JASC 5750
Service difficulty reports · 1,158
Reports filed under 5750 · Wing, Control Surfaces, 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 = '5750' 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 = '5750' 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 SWAA2022080425885Angle · crackedCRACK ON SUPPORT ANGLE LOCATED ORSS 272 TRAILING EDGE RT WING 2022-354731 / [01] REPLACED SUPPORT ANGLE LOCATED ORSS 272 TRAILING EDGE RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.M;[02] CORRECTED ITEM 1.<BR>REPLACED SUPPORT ANGLE LOCATED ORSS 272SDR SWAA2022080825441Panel · brokenBROKEN ACCESS PANEL 661AB TRAILING EDGE AT RT WING 2022-354561 / [01] TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 01-OCT-22.;[02] TOOL USED: SCALE P/N: SCA-301 S/N: AE-412133 DUE DATE: 14-MAR-23.;[03] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18SDR SWAA2022072825435Bracket · elongatedPANEL 651GB I/B AFT BRACKET ELONGATED HOLE / [01] REMOVED AND REPLACE BRACKET PER SRM 51-40-02-0G-0 AT PANEL 651GB;[02] VERIFIED 1SDR REXA2022072801688Fitting · wornLHOB FLAP VANE OB ATTACH FITTING WORN. WEAR MEASURE 1.0" X .50" X WORN DOWN TO FITTING SURFACE REMOVED AND REPLACED VANE FITTINGSDR REXA2022072701682Panel · wornLHIB FLAP VANE ACCESS PANEL 584ET CHAFED. BLENDED CHAFE DIMENSIONS AS FOLLOWS 1.25" X .50" X .019" DEEP. REMOVED AND REPLACED ACCESS PANEL 584ET.SDR REXA2022072001609Fitting · wornLHOB FLAP VANE OB ATTACH FITTING WORN. WEAR MEASURE 1.0" X .50" X WORN DOWN TO FITTING SURFACE REMOVED AND REPLACED VANE FITTINGSDR REXA2022072701681Panel · wornRHIB FLAP VANE ACCESS PANEL 684ET CHAFED. BLENDED CHAFE DIMENSIONS AS FOLLOWS 1.5" X .60" X .021" DEEP. REMOVED AND REPLACED ACCESS PANEL 684ET.SDR FDEA202207011725Spoiler · delaminatedRH WING - #5 SPOILER CENTER I/B HINGE ARM O/B SIDE FOUND DELAMINATION (AREA: 60MM*30MM, DEPTH: 1.59MM) AND CENTER O/B HINGE ARM O/B SIDE FOUND DELAMINATION (AREA: 40MM*30MM, DEPTH:1.54MM) REPAIRED THE RH WING #5 SPOILER CENTER I/B &O/B HINGE ARM O/B SIDE DSDR FDEA202207011723Spoiler · delaminatedLH WING - #5 SPOILER CENTER O/B HINGE ARM LOWER SURFACE FOUND DELAMINATION (AREA: 20MM*20MM, DEPTH: 2.1MM) AND CENTER O/B HINGE ARM O/B SIDE FOUND DELAMINATION (AREA: 80MM*90MM, DEPTH:1.64MM) REPAIRED THE LH WING #5 SPOILER CENTER O/B HINGE ARM LOWER SURFASDR SWAA2022072824337Panel · crackedRT WING LOWER MID SPAN T/E PANEL 661BB AT SEAL ATTACHMENT FLANGE HAS MULTIPLE FASTENER HOLES BULGING SOME WITH CRACKS AS VIEWED FROM INNER SKIN. / [01] PREPARED AREA FOR REPAIR MULTIPLE FASTERNER HOLES CRACKS AT RT WING LOWER PANEL #661BB AS PER B737 SRM 51-70SDR KCSA202206301083Stiffener · crackedLEFT WING I/B AILERON O/B CLOSURE RIB WEB HAS EVIDENCE OF CHAFFINGSDR FDEA202206231537Skin · crackedRIGHT HAND WING - INBOARD FLAP ASSEMBLY UPPER MID SEGMENT SURFACE STATION YIFH 165.300 FOUND CRACKED. CRACK SKIN AT RIGHT HAND WING INBOARD FLAP ASSEMBLY UPPER MID SEGMENT SURFACE STATION YIFH 165.300 REPAIRED AS PER SRM 57-00-01-2R REPAIR 1 FIGURE 201 ANSDR REXA2022070601476Flap · chafedCHAFING FOUND ON RH WING INBOARD FLAP UNDERNEATH PANEL 683BB REPAIRED CHAFING ON RH INBOARD FLAP IAW CRJ 900 SRM 57-52-01-201-005-A01.SDR SWAA2022072521682Fairing · debondedFLAP CANOE 642BB HAS INNER LINER DISBONDED AT FWD RT SIDE. 8-55 / [01] PREPARED FOR REPAIR AT FLAP CANOE 642BB IAW B737 SRM 51-70-06-2R-7;[02] VERIFIED STEP 1. OK TO REPAIR FLAP CANOE 642BB.;[03] REPAIRED FLAP FAIRING 644BB PER SRM 51-70-06-2R-7. MATERIAL USEDSDR SWAA2022062721549Fastener · shearedRIGHT WING T/E LOWER PANEL WIGGLE PLATE FASTENERS SHEARED I/B OF PYLON FAIRING / [01] REMOVED AND REPLACED RIGHT WING T/E LOWER PANEL WIGGLE PLATE PER SRM 51-40-02SDR SWAA2022072920815Fitting · crackedL/W REAR SPAR T/E FIXED DEFLECTION CONTROL RIB PANEL LOWER VERTICAL BULB SEAL FITTING CRACKED I/B SIDE MKD DOT / [01] REMOVED L/W REAR SPAR T/E FIXED DEFLECTION CONTROL RIB SEAL FITTING AS PER B-737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW L/W REAR SDR REXA2022071901547Panel · chafedRIGHT WING INBOARD FLAP PANEL 684EB HAS SEVERE CHAFING AND A CRACK. REMOVED & REPLACED PANEL 684EB IAW CRJ 900 SRM 51-40-11-001-001-A01.SDR SWAA2022071419110Panel · delaminatedPANEL 621SB PREVIOUS REPAIR IS DELAMINATED ON OUTER SURFACE / [01] IDENTIFIED PANEL 621SB IAW SRM 57-41-01-0I-4 FIGURE 3; TABLE 3; ITEM 1. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4. A. (5). (A) - (B). DAMAGE TO BE REPAIRED IAW SRM 51-70-05SDR SWAA2022072517970Panel · brokenPANEL 551FB FWD BRACKET TO 29' OF THE O/B SIDE IS BROKEN. / [01] REMOVED AND REPLACED BRACKET AT PANEL 551FB OF THE O/B SIDE AS PER B737 SRM 51-40-02-OG-0;[02] VERIFIED 1.SDR YENA2022061400599None · noneDURING HEAVY MAINTENANCE, CORROSION REAR SPAR TOP SKIN OVERHANG LOWER SURFACE BETWEEN RIB 7A TO RIB 8 ON LH WING; REF AEROMAN WO 2022-163/1, NR 2022-285006; ACCOMPLISHED REPAIR OF CORROSION IN AN PREVIOUSLY REPAIRED AREA ON THE WING TOP SKIN PANEL 2 TRAILING ESDR VNAA202206099918Slat Track · wornL/H SLAT TRACK 3-3 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKSSDR VNAA202206099917Slat Track · wornL/H SLAT TRACK 3-1 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKSSDR VNAA202206099916Slat Track · wornL/H SLAT TRACK 2-1HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKSSDR VNAA202206099915Slat Track · wornL/H SLAT TRACK 1-3 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKSSDR VNAA202206099914Slat Track · wornL/H SLAT TRACK 1-2 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKSSDR SWAA2022071417601Plate · crackedWING PANEL 621SB HAS CRACKED I/B BACKUP PLATE / [01] UPON WORKING OF REPAIRS TO COMPOSITE PANEL; BACKUP PLATE WAS FOUND TO BE CRACKED AND MODIFIED AND WILL REQUIRE NEW BACKUP PLATE FABRICATED DUE TO NO AVAILABILITY; IAW DRAWING 116A9110-6 SHEET 2; AND DRAWING SDR ASAA2022060839144Clevis · wornRH WING OB FLAP IB ROLLER FITTING CLEVIS WORN. GROUNDED - YES. REPAIRED DAMAGE IAW B737-800 SRM 57-51-02-2R-2.SDR SWAA2022071115458Access Panel · crackedCRACK ACCESS PANEL 551FB ANGLE AT LT WING (1 EA) 2022-268279 / [01] REPLACED ACCESS PANEL 551FB ANGLE AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; DWG 115A2710 REV: B.;[02] REPLACED ACCESS PANEL 551FB ANGLE AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; DWG 115ASDR SWAA2022071115125Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 215 RT WING 2022-305795 / [01] REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED IRSS 215 RT WING IAW B737-700 SRM 51-10-02 AND DWG 115A200; SHEET 30; REV. A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED CORRUSDR SWAA2022061615059Plate · crackedLOWER AFT WING SPAR TRAILING EDGE PANEL 551EB IB ATTACH WAFFLE PLATE IS CRACKED AT OB FASTENER. APPROXIMATELY IRSS 199+20. / [01] REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02;[02] INSPECTED AS REQUIREDSDR SWAA2022071114648Plate · crackedCRACK CORRUGATED PLATE LOCATED ON ORSS 272 TRAILING EDGE AT RT WING 2022-305712 / [01] REPLACED CORRUGATED PLATE ON IRSS 272 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10-02 AND DWG 115A2714; SHEET 2; REV. B. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED CORRSDR SWAA2022071114650Access Panel · crackedCRACK ACCESS PANEL 651FB ANGLE AT RT WING 2022-305720 / [01] REPLACED ANGLE ON ACCESS PANEL 651FB AT RT WING IAW B737-700 SRM 51-10-02. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1. REPLACED ANGLE ON ACCESS PANEL 651FB AT RT WING IAW B737-700 SRM 51-10SDR SWAA2022071114651Plate · brokenBROKEN CORRUGATED PLATE LOCATED ORSS 490 TRAILING EDGE AT RT WING 2022-305721 / [01] REPLACED CORRUGATED PLATE LOCATED ORSS 490 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A3700 SHEET 33 REV -. CORRUGATED PLATE P/N: 115A3760-1; P/O: 2022-1616SDR SWAA2022070114665Bracket · crackedCRACK SUPPORT BRACKET LOCATED ON ORSS 273 TRAILING EDGE AT RT WING 2022-287873 / [01] REPLACED SUPPORT BRACKET LOCATED ON ORSS 273 TRAILING EDGE AT RT WING I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] REPLACED SUPPORT BRACKET LOCATED ON ORSS 273 TSDR SWAA2022071114224Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE AT LEVEL WS 236 RT WING 2022-268137 / [01] REPLACED SUPPORT BRACKET TRAILING EDGE AT LEVEL WS 236 RT WING I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02;[02] REPLACED SUPPORT BRACKET TRAILING EDGE AT LEVEL WS 236 RT WING I.A.WSDR SWAA2022070114283Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT LT WING 2022-287863 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT LT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 REV. -. SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK CARD COSDR SWAA2022061614014Fitting · crackedCORNER ATTACH FITTING FOR RH WING PANEL 661AB IS CRACKED. (MARKED) / [01] REMOVED AND REPLACED FITTING PER SRM 51-40-02.;[02] VERIFIED REMOVED AND REPLACED FITTING PER SRM 51-40-02.;[03] ADJUSTMENT CK GOOD PER AMM 27-51-11;[04] SAFETIED PER AMM 27-51-11;[05] SSDR FDEA202206011351None · noneRH WING #5 SPOILER CENTER O/B HINGE ARM O/B SIDE FOUND 2EA DELAMINATIONS. SIZE: (1) 45MM*25MM, DEPTH: 1.57MM (2)45MM*25MM, DEPTH: 1.27MMSDR FDEA202206011350None · noneLH WING #5 SPOILER CENTER I/B HINGE ARM O/B SIDE FOUND DELAMINATION (SIZE: 20MM*33MM, DEPTH: 1.78MM) AND CENTER I/B & O/B HINGE ARM LWR SURFACE FOUND DELAMINATION (SIZE: (1)18MM*20MM, DEPTH: 2.06MM (2)50MM*40MM, DEPTH: 2.2MM)SDR FDEA202206011349None · noneLH WING #3 SPOILER CENTER O/B HINGE ARM O/B SIDE FOUND DELAMINATION (SIZE: 40MM*20MM, DEPTH: 1.9MM) AND CENTER I/B & O/B HINGE ARM LWR SURFACE FOUND DELAMINATION (SIZE: (1)30MM*40MM, DEPTH: 2.6MM (2)30MM*20MM, DEPTH: 2.3MM)SDR SWAA2022060713338Panel · crackedL/H CENTER WING-TO-B0DY FAIRING ACCESS PANEL 193CR UPPER SECTION HAS CRACK L/H CENTER WING-TO-B0DY FAIRING ACCESS PANEL 193CL UPPER SECTION HAS CRACK REMOVED PANEL 193CL FOR ACCESS TO REAPIR IRW B737-700 AMM 53-51-21-000-802; REMOVED THE DAMAGED PLIES AND PRESDR CALA2022060101407Skin · gougedLH WING L/E #5 SLAT AND #12 TRACK CAVITY UPPER SKIN GOUGE PER HA ECO LCQ NON ROUTINE 9294591/36591 GENERATED BY V061682 REPAIRED LH WING #5 SLAT AND #12 SLAT TRACK CAVITY UPPER 11-300- 037 FIG 001 SHEET 03 REPAIRED TOPCOAT IAW SRM 51-75-12-911-002SDR CALA2022060101406Skin · gougedLH WING #1 SLAT AND #2 TRACK CAVITY UPPER SKIN LOWER SIDE IS GOU GE AT BOTH SIDES PER HAECO LCQ NON ROUTINE 9294583/36583 GENERAT ED BY V061682 REPAIRED LH WING #1 SLAT AND #2 SLAT TRACK CAVITY UPPER SKIN IAW SRM 57-41-11-300-037 FIG 001 SHEET 03 REPAIRED TOP SDR CALA2022060101405Skin · gougedLH WING #1 SLAT AND #1 TRACK CAVITY UPPER SKIN LOWER SIDE IS GOUGE AT BOTH SIDE PER HAECO LCQ NON ROUTINE 9294584/36584 GENERATE D BY V061682 REPAIRED LH WING #1 SLAT AND #1 SLAT TRACK CAVITY UPPER SKIN IAW SRM 57-41-11-300-037 FIG 001 SHEET 03 REPAIRED TOPCOASDR SWAA2022072112011Plate · crackedCRACK ON CORRUGATE PLATE LOCATED TRAILING EDGE ORSS 261 AT RT WING 2022-274592 / [01] TOOL USED CALIPER PN 500-196-30 SN A20231600 CAL DUE DATE 10 AUG 22.;[02] REPLACED CORRUGATE PLATE LOC. TRAILING EDGE ORSS 261 AT RT WING I.A.W B737-700 SRM 51-40-02 AND 51-1SDR SWAA2022072112012Plate · crackedCRACK ON CORRUGATE PLATE LOCATED ON TRAILING EDGE ORSS 241 AT RT WING 2022-274609 / [01] REPLACED CORRUGATE PLATE LOC. ON TRAILING EDGE ORSS 241 AT RT WING I.A.W B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02; DWG 115A2001 SHEET 30 REV A. SEE INDIVIDUAL SIGNOFFS BESDR SWAA2022072112030Support Angle · crackedCRACK SUPPORT ANGLE LOCATED FALSE SPAR TRAILING EDGE ORSS 270 LT WING 2022-274639 / [01] REPLACED SUPPORT ANGLE LOCATED FALSE SPAR TRAILING EDGE ORSS 270 LT WING I.A.W B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02;[02] TASK CARD COMPLETEDSDR SWAA2022061610852Angle · crackedRH WING UPPER PANEL ANGLE JUST INBOARD OF DEFLECTION CONTROL RIB IS CRACKED AT OUTBOARD FASTENER HOLE. (MPN 115A2156-8) / [01] REMOVED RH WING UPPER PANEL ANGLE JUST INBOARD OF DEFLECTION RIB.;[02] LOCATED AND DRILLED UP NEW ANGLE P/N 115A2156U8 PER SRM 51-40-SDR SWAA2022070110913Bracket · crackedCRACK SUPPORT BRACKET LOCATED ACCESS PANEL 551FB TRAILING EDGE AT LT WING 2022-265977 / [01] REPLACED SUPPORT BRACKET LOCATED ACCESS PANEL 551FB TRAILING EDGE AT LT WING IAW SRM B737-700 51-40-02 AND SRM B737-700 51-10-02 ITEM 9;[02] JOB COMPLETEDSDR SWAA2022070110050Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 261 AT RT WING 2022-265835 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 261 AT RT WING IAW SRM B737-700-51-40-02; 51-10-02 ITEM 9 DRAWING 115A2001 REV-A DUE TO NO FOUND ALLOWABLE DAMAGE IN
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