N8886A

Service difficulty reports · 112

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 = 'N8886A' 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 REXA2016022400275Striker · dentedPASSENGER DOOR SILL STRIKER ON AFT SIDE, APPROX 6" FROM TOP, IS DENTED APPROX 1". REPAIR PAX DOOR SEAL STRIKER AFT SIDE IAW SRM 52-11-10, 51-24-21 & REO 601R-53-22-033 TYPE 1 & TYPE 3.Feb 24, 2016 · N8886A · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA2016022100310Hinge Fitting · damagedUPON REMOVAL OF RT INBD FLAP ASSEMBLY, NOTICED DAMAGE TO INBD HINGE ARM & BOX ATTACHMENT POINT. REPLACED RT INBD FLAP HINGE FITTING YOKE, IAW STEPS 1 - 5 FOR WORK PERFORMED IAW REO 601R-57-52-2105, REF PWI D538479 FOR DTA REQUIREMENTS.Feb 21, 2016 · N8886A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2016021900278Vane · chafedRIGHT INBD FLAP VANE IS CHAFED AT 3 LOCATIONS, WORST IS APPROX 1"" L X 1/2"" W X .010"" D. CONTINUATION CARD 8788611 OP 169. R & R RT INBD FLAP VANE MID SKIN IAW SRM 51-42-13. REPAIRED INBD & OTBD LOCATIONS IAW GREO 601R-57-52-004.Feb 19, 2016 · N8886A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2016021700304Intercostal · crackedTHREE EACH INTERCOSTALS CRACKED IN RADIUS AT FS 621 BULKHEAD, AT STRINGERS 13L - 15L. CONTINUATION CARD 8788611 OPS 173 & 174. REPLACED THREE EACH INTERCOSTALS AT 621 BULKHEAD, AT STRINGER 13L - 15L. REF STEPS 1 - 13 FOR WORK PERFORMED. THIS IS A MAJOR REPFeb 17, 2016 · N8886A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2016021700286Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE IS CRACKED AT PREVIOUS REPAIR. CONTINUATION CARD 8788611 OP 181. REPAIRED PAX DOOR AFT DRAG ANGLE IAW STEPS 1 - 6 FOR WORK PERFORMED ON MWC 8788611 OP 89.Feb 17, 2016 · N8886A · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA2016021600312Bulkhead · damagedFOUND REAR PRESS BULKHEAD WEB AT LBL 27.50, WL 130, HAS INDICATION NOTED APPROX .500" IN LENGTH 100% FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541 & REO 601R-53-61-5649. REF STEPS 1 - 3 FOR WORK PERFORMED.Feb 16, 2016 · N8886A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2016021600292Floorbeam · corrodedFLOORBEAM CAP IS CORRODED AT FS 585, BETWEEN RBL 9 - 27. REPLACED FLOORBEAM CAP IAW STEPS 1 - 2 FOR WORK PERFORMED.Feb 16, 2016 · N8886A · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR REXA2016021300285Skin · crackedPASSENGER DOOR, AFT SIDE SKIN IS CRACKED AT MID-FIXED STEP. CONTINUATION CARD 8788611 OP 168. REPAIRED PAX DOOR AFT SIDE SKIN CRACK, AT MID-FIXED STEP IAW EA CRJ252-04017 & REO 601R-52-11-702.Feb 13, 2016 · N8886A · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA2016021300283Retainer · crackedPANEL 412DB FWD & AFT SEPARATOR PANELS ARE CHAFED ALONG THE TOP EDGE, PLUS THE SEAL RETAINER IS CRACKED. REMOVED SEAL RETAINER IAW SRM 51-42-06. REPAIRED SEAL RETAINER IAW EA CRJ254-04028 REV IB. INSTALLED SEAL RETAINER IAW SRM 51-42-06. R & R FWD & AFT SEFeb 13, 2016 · N8886A · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR REXA2016021200300Seat Track · corrodedRIGHT SIDE FLOOR SEAT TRACK HAS MULTIPLE LOCATIONS OF CORROSION. TRACK 1 & 2. CONTINUATION CARD 8788611 OP 163. R & R RT SIDE FLOOR SEAT TRACKS 1 & 2 IAW AMM 53-01-11-000-802 & 53-01-11-400-802.Feb 12, 2016 · N8886A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016021200281Support Angle · crackedRIGHT SIDE ACCESS FAIRING SUPPORT ANGLES AT FS 461.5, 469.63 & 476.67 ON TOP OF WING ARE CRACKED, 3 EACH. R & R RT SIDE ACCESS FAIRING SUPPORT ANGLES IAW SRM 51-42-06, 51-42-21 & 51-40-11.Feb 12, 2016 · N8886A · Cndair CL6002B19 · Aerodynamic FairingsSDR REXA2016021100276Angle · crackedFS 621 OBLIQUE ANGLE IS CRACKED, STRINGER 14L. LOCATED, DRILLED & INSTALLED NEW SERVICEABLE OBLIQUE ANGLE, PN 601-35012-51, IAW SRM 51-40-11 & SRM 51-42-06. Feb 11, 2016 · N8886A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2016020900287Cap · dentedPASSENGER DOOR, 2 UPPER CORNER CAPS ARE DENTED, APPROX 1" IN DIAMETER. INSTALLED & REMOVED MARKING TAPE AS REQUIRED. REPLACED PAX DOOR, 2 EACH UPPER CORNER CAPS IAW SRM 51-42-13.Feb 9, 2016 · N8886A · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA2016020900277Vane · chafedLEFT INBD FLAP VANE IS CHAFED AT 3 LOCATIONS, APPROX 1" LX .5" W X .010" D. INSTALLED & REMOVED MARKING TAPE AS REQUIRED. REPLACED 3 EA LT INBD FLAP VANE LE CAPS IAW SRM 51-42-13, 51-23-00 & 51-25-26.Feb 9, 2016 · N8886A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2016020800282Fitting · brokenLEFT FLAP STUB FAIRING, FWD AIRFRAME MOUNT IS BROKEN OFF. R & R LT FLAP FITTING, PN 601R10371-1 IAW SRM 51-42-21.Feb 8, 2016 · N8886A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2016020700303Retainer · dentedCARGO DOOR BOTTOM AFT & BOTTOM AFT CORNER SEAL RETAINER FOUND DENTED, REQUIRES REPLACEMENT. REPLACED CARGO DOOR SEAL RETAINER BOTTOM AFT & BOTTOM AFT CORNER IAW SRM 51-40-11, 51-42-06, 51-25-00 & 51-23-00-910-801.Feb 7, 2016 · N8886A · Cndair CL6002B19 · Cargo/Baggage DoorsSDR REXA2016020700298Seat Track · corrodedLEFT SIDE FLOOR SEAT TRACK 2 HAS MULTIPLE LOCATIONS OF CORROSION. FABRICATED & REPLACED SEAT TRACK AT LBL 9, FROM FS 409 - 409+128 IAW GREO 601R-53-00-485 & AMM 53-01-11-400-802.Feb 7, 2016 · N8886A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016020700296Seat Track · damagedSEAT TRACK RAIL AT RBL 9, BETWEEN FS 559+80 - 559 HAS PITTING CORROSION & GOUGES AT MULTIPLE LOCATIONS. FABRICATED NEW SEAT TRACK IAW REO 601R-53-00-485. REMOVED & INSTALLED SEAT TRACK AT FS 559+80 - 559, RBL 9 IAW AMM 53-01-11-000 400-802.Feb 7, 2016 · N8886A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016020700291Seat Track · corrodedCARGO SEAT TRACK SEGMENT IS CORRODED AT LBL 9, BETWEEN FS 572 - 559+112. INSTALLED & REMOVED MARKING TAPE AS REQUIRED. REPLACED CARGO SEAT TRACK AT LBL 9, BETWEEN FS 572 - 559+112 IAW AMM 53-00-49-400 000-801.Feb 7, 2016 · N8886A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016020700284Stop Fitting · brokenPANEL 694JB HAS BUTTE DOOR STOP TAB BROKEN OFF THE END OF THE PANEL. R & R BUTTE DOOR STOP ASSEMBLY, PN 600-10196-16, IAW SRM 51-42-06.Feb 7, 2016 · N8886A · Cndair CL6002B19 · Wing Miscellaneous StructureSDR REXA2016020600318Door · lack of lubeLEFT OVERWING EMER EXIT FAILED FUNCTION CHECK. HANDLE REQUIRED MORE THAN 40 POUNDS OF FORCE TO OPEN. LUBRICATED LT WING OVERWING EMER EXIT IAW AMM 12-30-52-640-801 & ACCOMPLISHED FUNCTIONAL CHECK IAW AMM 52-21-00-720-801. FUNCTIONAL CHECK IS GOOD AT THIS TIFeb 6, 2016 · N8886A · Cndair CL6002B19 · Emergency ExitsSDR REXA2016020600295Seat Track · damagedSEAT TRACK RAIL AT LBL 9, BETWEEN FS 559.0 - 559+80, HAS PITTING CORROSION & GOUGES AT MULTIPLE LOCATIONS. R & R SEAT TRACK RAIL AT LBL 9, BETWEEN FS 559.0 - 559+80 IAW GREO 601R-53-00-485 REV DATED 09 28 12 & AMM 53-01-11-400-802.Feb 6, 2016 · N8886A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016020600290Seat Track · corrodedCARGO SEAT TRACK SEGMENT IS CORRODED AT LBL 27, BETWEEN FS 559+80 - 559+96. R & R CARGO SEAT TRACK SEGMENT AT LBL 27, BETWEEN FS 559+80 - 559+96 IAW AMM 53-01-11-400-802.Feb 6, 2016 · N8886A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2015011200052Oxygen Mask · unwanted deployUPON APPLYING EXTERNAL POWER TO ACFT PAX OXY MASKS DEPLOYED. REPACKED 02 MASKS IAW AMM 35-21-09. PERFORMED OPERATIONAL TEST OF PAX OXYGEN SYS IAW AMM 35-20-00. ACFT OK FOR SERVICE.Jan 12, 2015 · N8886A · Cndair CL6002B19 · Passenger Oxygen SystemSDR REXA2014122701235Cable · brokenPAX DOOR LOWER SUPPORT-WHEEL CABLE BROKEN. DEFERRED PASSENGER DOOR ASSIST IAW MEL 52-11-11 ENTERD INTO DMR PLACARD INSTALLED AUTHORIZATION 010183. R & R PAX DOOR LOWER SUPPORT-WHEEL CABLE IAW AMM 52-11-13, OPS CHECK GOOD, OK FOR SERVICE. PN ON/OFF 601R38370Dec 27, 2014 · N8886A · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA2014071300698Oxygen Mask · unwanted deployUPON STARTING THE ACFT THE PAX OXYGEN MASK DEPLOYED. RESET O2 DEPLOYMENT SYS STOWED MASK & PERFORMED OPERATIONS CHECK IAW AMM 35-20-00 & 35-21-09.Jul 13, 2014 · N8886A · Cndair CL6002B19 · Passenger Oxygen SystemSDR REXA2014012300131Life Vest · unserviceableFIRST OFFICER`S LIFE VEST BAG TORN. R & R FIRST OFFICER`S LIFE VEST IAW AMM 25-61-03.Jan 23, 2014 · N8886A · Cndair CL6002B19 · Life JacketSDR REXA2013120902291Oxygen Mask · brokenOBSERVER`S O2 MASK IS BROKEN. DEFERRED, R & R OBSERVER`S O2 MASK IAW AMM 35-11-12.Dec 9, 2013 · N8886A · Cndair CL6002B19 · Crew Oxygen SystemSDR REXA2013081601594Lock Pin · lack of lubeRIGHT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST (EXCEEDED 40 POUNDS). LUBED RT OVERWING EXIT LOCKPINS IAW AMM 12-20-52-640-802. REPERFORMED FUNCTIONAL TEST OF THE RT OVERWING EMERGENCY EXIT IAW AMM 52-21-00-720-801. OPENING FORCE DID NOT EXCEED 40 POUNDS.Aug 16, 2013 · N8886A · Cndair CL6002B19 · Emergency ExitsSDR REXA2013081601593Lock Pin · lack of lubeLEFT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST (EXCEEDED 40 POUNDS). LUBRICATED LT OVERWING EXIT LOCKPINS IAW AMM 12-20-52-640-802. REPERFORMED FUNCTIONAL TEST IAW AMM 52-21-00720-801. OPENING FORCE DID NOT EXCEED 40 POUNDS. NO DEFECTS NOTED.Aug 16, 2013 · N8886A · Cndair CL6002B19 · Emergency ExitsSDR REXA2013081601590Potentiometer · out of adjustFLAPS FAILED MESSAGE POSTED WHILE PERFORMING FUNCTIONAL TEST OF FLAP SYS AT STEP 4.A.16 (G-I) REF AMM 27-54-00-720-801. ADJUSTED LT FLAP POSITION TRANSMITTER POTENTIOMETER. PERFORMED FUNCTIONAL TEST OF FLAP SYS IAW AMM 27-54-00-720-801. NO DEFECTS NOTED.Aug 16, 2013 · N8886A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA2013080201108Structure · damagedSIX DAMAGED RIVETS AT WL 86.5, LBL AND RBL 9.5, 18, 27.5, TWO GOUGES AT WL 86.5, LBL 8 AND RBL 7, TEN DAMAGE MARKS AT WL 103, LBL 7.75, RBL 6.75, LBL AND RBL 9, 18, 27.5, AND 36.2, MEASURING 0.004" TO 0.014" DEEP. REPAIRED IAW REO 601R-53-61-2155.Jul 31, 2013 · N8886A · Cndair CL6002B19 · Fuselage Main, StructureSDR REXA2013071001341Light · inoperativeEMERGENCY LIGHT INOPERATIVE IN CABIN. PERFORMED OPS CHECK OF CABIN EMERGENCY LIGHT IAW AMM 33-51-00. OPS CHECKED GOOD.Jul 10, 2013 · N8886A · Cndair CL6002B19 · Emergency LightingSDR REXA2013070501336Light · dislodgedEMERGENCY LIGHTS AT ROW 1CD LOOSE. R & R EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.Jul 5, 2013 · N8886A · Cndair CL6002B19 · Emergency LightingSDR REXA2013006261214Flap System · malfunctionedFLAPS DEGRADED STATUS MESSAGE, COMPLETED OPS TEST OF SKEW DETECTION SYS (IBIT) AND RESET SYS MESSAGE WENT AWAY OPERATED FLAPS THROUGH MESSAGE DID NOT RETURN, WORK DONE IAW FIM 27-50-00 AND AMM 27-51-15.Jun 26, 2013 · N8886A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA2013062301205Tiller · out of positionAIRCRAFT PULLS CONSIDERABLY TO THE LEFT FROM 0 TO 080 KTS WITH BOTH TILLER AND LDG. REMOVED, INSPECTED AND CLEANED STEERING TILLER BUT TILLER WILL NOT CENTER. REINSTALLED TILLER . NOSE WHEEL STEERING TILLER NOT CENTERING PROPERLY WAS CAUSING THE DISCREPANCYJun 23, 2013 · N8886A · Cndair CL6002B19 · Landing Gear Steering SystemSDR REXA2012091901351Sign · inoperativeLIGHTED EXIT SIGN ON PASSENGER ENTRANCE INOP. REMOVED AND REPLACED LIGHTED EXIT SIGN IAW AMM 33-50-00. OPS CHECK GOOD.Sep 19, 2012 · N8886A · Cndair CL6002B19 · Emergency LightingSDR REXA2012091601345Battery · dischargedF/A'S FLASHLIGHT INOP. REMOVED AND REPLACED F/A FLASHLIGHT BATTERY IAW AMM 25-61-01. OPS CHECK GOOD. DM CLEARED.Sep 16, 2012 · N8886A · Cndair CL6002B19 · Emergency EquipmentSDR REXA2012042200551Life Vest · unserviceableF/A LIFE VEST BAG TORN. REMOVED AND REPLACED F/A LIFE VEST IAW AMM 25-61-03.Apr 22, 2012 · N8886A · Cndair CL6002B19 · Life JacketSDR REXA2012000150Bulkhead · crackedFS 559 SEMI-PRESSURE BULKHEAD CRACKED AT RBL 18. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 AND 601R-53-41-609 AS AUTHORIZED BY PA 53-025.Jan 13, 2012 · N8886A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100990Fitting · brokenRT REV UNLOCK CAUTION MSG IN FLIGHT. FOUND THE BOTTOM (2) ANTIROTATION TANGS ON BALLSCREW ACTUATORS BROKEN AND T/R OUT OF RIG. REMOVED AND REPLACED ANTI ROTATION TANGS IAW HONEYWELL CMM 78-30-29 RIGGED RT T/R IAW AMM 78-30-00 OP/C GOOD.Dec 19, 2011 · N8886A · Cndair CL6002B19 · Engine Thrust ReverserSDR REXA201100775Fuel Line · leakingXFLOW/APU PUMP-CAUTION MSG INFLIGHT DURING CRUISE W/ APU OFF FUEL QUANTITIES WERE NORMAL. FOUND FUEL LINE LEAKING FROM THE APU FUEL SOLENOID. RESCURED THE LINE AND PERFORMED OP CHECK APU IAW AMM 49-10-00. OP CHECK GOOD, LEAK CHECK GOOD.Oct 24, 2011 · N8886A · Cndair CL6002B19 · APU Engine Fuel and ControlSDR REXA201100492Bulkhead · chafedREAR PRESSURE BULKHEAD CHAFED ON PREVIOUS REPAIRS 3 LOCATIONS ON RT SIDE AT RBL 18, RBL 27, RBL 36, ALL LOCATED 30.00" ABOVE FLOOR LEVEL. REPAIRED IAW BOMBARDIER REO 601R-53-6-2155.Aug 2, 2011 · N8886A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100489Access Panel · corrodedLEFT LOWER WING PLANK FUEL ACCESS HOLE AT WS 12.245 HOLE NR 2 HAS PITTING CORROSION ON I/B, O/B, AND FWD EDGE OF CUTOUT MEASURING APPROX .003D X .025W X .025L IN BOTH CRITICAL AND NON-CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.Aug 2, 2011 · N8886A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA201100490Access Panel · corrodedRIGHT LOWER WING PLANK FUEL ACCESS HOLE AT WS 54.897 HOLE NR 1 HAS PITTING CORROSION ON I/B EDGE OF CUTOUT MEASURING APPROX .003D X .022W X .022L IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.Aug 1, 2011 · N8886A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA201100488Access Panel · corrodedLEFT LOWER WING PLANK FUEL ACCESS HOLE AT WS 54.897 HOLE NR 1 HAS PITTING CORROSION ON I/B, O/B, AND FWD EDGE OF CUTOUT MEASURING APPROX .004D X .030W X .030L IN BOTH CRITICAL AND NON-CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.Aug 1, 2011 · N8886A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA201100486Beam · damagedFS 280 TRANSVERSE BEAM IS CRACKED AND CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B.Jul 31, 2011 · N8886A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100487Skin · damagedRT ELEVATOR TOP SKIN HAS LIGHTNING STRIKE DAMAGE ON TRAILING EDGE AT ES 103.00. BURN MEASURES APPROX .500 LX .250W. REPAIRED IAW BOMBARDIER REO 601R-55-21-327.Jul 30, 2011 · N8886A · Cndair CL6002B19 · Elevator, Plate/SkinSDR REXA201100485Skin · damagedRT ELEVATOR TOP SKIN HAS LIGHTNING STRIKE DAMAGE ON TRAILING EDGE AT ES 103.00. BURN MEASURES APPROX 0.500 LX.250"W. REPAIRED IAW BOMBARDIER REO 601R-55-21-327.Jul 30, 2011 · N8886A · Cndair CL6002B19 · Elevator, Plate/SkinSDR REXA201100480Bulkhead · chafedREAR PRESSURE BULKHEAD CHAFED ON PREVIOUS REPAIRS 3 LOCATIONS ON RT SIDE AT RBL 18, RBL 27, AND RBL 36 ALL LOCATED 30 INCHES ABOVE THE FLOOR LEVEL. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Jul 29, 2011 · N8886A · Cndair CL6002B19 · Fuselage Main, Bulkhead
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