Boeing 737-79P
Service difficulty reports · 2,374
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 SWAA2025103016496Stringer Clip · no discrepancyFUSELAGE STRINGER CLIP BS 706, S10L CRACKED. HFEC INSPECTED AREA IAW NDTM PART 6, 51-00-00, PROCEDURE 23. NO CRACKS NOTED.SDR SWAA2025103016497Stringer Clip · no discrepancyFUSELAGE STRINGER CLIP BS 727A S15L CRACKED. HFEC INSPECTED AREA IAW NDTM PART 6; 51-00-00, PROCEDURE 23. NO CRACKS NOTED.SDR SWAA2025110316163Pressure Deck · crackedCRACK NOTED ON LEFT HORIZONTAL PRESSURE DECK WEB BS 673, LBL 32, WL 202.5. L: 0.4. REPAIRED THE PRESSURE DECK AND REMOVED & REPLACED ALL SHORT AND HIGH FASTENERS AND INSTALLED MISSING COLLARS AT THE REPAIR AREA AS A CORRECTION FOR STEP 10, ITEM 1 IAW SRM 53-SDR SWAA2025103015048Floor Panel · pulledFLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.SDR SWAA2025103015049Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.SDR SWAA2025103015050Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.SDR SWAA2025103015052Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241BF REPLACED WITH A NEW FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR SWAA2025103015054Floor Panel · pulledFLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.SDR SWAA2025103015057Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.SDR SWAA2025103015056Floor Panel · pulledFLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.SDR SWAA2025103015058Floor Panel · pulledFLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED A NEW FLOOR PANEL IAW DWG 144A5810 0123.SDR SWAA2025103015051Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0-A00938.SDR SWAA2025103015047Floor Panel · pulledFLOOR PANEL 232RF UPPER SKIN HAS AREAS OF PULLED STRANDS FABRICATION OF NEW FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0-A00938.SDR SWAA2025102315280Sill Drain · corrodedCORROSION LOWER SILL LOCATED BETWEEN STA794.3 TO STA847 AND RBL24 WL156 AT AFT CARGO COMPARTMENT. REPLACED LOWER SILL LOCATED BETWEEN STA794.3 TO STA847 AND RBL24 WL156 AT AFT CARGO COMPARTMENT IAW SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 146A8340; SHEESDR SWAA2025091915164Lamp · inoperativeLEFT FUSELAGE EMERGENCY LIGHT INOP RIGHT BEHIND LEFT WING TRAILING EDGE FLAPS. RELAMPED LEFT FUSELAGE EMERGENCY LIGHT PER AMM 33-51-04.SDR SWAA2025110415045Skin · no discrepancySUSPECT CRACK RT WING NR 5 SLAT LEADING EDGE AT ACTUATOR ATTACH FITTING, SLAT STATION 85.19. HFEC INSPECTED RT WING #5 SLAT LEADING EDGE AT ACTUATOR ATTACH FITTING SLAT STATION 85.19 IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS NOTED.SDR SWAA2025110415026Inlet · pulledPULLED THROUGH FASTENERS 2 O' CLOCK POSITION ON RIGHT INLET COWL OUTER LIP SKIN. REMOVED AND REPLACED RT INLET COWL OUTER LIP SKIN IAW SRM 54-10-01-1A-2 AND SRM 51-40-02. ACCOMPLISHED NDI INSPECTION IAW NDTM PART 6; 51-00-00. REMOVED AND REPLACED NR 2 ENGISDR SWAA2025102314819Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND DWG 212A1101; SHEET 3 REV-.SDR SWAA2025102314816Tie Clip · crackedCRACK TIE CLIP BS 277 AND STRINGER 10R PASSENGER CABIN. REPLACED TIE CLIP AND FASTENERS LOC.BS 277 AND STRINGER 10R PASSENGER CABIN IAW SRM 51-40-02; SRM B737-700 51-10-02 PARAGRAPH 9; DWG 141A1110 SHEET:18 REV:- AND DWG 141A8380 SHEET:14 REV-.SDR SWAA2025102314813Support Angle · crackedCRACK SUPPORT ANGLE BETWEEN BS 291.5 TO BS 294.5 AT LEVEL STRINGER 17R PASSENGER CABIN. REPLACED SUPPORT ANGLE LOC. BETWEEN BS 291.5 TO BS 294.5 AT LEVEL STRINGER 17R PASSENGER CABIN IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, DWG 141A8310 SHEET 25; REV.SDR SWAA2025102314821Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY . REPLACED SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY IAW SRM 51-40-02-0G-0.SDR SWAA2025102214625Vapor Barrier · crackedCRACK ON VAPOR BARRIER BS 663.75 LH SIDE MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER BS 663.75 LH SIDE MAIN WHEEL WELL COMPARTMENT IAW SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2025102214626Light · deterioratedDETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHT LT SIDE 7 EA AND RT SIDE 7 EA. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING IAW AMM 33-51-15-400-802.SDR SWAA2025102314618Strap · corrodedCORROSION STRAP LOCATED BETWEEN BS787 TO BS794 AND WL154 FROM STR25R TO STR26R AFT CARGO COMPARTMENT. REPLACED STRAP LOCATED BETWEEN BS787 TO BS794 AND WL154 FROM STR25R TO STR26R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 SDR SWAA2025102314619Strap · corrodedCORROSION STRAP LOCATED BETWEEN BS794 TO BS807 AND WL154 FROM STR25R TO STR26R AFT CARGO COMPARTMENT. REPLACED STRAP LOCATED BETWEEN BS794 TO BS807 AND WL154 FROM STR25R TO STR26R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 SDR SWAA2025102314554Access Panel · crackedCRACK ANGLE ACCESS PANEL 844DZ AT AFT GALLEY DOOR. REPLACED ANGLE ACCESS PANEL 844DZ AT AFT GALLEY DOOR DUE TO ALLOWABLE DAMAGE NOT FOUND IN SRM 52-10-02-1A-4; MEASURE OF CRACK IS: 0.310'. ANGLE REPLACED IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DRAWINSDR SWAA2025102214613Cargo Track · crackedCRACK TRACK LBBL 17.24 LOCATED BS767 AFT CARGO COMPARTMENT. REPAIRED CARGO TRACK LOC LBL17.24 BTW BS 747 TO BS 787 IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3.SDR SWAA2025093014344Light · deterioratedDETERIORATE PHOTOLUMINESCENT AT PASSENGER CABIN RH SIDE (7EA). THE REPLACEMENT PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN (7 EA) WILL BE ACCOMPLISHED IN TASK 733-080-00-01 (TTG8Q003FNTQ)SDR SWAA2025093014343Light · deterioratedDETERIORATE PHOTOLUMINESCENT STRIP AT PASSENGER CABIN LH SIDE (7EA). THE REPLACEMENT PHOTOLUMINESCENT STRIP AT PASSENGER CABIN LH SIDE (7EA) WILL BE ACCOMPLISHED IN TASK 733-080-00-01 (TTG8Q003FNTQ).SDR SWAA2025102314161Support · crackedCRACK CHANNEL SUPPORT LOCATED STA727 AND RBL 3 AT AFT CARGO COMPARTMENT. REPLACED CHANNEL SUPPORT LOCATED STA727 AND RBL 3 AT AFT CARGO COMPARTMENT IAW B737 700 SRM 51-10-02-0G STEP 9 AND DWG 144A2600 SHEET 566 REV -.SDR SWAA2025102314157Gusset · damagedELONGATED HOLE GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 143A7902; SHEET: 174; REV-.SDR SWAA2025102314160Web · corrodedCORROSION SHIELD WEB FLOOR STRUCTURE LOCATED BETWEEN STA767 TO STA794.3 AND RBL21 WL156 AT AFT CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOC. ON FLOOR STRUCTURE BETWEEN STA767 TO STA794.3 AND RBL21 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM51-SDR SWAA2025102214154Rib · crackedCRACKED INSPAR RIB LOCATED STAB STA 120.30 AND 34 INCHES FROM FRONT EDGE LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 51-40-02, AND SRM 55-10-09-2R-4, REPAIR 4, FIG 202, DETAIL A.SDR SWAA2025102214155Rib · crackedCRACKED INSPAR RIB LOCATED STAB STA 120.30 AND 27 INCHES FROM FRONT EDGE LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 51-40-02, AND SRM 55-10-09-2R-4, REPAIR 4 FIG 202, DETAIL A.SDR SWAA2025102214156Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 120.30 AND 19 INCHES FROM FRONT EDGE LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 51-40-02, AND SRM 55-10-09-2R-4, REPAIR 4, FIG 202, DETAIL A.SDR SWAA2025102314094Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 120.30 AND 27 INCHES FROM FRONT EDGE LT HORIZONTAL STAB.SDR SWAA2025102314093Rib · crackedCRACK INSPAR RIB LOCATED STAB STA120.30 AND 19 INCHES FROM FRONT EDGE LT HORIZONTAL STAB.SDR SWAA2025102214153Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 129.50 AND 34 INCH FROM FRONT EDGE AT RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 55-10-09-2R-5, REPAIR 5, FIG 204, DETAIL A.SDR SWAA2025102313442Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BS 695 AND RBL 24.75 AT PASSENGER CABIN. REPLACED ANGLE ON FLOOR STRUCTURE LOCATED BS 695 AND RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DWG: 273A9110 SHEET: 6 REV: A.SDR SWAA2025102313443Stiffener · crackedCRACK STIFFENER ASSY FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL 0 AND RBL 24.75 PASSENGER CABIN. REPLACED STIFFENER ASSY FLOOR STRUCTURE AND FASTENERS LOCATED BS 540 BETWEEN BL 0 AND RBL 24.75 PASSENGER CABIN IAW B737-700 SRM-51-10-02 ITEM 9 AND B737-700 SRM 5SDR SWAA2025102313453Beam · crackedCRACK INDICATION ON RADIUS OF FORWARD SERVICE DOOR 141A6536-14 BEAM #4.LENGTH OF CRACK: 0.625 IN. EO 5241-C-14093 OR 5241-C-14344 WILL BE ADDED TO REPAIR ORDER FOR REPAIR. REPLACED TRACE BEAM NR 4 BTW BS 299.10 AND 328.87, FWD SERVICE DOOR IAW SRM 51-10-02 PSDR SWAA2025102213441Angle · crackedCRACKED ANGLE LOCATED BS 695 BL0 AFT SIDE. REPLACED ANGLE IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.SDR SWAA2025102213444Angle · crackedCRACKED ANGLE LOCATED BS 695 AND BL0 FWD SIDE. REPLACED ANGLE IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.SDR SWAA2025100213378Angle · crackedCRACK ON ANGLE LOCATED ON ACCESS PANEL 651FB TRAILING EDGE AT RT WING. REPLACED ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-05, AND DWG#115A2710 SHEET 6 REV B DUE TO NOT FINDING ALLOWABLE DAMAGE IN SRM 57-51-02-1A-1. MEASUREMET OF CRACK IS L= 1.336.SDR SWAA2025100213158Paint · peelingCORROSION SUPPORT STRUCTURE ACCESS PANEL 551FB TRAILING EDGE AT LT WING. PERFORMED DETAIL VISUAL INSPECTION ON SUPPORT STRUCTURE ACCESS PANEL 551FB TRAILING EDGE AT LT WING AND NO CORROSION FOUND, ONLY PEELING PAINT IAW SRM 51-10-02. NO MAINTENANCE ACTION IF SDR SWAA2025100213026Fairing · crackedCRACKED FAIRING 644BB AT RT WING. PERFORMED PERMANENT REPAIR ON FAIRING PANEL 644BB AT RT WING IAW EA 25-157-02530-WIP1 AND STEPS ARE DOCUMENTED ON FAULT TTG8Q0157YT6.SDR SWAA2025100113159Web · corrodedCORROSION DOOR CUTOUT LOWER SILL BETWEEN BS 794 TO BS 847 AND STRINGER 25R AFT CARGO COMPARTMENT. REPLACED LOWER SILL LOCATED ON DOOR CUTOUT LOWER SILL BETWEEN BS 794 TO BS 847 AND STRINGER 25R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9; DWG: 14SDR SWAA2025100113020Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 243, LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 243, LT WING IAW SRM 51-40-02-0G-0; DWG 115A2781 SHEET: 7 REV - AND DWG 115AA2001 SHEET: 87 REV -.SDR SWAA2025100212827Support Bracket · crackedCRACK TRAILING EDGE SUPPORT BRACKET ORSS 271 AT RT WING. REPLACED TRAILING EDGE SUPPORT BRACKET ORSS 271 AT RT WING IAW SRM 51-40-02; SRM 51-40-05 AND DWG 115A2930;SHEET 6 AND REV -. MEASURE OF CRACK IS 0.951.SDR SWAA2025100112632Angle · crackedCRACK ANGLE, TRAILING EDGE ORSS 271 AT LT WING. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, STEP 9, AND DWG 115A2930, SHEET 7, REV-. DUE TO DID NOT FIND ALLOWED DAMAGE IN SRM 57-51-02-1A-1.
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