N544EA
Service difficulty reports · 90
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 = 'N544EA' 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.
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 = 'N544EA' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR VNAA202608210033Angle · corrodedAFT INNER SKIN WAS REMOVED, CORROSION ON INTERNAL ANGLE WAS FOUND AT PASSENGER DOOR. INTERNAL ANGLE OF PASSENGER DOOR WAS REPLACED IAW SRM 51-42-06-001-001-A01.SDR VNAA202608210032Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 108 OUT SIDE (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 108 OUT SIDE (1EA) ON GALLEY 1 WAS REPLACED IAW CMM 25-33-44, REV. 3.SDR VNAA202608210031Lug · corrodedSECONDARY NRC AFTER LH AILERON BUSHINGS REMOVAL CORROSION FOUND ON FITTING #1, CENTER FITTING L2, L3 , L5 AND FITTING #4 UPPER AND LOWER AT LH AILERON. FITTING #4 UPPER AND LOWER LUGS AT LH AILERON WERE CLEANED PER CRJ 700 SRM 51-26-00-001-001-A01 THEN INSPESDR VNAA202608210030Lug · corrodedAFTER RT AILERON BUSHINGS REMOVAL, CORROSION FOUND ON RT AILERON FITTING 1, LUG R2 & R5 ALSO ON FITTING 4 UPPER AND LOWER LUGS. UPPER & LOWER LUGS ON FITTNG 4 & HINGE FITTING 1 AT RT AILERON WERE CLEANED IAW SRM 51-26-00-001-001-A01, THEN INSPECTED IAW NDT MASDR VNAA202608210029Canister · crackedCRACK ON CANISTER WELDED NO. 3 ON STA WS 148.00 OF INTERNAL RH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 AT RH MAIN FUEL TANK. WAS REPAIR PER REO 670-57-42-577 REV. --.SDR VNAA202608210028Canister · crackedCRACK ON CANISTER WELDED NO. 3 ON STA WS 148.00 OF INTERNAL LH MAIN FUEL TANK. CANISTER, WELDED NR 3 IN STA. WS148 AT RH MAIN FUEL TANK. WAS REPAIR PER REO 670-57-42-577 REV. --.SDR VNAA202608210027Hinge Fitting · excess playFREEPLAY ON BEARING OF RUDDER HINGE FITTING #3 AT REAR SPAR OF VERTICAL STABILIZER. BEARING OF RUDDER HINGE FITTING #3 AT REAR SPAR OF VERTICAL STABILIZER WAS REPLACED PER RIL #2103. REV. B. AND RIL #1213. 03)SDR VNAA202608210026Seat Track · corrodedCORROSION ON SEAT RAIL RBL9 (02 SEGMENTS), (SEG 1) BTW FS 677.00 TO FS 863.00, (SEG 2) BTW FS 863.00 TO FS 977.00 AT PASSENGER CABIN. CORROSION ON SEAT RAIL RBL9 (02 SEGMENTS), (SEG 1) BTW FS 677.00 TO FS 863.00, (SEG 2) BTW FS 863.00 TO FS 977.00 AT PASSENGSDR VNAA202608210025Seat Track · corrodedCORROSION ON SEAT RAIL LBL9 (02 SEGMENTS), (SEG 1) BTW FS 677.00 TO FS 863.00, (SEG 2) BTW FS 863.00 TO FS 989.00 AT PASSENGER CABIN. CORROSION ON SEAT RAIL LBL9 (02 SEGMENTS), (SEG 1) BTW FS 677.00 TO FS 863.00, (SEG 2) BTW FS 863.00 TO FS 989.00 AT PASSENGESDR VNAA202608210016Seat Track · corrodedCORROSION ON SEAT RAILS LBL9 BTW FS 477.40 - FS 677.00 (3EA) AT PASSENGER CABIN. CORROSION ON SEAT RAILS LBL9 BTW FS 477.40 - FS 677.00 (3EA) AT PASSENGER CABIN WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED OUT LIMITS PER CRJ 900 53-31-49-101-00SDR VNAA202608210015Seat Track · corrodedCORROSION ON SEAT RAILS RBL9 BTW FS 477.40.00 TO FS 693.00 (SEVERAL LOCATIONS). CORROSION ON SEAT RAILS RBL9 BTW FS 477.40.00 TO FS 693.00 WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED OUT LIMITS PER CRJ 900 53-31-49-101-001-A02 AND REPLACED PESDR VNAA202608210014Seat Track · corrodedCORROSION ON SEAT RAILS RBL9 BTW FS 349.00 - FS 477.40 AT PASSENGER CABIN. SEAT RAILS RBL9 BTW FS 349.00 - FS 477.40 AT PASSENGER CABIN WERE REPLACED PER CRJ-900 AMM 53-00-49SDR VNAA202608210024Angle · corrodedCORROSION ON MID CAP ANGLE AND KICK PLATE BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME. CORROSION ON KICK PLATE BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME WAS REMOVED AND EVALUATED WITHIN OF LIMITS PER CRJ-700 SRM 51-21-06-001SDR VNAA202608210022Seat Track · corrodedCORROSION ON SEAT RAIL LBL9 (02 SEGMENTS), (SEG 1) BTW FS 485.00 TO FS 581.00, (SEG 2) BTW FS 581.00 TO FS 677.00 AT PASSENGER CABIN. CORROSION ON SEAT RAIL LBL9 (02 SEGMENTS), (SEG 1) BTW FS 485.00 TO FS 581.00, (SEG 2) BTW FS 581.00 TO FS 677.00 AT PASSENGSDR VNAA202608210012Web · crackedCRACK ON PREVIOUS REPAIR OF ADG COMPARTMENT UPPER WEB, BELOW SETTLEMENT ADG RETRACTION PUMP AREA. ADG COMPARTMENT UPPER WEB, BELOW SETTLEMENT ADG RETRACTION PUMP AREA WAS REPAIRED PER CRJ-700 SRM 53-11-43-201-001-A01SDR VNAA202608210023Seat Track · corrodedCORROSION ON SEAT RAIL RBL9 (03 SEGMENTS), (SEG 1) BTW FS 349.00 TO FS 485.00, (SEG 2) BTW FS 485.00 TO FS 581.00, (SEG 3) BTW FS 581.00 TO FS 677.00 AT PASSENGER CABIN. CORROSION ON SEAT RAIL RBL9 (03 SEGMENTS), (SEG 1) BTW FS 349.00 TO FS 485.00, (SEG 2) BSDR VNAA202608210021Seat Track · corrodedCORROSION ON SIDE SEAT RAILS (L/H AND R/H) (4 EAS) LOCATED APPROXIMATELY AT FS 785.15 TO 938.00 ON PAX CABIN. CORROSION ON SIDE SEAT RAILS (L/H AND R/H) (4 EAS) LOCATED APPROXIMATELY AT FS 785.15 TO 938.00 ON PAX CABIN WERE EVALUATED DUE TO EXCESSIVE DAMAGE PSDR VNAA202608210020Seat Track · corrodedCORROSION ON SIDE SEAT RAILS L/H (5 EAS) LOCATED APPROXIMATELY AT FS 379.00 TO 761.85 ON PAX CABIN. CORROSION ON SIDE SEAT RAILS L/H (5 EAS) LOCATED APPROXIMATELY AT FS 379.00 TO 761.85 ON PAX CABIN WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, WERE EVASDR VNAA202608210019Seat Track · corrodedCORROSION ON SIDE SEAT RAILS R/H (5 EAS) LOCATED APPROXIMATELY AT FS 485.00 TO 761.85 ON PAX CABIN. CORROSION ON SIDE SEAT RAILS R/H (5 EAS) LOCATED APPROXIMATELY AT FS 485.00 TO 761.85 ON PAX CABIN WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, WERE EVALSDR VNAA202608210018Fitting · corrodedCORROSION OF FITTING SUPPORT (2 EA) AT FWD GALLEY. CORROSION OF FITTING SUPPORT (2 EA) AT FWD GALEY WAS EVALUATED OUT LIMITS PER CRJ 700 SRM 53-00-00-101-001-A01 AND REPLACED
PER CRJ700 SRM 51-42-21-001-001-A01.SDR VNAA202608210017Access Panel · corrodedCORROSION ON CONTERSINKS OF ACCESS PANEL 542AT,642 AT ACCESS PANEL 642AT MUST BE REPLACED IAW TICKET #86402, AND ACCESS PANEL 542AT WAS REPAIRED PER REO 670-57-21-1146 REV. -ASDR VNAA202608210010Bracket · crackedCRACKS ON SUPPORT BASE MAIN BATTERY DIRECT BUS (JB6) AT FWD EQUIPMENT COMPARTMENT. CRACKED SUPPORT BASE MAIN BATTERY DIRECT BUS (JB6) AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01SDR VNAA202608210013Bracket · corrodedCORROSION BRACKETS MACHINE (5 EA) OF (LBL 2.6), (LBL 24), BTW FS 517-597, AT FWD SURROUND STRUCTURE CARGO COMPARMENT. PAINT ON BRACKETS MACHINE (2 EAS) WAS REMOVED AND NO DAMAGE WAS FOUND. FINISH PAINT WAS RESTORED PER CRJ700 SRM 51-26-01-001-001-A01 AND SRMSDR VNAA202608210011Web · crackedCRACK ON WEB BTW FS195 TO FS205 AND WL79.50 (LH SIDE) ON INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT. WEB BTW FS195 TO FS205 AND WL79.50 (LH SIDE) ON INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ 700 SRM 53-11-43-201-001-A01SDR VNAA202608210009Floorbeam · crackedCRACK ON CROSSBEAM FITTING BTW FS W280 LBL 12 (BELOW FLOOR) AT PASSENGER CABIN. FLOORBEAM BTW FS W280 LBL 12 AT PASSENGER CABIN WAS REPAIRED PER CRJ-700 SRM 53-11-43-201-003-A01SDR VNAA202608210008Drag Angle · crackedCRACK ON FWD DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE). FWD DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE) WAS REPAIRED PER CRJ 700 SRM 55-31-00-201-001-A01SDR VNAA202608210005Skin · crackedIAW TRFKE00F6TG7: 2800FH PERM REPAIR - TEMPORARY DISPOSITION FOR REWORKED DENT TO LHS SLAT#1 OUTER SKIN AND LOWER ANGLE AT WS58.75. ENGINEERING COMMENTS: ANGLE PN CC670-12648-1 MUST BE REPLACED. TRFKE00F6TG7 DISPLAYED THAT THE ENTIRE SLAT PN CC670-12600-3 IS SDR VNAA202608210007Stiffener · corrodedCORROSION ON STIFFENER 1EA, CLIP 1EA ALSO INTERNAL SKIN LP GROUND CONNECTION ACCESS SERVICING DOOR 182BR. CORROSION CLIP 1EA ALSO INTERNAL SKIN LP GROUND CONNECTION ACCESS SERVICING DOOR 182BR. WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND WAS EVALUATESDR VNAA202608210006Drag Angle · crackedCRACK ON AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE). AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE).WAS REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01SDR VNAA202608210004Drag Angle · crackedCRACK ON AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (LH SIDE). CRACK ON AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (LH SIDE) WAS REPAIRED PER CRJ-700 SRM 55-31-00-201-001-A01. PAX DOOR HINGE PN 601R318073-5 WASSDR VNAA202608210003Hinge · wornIN REF TO TRFKE00EQGY2: PERM REPAIR - PASSENGER DOOR HINGE REPLACEMENT REPLACE THE PASSENGER DOOR HINGE IN ACCORDANCE WITH CRJ700 SRM TASK 52-11-01-201-002-A01. AFTER HINGE REPLACEMENT. SEND E-MAIL REQUEST TO DL_PSA_MAINTENANCE_PROGRAMS@PSAAIRLINES.COM TO COMPSDR VNAA202608210002Skin · gougedGOUGE - LH PAX DOOR CUTOUT AT FS 349 WITHIN 5371.31 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. DISPOSITION FOR REWORKED GOUGE DAMAGE TO FUSELAGE SKIN AT FS349.00 BTW SSDR VNAA202608210001Hinge Fitting · corrodedIN REF TO TRFKE00A2A3A: PERM REPAIR - BLENDED GOUGE DAMAGE TO R/H OUTB'D HINGE FITTING GROUND SPOILER STA 21.8 REPAIR OR REPLACE PART IN ACCORDANCE WITH APPROVED PROCEDURES WITHIN 8000 FH. ENGINEERING COMMENTS: HINGE FITTING MUST BE REPLACED PN CC670-16052-4. SDR VNAA202509060001Attach Fitting · wornPAX DOOR FOLDING STEP (CONTROL ROD ATTACH L-BRACKET IS LOOSE AND SLOT FOR CONTROL ROD IS BINDING FROM ELONGATED JAGGED HOLE). REMOVED AND REPLACED BRACKET IAW SRM 51-40-11-001-001-A01 AND MHIRJ CMM 52-11-00.SDR VNAA2024062011101Control Handle · failedRED GEAR DISAGREE MSG AFTER TAKE OFF / FOUND LG SELECTOR PANEL DIRTY WITH TYPICAL FUZZY CONTAMINATION, REMOVED AS REQUIRED, NO OTHER DISCREPANCIES NOTED. REPLACED LG LEVER IAW CRJ 700 AMM 32-31-01-000/400-802. ALL OPS CHECKS GOOD AT THIS TIME, NO FAULTS NOTED,SDR VNAA202302180003None · dentedEA22-C7-57-1405 (PERM REPAIR BEFORE 27,133.27 FH - LH IB FLAP) WITHIN 800FLIGHT HOURS (27,133.27FH), REPAIR OR REPLACE OF THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES.SDR VNAA202302180002None · corrodedTWO HUCK-BOLTS ARE CORRODED AT FS 797 ON THE RH PRESSURE FLOOR TAB IN THE WHEEL WELL (RBL 36.)SDR VNAA202202180001None · noneTWO HUCK-BOLTS ARE CORRODED AT FS 797 ON THE RH PRESSURE FLOOR TAB IN THE WHEEL WELL (RBL 36.)SDR VNAA202302100004Doubler · corrodedANTENNA DOUBLER IS CORRODED BETWEEN F.S. 280 TO F.S. 295 AND AT STGR 27
CORRECTIVE ACTION REMOVED ANTENNA DOUBLER BETWEEN F.S.295-F.S.310 IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED NEW ANTENNA DOUBLER BETWEEN F.S.295-F.S.310 IAW CRJ 700 SRM 51-42-06-SDR VNAA202302090003Frame · corrodedDISCREPANCY: F.S. 1088.20 FRAME IS CORRODED BETWEEN STGR 26R TO STGR 26L.
CORRECTIVE ACTION:
COMPLIED WITH REPAIR TO F.S. 1088.20 FRAME BETWEEN STGR 26R TO STGR 26L IAW OLIVER WYMAN CAVOK EA 23-C7-53-0116, DATED 2/26/23, REV IR.SDR VNAA202302090002Frame · corrodedF.S. 333 FRAME IS CORRODED BETWEEN STGR 27 TO STGR 26L.
CORRECTIVE ACTION:
REPAIRED FS 333 LOWER FRAME SEGMENT IAW CRJ-700 SRM 53-00-06-201-006-A01.SDR VNAA202302090001None · corrodedNUT PLATE CHANNEL BETWEEN F.S. 1000 TO F.S. 1015 AND BETWEEN STGR 27 TO STGR 26L IS CORRODED.
CORRECTIVE ACTION:
INSTALLED NEW NUT PLATE CHANNEL P/N MM670-70327-001 BETWEEN F.S. 1000 TO F.S. 1015 AND BETWEEN STGR 27 TO STGR 26L IAW CRJ700 SRM 51-42-06-0SDR VNAA2023013198008Stringer · corrodedSTGR 26R IS CORRODED BETWEEN F.S. 295 TO F.S. 310.SDR VNAA202301298007Intercostal · corrodedSERVICE DOOR INTERCOSTAL IS CORRODED BETWEEN F.S. 310 TO F.S. 319.70 AND AT STGR19R.SDR VNAA202301298006Skin · gougedEXTERNAL FUSELAGE SKIN HAS 2EA.SCRATCHES APPROX. 1 INCH LONG AT F,S.265, 3 INCHES BELOW PILOT WINDSHIELD.
CORRECTIVE ACTION: REPAIRED FUSELAGE SKIN AT F.S. 265 STGR 12 IAW OLIVER WYMAN EA 23-C7-53-0096 REV IR, DATED 01/23/2023.SDR VNAA202301298005Attach Fitting · gougedL/H AFT WING TO FUSELAGE ATTACHMENT FITTING IS GOUGED ON THE AFT I/B EDGE APPROXIMATELY .009" DEEP AND 3" IN LENGTH. CORRECTIVE ACTION: REPAIRED L/H AFT WING FUSELAGE ATTACHMENT FITTING IAW OLIVER WYMAN EA 23-C7-57-0110 REV IR, DATED 01/23/2023.SDR VNAA202301298004Fitting · gougedR/H AFT WING TO FUSELAGE ATTACHMENT FITTING IS GOUGED ON THE AFT I/B EDGE APPROXIMATELY .008" DEEP AND 2" IN LENGTH. CORRECTIVE ACTION: REPAIRED R/H AFT WING FUSELAGE ATTACHMENT FITTING IAW OLIVER WYMAN EA 23-C7-57-0111 REV IR, DATED 01/23/2023.SDR VNAA202209281111None · arcedCA WINDSHIELD DELAMINATING AND ARCING. REMOVED AND REPLACED CA'S WINDSHIELD IAW CRJ 700 AMM 56-11-01-000/400-801-PSA. C/W (L/H) WINDSHIELD INSTALLATION IAW CRJ700 AMM 56-11-01-400-801-PSA. OPS CHECKS AND LEAK CHECKS GOOD AT THIS TIME, NO DEFCECTS NOTED."SDR VNAA2022092499981Stringer · crackedSTRINGER 3L LINTEL IS CRACKED FROM THE FWD EDGE OF THE STRINGER THRU .2" AFT OF THE 3RD AFT FASTENER HOLE. FAILED NDT INSPECTION. PERFORMED REPAIR OF STRINGER 3L LINTEL IAW REO 670-53-21-493 REV D.SDR V0XD20220714001Skin · damagedLH FUSELAGE SKIN AT FS565 AND STRINGER 17L HAS A PREVIOUS BLEND. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR TO THE LH FUSELAGE SKIN BY STRIPPING PAINT, PERFORMING UT AND UT INSPECTIONS AND RESTORING FINISH IAW OLIVER WYMAN CAVOK EA 22-C7-53-0443 REV A. N
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