Boeing 737-79P
Service difficulty reports · 2,376
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 = '73779P' 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 = '73779P' 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 SWAA2021120141292Stiffener · crackedLT HORIZONTAL STAB HSS 120.3, RIB 4, 4TH VERTICAL STIFFENER WAS CRACKED. CUT & REMOVED CRACK DAMAGE ON VERTICAL STIFFENER IAW SRM 55-10-09-2R-4 STEP 4.B. HFEC INSPECTED OPEN HOLES IAW NDTM PART 6 51-00-00 PROCEDURE 16. NO CRACKS NOTED. HFEC INSPECTED CUT OSDR SWAA2021120141291Stiffener · crackedLT HORIZONTAL STAB HSS 120.3 RIB 4; 3RD VERTICAL STIFFENER CRACKED. REMOVED LEFT HAND HORIZONTAL STAB INSPAR RIB TO ACCESS REPAIR IAW SRM 51-40-02-0G-0. CUT AND REMOVED CRACK DAMAGE ON VERTICAL STIFFENER IAW SRM 55-10-09-2R-4 STEP 4.B. HFEC INSPECTED OPEN SDR SWAA2021112332557None · brokenBROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (8 EA) ; 2021-486719 / [01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (8 EA) IAW B737-700 AMM-33-51-15-400-802 AND DWG-33500007 REV. 2; [02] TASK COMPLETEDSDR SWAA2021110833068Drag Brace · corrodedCORROSION FITTING ON DRAG BRACE FWD LOCATED AFT REAR SPAR LH POSITION AT VERTICAL STABILIZER. REPLACED FITTING REAR SPAR DRAG BRACE LH FWD POSITION O/B SIDE AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING # 148A8200 SHEET 4SDR SWAA2021110833067Drag Brace · corrodedCORROSION FITTING ON DRAG BRACE AFT POSITION LOCATED AFT REAR SPAR LH SIDE AT VERTICAL STABILIZER (1 EA). REPLACED FITTING DRAG BRACE LH AFT POSITION O/B SIDE AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DRAWING # 148A8200 SHEET SDR SWAA2021112332537Reveal · crackedCRACK SERVICE DOOR CUT OUT REVEAL LOCATED BS294.5 AND BTW STR 9R TO STR 10R AT FWD GALLEY AREA ; 2021-486655 / [01] REPLACED REVEAL LOCATED BS 294.5 AND BTW STR 9R TO STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02 AND DWG 141A8370 RSDR SWAA2021112332538Stub Frame · crackedCRACK SERVICE DOOR CUT OUT STUB FRAME LOCATED BS 294 AND BTW STR 8R AND STR 9R AT FWD GALLEY AREA ; 2021-486653 / [01] REPLACED STUB FRAME SERVICE DOOR CUT OUT AT BS 294.5 BTW STR 7R AND STR 9R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9 DWG 141A8SDR SWAA2021112332535Beam · elongatedELONGATED HOLE FLOOR STRUCTURE BEAM LOCATED BS986 AND BETWEEN RBL18 TO RBL39 AT AFT GALLEY AREA (2 EA) ; 2021-486671 / [01] REPLACED THE DAMAGE PART (TEE CHORD) TO RESTORE THE AIRCRAFT TO ITS APPROVED CONFIGURATION DEFINED IN EA 1-753-35993 REV IR. SEE INDIVIDSDR SWAA2021112332330Web · crackedCRACK WEB LOCATED BS 277-294.5, BL 0, FWD GALLEY AREA. REPLACED WEB IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, & DWG 141A5400, SHEET 20, REV: -.SDR SWAA2021112332331Web · crackedCRACK WEB LOCATED BS312 TO BS328 AT RBL33 AT FWD GALLEY AREA ; 2021-486652 / [01] REPLACED WEB LOCATED BS312 TO BS328 AT RBL33 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 141A5400 REV: -; [02] JOB COMPLETED AND CERTIFIED AS RSDR SWAA2021112332530None · crackedCRACK ANGLE - CLIP LOCATED BS500C AND RBL 21.0 AT FWD CARGO COMPARTMENT ; 2021-486659 / [01] TOOL USED ELECTRONIC CALIPER 0-6? PN 500-196-30 SN A20231699 DUE DATE 06SEP2S; [02] REPLACED NEW ANGLE-CLIP AND FASTENERS BS 500C; RBL21 AT FWD CARGO COMPARTMENT IAW BSDR SWAA2021112332531None · crackedCRACK ANGLE-CLIP BS 500B;LBL21 AT FWD CARGO COMPARTMENT ; 2021-486658 / [01] REPLACED NEW ANGLE-CLIP AND FASTENERS BS 500B;LBL21 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 Ï¿½TEM 9 DWG 143A7505 SHEET 5 REV B.; [02] REPLACED NEW ANGLE-CLIP ANDSDR SWAA2021112332534None · corrodedCORROSION WEB - INTERCOSTAL LOCATED BTW BSTA 500C AND BSTA 500D AT LEVEL STR 25L WL 156 LBL 21.84 AT FWD CARGO COMPARTMENT ; 2021-486669 / [01] TOOL USED: DIGITAL CALIPER P/N: DIGITAL150; S/N: AE-412610; DUE DATE: 21MAY22; [02] REPLACED WEB - INTERCOSTAL LOCATSDR SWAA2021112332536None · crackedCRACK WEB - INTERCOSTAL LOCATED BSTA 500B TO BSTA 500C AT LEVEL STR 25R WL 156 RBL 21.84 AT FWD CARGO COMPARTMENT ; 2021-486670 / [01] REPLACED WEB INTERCOSTAL LOCATED BSTA 500B TO BSTA 500C AT LEVEL STR 25R WL 156 RBL 21.84 AT FWD CARGO COMPARTMENT IN IAW B73SDR SWAA2021112332539None · corrodedCORROSION BILGE AREA BTW BS 440-460, S28L, LBL 6, WL 148.5, FWD CARGO COMPARTMENT. REPAIRED BILGE AREA IAW SRM 53-00-03-2R-1 REPAIR 1.SDR SWAA2021112332533Stringer · corrodedCORROSION STRINGER 26L BTW BS 480/500A; LBL 19 APPROX; WL 150 AT FWD CARGO COMPARTMENT. REPAIRED STRINGER 26L BTW BS 480/500A; LBL 19 APPROX; WL 150 AT FWD CARGO COMPARTMENT B737-700 SRM 53-00-03-2R-1 REPAIR 1.SDR SWAA2021112332532Stringer · corrodedCORROSION STRINGER 27L LOCATED BTW BS500-500A, RBL 12.5, WL 149, FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER IAW SRM 53-00-03-2R-1 REPAIR 1 TABLE 202 FIG. 206.SDR SWAA2021112332168None · crackedCRACK EXTERNAL GROUND ELECTRICAL POWER CUT OUT AT LOWER FUSELAGE ; 2021-486578 / [01] TOOL USED P/N:NORTEC 600D S/N: 210138503 CAL DUE DATE: 05-MAR-22; [02] TOOL USED DIGITAL CALIPER P/N: DIGITAL 150; S/N: AE-412600; DUE DATE: 21/JUL/22; [03] REPAIRED EXTERNALSDR SWAA2021112331837Floor Panel · corrodedCORROSION FLOOR PANEL 222BF (SLEEVE) AT FWD GALLEY AREA (6 EA) ; 2021-486550 / [01] REMOVED AND REPLACED SLEEVE (6EA) ON FLOOR PANEL 222BF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-0 PARAGRAPH 5.S. TOOL USED HOTBONDER P/N HCS9200B-AV S/N 18185733 DUE SDR SWAA2021112331818Battery Pack · inoperativeINOP EMERGENCY LIGHT BATTERY PACK ON BS 597 LT SIDE AT PASSENGER CABIN ; 2021-486508 / [01] REPLACED EMERGENCY LIGHT BATTERY PACK ON BS 597 LT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805; PERFORMED OPERATIONAL TEST. TEST IS OK.; [02] TASK COMPLETSDR SWAA2021112331823Tie Clip · crackedCRACK TIE CLIP LOCATED BS 277 AND S-10R AT PASSENGER CABIN ; 2021-486524 / [01] TOOL USED: CALIPER P/N: 500-197-30; S/N: A21043111; DUE DATE: 15-SEP-22; [02] REPLACED TIE CLIP LOCATED BS 277 AND S-10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PAR. 9; SRM 51SDR SWAA2021112331075Scuff Plate · crackedCRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT ; 2021-486397 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189510;DUE DATE:23-NOV-21.; [02] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 ASDR SWAA2021112331084Bear Strap · crackedCRACK INDICATION ON SERVICE DOOR CUT OUT BEAR STAP, BS 290-296, S8-9R. REPAIRED EXTERNAL SKIN IAW SRM 53-10-01-2R-6 REPAIR 6, EA 21-153-03267-WIP1, AND EA 21-153-03267.SDR SWAA2021100625862Panel · elongated194E ATTACH HOLES ELONGATED ; WHILE PERFORMING VISAL INSP. OF THE 194E PANEL FOND SEVERAL ATTACH HOLES CRACKED AND ELONGATED. / [01] INSTALLED NEW PANEL IAW AMM 53-51-21SDR SWAA2021100625863Panel · elongated193D PANEL ATTACH HOLES ELONGATED ; WHILE PERFORMING VISAL INSP. OF 193D PANEL FOND SEVERAL HOLES CRACKED AND ELONGATED. / [01] REMOVED AND REPLACED WING TO BODY FAIRING 193D PER MM 53-51-21.SDR SWAA2021101820586None · crackedCRACK INNER CHORD LOCATED BS303.9 AT LEVEL STR 17L LH SIDE AT FWD GALLEY AREA ; 2021-403943 / [16] REPLACED INNER CHORD LOC BS 277 TO BS 360 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 AND DWG 141A8110 SHEET 11 REV: -; [17] STEP 1SDR SWAA2021101818230Support Angle · corrodedCORROSION WATER SERVICE DOOR 146AR SUPPORT ANGLE LOCATED BETWEEN BS 907 TO BS 927 STR 25R TO STR 27R WL 168.1 AT LOWER FUSELAGE ; 2021-403934 / 14] REPLACED SUPPORT ANGLE ON WATER SERVICE DOOR 146AR LOCATED BETWEEN BS 907 TO BS 927 STR 25R TO STR 27R WL 168.1 SDR SWAA2021101818225Angle · crackedCRACKED ANGLE BS 695, RBL 24.5 FLOOR STRUCTURE AT CENTER WING BOX. REMOVED ANGLE NO FOUND ALLOWABLE DAMAGE LIMITS IAW SRM 51-40-02, MEASURE OF CRACK IS L=1.58. PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO MORE FOUND DAMAGE. FORMED ANGLE IAW DWG 2SDR SWAA2021092017713Lamp · inoperativeL/H EXTERIOR OVERWING EMERGENCY LIGHT INOP. ; / [01] RELAMPED L/H EXTERIOR OVERWING EMERGENCY LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.; [02] VERIFIED STEP 1.SDR SWAA2021092017708Connector · disconnectedR/H ROW 19 EMERGENCY LIGHT INOP ; / [01] RECONNECTED LIGHT ASSY. PERFORMED OPS CHECK; FOUND NORMAL AS PER B737 AMM 33-51-03-960-801.; [02] VERIFIED STEP 1.SDR SWAA2021101815560Rib · crackedCRACK LEADING EDGE RIB LOCATED AT ACCESS PANEL 314B LE STA 114.55 AT RT HORIZONTAL STABILIZER ; 2021-403770 / [11] INSTALLED NEW RIB AND FASTENER LOCATED AT ACCESS PANEL 341B LE STA 114.55 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 SDR SWAA2021093016029Spar · corrodedPITTING ON DORSAL FIN FRONT SPAR FITTING RH BOLT (STA 1016) AT VERTICAL STABILIZER (1EA) ; 2021-403818 / [01] REMOVED RH BOLT ON DORSAL FIN FRONT SPAR FITTING AT VERTICAL STABILIZER (STA 1016) IAW B737-700 AMM 55-30-00-000-801 STEP 2F(7)(B) AND PERFORMED GENERSDR SWAA2021101815537Tie Clip · crackedCRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN. REMOVED TIE CLIP IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION AND DID NOT FIND MORE DAMAGE. CRACK LENGTH: 0.656. DRILLED NEW TIE CLIP IAW SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT ON OPESDR SWAA2021101815535Angle · corrodedCORROSION ANGLE LOCATED BETWEEN BS312 TO BS328 AND STR4L TO STR6L; WL288 AT PASSENGER CABIN ; 2021-403724 / [21] REPLACED ANGLE LOCATED BETWEEN BS312 TO BS328 AND STR4L TO STR6L; WL288 AT PASSENGER CABIN IAW SRM B737-700 51-10-02 AND DWG# 141A1180 REV. F DUE TSDR SWAA2021101815554Web · corrodedCORROSION WEB LOCATED BETWEEN STA.303.9 TO STA348.2 AND STR6L; WL282.1 APPROX.LH SIDE AT FWD GALLEY AREA ; 2021-403723 / [23] REPLACED WEB LOCATED BETWEEN STA.303.9 TO STA348.2 AND STR6L; WL282.1 APPROX.LH SIDE AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEMSDR SWAA2021101815555Frame · crackedCRACK FRAME ON BS 312 LOCATED BETWEEN STR5L TO STR6L LH SIDE AT FWD GALLEY AREA ; 2021-403722 / [30] REPAIRED FRAME ON BS 312 LOCATED BETWEEN STR5L TO STR6L LH SIDE AT FWD GALLEY AREA IAW B737-700 SRM 5,NG,NRC,2021-09-23 23:36:55,18Y,Y,MX,0,0,,CRACK FRAME ON BSDR SWAA2021101815538Angle · corrodedCORROSION ANGLE LOCATED BETWEEN BS328 TO BS344 AND STR4L TO STR6L;WL287 AT PASSENGER CABIN ; 2021-403725 / [26] REPLACED ANGLE LOCATED BETWEEN BS328 TO BS344 AND STR4L TO STR6L;WL287 AT PASSENGER CABIN IAW SRM B737-700 51-10-02 AND DWG# 141A1180 REV. F. AND SRSDR SWAA2021101815543None · crackedCRACK STUD FRAME LOCATED ON BS294.5 AND STR17R AT FWD GALLEY AREA. INSTALLED REPAIR CLIP AND FASTENERS LOCATED AT BS 294.5 AND STR 17L IAW B737-700 SRM 51-40-02 AND 53-10-15-2R-7 REPAIR 7; [23] INSTALLED RII COMPLETE STEP 22; [24] REPAIRED STUD FRAME LOCATED SDR SWAA2021101815505Floor Panel · crackedCRACK FLOOR PANEL 231JF AT PASSENGER CABIN ; 2021-403669 / [23] REPAIRED FLOOR PANEL 231JF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [24] REPAIRED FLOOR PANEL 231JF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1 RII INSPECTSDR SWAA2021101815512Floor Panel · crackedCRACK FLOOR PANEL 242AF AT PASSENGER CABIN ; 2021-403677 / [21] REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [22] REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.RII INSPECTSDR SWAA2021101815540Floor Panel · crackedCRACK FLOOR PANEL 242RF LOCATED AT AFT GALLEY AREA ; 2021-403768 / [17] REPAIRED FLOOR PANEL 242RF LOCATED AT AFT GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [18] REPAIRED FLOOR PANEL 242RF LOCATED AT AFT GALLEY AREA AS PER B737-700 SRM 53-00-50-2RSDR SWAA2021101815536Floor Panel · crackedCRACK FLOOR PANEL 241ADF AT AFT GALLEY AND LAVATORY ; 2021-403754 / [21] REPAIRED FLOOR PANEL 241ADF AT AFT GALLEY AND LAVATORY AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [22] REPAIRED FLOOR PANEL 241ADF AT AFT GALLEY AND LAVATORY AS PER B737-700 SRM 53-00-50SDR SWAA2021101815514Floor Panel · missingMISSING MATERIAL FLOOR PANEL 221CF AT PASSENGER CABIN ; 2021-403689 / [21] REPAIRED FLOOR PANEL 221CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [22] REPAIRED FLOOR PANEL 221CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.SDR SWAA2021101815496Floor Panel · crackedCRACK FLOOR PANEL 221BF AT PASSENGER CABIN ; 2021-403681 / [22] REPAIRED FLOOR PANEL 221BF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [23] REPAIRED FLOOR PANEL 221BF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.RII INSPECTSDR SWAA2021101815495Floor Panel · missingMISSING MATERIAL FLOOR PANEL 221DF AT PASSENGER CABIN ; 2021-403679 / ; [22] REPAIRED FLOOR PANEL 221DF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [23] REPAIRED FLOOR PANEL 221DF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR SDR SWAA2021101815534None · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328; RBL30 AT FWD GALLEY AREA. REMOVED WEB AND FASTENERS LOCATED BETWEEN BS 312 TO BS 328, RBL 30 AT FWD GALLEY AREA IAW SRM 51-40-02 REMOVAL WEB AND DID NOT FIND ADDITIONAL DAMAGE. MEASUSDR SWAA2021101815551None · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS328 TO BS344; LBL46 AT FWD GALLEY AREA ; 2021-403742 / [11] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS328 TO BS344; LBL46 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9 SRM SDR SWAA2021101815552None · corrodedCORROSION INNER CHORD FLOOR STRUCTURE LOCATED BETWEEN BS 312 - 344, RBL 58, WL 208.1. INSTALLED NEW INNER CHORD 1(EA) AND FASTENERS IAW SRM 51-40-02 AND DWG 141A8310 SHEET 25 REV-.SDR SWAA2021101815506Angle · crackedCRACK ANGLE LOCATED BS500C BTW STR25 TO STR26R FWD CARGO COMPARTMENT. REMOVED ANGLE IAW SRM 51-40-02 DUE TO NO FOUND ALLOWABLE DAMAGE ON SRM LENGTH OF CRACK IS 0.202 INCH AND PERFORMED VISUAL INSPECTION ON AREA AND NO FOUND DAMAGE. DRILLED NEW ANGLE IAW SRSDR SWAA2021093015548Floor Panel · brokenBROKEN FLOOR PANEL 241AEF AT AFT GALLEY AND LAV ; 2021-403753 / [01] EVALUATED FLOOR PANEL 241AEF AT AFT GALLEY AND LAV AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 SRM 53-00-50-2R-1 REP 1; PAR 1A. DAMAGE SIZE IS L=1.48 W=1.11 TOOL USED CALIPER P/N 500-19
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