Service difficulty reports

1,771,708 reports of malfunctions and defects, newest first. Air carriers must report; general aviation reporting is voluntary.

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'
  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 FDEA202605040540Floor Panel · puncturedPUNCTURE ON 232NFF FLOOR PANEL OF MAIN CARGO COMPARTMENT. 232NFF FLOOR PANEL OF MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV.94 DEC15,2025May 4, 2026 · N271FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202605040539Floor Panel · puncturedPUNCTURE ON 231QFF FLOOR PANEL OF MAIN CARGO COMPARTMENT. 231QFF FLOOR PANEL OF MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV94 DEC 15,2025May 4, 2026 · N271FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202605040538Floor Panel · puncturedPUNCTURES ON 231DFF FLOOR PANEL OF MAIN CARGO COMPARTMENT. 231DFF FLOOR PANEL OF MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG201 SHEET 2 REV 94 DEC15,2025May 4, 2026 · N271FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202605040537Floor Panel · puncturedPUNCTURES ON 231EFF FLOOR PANEL OF MAIN CARGO COMPARTMENT. 231EFF FLOOR PANEL OF MAIN CARGO COMPARTMEN WAS REPAIRED IAW SRM 53-00-50-2R PAR 4- B FIG 201 SHEET 2 REV.94 DEC 15,2025May 4, 2026 · N271FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202605040536Floor Panel · puncturedPUNCTURES ON 221GFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL221GFF OF MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG201 SHEET 2 REV94 DEC 15/2025May 4, 2026 · N271FE · Boeing 7673S2F · Fuselage Floor PanelSDR JJBA20260505002Battery · inoperativeBOTH LT AND RT LATERAL WTF FAIRING EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY, INTERIOR LT OVERHEAD EMERGENCY EXIT LIGHT NOW FUNCTIONING. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER. NOW RT EXTERIOR OMay 4, 2026 · N14162 · Emb EMB145XR · Emergency LightingSDR REXA2026050500457Floorbeam · crackedRH COCKPIT FLOOR-BEAM IS CRACKED AT FS 280.00. REMOVED DAMAGED PREVIOUS REPAIR SEGMENT OF RH COCKPIT FLOOR BEAM IAW CRJ900 SRM 53-11-43-201-003-A01. INSTALLED THE NEW SERVICEABLE RH COCKPIT FLOOR BEAM P/N:670-53-11-755-2 AND THE SERVICEABLE REPAIR SPLICES IAW May 4, 2026 · N604LR · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026050500456Floorbeam · crackedLH COCKPIT FLOOR-BEAM IS CRACKED AT FS 280.00. LOCATED AND DRILLED NEW LBL12.00 COCKPIT FLOOR BEAM SECTION P/N: 690-53-11-228-003S IAW CRJ900 SRM 51-40-11-001-001-A01. AND CRJ900 SRM 53-11-43-201-003-A01. REPAIR TYPE 4. INSTALLED THE NEW LBL12.00 COCKPIT FLOOMay 4, 2026 · N604LR · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026050500455Floorbeam · corroded"FS 280.00 CROSSBEAM J ANGLE IS CORRODED. REMOVED CORRODED 280 CROSSBEAM J ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01 51-42-21-001-001-A01. INSTALLED NEW SERVICABLE FS 280.00 CROSSBEAM ""J"" ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01. AND CRJ900 SRM 51-42-21-May 4, 2026 · N604LR · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SIMA20260504001Warning Message · false activationENG 2 N1, ENG 2 ITT, AND ENG 2 FUEL FLOW INDICATIONS APPEARED INFLIGHT AND ENGNE FAIL INDCTION ON APPROACH. CREW DECLARED EMERGENCY. NORMAL LANDING. NO ISSUSE REPORTED. T/S IAW FIM 22-31-00-810-821-A AND PERFORMED ENGINE RUNS WITH CREW, FOUND TO BE TRANSITORY,May 4, 2026 · N222NS · Emb ERJ170200LR · Engine Indicating SystemSDR CALA2026050516011Adiru · faultedLEFT IRS FAULT LIGHT ON NON NORMAL COMP DEBRIEFED WITH CREW, CHECKED FOR FAULTS IN DFCS, REPLACE L ADIRU. REF FIM 34-21 TASK 839 REPLACED L ADIRU, OPS CHECK GOOD REF AMM 34-21-00.May 4, 2026 · N47280 · Boeing 7378 · Directional Gyro and Indicating SystemSDR 2026FA0000320Terminal · incorrectRIGHT CROSS TIE BUS WOULD NOT POWER ON (POWERS THE MFD, NAV LIGHTS, RUDDER TRIM, RH ALT FIELD). FOUND LOOSE TERMINAL CONNECTIONS AT THE THREE 50 AMP SUPPLY CIRCUIT BREAKERS (BATTERY, LH ALT AND RH ALT) LOCATED ON THE COPILOTS CIRCUIT BREAKER PANEL. THE FEEDEMay 4, 2026 · N605VA · Tecnam P2006T · Electrical Power System WiringSDR SCNA20260505186Slide · not reportedL2 DOOR OPENED BY CATERING WHILE DOOR WAS ARMED. REMOVED ESCAPE SLIDE PACK AND COVER IAW AMM 25-66-01. INSPECTED AND REINSTALLED ESAPE SLIDE PACK AND COVER IAW AMM 25-66-01. ACFT OK FOR SERVICE.May 4, 2026 · N808SY · Boeing 7378BK · Escape SlideSDR SCNA20260505185Light · inoperativeDURING OPERATIONAL CHECK OF THE EMERGENCY LIGHTS (AISLE 15 RH AND WING EMERG. LIGHT AFT RH), WERE FOUND INOPERATIVE. ROUBLESHOOTING WAS PERFORMED, BATTERY PACK (M1671) OF OVERWING EMERG LIGHT AFT RH AND EMERGENCY LIGHT LAMP (AISLE 15 RH) WERE REPLACED IAW FIMay 4, 2026 · N827SY · Boeing 7378F2 · Emergency LightingSDR DALA2026050502831Shaft · not reportedRIGHT WING REMOVE AND INSTALL TORQUE SHAFT 6282CM TO PERFORM REPAIR T/E OVERHANG AREA. : REMOVED AND REINSTALLED RT WING FLAP TORQUE SHAFT 6282CM IAW AMM TASK 27-54-45-000-013-A AND 27-54-45-400-013-A REV 135.00. (LP: 1577369)May 4, 2026 · N368NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2026050502830Floor Support · corrodedLEVEL 2 CORROSION, TASK 5320-6010, PAX CABIN, AFT SECTION, FLOOR STRUCTURE AT FR70 Y-464.8MM, LONGITUDINAL BEAM WITH CORROSION. REPLACED NEW BEAM P/N: D5347219520200 IAW A319 SRM 53-41-14-03A, FIG 303 SHEET 2, ITEM 155. REV 157.00 , AND INATALLED IAW DWG # DMay 4, 2026 · N368NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026050502829Floor Support · corrodedLEVEL 2 CORROSION, TASK 5320-6010. PAX CABIN, AFT SECTION, FLOOR STRUCTURE, BETWEEN FR67 AND FR68, Y-1292 AND Y-1162.5 LONGITUDINAL BEAM (2EA SECTIONS) WITH CORROSION. REPLACED LONGITUDINAL BEAM (2EA) LOCATED AT PAX CABIN, AFT SECTION BETWEEN FR66 AND FR69, YMay 4, 2026 · N368NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR YENA2026050500447Unknown · odorFLT 36, PHX-JFK. CREW REPORTED A DIRTY SOCK ODOR ON CLIMB AND DURING LANDING. CREW STATED WITH PACK 1 OFF THE ODOR DISSIPATED.May 4, 2026 · N709JB · Airbus A320232 · Air Distribution SystemSDR YENA2026050500446Unknown · odorFLT 580, MBJ-JFK. ODOR OF DITY SOCKS DURING DESENT AND LANDING AND ODOR OF ENG OIL AFTER 2 SHUT DOWN.May 4, 2026 · N623JB · Airbus A320232 · Air Distribution SystemSDR 2026FA0000317Structure · corrodedACCOMPLISHED REMOVAL OF CORROSION TO AFFECTED AREAS OF VERTICAL STABILIZER. INSPECTED THE REMAINING MATERIAL USING ULTRASONIC TESTING AND EDDY CURRENT FOR CRACKS. NO CRACKS NOTED. ACCOMPLISHED DOUBLER REPAIR TO ONE NOTED LOCATION AND RESTORED FINISH TO ALL SURMay 4, 2026 · N572QS · Cessna 680A · Vertical StabilizerSDR DALA2026050402795Bottle · low pressureL3 DOOR ASSIST BOTTLE LOW. CORRECTIVE ACTION: REPLACED BOTTLE AND SERVICED PER A330 AMM 52-15. OK FOR SERVICE. (8844675) AIRCRAFT WAS GROUNDED.May 4, 2026 · N853NW · Airbus A330223 · Passenger/Crew DoorsSDR DALA2026050402789Lens · missingWHILE WORKING FCP FOUND MISSING LENS FOR EMERGENCY LIGHT AT MID LAV. REPLACED MISSING LENS COVER FOR MID LAV EMERGENCY LIGHT AS PER A321 AMM 33-51. (LP 1576658 - AIRCRAFT WAS GROUNDED)May 4, 2026 · N536DN · Airbus A321271NX · Emergency LightingSDR DALA2026050402788Battery Pack · faultedCABIN EMER LIGHT CHECK FAULTING BATTERY OF EPSU 11WL. REPLACED EPSU BATTERY 11WL PER A321 AMM 33-51-38, OPS CHECK GOOD. (LP 8098882 - AIRCRAFT WAS GROUNDED)May 4, 2026 · N384DN · Airbus A321211 · Emergency LightingSDR QR9R2026050400001Bleed Valve · inoperativeNR 2 BLEED VALVE FLAG DOES NOT COME ON. IDLE, FLIGHT, LOW POWER, ETC., NO INDICATIONS. REMOVED AND REPLACED BLEED VALVE IAW 75-31-00-900-804-A01.May 4, 2026 · Bolkms BK117C2 · Compressor Bleed ValveSDR AALA202605049967Vapor Barrier · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER AT STA 663.75, BETWEEN RBL 31.83 AND RBL 40. REPAIRED VAPOR BARRIER PER SRM 57-10-10-2R-2.May 4, 2026 · N874NN · Boeing 737823 · Fuselage Main, BulkheadSDR 3J7R2026050400001Light Sys · dimRH OVER WING EMERGENCY LIGHT DIMMay 4, 2026 · N533QS · Cessna 680A · Emergency LightingSDR SWIA2026050377191Blowout Panel · corrodedLEFT MLG WHEEL WELL, BLOW-OUT PANEL INBD BRACKET WAS CORRODED. REPLACED CORRODED BLOW OUT PANEL FOR LT MLG WHEEL WELL IAW SRM 51-42-06 AND 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE.May 3, 2026 · N455SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026050377155Channel · crackedLEFT MLG WHEEL WELL, 2ND OTBD BATT RIB CHANNEL WAS CRACKED AT FORWARD SIDE OF RIB. REMOVED AND REPLACED LT MLG WHEEL WELL 2ND OTBD BATT RIB CHANNEL IAW SRM 51-42-21.May 3, 2026 · N455SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR IPXA2026070896552Fitting · gougedDURING RIG CHECK OF THE RH AFT INBD FLAP (MAIN FLAP IN EXTENDED POSTION), AFT FLAP INBD TRACK ROLLER ATTACH FITTING OUTBD FACE FOUND WITH GOUGE DAMAGE. INSTALLED INBD CARTRIDGE ASSEMBLY AT INBD FLAP RT WING IAW CMM 57-53-44 AND 57-53-43.May 3, 2026 · N428UP · Boeing 75724APF · Trailing Edge FlapsSDR REXA2026070301043Frame · corrodedCORROSION ON FRAMES (5E/A) FS 469 BTW STGR 26L TO STGR 25L,FS 661+74 BTW STGR 26R TO STGR 27, FS 661+62 BTW STGR 26R TO STGR 26L , FS 661+32 STGR 26R TO STGR 27 AND FS 661+41 STGR 26R TO STGR 27 AT FWD CARGO COMPARTMENT. CORROSION ON FRAMES FS 661+74 BTW STGRMay 3, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026070301041Frame · damagedSECONDARY NRC FROM NRC 006 DURING THE REMOVAL OF AFT RAIL DOUBLER (CHANNEL): TWO ELONGATE HOLES WERE FOUNDED ON FRAME STA 1047 BTW STRINGER 17LH AND 16LH ELONGATE HOLES ON FRAME STA 1047 BTW STRINGER 17LH AND 16LH WERE REPAIRED PER REO 690-53-61-1774 REV. - -May 3, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA2026050376418Floorbeam · crackedFS280.00 RBL 12, RH COCKPIT FLOOR BEAM IS CRACKED WHERE IS ATTACHES TO THE FS280.00 FLOOR CROSSBEAM. REMOVED AND REPLACED CRACKED COCKPIT FLOORBEAM AT RBL 12 AND FS280.00 WITH NEW FABRICATED FLOOR BEAM,USING ALL NEW FASTENERS ON ITEM 36 INBOARD ANGLE, ITEM -3May 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026050376408Floorbeam · crackedBS 280 FLOORBEAM TO RBL 9 FLOORBEAM, THE THE AFT SIDE OUTBD ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED CRACKED OUTBD ATTACH ANGLE ON THE AFT SIDE OF RBL 9.0 AT BS280 WITH NEW ANGLE USING ALL NEW FASTENERS IAW SRM 51-42-21-001-001-A01 AND DWG CC670-34010 REMay 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026050376401Fitting · wornAFT BAGGAGE-BAY DOOR SURROUND STRUCTURE, STOP FITTINGS WORN, REPAIRED AFT CARGO DOOR SURROUND STOP FITTINGS. PER REO 670-53-61-2721 REV --. NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-900-1002-SKY.May 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2026050376400Bulkhead · damagedRIGHT BS 280 BULKHEAD APPROXIMATELY RBL13-14, THE AFT SIDE LOWER FLOOR-TO-BULKHEAD ANGLE HAS FASTENER HOLE WITH DRILL DAMAGE. REMOVED AND REPLACED RT BS 280 BULKHEAD CROSSBEAM REF SRM 51-42-06-001-001-A01, SRM 51-42-22-001-001-A01, SRM 51-42-21-001-001-A01 ANDMay 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA2026050376376Hinge · gougedFORWARD BAGGAGE BAY DOOR SURROUND, FORWARD HINGE FUSELAGE SIDE IS GOUGED, REMOVED AND REPLACED GOUGED FWD BAGGAGE BAY DOOR, FWD HINGE WITH NEW SERVICEABLE HINGE USING NEW HARDWARE, REF REF CRJ 700 SRM 51-41-02-001-001-A01 AND DWGSH670-33750 REV AA. . CALIBRAMay 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA2026050376373Floor Panel · corrodedCOCKPIT ENTRANCE FLOOR PANEL AFT ATTACH ANGLE ON THE FS280 CROSSBEAM IS CORRODED. REMOVED AND REPLACED CORRODED COCKPIT ENTRANCE FLOOR PANEL AFT ATTACH ANGLE AT FS280.00 BETWEEN RBL 9.0 AND LBL 9.0 WITH NEW AFT ATTACH ANGLE (P/N CC670-34095-1SB) USING ALL NEWMay 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage Floor PanelSDR SWIA2026070276371Floorbeam · crackedBS 280, LBL 12, LT COCKPIT FLOORBEAM IS CRACKED WHERE IS ATTACHES TO THE BS 280 FLOORBEAM. REMOVED AND REPLACED CRACKED COCKPIT FLOORBEAM AT LBL 12 AND BS 280 WITH NEW FABRICATED FLOOR BEAM,USING ALL NEW FASTENERS ON ITEM 36 INBOARD ANGLE, ITEM -38 INBOARD LOMay 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026050376365Floorbeam · crackedFS280.00 FLOORBEAM TO LBL 9 FLOOR BEAM, THE THE AFT SIDE OUTBD ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED CRACKED OTBD ATTACH ANGLE ON THE AFT SIDE OF LBL 9.0 AT BS 280 WITH NEW ANGLE (P/N CC670-34099-1SB) USING ALL NEW FASTENERS, REF SRM 51-42-21-001-001-May 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR IPXA2026060903170Bulkhead · crackedNR 1 ENG, INLET INTAKE, AFT BULKHEAD AT 3 O'CLOCK POSITION WITH CRACK APPROX 2 INCHES LONG. INSTALLED NEW WEB IN ZONE 400 NR 1 ENG, INLET INTAKE, AFT BULKHEAD AT 3 O'CLOCK POSITION. IAW SRM 54-10-00 REPAIR NR 14, PAGE 201, AND SRM 51-40-21-001.May 3, 2026 · N156UP · Airbus A300F4622R · Nacelle/Pylon, Bulkhead/FirewallSDR VNAA202606120008Rib · crackedCRACK ON RIB OF LEADING EDGE SS 58.00 AT RT WING. CRACK ON RIB OF LEADING EDGE SS 58.00 AT RT WING WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-10-001-001-A01, AND SRM 51-42-21-001-001-A01.May 3, 2026 · N563NN · Cndair CL6002D24 · Leading Edge DevicesSDR VNAA202606120007Rib · crackedCRACK ON RIB OF LEADING EDGE STA SS 58.00 AT LH WING. CRACK ON RIB OF LEADING EDGE SS 58.00 AT LT WING WAS REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01.May 3, 2026 · N563NN · Cndair CL6002D24 · Leading Edge DevicesSDR IPXA2026051002662Floor Support · brokenAVIONICS COMPARTMENT RH SIDE AT FR 10 AND FLOOR SUPPORT Y-679 ANGLE BRACKET CRACKED. INSTALLED NEW WEB P/N: A53611977200 AT AVIONICS COMPARTMENT RH SIDE AT FR 10 AND FLOOR SUPPORT Y-679 I.A.W. SRM 51-40-21.May 3, 2026 · N156UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026060903366Sleeve · crackedNR 1 ENG, I/B T/R, TRANSLATING SLEEVE, LWR CENTER AREA, INTERNAL STRUCTURE, WITH A CRACK APPROX 3 INCHES LONG. INSTALLED ENG #1 I/B TRANSLATING SLEEVE ASSY IAW AMM A300 78-32-11/401 STEP 3C (1) THRU 3C (11)May 3, 2026 · N156UP · Airbus A300F4622R · Engine Thrust ReverserSDR CALA2026061016956Stringer · corrodedFWD CARGO COMPARTMENT AIR DISTRUBUTION BAY STR 27R IS POSSIBLE CORROSION, NEAR STA 540. INSTALLED REPAIR PARTS ON STR 27 RH, BTW BS 500I - 540 AT FWD CARGO BAY IAW SRM 53-00-03-2R-1 REPAIR 1 PAR. 4. K. AND SRM 51-40-02-0G-0. REMOVED AND EVALUATED CORROSION, May 3, 2026 · N14249 · Boeing 737824 · Fuselage Main, Longeron/StringerSDR J7SA2026060900484Anti-Ice System · noisyCREW REPORTS LOUD CABIN SQUEALING NOISE DURING CLIMB BETWEEN 6000 FT AND 7000 FT DURING ENGINE AND WING ANTI ICE SELF-TEST. THE NOISE LASTED 5-10 SECONDS AND DISSIPATED ENTIRELY AFTER SELF-TEST CONCLUSION. DURING DESCENT, CREW TESTED ANTI-ICE AT DIFFERENT ALTIMay 3, 2026 · N417FX · Emb EMB545 · Airfoil Anti/De-ice SystemSDR SWAA2026060895156Frame · crackedCRACKED FRAME, BS 312, BTW STR 5L & STR 6L IN THE PASSENGER CABIN. REPAIRED THE FRAME IAW EA M-22-153-01244.May 3, 2026 · N253WN · Boeing 7377H4 · Fuselage Main, FrameSDR REXA2026060400927Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE ATMay 3, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026060400926Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE May 3, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026060400923Hinge · corroded"CORROSION ON ACCESS PANEL 832EL AND CORROSION ON HINGE AT ACCESS DOOR 832ET CORROSION WAS REMOVED OF ACCESS PANEL 832EL PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN LIMITS PER CRJ-900 SRM 52-11-32-101-001-A01, HINGE (P/N: CC670-31981-3) AT ACCESS May 3, 2026 · N909XJ · Cndair CL6002D24 · Passenger/Crew Doors