JASC 5730
Service difficulty reports · 27,262
Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730' 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 = '5730' 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 SWAA2023110206103Access Panel · crackedCRACK INTERNAL AREA AFT FAIRING ACCESS PANEL 542BB AT LT WING 2023-614982<[01] TOOL USED:CALIPER PN:500-196-30 SN:B21140358; DUE DATE:21-NOV-23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B S/N:15102320 DUE DATE: 22-JAN-24.;[03] TOOL USED: SCALE P/N:SPX621 S/N: 83SDR SWAA2023102005073Doubler · crackedL/H WING LOWER SURFACE OF L/E SLAT NOSE SKIN AT ACTUATOR #2 HAS A SUSPECTED CRACK AT FASTENER (MARKED)<[01] UPDATED STEPS 2-4.;[02] REQ. HFEC FOR ALL INITIAL FASTENER HOLES IN THE NOSE SKIN AND THE UNDERLYING STRUCTURE FOR DAMAGE.;[03] VERIFIED STEP 7 IN PARTISDR SWAA2023100606118Access Panel · defectiveDOT A24-8 LEFT WING FUEL TANK ACCESS PANEL 532EB HAS DEFECTIVE PHENOLIC EDGE.<[01] EVALUATED PHENOLIC STRIP ON LEFT WING FUEL TANK ACCESS PANEL 532EB IAW B737 AMM 28-11-11-400-801 STEP 3J(1). PANEL FOUND TO BE UNSERVICEABLE. ORDERED AND RECEIVED SERVICEABLE PASDR UIEA2023092300852Unknown · unknownRH WING REAR SPAR UPPER SKIN CORROSION WS 616 - 798(<P>CORROSION WAS REWORKED AND FOUND WITHIN ALLOWABLE SRM 57-20-01-1A-1 & 51-10-02-0G-0 LIMITS </P>)SDR UIEA2023092200846Unknown · unknownRH WING, UPPER SKIN FOUND CORROSSIONS, NEXT TO RIB 1 FROM REAR SPAR TO FRONT SPAR.(<P>DAMAGES WERE REWORKED AND REPAIRED IAW BOEING CASE #CMA-TLS-23-0143. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023092200845Unknown · unknownRH WING, UPPER SKIN FOUND CORROSSION NEXT TO RIB 3.(<P>DAMAGES WERE REWORKED AND REPAIRED IAW BOEING CASE #CMA-TLS-23-0143. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023092200841Unknown · unknownLH WING, UPPER SURFACE, AT BEGINNING OF OUTER WING (WBL 98.0), OVERWING LONGERON, FROM STA 852 TO 955.1, THREE SEVERAL CORROSIONS(<P>WAS REPAIRED IAW TRE6757211 ISSUED DATE: 13 SEP 20 AND APROV NUMBER: CMA-TLS-12-0141-11C DATE 13 SEP 23. NO FURTHER DEFECTS NOTSDR UIEA2023092200840Unknown · unknownLH WING UPPER SURFACE WAS FOUND CORROSIONS AT SKIN BETWEEN FRONT SPAR AND REAR SPAR NEXT TO RIB 1(<P>WAS REPAIRED IAW TRE6757211 ISSUED DATE: 13 SEP 20 AND APROVED NUMBER: CMA-TLS-12-0141-11C DATE 13 SEP 23. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023092200839Unknown · unknownLH WING UPPER SURFACE FOUND CORROSION AT SKIN BETWEEN WBL 97- 9566 AND L-2, 26" OF REAR SPAR TO LEADING EDGE.(<P>WAS REPAIRED IAW TRE6757211 ISSUED DATE: 13 SEP 20 AND APROVED NUMBER: CMA-TLS-12-0141-11C DATE 13 SEP 23. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023092100838Unknown · unknownLH WING UPPER SURFACE WAS FOUND CORROSION AT SKIN BETWEEN WBL 97.- 9566 L-1, 15" OF REAR SPAR TO LEADING EDGE(<P>DAMAGES WERE REWORKED. BOEING APPROVED THE REWORKED AREAS IN "AS-IS" CONDITION. LH WING UPPER SURFACE CORROSION AT SKIN BETWEEN WBL 97.9566 L1, 15"SDR UIEA2023092100836Unknown · unknownRH WING - UPPER SKIN PANEL #1 - AT WBL 121.0 AND BETWEEN STRINGER U-17 AND REAR SPAR - CORROSION DAMAGE(<P>DAMAGES WERE REWORKED AND REPAIRED IAW BOEING CASE #CMA-TLS-23-0143. RH WING, UPPER SKIN, RIB 1 AT 33.5" FROM REAR SPAR TO FRONT SPAR CORROSION WAS REPAISDR DALA2023092907989Unknown · unknownSHIP 0668 CORROSION ON ANGLE (SILL) UPPER SURFACE BTW STA 730-690 LBL 65 AT L2 AT PAX CABIN. CORRECTIVE ACTION SUMMARY OF NRC 00352: ANGLE (SILL) BTW STA 660 TO STA 755 LBL 65 AT L2 AT PAX CABIN WAS REPLACED PER B757-200 SRM 51-40-02. (2989939)SDR DALA2023092908018Unknown · unknownSHIP 1602 ER/A 584096-14AD SECT. I REPAIR WAS ACCOMPLISHED ON A/C 1602 (12,986 TFC AND 95,158 TFH) IN THE LH WING LOWER SKIN AT STR L-9.5 AND WSTA 906.2. FOLLOW ON ACTION IS REQUIRED FOR SECT. III INSPECTION. CORRECTIVE ACTION: ACCOMPLISH ER/A 584096-14AD REV.SDR YENA2023092901145Unknown · unknownDURING HEAVY MAINTENANCE: CRACK ON RIB 23 AT RH WING FIXED LEADING EDGE; REF TOMX W.O. N239JB/2301/ E190/B8 CHECK & JB NR 0031 - RIB 23 AT RH WING FIXED LEADING EDGE WAS REPLACED PER EMB-190 SRM 51-41-02 AND SRM 51-43-04.SDR FDEA202309261651Doubler · delaminatedLEFT WING - TRAILING EDGE INBOARD ISLAND UPPER FIXED PANEL LOWER SURFACE FORWARD EDGE FINGER DOUBLER AT XW 398 FOUND DETACHED. LEFT WING - TRAILING EDGE INBOARD ISLAND UPPER FIXED PANEL LOWER SURFACE FORWARD EDGE FINGER DOUBLER AT XW 398 REPAIR CARRIED OUTSDR FDEA202309261650Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 760 FOUND CRACK. RIGHT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 760 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100.SDR FDEA202309261649Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 737 FOUND CRACK. RIGHT WING - FIXED LEADING EDGE DOUBLER AT STATION XOS 737 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100.SDR FDEA202309261648Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 711 FOUND CRACK. RIGHT WING - FIXED LEADING EDGE DOUBLER AT STATION XOS 711 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100.SDR FDEA202309261647Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 765 FOUND CRACK. LEFT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 765 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100.SDR DALA2024022202516Skin · unknownSHIP 695 ER/A 611934-14 ISSUED FOR LH WING FIXED LEADING EDGE COMPOSITE R EPAIR LOCATED BETWEEN ISS 169 TO 213. CORRECTIVE ACTION: REF ERA 611934-14. (2986998)SDR SWAA2023110704294Panel · elongatedRIGHT WING I/B LEADING EDGE PANEL#611AT FOUND ELONGATED FASTENER HOLES<[01] PREPARED DAMAGE AREA FOR REPAIR ON PANEL #611AT AS PER B737 SRM 51-70-04-2R-9 PARAG (4-C) AND B737 SRM 51-70-04-2R-0 PARAG (4-E)APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #611AT SDR SWAA2023103108443Access Panel · bulgedLEFT WING LOWER MID T/E ACCESS PANEL # 561CB HAS BULGING/CRACKED FASTENER HOLES<[01] PREPARED LEFT WING LOWER MID T/E ACCESS PANEL # 561CB. AS PER SRM 51-70-04-2R-9-B00345REPAIRED LEFT WING LOWER MID T/E ACCESS PANEL # 561CB. AS PER SRM 51-70-04-2R-9-B00345 MASDR SWAA2023110203940Skin · crackedCRACK SKIN LOWER SURFACE SLAT 7 LOCATED SLAT STA 322.71 RT WING 2023-614754<[01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138003; DUE DATE: 27-MAR-24.;[02] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[0SDR VNAA202310100002Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 597AB) AT LH WING LOWER SKIN. REPAIRED PER EA 23-C9-57-1243 REV IR, EA 23-C9-57-1276 REV.A, EA 23-C9-57-1277 REV.IR, EA23-C9-57-1278 REV.IR SECTION III-PERMANENT REPAIR.SDR AWKA2024052707201Skin Panel · corrodedCORROSION FOUND ON FUEL PANEL LAND 522DB. *** ACCOMPLISHED FIELD REPAIR - CORROSION, LH WING, LWR SKIN, PANEL 522DB (FR-750-0220-11461 REV.-).SDR SWAA2023110703295Access Panel · delaminatedRIGHT WING LOWER LEADING EDGE ACCESS PANEL 621UB DELAMINATED AT FLANGE TIP.<[01] REPAIRED RIGHT WING LOWER LEADING-EDGE ACCESS PANEL 621UB AS PER SRM 51-70-04-2R-13-A00757 MATERIAL USED PO.1791128 AND PO.1473815. PAINTED PANEL #621UB PER B737 AMM 51-21-99-300-SDR SWAA2023103003433Access Panel · crackedCRACK ACCESS PANEL 661CB TRAILING EDGE AROUND HOLE RT WING 2023-594300<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189527; DUE DATE: 26/DEC/23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 24-JAN-24.;[03] TOOL USED: SCALE P/N: SPX621 SSDR AALA202401038339Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN RIBS 7 AND 8. REPAIRED SKIN PANEL PER EA 348779.SDR AALA202401033667Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 8 PLUS 8 INCHES. REPAIRED SKIN PANEL PER EA 348779.SDR AALA202312189517Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR SPAR TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN WX 3495.5 AND WX 4490.5 AT RIB 8. REPAIRED SKIN PANEL PER EA 348780 .SDR DALA2023092207829Unknown · unknownSHIP 5647 #10 FASTENER ON RH PYLON DRAG FITTING HAS CRACKED PAINT AND DISCOLORATION AROUND FASTENER. CORRECTIVE ACTION: REMOVED AND REPLACED #10 FASTENER FROM RH PYLON DRAG FITTING IAW AMDS TASK CARD 5720-01100-02B, TORQUE CHECK WAS ACCOMPLISHED ON TASK CARD 5SDR DALA2023092207828Unknown · unknownSHIP 5647 #7 FASTENER ON RH PYLON DRAG FITTING HAS CRACKED PAINT AND DISCOLORATION AROUND FASTENER. CORRECTIVE ACTION REMOVED AND REPLACED #7 FASTENER FROM RH PYLON DRAG FITTING IAW AMDS TASK CARD 5720-01100-02B, TORQUE CHECK WAS ACCOMPLISHED ON TASK CARD 5720SDR DALA2023092207827Unknown · unknownSHIP 5647 #6 FASTENER ON RH PYLON DRAG FITTING HAS CRACKED PAINT AROUND PERIMETER OF FASTENER. CORRECTIVE ACTION: REMOVED AND REPLACED #6 FASTENER FROM RH PYLON DRAG FITTING IAW AMDS TASK CARD 5720-01100-02B, TORQUE CHECK WAS ACCOMPLISHED ON TASK CARD 5720-011SDR DALA2023092207826Unknown · unknownSHIP 5647 #5 FASTENER ON RH PYLON DRAG FITTING HAS CRACKED PAINT AND SINGS OF SPINNING. CORRECTIVE ACTION: REMOVED AND REPLACED #5 FASTENER FROM RH PYLON DRAG FITTING IAW AMDS TASK CARD 5720-01100-02B, TORQUE CHECK WAS ACCOMPLISHED ON TASK CARD 5720-01100-02B.SDR DALA2023092207825Unknown · unknownSHIP 5647 #2 FASTENER ON RH PYLON DRAG FITTING HAS CRACKED PAINT AND SIGNS OF ROTATION. CORRECTIVE ACTION: REMOVED AND REPLACED #2 FASTENER FROM RH PYLON DRAG FITTING IAW AMDS TASK CARD 5720-01100-02B, TORQUE CHECK WAS ACCOMPLISHED ON TASK CARD 5720-01100-02B.SDR DALA2023092207824Unknown · unknownSHIP 5647 #9 FASTENER ON RH PYLON DRAG FITTING HAS CRACKED PAINT AND DISCOLORATION AROUND FASTENER. CORRECTIVE ACTION: REMOVED AND REPLACED #9 FASTENER FROM RH PYLON DRAG FITTING IAW AMDS TASK CARD 5720-01100-02B, TORQUE CHECK WAS ACCOMPLISHED ON TASK CARD 572SDR DALA2023092207823Unknown · unknownSHIP 5647 #1 FASTENER OH RH PYLON DRAG FITTING HAS CRACKED PAINT AND SIGNS OF SPINNING. CORRECTIVE ACTION REMOVED AND REPLACED #1 FASTENER FROM RH PYLON DRAG FITTING IAW AMDS TASK CARD 5720-01100-02B, TORQUE CHECK WAS ACCOMPLISHED ON TASK CARD 5720-01100-02B. SDR DALA2023092207821Unknown · unknownSHIP 0668 DAMAGES WERE FOUND ON OPEN HOLE AT LH ENG DRAG FTG CLAMP-UP & DRAG BRACE AS FOLLOW: HOLE NO.3 CORROSION AND SCRATCHES ON SKIN AND FITTING BTW 1 TO 5 O CLOCK POSITION. CORRECTIVE ACTION SUMMARY OF NRC 00178: HOLE # 3 WAS REAMED TO DIAMETER 0.5780" PERSDR IPXA2023100416438Access Panel · delaminatedLH WING FUEL TANK DRY BAY ACCESS PANEL 532FZ WITH DELAMINATION. VERIFIED INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD T3F18E00260FV.SDR IPXA2023100416407Access Panel · delaminatedLH WING FUEL TANK DRY BAY ACCESS PANEL 532BZ WITH DELAMINATION. REMOVE DAMAGE AND REPAIRED DAMAGED AREA IAW B757 SRM 51-70-07-0G-0 PARA. 5.G.3SDR SWAA2023092503303Panel · delaminatedL/H WING PANEL 521VB HAS DELAMINATION AT LEADING EDGE OUTBOARD CORNER.<[01] COMPLIED WITH EA 23-157-02840.SDR DALA2023092207796Unknown · unknownSHIP 193 FOUND LH WING LOWER SKIN NOT FLASH AT RIB 31. CORRECTIVE ACTION: REPAIRED THE DAMAGED LOWER SKIN AT LH WING STR L-6.5 BETWEEN WSTA 990.2 AND WSTA 1018.2 AS PER PRI 611798-14 (2975132)SDR 2024FA0000108Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWSDR 2024FA0000107Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWSDR R61A2023100700559Skin · gougedLH WING FIXED L/E SKIN GOUGED @ RIB 41-42. MAJOR REPAIR PERFORMED IAW ETD 2023-170-023465. NO CRACKS FOUND.SDR DALA2023091807668Unknown · unknownSHIP 193 DURING CCK AT STAG, A DENT WAS NOTED ON THE LH LOWER WING SKIN, STR L-6.5, WSTA 1005. REPAIR WAS ACCOMPLISHED PER ER/A 611798-14AD SECTION I. FOLLOW ON INSPECTIONS ARE REQUIRED PER SECTION II. CORRECTIVE ACTION: ACCOMPLISH ER/A 611798-14AD SECTION II SDR JR2R20230915468Unknown · chafedLH WING LEADING EDGE PANEL CHAFFED AT #1 ENGINE PYLONSDR FDEA202309141597Skin · damagedDURING DVI INSPECTION OF L/E SKIN REPAIR ON #3 SLAT ON HECO CARD 9019, FOUND 2 BLIND FASTENERS THAT WERE LOOSE AND LOCKING PINS WERE NOT FLUSH WITH THE FASTENER HEAD. REMOVED AND REPLACED 2 EACH FASTENERS PER FEDEX EA# F-2780-T0350154 A P3 TITLE: FLIGHT COSDR SWAA2023101700420Panel · elongatedLEADING EDGE PANEL 521CB HAS MULTIPLE ELONGATED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #521CB AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 SRM 51-70-04-2R-9 PARAG (4-D-M) AND B737 SRM 51-70-04-2R-0 PARAG (4-L-M-N). MATERIAL USED SDR SWAA2023101700424Panel · elongatedLEADING EDGE PANEL 511AT HAS ELONGATED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #511AT AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 SRM 51-70-04-2R-9 PARAG (4-D-M) AND B737 SRM 51-70-04-2R-0 PARAG (4-L-M-N). MATERIAL USED PO#179112
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