# Service difficulty reports: N147PQ

A list on [N147PQ](https://openairdocs.org/aircraft/N147PQ.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 · 192 reports

- [SDR REXA2026091401824](https://openairdocs.org/sdr/REXA2026091401824.md): Elec Connector · misinstalled · Sep 10, 2026 · N147PQ · Cndair CL6002D24 · Light System Wiring
  > AFT MOST CEILING EMER LIGHT INOP. PERFORMED POWER CHECK ON AFT CEILING PANEL IAW CMM 25-28-63. FOUND NO POWER ON J3 PIN 5. FOUND CONNECTORS P5461 AND P5459 SWAPPED. INSTALLED P5461 AND P5459 IN THERE CORRECT POSITIONS IAW CRJ 900 AMM 25-26-05 OPS CHECK GOOD.
- [SDR REXA2026072201084](https://openairdocs.org/sdr/REXA2026072201084.md): Lug · damaged · Jul 21, 2026 · N147PQ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > "DURING THE REMOVAL OF THE RT WING SIDE AILERON BUSHINGS, IT WAS FOUND THAT THE LUG LABELED D (HINGE NR 2 OTBD) WAS PREVIOUSLY OVERSIZED. ENGINEERING IS REQUIRED. LUG D BORE MEASURES (0.8965). REPAIRED RT WING AILERON HINGE FITTING NR 2 OVERSIZED LUG BORES AT
- [SDR REXA2026072201083](https://openairdocs.org/sdr/REXA2026072201083.md): Lug · damaged · Jul 21, 2026 · N147PQ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > "DURING THE REMOVAL OF THE RT WING SIDE AILERON BUSHINGS, IT WAS FOUND THAT THE LUG LABELED C (HINGE NR 2 INBD) WAS PREVIOUSLY OVERSIZED. ENGINEERING IS REQUIRED. LUG C BORE MEASURES (0.8985). REPAIRED RT WING AILERON HINGE FITTING NR 2 OVERSIZED LUG BORES AT
- [SDR REXA2026072301088](https://openairdocs.org/sdr/REXA2026072301088.md): Lug · damaged · Jul 6, 2026 · N147PQ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > RH AILERON HAS 1 #9 BEARING LUG MARKED E FOUND TO BE OVER SIZED UPON BEARING REMOVAL. COMPLIED WITH STEPS 1 THRU 3 OF MHIRJ REO 690-57-61-273 REV-- DATED 2022-10-13. HFEC PERFORMED IAW MHIRJ REO 690-57-61-273 REV - DATED 2022-10-13 STEP 4 NO INDICATIONS NOTED
- [SDR REXA2026072301087](https://openairdocs.org/sdr/REXA2026072301087.md): Lug · damaged · Jul 6, 2026 · N147PQ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > LH AILERON BEARING LUG MARKED E FOUND TO BE OVERSIZED UPON REMOVAL OF BEARING. RECEIVED MHIRJ REO 690-57-61-534 REV -- DATED 2026-07-11 COMPLIED WITH STEPS 1 REAM AND 2 CHAMFER IAW MHIRJ REO 690-57-61-534 REV -- DATED 2027-07-11 COMPLIED WITH STEP 1 REAM AND S
- [SDR REXA2026072001078](https://openairdocs.org/sdr/REXA2026072001078.md): Bushing · damaged · Jul 6, 2026 · N147PQ · Cndair CL6002D24 · Ailerons
  > RH AILERON 4 EACH BUSHING LUGS MARKED B, C, F AND G FOUND TO BE OVER SIZED UPON BUSHING REMOVAL. REPAIRED RH AILERON BUSHING LUGS B, C, F, AND G IAW REO 670-57-61-237 REV -- DATED 2017-07-25.
- [SDR REXA2026072001077](https://openairdocs.org/sdr/REXA2026072001077.md): Bushing · damaged · Jul 6, 2026 · N147PQ · Cndair CL6002D24 · Ailerons
  > LH AILERON FOUND 3 BUSHING LUGS MARKED C, F AND G TO BE OVER SIZED AFTER BUSHING REMOVAL REPAIRED LH AILERON BUSHING LUGS C, F, AND G IAW REO 670-57-61-237 REV -- DATED 2017-07-25.
- [SDR REXA2026072801203](https://openairdocs.org/sdr/REXA2026072801203.md): Angle · corroded · Jun 29, 2026 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > UPON REMOVAL FOUND LWR SILL ANGLE (P/N: SH670-31986-1) TO BE CORRODED AT UPPER FWD CORNER (BEYOND 90% MATERIAL MISSING) AND REQUIRE REPLACEMENT. REMOVED UNSERVICEABLE GALLY SERVICE DOOR LWR SILL ANGLE FROM MOUNTING ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 &
- [SDR REXA2026062900985](https://openairdocs.org/sdr/REXA2026062900985.md): Door · cracked · Jun 16, 2026 · N147PQ · Cndair CL6002D24 · Emergency Exits
  > R/H FWD OVERWING EMERGENCY EXIT DOOR HAS POSSIBLE CRACKS ON THE UPPER BRACKETS. REPAIRED IAW MHIRJ REO 670-52-21-103, REV --, DATE 2024-11-06
- [SDR REXA2026062600981](https://openairdocs.org/sdr/REXA2026062600981.md): Bracket · cracked · Jun 16, 2026 · N147PQ · Cndair CL6002D24 · Emergency Exits
  > RIGHT AFT OVERWING EMERGENCY EXIT DOOR HAS POSSIBLE CRACKS ON THE UPPER BRACKETS. REPAIRED RT AFT OVERWING EMERGENCY EXIT DOOR UPPER BRACKETS IAW REO 670-52-21-103, REV --.
- [SDR REXA2026062600978](https://openairdocs.org/sdr/REXA2026062600978.md): Floorbeam · cracked · Jun 16, 2026 · N147PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LEFT COCKPIT FLOORBEAM LBL12 AT BS 280 CRACKED. REINSTALLED BS 280 LT COCKPIT DOOR POST IAW SRM 51-42-06-001-001-A01, & SRM 51-42-13-001-001-A01. REMOVED SHORING FROM BS 250 BTWN S23L AND S23R IAW SRM 53-11-43-201-003-A01. INSTALLED NEW SERVICEABLE SEGMENT OF
- [SDR REXA2026062400974](https://openairdocs.org/sdr/REXA2026062400974.md): Intercostal · corroded · Jun 14, 2026 · N147PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD4 CORRODED. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR MID DD4 INTERCOSTAL. IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR MID INTERCOSTAL DD4 IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR REXA2026072001076](https://openairdocs.org/sdr/REXA2026072001076.md): Floorbeam · corroded · Jun 12, 2026 · N147PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS280 R/H CROSSBEAM HAS HEAVY PITTING CORROSION. REMOVED DAMAGED RH FS 280.00 CROSSBEAM IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-001-001-A01. CRJ900 SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW RH FS 280.00 CROSSBEAM P/N:CC670-34094JP-2S I
- [SDR REXA2026072001075](https://openairdocs.org/sdr/REXA2026072001075.md): Floorbeam · corroded · Jun 12, 2026 · N147PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS280 L/H CROSSBEAM HAS HEAVY PITTING CORROSION. REMOVED AND REPLACED DAMAGED LH FS 280.00 CROSSBEAM IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-001-001-A01. CRJ900 SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW LH FS 280.00 CROSSBEAM P/N:CC6
- [SDR REXA2026062900984](https://openairdocs.org/sdr/REXA2026062900984.md): Door · cracked · Jun 12, 2026 · N147PQ · Cndair CL6002D24 · Emergency Exits
  > LEFT FWD OVERWING EMERGENCY EXIT DOOR HAS POSSIBLE CRACKS ON THE UPPER BRACKETS. REPAIRED THE LT FWD EMERGENCY EXIT IAW REO 670-52-21-103 REV -.
- [SDR REXA2026062900983](https://openairdocs.org/sdr/REXA2026062900983.md): Angle · corroded · Jun 12, 2026 · N147PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > FS 280 FORWARD J-ANGLE IS CORRODED INSTALLED NEW J-ANGLE IAW SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01. LOCATED AND DRILLED NEW FS 280. J-ANGLE IAW SRM 51-40-11-001-001-A01.
- [SDR REXA2026062600980](https://openairdocs.org/sdr/REXA2026062600980.md): Bracket · cracked · Jun 12, 2026 · N147PQ · Cndair CL6002D24 · Emergency Exits
  > LEFT AFT OVERWING EMERGENCY EXIT DOOR HAS POSSIBLE CRACKS ON THE UPPER BRACKETS. REPAIRED LT AFT OVERWING EMERGENCY EXIT DOOR UPPER BRACKETS IAW REO 670-52-21-103, REV -.
- [SDR REXA2022111502543](https://openairdocs.org/sdr/REXA2022111502543.md): Housing · chafed · Nov 10, 2022 · N147PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > AFT CARGO DOOR HAS CHAFES AROUND OUTER HANDLE CUTOUT. REMOVED AND REPLACED IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND AMM 52-31-03-400-801-A01.
- [SDR REXA2022111102536](https://openairdocs.org/sdr/REXA2022111102536.md): Housing · chafed · Nov 10, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR HAS CHAFES AROUND OUTER HANDLE CUTOUT. REMOVED AND REPLACED IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND CRJ 900 AMM 52-31-03-400-801-A01.
- [SDR REXA2022111102488](https://openairdocs.org/sdr/REXA2022111102488.md): Angle · corroded · Nov 9, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RBL 9 ATTACHING CLIP TO "J" ANGLE CORRODED AT FS 280. FABRICATED AND INSTALLED J ANGLE ATTACHMENT CLIP ON RBL 9 TO 'J' ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
- [SDR REXA2022111102487](https://openairdocs.org/sdr/REXA2022111102487.md): Floor Support · corroded · Nov 9, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND OF FLOOR BEAM LBL9 BETWEEN FS 1026-1036. REPAIRED IAW CRJ-900 SRM 53-00-41-201-001-A03.
- [SDR REXA2022111102533](https://openairdocs.org/sdr/REXA2022111102533.md): Contact · none · Nov 8, 2022 · N147PQ · Cndair CL6002D24 · Emergency Lighting
  > "EMERGENCY LIGHT BELOW AFT L/H OVERWING EXIT DOOR IS INOP. " "FOUND BROKEN WIRE AT CONNECTOR FOR LIGHT ASSEMBLY DS102 PIN #2, REQUIRES REPAIR. REPAIRED BROKEN WIRE AT CONNECTOR FOR LIGHT ASSEMBLY BY CRIMPING SERVICEABLE CONTACT PN# B0808002-037 ONTO
- [SDR REXA2022111002431](https://openairdocs.org/sdr/REXA2022111002431.md): Skin · corroded · Nov 6, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FUSELAGE INNER SKIN AT STGR 27 BETWEEN FS 677.00 AND 693.00 CORRODED. COMPLIED WITH REO 690-53-31-678 REV -- DATED 2022-10-14.
- [SDR REXA2022111002417](https://openairdocs.org/sdr/REXA2022111002417.md): Intercostal · cracked · Nov 4, 2022 · N147PQ · Cndair CL6002D24 · Service Doors
  > WHILE REPLACING SERVICE DOOR HANDLE FOUND INTERCOSTAL CRACKED REMOVED AND REPLACED INTERCOSTAL PN:CC670-38171-13 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022110302395](https://openairdocs.org/sdr/REXA2022110302395.md): Frame · corroded · Oct 31, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME AT FS 661.00 BETWEEN STGR 17L AND 18L IS CORRODED. REPAIRED IAW REO NO 690-53-31-680 AND CRJ900 SRM 53-00-06-201-001-A03, FIG. 53-00-06-991-883.
- [SDR REXA2022110302393](https://openairdocs.org/sdr/REXA2022110302393.md): Skin · chafed · Oct 31, 2022 · N147PQ · Cndair CL6002D24 · Wing, Control Surfaces
  > RH IB FLAP LOWER SKIN HAS CHAFING FROM CONTACT WITH IB FLAP FAIRING REPAIRED RIGHT HAND LOWER INBOARD FLAP IAW CRJ900 SRM 57-52-01-201-001-A01
- [SDR REXA2022110302387](https://openairdocs.org/sdr/REXA2022110302387.md): Stiffener · cracked · Oct 31, 2022 · N147PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > VERTICAL STIFFENER ON FWD PAX DOOR WEB IS CRACKED REMOVED CRACKED STIFFENER PN: 601R317742-1 IAW CRJ-900 SRM 51-42-06-001-001-A01. AND INSTALLED NEW STIFFENER P/N 601R317742-1 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01
- [SDR REXA2022110302386](https://openairdocs.org/sdr/REXA2022110302386.md): Intercostal · corroded · Oct 31, 2022 · N147PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > INTERCOSTAL PN 601R31902-485 AT FS311-FS320 ON DATUM 6 OF PAX DOOR HAS CORROSION INSTALLED NEW INTERCOSTAL PN 601R31902-485 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2022110302383](https://openairdocs.org/sdr/REXA2022110302383.md): Intercostal · corroded · Oct 31, 2022 · N147PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > INTERCOSTAL PN 601R31902-485 AT FS311-FS320 ON DATUM 6 OF PAX DOOR HAS CORROSION INSTALLED NEW INTERCOSTAL PN 601R31902-485 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2022111502542](https://openairdocs.org/sdr/REXA2022111502542.md): Seat Track · corroded · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON SEAT TRACK RBL 9 BETWEEN F.S. 661+32-F.S. 693.00. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.
- [SDR REXA2022111102535](https://openairdocs.org/sdr/REXA2022111102535.md): Seat Track · corroded · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON SEAT TRACK RBL 9 BETWEEN F.S. 661+32-F.S. 693.00 INSTALLED NEW SEAT TRACK ON RBL 9 BETWEEN F.S. 661+32-F.S. 693.00 IAW CRJ900 AMM 53-00-49-400-801 (CONFIG A07).
- [SDR REXA2022110302403](https://openairdocs.org/sdr/REXA2022110302403.md): None · corroded · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RBL 9 ATTACHING CLIP TO "J" ANGLE CORRODED AT FS 280 FABRICATED AND INSTALLED J ANGLE ATTACHMENT CLIP ON RBL 9 TO 'J' ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
- [SDR REXA2022110302402](https://openairdocs.org/sdr/REXA2022110302402.md): Seat Track · corroded · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON SEAT TRACK RBL 9 BETWEEN F.S. 661+32-F.S. 693.00 INSTALLED NEW SEAT TRACK ON RBL 9 BETWEEN F.S. 661+32-F.S. 693.00 IAW CRJ900 AMM 53-00-49-400-801 (CONFIG A07).
- [SDR REXA2022110302401](https://openairdocs.org/sdr/REXA2022110302401.md): Post · corroded · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL 9 POST AT FS 280.00 IS CORRODED BETWEEN LH AFT WEB. REPAIRED LBL 9 POST FS 280.00 CORROSION ON LH AFT WEB PN CC670-34094JP1 AND JP2 IAW CRJ 900 SRM 53-11-10-201-004-A01
- [SDR REXA2022110302400](https://openairdocs.org/sdr/REXA2022110302400.md): None · corroded · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH FLOOR SILL BETWEEN FS 913.00 AND 969.00 IS CORRODED IN MULTIPLE LOCATIONS. REMOVED AND REPLACED LH FLOOR SILL IAW CRJ900 SRM 51-42-06-001-001-A01 AND REO 690-53-51-350 REV-- DATED 2022-10-26
- [SDR REXA2022110302399](https://openairdocs.org/sdr/REXA2022110302399.md): Stringer · corroded · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON STGR 21R BETWEEN FS 409.00-485.00. INSTALLED STR21R PN SH670-31385-1S AND FS447.40 SPLICE PN SH670-33252-1 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2022110302398](https://openairdocs.org/sdr/REXA2022110302398.md): Cleat · corroded · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON SUPPORT ANGLE AT FS 394.00 AT STGR 19L. REMOVED FABRICATED AND INSTALLED NEW STRINGER CLEAT @ FS. 394.00 STGR 19R IAW CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2022110302397](https://openairdocs.org/sdr/REXA2022110302397.md): Stringer · corroded · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON STGR 20R BETWEEN FS 364.00-379.00. REMOVED AND REPLACED NEW STRINGER P/N SH670-31405-2S AT FS 364 IAW CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2022110302396](https://openairdocs.org/sdr/REXA2022110302396.md): Stringer · corroded · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON STGR 19R BETWEEN FS295-310. REMOVED AND REPLACED STRINGER 19R FROM F.S 280-F.S 319 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022110302394](https://openairdocs.org/sdr/REXA2022110302394.md): Frame · cracked · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > L/H COCKPIT FRAME F.S.235 IS CRACKED. REPAIRED L/H COCKPIT FRAME FS 235 CRACK IAW MHIRJ REO 690-53-11-1474
- [SDR REXA2022110302392](https://openairdocs.org/sdr/REXA2022110302392.md): None · corroded · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL 9 ATTACHING CLIP TO "J" ANGLE CORRODED AT FS 280 FABRICATED AND INSTALLED J ANGLE ATTACHMENT CLIP ON RBL 9 TO 'J' ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
- [SDR REXA2022110302390](https://openairdocs.org/sdr/REXA2022110302390.md): Frame · corroded · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME AT FS 927.00 IS CORRODED BETWEEN STGR 25R AND 26R. COMPLIED WITH SPLICE REPAIR OF FS 927.00 BETWEEN STGR 25R AND 26R IAW CRJ 900 SRM 53-00-06-201-001-A03.
- [SDR REXA2022110302389](https://openairdocs.org/sdr/REXA2022110302389.md): Stringer · corroded · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 20R BETWEEN FS 597.00 AND 613.00 IS CORRODED. COMPLIED WITH STRINGER SPLICE REPAIR ON STRINGER 20R BETWEEN FS 597.00 AND FS 613.00 IAW CRJ-900 SRM 53-00-03-201-001-A02 REPAIR S6295 TYPE Z8 REPAIR.
- [SDR REXA2022110302388](https://openairdocs.org/sdr/REXA2022110302388.md): Frame · cracked · Oct 30, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME AT FS 645.00 BETWEEN STGR 17L AND 18L IS CORRODED. REMOVED AND INSTALLED NEW SECTION FRAME AND SPLICE REPAIR ON FS645 BETWEEN STR16LH-STR18LH IAW REO NO 690-53-31-680 DATE 2022-10-14, AND SRM 53-00-06-201-001-A03, FIGURE 53-00-06-991-879, 51-42-06-001-00
- [SDR REXA2022110302391](https://openairdocs.org/sdr/REXA2022110302391.md): Stringer · corroded · Oct 29, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON STGR 26L BETWEEN FS 1015.00-1031.00 REPAIRED STGR 26L IAW MHIRJ REO 690-53-61-1126 REV. --, DATED 2022-10-24.
- [SDR REXA2022110302385](https://openairdocs.org/sdr/REXA2022110302385.md): Beam · corroded · Oct 28, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > TOP OF FLOOR BEAM AT RBL9 BETWEEN FS 693.00 AND 847.00 IS CORRODED IN MULTIPLE LOCATIONS. REPAIRED TOP OF FLOOR BEAM AT RBL 9 BETWEEN FS693.00 AND 847.00 CORROSION IAW MHIRJ REO 690-53-41-331 REV -- DATED 2022-10-21
- [SDR REXA2022110302404](https://openairdocs.org/sdr/REXA2022110302404.md): Bracket · cracked · Oct 22, 2022 · N147PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > FOUND PAX DOOR AFT HANDRAIL TO HAVE BROKEN SPRING BRACKET THAT KEEPS HANDRAIL LOCKED IN PLACE BROKEN. REMOVED AND REPLACE PAX DOOR AFT HANDRAIL SPRING BRACKET PN# 601R38587-19 PO# W 79466 IAW CRJ 900 SRM 51-42-06-001-001-A01 & CRJ 900 SRM 51-21-16-001-001-A01
- [SDR REXA2022110102347](https://openairdocs.org/sdr/REXA2022110102347.md): Cleat · corroded · Oct 22, 2022 · N147PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > CLEAT AT INTERSECTION OF FS320.16 AND DD6 IS CORRODED. REMOVED AND REPLACED CLEAT PN: 600-31902-269 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2022102802319](https://openairdocs.org/sdr/REXA2022102802319.md): Intercostal · corroded · Oct 22, 2022 · N147PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN FS 311-320 ON DATUM 2 HAS CORROSION. INSTALLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022102802318](https://openairdocs.org/sdr/REXA2022102802318.md): Stiffener · cracked · Oct 22, 2022 · N147PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR AFT STAIR WEB STIFFENER, SECOND UP FROM THE LATCH END OF THE STAIR IS CRACKED. INSTALLED NEW STIFFENER PN:601R317747-1 IAW CRJ 900 SRM 51-42-06-001-001-A01

Next page: https://openairdocs.org/aircraft/N147PQ/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 = 'N147PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N147PQ/reports

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