N7741C
Service difficulty reports · 233
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 = 'N7741C' 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 = 'N7741C' 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 SWAA2026022473255Girt Bar · unsecureRAMP REPORTS L2 SLIDE GIRT BAR NOT STOWED. STOWED L2 DOOR SLIDE GIRT BAR IAW AMM25-66-01.SDR SWAA2025122955405Sense Line · brokenAT 30000 CABIN ALT WARNING HORN CAME ON. THE CABIN ALT REACHED 10;000 FEET. STARTED QRH PROCEDURES AND DESCENDED TO 10;000. NO PAX MASKS DROPPED. FOUND SENSE LINE FROM BLEED AIR REGULATOR ON NR 1 ENG BROKEN. REPLACED THE LINE IAW SIP. FOUND SENSE LINE FROSDR SWAA2025032408178Slide · detachedFWD ENTRY DOORESCAPE SLIDE DETACHED FROM DOOR AFTER OPENING<[01] R/R FWD ENTRY DOOR SLIDE PER MT 725-61-06-FESDR SWAA2025031003497Slide · dislodgedFWD ENTRY DOOR SLIDE FELL OUT OF BOX<[01] REPACKED SLIDE INTO BOX PER 25-66-00. NO DEFECTS NOTEDSDR SWAA2025011384827Lamp · inoperativeONE EMERGENCY LIGHT INOP BELOW AFT ENTRY DOOR<[01] RELAMPED ONE EMERGENCY LIGHT BELOW AFT ENTRY DOOR REF AMM 33-51-04. OPS CHECK GOOD.SDR SWAA2024121776126Cabin Air Sys · odorSHORTLY BEFORE DESCENT CABIN CREW REPORTED A BURN POPCORN SMELL MID CABIN. SMELL DISSIPATED AND DID NOT RETURN<[01] PERFORMED FIM 21-00 TASK 806 AND SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION PER AMM 05-51-56. NO DEFECTS NOTED.SDR SWAA2024112561272Light · inoperativeFWD SERVICE DOOR SLIDE LIGHT INOP<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF FWD SERVICE DOOR SLIDE LIGHT IAW AMM 33-51-04-960-801.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024112560649Battery Pack · failedEMERGENCY BATERY PACK M1668 FAIL TEST<[01] REMOVED AND REPLACED EMERGENCY BATERY PACK M1668 AND TESTED GOOD PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.SDR SWAA2024112553044Support · crackedMAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75.<[01] REMOVED AND REPLACED MAIN CABIN FLOOR STRUCTURE WITH NEW SUPPORT AT STA 540; BL 0 TO RBL 24.75 IAW SRM 51-40-02 AND BOEING DWG 143A0060 REV:-; AMM 20-60-07-913-801;[02] VERIFIED SDR SWAA2024112151884Floor Panel · delaminatedCABIN FLOOR PANEL 221BF TOP SURFACE IS DELAMINATED.<[01] 221BF UPPER SURFACE DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.SDR SWAA2024112551348Frame · crackedFWD SERVICE DOOR FRAME BS 294 CRACKED AT LOWER END RBL 56 WL 208.<[01] REFER TO FAULT TTG8Q00WJ92N FOR REPAIR RESOLUTION;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024112551351Frame · crackedCRACK ON BS 312 FRAME COMMON TO STR 5L LBL 33 WL 282.<[01] REMOVED CRACK ON BS 312 FRAME COMMON TO STR 5L LBL 33 WL 282 PER M-22-153-01244 ON FAULT# TTG8Q00WKNT8.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024112150854Stub Frame · crackedCRACK ON R1 DOORWAY FWD STUB FRAME IB SURFACE; BS 295 STR 17R<[01] NDT HFEC INSPECTED SURFACE PER 737 NDTM PART 6; 51-00-00; PROC 23; VERIFIED 1 INCH LONG CRACK FOUND; MARKED. <BR>EQUIP ID IS000680 DUE 07/25;[02] REMOVED DAMAGE PART OF THE R1 DOORWAY FWD STUB SDR SWAA2024112150857Skin · corrodedL/W FRONT SPAR - PITTING CORROSION ON UPPER ROLLER SURFACE AT INB MAIN SLAT TRACK #3 SLAT (MARKED)<[01] FAULT WILL BE RESOLVED ON CUSTOMER CARD:TTG8Q00WJA0T;[02] DISREGARD CORRECTIVE ACTION BLOCK 1;[03] REMOVED AND REPLACED DAMAGED I/B MAIN SLAT TRACK ON #3 SLSDR SWAA2024112550123Threshold · crackedAFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED<[01] REPAIRED AFT CARGO BAY AFT CORNER THRESHOLD PER SRM 53-60-15-2R-1;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2024112550607Support Angle · crackedRIGHT WING UPPER T/E PANEL BULB SEAL SUPPORT ANGLE IS CRACKED AT RSS 274<[01] REMOVED; REPLACED; AND INSTALLED A NEW BULB SEAL SUPPORT ANGLE AT R/W UPPER T/E PANEL AT RSS 274 IAW SRM 51-40-02 AND IPC 57-50-00-25.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024112550614Support · crackedBULB SEAL RETAINER SUPPORT IS CRACKED AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON ORSS 269. MARKED<[01] REMOVED AND REPLACED BULB SEAL RETAINER SUPPORT FITTING P/N 115A2953-1; PO # 1000542/1; IAW SRM 51-40-02-0G-0 AND DWG. 115A2930; REV. -;[02] VERIFIEDSDR SWAA2024112150125Track · crackedAFT CARGO BAY CARGO TRACK IS CRACKED AT BS767 AND BS747 RBL13 WL156<[01] REMOVED AND REPLACED AFT CARGO BAY CARGO TRACK FROM BS727+4 - BS887 RBL13 WL156 IAW SRM 51-40-02-0G-0; DWG 146A7500; DWG 147A7500 AND 146A0061. ALSO INSTALLED ALL REPAIR PARTS ON AFT CARGSDR SWAA2024112150124Shield · corrodedCORROSION FWD CARGO BAY AFT SHIELD BS500+1 TO BS500+19 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] REMOVED AND REMPLACED SHIELD BS500A? TO BS500+19? RBL22 WL156 PER SRM 51-40-02 AND DWG 143A0080; REV:-;[02] VERIFIED STEP 2 COMPLETE;[03] ALL STEPSDR SWAA2024112150126Plate · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] LINE ITEM 2 ON PART REQUIREMENTS FOR P/N 146A7502-27 WAS BAD FROM STOCK AND NOT ISSUED TO N7741C FOR USE; THAT PART WAS RETURNED SDR SWAA2024112150127Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED AND REPLACED FWD SHIELD BETWEEN BS767 TO BS787 RBL 22 WL 156 ACB PER SRM 51-40-02 AND BOEING DWG 146A0081.;[02] ADDED REV LEVEL TO DWG; SSDR SWAA2024112150128Support · 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 SUPPORT WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED SUPPORT AS PER SRM 51-40-02-0G-0; DWG 146A7500 REV: ASDR SWAA2024112550083Attach Angle · crackedATTACH ANGLE CRACKED BS 294 FWD SIDE OF STUB FRAME RBL 54 WL 208.<[01] REMOVED DAMAGE CLIP I.A.W SRM 51-10-02-0G-0 AND SRM 51-40-02-0G-0; FABRICATION AND INSTALLATION TO BE ACCOMPLISHED ON CCN TTG8Q00WJ92N DUE TO CRACK ON STUB FRAME;[02] VERIFIED CORRECTIVE ACSDR SWAA2024112550108Strap · corrodedCORROSION ON L/H REINFORCEMENT STRAP BS 1017-1020 LBL 27 WL 208.<[01] REMOVED LH REINFORCEMENT STRAP AND INSTALLED NEW LH REINFORCEMENT STRAP BS1006-1020 LBL27 WL208 IAW SRM 51-40-02-0G-0. APPLIED PRIMER TO LH REINFORCEMENT STRAP REPLACEMENT BS1017-1020 LBL 27SDR SWAA2024112550109Strap · corrodedCORROSION ON L/H REINFORCEMENT STRAP BS 1017 LBL 19 WL 208.<[01] REMOVED LH REINFORCEMENT STRAP AND REPLACED WITH NEW LH REINFORCEMENT STRAP BS1006-1025 LBL19 WL208 IAW SRM 51-40-02-0G-0. APPLIED PRIMER TO LH REINFORCEMENT STRAP REPLACEMENT BS1017-1020 LBL 19 SDR SWAA2024112549565Former · crackedR/H FAIRING FORMER BS 500D BETWEEN STRINGER 18 R/H AND 19 R/H IS CRACKED<[01] EVALUATED CRACK ON FAIRING FORMER AT BS 500D BETWEEN STRINGER 18R/H AND 19R/H FOUND TO BE OUT OF LIMITS THEREFORE FAIRING FORMER WILL BE REPAIRED BY REPLACEMENT OF PART PER 53-30-71-SDR SWAA2024112550098Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS685 S-3L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 685 S-3L PER SRM 51-40-02-0G-0 AND BOEING DWG 144A1106 REV. A.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550099Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS706 S-2L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 706 S-2L PER SRM 51-40-02-0G-0 AND BOEING DWG 144A1107 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550093Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-5R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-5R PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550094Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727A S-3R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727A S-3R PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1101 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550095Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727B S-6L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727B S-6L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1102 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550100Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727C S-6L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727C S-6L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1103 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550096Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-4L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-4L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550097Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-5L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-5L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550101Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-6L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727C S-6L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550102Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-7L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-7L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550103Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS767 S-6L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 767 S-6L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1132 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550104Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS767 S-5L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP FROM BS 767 S-5L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1132 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112549904Seat Track · corrodedCORROSION ON PAX CABIN SEAT TRACK LBL25 BS500B+12 WL208. MARKED<[01] REMOVED CORROSION ON SEAT TRACK LBL25 BS500B+12 AND APPLIED CHEMICAL CONVERSION AND PRIMER ON BLENDED AREAS IAW AMM 51-21-41-370-801 AND AMM 51-21-72-370-804;[02] VERIFIED TASK COMPLETESDR SWAA2024112150107Floorbeam · corrodedCORROSION AROUND FASTENER HOLE BS 986 FLOOR BEAM RBL 45 WL 208. CORROSION AROUND FASTENER HOLE PREVIOUS REPAIR BS 986 FLOOR BEAM RBL 45 WL 208<[01] REMOVED AND REPLACED BS986 LBL50-RBL50 WL206-WL208 UPPER T-CHORD REPAIR PARTS PER 737-700 SRM 51-40-02-0G-0 AS SSDR SWAA2024112150092Floorbeam · crackedBS 294 FLOOR BEAM IS CRACKED ON UPPER FLANGE RBL 52 WL 208.<[01] REMOVED DAMAGE PART OF THE FLOOR BEAM BS294 RBL24-RBL60 WL208 AND REPAIRED I.A.W SRM 53-10-51-2R-16 REPAIR 16 TASK COMPLETED;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024112149568Floor Panel · crackedCABIN FLOOR PANEL 221GF FWD O/B CORNER TANG IS CRACKED.<[01] CABIN FLOOR PANEL 221GF FWD O/B CORNER TANG WITH CRACK 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 ITEM 1SDR SWAA2024112150081Floor Panel · delaminatedCABIN FLOOR PANEL 232AF TOP SURFACE 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] JOB COMPLETE.SDR SWAA2024112549551Floor Panel · delaminatedCABIN FLOOR PANEL 242VF CORRODED INSERTS AND TOP SURFACE DELAMINATION.<[01] CABIN FLOOR PANEL 242VF WITH TOP SURFACE DELAMINATION WAS REPAIRED AND CORRODED INSERTS WERE REPLACED IAW SRM 53-00-50-2R-1AND DWG 147A5810 ID:0350; DWG D1040M003-309.;[02] JOB COMPLETSDR SWAA2024112549553Floor Panel · delaminatedCABIN FLOOR PANEL 241ACF HAS CORRODED INSERTS AND TOP SURFACE DELAMINATION.<[01] TOP SURFACE DAMAGE WAS REPAIRED AND DAMAGED INSERTS WERE REMOVED AND REPLACED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024112549378Rib · crackedFOUND CRACK ON R/H HORIZONTAL STAB LEADING EDGE RIB AT L/E STA 95.96<[01] REMOVED AND REPLACED R/H HORIZONTAL STAB LEADING EDGE RIB AT L/E STA 95.96<BR>I.A.W SRM 51-40-02-0G-0 AND DWG 186A1001;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112149549Floor Panel · delaminatedCABIN FLOOR PANEL 241ZF HAS TOP SURFACE DELAMINATION.<[01] TOP SURFACE DELAMINATION ON CABIN FLOOR PANEL 241ZF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024112149548Floor Panel · delaminatedCABIN FLOOR PANEL 241XF HAS TOP SURFACE DELAMINATION.<[01] 241XF FLOOR PANEL UPPER SURFACE DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEETS SDR SWAA2024112149367Floor Panel · delaminatedCABIN FLOOR PANEL 222CF HAS TOP SURFACE DELAMINATION.<[01] CABIN FLOOR PANEL 222CF WITH TOP SURFACE DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024112149362Floor Panel · delaminatedCABIN FLOOR PANEL 221BF CORRODED INSERTS; BROKEN TAB AND TOP SURFACE DELAMINATION.<[01] 221BF FLOOR PANEL DAMAGED AREAS HAVE BEEN REPAIRED PER [SRM 53-00-50-2R-6-A00944 (REPAIR 6 - REPAIR OF DAMAGE LESS THAN 10 SQUARE INCHES IN AREA TO TWO FACESHEETS AND THE C
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