# Service difficulty reports: N166PQ

A list on [N166PQ](https://openairdocs.org/aircraft/N166PQ.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 · 155 reports

- [SDR REXA2025062600686](https://openairdocs.org/sdr/REXA2025062600686.md): Charger · inoperative · Jun 25, 2025 · N166PQ · Cndair CL6002D24 · Emergency Lighting
  > RH AFT OVERWING EMERGENCY LIGHT INOP REMOVED AND REPLACED BATTERY CHARGER IAW AMM 33-51-17 P/N ON/OFF 11-0049 S/N OFF 22880 S/N ON 25853 ALSO REMOVED AND REPLACED EXTERNAL LIGHT IAW AMM 33-51-15 P/N ON/OFF 2LA006454-00
- [SDR REXA2025062600685](https://openairdocs.org/sdr/REXA2025062600685.md): Terminal · shorted · Jun 25, 2025 · N166PQ · Cndair CL6002D24 · Light System Wiring
  > WHILE PERFORMING LINE-900, RIGHT AFT EMERGENCY EXIT EMERGENCY LIGHT INOP. FOUND SHORTED FROM P5424 PIN H TO + TERM ON LIGHT DS101. OK TO DEFER IAW MEL 33-51-2A. MM02 UPDATED, PLACARD INSTALLED, MOC NOTIFIED #43294. REMOVED AND REINSTALLED AFT OVERWING EMERGAN
- [SDR REXA2024122701611](https://openairdocs.org/sdr/REXA2024122701611.md): Lamp · inoperative · Dec 26, 2024 · N166PQ · Cndair CL6002D24 · Emergency Lighting
  > LH AFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LH AFT OVERWING EMERGENCY LIGHT IAW AMM 33-51-15. OP'S CHECKS CONDUCTED AND CHECK GOOD. NO FURTHER DEFECTS AT THIS TIME.
- [SDR REXA2024121301584](https://openairdocs.org/sdr/REXA2024121301584.md): Latch · dirty · Dec 12, 2024 · N166PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > UPON PARKING AT THE GATE IN LGA FA TRIED TO OPEN PASSENGER DOOR & THE DOOR WOULD NOT OPEN. HANDLE STUCK. CLEANED & LUBED PAX DOOR LATCH PINS & LATCH CAMS IAW CRJ 900 AMM 12-20-52. PERFORMED OPS CHECK ON PAX DOOR IAW CRJ 900 AMM 52-11-00. OPS TEST GOOD. A/C OK
- [SDR REXA2024100900863](https://openairdocs.org/sdr/REXA2024100900863.md): Lamp · inoperative · Oct 8, 2024 · N166PQ · Cndair CL6002D24 · Emergency Lighting
  > EMER EXIT SIGN BY SERVICE DOOR HAS BURNT OUT BULBS RELAMPED EMER EXIT SIGN BY SERVICE DOOR IAW CRJ900 AMM 33-51-07 OPS CHECK GOOD P/N ON/OFF:3071BPEGPL
- [SDR REXA2024080500606](https://openairdocs.org/sdr/REXA2024080500606.md): Connector · unsecure · Jul 28, 2024 · N166PQ · Cndair CL6002D24 · Light System Wiring
  > FOUND RH EXIT LIGHTS AT EMERGENCY EXITS INOP INSTALLED SEATS 11CD AND 12CD IAW CRJ 900 AMM 25-21-01-400-804-A06 INSTALLED WALL PANELS 262PRW AND 262NRW IAW CRJ 900 AMM 25-26-09-400--801-A02. INSTALLED CEILING PANELS 263PLC 264PRC AND 263NLC IAW CRJ 900 A
- [SDR REXA2024093000737](https://openairdocs.org/sdr/REXA2024093000737.md): Stringer Clip · corroded · Jul 7, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > "UPON REMOVAL OF STRINGER 23R CLEAT COMMON TO FS693.00 FRAME, FOUND CORROSION AROUND FASTENER HOLES AND REQUIRES REPLACEMENT. REMOVED AND REPLACED STRINGER ""CLEAT"" (PN: SH670-35904-4) IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-24-21-00
- [SDR REXA2024100300774](https://openairdocs.org/sdr/REXA2024100300774.md): Striker · deformed · Jun 20, 2024 · N166PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > FOUND 3EA HOLES TO BE ELONGATED IN PAX DOOR SILL ANGLE. (1EA THROUGH FWD HANDRAIL FITTING AFT OTBD HOLE, 1EA HOLE THROUGH AFT HANDRAIL FITTING FWD OTBD HOLE, AND 1EA HOLE 5 HOLES BACK FROM FWD EDGE OF SILL ANGLE.) ALL ARE CIRCLED IN RED. REPAIRED PASSENGER DOO
- [SDR REXA2024061400442](https://openairdocs.org/sdr/REXA2024061400442.md): Intercostal · corroded · Jun 14, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVIONICS BAY DOOR SURROUND STRUCTURE AT FS 401-403 LBL 2 ON BOTTOM FLANGE OF INTERCOSTAL IS CORRODED. AVI-BAY DOOR SURROUND STRUCTURE INTERCOSTAL AT F.S. 394 - F.S. 409 LBL 2 FOUND TO BE CORRODED OUT OF LIMITS DUE TO NO DAMAGE ALLOWED IAW CRJ-900 SRM 53-21-23-
- [SDR REXA2024080100603](https://openairdocs.org/sdr/REXA2024080100603.md): Intercostal · corroded · Jun 10, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > R/H INTERCOSTAL AT NOSE JACKING FITTING IS CORRODED. REMOVED AND REPLACED INERCOSTAL IAW EOCRJ953-16804 REV A DATED 7/14/2024
- [SDR REXA2024071600537](https://openairdocs.org/sdr/REXA2024071600537.md): Frame · corroded · Jun 10, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > "FUSELAGE FRAME 847+32 IS CORRODED BETWEEN STGR 26R TO STGR 26L. REMOVED CORROSION AT FRAME FS 847+32 BTW STR 26L - 26R IAW CRJ 900 SRM 51-21-06-001-001-A01 ORIGINAL MATERIAL THICKNESS IS 0.063"". FRAME AT 847+32 FOUND TO BE OUT OF LIMITS IAW CRJ-900 SRM 53-
- [SDR REXA2024071600535](https://openairdocs.org/sdr/REXA2024071600535.md): Angle · corroded · Jun 10, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL ANGLE IS CORRODED. UPON FURTHER INVESTIGATION, FOUND PAX DOOR KICKPLATE ANGLE P.N. SH670-31875-3 TO BE OUT OF LIMITS IAW CRJ900SRM TASK 53-21-23-101-001-A02 DUE TO 100% COVERAGE ACROSS ALL ELEMENTS. REMOVED OUT OF LIMITS PAX DOOR KICKPLAT
- [SDR REXA2024071100516](https://openairdocs.org/sdr/REXA2024071100516.md): Stringer · corroded · Jun 10, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 19R IS CORRODED BETWEEN FS 581.00 AND 613.00. REMOVED STRINGER 19R FROM F.S. 477 TO F.S. 661+90 IAW CRJ-900 SRM 51-42-06-001-001-A01 LOCATED AND DRILLED NEW STRINGER P/N SH690-33151-5A IAW CRJ900 SRM 51-40-11-001-001-A01 INSTALLED NEW STRINGER 19
- [SDR REXA2024071000514](https://openairdocs.org/sdr/REXA2024071000514.md): Stringer Splice · corroded · Jun 10, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "STGR 18R IS CORRODED BETWEEN F.S. 421 TO F.S. 477. REMOVED AND REPLACED STRINGER 18R SEGMENT FROM FS364 AND FS477 IAW CRJ900SRM 51-42-06-001-001-A01. PAINTED NEWLY FABRICATED STRINGER 18R SEGMENT FROM FS379 AND FS 477 IAW CRJ900SRM 51-25-06-001-001-A01 AN
- [SDR REXA2024070900513](https://openairdocs.org/sdr/REXA2024070900513.md): Stringer Splice · corroded · Jun 10, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 20R SPLICE IS CORRODED BETWEEN F.S. 469 TO F.S. 501. REMOVED DAMAGED STRG20R SPLICE AT FS477 IAW CRJ900 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED UP NEW SERVICEABLE STRG 20R FS 477 CIRCUMFERENTIAL JOINT PN SH 670-33264-1 AS REQUIRED IAW CRJ 900 SRM
- [SDR REXA2024070300495](https://openairdocs.org/sdr/REXA2024070300495.md): Stringer · corroded · Jun 10, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 18R HAS HEAVY PITTING (CORROSION) BETWEEN FS 517 TO 533. INSTALLED NEW STGR 18R SEGMENT FROM FS 477 - FS 533 THROUGH THE SKIN IAW CRJ 900 SRM 51-42-06-001-001-A01 FABRICATED, LOCATED AND DRILLED STRINGER 18R REPAIR SPLICE BETWEEN FS533.00 AND FS549.
- [SDR REXA2024070300494](https://openairdocs.org/sdr/REXA2024070300494.md): Stringer · corroded · Jun 10, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R HAS A DEEP SPOT OF CORROSION BETWEEN FS 501 TO 517. REPAIRED IAW CRJ 900 SRM 53-00-03-201-001-A02.
- [SDR REXA2024070300493](https://openairdocs.org/sdr/REXA2024070300493.md): Stringer Splice · corroded · Jun 10, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 22R SPLICE IS CORRODED AT FS 477. INSTALLED NEW STRINGER SPLICE P/N SH670-33252-1 R22 @ FS 477 IAW CRJ-900 SRM 51-42-06-001-001-A01 STRG 22R SPLICE @FS477 FASTENERS PAINTED AND APPLIED CIC IAW CRJ900 SRM 51-25-16-001-001-A01 AND 51-21-11-001-001-A0
- [SDR REXA2024070300491](https://openairdocs.org/sdr/REXA2024070300491.md): Stringer Splice · corroded · Jun 10, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 21R SPLICE A@ F.S. 477 FOUND TO BE CORRODED. INSTALLED STRINGER SPLICE @FS 477 S21R IAW CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2024070300490](https://openairdocs.org/sdr/REXA2024070300490.md): Stringer · corroded · Jun 10, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 21R IS CORRODED BETWEEN F.S. 409 TO F.S. 421. REMOVED STRINGER 21R P/N SH670-31385-1 FROM F.S 394 TO F.S 477. LOCATED AND DRILLED NEW STGR 21R (PN: SH670-31385-1) IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE STRINGER 21R PN ( SH670-313
- [SDR REXA2024062000448](https://openairdocs.org/sdr/REXA2024062000448.md): Bushing · corroded · Jun 10, 2024 · N166PQ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > "THE R/H AILERON HAS CORROSION & PITTING INSIDE OF THE LUG BORE LABELED ""B"". REMOVAL OF DAMAGE IS REQUIRED. COMPLIED WITH STEPS F. #1 - #4 OF BOMBARDIER REO 670-57-61-237 REV - DATED 2017-07-25. STEP F. #3 - FINAL REAMED DIAMETER OF LUG ""B"" IS (0.9538"").
- [SDR REXA2024062000447](https://openairdocs.org/sdr/REXA2024062000447.md): Lug · corroded · Jun 10, 2024 · N166PQ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > "THE L/H AILERON HAS CORROSION & PITTING INSIDE OF THE LUG BORE LABELED ""C"". REMOVAL OF DAMAGE IS REQUIRED. REPAIRED IAW REO 670-57-61-237 REV -- DATED 2017-07-25 REFERENCE HR0043033 FOR INSTALLATION OF FABRICATED BUSHING"
- [SDR REXA2024102501008](https://openairdocs.org/sdr/REXA2024102501008.md): Frame · corroded · Jun 9, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME CORRODED AT FS 310 FROM STGR 26L TO 27L ON FWD AND AFT FACE. REPAIRED IAW CRJ900 SRM 53-00-06-201-004-A01.
- [SDR REXA2024102501007](https://openairdocs.org/sdr/REXA2024102501007.md): Intercostal · corroded · Jun 9, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVIONICS BAY DOOR SURROUND STRUCTURE AT FS 399 RBL 2 ON BOTTOM FLANGE OF INTERCOSTAL IS CORRODED.. AVI-BAY DOOR SURROUND STRUCTURE INTERCOSTAL AT F.S. 394 - F.S. 409 RBL 2 FOUND TO BE CORRODED OUT OF LIMITS DUE TO NO DAMAGE ALLOWED IAW CRJ-900 SRM 53-21-23-10
- [SDR REXA2024071600534](https://openairdocs.org/sdr/REXA2024071600534.md): Stringer · corroded · Jun 9, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "STRINGER 20R IS CORRODED BETWEEN FS 501.00 AND 613.00. FOUND STRINGER 20R TO BE CORRODED BETWEEN FS 477 AND 613. STGR 20R PN: (SH690-33314-1) FROM FS 477.40- 613 REQUIRES REPLACEMENT. DUE TO MULTIPLE DEEP PITS THROUGHOUT AND STGR 20R BEING A NO ALLOWABLE DA
- [SDR REXA2024071600533](https://openairdocs.org/sdr/REXA2024071600533.md): Frame · corroded · Jun 9, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > FS 693 PARTIAL BULKHEAD BOTTOM CAP ANGLE CORRODED AT RBL27 REMOVED AND REINSTALLED DUCT BRACKET ATTACHED TO STRINGER 24R BETWEEN FS 677 TO 693, SERVICEABLE STRINGER TO FRAME CLEATS COMMON TO FS693 FRAME AT STRINGERS 21L, 22L, 23L, 24L, 25L,26L, 26R, 25R, 24R
- [SDR REXA2024071600532](https://openairdocs.org/sdr/REXA2024071600532.md): Stringer · corroded · Jun 9, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L CORRODED BETWEEN FS985 AND FS1000 REMOVED STGR 26L FROM FS 977.00 TO FS 1098.00 IAW CRJ900 SRM 51-42-06-001-001-A01. AND CRJ900 SRM 51-42-21-001-001-A01. LOCATED AND DRILLED NEW STRINGER 26L P/N MM670-35151-59 AT PRODUCTION SPLICE AND 8 EA. STRI
- [SDR REXA2024070300489](https://openairdocs.org/sdr/REXA2024070300489.md): Door Frame · cracked · Jun 9, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > LH AFT EMERGENCY EXIT DOOR (S/N: SB0683) CRACKED ALONG UPPER FORMER AT AFT LUG REPAIRED LH AFT EMERGENCY EXIT DOOR (S/N: SB0683) CRACK ALONG UPPER FORMER AT AFT LUG IAW REO 690-52-21-171 REV -- DATED 06/12/2024.
- [SDR REXA2024073000582](https://openairdocs.org/sdr/REXA2024073000582.md): Fitting · chafed · May 29, 2024 · N166PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > FOUND PASENGER DOOR AFT CAM FITTING TO BE CHAFED. INSTALLED NEW FWD CAM FITTING P/N SH670-31913-3 IAW CRJ900 AMM 53-21-23-400-808 (CONFIG A01). I
- [SDR REXA2024073000565](https://openairdocs.org/sdr/REXA2024073000565.md): Fitting · chafed · May 29, 2024 · N166PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > FOUND PASENGER DOOR FWD CAM FITTING TO BE CHAFED. INSTALLED NEW FWD CAM FITTING P/N SH670-31913-4 IAW CRJ900 AMM 53-21-23-400-808 (CONFIG A01). I
- [SDR REXA2024071600529](https://openairdocs.org/sdr/REXA2024071600529.md): Stringer · corroded · May 29, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 20R IS CORRODED BETWEEN F.S. 421 TO F.S.477. UPON FURTHER INVESTIGATION FOUND CORROSION PRESENT ON STGR 20R (P/N:SH670-31405-- 2) FROM FS 349 - FS 477 AND REQUIRES REPLACEMENT. DUE TO MULTIPLE DEEP PITS THROUGHOUT AND STGR20R BEING A NO ALLOWABLE DAMAGE
- [SDR REXA2024071600528](https://openairdocs.org/sdr/REXA2024071600528.md): Angle · corroded · May 29, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR MID CAP ANGLE IS CORRODED. REMOVED AND REPLACED PAX DOOR MID CAP ANGLE P.N. SH670-31825-7 IAW CRJ900SRM 51-41-02-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE MID CAP ANGLE P/N: SH670-31825-9 ON PAX DOOR IAW CRJ900SRM 51-40-11-001-001-A01. PAX DOO
- [SDR REXA2024071600525](https://openairdocs.org/sdr/REXA2024071600525.md): Door Frame · cracked · May 29, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > RH AFT EMERGENCY EXIT DOOR (S/N: SB0681) CRACKED ALONG UPPER FORMER AT AFT LUG. REPAIRED RH AFT EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA CRJ952-16695 REV IR DATED 6/7/2024.
- [SDR REXA2024071600524](https://openairdocs.org/sdr/REXA2024071600524.md): Door Frame · cracked · May 29, 2024 · N166PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > RH FWD EMERGENCY EXIT DOOR (S/N: SB0682) CRACKED ALONG UPPER FORMER AT AFT LUG REPAIRED RH FWD EMERGENCY EXIT DOOR (S/N: SB0682) IAW ENDEAVOR AIR EA CRJ952-16696 DATED 6/5/2024 REV IR.
- [SDR REXA2020010710042](https://openairdocs.org/sdr/REXA2020010710042.md): Hinge Fitting · cracked · Jan 1, 2020 · N166PQ · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > "DAMAGE T: DURING LH ENGINE COWLS CLOSE UP THE FAIRING 433BB HIT THE LWR TRANSCOWL INBD FAIRING. BOTH THE TRANSCOWL FAIRING AND THE FAIRING 433BB ARE BENT AND WITH SCRATCHES. "TRANSCOWL HINGE FAIRING WAS REPAIRED PER CRJ-9
- [SDR REXA2020010710041](https://openairdocs.org/sdr/REXA2020010710041.md): Housing · cracked · Jan 1, 2020 · N166PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > "AWR HIDDEN DAMAGE: CRACKED HOUSING BEARING OF LOWER TORQUE TUBE AT MAIN PASSENGER DOOR IN REF 00374. "SUMMARY OF NRC 425: HOUSING WAS REPLACED PER CRJ-900 SRM 51-42-21 AND CMM 52-11-00
- [SDR REXA2020010710008](https://openairdocs.org/sdr/REXA2020010710008.md): Retainer · bent · Dec 31, 2019 · N166PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > "INITIAL INSPECTION: BENT ON INNER RETAINER OF PRESSURE SEAL AT CENTER BAGGAGE BAY DOOR ( CCD) "SUMMARY: LOWER PLATE OF THE CENTER BAGGAGE BAY DOOR SEAL WAS REPLACED PER CRJ-900 AMM 52-35-07-400-802 (CONF A02) AN
- [SDR REXA2020010710007](https://openairdocs.org/sdr/REXA2020010710007.md): Retainer · bent · Dec 31, 2019 · N166PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > "INITIAL INSPECTION: BENT ON INNER AND OUTER RETAINERS OF PRESSURE SEAL AT FWD BAGGAGE BAY DOOR ( CCD) "SUMMARY: DAMAGE ON LOWER SEAL WAS REMOVED PER CRJ-900 SRM 52-35-07-201-001-A01 PAR. 6 B.(3), NEW INNER RETAINER (LOW
- [SDR REXA2020010723034](https://openairdocs.org/sdr/REXA2020010723034.md): Stringer · corroded · Dec 30, 2019 · N166PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "AWR HIDDEN DAMAGE: AFTER REMOVE INSULATION ON MAIN AVIONICS COMPARTMENT, CORROSION ON STGR 19R BTW FS280/310 WAS FOUND IN REF EO: R25120 (SM)[E/E]. "SUMMARY OF NRC 00366: CORRODED AREA ON STGR 19
- [SDR REXA2020010729013](https://openairdocs.org/sdr/REXA2020010729013.md): Stringer · corroded · Dec 29, 2019 · N166PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "INITIAL INSPECTION: (DUE WET INSULATIONS) MAIN AVIONICS COMPARTMENT, CORROSION ON STGR 26L FROM FS295/FS349 (SM)[E/E]. "SUMMARY: OF NRC. 00221 CORROSION LEVEL 2. STRINGERS 26 LH FS=280 TO FS=364 WERE REPLACED PER CRJ-900 SRM 51-42-06-00
- [SDR REXA2020010729011](https://openairdocs.org/sdr/REXA2020010729011.md): Stringer · corroded · Dec 29, 2019 · N166PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "INITIAL INSPECTION: (DUE WET INSULATIONS) MAIN AVIONICS COMPARTMENT, CORROSION ON STGR 26R FROM FS295/FS364 (SM)[E/E]. "SUMMARY: OF NRC. 00219 CORROSION LEVEL 2. STGR 26 RH FROM FS294/FS333 AND FS333/FS364 WERE REPLACED PER CRJ-900 SRM
- [SDR REXA2020010728040](https://openairdocs.org/sdr/REXA2020010728040.md): Angle · cracked · Dec 28, 2019 · N166PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "LATE FINDING: PART RACKS: CRACKED ANGLE AT ACCESS PANEL NBR 195DL FUSELAGE ( FUS) "SUMMARY: ON NRC 404:ANGLE WAS REPLACED PER PER CRJ-900 SRM 51-42-13-001-001-A01 AND EO R53573 REVISION 2
- [SDR REXA2020010728037](https://openairdocs.org/sdr/REXA2020010728037.md): Stringer · corroded · Dec 28, 2019 · N166PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "AWR HIDDEN DAMAGE: AFTER REMOVE INSULATION ON MAIN AVIONICS COMPARTMENT, CORROSION ON STGR 22R BTW FS295/349 AND ANGLE WAS FOUND IN REF EO: R25120 (SM)[E/E]. "SUMMARY: CORROSION LEVEL 2, STGR 22RH FS280 TO
- [SDR REXA2020010728036](https://openairdocs.org/sdr/REXA2020010728036.md): Stringer · corroded · Dec 28, 2019 · N166PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "AWR HIDDEN DAMAGE: AFTER REMOVE INSULATION ON MAIN AVIONICS COMPARTMENT, CORROSION ON STGR 21R BTW FS280/349 AND SPLICE WAS FOUND IN REF EO: R25120 (SM)[E/E]. ""SUMMARY: CORROSION LEVEL 2, STGR 21R BTW FS28
- [SDR REXA2020010727038](https://openairdocs.org/sdr/REXA2020010727038.md): Intercostal · corroded · Dec 27, 2019 · N166PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "AWR HIDDEN DAMAGE: AFTER REMOVE INSULATION ON MAIN AVIONICS COMPARTMENT, CORROSION ON INTERCOSTAL AT STGR 20R BTW FS310/364 WAS FOUND IN REF EO: R25120 (SM)[E/E]. "SUMMARY: CORROSION LEVEL 2, INTERCOSTALS AT ST
- [SDR REXA2020010720018](https://openairdocs.org/sdr/REXA2020010720018.md): Intercostal · corroded · Dec 27, 2019 · N166PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION: (DUE WET INSULATIONS) MAIN AVIONICS COMPARTMENT, CORROSION ON INTERCOSTALS (4 E/A) BTW FS349/FS364 AND STGR 26L/26R (SM)[E/E]. "SUMMARY: CORROSION LEVEL 2, INTERCOSTALS (4 E/
- [SDR REXA2020010720017](https://openairdocs.org/sdr/REXA2020010720017.md): Frame · corroded · Dec 27, 2019 · N166PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > "INITIAL INSPECTION: (DUE WET INSULATIONS) MAIN AVIONICS COMPARTMENT, CORROSION ON FRAME FS 349 BTW STGR 25L/25R (SM)[E/E]. "SUMMARY OF NRC 00232 CORROSION LEVEL 2:FRAME SECTION AT FS 349 AND BTW STRINGER 23LH TO 23RH WAS REPLACED PER CRJ-90
- [SDR REXA2020010770006](https://openairdocs.org/sdr/REXA2020010770006.md): Grill · cracked · Dec 27, 2019 · N166PQ · Cndair CL6002D24 · Smoke Detection
  > "INITIAL INSPECTION: CRACKED AND BENT ON SMOKE DETECTOR UPPER GRILLS BTW STA FS460 TO FS581 ( 2EA) AND FS613 TO FS661+90 ( 3EA) AT FWD BAGGAGE BAY ( CCD) "SUMMARY:ON NRC 00116: SMOKE DETECTOR UPPER GRI
- [SDR REXA2020010770005](https://openairdocs.org/sdr/REXA2020010770005.md): Spigot · worn · Dec 27, 2019 · N166PQ · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > "INITIAL INSPECTION: WEAR ON SPIGOT AT LATCH DOOR ASSEMBLY OF LOWER HALF TRANSCOWL LH ENGINE ( MOT 1) "SUMMARY OF NRC 00049: SPIGOT AT LATCH DOOR ASSEMBLY OF LOWER HALF TRANSCOWL LH ENGINE WAS REPLACED PER CRJ-900 SRM 5
- [SDR REXA2020010700002](https://openairdocs.org/sdr/REXA2020010700002.md): Latch · damaged · Dec 27, 2019 · N166PQ · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > "INITIAL INSPECTION: ELONGATED HOLE ON COAMING LATCH DOOR AT LOWER HALF TRANSCOWL RH ENGINE ( MOT 2) "SUMMARY: ON NRC. 00038 COAMING LATCH DOOR, DOUBLER COAMING LATCH DOOR AND PAD BEARINGAT ON LOWER HALF TRANSCOWL RH E

Next page: https://openairdocs.org/aircraft/N166PQ/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 = 'N166PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N166PQ/reports

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