N8908D

Service difficulty reports · 118

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 = 'N8908D' 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 REXA2016100801934Seat Track · corrodedLEFT AISLE SEAT TRACK HAS CORROSION BETWEEN BS 394 TO 409+112. REMOVED AND REPLACE THE SEAT TRACK IAW AMM 53-01-11.Oct 8, 2016 · N8908D · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2016100401962Bulkhead Web · crackedREAR PRESSURE BULKHEAD FORWARD FACE HAS A CRACK EXTENDING FROM END OF DOOR TRACK AT LBL 18 APPROX 1/2 LONG. REPAIRED IAW REO 601R-53-61-1541.Oct 4, 2016 · N8908D · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2016100401917Hinge · crackedCARGO DOOR THRESHOLD HAS CRACKED HINGE. REMOVED AND REPLACED CARGO DOOR THRESHOLD HINGE IAW SRM 51-42-11 TOPCOATED IAW SRM 51-25-16.Oct 4, 2016 · N8908D · Cndair CL6002B19 · Fuselage, Door HingeSDR REXA2016100301961Attach Angle · crackedAFT PRESSURE BULKHEAD INTERCOSTAL AT STRINGER 14L HAS CRACKED ANGLE. REMOVED AND REPLACED THE IAW SRM 51-42-21, AND REO 601R-53-61-5265.Oct 3, 2016 · N8908D · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR REXA2016100301960Attach Angle · crackedAFT PRESSURE BULKHEAD INTERCOSTAL AT LONGERON 13L HAS CRACKED ANGLE. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-21, AND REO 601R-53-61-5265.Oct 3, 2016 · N8908D · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR REXA2016100301959Attach Angle · crackedAFT PRESSURE BULKHEAD INTERCOSTAL AT STRINGER 16L HAS CRACKED ANGLE. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-5265.Oct 3, 2016 · N8908D · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR REXA2016100201968Flange · crackedAPU ENCLOSURE AFT UPPER FLANGE HAS TWO BROKEN WELDS AT SUPPORT RIBS. REMOVED DAMAGE AND REPAIRED IAW REO 601R-49-11-071.Oct 2, 2016 · N8908D · Cndair CL6002B19 · APU Cowling/ContainmentSDR REXA2016100101974Oxygen Bottle · inoperativePORTABLE OXYGEN BOTTLE S/N: 184341 FAILED OPS CK. REMOVED & REPLACED PORTABLE OXYGEN BOTTLE S/N 184341 IAW TS000340-2012. C/W OPERATIONAL CHECK IAW AMM 35-31-01-710-801. CHECKS GOOD.Oct 1, 2016 · N8908D · Cndair CL6002B19 · Portable Oxygen SystemSDR REXA2016093001966Rub Strip · chafedNR 2 ENGINE UPPER NOSE INLET COWL RUBSTRIP IS CHAFED IN NUMEROUS AREAS. REMOVED & REPLACED IAW CMM 71-14-01.Sep 30, 2016 · N8908D · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR REXA2016092901963Floorbeam · corrodedCARGO FLOORBEAM ANGLE AT BS 621 BETWEEN RBL 45 AND LBL 45 HAS CORROSION. REMOVED CORROSION AND FOUND AREA IN LIMITS IAW REO 601R-53-61-4690. ONE AREA AT LBL 15 OUT OF LIMITS, REPAIRED IAW EA CRJ253-04812.Sep 29, 2016 · N8908D · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR REXA2016092901941Seat Track · corrodedLEFT SEAT TRACK HAS CORROSION AT BS 550 TO 566, 559+23 TO 559+40 AND 559+55 TO 559+72. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.Sep 29, 2016 · N8908D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092901940Seat Track · corrodedLEFT SEAT TRACK HAS CORROSION FROM BS 520 TO 537. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.Sep 29, 2016 · N8908D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092901939Seat Track · corrodedLEFT SEAT TRACK HAS CORROSION AT BS 457 TO 477 AND 486 TO 499. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.Sep 29, 2016 · N8908D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092901938Seat Track · corrodedLEFT SEAT TRACK HAS CORROSION AT BS 409+113 TO 409+131 AND 426 TO 443. REMOVED & REPLACED THE SEAT TRACK IAW REO 601R-53-00-055. REV B.Sep 29, 2016 · N8908D · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2016092901937Seat Track · corrodedLEFT SEAT TRACK HAS CORROSION AT BS 409+21 TO 409+37, 409+50 TO 409+68 AND 409+83 TO 409+100. REMOVED & REPLACED SEAT TRACK IAW AMM 53-01-11.Sep 29, 2016 · N8908D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092701952Floor Support · corrodedFLOOR SUPPORT LBL 9 HAS NUMEROUS CORROSION SPOTS BETWEEN BS 409+16 TO FS 409+128, IN CABIN. REMOVED & REPLACED THE FLOOR SUPPORT IAW SRM 51-42-21.Sep 27, 2016 · N8908D · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2016092701948Seat Track · corrodedRIGHT SEAT TRACK HAS CORROSION AT BS 550 TO 553 AND 559+23 TO 559+28. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.Sep 27, 2016 · N8908D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092701947Seat Track · corrodedRIGHT SEAT TRACK HAS CORROSION AT BS 501 TO 506 AND 521 TO 537. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.Sep 27, 2016 · N8908D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092701946Seat Track · corrodedRIGHT SIDE SEAT TRACK HAS CORROSION FROM BS 449 TO 500. REMOVED & REPLACED SEAT TRACK IAW AMM 53-01-11.Sep 27, 2016 · N8908D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092701945Seat Track · corrodedRIGHT SEAT TRACK HAS CORROSION FROM FWD END AT BS 409+114 TO 449. REMOVED & REPLACED THE SEAT TRACK IAW REO 601R-53-00-055 REV. B.Sep 27, 2016 · N8908D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092701944Seat Track · corrodedRIGHT SEAT TRACK HAS CORROSION AT BS 409+121 TO 409+137, 409+52 TO 409+55, 409+65 TO 409+69, 409+80 TO 409+89, 409+93 TO 409+101, AND 409+105 TO 409+110. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.Sep 27, 2016 · N8908D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092701942Seat Track · corrodedRIGHT SEAT TRACK HAS CORROSION AT BS 367 TO 372, 382 TO 387, 399 TO 409+6. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.Sep 27, 2016 · N8908D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092101969Bracket · crackedSINGLE POINT REFUEL/DEFUEL RECEPTACLE MOUNT STRUCTURE IS CRACKED LWR O/B CORNER. REMOVED AND REPLACED SINGLE POINT REFUEL/DEFUEL MOUNT STRUCTURE BRACKET IAW CRJ200 SRM'S 51-42-06.Sep 21, 2016 · N8908D · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2016092101954Attach Bracket · crackedR/H WING TO FUSELAGE PANEL ATTACHMENT BRACKET FS. 461 IS CRACKED. REMOVED & REPLACED BRACKET BS 461.00 IAW SRM 51-42-06.Sep 21, 2016 · N8908D · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR REXA2016092101953Attach Bracket · crackedRIGHT WING TO FUSELAGE PANNL ATTACHMENT BRACKET BS 449.85 IS CRACKED. REMOVED & REPLACED BROKEN BRACKET IAW SRM 51-42-06.Sep 21, 2016 · N8908D · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR REXA2016092001973Oxygen Mask · damagedOXYGEN MASK AT SEAT 6AC HAS CUT SUPPLY LINE. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-21-09-020-801, 35-21-09-860-802, 35-21-09-020-801, 35-21-09-420-801 AND 35-21-09-860-802.Sep 20, 2016 · N8908D · Cndair CL6002B19 · Passenger Oxygen SystemSDR REXA2016092001972Oxygen Mask · damagedOXYGEN MASK AT 4AC HAS CUT SUPPLY LINE. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-21-09-020-801, 35-21-09-860-802, 35-21-09-020-801, 35-21-09-420-801 AND 35-21-09-860-802.Sep 20, 2016 · N8908D · Cndair CL6002B19 · Passenger Oxygen SystemSDR REXA2016091901970Fitting · crackedFLIGHT DECK LT WINDSHIELD SIDE POST AFT FITTING IS CRACKED. REMOVED AND REPLACE WINDSHIELD SIDE POST FITTING IAW SRM 51-42-21.Sep 19, 2016 · N8908D · Cndair CL6002B19 · Fuselage Main, StructureSDR REXA2016091801950Stringer Clip · crackedSTRINGER CLIP 3L BS 280 IS CRACKED. REMOVED AND REPLACE THE STRINGER CLIP IAW SRM 51-40-11, SRM 51-24-21, AND SRM 51-42-06.Sep 18, 2016 · N8908D · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR REXA2016091701971Mount · corrodedFWD INBD GALLEY MOUNT IS CORRODED. REMOVED AND REPLACED THE GALLEY MOUNT IAW SRM 51-42-06.Sep 17, 2016 · N8908D · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR REXA2013091801739Connector · looseLAST ROWS OF EMERGENCY FLOOR LIGHTS ARE OUT. FOUND LOOSE CONNECTOR ON EMERGENCY LIGHT STRIP, SECURED CONNECTOR. OPS CHECKED GOOD IAW AMM 33-51-01.Sep 18, 2013 · N8908D · Cndair CL6002B19 · Light System WiringSDR REXA2013031700568Coalescer Bag · dirtyON FLIGHT 4109 (DAY TO MSP) FUEL SMELL IN ACS WHEN BLEEDS ARE TURNED ON FROM APU. RESIDUAL SMELL REMAINED THROUGHOUT FLIGHT. CREW NOTED SMELL PRESENT WHEN BLEED SOURCE FROM APU. SMELL DISSIPATED WITH APU OFF AND ENGINE BLEEDS ON. COMPLETED LEAK CHECK OF APMar 17, 2013 · N8908D · Cndair CL6002B19 · Humidity Control SystemSDR REXA2012110701662Life Vest · unserviceableFLIGHT ATTENDANT LIFE VEST BAG TORN. REMOVED AND REPLACED FLIGHT ATTENDANT LIFE VEST IAW AMM 25-61-03.Nov 7, 2012 · N8908D · Cndair CL6002B19 · Life JacketSDR REXA2012080401231Door · lack of lubePASSENGER DOOR VERY DIFFICULT TO OPEN. INSPECTED, CLEANED AND LUBED DOOR AFTER OPENING AS REQUIRED. DOOR OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE.Aug 4, 2012 · N8908D · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA2012072301183Unknown · odorGAS ODOR IN AIRCRAFT WHEN BLEEDS SWITCHED TO APU. REMOVED AND REPLACED APU COOLING FAN IAW AMM 49-52-05. LEAK AND OPS CHECKED GOOD.Jul 23, 2012 · N8908D · Cndair CL6002B19 · Air Distribution SystemSDR REXA2010630201038Latch · out of adjustMAIN CABIN DOOR HANDLE HARD TO RELEASE ON OPENING ALSO DURING CLOSE OUTER LATCH NOT FLUSH. ADJUSTED PAX DOOR LATCH MECHANISM IAW AMM 52-11-21. OPS CHECKED GOOD, AIRCRAFT OK FOR SERVICE.Jun 30, 2012 · N8908D · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA2012051300730Handle · bindingMAIN PASSENGER DOOR HANDLE IS JAMMING AND DIFFICULT TO OPEN AND CLOSED. COMPLIED WITH OPS CHECK OF PASSENGER DOOR IAW AMM 52-10-00. NO DEFECTS NOTED.May 13, 2012 · N8908D · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA201200022Warning System · intermittentAIR RETURN FOR IDG NR 2 CAUTION MSG INTERMITTENT ON CLIMBOUT.Dec 30, 2011 · N8908D · Cndair CL6002B19 · AC Indicating SystemSDR REXA201101019Wire · brokenREPLACE ELT ASSY DUE TO BROKEN WIRE INSIDE OF UNIT & BATTERY EXPIRES MAR/2012. REMOVED AND REPLACED ELT IAW AMM 25-62-01. OPS CHECK GOOD.Dec 25, 2011 · N8908D · Cndair CL6002B19 · Emergency Locator BeaconSDR REXA2011122511011Wire · brokenREPLACED ELT ASSY DUE TO BROKEN WIRE INSIDE OF UNIT. REMOVED AND REPLACED ELT IAW AMM 25-62-01. OPS CHECKED GOOD.Dec 25, 2011 · N8908D · Cndair CL6002B19 · Equipment/Furnishings WiringSDR REXA201100980Bulkhead · crackedFWD PRESS BULKHEAD CRACKED AT PARKING BRAKE CABLE PASS-THRU.Dec 16, 2011 · N8908D · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100979Bulkhead · crackedAFT BULKHEAD (FS 621) CRACKED AT LINTEL FITTINGS.Dec 16, 2011 · N8908D · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100880Shaft · saturatedFLAPS FAIL CAUTION MESSAGE (8 DEGREES) AT 4000 FT MSL ON APPROACH INTO DTW. NOTIFIED ATC - DECLARED AN EMERGENCY - DISCONTUNUED THE APPROACH. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD2009-06-12 PARAGRAPH (H) 96 (I), AMOC DATED MARCH 27,2009,Nov 28, 2011 · N8908D · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201100889Coax · looseGEAR WARNING HORN AT 235 KIAS WITH THRUST LEVERS AT IDLE. GEAR WARNING ASSOCIATION WITH RAD ALT CODES IN PSEU. FOUND LOOSE COAX CABLES ON NR 1 & NR 2 RAD ALT. TIGHTENED CABLES IAW CRJ 200 AMM 34-44-01. OPS CHECK GOOD. A/C OK FOR SERVICE.Nov 27, 2011 · N8908D · Cndair CL6002B19 · Navigation System WiringSDR REXA201100872Proximity Sensor · dirtyGEAR WARNING HORN INTERMITTENT ON APPROACH. FLAPS AT 20 AND THRUST AT 50 PERCENT. AIRSPEED 180-200 KTS. SEEMS TO BE AN ISSUE WITH THE THRUST QUADRANT. PERFORM BIT + F/C OF PSEU IAW CRJ 200 AMM 32-61-01. NO FAULTS FOUND. PERFORMED VISUAL INSPECTION AND CHNov 25, 2011 · N8908D · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA201100851Generator · failedFLT 3850-20 DID AN AIR RETURN DUE TO GEN 2 FAILURE. HYD EDP WAS PREVIOUSLY DEFERRED AND CAN`T HAVE BOTH INOP. NO EMERGENCY WAS DECLARED AND AIRCRAFT LANDED SAFELY IN MEM.Nov 20, 2011 · N8908D · Cndair CL6002B19 · AC Generator-AlternatorSDR REXA201100711Fitting · crackedCLIPS CRACKED AT 280.00 FLOORBEAM RBL 9 AND LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND BOMBARDIER SERVICE CORPORATION STANDARD REPAIR 601R-53-0110.Nov 12, 2011 · N8908D · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100813Skin · dentedTHE FUSELAGE SKIN TO BE DENTED APPROXIMATELY 2.5 FORWARD OF FS 654 BETWEEN S-2OL AND S-21L. REPAIRED IAW EA CRJ253-00188 REV A AS APPROVED BY ASSOCIATED 8110-3 DATED 11/7/2011.Nov 7, 2011 · N8908D · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201100812Rib · crackedLEFT WING BATT RIB ASSEMBLY AT WS 53.60 CRACKED AT TOP AFT FASTENER APPROXIMATELY 1 INCH LONG. REPAIRED IAW BOMBARDIER REO 601R-57-51-046.Nov 7, 2011 · N8908D · Cndair CL6002B19 · Wing, Rib/BulkheadSDR REXA201100752Spar · damagedNR 30 HOLE DRILLED IN LT FWD SPAR FLANGE AT WS 349. REPAIRED IAW BOMBARDIER REO 601R-57-21-1539.Nov 2, 2011 · N8908D · Cndair CL6002B19 · Wing Spar
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