Boeing 737-71B
Service difficulty reports · 756
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 = '73771B' 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 = '73771B' 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 SWAA2024100238674Tee Fitting · corrodedCORROSION ON ACB TEE ASSY STA 772; LBL 21-RBL 21; WL 156.<[01] UPDATED TABLE;[02] ENTERED STEPS 2-3 IN ERROR.;[03] INCORRECT LABOR ROW WAS SELECTED.;[04] REPLACED TO NEW PART AND APPLIED PAINT AND TWO COAT CIC ON ACB TEE ASSY STA 772; LBL 21-RBL 21; WL 156 IAWSDR SWAA2024102338079Scuff Plate · crackedCRACK ON FWD CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT 2024-572857<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: A23046084; DUE DATE 23-MAY-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1753759 ; DUE DATE : 07/DEC/24;[03] REPAIRED FSDR SWAA2024102338334Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-572867<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN I.A.W DWG 146A7901 SHEET: 66 REV: A AND B737-700 SRM 51-40-02-0G-0; B737-700 SRM 51SDR SWAA2024102338332Angle · crackedCRACK ON ANGLE OF ACCESS PANEL 551FB AT LT WING 2024-572864<[01] REPLACED ANGLE OF ACCESS PANEL 551FB AT LT WING IAW B737-700 SRM 51-40-02 AND DRAWING 115A2710 SHEET 8 REV A MEASURE OF CRACK IS L=1.500' TOOL USED CALIPER P/N: 500-196-30 S/N: A23325478 DUE DATESDR SWAA2024102338078Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 295 AT RT WING 2024-572854<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 295 AT RT WING I.A.W DWG 115A3712 SHEET: 7 REV: A ; DWG 115A3700 SHEET: 41 REV: - AND B737-700 SRM 51-10-02SDR SWAA2024102338077Web · crackedCRACK ON WEB LOCATED AT LEVEL ORSS 270 DEFLECTION CONTROL RIB AREA AT RT WING 2024-572852<[01] REPLACED WEB LOCATED AT LEVEL ORSS 270 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0; 51-102G-0 ITEM 9 AND DWG 115A2512 SHEET 14 REV A SEE INSDR SWAA2024102337956Frame Splice · corrodedCORROSION FRAME STA 500A AND BTW S-25R TO S-26R AND WL 154.0 AT FWD CARGO COMPARTMENT 2024-572841 CORROSION ON SPLICE STA 500A AND BTW S-25R TO S-26R AND WL 154.0 AT FWD CARGO COMPARTMENT.<[01] REPLACED SPLICE AND FASTENERS LOC. FRAME STA 500A AND BTW S-25R TOSDR SWAA2024102337845Seat Track · crackedCRACK ON CAPTAIN AND F/O SEAT TRACK INBOARD SIDE AT CONTROL CABIN (2EA) 2024-572805<[01] REPLACED ON CAPTAIN AND F/O SEAT TRACK INBOARD SIDE AT CONTROL CABIN (2EA) IAW B737-700 AMM 25-11-11-400-801.;[02] CERTIFIED WORK PERFORMEDSDR SWAA2024102348913Battery Pack · inoperativeINOP BATTERY PACK LOCATED BTW BS 500C AND 500D S-16 AND S-17 LH SIDE ON PASSENGER CABIN 2024-572766<[01] REPLACED BATTERY PACK LOCATED BTW BS 500C AND 500D S-16 AND S-17 LH SIDE ON PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805.<BR><BR>TEST IS OK.;[02] REPLSDR SWAA2024102348911Battery Pack · inoperativeINOP BATTERY PACK LOCATED BTW BS 597 UP TO BS 616 AND S-16 TO S-17 RH SIDE ON PASSENGER CABIN 2024-572769<[01] REPLACED BATTERY PACK LOCATED BTW BS 597 UP TO BS 616 AND S-16 TO S-17 RH SIDE ON PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805.<BR><BR>TEST IS OSDR SWAA2024102348912Battery Pack · inoperativeINOP BATTERY PACK LOCATED BTW BS 727C UP TO BS 727D S-16 TO S17 LH SIDE ON PASSENGER CABIN 2024-572770<[01] REPLACED BATTERY PACK LOCATED BTW BS 727C UP TO BS 727D S-16 TO S17 LH SIDE ON PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805.<BR><BR>TEST IS OK.;[02SDR SWAA2024102337559Skin · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. 2024-572755<[01] TOOL USED ON STEP 7 AND 8 ET EQUIPMENT: P/N: NORTEC 600D; SDR SWAA2024102337747Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 216 AT RT WING 2024-572793<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 216 AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEMP 9.;[02] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS SDR SWAA2024102337746Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATE ORSS 270 INTERNAL CAVITY TRAILING EDGE AT LT WING 2024-572791<[01] REPLACED SUPPORT ANGLE LOCATE ORSS 270 INTERNAL CAVITY TRAILING EDGE AT LT WING IAW B737-700 SRM 51-10-02. ITEM 9 ; SRM 51-40-02 <BR>MEASURE OF CRACK : L= 0.900. TSDR SWAA2024102337742Access Panel · damagedELONGATE HOLES ON ACCESS PANEL 561BB AT LEFT WING 2024-572792<[01] TOOL USED : CALIPER P/N:500-197-30 S/N:A21042057 DUE DATE: 17-APR-25.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196126 DUE DATE: 03-APR-25;[03] STEP 12 TOOL USED ULTRASONIC FLAW DETECTSDR SWAA2024102337743Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED AT LEVEL ORSS 269 DEFLECTION CONTROL RIB AREA TRAILING EDGE AT RT WING 2024-572785<[01] REPLACED SUPPORT BRACKET LOCATED AT LEVEL ORSS 269 DEFLECTION CONTROL RIB AREA TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 5SDR SWAA2024102337744Retainer · corrodedCORROSION ON NUTPLATE RETAINER INTERNAL CAVITY LEADING EDGE LOCATED ORSS 449 AT LT WING 2024-572786<[01] REPLACED NUTPLATE RETAINER ( GANG CHANNEL) INTERNAL CAVITY LEADING EDGE LOCATED ORSS 449 AT LT AND PERFORMED GENERAL VISUAL INSPECTION ON ADJACENT AREA ANDSDR SWAA2024102337745Retainer · corrodedCORROSION ON NUTPLATE RETAINER INTERNAL CAVITY LEADING EDGE LOCATED ORSS 570 AT LT WING 2024-572787<[01] REPLACED NUTPLATE RETAINER ( GANG CHANNEL) INTERNAL CAVITY LEADING EDGE LOCATED ORSS 570 AT LT AND PERFORMED GENERAL VISUAL INSPECTION ON ADJACENT AREA ANDSDR SWAA2024102337551Intercostal · crackedCRACK INTERCOSTAL WEB LOCATED BETWEEN STA 294.5 AND STA 303.9 AND S-15L AT FWD PASSENGER COMPARTMENT 2024-572737<[01] REPLACED INTERCOSTAL WEB LOCATED BETWEEN STA 294.5 AND STA 303.9 AND S-15L AT FWD PASSENGER COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-0SDR SWAA2024102337535Floor Support · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 AT FWD GALLEY AREA 2024-572718<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 ANSDR SWAA2024102337529Floorbeam · corrodedCORROSION FLOOR STRUCTURE BEAM BS 986.5 BETWEEN RBL 29 TO RBL 43 AT AFT GALLEY AREA 2024-572703 CORROSION FLOOR STRUCTURE BEAM BS 986.5 BETWEEN RBL 40 TO RBL 43 APPROX. AT AFT GALLEY AREA<[01] EQUIPMENT P/N 45MG; S/N 221861811; DUE DATE 30-NOV-24 WAS USED ON SSDR SWAA2024102337536Floor Support · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 344 TO BS 360 AND LBL 12 AT FWD GALLEY AREA 2024-572719<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 344 TO BS 360 AND LBL 12 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH SDR SWAA2024102337547Floor Support · corrodedCORROSION FLOOR STRUCTURE INNER CHORD AT RBL 50 AND BTW STA 947.5 AND STA 986.6 AND WL 210 AFT GALLEY AREA. 2024-572733<[01] TOOL USED STEP 5: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 221859911; DUE DATE: 17 NOV 24.;[02] EVALUATED CORROSION FLOOR STRUCTURE ISDR SWAA2024102337549Frame · crackedCRACK FRAME BS 312 LOCATED BETWEEN STRINGER 5L TO STRINGER 6L AT PASSENGER CABIN 2024-572738<[01] PERFORMED TRIM OUT ON FRAME BS 312 LOCATED BETWEEN STRINGER 5L TO STRINGER 6L AT PASSENGER CABIN I.A.W EA M-22-153-01244. SEE INDIVIDUAL SIGN OFF BELOW.;[02] PERFSDR SWAA2024102337550Tie Clip · crackedCRACK TIE CLIP LOCATED AT STA 277 AND S-10R AT PASSENGER CABIN 2024-572739<[01] REPLACED TIE CLIP LOCATED AT STA 277 AND S-10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DRAWING 141A1110 SHEET: 18 REV: - ; DRASDR SWAA2024102337543Slat Track · crackedCRACK SLAT 2 I/B AUXILIARY TRACK I/B SUPPORT ANGLE AT LT WING 2024-572734<[01] REPLACED SUPPORT ANGLE LOCATED SLAT 2 I/B AUXILIARY TRACK I/B AT LT WING IAW B737-700 SRM 51-40-02-0G-0 AND MEASURES OF CRACK IS:2.000 INCHES TOOL USED: CALIPER P/N: 500-196-30 S/N:SDR SWAA2024102237532Floor Support · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 344 TO BS 360 AND BL 0 AT FWD GALLEY AREA 2024-572721<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 344 TO BS 360 AND BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWGSDR SWAA2024100236984Scuff Plate · crackedAFT CARGO BAY; AFT CORNER SCUFFPLATE IS CRACKED.<[01] WELD THE CORNER SCUFF PLATE USING ER4043 FILLER ROD PER SRM 53-60-15-2R-1 PARA 4.B.(4) REFER TO BAC5975<BR>PT INSPECTED AREA IAW SOPM 20-20-02.<BR>NO CRACKS NOTED<BR>SANDED THE REWORKED SURFACES AND EDGES OSDR SWAA2024102336380Strap · corrodedCORROSION ON SUPPORT STRAP LOCATED ON BS 787 AND STRINGER 26R AFT CARGO COMPARTMENT 2024-572513<[01] REPLACED SUPPORT STRAP LOCATED ON BS 787 AND STRINGER 26R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02. MEASURES OF CORROSION ARE: L: 1.1200 IN W: 0.4785 INSDR SWAA2024102336851Scuff Plate · crackedCRACK SCUFF PLATE ON SERVICE DOOR AT FWD GALLEY AREA 2024-572624<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30;S/N:A23046084;DUE DATE:23-MAY-25.;[02] EQUIPMENT P/N XRP-3000; S/N 1753759; DUE DATE 17-DEC-24 WAS USED ON STEP 4;[03] REPAIRED SCUFF PLATE ON SERVICSDR SWAA2024102336846Vapor Barrier · cracked(CUSTOMER REQUEST) CRACK ON VAPOR BARRIER LOCATED AT BS 663.75 BETWEEN LBL 31.83 TO LBL 5.64 2024-572609 (CUSTOMER REQUEST) CRACK ON VAPOR BARRIER LOCATED AT BS 663.75 BETWEEN LBL 31.83 TO LBL 5.64 LH SIDE WHEEL WELL COMPARTMENT<[01] TOOL USED HOT BONDER P/N: SDR SWAA2024102336844Support Bracket · crackedCRACK SUPPORT BRACKET ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2024-572592<[01] REPLACED SUPPORT BRACKET ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND B737-700 SRM 51-40-02-0G-0.;[02] JOB COMPLETEDSDR SWAA2024102336845Access Panel · crackedCRACK BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB 2024-572586<[01] REPLACED BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND B737-700 SRM 51-40-02-0G-0.;[02] JOB COMPLETEDSDR SWAA2024102236376Fitting · deterioratedDETERIORATED HARDWARE AND PLATE ON GIRT BAR FITTING FWD SERVICE DOOR AT FWD GALLEY AREA 2024-572493<[01] REPLACED HARDWARE AND PLATE ON GIRT BAR FITTING FWD SERVICE DOOR AT FWD GALLEY AREA IAW SOPM 20-50-01 REV 38;[02] REPLACED HARDWARE AND PLATE ON GIRT BAR FSDR SWAA2024102236377Fitting · deterioratedDETERIORATED HARDWARE AND PLATE ON GIRT BAR FITTING FWD ENTRY DOOR AT FWD GALLEY AREA 2024-572496<[01] REPLACED HARDWARE AND PLATE ON GIRT BAR FITTING FWD ENTRY DOOR AT FWD GALLEY AREA IAW SOPM 20-50-01 REV 38;[02] REPLACED HARDWARE AND PLATE ON GIRT BAR FITTISDR SWAA2024102335633Handle · deterioratedDETERIORATED FWD SERVICE DOOR ASSIST HANDLE NUTS (2EA) 2024-572428<[01] REPLACED FWD SERVICE DOOR ASSIST HANDLE NUTS (2EA) IAW B737-700 AMM 52-41-31-400-802; STEP 3F(2);[02] TASK COMPLETEDSDR SWAA2024102235746Fitting · deterioratedDETERIORATED GIRT BAR FITTING HARDWARE ON ENTRY DOOR AT AFT GALLEY AREA 2024-572429<[01] REPLACED GIRT BAR FITTING HARDWARE ON ENTRY DOOR AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801; FOR INSTALLATION STEPS SEE TASK 725-025-00-02Y (TTG8Q002GMB5; STEP13SDR SWAA2024102235747Fitting · deterioratedDETERIORATED GIRT BAR FITTING HARDWARE ON GALLEY SERVICE DOOR AT AFT GALLEY AREA 2024-572430<[01] REPLACED GIRT BAR FITTING HARDWARE ON GALLEY SERVICE DOOR AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801; FOR INSTALLATION STEPS SEE TASK 725-025-00-02Y (TTSDR SWAA2024102335333Light · brokenBROKEN CENTER EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA 2024-572414<[01] REPLACED CENTER EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY ARE IAW B737-700 AMM 33-51-01-960-802 TEST IS OK;[02] CERTIFIED WORK PERFORMED.SDR SWAA2024091135259Nonskid · peelingFWD ENTRY DOOR SILL NON-SLIP TAPE IS PEELING UP.<[01] REMOVED AND REPLACED NON SKID ; FORWARD ENTRY DOOR SCUFF PLATE. REF AMM 53-11-01.SDR SWAA2024102335041Light · brokenBROKEN PHOTOLUMINESCENT STRIP (10 EA) AT PASSENGER CABIN 2024: 572313<[01] REPLACED PHOTOLUMINESCENT STRIP (10 EA) AT PASSENGER CABIN IAW B737-700 AMM 33-51-15-400-802 AND DWG 33500007 REV 2.;[02] CERTIFIED WORK PERFORMEDSDR SWAA2024100130590Balance Weight · corrodedRUDDER BALANCE ARM WEIGHT CORRODED<[01] RUDDER BALANCE ARM WEIGHT REPLACED ON CSD WORK ORDER #575213; CUSTOMER PO #P8436615-1; FORM TRACKING #N-197042;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.SDR SWAA2024100230067Doubler · crackedL/H BS 663 LOWER VAPOR BARRIER DOUBLER 111A1521-9 CRACKED AT FASTENER HOLE<[01] FABRICATED DOUBLER IAW SRM 51-30-01-0G-0 AND DWG 111A1521 REV:C AND DWG 111A1521 REV:- FROM 2024 T3 0.040' LOT 1572886-1SDR SWAA2024100229218Attach Angle · crackedCRACKED ATTACH ANGLE AT FWD CABIN BS293 RBL55 WL208. MARKED<[01] REMOVED ANGLE BS294 RBL55 WL208 AND INSTALLED NEW ANGLE BS294 RBL55 WL208 I.A.W SRM 51-40-02-0G-0 AND DWG 143A8310 REV.B.;[02] CC COMPLETESDR SWAA2024100229219Sill Drain · crackedCRACKED FWD ENTRY DOOR MOP SILL BS294+8 LBL55 WL208. MARKED.<[01] UPDATED STEP 2;[02] UPDATED STEP 2;[03] REJECT - STEP 2; ITEM 5.; FOUND 14EA LOOSE TEMP. FASTENERS; 11EA OPEN HOLES W/O FASTENERS. TTG8Q00VMXKN;[04] REMOVED FWD ENTRY DOOR MOPSILL AND LOCATED; DSDR SWAA2024100229220Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT FWD WET AREA BS304 LBL11 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL (FLOOR SUPPORT) AT FWD WET AREA FROM BS 294.5 TO BS 312 LBL 11 PER SRM 51-40-02-0G-0 AND BOEING DWG 141A5600 REV. N.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024100229221Floor Support · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS328 - BS344 LBL45 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL AT BS328 TO BS344 LBL45; WL208 PER SRM 51-40-02 AND DWG:141A5400 REV:-.;[02] VERIFIED CORRECTIVE ACTION #1;[03] CARD COMPLETED;[04] VERIFIED.SDR SWAA2024100229225Intercostal · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS394 LBL13 WL208.<[01] UPDATED STEP 1-3;[02] CORRECTED STEP 2;[03] REMOVED AND REPLACED INTERCOSTAL ANGLE AT FWD WET AREA BS394 LBL13 WL 208 PER SRM 51-40-02-0G-0-A00729 AND DWG 143A5400 REV:A;[04] VERIFIED CORRECTIVE ACTIOSDR SWAA2024100228407Web · corrodedCORROSION ON SUBTHRESHOLD WEB FCB<[01] REMOVED AND REPLACED SUBTHRESHOLD WE AT FCB BETWEEN BS 440 TO BS 492 RBL 23 WL 156 PER SRM 51-40-02 ;DWG 143A8330; REV:-.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024100228848Support Angle · crackedCRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS914 RBL12 WL170.<[01] REMOVED AND REPLACED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS914 RBL12 WL170.IAW SRM 51-40-05 AND BOEING DWG 147A7221. REV: -;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD
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