JASC 5720
Service difficulty reports · 13,638
Reports filed under 5720 · Wing Miscellaneous Structure, 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 jasc_code = '5720' 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 jasc_code = '5720' 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 IPXA2022012078082Skin · corrodedINSPECTION TYPE:1CR/H WING UPPER SKIN HAS CORROSION AT STA. XORS= 1006 & XORS=1012 AT STR. 4.REPAIRED CORRODED R/H WING SKIN IAW VT-SAA EA 011-5730-01-A9453 AND UPS EO MD11-5730-82592-A. (MINOR)SDR IPXA2022011978029Skin · noneINSPECTION TYPE:1CRT O/B WING L/E UPPER SKIN SURFACE GOUGE O/B OF #8 SLAT.REPAIRED RT WING L/E GOUGE SKIN IAW SRM 57-40-01 REPAIR 16 (MINOR).SDR SWAA2022012458103Winglet · corrodedRIGHT WINGLET; SURFACE CORROSION ON LOWER STRAKE AFT TRAILING EDGE (BOTH SIDES) ; / [01] R&R R/H LWR STRAKE PER APB SUPPLEMENT AMM DOCUMENT NUMBER AP37.8-0618 57-31-02. FINAL INSTALL WILL BE ACCOMPLISHED ON FAULT #TTG8R007GSE4 LINE 911; [02] N/A MEASUREMENTS DSDR SWAA2022021457753Support · corrodedCORROSION WINGLET SUPPORT PLATE LOCATED LOWER SURFACE AFT POSITION AT LT WING ; 2021-585057 / [01] REPLACED WINGLET SUPPORT PLATE LOCATED LOWER SURFACE AFT POSITION AT LT WING IAW B737-700 SRM 51-40-02; [02] COMPLETE TASK CERTIFIEDSDR SWAA2022013156777Plate · crackedLT WING WAFFLE PLATE CRACKED I/B #3 FLAP TRACK ; / [01] REMOVED FASTENERS PER SRM 51-40-02; [02] REMOVED AND REPLACED PER SRM 51-40-02.; [03] INSPECTION C/W R@R OF WAFFLE PLATE PER SRM 51-40-02SDR SWAA2022013156781Support · crackedLT WING I/B UPPER WING ROOT PANEL SUPPORT CLIP CRACKED ABOVE TANK 1 BOOST PUMP ; / [01] R/R SUPPORT CLIP PER SRM 51-40-02SDR SWAA2022013155876Angle · crackedCRACK TRAILING EDGE SUPPORT ANGLE LOCATED ON ORSS 273 AT RT WING ; 2021-577400 / [01] REPLACED TRAILING EDGE SUPPORT ANGLE LOCATED ON ORSS 273 AT RT WING IAW SRM B737-700 51-10-02 ITEM 9 AND SRM B737-700 51-40-02; [02] TASK CARD COMPLETEDSDR SWAA2021122755277Angle · crackedRIGHT WING FIXED PANEL LOWER SURFACE HAS CRACK IN SUPPORT WEB ANGLE. ; / [01] REMOVED BULKHEAD ASSEMBLY (REF IPC 57-50-00-25 ITEM 10) AND WEB (REF IPC 57-50-00-25 ITEM 290) REF SRM 51-40-02. ALL REMOVED HARDWARE IS BAGGED AND LABELED WITH ASSOCIATED REMOVED COSDR SWAA2022013155361Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 273 LT WING ; 2021-577248 / [01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 273 LT WING IAW B7E7-700 SRM 51-10-02 ITEM 9;SRM 51-40-02 AND DWG 115A2930 REV.-SEE INDIVIDUAL SIGN-OFFS BELOW; [02] REPLACED ANGLE TRAILING EDGE SDR SWAA2021122755020Web · crackedRH WING TRAILING EDGE DEFLECTION RIB/PANEL SUPPORT WEB CRACKED AT OUTBOARD FASTENER. ; / [01] REMOVED AND REPLACED SUPPORT WEB REF SRM 51-40-02.SDR MASA20211221638Panel · noneA MISS DERILLED HOLE WAS FOUND ON THE RH OUTBOARD LEADING EDGE ACESS PANEL #632EB. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 57-42-32-991-801, 29A (REV 38 DATED 9 JUL 2021). PANEL/LE INBD RH PANEL #632EBSDR SWAA2022012454177Attach Bracket · crackedPNEUMATIC DUCT TIE ROD SUPPORT ATTACH POINT BRACKET AT BS 540 LBL 58 IS CRACKED ; / [01] REMOVAL OF PNEUMATIC DUCT TIE ROD SUPPORT ATTACH BRACKET AT B.S. 540 LBL 58 ACCOMPLISHED ON CUSTOMER CARD NUMBER TTG8Q009Y54G; [02] RECIEVED NEW PNEUMATIC DUCT TIE ROD SUPSDR SWAA2021122053483Angle · crackedSUPPLEMENTAL INFORMATION: BS 663; RBL 33; WL 194; .200' CRACK AT FASTENER HOLE ON 663 BULKHEAD TO CENTER WING BOX UPPER SKIN ATTACH ANGLE; END OF CRACK MARKED IN BLACK. ; / [01] CUT AND REMOVED DAMAGE IAW SRM 57-10-10-2R-6 REPAIR 6; [02] -1 FILLER MATERIAL VERSDR SWAA2022011253153Angle · crackedRIGHT WING; 20' INBOARD OF DEFLECTION CONTROL RIB; ATTACH ANGLE TO PANEL SUPPORT IS CRACKED. A045-003 ; / [01] REMOVED ANGLE IAW SRM 51-40-02.; [02] LOCATED & DRILLED FASTENER HOLES IN NEW ANGLE; 115A2156-18 A TAG # A107454; IAW SRM 51-40-05.; [03] INSTALLED NSDR SWAA2022011253146Angle · crackedL/H WING FIXED T/E; ATTACHED TO INBD SIDE OF DEFLECTOR CONTROL RIB; PANEL SUPPORT L-ANGLE CRACKED. DOT 224-006 ; / [01] REMOVED L-ANGLE IAW SRM 51-40-02-0G-0; [02] INSTALLED NEW L-ANGLE IAW SRM 51-40-02-0G-0 AND IPC 57-42-51-03; [03] VERIFIED STEP 2.SDR SWAA2022011253157Angle · crackedL/H WING FIXED T/E AT OTBD EDGE OF #6 SPOILER; PANEL SUPPORT IS CRACKED. A224-007 ; / [01] REMOVED PANEL SUPPORT IAW SRM 51-40-02-0G-0; [02] LOCATED & DRILLED NEW ANGLE 115A2156-17 / A TAG # A107452 IAW SRM 51-40-05.; [03] VERIFIED STEP 2; [04] INSTALLED ANGLESDR SWAA2022011352783Attach Angle · crackedRIGHT WING; DEFLECTION CONTROL RIB; INBOARD ATTACH ANGLE TO WEB IS CRACKED AT FASTENER HOLES COMMON TO DEFLECTION CONTROL RIB. A045-006 ; / [01] REMOVED AND REPLACED R/W DEFLECTION RIB INBD ATTCH ANGLE IAW DWG 115A6200 REV:A SRM 51-40-02-OG-O; [02] REMOVED ANDSDR SWAA2021122751776Clevis · crackedSUPPLEMENTAL INFORMATION: LH ACM ROD ATTACHMENT CLEVIS CRACKED AND BROKEN ; / [01] LH ACM REMOVED ON TTG8Q009GE9D; [02] MEASUREMENTS; [03] PREPARED SERVICABLE L/H ACM PER AMM 21-51-09-400-801 STEPS 3.A.-F.(1)(2)(A)-(D); (J)-(M) AND AMM 21-51-04-400-801-001 STESDR SWAA2021122350679Access Panel · corrodedCORROSION ACCESS PANEL 532PB ON CLAMP RING AT LT WING (1) ; 2021-520755 / [01] PERFORMED PERMANENT REPAIR ON CLAMP RING ACCESS PANEL 532PB LT WING IAW B737-700 SRM 51-20-01-2R-1 REPAIR 1; [02] CORRECTED STEP 1 PERFORMED REPAIR ON CLAMP RING ACCESS PANEL 532PB SDR SWAA2021122350680Access Panel · corrodedCORROSION ACCESS PANEL 532QB ON CLAMP RING AT LT WING ; 2021-520756 / [01] PERFORMED PERMANENT REPAIR ON CLAMP RING ACCESS PANEL 532QB LT WING IAW B737-700 SRM 51-20-01-2R-1 REPAIR 1; [02] PERFORMED REPAIR ON CLAMP RING ACCESS PANEL 532QB LT WING IAW B737-700 SDR SWAA2022010550229Access Panel · crackedSUPPLEMENTAL INFORMATION: CRACK ACCESS PANEL 651GB CORRUGATED PLATE AT RT WING ; 2021-549847 / [01] REPLACED CORRUGATED PLATE ON ACCESS PANEL 651GB AT RT WING. I.A.W B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A2001 REV:A SHEET 7; [02] INSTALLED CORRUGATSDR SWAA2022010549598Access Panel · crackedSUPPLEMENTAL INFORMATION: CRACK ACCESS PANEL 532NB FUEL TANK FLOAT AT LT WING ; 2021-549811 / [01] FAULT RESOLVED ON OTHER FAULT REPLACED FUEL TANK FLOAT ON ACCESS PANEL 532NB AT LT WING ON TTG8Q009MYPM; [02] TASK CARD COMPLETEDSDR SWAA2022010549024Plate · brokenBROKEN TRAILING EDGE CORRUGATED PLATE LOCATED WS180.00 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING ; 2021-549676 / [01] REPLACED CORRUGATED PLATE LOCATED WS180.00 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING. I.A.W B737-700 SRM 51-40-02; 51-10-02 ITEM 9 ASDR SWAA2022010549025Plate · brokenBROKEN TRAILING EDGE CORRUGATED PLATE LOCATED WS204.25 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING ; 2021-549674 / [01] REPLACED CORRUGATED PLATE LOCATED WS204.25 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING. IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 ANDSDR SWAA2022010549030Bracket · brokenBROKEN SUPPORT BRACKET LOCATED IRSS140 REAR SPAR UPPER AREA AT LT WING ; 2021-549710 / [01] REPLACED SUPPORT BRACKET LOCATED IRSS140 REAR SPAR UPPER AREA AT LT WING IAW B737-700 SRM 51-10-02-0G-0 STEP 9; [02] TASK COMPLETEDSDR SWAA2022010549032Angle · brokenBROKEN ANGLE TRAILING EDGE LOCATED ORSS174 REAR SPAR UPPER AREA AT RT WING ; 2021-549722 / [01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS174 REAR SPAR UPPER AREA AT RT WING I.A.W B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 SEE INDIVIDUAL SIGNOFFS BELOW.SDR SWAA2021122048830Panel · crackedDURANT OK TO CLOSE FOUND PANEL 651BB CRACKED AT INTERNAL SURFACE ; / [01] CLANER AND PREPAIRED FOR REPAIR FOUND PANEL 651 BB AS PER B737-700 SRM 51-70-04-2R-1; [02] CLEANED AND PREPPED FOR REPAIR NEEDED ON PANEL 651BB AS PER B737-700 SRM 51-70-04-2R-1; [03] VESDR SWAA2022010348527Bracket · crackedSUPPLEMENTAL INFORMATION: CRACK SUPPORT BRACKET ON ACCESS PANEL 551GB AT LT WING ; 2021-544618. / [01] REPLACED SUPPORT BRACKET ON ACCESS PANEL 551GB AT LT WING IAW SRM 51-40-02-0G-0.; [02] REPLACED SUPPORT BRACKET ON ACCESS PANEL 551GB AT LT WING IAW SRM 51-4SDR SWAA2022010548688Access Panel · crackedCRACK ACCESS PANEL 561BB HOLES AT LT WING ; 2021-549549 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: 15331932; DUE DATE: 26-OCT-22; [02] HOT BONDER PN: HCS9200B-AV; SN: 18196021; DUE DATE: 14/DEC/21.; [03] SCALE P/N: 1863T62; S/N: AE-40571; DUE DATE: 19-MAY-22SDR SWAA2021122248561Angle · crackedCABIN CENTER SECTION FLOOR PANEL BRAKE ASSY. SUPPORT ANGLE IS CRACKED AT F.S. 540 BETWEEN #2 SEAT TRACK AND CENTER BEAM BL.0 ; / [01] REMOVED AND REPLACED SUPPORT ANGLE AT STA 540 BETWEEN #2 SEAT TRACK AND BL ZERO PER SRM 51-40-02.SDR SWAA2022010353613Access Panel · corrodedPITTING ON ACCESS PANEL 532HB FUEL TANK CLAMP RING AT LT WING ; 2021-544610. / [01] REPLACED ACCESS PANEL 532HB FUEL TANK CLAMP RING AT LT WING I.A.W B7373-700 SRM 51-10-02-0G-0 PARAGRAPH 9; SEE INDIVIDUAL SIGNOFFS BELOW; [02] REPLACED ACCESS PANEL 532HB FUEL SDR SWAA2022010548031Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT ORSS 261 APPROX AT LT WING ; 2021-536697 / [01] REPLACED CORRUGATED PLATE AND FASTENERS LOC TRAILING EDGE LOCATED AT ORSS 261 APPROX AT LT WING IAW B737-700 SRM 51-40-02 AND 51-10-02.; [02] REPLACED CORRUGATED PLSDR SWAA2022010548032Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED AT ORSS 270 APPROX INTERNAL CABITY AT LT WING ; 2021-536695 / [01] REPLACED ANGLE (FITTING) TRAILING EDGE LOCATED AT ORSS 270 APPROX INTERNAL CABITY AT LT WING IAW SRM B737-700 51-40-02 AND 51-10-02; [02] JOB COMPLETED.SDR SWAA2022010548033Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED AT ORSS 270 APPROX AT LT WING ; 2021-536694 / [01] REPLACED ANGLE TRAILING EDGE (WEB) LOCATED AT ORSS 270 APPROX AT LT WING IAW SRM B737-70O 51-40-02 AND 51-10-02; [02] REPLACED ANGLE TRAILING EDGE (WEB) LOCATED AT ORSS 270 APSDR SWAA2022010548035Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED AT ORSS 280 APPROX INTERNAL CABITY AT LT WING ; 2021-536696 / [01] REPLACED ANGLE AND FASTENER; TRAILING EDGE LOCATED AT ORSS 280 APPROX INTERNAL CABITY AT LT WING IAW B737-700 SRM 51-40-02.SDR SWAA2022010348082Bracket · crackedSUPPLEMENTAL INFORMATION: CRACK SUPPORT BRACKET LOCATED TRAILING EDGE ORSS 273 AT LT WING ; 2021-544514 / [01] REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE ORSS 273 AT LT WING DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS. IAW B737-700 SRM 51-10-02 ITEM 9 AND SRMSDR SWAA2022010348080Plate · crackedSUPPLEMENTAL INFORMATION: CRACK CORRUGATED PLATE TRAILING EDGE LOCATED WS 204.25 AT LT WING ; 2021-544509 / [01] REMOVED AND REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED WS 204.25 AT LT WING; IAW B737-700 SRM 51-10-02 AND SRM B737-700 51-40-02; LENGHT OF CRSDR SWAA2022010347877Plate · crackedSUPPLEMENTAL INFORMATION: CRACK CORRUGATED PLATE TRAILING EDGE LOCATED WS 228.25 AT RT WING ; 2021-544437 / [01] REMOVED AND REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED WS 228.25 AT RT WING IAW B737-700 SRM 51-10-02 AND SRM B737-700 51-40-02; LENGHT OF CRASDR SWAA2022010347897Plate · crackedRT WING T/E WIGGLE PLATE CRACKED INBD OF #6 FLAP TRACK. REMOVED AND REPLACE WITH NEW WIGGLE PLATE ASSAY. PER SRM 51-40-02SDR SWAA2022010547683Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 279 APPROX AT RT WING ; 2021-536607 / [01] REPLACED ANGLE AND FASTENER TRAILING EDGE LOCATED ORSS 279 APPROX AT RT WING; IAW B737-700 SRM 51-40-02; AND TOOL USED CALIPER P/N 500-196-30; S/N: A20226522; DUE DATE: 11-AUG-22SDR SWAA2022010355977Angle · crackedCRACK ANGLE TRAILING EDGE BETWEEN WS 253.00 AND WS 278.50 AT RT WING ; 2021-544262 / [01] REPLACED ANGLE TRAILING EDGE BETWEEN WS 253.00 AND WS 278.50 AT RT WING AND FASTENERS. I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A3758 REV - . SEE INDIVIDUAL SIGN OFFSDR SWAA2022010547389Plate · crackedCRACK ON CORRUGATED PLATE LOCATED ORSS 297 TRAILING EDGE AREA ACCESS PANEL 661AB AT RT WING ; 2021-536492 / [01] REPLACED CORRUGATED PLATE LOCATED ORSS 297 TRAILING EDGE AREA ACCESS PANEL 661AB AT RT WING IAW SRM B737-700 51-40-02 AND DRAWING 115A3700 REV:-; [SDR SWAA2021112947963Fitting · corrodedSUPPLEMENTAL INFORMATION: RIGHT WING PICKLE FORK KICK FITTING HAS CORROSION AROUND BUSHING ON INBOARD SIDE. / REQUEST NDI TO VERIFY CRACK FREE ON REMOVED BUSHING ON L/H KICK FITING PER SOPM 20-50-03 CORRECTION TO STEP 1 REMOVAL OF BUSHING IS ON R/H PER SOPM 20SDR SWAA2022010347234Access Panel · delaminatedSUPPLEMENTAL INFORMATION: DELAMINATED ACCESS PANEL 621DB LEADING EDGE AT RT WING ; 2021-544057 / [01] TOOL USED: CALIPER P/N 500-197-30 S/N A18229508 DUE DATE: 29-SEP-22.; [02] TOOL USED SCALE P/N:CL5000; S/N:AE-408753; DUE DATE:19-MAR-22.; [03] TOOL USED HOTBSDR SWAA2022010347047Access Panel · delaminatedSUPPLEMENTAL INFORMATION: DELAMINATED ACCESS PANEL 521DB AT LT WING ; 2021-544045 / [01] TOOL USED: CALIPER P/N:500-197-30 S/N:A18229508 DUE DATE: 29-SEP-22.; [02] TOOL USED: HOT BONDER P/N HCS9200B-AV S/N 18185733 DUE DATE 11-DEC-21.; [03] TOOL USED SCALE P/NSDR SWAA2021121747962Fitting · corrodedLEFT WING PICKLE FORK KICK FITTING HAS CORROSION AROUND BUSHING ON INBOARD SIDE. ; / [01] REMOVED BUSHNG FROM LH KICK FITTING PER SOPM 20-50-03; 06] REMOVED LH KICK FITTING PER SRM 51-40-02; [14] INSTALLED AND TORQUED UPPER KICK FITTING BOLT; SHIM AND BUSHING SDR SWAA2022011146896Angle · crackedSUPPLEMENTAL INFORMATION: CRACKED ANGLE AT CABLE QUADRANT BS 685+10 ON THE RT SIDE OF BL 0 BEAM WL 207 ; / [01] UPDATED STEP 1.; [02] UPDATED STEP 1 FOR FABRICATION.; [03] UPDATED PARTIAL STEP<BR>OK TO ALODINE AND PRIME; [04] UPDATED PARTIAL STEP 1.; [05] VERISDR SWAA2021122746023Access Panel · crackedCRACK ACCESS PANEL 532NB INDICATOR FUEL FLOAT AT LT WING ; 2021-520600 / [01] REPLACED ACCESS PANEL 532NB INDICATOR FUEL FLOAT AT LT WING IAW ROCKWELL COLLINS CMM 28-40-11.; [02] VERIFIED TASK COMPLETESDR SWAA2021121345626Access Panel · crackedSUPPLEMENTAL INFORMATION: CRACK ACCESS PANEL 561BB HOLES AT LT WING ; 2021-525934 / [01] CALIPER PN: 500-197-30; SN: A18229508; DUE DATE: 29/SEP/22.; [02] HOT BONDER PN: HCS9200B; SN: 18165044; DUE DATE: 15/FEB/22.; [03] HOT BONDER P/N: HCS9200B-AV; S/N: 18196SDR SWAA2021122045675Stringer · crackedR/W L/E INB FRONT SPAR LOWER CHORD ATTACHED ANGLE BRACKET CRACKED I/B OF PYLON # 2. REMOVED ANGLE PER B737-700 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW STRINGER ANGLE IAW SRM 51-40-05-0G-0; [03] VERIFIED STEP 2; VERIFIED STEP 1; OK TO TREAT AND PRIME;
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