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 SWAA2024042566105Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS907 PLUS 11 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT 2024-206504<[01] REPLACED ANGLE - SUPPORT LOCATED BS907 PLUS 11 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMEN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 147SDR SWAA2024042566106Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS867 AND BTW STR26L TO STR27L AFT CARGO COMPARTMENT 2024-206505<[01] REPLACED ANGLE - SUPPORT LOCATED BS867 AND BTW STR26L TO STR27L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 149A8102; SHEET 17;SDR SWAA2024042566509Support Angle · crackedCRACK ANGLE SUPPORT TRAILING EDGE LOCATED ORSS273 LT WING. REPLACED ANGLE SUPPORT TRAILING EDGE LOCATED ORSS273 LT WING IAW B737-700 SRM 51-10-02 ITEM 9.SDR SWAA2024042466107Cargo Track · crackedCRACK ON TRACK RBL 13.84 LOCATED BS767 AFT CARGO COMPARTMENT 2024-206506<[01] PERFORMED PERMANENT REPAIR ON CARGO TRACK RBL 13.84 LOCATED BTW BS 727E TO BS 787 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[0SDR SWAA2024041866328Hinge Fitting · corrodedFWD ENTRY DOOR CUTOUT LOWER HINGE SUPPORT FITTING HAS CORROSION AROUND BOLT HOLE.<[01] REMOVED AND REPLACED FWD ENTRY LOWER HINGE BOX FITTINGS AS PER B737-700 SRM 51-40-02-0G-0 AND BOEING DWG 141A8180 SHEET 27; 30; 31 AND 32.;[02] VERIFIED STEP 1.SDR SWAA2024041866027Support · corrodedCORROSION FOUND ON L/W T/E PANEL 561BB SUPPORT STRUCTURE AROUND FASTENER HOLES.<[01] REMOVED AND REPLACED ATTACHMENT SUPPORT STRUCTURE BEAM L/W FOR PANEL 561BB; REF SRM 51-40-02-0G-0 AND DWG# 115A3758;[02] VERIFIED STEP 1.SDR SWAA2024042565596Floorbeam · corrodedCORROSION FLOOR BEAM LOCATED BS 294.5; RBL 28; WL 208.1 AT PASSENGER CABIN 2024-206368<[01] TOOL USED ON STEP 3. UT EQUIPMENT P/N: 45MG; S/N: 130061901; CAL DUE DATE: 09-JUN-24;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DASDR SWAA2024042465603Support · crackedCRACK SUPPORT -ZEE LOCATED STA 500A AND STR 26L AT FWD CARGO COMPARTMENT 2024-206391<[01] REPLACED SUPPORT-ZEE LOCATED STA 400 TO STA 500D S26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 147A7500 SHEET: 58; REV:- . REPAIR STEPS WAS DOCUSDR SWAA2024042465601Web · crackedCRACK WEB - INTERCOSTAL LOCATED BTW STA 500 TO STA 500A AT LEVEL STR 26L FWD CARGO COMPARTMENT 2024-206375<[01] REPLACED WEB - INTERCOSTAL LOCATED BTW STA 500 TO STA 500A AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 ANDSDR SWAA2024042465602Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BTW STA 440 TO STA 460 AND STR 26L FWD CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL LOCATED BTW STA 440 TO STA 460 AND STR 26L FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505, SHEET 82, REV -.SDR SWAA2024042565226Floorbeam · corrodedCORROSION ON FLOOR BEAM LOCATED BS986.5 AT LEVEL RBL44 AND WL208.1 AT AFT GALLEY AREA 2024-206339<[01] EDDY CURRENT EQUIPMENT USED P/N : NORTE 600D ; S/N : 210138103 AND DUE DATE : 02- MAY-24 .;[02] ULTRASONIC EQUIPMENT USED P/N : 45MG ; S/N : 130066401 AND DUSDR SWAA2024042465229Web · crackedCRACK WEB LOCATED BS294.5 TO BS303.9 AT LEVEL STR16L AT PASSENGER CABIN 2024-206345<[01] REPLACED WEB LOCATED BS294.5 TO BS303.9 AT LEVEL STR16L AT PASSENGER CABIN IAW B737-700 SRM SRM 51-40-02; SRM B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8180 SHEET 27 REV - SDR SWAA2024042465222Not Reported · crackedCRACK INNER CHORD LOCATED BS 294.5 PLUS 8 INCHES; LBL 55 AT FWD GALLEY AREA 2024-206333<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A20231600 DUE DATE: 03-OCT-24.;[02] REPLACED INNER CHORD AND FASTENERS LOCATED BS 270 TO BS 360 AND S-17L AT FWD GALLEY SDR SWAA2024042365221Web · crackedCRACK FLOOR STRUCTURE WEB LOCATED BETWEEN BS 312 AND BS 328; RBL 30.5 AT FWD GALLEY AREA 2024-206332<[01] REPLACED WEB LOCATED BETWEEN BS 312 AND BS 328; RBL 30.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG:141A5400; SHEET: 39; REV:-;[02] REPLASDR SWAA2024041965228Frame · crackedCRACK FRAME LOCATED BS 312 AT LEVEL STR 5L TO 6L AT PASSENGER CABIN. REPAIRED FRAME LOCATED BS312 AT LEVEL STR5L TO STR6L AT PASSENGER CABIN IAW EA#M-22-153-01244.SDR SWAA2024041965223Tie Clip · crackedCRACK TIE CLIP LOCATED BS277 AT LEVEL STR10R AT PASSENGER CABIN 2024-206334<[01] REPLACED TIE CLIP LOCATED BS277 AT LEVEL STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND 51-10-02 PARAGRAPH 9. DWG 141A1110 SHEET: 18 REV: -;[02] STEP 1 CORRECTED:<BR>REPLSDR SWAA2024041865125Seal · crackedLEFT HORIZONTAL STABILIZER TO FUSELAGE UPPER FWD SLIDING METAL SEAL IS CRACKED.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER TO FUSELAGE UPPER FWD SLIDING SEAL AS PER B737-700 AMM 53-31-31-000-802 AND AMM 53-31-31-400-802.;[02] CERTIFIED WORK STEPS ACCSDR SWAA2024041865017Floor Panel · deformedFLIGHT DECK FLOOR PANEL#211AF IS DEFORMED.<[01] REPLACED FLIGHT DECK FLOOR PANEL #211AF AS PER REF 51-40-02-0G-0. INSTALLATION TO BE ACCOMPLISHED ON FAULT TTG8Q00RQGC6.;[02] VERIFIED STEP 1SDR SWAA2024031864954Connector · inoperativeL EMER EXIT DOOR FLOOR PROX SIGN L1189 INOP<[01] T/S AND FOUND CONNECTORS SWAPPED WITH CONNECTORS FOR L EMER EXIT DOOR HEATER. SWAPPED CONNECTORS TO CORRECT POSITIONS AND OPS CHECK GOOD IAW AMM 33-51-00.SDR SWAA2024041974173Plate · damagedAFTER INSPECTED L/H WING DEFLECTION RIB FOUND SERRATED PLATE WITH ELONGATED HOLE AND HARDWARE WORN (PREVIOUS REPAIR)<[01] REMOVED AND REPLACED LEFT WING DEFLECTION RIB SERRATED PLATE AND CHECKED ADJUSTMENT OF I/B FIXED TRAILING EDGE UPPER PANEL; REF: B737 SRM SDR SWAA2024041964818Fitting · crackedRIGHT WING REAR SPAR DEFLECTOR CONTROL RIB FIXED PANEL VERTICAL SEAL FITTING CRACKED MKD DOT<[01] REMOVED AND REPLACED SEAL FITTING AND SEAL AT RT WING REAR SPAR DEFLECTION CONTROL RIB AREA AS PER B737-700 SRM 51-40-02-0G-0 PARAGRAPH 4.;[02] VERIFIED STEP 1SDR SWAA2024041964703Seat Track · corrodedCORROSION *** MAIN CABIN CENTER SECTION FLOOR R/H O/B SEAT TRACK I/B FLANGE RBL 45 STA 639+20' MKD DOT<[01] ACCOMPLISHED EA 24-153-00729. REF TASK CARDS TTG8Q00SAKBB ; TTG8Q00SDS5N ; TTG8Q00SAKBB;[02] CORRECTION TO STEP 1 SHOULD READ: ACCOMPLISHED EA 24-153-00SDR SWAA2024041864696Fitting · corrodedCORROSION ** FWD CABIN FWD ENTRY L-1 DOOR CUTOUT AFT SAFETY STRAP FITTING CORR. MKD DOT<[01] REMOVED AND REPLACED L-1 DOOR CUTOUT AFT SAFETY STRAP FITTING IAW B737-700 AMM 25-61-13-000-801 AND AMM 25-61-13-400-801.;[02] VERIFIED OF DOOR SAFETY STRAP INSTALLATISDR SWAA2024041864700Floorbeam · crackedMAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED @ RBL 1 STA 540 MKD DOT<[01] REMOVED AND REPLACED BREAK PANEL ASSY AT MAIN CABIN CENTER SECTION; RBL 1 STA 540ER B 737-700 SRM 51-40-02-0G-0;[02] REMOVED AND REPLACED BREAK PANEL ASSY AT MAIN CABIN CENTER SSDR SWAA2024041864698Floorbeam · delaminatedMAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK TOP LAYER DELAMINATED BETWEEN RBL 45.5 AND RBL 64 STA 540 MKD DOT<[01] REMOVED AND REPLACED FLOOR SUPPORT BREAK ;TOP LAYER AT MAIN CABIN RBL 45.35 AND RBL 64; STA 540; PER B 737-700-SRM 51-40-02-0G-0.;[02] VERIFIEDSDR SWAA2024041864821Attach Bracket · crackedLEFT WING REAR SPAR DEFLECTOR CONTROL RIB HORIZONTAL BULB RETAINER O/B ATTACHED BRACKET CRACKED MKD DOT<[01] REMOVED AND REPLACED HORIZONTAL RETAINER TO DEFLECTION CONTROL RIB O/B ATTACHMENT BRACKET AT LT WING AS PER B737-700 SRM 51-40-02-0G-0.;[02] CERTIFIED SDR SWAA2024042464448Floor Panel · damagedELONGATED HOLE FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT 2024-206192<[01] REPLACED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-05; SRM 51-40-08 AND DWG 453A2610 SHEET 22 REV B;[02] REPLACED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW SDR SWAA2024042464551Pressure Deck · crackedCRACK INDICATION FOUND IN HORIZONTAL PRESSURE DECK WEB LOCATED AT BS 663 AND LBL 32. CRACK LENGTH IS L= 0.350 INCHES. REPAIRED HORIZONTAL PRESSURE DECK WEB LOC BS 663 AND BTW LBL 25 TO LBL 60 IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2.SDR SWAA2024042464547Fitting · deterioratedDETERIORATE GIRT BAR FITTING PLATE (4EA) AND SHIM (4EA) ON POSITION SERVICE DOOR AND ENTRY DOOR AT AFT GALLEY AREA 2024-206212<[01] REPLACED GIRT BAR FITTING PLATE (4EA) AND SHIM (4EA) ON POSITION SERVICE DOOR AND ENTRY DOOR AT AFT GALLEY AREA IAW SOPM 20-50-0SDR SWAA2024041964438Floor Panel · damagedELONGATED HOLE FLOOR PANEL 140DF AT AFT CARGO COMPARTMENT 2024-206193<[01] FABRICATED FLOOR PANEL 140DF AT AFT CARGO COMPARTMENT IAW AMM 25-52-01-201-801 SEE INDIVITUAL SIGN OFF BELOW;[02] COMPLETE TASK CERTIFIEDSDR SWAA2024041964548Light · brokenBROKEN EMERGENCY LIGHT ASSY ON LOWERED CEILING PANEL AT AFT GALLEY AREA (1EA) 2024-206213<[01] REPLACED EMERGENCY LIGHT ASSY ON LOWERED CEILING PANEL AT AFT GALLEY AREA (1EA) IAW B737-700 AMM 33-51-01-960-802 TEST IS OK;[02] CERTIFIED WORK PERFORMEDSDR SWAA2024031964415Slide · dislodgedFAULT RAISED TO ADD MX TASK MT 725-61-06 FOR PREVIOUSLY WORKED FAULT' L1 DOOR SLIDE DISLODGED'; REF TTQ8Q00S5R6W (LP 2721617)<[01] CW MT 725-61-06SDR SWAA2024041964200Scuff Plate · crackedCRACK SCUFF PLATE FWD CORNER AT FWD CARGO COMPARTMENT 2024-206148<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30; S/N: A23329368; DUE DATE: 06/MAR/25.;[02] TOOL USED: RADIOMETER PHOTOMETER. P/N: XRP-3000. S/N: 1753759. DUE DATE: 12-APR-24.;[03] REPAIRED THE FWDSDR SWAA2024041863556Channel · corrodedCORROSION FOUND AFT CARGO RH 'Z' CHANNEL FROM STA 727B TO STA 727C RBL 21 WL 155.5 HAS SPOT OF CORROSION.<[01] REMOVED AND REPLACED R/H Z-CHANNEL AT AFT CARGO COMPT FROM STA 727 TO STA 767 RBL 21 PER REF SRM 51-40-02-0G-0 AND DWG #146A7500;[02] VERIFIED 1.SDR SWAA2024041863550Channel · corrodedCORROSION FOUND AFT CARGO RH 'Z' CHANNEL FROM STA 727D TO STA 727E RBL 21 WL 155.5 HAS SPOTS OF CORROSION.<[01] R/H Z-CHANNEL WAS REMOVED AND REPLACED ON TASK CARD TTG8Q00S52GA.;[02] VERIFIED 1.SDR SWAA2024041863557Channel · corrodedCORROSION FOUND AFT CARGO RH 'Z' CHANNEL FROM STA 727E TO STA 747 RBL 21 WL 155.5 HAS SPOTS OF CORROSION.<[01] R/H Z-CHANNEL WAS REMOVED AND REPLACED ON TASK CARD TTG8Q00S52GA.;[02] VERIFIED 1.SDR SWAA2024041863558Channel · corrodedCORROSION FOUND AFT CARGO RH 'Z' CHANNEL FROM STA 747 TO STA 767 RBL 21 WL 155.5 HAS SPOTS OF CORROSION.<[01] R/H Z-CHANNEL WAS REMOVED AND REPLACED ON TASK CARD TTG8Q00S52GA.;[02] VERIFIED 1.SDR SWAA2024041864013Support Angle · corrodedCORROSION ** AFT OF AFT CARGO COMPARTMENT R/H LOWER SIDEWALL SUPPORT ANGLE LOWER END UNDER AROUND DOME NUT PLATE MKD DOT<[01] REMOVED AND REPLACED LWR FLOOR SUPPORT ANGLE AT AFT CARGO COMPT STA 947 PER REF SRM 51-40-02-0G-0 AND DWG #149A8117;[02] VERIFIED STEPSDR SWAA2024041864146Support · corroded**CORROSION** FWD CARGO AFT BULKHEAD R/H LOWER SUPPORT HAS CORROSION AT UPPER SURFACE I/B END MKD (107-002)<[01] REMOVE CORROSION AT FWD CARGO AFT BULKHEAD R/H LOWER SUPPORT PER REF SRM 51-10-02-0G-0; EVALUATED REWORKED AREA; ORIGINAL MAT:0.071'; MAT LOSS:0.00SDR SWAA2024041864148Support Plate · corroded**CORROSSION** FWD CARGO R/H SIDE PLATE SUPPORT UPPER SURFACE BETWEEN STA 480+12' AND 500A HAS CORROSION AROUND FASTENER HOLES MKD (107-004)<[01] REMOVED AND REPLACED NEW PLATE (SHIELD) AT FWD CARGO R/H SIDE FROM STA 480+12' TO STA 500A PER REF SRM 51-40-02-0GSDR SWAA2024031864410Slide · dislodgedCREW REPORTS L1 SLIDE DISLODGED<[01] RESECURED L1 DOOR SLIDE PER AMM 25-66-01 AND MT 725-61-06;[02] UPDATING CORRECTIVE ACTION ONLY AS PER TELECOM REQUEST TO ADD FAULT REF FOR ADDED MT 725-61-06 PERFORMED ON TTG8Q00S5REE BY E90554SDR SWAA2024042463466Nut · deterioratedDETERIORATE NUT OF HANDLE ON ENTRY DOORWAY LINING AT FWD GALLEY AREA (2EA) 2024-206070<[01] REPLACED NUT OF HANDLE ON ENTRY DOORWAY LINING AT FWD GALLEY AREA (2EA) IAW SOPM 20-50-01;[02] REPLACED NUT OF HANDLE ON ENTRY DOORWAY LINING AT FWD GALLEY AREA (2EA) ISDR SWAA2024041863396Balance Weight · corrodedRUDDER FRONT SPAR WEIGHT BALANCE PANEL- CORROSION<[01] REMOVED AND REPLACED RUDDER BALANCE WEIGHT; REF CMM 55-40-09 AND AMM 20-50-11-910-801.;[02] RII--VERIFIED STEP 1.SDR SWAA2024041862882Bonding Jumper · corrodedTOILET SERVICE DOOR HAS PITTING CORROSION AROUND BONDING JUMPER ATTACHMENT HOLE<[01] CORROSION FOUND TO BE OUT OF LIMITS. PASSED 100% THROUGH MATERIAL; PER SRM 52-40-01-1A-4. REMOVED AND INSTALLED NEW TOILET SERVICE DOOR ASSY. AS PER REF AMM 59-49-07-400-801.;SDR SWAA2024041862386Skin · crackedCRACK FOUND AT LH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90; 16.25' FROM FRONT SPAR; I/B ROW. CRACK LENGTH:0.5' CRACK FOUND AT LH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 16.25' FROM FRONT SPAR I/B ROW. CRACK LENGTH:0.5'<[01] COMPLETED SMESDR SWAA2024041862388Floor Panel · delaminatedFLOOR PANEL 232SF HAS ONE INTERNAL DELAMINATION.<[01] REPLACED FLOOR PANEL 232SF. REF. B737-700 AMM 53-21-00-400-801. INSTALLATION WILL BE ACCOMPLISHED ON FAULT #TTG8Q00RQFYW;[02] VERIFIED REPLACEMENT AND TTG8Q00RQFYW FOR CLOSING.SDR SWAA2024041862385Floor Panel · delaminatedFLOOR PANEL 242DF HAS DELAMINATION AT INBOARD CORNER.<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #242DF AS PER B737 SRM 53-00-50-2R-4 PARAG 3-K; MATERIAL USED: PO#1608196 AND PO#2040692.;[02] RII--VERIFIED STEP 1.SDR SWAA2024041862389Floor Panel · peelingFLOOR PANEL 231ZF HAS LOST ONE LAYER OF COMPOSITE MATERIAL ALONG FLOOR PANEL.<[01] REPLACED FLOOR PANEL 231ZF. REF. B737-700 AMM 53-21-00-400-801. INSTALLATION WILL BE ACCOMPLISHED ON FAULT #TTG8Q00RQFZ0;[02] VERIFIED REPLACEMENT AND TTG8Q00RQFZ0 FOR CLOSING.SDR SWAA2024041962380Bullnose · crackedR/W #3 L/E KRUEGER FLAP BULLNOSE O/B HINGE CRACKED.<[01] REMOVED AND REPLACED R/W #3 L/E KRUEGER FLAP BULLNOSE IN REFERENCE CMM 57-56-44.;[02] RII -- VERIFIED R/W #3 L/E KRUEGER FLAP BULLNOSE REPLACEMENT.SDR SWAA2024041961879Skin · damaged# 7 SLAT LOWER SURFACE OF LEADING EDGE SLAT NOSE SKIN ACTUATOR HAS FOUR FASTENERS PULLED OUT/IN.<[01] ACCOMPLISHED LOWER SKIN REPAIR AT SLAT #7 L/E; REF SRM 57-42-01-2R-8;[02] VERIFIED STEP 1
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