# Service difficulty reports: N279PQ

A list on [N279PQ](https://openairdocs.org/aircraft/N279PQ.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 REXA2026050500484](https://openairdocs.org/sdr/REXA2026050500484.md): Stringer · corroded · Apr 27, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRG 26 RH/LH BTW FS 265 TO FS 280 AT MAIN AVIONICS COMPARTMENT STRG 26 LH BTW FS 265 TO FS 280 WAS CLEANED AND NOT DAMAGE WAS FOUND PER CRJ-900 SRM 51-26-00-001-001-A01 AND CORROSION ON STRG 26RH BTW FS 265 TO FS 280 AT MAIN AVIONICS COMPARTMENT
- [SDR REXA2026050500468](https://openairdocs.org/sdr/REXA2026050500468.md): Plate · worn · Apr 10, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WEAR ON FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND SRM CRJ-900 51-41-02-001-001-
- [SDR REXA2026050500467](https://openairdocs.org/sdr/REXA2026050500467.md): Plate · worn · Apr 10, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WEAR ON FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND SRM CRJ-900 51-41-02-001-001-
- [SDR REXA2026050500466](https://openairdocs.org/sdr/REXA2026050500466.md): Fitting · worn · Apr 10, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WEAR ON FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND SRM CRJ-900 51-41-02-001-001-
- [SDR REXA2026050500465](https://openairdocs.org/sdr/REXA2026050500465.md): Fitting · worn · Apr 10, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WEAR ON FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND SRM CRJ-900 51-41-02-001-001-
- [SDR REXA2026050500479](https://openairdocs.org/sdr/REXA2026050500479.md): Floorbeam · corroded · Apr 6, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM ANGLE S280, BTW RBL 12 TO LBL 12 AT FWD FLOOR CABIN DUE TO EXCESSIVE CORROSION ON FLOOR SUPORT ANGLE S280, BTW RBL 12 TO LBL 12 AT FWD FLOOR CABIN WAS REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-A01 AND AND SRM 51
- [SDR REXA2026050500494](https://openairdocs.org/sdr/REXA2026050500494.md): Frame · corroded · Apr 5, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME FS319.00 SETTLEMENT BTW STGR17LH / STGR20LH. DUE TO EXCESSIVE DAMAGE ON FRAME FS319.00 SETTLEMENT BTW STGR17LH / STGR20LH WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01 AND SRM 51-42-06-001-001-A01
- [SDR REXA2026050500480](https://openairdocs.org/sdr/REXA2026050500480.md): Skin · chafed · Apr 3, 2026 · N279PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > CHAFING ON UPPER SKIN ON FLAP-VANE BTW WS 95 TO WS 98 AT LH WING. CHAFING ON UPPER SKIN ON FLAP-VANE BTW WS 95 TO WS 98 AT LH WING WAS REPAIRED PER EA NO: CRJ957-22003 REV IR
- [SDR REXA2026050500493](https://openairdocs.org/sdr/REXA2026050500493.md): Floorbeam · corroded · Mar 18, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > AFTER REMOVAL OF FLOOR PANEL SUPPORT ANGLE OVER FS 280.00, IT WAS DETECTED CORROSION ON RH CROSSBEAM AT FS 280.00 AT LBL 9.00. CORROSION ON RH CROSSBEAM AT FS 280.00 AT LBL 9.00. WAS EVALUATED OUT OF LIMITS, THEREFORE WAS REPLACED PER CRJ900 SRM 51-10-06-001-0
- [SDR REXA2026050500492](https://openairdocs.org/sdr/REXA2026050500492.md): Floor Support · corroded · Mar 18, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERNAL STRUCTURE OVER STGR25RH BTW FS280.00 / FS295.00 AT MAIN AVIONICS COMPARTMENT DUE TO EXCESSIVE DAMAGE ON STGR25RH BTW FS280.00 / FS295.00 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-
- [SDR REXA2026050500491](https://openairdocs.org/sdr/REXA2026050500491.md): Strap · corroded · Mar 18, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION IN STRAP MACHINED FS=349.00 AND STGR17 LH (LOWER AFT DOOR L1 CORNER). DUE TO EXCESSIVE DAMAGE IN STRAP MACHINED FS=349.00 AND STGR17 LH (LOWER AFT DOOR L1 CORNER) WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR REXA2026050500474](https://openairdocs.org/sdr/REXA2026050500474.md): Stringer · corroded · Mar 18, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON INTERNAL STRUCTURE OVER STGR25RH BTW FS280.00 / FS295.00 AT MAIN AVIONICS COMPARTMENT DUE TO EXCESSIVE DAMAGE ON STGR25RH BTW FS280.00 / FS295.00 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-
- [SDR REXA2026050500490](https://openairdocs.org/sdr/REXA2026050500490.md): Hinge · corroded · Mar 17, 2026 · N279PQ · Cndair CL6002D24 · Ailerons
  > SECONDARY NRC IN REF TO RC 900-27-900-910: CORROSION ON LUG BORES L5 AND L6 IN CENTER FITTING AT LEFT AILERON. LUG BORES L5, L6 AND L1 IN CENTER FITTING AT LEFT AILERON WERE REPAIRED PER REO 670-57-61-237 REV -- & REO 690-57-61-511 REV - A
- [SDR REXA2026080501484](https://openairdocs.org/sdr/REXA2026080501484.md): Support Bracket · cracked · Mar 16, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON BRACKET SUPPORT OF JB6 AT FWD EQUIPMENT COMPARTMENT BRACKET SUPPORT OF JB6 AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2026050500489](https://openairdocs.org/sdr/REXA2026050500489.md): Support Bracket · cracked · Mar 16, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON BRACKET SUPPORT OF JB6 AT FWD EQUIPMENT COMPARTMENT BRACKET SUPPORT OF JB6 AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2026080501487](https://openairdocs.org/sdr/REXA2026080501487.md): Strap · corroded · Mar 15, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION STRAPS ON LEADING EDGE ACCESS PANEL 193AB LH AND RH ( 2 EA) STRAP ON LEADING EDGE ACCESS PANEL 193AB LH AND RH WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01.
- [SDR REXA2026080501486](https://openairdocs.org/sdr/REXA2026080501486.md): Strap · corroded · Mar 15, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION STRAPS ON LEADING EDGE ACCESS PANEL 193AB LH AND RH ( 2 EA) STRAP ON LEADING EDGE ACCESS PANEL 193AB LH AND RH WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01.
- [SDR REXA2026080501485](https://openairdocs.org/sdr/REXA2026080501485.md): Strap · corroded · Mar 15, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK AT INNER STRAP & AFT C-CHANNEL ALONG AFT WING TI FUSELAGE FAIRING (196DR AND 195DL) SUPPORT STRUCTURE AFT C-CHANNEL WAS CLEANED AND GVI WAS PERFORMED PER CRJ-900 SRM 51-26-00-001-001-A01 AND NO DAMAGE WAS FOUND. STRAP WAS FABRICATED AND REPLACED UNDER N
- [SDR REXA2026050500483](https://openairdocs.org/sdr/REXA2026050500483.md): Angle · corroded · Mar 15, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AT FWD WASTE SERVICE DOOR INTERNAL STRUCTURE, INCLUDING IMPACT ANGLE, FWD FRAME, AFT FRAME, UPPER & LOWER MEMBRANE. CORROSION ON FWD WASTE SERVICE DOOR INTERNAL STRUCTURE, INCLUDING FWD FRAME, AFT FRAME, UPPER & LOWER MEMBRANE WAS REMOVED AND EVALUAT
- [SDR REXA2026050500478](https://openairdocs.org/sdr/REXA2026050500478.md): Seat Track · corroded · Mar 13, 2026 · N279PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS STRG 15RH FROM FS 661+16 TO FS 977.00. SIDE SEAT RAILS (7 EAS) STRG 15RH FROM FS 667 TO FS 977 WERE REPLACED AND SIDE SEAT RAILS OVER STRG 15RH BTW FS 661+16 TO FS 677 WERE CLEANED AND CORROSION WERE NOT FOUND PER CRJ-900 SRM 53-31
- [SDR REXA2026050500477](https://openairdocs.org/sdr/REXA2026050500477.md): Seat Track · corroded · Mar 13, 2026 · N279PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS STRG15LH FS 485.00 TO FS 565.00 AND FS669.40 TO FS897.70 SUMMARY: SIDE SEAT RAILS OVER STRG 15LH BTW FS 485.00 TO FS661.00 + 74.00 WERE CLEANED AND CORROSION NOT WAS FOUND PER CRJ-900 SRM 51-26-00-001-001-A01, SIDE SEAT RAILS (5 EA
- [SDR REXA2026050500475](https://openairdocs.org/sdr/REXA2026050500475.md): Intercostal · cracked · Mar 13, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BTW FS349.00 / FS310.00 OVER STGR21LH AT MAIN AVIONICS COMPARTMENT. DUE TO EXCESSIVE DAMAGE ON INTERCOSTAL (2EAS) BTW FS349.00 / FS310.00 OVER STGR21LH AT MAIN AVIONICS COMPARTMENT WERE REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01, SR
- [SDR REXA2026050500472](https://openairdocs.org/sdr/REXA2026050500472.md): Canister · cracked · Mar 12, 2026 · N279PQ · Cndair CL6002D24 · Wing Main, Frame Structure
  > CRACK ON SLAT TRACK CANISTER 1-3 AT LH WING MAIN FUEL TANK WS 148. SLAT TRACK CANISTER 1-3 AT LH WING MAIN FUEL TANK WS 148 WAS REPAIRED PER REO 670-57-42-577 REV --
- [SDR REXA2026050500471](https://openairdocs.org/sdr/REXA2026050500471.md): Floor Support · cracked · Mar 10, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK ON FLOOR BEAM RBL & LBL 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 & LBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPART
- [SDR REXA2026050500470](https://openairdocs.org/sdr/REXA2026050500470.md): Attach Angle · cracked · Mar 10, 2026 · N279PQ · Cndair CL6002D24 · Wing, Attach Fittings
  > CRACK ON ATTACHMENT ANGLES OF TIRE BURST STRUCTURE ACCESS PANELS 542AZ AND 642AZ AT LH AND RH MLG SHOCK STRUT BAY. ANGLES OF TIRE BURST STRUCTURE ACCESS PANELS 542AZ AND 642AZ AT LH AND RH MLG SHOCK STRUT BAY WERE REPLACED IAW SRM 51-42-21-001-001-A01
- [SDR REXA2026050500469](https://openairdocs.org/sdr/REXA2026050500469.md): Attach Angle · cracked · Mar 10, 2026 · N279PQ · Cndair CL6002D24 · Wing, Attach Fittings
  > CRACK ON ATTACHMENT ANGLES OF TIRE BURST STRUCTURE ACCESS PANELS 542AZ AND 642AZ AT LH AND RH MLG SHOCK STRUT BAY. ANGLES OF TIRE BURST STRUCTURE ACCESS PANELS 542AZ AND 642AZ AT LH AND RH MLG SHOCK STRUT BAY WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
- [SDR REXA2026050500464](https://openairdocs.org/sdr/REXA2026050500464.md): Door Sill · cracked · Mar 10, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > INITIAL INSPECTION: CRACK ON RH DOOR LANDING (AFT CUTOUT AREA OF ACCESS 212AR LATCH) AT FWD ACCESORY COMPARTMENT. RH DOOR LANDING (AFT CUTOUT AREA OF ACCESS 212AR LATCH) AT FWD ACCESORY COMPARTMENT WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01, SRM 51-42-
- [SDR REXA2026050500463](https://openairdocs.org/sdr/REXA2026050500463.md): Hinge · cracked · Mar 10, 2026 · N279PQ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CRACK AND BENT HINGE PLATE OF AC GROUND CONNECTION ACCESS DOOR AT FWD LOWER FUSELAGE. HINGE PLATE OF AC GROUND CONNECTION ACCESS DOOR AT FWD LOWER FUSELAGE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, RJ-900 SRM 51-41-02-001-001-A01 AND CRJ-900 AMM 52-45
- [SDR REXA2026050500461](https://openairdocs.org/sdr/REXA2026050500461.md): Retainer · cracked · Mar 10, 2026 · N279PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACK AND WEAR ON RETEINER SEAL AT FWD/CTR BAGGAGE BAY DOORS COMPARTMENT (LOWER SIDE) NEW RETEINER SEAL AT FWD/CTR BAGGAGE BAY DOORS COMPARTMENT (LOWER SIDE) WERE REPLACED PER CRJ-900 SRM 51-42-06-001-A01, LEAK TEST AT FORWARD AND CENTER DOOR WAS PERFORMED PER
- [SDR REXA2026080501483](https://openairdocs.org/sdr/REXA2026080501483.md): Panel · cracked · Mar 7, 2026 · N279PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > CRACK ON AFT SECTION OF TOP PANEL EDGE MEMBER OF PASSENGER DOOR STAIR STEPS INTERNAL STRUCTURE. BELOW STEP 832ET. TOP PANEL EDGE MEMBER OF PASSENGER DOOR STAIR STEPS INTERNAL STRUCTURE. BELOW STEP 832ET WAS REPAIRED PER CRJ-900 SRM 52-11-04-201-006-A01
- [SDR REXA2026050500460](https://openairdocs.org/sdr/REXA2026050500460.md): Drag Angle · cracked · Mar 7, 2026 · N279PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON RH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER CRACK ON RH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER WERE REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01
- [SDR REXA2026050500459](https://openairdocs.org/sdr/REXA2026050500459.md): Drag Angle · cracked · Mar 7, 2026 · N279PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON LH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER CRACK ON LH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER WERE REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01
- [SDR REXA2026050500458](https://openairdocs.org/sdr/REXA2026050500458.md): Angle · chafed · Mar 7, 2026 · N279PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > WEAR AND BENT ANGLE OF AFT DOOR TRACK LOWER SIDE AT AFT BAGGAGE COMPARTMENT. ANGLE OF AFT DOOR TRACK LOWER SIDE AT AFT BAGGAGE COMPARTMENT WAS EVALUATED OUT OF LIMITS, THEREFORE WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A
- [SDR REXA2022123002730](https://openairdocs.org/sdr/REXA2022123002730.md): Floorbeam · corroded · Dec 24, 2022 · N279PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LEFT BS 280 FLOORBEAM WAS FOUND TO BE CORRODED. REPLACED THE FLOORBEAM IAW SRM 51-42-06-001-001-A01, 51-42-22-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022123002729](https://openairdocs.org/sdr/REXA2022123002729.md): Bulkhead Web · corroded · Dec 24, 2022 · N279PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > LEFT AFT LOWER BS 280 WEB WAS CORRODED. COMPLIED WITH STEPS B, 1-3 AND FABRICATED NEW LOWER WEB AND BUTTSTRAP IAW SRM 53-11-10-201-004-A01.
- [SDR REXA2022122802725](https://openairdocs.org/sdr/REXA2022122802725.md): Floorbeam · corroded · Dec 24, 2022 · N279PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > BS 280 FLOORBEAM WAS FOUND TO BE CORRODED. REPLACED BS 280 FLOORBEAM IAW SRM 51-42-06-001-001-A01, 51-42-22-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2019070301089](https://openairdocs.org/sdr/REXA2019070301089.md): Panel · cracked · Jul 3, 2019 · N279PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > INITIAL INSPECTION: CRACKS ON AFT SIDE PANEL OF STEPS AT PASSENGER DOOR (PTAS) (SM). SUMMARY OF NRC 00195: DOUBLER AND REPAIR ANGLES (2 EA'S), WERE FABRICATED PER SRM 52-11-04-201-004-A01, FIG. 52-11-04-995-802 (SHEET7 OF 13) AND DOUBLER AND REPAIR ANGLES (2 E
- [SDR REXA2019070301042](https://openairdocs.org/sdr/REXA2019070301042.md): Lever · worn · Jul 3, 2019 · N279PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > "INITIAL INSPECTION: WEAR ON FWD PULL-IN LEVER AT PASSAGER DOOR (PTAS)(AYP). "SUMMARY NRC 193: FWD PULL-IN LEVER AT PASSAGER DOOR WAS REPLACED PER AMM 52-11-02 AND TEST WAS PERFORMED PER AMM 52-11-00 TEST OK.
- [SDR REXA2019070301051](https://openairdocs.org/sdr/REXA2019070301051.md): Access Panel · worn · Jul 3, 2019 · N279PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > PART RACKS: WEAR ON ACCESS PANELS AT INBOARD FLAP VANE ACTUATOR 584AB, 584JB, 584EB AND 584GT. (SM)(LT WING) SUMMARY OF NRC 00292: WEAR ON ACCESS PANELS AT INBOARD FLAP VANE ACTUATOR 584AB, 584JB, 584EB AND 584GT WAS BLENDED OUT PER SRM 51-12-00-001-001-A01 PA
- [SDR REXA2019070201041](https://openairdocs.org/sdr/REXA2019070201041.md): Cap · corroded · Jul 2, 2019 · N279PQ · 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 00189, CORROSION LEVEL 2. ANGLE MID CAP BTW FS=310 / 349 AND LBL 40 AT INTERNAL
- [SDR REXA2019070101088](https://openairdocs.org/sdr/REXA2019070101088.md): Seal · torn · Jul 1, 2019 · N279PQ · Cndair CL6002D24 · APU Exhaust System
  > AWR. HIDDEN DISCREPANCY: TORN SEAL IN APU TAILCONE EXHAUST CONE ASSY [IN REF W634079 PERM REPAIR APU EXHAUST CONE] (APU) (SM). SUMMARY OF NRC 00398: NEW CLAMP, BAND, AFT AND NEW B-SEAL-AFT WERE INSTALLED PER AMM 49-81-00-960-801 (CONFIG A02) PAR.4.A. AND CMM H
- [SDR REXA2019070101043](https://openairdocs.org/sdr/REXA2019070101043.md): Angle · cracked · Jul 1, 2019 · N279PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > "INITIAL INSPECTION: CRACKS ON FWD SIDE PANEL OF STEPS AT PASSENGER DOOR (PTAS) (SM). "SUMMARY: OF NRC 00194: REPAIR PARTS WERE FABRICATED PER SRM 52-11-04-201-004-A01, FIG. 52-11-04-995-802 (SHEET 8 OF 13).AND DOUBLER AND REPAIR ANGLES (3 EA'S), WERE INSTALLE
- [SDR REXA2019063001029](https://openairdocs.org/sdr/REXA2019063001029.md): Intercostal · corroded · Jun 30, 2019 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "[ IN REFERENCE NRC **** ] INITIAL INSPECTION: CORROSION ON INTERCOSTALS (2 EAS) IN STA. FS= 349 TO FS= 364 NEAR STR 27 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09 "SUMMARY: ON NRC. 00096 CORROSION LEVEL 2. ON INTERCOST
- [SDR REXA2019062901045](https://openairdocs.org/sdr/REXA2019062901045.md): Floorbeam · corroded · Jun 29, 2019 · N279PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > INITIAL INSPECTION: CORROSION ON FLOORBEAM LBL 09.00 STA FS 1015 TO FS 1031 AT AFT CARGO COMPARTMENT (CCT) (TCI 100-15) SUMMARY OF NRC 00201: DUE CORROSION LEVEL 2 ON FLOORBEAM LBL 09.00 STA FS 1015 TO FS 1031 AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 53-0
- [SDR REXA2019062901034](https://openairdocs.org/sdr/REXA2019062901034.md): Mount · corroded · Jun 29, 2019 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION: CORROSION ON LOWER FRAME BETWEEN FS319 TO FS349 OF THE GALLEY SERVICE DOOR SURROUND STRUCTURE (SM) (CPAX) "SUMMARY OF NRC:00177 CORROSION LEVEL: 2 DUE TO EXCESSIVE CORROSION ON ANGLE MOUNTING BETWEEN FS319 TO FS349 WILL BE REPLACED: ORIGIN
- [SDR REXA2019062901026](https://openairdocs.org/sdr/REXA2019062901026.md): Stringer · corroded · Jun 29, 2019 · N279PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "[ IN REFERENCE NRC 0035 ] INITIAL INSPECTION: CORROSION ON STRINGER 26RH IN STA. FS= 280 TO FS= 310 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, "SUMMARY: STRINGER 26RH IN FS= 280 TO FS= 333 AT MAIN AVIONICS COMPARTMENT
- [SDR REXA2019062701053](https://openairdocs.org/sdr/REXA2019062701053.md): Seat Track · corroded · Jun 27, 2019 · N279PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LATE FINDING: CORROSION ON FLOOR SEAT RAIL IN FS= 379 9LBL AT PAX CABIN. (CPAX) (TCI: 53-20-243) SUMMARY OF NRC 00383: CORROSION LEVEL-2: FLOOR SEAT RAIL ON FS=379 9LBL AT PAX CABIN WAS REPLACED PER SRM 51-21-06-001-001-A01 AND SRM 53-21-49-101-001-A01.
- [SDR REXA2019062701052](https://openairdocs.org/sdr/REXA2019062701052.md): Fitting · corroded · Jun 27, 2019 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR HIDDEN DAMAGE: DURING REPLACE OF NLG DOOR AFT HINGE PIN BUSHINGS, CORROSION AIRFRAME FITTING ASSY (2 E/A) WAS FOUND IN REF JOB CARD 900-32-710-902 (NLG WHEEL WELL). SUMMARY OF NRC 00339, CORROSION LEVEL-2: NEW FITTING ASSY (2 E/A) WERE DRILLED PER SRM 51-4
- [SDR REXA2019062701046](https://openairdocs.org/sdr/REXA2019062701046.md): Floorbeam · corroded · Jun 27, 2019 · N279PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > INITIAL INSPECTION: CORROSION ON FLOORBEAM RBL 09.00 STA FS 1015 TO FS 1031 AT AFT CARGO COMPARTMENT (CCT) (TCI 100-15). SUMMARY OF NRC 00202, CORROSION LEVEL-2: THE DAMAGED SECTION OF THE FLOORBEAM SECTION RBL 09.00 STA FS 1000.00+4.500"" TO FS 1031.00+5.500"
- [SDR REXA2019062601048](https://openairdocs.org/sdr/REXA2019062601048.md): Support · corroded · Jun 26, 2019 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON SCUFF PLATE SUPPORTS INCLUDING ANGLES BTW FS=319 / 349 AND RBL 39 AT INTERNAL SURROUND STRUCTURE OF GALLEY SERVICE DOOR (CPAX) (SM). SUMMARY: CORROSION LEVEL 2 ON SCUFF PLATE SUPPORTS INCLUDING ANGLES BTW FS=319 / 349 AND RBL 3

Next page: https://openairdocs.org/aircraft/N279PQ/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 = 'N279PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N279PQ/reports

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