Boeing 737-7BD
Service difficulty reports · 7,528
Newest first. 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' WHERE aircraft_model_key = '7377BD' 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 aircraft_model_key = '7377BD' 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 SWAA2025030693039Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AAF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR SWAA2025030693048Floor Panel · crackedAFT FLOOR PANEL 242XF IS CRACKED ACROSS CENTER OF PANEL.<[01] AFT FLOOR PANEL 242XF WITH CRACK ACROSS CENTER OF PANEL WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF DAMAGE.SDR SWAA2025030693056Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF PULLED STRANDS 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 SWAA2025030693053Floor Panel · pulledFWD FLOOR PANEL 221GF FWD O/B TANG IS CRACKED.<[01] FWD FLOOR PANEL 221GF O/B TANG REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025030693055Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222CF UPPER SKIN AREAS OF PULLED STRANDS WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2025030693499Shield · corrodedCORROSION AT FWD CARGO AFT SHIELD; BS 506 AND BS 514; RBL 23; WL 156.<[01] REMOVED AND REPLACED AT FWD CARGO AFT SHIELD LOCATED BETWEEN BS.492.4 - BS500A RBL.23 WL.156 IAW SRM 51-10-02 SRM 51-40-02 DWG#143A0080 REV: -;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2025030693503Sidewall Support · corrodedCORROSION AT FWD CARGO SIDEWALL SUPPORT; BS 514; BS 500C; AND BS 500D; LBL 25; WL 156<[01] UPDATED MEASUREMENT FIELD FOR P/N;[02] REMOVED AND REPLACED FCB SIDEWALL SUPPORT FROM BS 396 - BS 500D IAW SRM 51-40-02 AND DWG#143A7500 ID: 0071 REV: -;[03] VERIFIED COSDR SWAA2025030693493Floor Support · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS321 LBL46 WL208. MARKED<[01] REMOVED AND INSTALLED NEW INTERCOSTAL AT FWD WET AREA BS321 LBL46 WL208 PER REF SRM 51-40-02 AND DWG NBR 141A5400;[02] CORRECTIVE ACTION COMPLETED.SDR SWAA2025030693494Floor Support · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS394 LBL13 WL208. MARKED<[01] REMOVED AND INSTALLED NEW INTERCOSTAL AT FWD WET AREA BS394 LBL13 WL208 PER REF SRM 51-40-02 AND DWG NBR 143A5400;[02] CORRECTIVE ACTION COMPLETED.SDR SWAA2025030693495Floor Support · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS394 RBL9 WL208. MARKED<[01] REMOVED AND INSTALLED NEW INTERCOSTAL AT FWD WET AREA BS394 RBL9 WL208 PER REF SRM 51-40-02 AND DWG NBR 143A5400;[02] CORRECTIVE ACTION COMPLETED.SDR SWAA2025030693496Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS295.5 S-16L WL216.<[01] REMOVED AND REPLACED INTERCOSTAL FROM BS 294.5 TO BS 303.9 COMMON TO STR-16L IAW SRM 51-40-02-0G-0 AND DWG# 141A8180 REV:C;[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2025030693489Skin · crackedCRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 25.5' FROM FWD EDGE; .75' IN LENGTH (MARKED)<[01] REMOVED THE DAMAGED PART ON RH HORIZONTAL STABILIZER LOWER SKIN STA 193.9 25.5' FROM FWD EDGE; AND INSTALLED REPAIR PARTS IAW SRM 55-10-01-2R-11SDR SWAA2025030693486Attach Angle · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE AT AFT CABIN BS927+4 BL0 WL208. MARKED<[01] REMOVED AND REPLACED UPPER ATTACH ANGLE PN#147A5430U1 FROM BS927-BS947 AT BL0; WL208 IAW SRM 51-40-02 AND IAW DWG#147A5400 REV:-.;[02] CORRECTIVE ACTION COMPLETED.SDR SWAA2025030593487Skin · crackedCRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 25.5' FROM FWD EDGE; .3' IN LENGTH (MARKED)<[01] REMOVED THE DAMAGED PART ON LH HORIZONTAL STABILIZER LOWER SKIN STA 193.9 25.5' FROM FWD EDGE; AND INSTALLED REPAIR PARTS IAW SRM 55-10-01-2R-11;SDR SWAA2025031095377Vapor Barrier · crackedTHE L/H B.S. 663 VAPOR BARRIER HAS AN ALUMINUM FOIL PREVIOUS REPAIR LOCATED AT APPROXIMATELY LBL 55 <[01]. PREVIOUS ALUMINUM FOIL REPAIR ON L/H B.S. 663 VAPOR BARRIER LOCATED AT APPROXIMATELY LBL 55 WAS REMOVED; AND PERMANENT REPAIR WAS ACCOMPLISHED IAW SRM 5SDR SWAA2025031092940Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS847 LBL21 AND WL156 AFT CARGO COMPARTMENT 2025-110533 <[01]. REPLACED SUPPORT ZEE LOCATED BETWEEN BS727 TO BS847 LBL21 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146ASDR SWAA2025031092941Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS727D TO BS787 RBL21 AND WL156 AFT CARGO COMPARTMENT 2025-110534 CORROSION SUPPORT ZEE LOCATED BETWEEN BS727D TO BS767 RBL21 AND WL156 AFT CARGO <[01]. REPLACED SUPPORT ZEE LOCATED BETWEEN BS727D TO BS767 RBL21 AND WL156SDR SWAA2025031093189Bracket · deterioratedDETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS SIDE ENTRY AND SERVICE AT FWD GALLEY AREA 2025-110611<[01]. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS SIDE ENTRY AND SERVICE AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801. THE INSTALLATION IS DOCUMENTED ONSDR SWAA2025031093190Bracket · deterioratedDETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS SIDE ENTRY AND GALLEY AT AFT GALLEY AREA 2025-110612 <[01]. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS SIDE ENTRY AND GALLEY AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS DOCUMENTED ON TASDR SWAA2025030692615Floor Panel · pulledFLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231YF; WITH UPPER SKIN AREAS OF PULLED STRANDS; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR SWAA2025030692621Floor Panel · pulledFLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241CF UPPER SKIN HAS PULLED STRANDS REPAIRED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]SDR SWAA2025030692616Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF UPPER SKIN HAS PULLED STRAINDS REPAIRED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]SDR SWAA2025030692623Floor Panel · pulledFLOOR PANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241FF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030692619Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231ZF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030692620Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030692622Floor Panel · pulledFLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241EF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030692624Floor Panel · pulledFLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 242AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030592618Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF; WITH UPPER SKIN AREAS OF PULLED STRANDS; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR SWAA2025020492661Seat · looseSEAT ROWS ARE LOOSE IN TRACK AT SEAT ROWS 13 ABC AND 14 DEF.<[01] TIGHTENED SEAT MOUNTING HARDWARE PER AMM 25-22-00.SDR SWAA2025031092613Attach Angle · crackedCRACKED ATTACH ANGLE AT MIDCABIN; RBL 24; STA 693; WL 203 <[01]. REMOVED AND REPLACED ATTACH ANGLE AT MIDCABIN RBL 24 BS 693 WL 203 PER SRM 51-40-02 AND DWG 273A9110 REV A;[02] VERIFIED ALL STEP; CORRECTION ACTION ITEM 1 MEASUREMENT FIELD COMPLETE; CARD COMPLSDR SWAA2025031092767Web · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK BETWEEN STA. 663 TO STA. 675 LBL 30. CRACK LENGTH 0.875 IN. PASSENGER CABIN 2025-110513 <[01]. TOOL USED ON STEP 5; 6 AND 7: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 28-MAY-25; [02] SDR SWAA2025031092764Door Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.312 IN. APROX.AT PASSENGER CABIN 2025-110503<[01] REPLACED STUD FRAME LOC. ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA I.A.W B737-700 SRM 51-40-SDR SWAA2025031092771Stub Frame · crackedCRACK FRAME STUB LOCATED ON BS 294.5 AT LEVEL STR 17R AT PASSENGER CABIN 2025-110507<[01] EQUIPMENT P/N PHASEC 3D; S/N 800YBRK; DUE DATE 16-JUL-25 WAS USED ON STEP 4;[02] EQUIPMENT P/N PHASEC 3D; S/N 800YBRK; DUE DATE 16-JUL-25 WAS USED ON STEP 6;[03] REPAIREDSDR SWAA2025031092765Web · crackedCRACK WEB BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT PASSENGER CABIN 2025-110509<[01] REPLACED INTERCOSTAL WEB LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG 141A8180 SHEET 27 REV C ANSDR SWAA2025031092772Support Angle · crackedCRACK SUPPORT ANGLE ON BS 685 PLUS 6 INCHES ON BL 0 AT PASSENGER CABIN 2025-110515<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 29-JAN-26SDR SWAA2025031092766Stringer Clip · crackedCRACK TIE CLIP ON BS 277 AT STR 10R AT PASSENGER CABIN 2025-110510<[01] REPLACED TIE CLIP LOC.ON BS 277 AT STR 10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9;SRM 51-40-02 AND DWG: AND DWG 141A1110 SHEET 18 REV.-; DWG 141A8380 SHEET 21 REV.- SEE INDIVISDR SWAA2025031092350Floor Panel · crackedCRACK FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT 2025-110408 <[01]. REPLACED FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801; B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 453A2610 SHEET 20 REV E. SEE INDIVIDUAL SIGN OFF BELOW.;SDR SWAA2025031091983Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2025-110375<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B23399190; DUE DATE: 04-MAR-25.;[02] TOOL USED STEP 4: RADIOMETER/PHOTOMETER; P/N: XRP-3000; S/N: 1753759; DUE DATE: 30 JUN 25.;[03] REPAIRED SDR SWAA2025030692222Scuff Plate · crackedFSD AFT CORNER SCUFF PLATE CRACKED<[01] PROCURED SCUFF PLATE P/N 141A8431-3 LOT: 1594959-1. IAW IPC 53-13-00-13;[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2025020392096Girt Bar · looseFORWARD GALLEY DOOR GIRT BAR RETAINING BRACKET LOOSE<[01] RE-SECURE FWD GALLEY DOOR GIRT BAR BRACKET PER AMM 25-66-01.SDR SWAA2025031091880Floor Panel · crackedCRACK FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2025-110336 <[01]. REPLACED FLOOR PANEL 140CF LOCATED AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DRAWING # 453A2610 SHEET 11 REV C. SEE INDIVIDUAL SIGN-OFF BELOW.; [02] CORRECTESDR SWAA2025013090851Sign · missingL2 DOOR LOWER EMERGENCY EXIT SIGN DIRECTIONAL ARROW MISSING. <[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACTICES - PERMANENT)].SDR SWAA2025022590630Skin · crackedCRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.875 INCHES. 2025-80794 <[01]. TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 190023010; DUE DATE: 0SDR SWAA2025012789702Door · crackedDURING CENTER AND INNER GEAR DOOR INSTALLATION FOUND L/H OUTER GEAR DOOR CRACKED.<[01] C/W;[02] R&R?D L/H OUTER GEAR DOOR ADJUSTMENT CHECK GOOD PER AMM 32-13-21;[03] VERIFIED<BR>R&R?D L/H OUTER GEAR DOOR ADJUSTMENT CHECK GOOD PER AMM 32-13-21SDR SWAA2025012789563Slide Raft · dislodgedL1 DOOR RAFT FELL OUT OF DOOR (ESCAPE SLIDE)<[01] SECURED L1 DOOR SLIDE IN CONTAINER PER M/M 25-66-01 AND MT #725-SWA-105. SLIDE SECURED / INSTALLED BY EMP #141028.SDR SWAA2025012789467Bottle · low pressureAFT SERVICE DOOR SLIDE PRESSURE BELOW LIMITS<[01] REMOVED AND REPLACED AFT SERVICE DOOR SLIDE PER SWA MT 725-61-06-AS AND AMM 25-66-01.SDR SWAA2025022589281Tie Clip · crackedCRACK TIE CLIP LOCATED BS277 AND S-10R PASSENGER CABIN 2025-80691<[01]. REPLACED TIE CLIP LOCATED BS277 AND S-10R PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV -. SEE INDIVIDUAL SIGN OFF BELOW; [02] CERTIFIED AS ITEM RII. REPLACED SDR SWAA2025022589378Rib · crackedCRACK RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER 2025-80697 <[01]. REPLACED RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: DWG: 186A1001 SHEET: 19 REV - ; DWG: 186A1304 SHEET: 1 REV - SSDR SWAA2025022589377Rib · crackedCRACK LEADING EDGE RIB ACCESS PANEL 341B LOCATED LE STA 105.26 AT RT HORIZONTAL STABILIZER 2025-80698 <[01]. REPLACED RIB LOCATED ACCESS PANEL 341B LOCATED LE STA 105.26 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 186A1SDR SWAA2025022489278Web · crackedCRACK WEB LOCATED BS 294.5 TO BS 303.9 AND S-16L AT PASSENGER CABIN 2025-80693<[01] REPLACED WEB LOCATED BS 294.5 TO BS 303.9 AND S-16L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A3120 SHEET 39 REV A AND DWG 141A8180 SHEET 27 REV C.SEE INDIVIDUAL
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