# Service difficulty reports: N176PQ

A list on [N176PQ](https://openairdocs.org/aircraft/N176PQ.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 4 · 180 reports

- [SDR REXA2026052600666](https://openairdocs.org/sdr/REXA2026052600666.md): Stringer · corroded · Dec 30, 2025 · N176PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > SECONDARY NRC FROM NRC 358: AFTER REMOVAL OF FRAME ANGLE, CORROSION AT STGR 19RH BTW FS 661.00 + 74.00 AND FS 661.00 + 90.00. STGR 19RH BTW FS 661.00 + 74.00 AND FS 661.00 + 90.00 WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-31-03-101-004-A05 AND SRM 53-00-00-1
- [SDR REXA2026052600678](https://openairdocs.org/sdr/REXA2026052600678.md): Shear Tie · corroded · Dec 28, 2025 · N176PQ · Cndair CL6002D24 · Fuselage Internal Mounting Structure
  > CORROSION ON FRAME ANGLE AT INTERNAL FUSELAGE STRUCTURE FS661.00 + 90.00 AND STGR 19RH. FRAME ANGLE AT INTERNAL FUSELAGE STRUCTURE FS661.00 + 90.00 AND STGR 19RH WAS REPAIRED PER EA CRJ953-21186 REV IR
- [SDR REXA2026052600676](https://openairdocs.org/sdr/REXA2026052600676.md): Lug · corroded · Dec 25, 2025 · N176PQ · Cndair CL6002D24 · Ailerons
  > AFTER RH AILERON BUSHINGS REMOVAL, CORROSION AND WEAR ON BORE LUGS AND FACES FITTINGS OF (R1,R2,R5,R6) AT CENTER HINGE FITTING WAS FOUND. LUGS AND FACES FITTINGS OF (R1,R2,R5,R6) AT CENTER HINGE FITTING WERE REPAIRED PER REO 690-57-61-477 REV. -- & REO 670-57-
- [SDR REXA2026052600675](https://openairdocs.org/sdr/REXA2026052600675.md): Hinge · corroded · Dec 25, 2025 · N176PQ · Cndair CL6002D24 · Ailerons
  > AFTER LH AILERON BUSHINGS REMOVAL, WEAR WAS FOUND ON LUGS BORES AND LUGS FACES OF L1, L2, L4, L5 AND L6 AT CENTER FITTING. CENTER FITTING LUG BORES L1, L5 AND L6 AILERON LH WERE REPAIRED PER REO 670-57-61-107 REV -B, L2 WAS REPAIRED REO 690-57-61-482 REV-
- [SDR REXA2026052600677](https://openairdocs.org/sdr/REXA2026052600677.md): Stringer Splice · corroded · Dec 19, 2025 · N176PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR SPLICE LOCATED BTW STGR-25R FROM FS329.00 TO FS339.00. STGR SPLICE LOCATED BTW STGR-25R FROM FS329.00 TO FS339.00. WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
- [SDR REXA2026052600665](https://openairdocs.org/sdr/REXA2026052600665.md): Stringer · corroded · Dec 19, 2025 · N176PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > SECONDARY NRC FROM NRC 00183: CORROSION ON STGR-25R FROM FS339.00 TO FS364.00. CORROSION ON STGR-25R FROM FS339.00 TO FS364.00 WAS EVALUATED OUT LIMITS PER CRJ900 SRM 53-21-03-101-006-A04 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2026052600674](https://openairdocs.org/sdr/REXA2026052600674.md): Fitting · corroded · Dec 16, 2025 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR FITTING ACCESS 305 (1EA) AISLE SIDE ON GALLEY 3 FLOOR FITTING ON ACCESS 305 (1 EA) AISLE SIDE AT GALLEY 3 WAS REPLACED PER C&D ZODIAC AEROSPACE CMM 25-33-18
- [SDR REXA2026052600673](https://openairdocs.org/sdr/REXA2026052600673.md): Fitting · corroded · Dec 16, 2025 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR FITTING ACCESS 109 (1EA) ON GALLEY 1 FLOOR FITTING ON ACCESS 109 (1 EA) AT GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67
- [SDR REXA2026052600662](https://openairdocs.org/sdr/REXA2026052600662.md): Doubler · worn · Dec 16, 2025 · N176PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > WEAR ON REPAIR DOUBLER LOCATED ON STGR-27 FROM FS907.00 TO FS920.00 AT EXTERNAL FUSELAGE CENTER SECTION. DUE TO EXCESSIVE DAMAGE ON DOUBLER LOCATED ON STGR-27 FROM FS907.00 TO FS920.00 AT EXTERNAL FUSELAGE CENTER SECTION MUST BE REPLACED PER CRJ900 SRM 51-10-
- [SDR REXA2026052600672](https://openairdocs.org/sdr/REXA2026052600672.md): Support Angle · cracked · Dec 15, 2025 · N176PQ · Cndair CL6002D24 · Service Doors
  > CRACKED INTERNAL SUPPORT ANGLE (BELOW THE BOX) AT SERVICE PANEL DOOR 122CR. CRACKED INTERNAL SUPPORT ANGLE (BELOW THE BOX) AT SERVICE PANEL DOOR 122CR WAS REPAIRED PER EA NO: CRJ953-21233 REV: IR
- [SDR REXA2026052600657](https://openairdocs.org/sdr/REXA2026052600657.md): Support Angle · cracked · Dec 15, 2025 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > OUT OF SCOPE: CRACKED INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE. INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01.
- [SDR REXA2026052600664](https://openairdocs.org/sdr/REXA2026052600664.md): Drag Angle · cracked · Dec 14, 2025 · N176PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON LEFT STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) LEFT STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00)
- [SDR REXA2026052600663](https://openairdocs.org/sdr/REXA2026052600663.md): Attach Angle · cracked · Dec 14, 2025 · N176PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON RIGHT STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) RIGHT STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.
- [SDR REXA2024101600881](https://openairdocs.org/sdr/REXA2024101600881.md): Lamp · inoperative · Oct 16, 2024 · N176PQ · Cndair CL6002D24 · Emergency Lighting
  > AFT RH EXTERIOR EMERGENCY LIGHT INOP RE-LAMPED AFT RH EXTERIOR EMERGENCY LIGHT IAW CRJ900 AMM 33-51-15 OPS CHECK GOOD.
- [SDR REXA2024080500608](https://openairdocs.org/sdr/REXA2024080500608.md): Brake · inoperative · Jul 29, 2024 · N176PQ · Cndair CL6002D24 · Landing Gear Brake System
  > DESENDING THROUGH 10,000 FEET ON ARRIVAL, BRAKE OVHT WARNING MESSAGE SHOWED AT 200 KNOTS AND LOWERED GEAR. RAN QRH AND MESSAGE CLEARED. DEFERED RH OUTBOARD BRAKE TEMP INDICATION MEL 2-46-1D CAT C M PROCEDURE C/W MOC NOTIFIED 7821 PLACARD INSTALLE BACK DATE 23
- [SDR REXA2022070501467](https://openairdocs.org/sdr/REXA2022070501467.md): Light · inoperative · Jun 27, 2022 · N176PQ · Cndair CL6002D24 · Emergency Lighting
  > RHOB SIDE EMERGENCY LIGHT, THIRD FROM FWD INOP (RIGHT AFT O/W). REMOVED & REPLACED LAMP IAW AMM 33-51-15. OPS CHECK GOOD. P/N ON & OFF 8GH005123-06.
- [SDR REXA2022070101437](https://openairdocs.org/sdr/REXA2022070101437.md): Lamp · inoperative · Jun 27, 2022 · N176PQ · Cndair CL6002D24 · Emergency Lighting
  > RHOB SIDE EMERGENCY LIGHT, THIRD FROM FWD INOP. REMOVED & REPLACED LAMP IAW AMM 33-51-15. OPS CHECK GOOD. P/N ON & OFF 8GH005123-06.
- [SDR REXA2022053101040](https://openairdocs.org/sdr/REXA2022053101040.md): Stringer · corroded · May 23, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER SEGMENT AT 25R HAS MULTIPLE SPOTS OF CORROSION FROM FS 985 TO FS 1098. SPLICE REPAIRED STRINGER 25R IAW ENDEAVOR AIR EA CRJ953-13267.
- [SDR REXA2022053101039](https://openairdocs.org/sdr/REXA2022053101039.md): Splice · corroded · May 23, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280.00 TO FS 319, SPLICE ANGLE CORRODED. REMOVED & REPLACED SPLICE ANGLE IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-13-001-001-A01 & 51-42-06-001-001-A01.
- [SDR REXA2022053101038](https://openairdocs.org/sdr/REXA2022053101038.md): None · corroded · May 23, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280.00 TO FS 319, FLOOR SILL CORRODED. REMOVED & REPLACED RH FLOOR SILL IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-13-001-001-A01 & 51-42-06-001-001-A01.
- [SDR REXA2022053101041](https://openairdocs.org/sdr/REXA2022053101041.md): Piston · corroded · May 18, 2022 · N176PQ · Cndair CL6002D24 · Nose/Tail Landing Gear
  > NLG PISTON/AXLE ASSY CORRODED BELOW PISTON CHROME. REPAIRED NLG PISTON/AXLE ASSY IAW MHIRJ REO 690-32-21-129 DATED 2022-05-16
- [SDR REXA2022053100963](https://openairdocs.org/sdr/REXA2022053100963.md): Frame · corroded · May 15, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION FOUND ON FRAME 379 FROM STR 20R TO STR 25R. REMOVED & REPLACED FRAME SECTOR IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01 & 51-42-06-001-001-A01.
- [SDR REXA2022053100960](https://openairdocs.org/sdr/REXA2022053100960.md): Frame · corroded · May 10, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME FS 295 BETWEEN STGR 26L TO 27 IS CORRODED. REMOVED & REPLACED FRAME SECTOR IAW CRJ 900 SRM 53-00-06-201-006-A01.
- [SDR REXA2022053100959](https://openairdocs.org/sdr/REXA2022053100959.md): Stringer · corroded · May 10, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 21R BETWEEN FS 333 AND FS 280 IS CORRODED. REMOVED, FABRICATED & REPLACED STRINGER IAW ENDEAVOR AIR EA CRJ953-12976.
- [SDR REXA2022053100957](https://openairdocs.org/sdr/REXA2022053100957.md): Angle · corroded · May 9, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER INBD MOUNTING ANGLE CORRODED. REPLACED SERVICE DOOR LOWER INBD MOUNTING ANGLE PN SH670-31996-3 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022053100937](https://openairdocs.org/sdr/REXA2022053100937.md): Joint · corroded · May 9, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WATER WASTE SERVICE DOOR SURROUND STRUCTURE JOINT AT FS 379 STGR 21R IS CORRODED. REPLACED JOINT IAW CRJ 900 SRM 51-40-11-001-001-A01.
- [SDR REXA2022053100935](https://openairdocs.org/sdr/REXA2022053100935.md): Angle · corroded · May 9, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER INBD SILL ANGLE CORRODED. REPLACED SERVICE DOOR LOWER INBD SILL ANGLE PN SH670-31982-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022053100962](https://openairdocs.org/sdr/REXA2022053100962.md): Strap · cracked · May 5, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PANEL195DR FAIRING STRAP CRACKED REMOVED AND REPLACED STRAP AND MODIFIED AFT PANEL "C" CHANNEL ON PNL 195DR IAW CRJ-900 SRM 51-41-02-001-001-A01 AND ENDEAVOR AIR EO R53573 REV 2 DATED 22FEB18.
- [SDR REXA2022053100958](https://openairdocs.org/sdr/REXA2022053100958.md): Stringer · corroded · May 5, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 23R BETWEEN FS333 AND FS379 IS CORRODED. REPLACED STGR 23R BETWEEN FS333 AND FS379 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022053100932](https://openairdocs.org/sdr/REXA2022053100932.md): Stringer · corroded · May 5, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS295 TO FS333 STGR 24R IS CORRODED. REPLACED STGR 24R FS295 TO FS333 IAW ENDEAVOR AIR EA CRJ953-13308 REV IR DATED 4/23/2022
- [SDR REXA2022053100920](https://openairdocs.org/sdr/REXA2022053100920.md): Frame · cracked · May 5, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS333 FRAME IS CRACKED BETWEEN STGR1R AND STGR2R. REPAIRED FS333 FRAME BETWEEN STGR1R AND 2R IAW ENDEAVOR AIR EA CRJ953-13368 REVIR DATED 4/13/2022.
- [SDR REXA2022053100918](https://openairdocs.org/sdr/REXA2022053100918.md): Stringer · corroded · May 5, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS333 TO FS349 STGR21R IS CORRODED. REPLACED STGR 21R BETWEEN FS333 AND FS349 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022053100961](https://openairdocs.org/sdr/REXA2022053100961.md): Splice · corroded · May 4, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SPLICE AT FS333 AND STRINGER 22R IS CORRODED. REPLACED STGR 22R SPLICE AT FS333 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2022053100956](https://openairdocs.org/sdr/REXA2022053100956.md): Stringer · corroded · May 4, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS333 TO FS349 STR24R IS CORRODED REPAIRED STR24R IAW CRJ SRM 51-21-06-001-001-A01 AND 53-00-03-201-001-A02
- [SDR REXA2022053100945](https://openairdocs.org/sdr/REXA2022053100945.md): Splice · corroded · May 4, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SPLICE AT FS333 AND STRINGER 23R IS CORRODED. REPLACED STGR 23R SPLICE AT FS333 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2022053100938](https://openairdocs.org/sdr/REXA2022053100938.md): Intercostal · corroded · May 4, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT 20R BETWEEN FS349 AND FS364 IS CORRODED REPLACED INTERCOSTAL AT 20R BETWEEN FS349 AND FS364 IAW CRJ-900 SRM 51-42-06-001-001-A01.
- [SDR REXA2022053100936](https://openairdocs.org/sdr/REXA2022053100936.md): Frame · corroded · May 4, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS319 FRAME CORRODED BETWEEN STGR 24R AND STGR 25R. REPAIRED FS319 FRAME BETWEEN STGR 25L AND STGR 23R IAW CRJ-900 SRM 53-00-06-201-006-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01
- [SDR REXA2022053100927](https://openairdocs.org/sdr/REXA2022053100927.md): Beam · corroded · May 4, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR BEAM AT LBL27,FS 969.00 - FS1051.00, IS CORRODED. CORRODED FLOOR BEAM REPAIRED I.A.W CRJ 900 SRM # 53-00-41-201-001-A03.
- [SDR REXA2022053100923](https://openairdocs.org/sdr/REXA2022053100923.md): Retainer · corroded · May 4, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > L/H SIDE SEAT RAIL STRUCTURE @ F.S.744.15 IS CORRODED/CRACKED. REMOVED DAMAGED L/H SIDE SEAT RAIL RETAINER AT F.S.744.15 AND INSTALLED NEW SERVICABLE SEAT RAIL RETAINER IAW CRJ 900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022053100921](https://openairdocs.org/sdr/REXA2022053100921.md): Seat Track · corroded · May 4, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL9 FLOOR SEAT TRACK BETWEEN F.S.661+32 TO F.S.693 IS CORRODED. REMOVED CORRODED LBL9 SEAT TRACK FROM F.S.661+32 TO F.S.693 AND INSTALLED NEW SERVICABLE SEAT TRACK IAW CRJ 900 AMM 53-00-49-400-801-A07 AND SRM 53-00-49-201-002-A01.
- [SDR REXA2022053100916](https://openairdocs.org/sdr/REXA2022053100916.md): Stringer · corroded · May 4, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS333 TO FS349 STGR 22R IS CORRODED. REPLACED STGR 22R BETWEEN FS333 AND FS349 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022053100905](https://openairdocs.org/sdr/REXA2022053100905.md): Panel · chafed · May 4, 2022 · N176PQ · Cndair CL6002D24 · Wing, Control Surfaces
  > PANELS 684ET AND HT HAS CHAFFING DAMAGE. REPAIRED CHAFFING DAMAGE TO PANEL 684ET IAW CRJ 900 SRM 51-12-00-001-001-A01. REPLACED DAMAGED PANEL 684HT IAW CRJ 900 SRM 51-40-11-001-001-A01.
- [SDR REXA2022053100964](https://openairdocs.org/sdr/REXA2022053100964.md): Mount · chafed · May 3, 2022 · N176PQ · Cndair CL6002D24 · Engine Mount Section
  > R/H ENGINE YOKE MOUNT IS CHAFED AT 2 LOCATIONS. REPAIRED R/H ENGINE YOKE IAW MHIRJ REO 690-71-21-041 REV -- DATED 2022-04-23 AND BOMBARDIER REO 670-71-21-057 EV -- DATED 2013-09-13.
- [SDR REXA2022053100925](https://openairdocs.org/sdr/REXA2022053100925.md): Intercostal · corroded · May 3, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN F.S.865 TO F.S.881 AT STGR 21R IS CORRODED. REPAIRED INTERCOSTAL IAW ENDEAVOR AIR EA CRJ953-13249 REV B DATED 4-26-2022.
- [SDR REXA2022053100917](https://openairdocs.org/sdr/REXA2022053100917.md): Stringer · corroded · May 3, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > F.S.349 TO F.S.409 STGR 19R IS CORRODED. REPAIRED FUSELAGE STRINGER 19R FROM F.S.349 TO F.S.409 IAW CRJ 900 SRM 53-00-03-201-001-A02.
- [SDR REXA2022053100924](https://openairdocs.org/sdr/REXA2022053100924.md): Striker · corroded · Apr 30, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LWR SEAL STRIKER FASTENER HOLES CORRODED. REPLACED THE SERVICE DOOR LWR SEAL STRIIKER P/N SH670-31412-7 IAW CRJ-900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
- [SDR REXA2022053100919](https://openairdocs.org/sdr/REXA2022053100919.md): Intercostal · corroded · Apr 30, 2022 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CORRODED AT FS645 BETWEEN STGR 25L AND STGR 26L. REPLACED INTERCOSTAL AT FS645 BETWEEN STGR 25L AND 26L IAW CRJ-900 SRM 51-42-06-001-001-A01,51-52-21-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-21-16-001-001-A01
- [SDR REXA2022053100942](https://openairdocs.org/sdr/REXA2022053100942.md): Intercostal · corroded · Apr 29, 2022 · N176PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD INTERCOSTAL INTERCOSTAL DD5 IS CORRODED REMOVED AND REPLACED INTERCOSTAL DD5 P/N 601R318091-5 IAW CRJ-900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
- [SDR REXA2022053100941](https://openairdocs.org/sdr/REXA2022053100941.md): Former · corroded · Apr 29, 2022 · N176PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER IS CORRODED PN 601R318034-5S. REMOVED AND REPLACED PAX DOOR AFT FORMER P/N 601R318034-5 IAW CRJ-900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2022053100940](https://openairdocs.org/sdr/REXA2022053100940.md): Intercostal · corroded · Apr 29, 2022 · N176PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > INTERCOSTAL/ 601R318057-1/CORRODED/INTERCOSTAL/ 601R318057-1 INTERCOSTAL/ 601R318057-1/CORRODED

Next page: https://openairdocs.org/aircraft/N176PQ/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 = 'N176PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N176PQ/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.
