N176PQ

Service difficulty reports · 180

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR REXA2018070200594Life Vest · missingLIFE VEST MISSING 12C. INSTALLED LIFE VEST IAW AMM 25-61-03 AS REQUIRED.Jul 2, 2018 · N176PQ · Cndair CL6002D24 · Life JacketSDR REXA2018052700421Light · inoperativeFLOOR LEVEL EXIT SIGNS HAVE A FEW BURNT OUT. BULBS REPLACED ALL BURNED OUT LAMPS AND OPS CHECKS GOOD IAW AMM 33-51-00.May 27, 2018 · N176PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2018052700419Oxygen Mask · damagedOXYGEN MASK HOSE IS DAMAGED DUE TO KINKING IN FWD LAV. REMOVED AND REPLACED DAMAGED OXYGEN MASK IN FWD LAVATORY PER AMM 35-21-09. PN ON/OFF: 289-301-066-2 SN ON/OFF: NSNMay 27, 2018 · N176PQ · Cndair CL6002D24 · Passenger Oxygen SystemSDR REXA2018052700418Oxygen Mask · damagedHOSE TO BOTH FWD FA O2 MASKS ARE DAMAGED DUE TO KINKING. INSTALLED 2 OXYGEN MASKS ASSY PN 289-601-066-2 AT FWD FLIGHT ATTENDANT POSITION IAW AMM 35-21-09.May 27, 2018 · N176PQ · Cndair CL6002D24 · Passenger Oxygen SystemSDR REXA2018012300095Strut · deflatedAFTER TAKEOFF, A STEERING INOPERATIVE CAUTION MESSAGE DISPLAYED. A VIBRATION FELT IN NOSE. AFTER APPROXIMATELY 20 SECONDS, A GEAR DISAGREE WARNING MESSAGE. FOLLOWED QRH. VIBRATION FELT UNTIL GEAR HANDLE WAS PUT DOWN & HYD PUMP 3B TURNED ON VIA QRH CHECKLIJan 23, 2018 · N176PQ · Cndair CL6002D24 · Nose/Tail Landing Gear Strut/AxleSDR REXA2017111101167Light · malfunctionedEMERGENCY LIGHT INOPERATIVE. FORWARD CABIN LIGHTS COME ON MOMENTARILY,THEN GO OUT. AFT CABIN LIGHT STAY ON. PERFORMED OPS CHECK OF THE EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD.Nov 11, 2017 · N176PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2017110501157Battery Pack · inoperativeMX NOTED DURING WAKE-UP CHECKLIST THE FIRST OFFICER`S FLASHLIGHT BATTERY DISCHARGED. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-61-02. OPS TESTED GOOD IAW AMM 25-61-00.Nov 5, 2017 · N176PQ · Cndair CL6002D24 · Emergency EquipmentSDR REXA2017101401144Mount Bracket · crackedAFT CARGO DOOR FWD DOOR TRACK CENTER MOUNT BRACKET CRACKED. REMOVED & REPLACED NE BRACKET AT AFT CARGO DOOR FWD DOOR TRACK. CENTER MOUNT TREATED AND TOP COAT, IAW SRM 53-61-58 PG 6 ITEM 8, SRM 51-21-11 + SRM 51-42-06.Oct 14, 2017 · N176PQ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR ASOA201701161065Engine · vibrationON T/O LEFT ENGINE VIBE AT 2.1 - RETURN TO ATL. REMOVED BLADES, PINS AND BUMPERS. PERFORMED GENERAL VISUAL INSPECTION OF FAN BLADES. RE-MAPPED FAN BLADES, LUBRICATED RETAINING PINS, INSTALLED FAN BLADES, PERFORMED CHECK OF THE ENGINE N1 VIBRATION LEVEL IAW TASJan 16, 2017 · N176PQ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR ASOA2016081015232Skin · damagedFUSELAGE DAMAGE BETWEEN BS 1031 AND 1051 BETWEEN STRINGERS 21 - 27R. BLENDED IAW SRM 51-12-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-61-01. T MAJOR REPAIR IAW GMM 5-3.Aug 10, 2016 · N176PQ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR ASOA2016013114429Smoke Detector · false indicationFWD LAV SMOKE WARNING MSG IN FLIGHT. COMPLIED WITH QRH NO SMOKE DETECTED. R & R FWD LAV SMOKE DETECTOR IAW AMM 26-16-01. OPS TEST GOOD AT THIS TIME.Jan 31, 2016 · N176PQ · Cndair CL6002D24 · Smoke DetectionSDR ASOA2016011214338Smoke Detector · false indicationSMOKE FWD LAV MESSAGE DURING FLIGHT, ENROUTE. ACFT DIVERTED DUE TO MAINTENANCE, LAVATORY SMOKE DETECTION SYSTEM. PERFORMED OPS CK OF FWD LAV SMOKE DETECTOR IAW AMM 26-16-00. OPS CHECKED GOOD. COULD NOT DUPLICATE.Jan 12, 2016 · N176PQ · Cndair CL6002D24 · Smoke DetectionSDR ASOA2016010714313Door Frame · chafedLEFT NLG DOOR BONDING WIRE HAS CHAFED INTO THE FRAME. BLENDED DAMAGE TO AIRFRAME IAW SRM 51-12-00. RECEIVED AND COMPLIED WITH STS EA 20-2016-006 . REPAIR IS PERMANENT AND CLASSIFIED AS MINOR.Jan 7, 2016 · N176PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR ASOA2015091113735Light · missingEMERGENCY LIGHT STRIP BY GALLEY 3 CART MISSING. INSTALLED EMERGENCY LIGHT IAW AMM IAW 33-51-01.Sep 11, 2015 · N176PQ · Cndair CL6002D24 · Emergency LightingSDR ASOA2015050812786Door Sill · corrodedCORROSION ON SERVICE DOOR LOWER SILL ANGLE, BELOW CAP ANGLE. REMOVED THE GALLEY DOOR FLOOR PROTECTOR MOUNTING ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW LOWER SILL ANGLE AT SERVICE DOOR IAW SRM 51-42-06-001-001-A01.Apr 18, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015050812785Floorbeam · crackedRIGHT COCKPIT FLOORBEAM IS CRACKED. RECEIVED REO 690-53-11-752 FORMED AND HEAT TREATED REPAIR ANGLE -2 IAW SRM 51-24-06-001-001-A01. FORMED AND HEAT TREATED ANGLE -8 IAW SRM 51-24-06-001-001-A01. COMPLIED WITH REO 690-53-11-752. COMPLIED WITH ECTC REO 690-Apr 16, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR ASOA2015050812784Floorbeam · crackedLEFT COCKPIT FLOORBEAM IS CRACKED. RECEIVED REO 690-53-11-752 FORMED AND AND HEAT TREATED REPAIR ANGLE -1 IAW SRM 51-24-06-001-001-A01. FORMED AND HEAT TREATED ANGLE -7 IAW SRM 51-24-06-001-001-A01. COMPLIED WITH REO 690-53-11-752. COMPLIED WITH ECTC REO 6Apr 16, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR ASOA2015050812783Skin · dentedRUDDER DENTED ON LOWER RT SIDE BETWEEN RIB'S 3 & 4. COMPLIED WITH APPLICABLE REPAIR IAW SRM 51-41-01-201-001-A01. FOUND HINGE LINE WEIGHT ROTATIONAL INERTIA INCREASE TO BE WITHIN LIMTS. = 432.18 LBF TECH: 570634, DATE: 4-17-15. RECEIVED EC/TC AND COMPLIED WApr 16, 2015 · N176PQ · Cndair CL6002D24 · Rudder, Plate/SkinSDR ASOA2015050812782Bulkhead Web · corrodedRIGHT 280 WEB CORRODED. COMPLIED WITH ECTC REO 670-53-11-59401 AND GREO 670-53-11-594, REV--.Apr 14, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Main, BulkheadSDR ASOA2015050812781Bulkhead Web · corrodedLEFT 280 WEB CORRODED. COMPLIED WITH ECTC REO 670-53-11-59401 AND GREO 670-53-11-594, REV-- .Apr 14, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Main, BulkheadSDR ASOA2015050812780Lens · crackedPANEL 262NRW EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED CRACKED EMERGENCY EXIT LIGHT LENS. REPLACED EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-05-05-400-801-A13 4L, 4.Apr 14, 2015 · N176PQ · Cndair CL6002D24 · Emergency LightingSDR ASOA2015050812779Attach Angle · crackedRT LOWER 280 WEB ATTACH ANGLE AT BL26.00 IS CRACKED. REMOVED RT LOWER 280 WEB ATTACH ANGLE AT RBL 26 IAW SRM 51-42-06-001-001-A01. INSTALLED RT LOWER 280 WEB ATTACH ANGLE AT RBL 26 IAW SRM 51-42-06-001-001-A01.Apr 14, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR ASOA2015050812789Skin · damagedRUDDER T/E MADE CONTACT WITH TAIL STAND PULL OUT SLIDER. COMPLIED WITH SRM 51-41-01-201-001-A01 RUDDER REPAIR TOTAL HINGE LINE ROTATIONAL INERTIA IS 167.04, REPAIR WEIGHT .450, REMOVED WEIGHT .160, HINGE LINE IS 24". RECEIVED EC/TC EO 900-55-0005 & COMPLIEDApr 13, 2015 · N176PQ · Cndair CL6002D24 · Rudder, Plate/SkinSDR ASOA2015050812788Skin · dentedSKIN DENTED BETWEEN BS 581-597, STRINGERS 16 & 17. COMPLIED WITH EA 32-2015-149. RECEIVED EC/TC EA 32-2015-149 AND COMPLIED WITH EC/TC EA 32-2015-149.Apr 11, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR ASOA2015050712773Seat Track · corrodedRT SIDE SEAT RAIL IS CORRODED AT FS 785.15. REMOVED RT SIDE SEAT RAIL AT FS 785.15 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT RAIL RT STA 784 TO 847.+16 IAW AMM 53-00-49-400-801-A07.Apr 11, 2015 · N176PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015050712772Seat Track · corrodedRIGHT SIDE SEAT RAIL IS CORRODED AT FS 744.15. REMOVED RT SIDE SEAT RAIL AT FS 744.15 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT RAIL RT STA 744.15 TO 761.85 IAW AMM 53-00-49-400-801-A07.Apr 11, 2015 · N176PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015050712771Seat Track · corrodedRIGHT SIDE SEAT RAIL IS CORRODED AT FS 720.85. BLENDED CORROSION AT FS 720.85 IAW SRM 51-21-06-001-001-A01 & REO 670-53-00-013 ON SIDE SEAT RAIL RT. REMOVED RT SIDE RAIL AT FS 720.85 IAW AMM 53-00-49-000-801, CONFIG A07. INSTALLED NEW SEAT RAIL RT STA 672.0Apr 11, 2015 · N176PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015050712770Seat Track · corrodedLT SIDE SEAT RAIL IS CORRODED AT FS 785.15. REMOVED LT SIDE SEAT RAIL FS 785.15 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT RAIL LT STA 784.0 TO 847+16 IAW AMM 53-00-49-400-801-A07.Apr 11, 2015 · N176PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015050712769Seat Track · corrodedLEFT SIDE SEAT RAIL IS CORRODED AT FS 744.15. REMOVED LT SIDE SEAT RAIL AT FS 744.15 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW LT SEAT RAIL, STA 744.15 TO 761.85 IAW AMM 53-11-49-400-801-A07.Apr 11, 2015 · N176PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015050712768Door Sill · corrodedCORROSION ON SERVICE DOOR SILL CAP ANGLE AT FS 310. REMOVED CORROSION ON SERVICE DOOR SILL & DAMAGE AT FS 310-333 IAW SRM 51-21-001-001-A01 & 51-12-00-001-001-A1. INSTALLED NEW SERVICEABLE SERVICE DOOR SILL CAP ANGLE WHEN RECEIVED. INSTALLED NEW SERVICE DOApr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015050712767Structure · corrodedPACKERS CORRODED AT FS 333 AND ON RBL 9 ON BOTH SIDES OF FLOORBEAM. REMOVED, 2 EA CORRODED PACKERS AND INSTALLED 2 EA NEW SERIVCABLE PACKERS IAW SRM 51-42-06-001-001 AND DWG SH670-32120.Apr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015050712766Seat Track · corrodedFLOOR SEAT RAIL SEGMENT FROM FS 349 TO FS 485 AT RBL 9 IS CORRODED OUT OF LIMITS. R & R SEAT RAIL IAW AMM 53-00-49-000-801-A07, AND 53-00-49-400-801-A07.Apr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015050712765Seat Track · corrodedFLOOR SEAT RAIL SEGMENT FROM APPROXIMATELY FS 370 TO FS 485 AT LBL 9 IS CORRODED AT FS 370. REMOVED CORROSION FROM SEAT RAIL LBL 9.0, STA 370.0 OUT OF LIMITS IAW SRM 53-21-49-991-804, SHTS 1-3. R & R SEAT RAIL LBL9.0, FS370 TO 485 IAW AMM 53-00-49-000-801-A0Apr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015050712764Structure · corrodedPACKER CORRODED AT FS 349 AND RBL 9. REMOVED CORRODED PACKER AND INSTALLED 1 EA NEW SERVICEABLE PACKER IAW SRM 51-42-06-001-001 AND DWG SH670-32120.Apr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015050612763Floor Support · corrodedASD FLOOR SILL CAP ANGLE IS CORRODED. CAP SILL ANGLE BEYOND ALLOWABLE DAMAGE IAW SRM 53-21-23-101-001-A02. REPLACE PART WHEN REQUESTED. REMOVED LOCATED AND DRILLED AND INSTALLED NEW ASD FLOOR SILL CAP ANGLE IAW SRM 51-42-06-001-001-A01, AND 51-40-11-001-001Apr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015050612762Floorbeam · corrodedLT 280 SHEAR BOX BEAM CORRODED. UPON INCORPORATION OF SB 670BA-53-041, SHEAR BOX BEAM. LONGITUDINAL BEAM CAP & FASTENERS REPLACED.Apr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR ASOA2015050612761Floorbeam · corrodedRT 280, SHEAR BOX BEAM CORRODED. UPON INCORPORATION OF SB 670BA-53-041, SHEAR BOX BEAM, LONGITUDINAL BEAM CAP & FASTENERS REPLACED.Apr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR ASOA2015050612760Floor Support · corrodedAFT FLIGHT DECK FLOOR SUPPORT BEAM IS CORRODED IN MULIPLE AREAS. REMOVED FLIGHT DECK FLOOR SUPPORT AND WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-991-804. R & R FLIGHT DECK FLOR SUPPORT BEAM IAW SRM 51-42-06-001-001, CC670-34095.Apr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015050612759Floor Support · crackedRT FLOOR SILL AT FS 280- FS 319 CORRODED IN MULTIPLE AREAS. REMOVED FASTENER FROM RT FLOOR SILL STA 280-319 IAW SRM 51-42-06-001-001-A01. REMOVED AND DRILLED NEW FLOOR SILL STA 280-319 RT IAW SRM 51-42-06-001-001-A01. INSTALLED NEW FLOOR SILL, RT STA 280-31Apr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015050612758Floorbeam · corrodedRT 280 CROSSBEAM CORRODED IN MULTIPLE AREAS. UPON REMOVAL OF DRIP TRAY FOR INCORPORATIONS OF SB 670BA-53-041 BEAM WAS FOUND TO ALSO BE CRACKED AT RBL12. R & R RT BEAM IAW SRM 51-42-10-001-001-A01 & 51-42-06-001-001-A01 AND DWG CC670-34010. REMOVED INTERCOSTApr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR ASOA2015050612757Floorbeam · corrodedLT 280 CROSSBEAM CORRODED IN MULTIPLE AREAS. UPON REMOVAL OF DRIP TRAY FOR INCORPORATION OF SB 670BA-53-041 BEAM WAS FOUND TO ALSO BE CRACKED AT LBL 12. R & R LT BEAM IAW SRM 51-42-10-001-001-A01 & 51-42-06-001-001-A01 AND DWG CC670-34010. REMOVED INTERCOSTApr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR ASOA2015050612756Frame · corrodedFS310 AT STR 25RT IS CORRODED. REMOVED CORROSION FROM FRAME STA 295, STR 25R IAW SRM 51-21-06-001-001-A01. BLEND AREA IS OUT OF LIMITS IAW SRM 53-21-06-101-002-A02, DAMAGE IS ON 2 ELEMENTS IAW NOTE 1. COMPLIED WITH EA 32-2015-148. RECEIVED EC/TC EA 32-2015Apr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Main, FrameSDR ASOA2015050612755Step · corrodedPAX DOOR HAS CORROSION AT BASE OF FIRST STEP. REMOVED CORROSION ON PAX DOOR BASE OF FIRST STEP, INNER SKIN IAW SRM 51-21-06-001-001-A01 AND 51-12-00-001-001-A01. COMPLIED WITH EA 32-2015-154 SECTION 1, PERMANENT REPAIR. RECEIVED ECTC EA 32-2015-154 AND COMApr 10, 2015 · N176PQ · Cndair CL6002D24 · Passenger/Crew DoorsSDR ASOA2015050612754Intercostal · corrodedINTERCOSTAL CORRODED BETWEEN FS 349 AND FS 364 AT STR 27L. REMOVED CORROSION FROM INTERCOSTAL STR 27L, FS 349 TO 364 IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-21-23-101-003-A01. RESTORED TO ORIGINAL DWG FINISH IAW SRM 51-2Apr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015050612753Intercostal · corrodedINTERCOSTAL CORRODED BETWEEN FS 349 AND FS 364 AT STR 27, R. REMOVED CORROSION FROM INTERCOSTAL FS349 TO 364 IAW SRM 51-21-06-001-001-A01 AT STR 27R. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-21-23-101-003-A01. RESTORED TO ORIGINAL DWG FINISH IAW SRM Apr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015050612752Floor Support · crackedFLOOR SILL CRACKED UNDER ADG HYD PUMP. COMPLIED WITH EC TC REO 670-53-11-509 AND GRO 670-53-11-509, REV B, DATED 1/28/14.Apr 10, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015050812793Skin · dentedFOUND A DENT ON OUTER SKIN MIDDLE OF PAX DOOR. INSTALLED ALL MAS1241 FASTENER IAW EA 32-2015-150 AD REV A. COMPLIED ECTC EA32-2015-150 AND STS EA 32-2015-150, REV A.Apr 8, 2015 · N176PQ · Cndair CL6002D24 · Passenger/Crew DoorsSDR ASOA2015050812792Door Sill · damaged2 DRILL STARTS AND 11 TEMP FASTENERS LOCATED BETWEEN FS 349-FS 409 LT SIDE AT STR 17L. COMPLIED IWTH EC/TC REO 690-53-21-736 PERMANENT REPAIR REFER TO W/O 364816, N/R 00018. COMPLIED WITH REO 690-53-21-736. RECEIVED ECTC REO 690-53-21-736 AND COMPLIED WITH Apr 8, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015050812790Skin · gougedSCRATCH/DENT FOUND ON FUSELAGE AT FS 1144.00 AND FS 1162.00 AND STR 21R AND STR 22R. COMPLIED WITH EC/TC REO 690-53-61-453. RECEIVED FINAL REO 690-53-61-453. COMPLIED WITH EC/TC REO 690-53-61-453.Apr 8, 2015 · N176PQ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR ASOA2014040310267Wire · brokenRT OVERWING EMERGENCY LIGHT HAS A BROKEN WIRE. TERMINATED WIRE IAW ESPM 20-16-00. PERFORMED OPS TEST IAW AMM 33-51-15-710-801. OPS TESTED GOOD.Apr 1, 2014 · N176PQ · Cndair CL6002D24 · Light System Wiring
Back to N176PQ