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL SKIN BTW FS 677.00 AND FS693.00 STGR 26L TO 26R BELOW FLOOR. CORROSION ON INTERNAL SKIN BTW FS 677.00 AND FS693.00 STGR 26L TO 26R BELOW FLOOR WAS REPAIRED PER REO 690-53-31-1118 REV - -
- [SDR REXA2026030900229](https://openairdocs.org/sdr/REXA2026030900229.md): Retainer · corroded · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > CORROSION ON INNER FACE SEAL RETAINER, AFTER REMOVAL AT FWR BAGGAGE DOOR DUE TO EXCESSIVE DAMAGE INNER FACE SEAL RETAINER WAS REPLACED PER SRM CRJ-900 SRM 51-10-06-001-001-A01 AND WILL BE INSTALLED UNDER NRC: 00101
- [SDR REXA2026030900228](https://openairdocs.org/sdr/REXA2026030900228.md): Retainer · damaged · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > REMOVE SEAL RETAINER AFT P/N: CC670-38662-5 OF MAIN AVIONICS COMPARTMENT DOOR TO BE INSTALLED ON A/C 921 THEN INSTALL SERVICEABLE PART. NEW SEAL RETAINER AFT P/N: CC670-38662-5S OF MAIN AVIONICS WAS INSTALLED PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2026030900227](https://openairdocs.org/sdr/REXA2026030900227.md): Floorbeam · cracked · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50 CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR ST
- [SDR REXA2026030900226](https://openairdocs.org/sdr/REXA2026030900226.md): Pressure Blkhd · corroded · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > CORROSION ON FWD CENTER PRESSURE BULKHEAD FS693.00 BTW STGR 26L AND STGR 26R. DUE EXCESSIVE DAMAGE ON FRAME FWD CENTER PRESSURE BULKHEAD WAS REPLACED PER CRJ900 SRM 53-41-10-101-001-A02, SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01
- [SDR REXA2026030900225](https://openairdocs.org/sdr/REXA2026030900225.md): Rib · cracked · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT RIGHT WING. MACHINED RIB OF LEADING EDGE SS57.16 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-240 REV --
- [SDR REXA2026030900224](https://openairdocs.org/sdr/REXA2026030900224.md): Support Angle · cracked · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK LOWER FWD SUPPORT ANGLE OF EXTERNAL POWER SERVICE PANEL SUPPORT STRUCTURE LOWER FWD SUPPORT ANGLE OF EXTERNAL POWER SERVICE PANEL SUPPORT STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
- [SDR REXA2026030900223](https://openairdocs.org/sdr/REXA2026030900223.md): Canister · cracked · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Wing Main, Frame Structure
  > CRACK ON SLAT TRACK CANISTER 1-3 AT RH WING MAIN FUEL TANK WS 148 CRACK ON SLAT TRACK CANISTER 1-3 AT RH WING MAIN FUEL TANK WS 148 WAS REPAIRED PER REO 670-57-42-577 REV --
- [SDR REXA2026030900220](https://openairdocs.org/sdr/REXA2026030900220.md): Support Angle · cracked · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON FWD SUPPORT ANGLES (2EAS) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARMENT INTERNAL STRUCTURE FWD SUPPORT ANGLES (2EAS) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARMENT INTERNAL STRUCTURE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
- [SDR REXA2026030900219](https://openairdocs.org/sdr/REXA2026030900219.md): Support Plate · corroded · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON RH WHEEL WELL HYD. LINES SUPPORT PLATE (IB BK, LG EX, OB BK, LG DN AST AND LG RET) DUE TO EXCESIVE DAMAGE ON RH WHEEL WELL HYD. LINES SUPPORT PLATE IB BK, LG EX, OB BK, LG DN AST AND LG RET) WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, SRM 5
- [SDR REXA2026030900218](https://openairdocs.org/sdr/REXA2026030900218.md): Bracket · damaged · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > ELONGATED BRACKET MOUNTING PULLEY OF PASSENGER DOOR BRACKET MOUNTING PULLEY OF PASSENGER DOOR WAS REPLACED PER CRJ 900 SRM 51-42-22-001-001-A01
- [SDR REXA2026030900215](https://openairdocs.org/sdr/REXA2026030900215.md): Support · corroded · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LBL27.00 BTW FS977.00 / FS1051.00 AT AFT CARGO COMPARTMENT DUE TO EXCESSIVE DAMAGE ( CORROSION) NO DAMAGE IS ALLOWED ON LONGITUDINAL BEAM UPPER FACE AT LBL27.00 BTW FS977.00 / FS1051.00 AFT BAGGAGE COMPARTMENT STRUCTURE WAS REPLACED PER CRJ900 SR
- [SDR REXA2026030900213](https://openairdocs.org/sdr/REXA2026030900213.md): Floorbeam · cracked · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2136 R
- [SDR REXA2026030900210](https://openairdocs.org/sdr/REXA2026030900210.md): Seat Track · corroded · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS 4EA BTW FS 349.00 TO FS 677.00 RBL 9 AT FLOOR PASSENGER CABIN SEAT RAILS 4EA BTW FS 349.00 TO FS 677.00 RBL 9 AT FLOOR PASSENGER CABIN WERE EVALUATED OUT LIMITS THEREFORE WERE REPLACED PER CRJ-900 SRM 53-21-49-101-001-A01 AND AMM 53-00-
- [SDR REXA2026030900209](https://openairdocs.org/sdr/REXA2026030900209.md): Angle · corroded · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE FLOOR SUPPORT FS310 TO FS349 LBL=43 AT CPAX CORROSION ON ANGLE FLOOR SUPPORT FS310 TO FS349 LBL=43 AT CPAX WAS REMOVED AND EVALUATED OUT OF LIMITS THEREFORE ANGLE AFT CAP AND ANGLE MID CAP WERE REPLACED AND CORROSION ON ANGLE FWD CAP WAS REM
- [SDR REXA2026030900208](https://openairdocs.org/sdr/REXA2026030900208.md): Floor Support · corroded · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE FLOOR SUPPORT FS310 TO FS349 LBL=43 AT CPAX CORROSION ON ANGLE FLOOR SUPPORT FS310 TO FS349 LBL=43 AT CPAX WAS REMOVED AND EVALUATED OUT OF LIMITS THEREFORE ANGLE AFT CAP AND ANGLE MID CAP WERE REPLACED AND CORROSION ON ANGLE FWD CAP WAS REM
- [SDR REXA2026030900207](https://openairdocs.org/sdr/REXA2026030900207.md): Panel · cracked · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > CRACK ON TOP PANEL EDGE MEMBER OF PASSENGER DOOR STAIR STEPS INTERNAL STRUCTURE, FWD & AFT EDGE SECTION. TOP PANEL EDGE MEMBER OF PASSENGER DOOR STAIR STEP WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 AND SRM 51-42-06-001-001-A01
- [SDR REXA2026030900200](https://openairdocs.org/sdr/REXA2026030900200.md): Seat Track · corroded · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE RAIL SEAT TRACK BTW FS437 TO FS445, FS501 TO FS517, FS597 TO FS613, FS629 TO FS645, FS661 TO FS661+16, FS661+46 TO FS661+50, FS669 TO FS677 AT CPAX CORROSION ON LH SIDE RAIL SEAT TRACK BTW FS437 TO FS445, FS501 TO FS517, FS597 TO FS613, FS
- [SDR REXA2026030900157](https://openairdocs.org/sdr/REXA2026030900157.md): Seat Track · corroded · Jan 19, 2026 · N272PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > " CORROSION ON SEAT RAILS 4EA BTW FS 374 TO FS 677 LBL 9 AT FLOOR PASSENGER CABIN. CORROSION ON SEAT RAILS (3EAS) BTW FS 374 TO FS 485 AND FS 581 TO 677 LBL 9 AT FLOOR PASSENGER CABIN WAS EVALUATED OUT OFF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-
- [SDR REXA2026030900205](https://openairdocs.org/sdr/REXA2026030900205.md): Seal · cracked · Jan 17, 2026 · N272PQ · Cndair CL6002D24 · Wing Main, Frame Structure
  > BROKEN SEAL NEXT TO ACCESS PANEL 591JB UPPER, LH WING BROKEN SEAL NEXT TO ACCESS PANEL 591JB UPPER, LH WING WAS REPLACED PER CRJ 900 SRM 51-42-10-001-001-A07
- [SDR REXA2026030900217](https://openairdocs.org/sdr/REXA2026030900217.md): Attach Angle · cracked · Jan 15, 2026 · N272PQ · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CRACK ON ATTACHMENT ANGLE OF ACCESS PANEL 542AZ ON MLG SHOCK STRUT BAY DUE TO EXCESSIVE DAMAGE ON ATTACHMENT ANGLE OF ACCESS PANEL 542AZ WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2026030900204](https://openairdocs.org/sdr/REXA2026030900204.md): Web · cracked · Jan 15, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON LH ELECTRICAL BAY WEB FLOOR FS 193.00 AT FWD EQUIPMENT COMPARTMENT LH ELECTRICAL BAY WEB FLOOR FS 193.00 AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ 900 SRM 53-11-43-201-001-A01 CHARGE VALVE AND GAUGE WERE REMOVED/INSTALLED, SERVICING OF HYDRAUL
- [SDR REXA2026030900212](https://openairdocs.org/sdr/REXA2026030900212.md): Fitting · worn · Jan 13, 2026 · N272PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > WEAR ON FLAP FITTING AND PLATE SUPPORT OF FLAP STUB FAIRING 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING (2EAS) OF FLAP STUB FAIRING 171DL AND 172DR AT RT & LT WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01, CRJ900 SRM 51-42-
- [SDR REXA2026030900203](https://openairdocs.org/sdr/REXA2026030900203.md): Retainer · cracked · Jan 13, 2026 · N272PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK ON MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE RH (FS 797.00 AND RBL 34) BINS SUPPORT STRUCTURE RETAINER ANGLE RH (FS 797.00 AND RBL 34) WAS REPLACED PER CRJ 900 SRM 51-41-02-001-001-A01
- [SDR REXA2026030900202](https://openairdocs.org/sdr/REXA2026030900202.md): Drag Angle · cracked · Jan 13, 2026 · N272PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CR
- [SDR REXA2025111000983](https://openairdocs.org/sdr/REXA2025111000983.md): Stringer · chafed · Nov 7, 2025 · N272PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CHAFE DAMAGE TO STGR 6L AND 7L AT FS 1144 TO 1162 PERFORMED PERMANENT REPAIR TO STGRS 6L AND 7L PER REO 690-53-61-1698 REF EA CRJ953-20703 AND CRJ953-20704
- [SDR REXA2025111000982](https://openairdocs.org/sdr/REXA2025111000982.md): Frame · chafed · Nov 7, 2025 · N272PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > CHAFE DAMAGE TO FRAME SECTOR AT FS 1162 PERFORMED TEMPORARY REPAIR TO FRAME SECTOR AT FS 1162 PER REO 690-53-71-098
- [SDR REXA2025102900968](https://openairdocs.org/sdr/REXA2025102900968.md): Engine · contaminated · Oct 15, 2025 · N272PQ · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > AFTER ROTATION CA AND FO STARTED TO SMELL SMOKE. VERY FAINT WHITE SMOKE SEEN BY PILOTS AND FAS WITH CHEMICAL ODOR. RAN CHECKING CARD AND QRH SMOKE AND FUMES REMOVAL PROCEDURE. TURNING PACKS AND RECIRC FAN OFF REDUCED ODOR SIGNIFICANTLY. FIRE RESCUE DID NOT N
- [SDR REXA2022101702278](https://openairdocs.org/sdr/REXA2022101702278.md): None · corroded · Oct 13, 2022 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH SIDE FLOOR SILL AT F.S. 310.00 CORRODED COMPLIED WITH REO 690-53-21-1549 REV -- DATED 2022-10-03
- [SDR REXA2020082000626](https://openairdocs.org/sdr/REXA2020082000626.md): Charger · not grounded · Aug 19, 2020 · N272PQ · Cndair CL6002D24 · Emergency Lighting
  > DURING MX NOTED EMER. LIGHT JUST AFT OF THE SERVICE DOOR (EXTERIOR FUSELAGE) DOES NOT ILLUMINATE. FOUND EPSU BATTERY CHARGER NOT GROUNDING CORRECTLY AT PS36 REMOVED & REPLACED EPSU BATTERY CHARGER & BATTERY AT PS36 IAW CRJ 900 AMM 33-51-17 OPS CHECK GOOD ALL E
- [SDR REXA2020082000625](https://openairdocs.org/sdr/REXA2020082000625.md): Battery Pack · failed · Aug 19, 2020 · N272PQ · Cndair CL6002D24 · Emergency Lighting
  > CREW REPORTED FWD(4) OVERHEAD CENTER LIGHTS CAME ON IN FLIGHT, WILL NOT EXTINGUISH. ALL OTHER EMERGENCY LIGHTS OPERATE AS PRESCRIBED. REMOVED & REPLACED EPSU BATTERY PACK AT PS36&EPSU BATTERY CHARGER IAW CRJ900 AMM 33-51-17. OPS CHECK GOOD ALL LIGHTS ILLUMI
- [SDR REXA2019052800741](https://openairdocs.org/sdr/REXA2019052800741.md): Floorbeam · corroded · May 28, 2019 · N272PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > INITIAL INSPECTION: CORROSION ON FLOORBEAM LBL9.00 BTW FS1015.00 - FS1051.30 AFTER BAGGAGE BAY (C3)[SM]. SUMMARY: CORROSION LEVEL 2. FLOORBEAM LBL9.00 BTW FS1015.00 - FS1051.30 AFTER BAGGAGE BAY, WAS REPAIRED PER SRM 53-00-41-201-001-A03. NEW BEAM WAS DRILLED
- [SDR REXA2019052700744](https://openairdocs.org/sdr/REXA2019052700744.md): Support · corroded · May 27, 2019 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON FLOOR FITTING SUPPORT BTW FS=565 / FS=629 AND STGR 22L / 27L (4 EAS) AT INTERNAL STRUCTURE OF FWD CARGO COMPARTMENT (C1) (SM) (TCI 53-20-306). SUMMARY:CORROSION LEVEL 2, FLOOR FITTING SUPPORTS BTW FS=565 / FS=629 AND STR 22L /
- [SDR REXA2019052700743](https://openairdocs.org/sdr/REXA2019052700743.md): Angle · corroded · May 27, 2019 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "AWR INITIAL INSPECTION: CORROSION ON ANGLE MID CAP, BTW FS=310 / 349 AND LBL 40 AT INTERNAL STRUCTURE OF FWD WET AREA (W1) (SM) IN REFERENCE EO NBR R53520 STEP 7. SUMMARY OF NRC: 00231 CORROSION LEVEL: 2 DUE TO EXCESSIVE CORROSION ON ANGLE MID CAP BTW FS=310
- [SDR REXA2019052700740](https://openairdocs.org/sdr/REXA2019052700740.md): Floorbeam · corroded · May 27, 2019 · N272PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > INITIAL INSPECTION: CORROSION ON FLOORBEAM LBL27.00 BTW FS1000.00 - FS1051.30 AFTER BAGGAGE BAY (C3)[SM]. SUMMARY OF NRC 306: LEVEL CORROSION 2. FLOORBEAM LBL27.00 BTW FS1000.00 - FS1051.30 AFTER BAGGAGE BAY, WAS REPAIRED PER SRM 53-00-41-201-001-A03.
- [SDR REXA2019052400733](https://openairdocs.org/sdr/REXA2019052400733.md): Seat Track · corroded · May 24, 2019 · N272PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 669 TO FS= 720, STGR 15L/R ] [ FS= 744 TO FS= 761, STR 15L/R ] [ FS=785 TO FS= 847+8, STR 15L/R], [ FS= 847+8 TO FS= 847+16, STR 15L/R], [ FS= 847+16 TO FS= 913, STR 15L/R] AND [ FS= 913 TO FS=
- [SDR REXA2019052100742](https://openairdocs.org/sdr/REXA2019052100742.md): Angle · corroded · May 21, 2019 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON ANGLE, BTW FS=310 / 349 AND LBL 40 AT INTERNAL SURROUND STRUCTURE OF PASSENGER DOOR (CPAX) (SM) (TCI 53-20-216). SUMMARY: ON NRC. 00234 CORROSION LEVEL 2. ON ANGLE, BTW FS=310 / 349 AND LBL 40 AT INTERNAL SURROUND STRUCTURE OF
- [SDR REXA201905190739](https://openairdocs.org/sdr/REXA201905190739.md): Angle · corroded · May 19, 2019 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON ANGLE, BTW FS=319 / 349 AND RBL 40 AT INTERNAL SURROUND STRUCTURE OF GALLEY SERVICE DOOR (CPAX) (SM) (TCI 53-20-215). SUMMARY: SUMMARY OF NRC: 00235 CORROSION LEVEL: 2. CORROSION ON ANGLE BTW FS= 319/ FS= 349 AND RBL 40 AT INT
- [SDR REXA2019051900738](https://openairdocs.org/sdr/REXA2019051900738.md): Canister · cracked · May 19, 2019 · N272PQ · Cndair CL6002D24 · Wing, Attach Fittings
  > INITIAL INSPECTION: CRACK IN CANISTER, WELDED NR 3 IN STA. WS=148 AT LT MAIN FUEL TANK. (AI) SUMMARY OF NRC 00188: CANISTER WELDED NR 3 IN STA. WS=148 AT LT MAIN FUEL TANK. WAS REPAIRED PER REO 670-57-42-577 REV. --.
- [SDR REXA2019051900736](https://openairdocs.org/sdr/REXA2019051900736.md): Intercostal · corroded · May 19, 2019 · N272PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR HIDDEN DAMAGE: CORROSION ON INTERCOSTALS BTW FS=310.00 / FS=333.00 AND STR 20R AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE JOBCARD NRB R25120. "SUMMARY OF NRC 00213 CORROSION LEVEL 2 ON INTERCOSTALS BTW FS=310.00 / FS=333.00
- [SDR REXA2019051900734](https://openairdocs.org/sdr/REXA2019051900734.md): Seat Track · corroded · May 19, 2019 · N272PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTION [ FS= 661+16 TO FS= 669, STR 15L ] AND [ FS= 661+16 TO 661+90, STR 15R ] AT PAX CABIN. (CPAX) (TCI: 53-20-217) "SUMMARY: OF NRC 00139, CORROSION LEVEL 2. SECTION SEAT RAILS IN SECTION [ FS= 661+16 TO
- [SDR REXA2019051900728](https://openairdocs.org/sdr/REXA2019051900728.md): Seat Track · corroded · May 19, 2019 · N272PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS [ FS= 677 TO FS= 847+16, 9LBL/RBL ] AND [FS= 846+16 TO FS= 977, 9LBL/9RBL ] AT PAX CABIN. (CPAX) (TCI: 53-20-233) SUMMARY OF NRC 00136, CORROSION LEVEL-2: SECTION IN SEAT RAIL SECTIONS [ FS= 677 T
- [SDR REXA2019051700737](https://openairdocs.org/sdr/REXA2019051700737.md): Panel · cracked · May 17, 2019 · N272PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > INITIAL INSPECTION: CRACKS ON AFT SIDE PANEL OF STEPS AT PASSENGER DOOR (PTAS) (SM). SUMMARY OF NRC 00166: CRACK ON AFT SIDE PANEL OF STEPS AT PASSENGER DOOR WAS REPAIRED PER SRM 52-11-04-201-004-A01, ZONE 5 DETAIL X AND Y; FIGURE 52-11-04-995-802.
- [SDR REXA2019051700735](https://openairdocs.org/sdr/REXA2019051700735.md): Panel · cracked · May 17, 2019 · N272PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > "INITIAL INSPECTION: CRACKS ON FWD SIDE PANEL OF STEPS AT PASSENGER DOOR (PTAS) (SM). "SUMMARY OF NRC. 00165: CRACKS ON FWD SIDE PANEL OF STEPS AT PASSENGER DOOR (PTAS) (SM). WERE REPAIRED PER SRM 52-11-04-201-004-A01 PAR. 5.B.(1) ZONE 4 DETAIL V AND W FIGURE

Next page: https://openairdocs.org/aircraft/N272PQ/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 = 'N272PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N272PQ/reports

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