N7713A
Service difficulty reports · 229
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N7713A' AND registry_match = 'registration' 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 n_number = 'N7713A' AND registry_match = 'registration' 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 SWAA2026091601309Valve · leakingSUSPECTED FUEL LEAK ON NUMBER 1 ENGINE PERFORMED ENGINE VENTS AND DRAINS INSPECTION PER AMM 71-71-00. FOUND FUEL TO BE LEAKING OUT OF BSV & LPTACC DRAIN HOLE AT A RATE GREATER THAN 90 DROPS PER MINUTE AT IDLE REMOVED AND REPLACED #1 ENGINE LPTACC VALVE IAW AMMSDR SWAA2026050594423Battery Pack · no testFWD LEFT ENTRY EMERGENCY BATTERY PACK M1675 FAILED A CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.SDR SWAA2025093018940Fan · odorFA SMELLED SOMETHING IN THE CABIN, OK TO CONTINUE PER MEL 21-31-02 SP 1 AND 2. AFTER INSPECTION OF CABIN ROWS 7-9 ABC AND DEF AREA AND PSU. FOUND RECIRCULATING FAN GRINDING AND NOISY. REMOVED AND REPLACED THE RECIRCULATION FAN IAW AMM 21-25-02. OPS CHECK GOSDR SWAA2025082206571Handle · missingAFT CARGO DOOR HANDLE STUD CAP IS MISSING.<[01] REPLACED AFT CARGO DOOR HANDLE STUD PER AMM 52-31-14;[02] INSP AFT CARGO DOOR HANDLE STUD PER AMM 52-31-14SDR SWAA2025081905397Bracket · looseAFT ENTRY SLIDE BRACKET LOOSE. SECURED SLIDE PACK AND COVER HARDWARE IAW AMM 25-66-01.SDR SWAA2025011786751Battery Pack · inoperativeL-1 DOOR FORWARD LOWER EMERGENCY EXIT LIGHT INOP 2024-759682<[01] PERFORMED FUSE REPLACE AT M1674 EMERGENCY EXIT BATTERY PACK TEST OK IAW B737-700 AMM 33-51-06-960-804<BR>TOOL USED MULTIMETER P/N: FLUKE 179 S/N: 97220166 DUE DATE 17/MAR/25;[02] CERTIFIED WORK SDR SWAA2025011786748Battery Pack · inoperativeEMERGENCY ESCAPE LIGHTS INOP ON OVERHEAD BIN BULLNOSE ROWS 4ABC; 9ABC; 11BC AND 8DEF 2024-759683<[01] PERFORMED FUSE REPLACE AT M2335 EMERGENCY EXIT BATTERY PACK TEST OK IAW B737-700 AMM 33-51-06-960-804 <BR>TOOL USED MULTIMETER P/N: FLUKE 179 S/N: 97220166 DUSDR SWAA2025011786750Bulb · burned outEMERGENCY EXIT LIGHT R-2 DOOR HAS BULB BURNED OUT 2024-759689<[01] REPLACED EXIT LIGHT R-2 DOOR LAMP TEST IS OK IAW B737-700 AMM 33-51-01-960-801;[02] CORRECTED STEP 1: REPLACED EXIT LIGHT R-2 DOOR LAMP IAW B737-700 AMM 33-51-01-960-801. PERFORM OPERATIONAL TESDR SWAA2025011585530Skin · crackedCRACK ON LOWER SURFACE OF SLAT 7 AT RIGHT WING. REPAIRED L/E SLAT FLEX SKIN ON LOWER SURFACE OF SLAT 7 AT RIGHT WING. IAW SRM 57-42-01-2R-13 REPAIR 13.SDR SWAA2025011578976Floor Panel · crackedCRACK FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT 2024-759629<[01] FABRICATED FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DWG 453A2610; SHEET 20; REV E: MATERIAL USED ALUMINUM SHEET P/N: 2024T3-071; PO: 2024 254382 AND APPLISDR SWAA2025011582818Angle · crackedCRACK ANGLE LOCATED WEATHER RADAR SUPPORT BETWEEN STA188 TO STA203.8 AT LOWER NOSE COMPARTMENT 2024-759635<[01] REPLACED ANGLE LOCATED WEATHER RADAR SUPPORT BETWEEN STA188 TO STA203.8 AT LOWER NOSE COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 ANDSDR SWAA2025011578741Floor Panel · damagedELONGATED HOLES ON FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2024-759626<[01] FABRICATED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DWG 453A2610; SHEET 11; REV C: MATERIAL USED ALUMINUM SHEET P/N: 2024T3-071; PO: 2024 254SDR SWAA2025011577946Support Bracket · crackedCRACK SUPPORT BRACKET BODY STATION 540 AND RBL6 KEEL BEAM 2024-759614<[01] REPLACED SUPPORT BRACKET BODY STATION 540 AND RBL6 KEEL BEAM IAW B737-700 SRM51-10-02 ITEM 9;B737-700 SRM 51-40-02 AND DRAWING 212A1101 REV.;[02] CORRECTED STEP 1:<BR>REPLACED SUPPORT BSDR SWAA2025011577947Support Bracket · crackedCRACK SUPPORT BRACKET BODY STATION 540 AND LBL6 KEEL BEAM. REPLACED SUPPORT BRACKET BODY STATION 540 AND LBL6 KEEL BEAM IAW B737-700 SRM 51-10-02 ITEM 9 ;B737-700 SRM51-40-02 AND DRAWING 212A1101 REV.-;[02] REPLACED SUPPORT BRACKET BODY STATION 540 AND LBL6 KSDR SWAA2025011577516Fitting · wornWEAR HARDWARE GIRT BAR FITTING SERVICE DOOR AT FWD GALLEY AREA 2024-759600<[01] REPLACED HARDWARE GIRT BAR FITTING SERVICE DOOR AT FWD GALLEY AREA IAW AMM 25-66-02-400-801;[02] TASK COMPLETEDSDR SWAA2025011577517Fitting · wornWEAR HARDWARE GIRT BAR FITTING ENTRY DOOR AT FWD GALLEY AREA (1EA) 2024-759601<[01] REPLACED HARDWARE GIRT BAR FITTING ENTRY DOOR AT FWD GALLEY AREA IAW B737-700 AMM-25-66-02-400-801 STEP 3.D;[02] REPLACED HARDWARE GIRT BAR FITTING ENTRY DOOR AT FWD GALLEY ARESDR SWAA2025011577753Web · cracked(CUSTOMER REQUEST)CRACK ON WEB LOCATED BETWEEN BS 294.5 TO BS 303.9 AT LEVEL STR16L AT PASSENGER CABIN. REPAIRED AREA ON WEB BETWEEN BS 294.5 TO BS 303.9 AT LEVEL STR16L AT PASSENGER CABIN IAW EA: 24-153-03556-WIP1 REV: A FIGURE 1 PAGE 2.SDR SWAA2025011577170Light · brokenBROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2024-759569<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) I.A.W B737-700 AMM-33-51-15-960-801;[02] COMPLETEDSDR SWAA2025011577168Angle · crackedCRACK ANGLE LOCATED BS663 AND RBL42 AT CENTER WING BOX 2024-759565<[01] REPLACED ANGLE LOCATED BS663 BTW RBL5 AND RBL63 IS DOCUMENTED FAULT TTG8Q00CLVQD; SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE LOCATED BS663 BTW RBL5 AND RBL63 IS DOCUMENTED FAULT TTGSDR SWAA2025011577167Angle · crackedCRACK ANGLE LOCATED BS663 AND LBL42 AT CENTER WING BOX 2024-759564<[01] REPLACED ANGLE LOCATED BS663 AND LBL5 TO LBL65 AT WING CENTER SECTION IAW B737 700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG #111A1000 SHEET 169 REV.- SEE INDIVIDUAL SIGNS OFFS BELOW.;[02]SDR SWAA2025011577169Angle · crackedCRACK ANGLE LOCATED BS663 AND RBL9 AT CENTER WING BOX 2024-759566<[01] REPLACED ANGLE AND FASTENERS LOCATED BS663 BTW RBL5 AND RBL63 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #111A1000 SHEET 171 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPSDR SWAA2025011576780Angle · crackedCRACK ANGLE LOCATED STA294.5 AND STR13L AT PASSENGER CABIN 2024-759559<[01] REPLACED ANGLE AND FASTENERS LOCATED STA294.5 AND STR13L AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #141A1311 SHEET 1 REV C.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] JOBSDR SWAA2025011576778Tie Clip · crackedCRACK TIE CLIP LOCATED BS360 AND STR8R PASSENGER CABIN 2024-759560<[01] REPLACED TIE CLIP LOCATED BS360 AND STR8R PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 140A9111 REV: - SHEET 62.<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] TASK COMPLETED; RII<BR><BRSDR SWAA2025011576779Tie Clip · crackedCRACK TIE CLIP LOCATED STA277 AND STR10R PASSENGER CABIN 2024-759558<[01] REPLACED TIE CLIP LOCATED STA277 AND STR10R PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 17 REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1<BR>RESDR SWAA2025011576584Stringer · crackedCRACK STRINGER 24R LOCATED BS540 AT FWD CARGO COMPARTMENT 2024-759518<[01] TOOL USED ON STEP 2: ULTRASONIC EQUIPMENT P/N 45MG; S/N;232019809; DUE DATE 08-OCT-25.;[02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3SDR SWAA2025011576774Stringer · crackedCRACK STRINGER 9 INTERNAL AREA FUEL TANK LOC. BTW RIB 21 AND RIB 22 UPPER SKIN LOWER SURFACE AFT AREA AT RT WING 2024-759516<[01] REPAIRED STRINGER 9 INTERNAL AREA FUEL TANK LOC. BTW RIB 21 AND RIB 22 UPPER SKIN LOWER SURFACE AFT AREA AT RT WING IAW B737-700 ESDR SWAA2025011576585Stringer · crackedCRACK STRINGER 23R LOCATED BS540 AT FWD CARGO COMPARTMENT 2024-759517<[01] TOOL USED ON STEP 2:ULTRASONIC EQUIPMENT P/N 45MG; S/N;232019809; DUE DATE 08-OCT-25;[02] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A23329415 DUE DATE: 06/MAR/25;[03] TOOL USED: TESDR SWAA2025011576586Stringer · crackedCRACK STRINGER 26R LOCATED BS540 AT FWD CARGO COMPARTMENT 2024-759519<[01] TOOL USED ON STEP 2: ULTRASONIC EQUIPMENT P/N 45MG; S/N;232019809; DUE DATE 08-OCT-25.;[02] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A23329415 DUE DATE: 06/MAR/25;[03] TOOL USED OSDR SWAA2025011576587Stringer · crackedCRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT 2024-759520<[01] TOOL USED ON STEP 2: ULTRASONIC EQUIPMENT P/N 45MG; S/N;232019809; DUE DATE 08-OCT-25.;[02] TOOL USED ON STEP 8 EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 60009161631 DUE DATE: 11-MAR-SDR SWAA2025011576322Frame · crackedCRACK FRAME LOCATED STA 440 AND BETWEEN STR 8R TO STR 9R AT PASSENGER CABIN 2024-759490<[01] REPAIRED FRAME LOCATED STA 440 AND BETWEEN STR 8R TO STR 9R AT PASSENGER CABIN IAW B737-700 EA#25-153-00006-WIP1 AND EA #25-153-00006. THIS REPAIR IS CLASSIFIED AS MAJSDR SWAA2025011576323Frame · crackedCRACK FRAME LOCATED STA 440 AND BETWEEN STR 8L TO STR 9L AT PASSENGER CABIN 2024-759491<[01] REPAIRED FRAME LOCATED STA 440 AND BETWEEN STR 8L TO STR 9L AT PASSENGER CABIN IAW B737-700 EA #24-153-03566-WIP1 AND EA #24-153-03566. THIS REPAIR IS CLASSIFIED AS MASDR SWAA2025011576319Support · crackedCRACK SUPPORT ZEE LOCATED BETWEEN STA 747 TO STA 767 AND LBL 21 AFT CARGO COMPARTMENT 2024-759484<[01] REPAIRED SUPPORT ZEE AND FASTENERS SECTION LOCATED BETWEEN STA 727E TO STA 847 AND LBL 21 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 DWG 1SDR SWAA2025011576327Frame · crackedCRACK FRAME LOCATED STA867 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN 2024-759492<[01] REPAIRED FRAME LOCATED STA867 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN IAW B737-700 EA #25-153-00018-WIP1 REV 2 AND EA #25-153-00018. THIS REPAIR IS CLASSIFIED AS MASDR SWAA2025011576320Frame · crackedCRACK FRAME LOCATED STA907 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN. REPAIRED FRAME LOCATED ON STA907 AND BETWEEN STR 7R TO STR 9R AT PASSENGER CABIN IAW EA: 24-153-03583-WIP1 AND EA SUMMARY 24-153-03583.SDR SWAA2025011576321Frame · crackedCRACK FRAME LOCATED STA 360 AND BETWEEN STR 8R TO STR 9R AT PASSENGER CABIN. REPAIRED FRAME LOCATED STA 360 AND BETWEEN STR 6R TO STR 9R AT PASSENGER CABIN IAW EA: 25-153-00022-WIP1 AND EA SUMMARY 25-153-00022.SDR SWAA2025011576333Support Angle · crackedCRACK SUPPORT ANGLE LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN 2024-759507<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE 23 JAN 25.;[02] REPLACED SUPPORT ANGLE LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASDR SWAA2025011575915Skin · crackedCRACK ON LOWER SURFACE OF SLAT 7 AT RIGHT WING. PERFORMED REPAIR ON LOWER SURFACE OF SLAT 7 AT RIGHT WING SEE INDIVIDUAL SIGN OFF BELOW. APPLICABILITY EVALUATION: AS PER THE APB SUPPLEMENT TO THE 737-700 SRM [AP37.7-0602]; THE SRM 57-42-01-2R-13 REPAIR 13 [DSDR SWAA2025011575914Handle · deterioratedDETERIORATE ASSIST HANDLE ASSY AFT SERVICE DOORWAY AT AFT GALLEY AREA 2024-759442<[01] REPLACED ASSIST HANDLE ASSY AFT SERVICE DOORWAY AT AFT GALLEY AREA IAW B737-700 AMM 25-21-25-420-801 STEP 3.B.(5);[02] TASK CARD COMPLETE.SDR SWAA2025011575695Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED STA540 AND RBL1 PASSENGER CABIN 2024-759431<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATED STA540 AND RBL1 PASSENGER CABIN IAW B737-700 SRM 51-10-02; ITEP 9 AND DWG 143A0060; SHEET 44; REV A.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[0SDR SWAA2025011575703Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED STA540 AND LBL1 PASSENGER CABIN 2024-759432<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATED STA540 AND LBL1 PASSENGER CABIN IAW B737-700 SRM 51-10-02; ITEM 9 AND DWG 143A0060; SHEET 44; REV A.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[0SDR SWAA2025011575911Filler · corrodedCORROSION ON TAPERED FILLER LOCATED ON BS344 LOWER SURFACE OF STR26R AT E/E COMPARTMENT 2024-759461<[01] REPLACED TAPERED FILLER AND FASTENERS LOCATED ON BS344 LOWER SURFACE OF STR26R AT E/E COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 DWG 141A3502 SHEET 51 RESDR SWAA2025011575899Support Bracket · crackedCRACK SUPPORT BRACKET KRUEGER FLAP INTERNAL AREA LOCATED IFSS152 AT LT WING 2024-759460<[01] REPLACED SUPPORT BRACKET KRUEGER FLAP INTERNAL AREA LOCATED IFSS152 AT LT WING IAW B737-700 SRM 51-40-02;[02] COMPLETED TASK CERTIFIEDSDR SWAA2025011575290Skin · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING 2024-759336<[01] TOOL USED CALIPER PN: 500-196-30; SN: A23325649; DUE DATE: 31/DEC/24.;[02] TOOL USED CALIPER PN: 500-197-30; SN: A189508; DUE DATE: 14/JAN/25.;[03] CORRECTIVE ACTIONSDR SWAA2025011575114Fitting · crackedCRACK INDICATION FOUND IN UPPER BOLT HOLE LOCATED ON BS 727 FRAME INNER CHORD AREA AT S-18 A RH SIDE; CRACK DIRECTION: 3 OCLOCK. 2024-759236<[01] TOOL USED ON STEP 2 EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 60009161631 DUE DATE: 11-MAR-25;[02] ACOMPLISHED ESDR SWAA2025011575292Skin · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT RT WING. TOOL USED: POSITECTOR PN: NS2; SN: 110098; DUE DATE: 05/SEP/25.<BR>TOOL USED: HOT BONDER PN: HCS9200B-AV; SN: 18185733; DUE DATE: 25/JAN/25.;[02] TOOL USED ON STEP 11 ULTRASONIC FLSDR SWAA2025011575047Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2024-759209<[01] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7902; SHEET: 174; REV-. SEE INDIVIDUAL SIGN-OFF BELOW.;[02]SDR SWAA2025011575046Gusset · crackedCRACK GUSSET LOCATED STA500D AND STR19R FWD CARGO COMPARTMENT 2024-759210<[01] REPLACED GUSSET LOCATED STA500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7902; SHEET: 174; REV-. SEE INDIVIDUAL SIGN-OFF BELOW.;[0SDR SWAA2024111861144Module · faultyANTI SKID INOP LIGHT ILLUMINATED INFLIGHT. 32-44-21-000-801. OK TO CONTINUE PER MEL 32-2-01 SP1+SP2. PERFORMED AACU BITE CHECK PER FIM 32-42 TASK 801. FAULT BOX 1-4. PERFORMED RESISTANCE CHECK OF NORM ANTI-SKID VALVES 1-4 PER FIM 32-42 TASK 804. ALT ANTI-SKSDR SWAA2024111868440Control Unit · faultyANTI SKID INOP LIGHT ILLUMINATED INFLIGHT. 32-44-21-000-801<[01] OK TO CONTINUE PER MEL 32-2-01 SP1+SP2;[02] PERFORMED AACU BITE CHECK PER FIM 32-42 TASK 801. FAULT ? BOX 1-4?. PERFORMED RESISTANCE CHECK OF NORM ANTI-SKID VALVES 1-4 PER FIM 32-42 TASK 804. ALTSDR SWAA2024111868441Anti-Skid Valve · faultyANTI SKID INOP LIGHT ILLUMINATED INFLIGHT. 32-44-21-000-801<[01] OK TO CONTINUE PER MEL 32-2-01 SP1+SP2;[02] PERFORMED AACU BITE CHECK PER FIM 32-42 TASK 801. FAULT ? BOX 1-4?. PERFORMED RESISTANCE CHECK OF NORM ANTI-SKID VALVES 1-4 PER FIM 32-42 TASK 804. ALT
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