Boeing 737-73V
Service difficulty reports · 1,826
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 = '73773V' 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 = '73773V' 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 SWAA2022021668985Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2022-58310 / [01] REPAIRED BY WELDS AFT CORNER SCUFF PLATE OF FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1; REPAIR 1 PARAGRAPH 4.B. STEPS ( 2 ) TO ( 7 ) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BSDR SWAA2022020265510Panel · cracked193D PANEL HAS TWO FASTENER HOLE WITH CRACKS EMANATING FROM HOLES.(MARKED) / [01] REPLACED PANEL 193D; REF AMM 53-51-21; TSR 202200756SDR SWAA2022020265511Panel · cracked194E PANEL HAS TWO FASTENER HOLES WITH CRACKS EMANATING FROM HOLES. (MARKED) / [01] INSTALLED NEW PANEL IAW 53-51-21. REF TSR 202200756SDR SWAA2022021663788Light · missingMISSING STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 335.25 TO STA 663 RT SIDE AT PASSENGER CABIN (10 EA) 2022-58154 / [01] INSTALLED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 335.25 TO STA 663 RT SIDE AT PASSENGER CABISDR SWAA2022021663789Light · missingMISSING STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 663 TO STA 953 RT SIDE AT PASSENGER CABIN (10 EA) 2022-58155 / [01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 663 TO STA 953 RT SIDE AT PASSENGER CABIN (10 ESDR SWAA2022021663790Light · missingMISSING STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 335.25 TO STA 663 LT SIDE AT PASSENGER CABIN (10 EA) 2022-58157 / [01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 335.25 TO STA 663 LT SIDE AT PASSENGER CABINSDR SWAA2022021663791Light · missingMISSING STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 663 TO STA 953 LT SIDE AT PASSENGER CABIN (10 EA) 2022-58159 / [01] INSTALLED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 663 TO STA 953 LT SIDE AT PASSENGER CABIN (10 SDR SWAA2022021663347Stringer · crackedCRACK STRINGER 26L LOCATED BS.540 AT FWD CARGO COMPARTMENT 2022-58135 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 03-FEB-22; TEMPERATURE CONSDR SWAA2022021663348Stringer · crackedCRACK STRINGER 27L LOCATED BS. 540 AT FWD CARGO COMPARTMENT 2022-58136 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 03-FEB-22; TEMPERATURE COSDR SWAA2022021663352Stringer · crackedCRACK STRINGER 27R LOCATED BS. 540 AT FWD CARGO COMPARTMENT 2022-58137 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] CORRECT STEP: NOMINAL THICKNESS IS: 0.056? PER NDT MANUAL 51-00-00 PART 4; PROCEDURE 3.;[03] TOOL USED THICSDR SWAA2022021663351Stringer · crackedCRACK STRINGER 25R LOCATED BS. 540 AT FWD CARGO COMPARTMENT 2022-58138 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-22; TEMPERATURE COSDR SWAA2022021663353Stringer · crackedCRACK STRINGER 26R LOCATED BS540 FWD CARGO COMPARTMENT 2022-58140 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-22; TEMPERATURE CONTROLSDR SWAA2022021663335Panel · crackedCRACK ACCESS PANEL 194E BODY FAIRING AROUND HOLES AT LOWER FUSELAGE 2022-58095 / [01] TOOL USED CALIPER P/N 500-464 S/N 15331932 DUE DATE 26/OCT/22.;[02] TOOL USED HOTBONDER P/N HCS9200B S/N 18175478 DUE DATE 05-AUG-22;[03] TOOL USED SCALE P/N: CL5000 S/N: AE-SDR SWAA2022021763342Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION ; 2022-58102 / REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02 PART SDR SWAA2022021772410Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION 2022-58102 / [01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02 PASDR SWAA2022021872408Support Bracket · crackedCRACK LEADING EDGE SUPPORT BRACKET LOCATED AT BS 1016 BETWEEN S-2R AND S-2L AT VERTICAL STABILIZER 2022-58053 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.;[02] REPLACED SUPPORT BRACKET (SPRING) AND FASTENERSDR SWAA2022021663007Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 693 AT BL 0 AT PASSENGER CABIN 2022-58012 / [01] REPLACED ANGLE AND FASTENERS LOCATED ON BS 693 AT BL 0 AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 273A9110 REV. A SEE INDIVIDUAL SIGN OFFSDR SWAA2022021663008Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 690 AT BL 0 AT PASSENGER CABIN 2022-58007. REPLACED ANGLE LOC. ON FLOOR STRUCTURE BS 690 AT BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 273A9110 REV. A;[03] CORRECTED STEP 2: REPLACESDR SWAA2022021763323Support Bracket · crackedCRACK LEADING EDGE SUPPORT BRACKET LOCATED AT BS 1016 BETWEEN S-2R AND S-2L AT VERTICAL STABILIZER ; 2022-58053 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.; [02] REPLACED SUPPORT BRACKET (SPRING) AND FASTESDR SWAA2022012562831Flap System · failedON APPROCH FLAPS STOPPED AT 25 NO ASSYBELLY BRAKE FLAG / [01] CHECKED FSEU FOR FAULTS NO CURRENT FAULTS NOTED PERFORMED AMM 27-51-00 AND FIM 27-51 TASK 836 AS REQ. SYSTEM OOPS CK NORMAL AT THIS TIME COULD NOT DUPLICATESDR SWAA2022012462873Seal Plate · crackedCRACK SEAL - PLATE ACCESS PANEL 333AT AT LT HORIZONTAL STAB. REPLACED THE SEAL PLATE ACCESS PANEL 333AT IAW SRM 51-10-02 ITEM 9 AND 51-40-02.SDR SWAA2022012462877Seal Plate · crackedCRACK SEAL - PLATE ACCESS PANEL 343AT AT RT HORIZONTAL STAB. REPLACED THE SEAL PLATE ACCESS PANEL 343AT IAW SRM 51-10-02 ITEM 9 AND 51-40-02.SDR SWAA2022011360711Panel · elongated193 B PANEL HAS 2 EACH OBLONG FASTERNER HOLES ON PANEL #33 AND #34 PANEL NEEDS TO BE CHANGED ; 193 B PANEL HAS 2 EACH OLONG FASTERNER HOLES ON PANEL #33 AND #34 PANEL NEEDS TO E CHANGED / [01] R&R 193 PANEL REF. SRM 51-40-02SDR SWAA2022011260724Light · inoperativeEMERGENCY EXIT LIGHTS AT L1 EXTERIOR AND R1 INTERIOR ARE INOP. / [01] REMOVED AND REPLACED BATTERY PACK AT FWD LEFT LOCATION. REF AMM 33-51-06. OP CHK GOOD.SDR SWAA2021110138234Sensor · fluctuatesON APPROACH WHEN PLACING THE FLAPS TO 15; THE LE FLAPS TRANSIT AND LE FLAPS EXT FLUCTUATED BETWEEN THE TWO LIGHTS. OVERHEAD LE DEVICES FLAPS ILLUMINATED ALL GREEN .AIRSPEED LOW AURAL AND SLOW SPEED ; RED FOOTER FLCTATED WITH ARAL WARNING. / [01] R&R LEADING EDSDR SWAA2021101228624Slide · missingCREW REPORTS FROWARD SERVICE DOOR EMERGENCY SLIDE FELL OUT ; / [01] REPACKED FS SLIDE PER MT725-61-06 AND AMM 25-66-01SDR SWAA2021100827412Girt Bar · out of adjustFA REPORTS FWD SERVICE DOOR GIRT BAR HARD TO INSERT AND RELEASE ; / [01] ADJUSTED GIRT BAR TENSION AS PER SIPSDR SWAA2021090212712Frame · damagedREJECT- TOP FASTENER HOLE AT O/B FLANGE COMMON TO BS 500A FRAME IS ELONGATED AT FRAME REPAIR STR 7R - STR 10R ; / [01] DRILLED OVERZISE HOLE .216 FINAL SIZE AT TOP FASTENER HOLE AT O/B FLANGE COMMON TO BS 500A FRAME PER SRM 51-40-05; [02] VERIFIED CORRECTIVE ASDR SWAA2021090312705Bear Strap · crackedAMOC NEEDED FOR CRACK ON THE BEAR STRAP AT THE FWD UPPER CORNER OF THE FWD GALLEY DOORWAY CUTOUT; BS 294.5 ABOVE STR 9R ; / [01] DAMAGE REPAIRED PER EA 21-153-02498 (737-700 SRM 53-10-01-2R-6; REPAIR 6). REPETITIVE INSPECTION PROGRAM DEFINED IN EA 21-153-02498SDR SWAA2021090212014Lens · missingLAV A EMERGENCY EXIT LIGHT LENS IS MISSING. / [01] REPLACED LAV A LIGHT LENS IAW AMM 33-51-01-960-802; [02] VERIFIED REPLACED LAV A LIGHT LENS IAW AMM 33-51-01-960-802SDR SWAA2021090212015Connector · not seatedLEFT OVER WING EMERGENCY EXIT LIGHT IS INOP. / [01] RESEATED CONNECTOR D11078 AT OVER WING EMERGENCY EXIT LIGHT IAW SWPM 20-61-28. PERFORMED GOOD TEST IAW AMM 33-51-00-710-801.; [02] VERIFIED CORRECTIVE ACTION #1.; [03] VERIFIED TASK IS COMPLETE.SDR SWAA2021090210794Power Supply · no testEMERGENCY EXIT LIGHTS ASSOCIATED WITH M1668 ARE OUT ; / [01] UPDATED PART INFORMATION; [02] REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY M1668 AND PERFORMED GOOD TEST OF NEW POWER SUPPLY PER AMM 33-51-06-960-806.; [03] VERIFIED STEP 2; [04] VERIFIED CORRSDR SWAA2021090308811Baffle · crackedFWD CARGO BAY BAFFLE IS CRACKED; BS 400-420; LBL 24; WL 154 ; / [01] LOCATED AND DRILLED (OVERSIZED ALL HOLES TO NEXT DIAMETER) NEW FWD CARGO BAY BAFFLE BS400-420; LBL 24; WL 154. PER SRM 51-40-02-0G-0 STEP 4. D. (2); BOEING DWG: 143A7505; AND SRM 51-40-05. <BSDR SWAA2021090207675Attach Angle · crackedFRAME ATTACH ANGLE AT BS 807 RBL 21 COMMON TO THRESHOLD VERTICAL WEB IS CRACKED ; / [01] REMOVED FROM FRAME ATTACH ANGLE AT BS 807 RBL 21 COMMON TO THRESHOLD VERTICAL WEB IAW SRM 51-40-02-0G-0 . PART NO HAVE ENTRIES ALLOWABLE DAMAGE IN SRM ; MUST BE REPAIRED BSDR SWAA2021090307285Skin · corrodedCORROSION AROUND ADF ANTENNA MOUNTING FASTENERS HOLES. BS 694; RBL 4.8 WL 308.25. ; / [01] REMOVED CORROSION AROUND ADF ANTENNA MOUNTING FASTENERS HOLES L=1 W=1 PER REF SRM 53-00-01-1A -1 AND ARM90-7023-01; [02] VERIFIED DAMAGE REMOVED; L=32.5 W=1; PER SRM 53-SDR SWAA2021090306406Frame · damagedDAMAGE REMOVAL CUT EXTENDED INTO FRAME I/B FLANGE RADIUS AT BS 500A; STR-8R ; / [01] REPAIRED BS 500A FRAME AT STR 8 R/H IAW EA 21-153-02349; [02] COMPLETE; [03] VERIFIED COMPLETESDR SWAA2021090305896Support Angle · crackedCRACKED VERTICAL SUPPORT ANGLE ON AFT SIDE OF B.S. 663 LOWER COMPOSITE BULKHEAD AT L.B.L. 26; W.L. 150. ; / REMOVED VERTICAL SUPPORT ANGLE AFT SIDE BS 663 LOWER BULKHEAD LBL 26; WL 150 PER SRM 51-40-02; DAMAGE FOUND ON VERTICAL SUPPORT ANGLE ON AFT SIDE OF BS6SDR SWAA2021081605794Retainer · out of adjustFWD SERVICE GIRT BAR FALLS OUT OF CLIPS ; / [01] INSPECTED BAR CLIPS & NO DAMAGE NOTED. ADJUSTED CLIPS PER SIPSDR SWAA2021090304845Support · crackedBAFFLE UNDER FLOOR TO SIDEWALL SUPPORT IS CRACKED; FWD CARGO BAY BS 500A-500B; RBL 24; WL 154 ; / [01] FOUND THERE TO BE NO ALLOWABLE DAMAGE FOR THIS PART THEREFOR IT IS ONLY REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-O STEP 9.; [02] REMOVED BAFFLE UNDER FLSDR SWAA2021090303915Plate · crackedRIGHT HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE IS CRACKED. ; / [01] REMOVED AND REPLACED RIGHT HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE PER AMM 53-31-31-000-802 AND AMM 53-31-31-400-802; [02] INSPECTION COMPLETESDR SWAA2021090303908Panel · damagedPANEL 194 BR LOWER CENTER FASTENER HOLE ELONGATED ; PANEL 194BR LOWER CENTER FASTENER HOLE ELONGATED / DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-60-70-1A-1 PAR 4. REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05-2R-9 PER SRM 53-60-70-2R-1 PAR 4B(3).;SDR SWAA2021090203913Hook · corrodedRIGHT HAND EMERGENCY EXIT HATCH ESCAPE STRAP HOOK IS CORRODED. ; / [01] REMOVED AND REPLACED RIGHT HAND EMERGENCY EXIT HATCH ESCAPE STRAP. IAW AMM 25-61-10-000-802 AND AMM 25-61-10-400-802.; [02] VERIFIED REPLACEMENT OF R/H OWE HATCH ESCAPE STRAP PER AMM 25-61SDR SWAA2021090203914Strap · corrodedLEFT HAND EMERGENCY EXIT HATCH ESCAPE STRAP HOOK IS CORRODED. ; / [01] REMOVED AND REPLACED LEFT HAND EMERGENCY EXIT HATCH ESCAPE STRAP. IAW AMM 25-61-10-000-802 AND AMM 25-61-10-400-802; [02] VERIFIED REPLACEMENT OF L/H OWE HATCH ESCAPE STRAP PER AMM 25-61-10SDR SWAA2021090203917Stringer Clip · chafedP18 PANEL ATTACH CLIP IS CHAFED AT STRINGER 6 LEFT; B.S. 262. ; / [01] REMOVED CLIP LOCATED AT BS. 262 STR6L IAW 51-40-02 AND SRM 51-20-02 ITEM 9.C MUST BE REPAIRED BY REPLACEMENT NO ENTRIES EN SRM .; [02] FABRICATED CLIP FROM MATERIAL 6013T4. BARE 0.050' LOT.SDR SWAA2021080903912Hook · corrodedLEFT HAND EMERGENCY EXIT HATCH ESCAPE STRAP HOOK IS CORRODED. ; / [01] FAULT WILL BE RESOLVED ON FAULT TTG8Q0061VHR.; [02] VERIFIED FAULT WILL BE RESOLVED ON FAULT TTG8Q0061VHR.SDR SWAA2021090303506Support · crackedCRACKED INTERCOSTAL AT AFT PASSENGER CABIN BS943 BL0 WL208. ; / [01] REMOVED INTERCOSTAL AY BS 943 BL 0 WL 208 PER SRM 51-40-02-GO-0; [02] EVALUATED CRACK ON INTERCOSTAL AT AFT PASSENGER CABIN BS 943 BL0 WL208 AND FOUND OUT OF LIMITS IAW SRM 53-70-51-1A-1 PAR.SDR SWAA2021090303503Channel · corrodedCORROSION ON MOP SILL AT AFT PASSENGER CABIN BS951-BS991 LBL49 WL208. ; / REMOVED CORROSION ON AFT PASSENGER CABIN MOP SILL BS 951 - BS 991 LBL 49 WL 208 MAX. MAT. LOSS 6' X 3' X .012' ORIGINAL THICKNESS .080' FOUND TO BE OUT OF LIMITS I.A.W. SRM 53-70-15-1A-]SDR SWAA2021090303502Strap · corrodedCORROSION ON TENSION STRAP AT AFT PASSENGER CABIN BS1026 RBL3 WL208. ; / [01] VERIFIED NO ALLOWABLE DAMAGE PARTS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARAGRAPH 9C.; [02] CORRECTED MEASUREMENT; [03] VERIFIED CORRECSDR SWAA2021090303494Support · damagedPNEUMATIC DUCT CLAMP SUPPORT HAS ELONGATED MOUNT HOLE AT INBOARD FRONT SPAR STATION 151 ON LEFT WING INBOARD FRONT SPAR. ; / [01] REMOVED AND REPLACED PNEUMATIC DUCT CLAMP SUPPORT AT INBOARD FRONT SPAR STA.151 ON LEFT WING INBOARD SPAR IAW: <BR>AMM 36-13-01-00SDR SWAA2021090203507Support · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS317 RBL31 WL208. ; / [01] VERIFIED APPLICABILITY OF SRM 53-10-51-0I-2 FOR IDENTIFICATION AND NO FOUND ALLOWABLE DAMAGE FOR THIS PART. REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; PAR.9.C.; [02] VERIFIED APPLICABILITY O
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