N289CT
Service difficulty reports · 260
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 = 'N289CT' 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 = 'N289CT' 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 SWAA2025101323850Slide · detachedFORWARD ENTRY SLIDE HARD TO ARM AND PART OF SLIDE FELL OUT. RE-ATTACHED VELCRO AT BOTTOM OF FWD ENTRY DOOR SLIDE IAW AMM 25-66-01SDR SWAA2025032002743Panel · crackedPANEL 621PB CRACKED AT FWD I/B END. <[01] CRACK AT FWD I/B END OF PANEL 621PB WAS REPAIRED IAW SRM 51-70-05-2R-6.; [02] VERIFIED CORRECTIVE ACTION #1.SDR SWAA2025032498497Attach Angle · crackedVERTICAL FIN FRONT SPAR; FWD SPRING ANGLE (176A3101-26) CRACKED AT LT ATTACH POINT<[01] REMOVED AND REPLACED VERTICAL FIN FRONT SPAR FWD SPRING ANGLE IAW SRM 51-40-02-0G-0 AND DWG #176A3101 SHEET 4 REV-.SDR SWAA2025032498188Skin · crackedCRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 25' FROM FWD EDGE; 0.6' IN LENGTH (MARKED)<[01] REPAIRED RH LOWER HORIZONTAL STABILIZER SKIN AT STAB STA 193.90; 25' FROM FWD EDGE IAW SRM 55-10-01-2R-11 REPAIR 11.;[02] VERIFIED COMPLETION CORRSDR SWAA2025032497561Stub Frame · crackedCRACK FOUND ON R1 DOOR STUB FRAME 0.7' ABOVE SEAL DEPRESSOR; 0.6' FWD FROM DOOR CUT OUT. L: 0.5' MARKED. <[01] REMOVED CRACKED R1 DOOR STUB FRAME AND REPLACED ALL I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8370 REV: D; [02] VERIFIED COMPLETION CORRECTIVE ACTISDR SWAA2025032497558Frame · corrodedCORROSION ON BS 303 FRAME LBL 56 WL 208. <[01] REPAIRED CORROSION ON BS 303 FRAME LBL 56 WL 208 PER EA 25-153-00457-WIP1; [02] VERIFIED ITEM 1.SDR SWAA2025032497560Support Angle · corrodedCORROSION ON FWD ENTRY DOOR THRESHOLD SUPPORT ANGLE BS 320 AND 338 LBL 56 WL 208. <[01] REMOVED AND REPLACED FWD ENTRY DOOR THRESHOLD SUPPORT ANGLE I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8110 REV A; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASURESDR SWAA2025032497565Intercostal · crackedCRACKED INTERCOSTAL BS 380-400 RBL 40 WL 208. <[01] REMOVED AND REPLACED CRACKED INTERCOSTAL WITH NEW AT BS 380-400 RBL 40 WL 208. VERIFIED SRM 53-00-04-1A-1 IS APPLICABLE FOR ALLOWABLE DAMAGE ON CRACKED INTERCOSTAL BS 380-400 RBL 40 WL 208. REMOVED CRACKED ISDR SWAA2025032497573Strap · corrodedCORROSION ON STRAP BS 1028 RBL 18 WL 208. <[01] REMOVED AND REPLACED NEW STRAP BS 1016-1026 RBL 18 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5730 REV:C; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2025032497569Strap · corrodedCORROSION ON STRAP BS 1016-1026 RBL 3 WL 208. <[01] REMOVED AND REPLACED NEW STRAP BS 1016-1026 RBL 3 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5730 REV:C; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2025032497570Strap · corrodedCORROSION ON STRAP BS 1017 LBL 3 WL 208. <[01] REMOVED AND REPLACED STRAP BS1017 LBL3 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 REV:B; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2025032497559Sill Drain · corrodedCORROSION ON FWD ENTRY DOOR MOP SILL BS 303 LBL 56 WL 208.<[01] REMOVED AND REPLACED FED MOPSILL I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8110 REV A;[02] VERIFIED CORRECTIVE ACTION. CARD COMPLETE.SDR SWAA2025032497098Stub Frame · crackedFOLDING AND PEELING OFF INTERNAL FUSELAGE SKIN ON UPPER-FWD COUNTER FRAME OF R1 DOOR; DIMENSIONS OF 3' LONG; 1' DEEP; AND 3/32' PEELING OFF.<[01] DURING INSPECTION STUB FRAME FOUND CRACK AND GENERATED CCN TTG8Q00YSN5X THEREFORE DISCREPANCY REPORTED BEING NULL SDR SWAA2025032497564Floor Support · crackedCRACKED INTERCOSTAL BS 312-328 LBL45 WL 208.<[01] REMOVED CRACKED INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL BS 312-328 LBL45 WL 208.;[02] ALL TASK STEPS COMPLETED;[03] JOB COMPLETESDR SWAA2025032497562Floor Support · crackedCRACKED INTERCOSTAL BS 312-328 RBL 30 WL 208.<[01] REMOVED CRACKED INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL BS 312-328 RBL 30 WL 208.;[02] ALL TASKS STEPS COMPLETED;[03] JOB COMPLETESDR SWAA2025032497082Plate · corrodedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156 <[01]. CORROSION ON AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT LIMITS. REMOVE AND REPLACE R/H FLOOR TO SISDR SWAA2025032497079Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED <[01]. AFT CARGO BAY AFT CORNER SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1.SDR SWAA2025032097081Support Plate · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156 <[01]. CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT LIMITS. REMOVE AND REPLACE L/H FLOOR TO SIDEWASDR SWAA2025031997078Scuff Plate · crackedFWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED <[01]. FWD CARGO BAY FWD CORNER SCUFF PLATE WAS REPAIRED PER SRM 53-30-15-2R-1.SDR SWAA2025031997085Floor Panel · delaminatedCABIN FLOOR PANEL 232AF TOP SURFACE IS DELAMINATED. <[01] CABIN FLOOR PANEL 232AF WITH TOP SURFACE DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.; [02] VERIFIED CORRECTIVE ACTION #1.SDR SWAA2025031997096Floor Panel · delaminatedCABIN FLOOR PANEL 221FF TOP SURFACE IS DELAMINATED. <[01] CABIN FLOOR PANEL 221FF TOP SURFACE WITH DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2025031997090Floor Panel · delaminatedCABIN FLOOR PANEL 241ACF HAS TOP SURFACE DELAMINATION. <[01] CABIN FLOOR PANEL 241ACF WITH TOP SURFACE DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2025031997092Floor Panel · delaminatedCABIN FLOOR PANEL 241UF HAS TOP SURFACE DELAMINATION. <[01] CABIN FLOOR PANEL 241UF; WITH TOP SURFACE DELAMINATION; WAS REPAIRED IAW SRM 53-00-50-2R-0.; [02] ITEM 1 SHOULD READ: CABIN FLOOR PANEL 241UF; WITH TOP SURFACE DELAMINATION; WAS REPLACED WITH A NEWLY SDR SWAA2025031997080Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] CORROSION ON AFT CARGO BAY R/H SHIELD; FOUND TO BE OUT LIMITS. REMOVE AND REPLACE R/H SHIELD; BS 767 TO BS 794 IAW SRM 51-40-02-0G-0; SRM 51-40-0SDR SWAA2025031997087Cargo Track · crackedAFT CARGO BAY CARGO TRACK IS CRACKED BS747 AND BS727E RBL13 WL156<[01] REMOVED AND REPLACED AFT CARGO BAY CARGO TRACK BS727+4 - BS887 RBL13 WL156 IAW SRM 51-40-02-0G-0; DWG 146A7500 REV:- ; DWG 147A7500 REV:- AND DWG 146A0061 REV:A;[02] REPAIRED AS PER SRM 53-SDR SWAA2025032496721Structure · corrodedCORROSION ON INNER CHORD AT BS 698 RBL 63 WL 208. (MARKED) <[01] REFER TO FAULT TTG8Q00YQ2WS WHERE EA 25-153-00417 WAS ADDED AS A SUBTASK; [02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2025032095952Panel · crackedPANEL 621YB CRACKED ON O/B FWD. END <[01] PANEL 621YB WITH CRACK ON O/B FWD END WAS REPAIRED PER SRM 51-70-05-2R-6.SDR SWAA2025031995954Floor Panel · debondedCABIN FLOOR PANEL 231JF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 231JF DISBONDED TOP SURFACE REPAIRED IAW SRM 53-00-50-2R-0; [02] CORRECTION TO ITEM 1: FABRICATED NEW CABIN FLOOR PANEL 231JF IAW SRM 53-00-50-2R-0.; [03] VERIFIED CORRECTIVE ACTION ITESDR SWAA2025031995955Floor Panel · delaminatedCABIN FLOOR PANEL 242DF HAS DELAMINATED TOP SURFACE. <[01] REPLACED DAMAGED 242DF FLOOR PANEL WITH SERVICEABLE PANEL P/N:144A5810-150 IAW SRM 51-10-02-0G-0 PARA 9.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025031995959Floor Panel · debondedCABIN FLOOR PANEL 241EF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 241EF WITH DISBONDED TOP SURFACE WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.; [02] VERIFIED CORRECTIVE ACTION #1.SDR SWAA2025031995961Floor Panel · debondedCABIN FLOOR PANEL 232FF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 232FF DISBONDED TOP SURFACE REPAIRED IAW SRM 53-00-50-2R-0.; [02] CORRECTION TO ITEM 1: FABRICATED NEW CABIN FLOOR PANEL 232FF IAW SRM 53-00-50-2R-0.; [03] VERIFIED CORRECTIVE ACTION ITSDR SWAA2025031995963Floor Panel · delaminatedCABIN FLOOR PANEL 242BF HAS DELAMINATED TOP SURFACE. <[01] REPLACED DAMAGED 242BF FLOOR PANEL WITH SERVICEABLE PANEL P/N:144A5810-149 IAW SRM 51-10-02-0G-0 PARA 9.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025031995967Floor Panel · debondedCABIN FLOOR PANEL 231ZF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 231ZF; WITH DISBONDED TOP SURFACE; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION #1.SDR SWAA2025031995962Floor Panel · debondedCABIN FLOOR PANEL 231MF HAS DISBONDED TOP SURFACE. <[01] 231MF FLOOR PANEL DISBOND DAMAGE ON UPPER AND LOWER SURFACE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]. ATTACHESDR SWAA2025031995957Floor Panel · delaminatedCABIN FLOOR PANEL 242AF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 242AF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2025031995964Floor Panel · delaminatedCABIN FLOOR PANEL 231XF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 231XF; WITH TOP SURFACE DELAMINATION; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025031995958Floor Panel · delaminatedCABIN FLOOR PANEL 241AF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 241AF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0127.; [02] VERIFIED CORRECTIVE SDR SWAA2025031995965Floor Panel · delaminatedCABIN FLOOR PANEL 231YF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 231YF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025031995966Floor Panel · delaminatedCABIN FLOOR PANEL 241BF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 241BF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2025031995956Floor Panel · delaminatedCABIN FLOOR PANEL 232RF HAS DELAMINATED TOP SURFACE. <[01] DAMAGE TO CABIN FLOOR PANEL 232RF WAS BEYOND ECONOMICAL REPAIR; FABRICATED NEW PANEL IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2025032495947Strap · corrodedCORROSION ON STRAP AT MID CABIN BS696 RBL67 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID PROVIDE STRUCTURE ID/DRAWING AS REQUIRED IAW 737 NDTM PART 4; 51-00-00; PROC 2 STEP 4. C.; [02] EDIT: 'DID NOT PROVIDESDR SWAA2025032495948Strap · corrodedCORROSION ON STRAP AT MID CABIN BS703 RBL64 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID PROVIDE STRUCTURE ID/DRAWING AS REQUIRED IAW 737 NDTM PART 4; 51-00-00; PROC 2 STEP 4. C.; [02] EDIT: 'DID NOT PROVIDE SDR SWAA2025032495942Strap · corrodedCORROSION ON STRAP AT MID CABIN BS707 RBL63 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID NOT PROVIDE STRUCTURE ID/DRAWING AS REQUIRED IAW 737 NDTM PART 4; 51-00-00; PROC 2 STEP 4. C.; [02] REMOVED CORROSION OSDR SWAA2025032495945Structure · corrodedCORROSION ON INNER CHORD AT MID CABIN BS696; BS704 RBL63 WL208. MARKED <[01] REMOVED CORROSION IN MULTIPLE AREAS AREAS BS695 RBL63 WL 208 BLEND WAS .080'X.070'X.003; BS696 RBL63 WL 208 WAS .009'X.007'X.003'; BS704 RBL63 WL 208 WAS 1'X.080'X.004'; BS 706 RBL63 SDR SWAA2025032495946Strap · corrodedCORROSION ON STRAP AT MID CABIN BS692 RBL62 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID PROVIDE STRUCTURE ID/DRAWING AS REQUIRED IAW 737 NDTM PART 4; 51-00-00; PROC 2 STEP 4. C.; [02] EDIT: 'DID NOT PROVIDE SDR SWAA2025012086531Mount Bracket · crackedR/H A/C BAY FWD PNEUMATIC APU BLEED AIR TO PACK VALVE DUCT MOUNT BRACKET CRACKED JUST OTBD OF KEEL BEAM BOX STRUCTURE. (SEE PIC)<[01] REMOVED AND REPLACED PER AMM 20-50-11.SDR SWAA2025012086512Bracket · crackedRIGHT MLG WHEEL WELL; FWD. BULKHEAD; ABOVE BOOST PUMP; BRACKET CRACKED<[01] REMOVED AND REPLACED RIGHT MLG WHEEL WELL FWD BULKHEAD; ABOVE BOOST PUMP BRACKET IN REF SRM 51-10-02 AND 51-40-02.SDR SWAA2025011686522Handle · looseR1 DOOR INTERIOR HANDLE LOOSE<[01] TIGHTENED R1 DOOR INTERIOR HANDLE PER AMM 52-41-11.SDR SWAA2025011686524Handle · looseR1 DOOR ASSIST HANDLE LOOSE<[01] TIGHTENED R1 DOOR ASSIST HANDLE PER AMM 52-41-31.SDR SWAA2025011686508Door · crackedLEFT MLG CENTER GEAR DOOR CRACKED AT FORWARD ATTACH POINT<[01] REMOVED LEFT MLG CENTER AND LOWER/INNER DOOR ASSEMBLY IN REF AMM 32-13-11.
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