N525AE

Service difficulty reports · 133

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 = 'N525AE' 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 V0XD20220321010Floor Support · corrodedAFT CARGO FLOOR BEAM LBL 27 BETWEEN F.S. 985.00 AND F.S. 1088 IS CORRODED. CORRECTIVE ACTION: REPAIRED THE FLOOR BEAM AT LBL 27 BETWEEN F.S. 985 AND F.S. 1088 IAW BOMBARDIER REO 670-53-61-2054 REV. -- DATED 2022-02-01.Mar 21, 2022 · N525AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20220225002Intercostal · corrodedINTERCOSTAL AT F.S 364 AT STGR 27 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED THE INTERCOSTAL AT F.S 364 AND STGR 27 IAW CRJ 700 SRM 51-42-06.Feb 25, 2022 · N525AE · Cndair CL6002C10 · Fuselage Main, StructureSDR V0XD202202250001Actuator · corrodedL/H O/B CENTER FLAP /CENTER BUTE DOOR ACTUATOR ASSY SPRING IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED THE BUTE DOOR ACTUATOR IAW CRJ 700 AMM 57-54-02-400-804/000-804Feb 25, 2022 · N525AE · Cndair CL600* · Ventral StructureSDR V0XD20220216002Stringer · corrodedSIGNS OF CORROSION ON STR 25R FROM FS 280- 349 MULTIPLE AREAS: CORRECTIVE ACTION REMOVED AND REPLACED FROM STA STR 25R 280-333 IAW CRJ 700 SRM 51-42-06-001-001-A01Feb 16, 2022 · N525AE · Cndair CL600* · Fuselage Main, StructureSDR V0XD20220215001Hinge · damagedPAX DOOR HINGE ON AC SIDE AND DOOR SIDE HAS DAMAGE TO HINGE PIN BORES- REMOVED AND REPLACED HINGE HALF ON FUSELAGE SIDE IAW BOMBARDIRE CRJ 700 SRM 53-21-23-201-007-A01, DOOR HINGE REPLACED BY OSV MHIRJ AVIATION INC. IAW CRJ 700 SRM REV 38 DATED JUL 25/20 TASK Feb 15, 2022 · N525AE · Cndair CL6002C10 · Fuselage, Door HingeSDR V0XD20220205001Drag Angle · crackedLEFT VERT STAB AFT DRAG ANGLE CRACKED .090" - CORRECTIVE ACTION: CUT OUT 2.2" DAMAGED SECTION AND REPAIRED LEFT VERTICAL STAB DRAG ANGLE IAW BOMBARDIER REO 670-55-31-018 REV-A 2016-11-10, EA 22-C7-55-122 REV IR 01/26/2022Feb 5, 2022 · N525AE · Cndair CL6002C10 · Vertical StabilizerSDR V0XD20220202001Door Frame · crackedPAX DOOR FRAME CRACKED AT STA 280 STR3L LENTIL CLIP CORRECTIVE ACTION: REPAIRED PAX DOOR FRAME AT STA 280 STR 3L LENTIL CLIP IAW REO 670-53-21-493 REV D 2015-07-10 AND SB 670BA-53-40 REV C SEPT 20 2012Feb 2, 2022 · N525AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR V0XD202202010001Skin · corrodedCORRODED ON LOWER SKIN ON FS 295.00 - FS 310.00 ON STR. 27. CORRECTIVE ACTION: REMOVED, BLENDED AND SMOOTH CORROSION ON LOWER SKIN ON FS 295.00 - FS 310.00 ON STR. 27 IN LIMITS IAW OLIVER WYMAN CAVOK ENGINEERING AUTHORIZATION 22-C7-53-152.Jan 27, 2022 · N525AE · Cndair CL6002C10 · Fuselage Main, StructureSDR V0XD20220321001Intercostal · corrodedINTERCOSTAL AT F.S. 364 AT STRG 27 R/H INTERCOSTAL IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL (PN: SH670-320-75-4S) IAW CRJ 200 SRM 51-42-06-001-001A01.Jan 25, 2022 · N525AE · Cndair CL6002C10 · Fuselage Main, StructureSDR V0XD20220321002Angle · corrodedAVIONICS BAY FLOOR BOARD SUPPORT ANGEL AT F.S. 280 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR BOARD SUPPORT ANGLE(PN: CC670-34256-3) IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Jan 18, 2022 · N525AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20220216001Frame · damagedSPLICE REPAIR AT FS 319 AT STR 27 IN FWD AVIONICS BAY. CORRECTIVE ACTION: PERFORMED REPAIR TO FS 319 (P/N: SH670-31355-1) AT STR 27 IAW BOMBARDIER REO 670-53-21-799 REV A DATE 2016-11-27.Jan 17, 2022 · N525AE · Cndair CL600* · Fuselage Main, StructureSDR V0XD20220224001Skin · dentedPAX DOOR OUTER SKIN DENT. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR TO THE DENT ON THE PAX DOOR OUTER SKIN BY DRESSING OUT DENT TO ORIGINAL CONTOUR REMAINING DEFORMATION OF .004 INCHES WITH IN LIMITS IAW OLIVER WYMAN, CAVOK ENGINEERING AUTHORIZATION 21-Jan 13, 2022 · N525AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR V0XD20220206002Rib · damagedL/H INBD FLAP LEADING EDGE RIB HAS HOLE DAMAGE AT PANEL 584FB. CORRECTIVE ACTION: PERFORMED THE REPAIR TO THE INBD FLAP LEADING EDGE RIB (MISS-DRILL DAMAGE). BETWEEN FLS 25.50 AND FLS 30.00 IN ACCORDANCE WITH MHIRT REPAIR ENGINEERING ORDER # 670-57-52-517 DATEJan 12, 2022 · N525AE · Cndair CL6002C10 · Trailing Edge FlapsSDR V0XD20220225001Angle · corrodedCORRODED ON FWD BRACKET OF FLOOR BOARD A41 ALF AT F.S. 280. CORRECTIVE ACTION REMOVED AND REPLACED (P/N: CC670-34256-3) ANGLE AT FWD BRACKET FLOOR SUPPORT 141 ALF AT F.S. 280 IAW CRJ 700 SRM 51-42-21 AND 51-42-06.Jan 9, 2022 · N525AE · Cndair CL600* · Fuselage Miscellaneous StructureSDR V0XD20220206003Bracket · corrodedCORRODED AT BRACKET. LOCATION: FRAME STATION: 285.00, RIGHT BUTT LINE: 9. CORRECTIVE ACTION: REMOVED AND REPLACED BRACKET FITTING (P/N: SH670-32149-3) AT FRAME STATION 285.00, RIGHT BUTT LINE 09 IN ACCORDANCE WITH CRJ STRUCTURAL REPAIR MANUAL 51-40-21-001-001-Jan 6, 2022 · N525AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR V0XD20220127003Housing · gougedR/H ENG LOWER COWLING AFT LATCH HOUSING UNDER PANEL 443 AR HAS A GOUGED. CORRECTIVE ACTION: BLENDED TO SMOOTH PROFILE GOUGED AREA AT AFT LATCH HOUSING UNDER PANEL 443 AR IAW CRJ 700 A.E # 22-C7-54-062.Jan 6, 2022 · N525AE · Cndair CL6002C10 · Engine Cowling SystemSDR V0XD20220206001Joint · corrodedCORRODED ON THE CIRCUMFERENTIAL JOINT AT FS 280.00 FROM STR. 25L TO STR. 24 R. CORRECTIVE ACTION: REMOVED, BLENDED AND SMOOTH DEPTH BLEND RATIO OF 20:1 CORROSION ON THE CIRCUMFERENTIAL JOINT AT FS 280.00 FROM STR. 25L TO STR. 24 R IAW OLIVER WYMAN CAVOK ENGINEJan 5, 2022 · N525AE · Cndair CL6002C10 · Fuselage Main, StructureSDR V0XD20220127002Intercostal · corrodedCORRODED ON INTERCOSTAL ADJACENT TO THE LEFT OF STR. 27 AT F.S. 364. CORRECTIVE ACTION: REMOVED AND REPLACED (P/N: SH670-32075-3S) INTERCOSTAL ADJACENT TO THE LEFT OF STR. 27 AT F.S. 364 IAW CRJ 700 51-42-06-001-001.Jan 5, 2022 · N525AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20220124001Angle · corrodedPASSENGER DOOR KICK ANGLE IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED CORRODED KICK ANGLE IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01Jan 5, 2022 · N525AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR V0XD20220202002Stringer · corrodedCORRODED ON STR 26R FROM FS 280.00 TO FS 319.00. CORRECTIVE ACTION: REMOVED AND REPLACED STR 26 R (P/N: SH670-31634-2) FROM FS 280.00 TO FS 319.00 IAW CRJ 700 SRM 51-42-06-001-001.Jan 3, 2022 · N525AE · Cndair CL6002C10 · Fuselage Main, StructureSDR V0XD20220113001Splice Angle · corrodedCORROSION ON SPLICE ANGLE ON RIB STA. FS939 BETWEEN SRT 26R -26L- CORROSION OUT OF LIMITS REMOVED AND REPLACED PART IAW CRJ SRM 51-40-11, 51-42-06Jan 3, 2022 · N525AE · Cndair CL6002C10 · Fuselage Main, FrameSDR V0XD20220127001Door Sill · corrodedCORRODED ON LOWER SILL AT AFT CARGO DOOR. CORRECTIVE ACTION: REMOVED AND REPLACE (P/N: MM670-35655-003) LOWER SILL AT AFT CARGO DOOR IAW CRJ 700 SRM 51-42-21-001-001 AND 51-42-13-001-001.Dec 31, 2021 · N525AE · Cndair CL6002C10 · Cargo/Baggage DoorsSDR VNAA202107291111Panel · crackedPAX DOOR HAS CRACK IN ZONE 2 AFT SIDE OF DOOR / COMPLIED WITH PERMANENT REPAIR OF AFT PAX DOOR SIDE PANEL IAW REO 670-52-11-104 STEP 8 FOR REPAIR ZONE 4 TYPE 1 + ZONE 2 THRU COMPLETION. NO DEFECTS NOTED. SEE FOUND FAULTS FOR NDT AND FORM 337 FILED. PERFORMEDJul 28, 2021 · N525AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR V0XD2022012101Frame · crackedFRAME FS 333 CRACKED BETWEEN STR 1R-2RJan 21, 2021 · N525AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2019121091101Transducer · failedLOSS OF BRAKING EFFECTIVENESS ON LANDING. BTMS SHOWING 05/06/04/00. NO INDICATION RH OB BRAKE TEMPERATURE. MX TROUBLESHOT TO RH OB WHEEL SPEED TRANSDUCER NOT ROTATING. R&R #4 WHEEL SPEED TRANSDUCER. OPS CHECK GOOD.Dec 9, 2019 · N525AE · Cndair CL6002C10 · Landing Gear Brake SystemSDR VNAA2019041199903Frame · corrodedCOSSOSION FOUND FS319,STGR 27 TO 25R ON FRAME. REMOVED DAMAGE IAW REO 670-53-21-1308.Apr 11, 2019 · N525AE · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA2019041199902Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. C/W CRJ700 SRM 52-11-04-201-002-A01 REPAIR #1 REF SRM 52-11-04-201-002-A01Apr 11, 2019 · N525AE · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA2019041199901Support Bracket · crackedPAX DOOR AFT WEB CRACKED 2 PLACES NEXT TO HAND RAIL SUPPORT BRACKET. COMPLIED WITH STEPS 1-7 OF PAX DOOR SIDE PANEL REPAIR CRJ 700 SRM 52-11-04-201-004-A01.Apr 11, 2019 · N525AE · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA2018090811101Pcu · leakingWHILE DESCENDING INTO TOL AT ABOUT FL260 THE FLIGHT CREW RECEIVED A HYDRAULIC SYSTEM 2 WARNING AND AILERON WARNINGS. DECLARED AN EMERGENCY AND THE CREW RAN THE QRH. AFTER RUNNING THROUGH THE QRH THE COURSE OF ACTION WAS TO LAND AT THE NEAREST AIRPORT. MAINTENASep 8, 2018 · N525AE · Cndair CL6002C10 · Drag Control SystemSDR SIMA20180209002Web · corrodedLEFT WEB AT BS 280 IS CORRODED. REMOVED AND REPLACED THE WEB IAW 51-42-06, AND SRM 51-42-13.Feb 9, 2018 · N525AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20180208004Floorbeam · crackedFLOORBEAM LBL 12 CRACKED FORWARD OF BS 280. REPAIRED IAW ERS-CR-53MR-3155.Feb 8, 2018 · N525AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20180208005Floorbeam · crackedRIGHT FLOORBEAM LBL 12 CRACKED, FORWARD OF BS 280. REPAIRED IAW ERS-CR-53MR-3155.Feb 8, 2018 · N525AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20180208002Floorbeam · corrodedBS 280 FLOORBEAM IS CORRODED ON THE FWD SIDE. REPLACED THE FLOORBEAM IAW SRM 51-42-06, AND 51-42-13.Feb 8, 2018 · N525AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20180202005Floor Panel · crackedLEFT SIDE OF THE FWD EQUIPMENT BAY FLOOR HAS EVIDENCE OF A CRACK. APPROXIMATELY 3/8 INCH LONG ON THE AFT CORNER. REPAIRED IAW SRM 53-11-43.Feb 2, 2018 · N525AE · Cndair CL6002C10 · Fuselage Floor PanelSDR SIMA20171205001Roller · lack of lubeCREW REPORTS MAIN CABIN DOOR HANDLE STICKS CAUSING DOOR TO BECOME HARD TO OPEN. LUBRICATED MAIN CABIN DOOR ROLLERS AND GUIDE POINTS AS REQUIRED. PERFORMED SEVERAL OPEN/CLOSE/LOCKING CYCLES. DOOR HANDLE OPERATES SMOOTHLY AND SECURELY IAW AMM 52-11-00. OPS CHECKDec 5, 2017 · N525AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20170819003Sensor · failedSLATS FAILED. REMOVED AND REPLACED RT SLAT ACTUATOR NR 3, PERFORMED FULL MECHANICAL RIG OF RT SLATS, AND REMOVED AND REPLACED SLAT 1 & 2 DISCONNECT SENSORS. ALL OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.Aug 19, 2017 · N525AE · Cndair CL6002C10 · Leading Edge Slat Control SystemSDR SIMA20170817001Cable · brokenPAX DOOR DIFFICULT TO OPEN. CLEANED AND LUBRICATED THE LATCH PINS AND CAMS IAW AMM 12-20-52. DOOR STILL HARD TO OPEN. NO OTHER DESCREPANCIES NOTED. FOUND PASSENGER DOOR SUPPORT WHEEL CABLE BROKEN AND HANDLE LEVER SHAFT BENT. REMOVED AND REPLACED DOOR SUPPORTAug 17, 2017 · N525AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20170808001Actuator · failedSLATS FAIL ON ON EICAS INDICATE ON LEFT OR RIGHT WING. COMPLIED WITH AOM LANDED WITHOUT INCIDENT. CLEARED INHIBITS IAW AMM 45-45-00 . PERFORMED OPS CK IAW 27-50-00. OPS CHECK GOOD. NO FURTHER MESSAGES NOTED AIRCRAFT OK FOR SERVICE. REMOVED AND REPLACED SLAT ACAug 8, 2017 · N525AE · Cndair CL6002C10 · Leading Edge Slat ActuatorSDR SIMA20170627001Actuator · failed'SLAT FAIL' CAUTION MSG ON APPROACH, SLATS DID NOT DEPLOY FLAPS DEPLOYED AS PER FLAP SCHEDULE TO 45'. REPLACED RT SLAT ACTUATORS 3-3, 2-3 AND 3-1 FOR BEING TRIPPED. IAW AMM 27-81-09 OPS TEST GOOD. PERFORMED MECHANICAL RIGGING OF LT AND RT SLATS IAW AMM 27-81-0Jun 27, 2017 · N525AE · Cndair CL6002C10 · Leading Edge Slat ActuatorSDR SIMA20170413001Motor · failedSLATS FAIL CAUTION MESSAGE WHEN SELECTING SLATS TO 1. REMOVED AND REPLACED SLAT PDU MOTOR NR 2 IAW AMM 27-81-37. OPS CHECKED GOOD.Apr 13, 2017 · N525AE · Cndair CL6002C10 · Leading Edge Slat Control SystemSDR SIMA20170105003Anti-Ice Valve · failedDURING TAKE OFF, RECIEVED A LT COWL ANTI-ICE CAUTION MESSAGE. COMPLIED WITH ACM-1 PROCEDURES. REMOVED AND REPLACED THE LT COWL ANTI-ICE VALVE IAW AMM 30-22-01 OPT'S AND LEAK CHECKED GOOD.Jan 5, 2017 · N525AE · Cndair CL6002C10 · Air Intake Anti/De-Ice SystemSDR SIMA20160821003Pcu · faultyINBD FLIGHT SPOILERS, INBD SPOILERONS CAUTIONS POSTED ON FINAL APPROACH. INTERROGATED MDC FOUND RT INBD MFS PCU FAILED PCU JAM. PERFORMED SPOST1 RESET, PERFORMED OPS CHECK IAW ETN-CR-27-093. OPS CHECK GOOD. OPEN TDMI 525T2761 TO R & R R-INBD MFS PCU IN 10 Aug 21, 2016 · N525AE · Cndair CL6002C10 · Drag Control ActuatorSDR SIMA20160603005Skin · crackedPAX DOOR AFT SKIN CRACKED AT DOOR CABLE ASSIST SUPPORT. COMPLETED INSTALLATION OF THE AFT SKIN IAW SRM 51-42-06.Jun 3, 2016 · N525AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20160601004Window · distortedRIGHT OVERWING EMERGENCY EXIT DOOR WINDOW VIEW IS CLOUDY AND DISTORTED. R & R EMERGENCY EXIT WINDOW IAW AMM 56-30-02. LEAK CHECK GOOD.Jun 1, 2016 · N525AE · Cndair CL6002C10 · Emergency ExitsSDR SIMA20160601005Window · distortedLEFT OVERWING EMERGENCY EXIT DOOR WINDOW VIEW IS CLOUDY AND DISTORTED. R & R EMERGENCY EXIT WINDOW IAW AMM 56-30-02. LEAK CHECK GOOD.Jun 1, 2016 · N525AE · Cndair CL6002C10 · Emergency ExitsSDR SIMA20160601003Structure · crackedFWD EQUIPMENT BAY FLOOR CRACKED UNDER THE ADG HYD PUMP. REPAIRED FWD EQUIPMENT BAY FLOOR IAW ETN-CR-53-099.Jun 1, 2016 · N525AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20160601002Support Angle · crackedPASSENGER DOOR AFT SIDE SUPPORT ANGLE IS CRACKED NEAR THE RETRACT CABLE PULLEY SUPPORT. REPAIRED AFT ANGLE IAW SRM 52-11-04.Jun 1, 2016 · N525AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20160529002Warning System · false activationOUTBOARD SPOILERONS CAUTION. INTERROGATED MDC FOUND RT OTBD MFS PCU & PCU JAM MSGS. PERFORMED SPOST 1 RESET. PERFORMED OPERATIONS CHECK IAW ETN-CR-27-093. OPERATIONS CHECKED GOOD.May 29, 2016 · N525AE · Cndair CL6002C10 · Drag Control SystemSDR SIMA20160506002Pcu · failedIN FLIGHT SPOILERONS CAUTION MSG. INITIAL MINOR ROLL ON DEPLOYMENT AFTER CONTROL STABILIZED. R & R LT INBD MFS PCU IAW AMM 27-62-01. OPERATIONS CHECK AND LEAK CHECKED GOOD. NO FURTHER DEFECTS NOTED.May 6, 2016 · N525AE · Cndair CL6002C10 · Drag Control ActuatorSDR SIMA20151123002Light · inoperativeEMERGENCY LIGHT EXTERIOR RT FUSELAGE INOPERATIVE BY EMER DOOR. R & R EMER LIGHT RT EXTERIOR BY EMER DOOR. OPERATIONS CHECKED GOOD.Nov 23, 2015 · N525AE · Cndair CL6002C10 · Emergency Lighting
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