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 VNAA202404080001Skin · corrodedCORROSION AT RH WINGLET LOWER AREA BTW WGLTS0.00./WS398.93 AND FS695.00 /FS794.50. RH WINGLET LOWER AREA BTW WGLTS0.00./WS398.93 AND FS695.00 /FS794.50 WAS REPAIRED PER REO 690-57-31-228 REV. --SDR AALA202403057683Access Panel · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING FUEL ACCESS PANEL 540FB FASTENER HOLES WORN. REPLACED PANEL PER TASK CARD 26C54057007.SDR JR2R20240302419Skin · chafedRH WING FIXED L/E BETWEEN SLAT #1 AND #2 ABOVE PYLON CHAFED. REPAIRED PER SRMSDR JR2R20240302420Skin · chafedLH WING FIXED L/E BETWEEN SLAT #1 AND #2 ABOVE PYLON CHAFED. REPAIRED PER SRMSDR SWAA2024041157780Panel · delaminatedRIGHT-WING LEADING-EDGE PANEL 621SB FASTENER HOLES DELAMINATED RT WING LEADING EDGE PANEL 621SB FASTENER HOLES DELAMINATED. LAID UP BMS 8-289 (FOIL) USING BMS 8-301 TY 1 (EA9390) IAW SRM 51-70-14-2R-3.SDR AALA202403080411Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING UPPER SURFACE TRAILING EDGE TOP SKIN PANEL AT WMRX 5855.6 AND RIB 17. REPAIRED SKIN PANEL PER EA 351170 AND SRM 57-21-11-283-026.SDR IPXA2024031197280Access Panel · crackedFOUND RH WING LOWER OUTBOARD MAIN FUEL PUMP ACCESS CRACK (REPLACE) 1.I.A.W AMM 20-11-00-910-802 REV.141 REPLACED THE ACCESS PANEL. COND CHECK NORMAL. ATTACHMENT ARE UPLOADEDSDR AALA202403087711Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING UPPER SURFACE TRAILING EDGE TOP SKIN PANEL BETWEEN WMRX 6875 AND WMRX 7176 AND BETWEEN RIBS 18 AND 19. REPAIRED SKIN PANEL PER EA 351170 AND SRM 57-21-11-283-026.SDR AALA202403085692Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING UPPER SURFACE TRAILING EDGE TOP SKIN PANEL AT WMRX 4400 AND RIB 13. REPAIRED SKIN PANEL PER EA 351170 AND SRM 57-21-11-283-026.SDR ABXA2024022849Skin · corrodedDURING AIRCRAFT CURRENT CHECK, MAINTENANCE DISCOVERED CORROSION ON THE UPPER SURFACE OF THE RIGH-HAND WING TOP SKIN PANEL #2 (PIN L 12T3302-4) BETWEEN STA 255-263 AND SU17. THE CORROSION WAS REMOVED BY BLENDING PER B767-300 SRM 57-20-01, AND FOUND TO BE OUT OFSDR ABXA2024022848Skin · corrodedDURING AIRCRAFT CURRENT CHECK, MAINTENANCE DISCOVERED CORROSION ON THE LOWER SURFACE OF THE LEFT-HAND WING BOTTOM SKIN PANEL #3 (P/N 112T4703-1) AT RIB NO. 28 & 26 AND STRINGER 9 &10. THE CORROSION WAS REMOVED BY BLENDING PER SRM 57-20-01, AND FOUND TO BE OUT SDR EE4Y2024022819558Skin Panel · misrepairedRH WING, MAIN BOX T/E SECTION LOWER SKIN AT RIB 10 WITH EXISTING REPAIR WITHOUT RECORDS AND AT RIB 10+35MM LOWER SKIN WITH CRACK. NOTE: THE WING SKIN WAS REPAIRED AS PER SRM 57-10-01 REPAIR 54 PARAGRAPH 9. REPAIR INSTRUCTIONS: THERE IS NO CHANGE IN THE MAINTENSDR AALA202405018906Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL UPPER SURFACE BETWEEN RIB 20 AND RIB 21. REPAIRED SKIN PANEL PER EA 352121.SDR DALA2024022702750Skin · unknownSHIP 5641 MULTIPLE AREAS OF BUBBLING PAINT ON L/H WING UPPER SURFACE IN WALKWAY. CORRECTIVE ACTION: C/W ER/A 523968-14 REV A AT L/H WING UPPER SURFACE WALKWAY AREA AS REQ WITHOUT DEVIATIONS (0219374)SDR IXXA2024041801Skin · crackedRIGHT WING FIXED L/E CRACK ABOVE OUTBOARD END OF #8 SLATSDR SWAA2024031555869Skin · crackedLEFT WING TRAILING EDGE PANEL 561AB SUPPORT STRUCTURE CRACKED.(MARKED)<[01] REMOVED DAMAGED LEFT WING TRAILING EDGE PANEL 561AB SUPPORT STRUCTURE PER SRM 51-40-02.;[02] LOCATED AND DRILLED NEW SUPPORT STRUCTURE PER SRM 51-40-05.;[03] VERIFIED LOCATED AND DRILLSDR SWAA2024031563534Doubler · separatedRIGHT DEFLECTION RIB SERRATED PLATES LOOSE; ELONGATE.<[01] CUT OUT DAMAGE FROM R/H DEFLECTION CONTROL RIB PER SRM 57051-02-2R-4.;[02] C/W H.F.E.C SURFACE INSP. PER PART 6; 51-00-00 PROCEDURE 23. C/W HOLE PROBE INSP. PER NDT PER PART 6; 51-00-00 PROCEDURE 16. NSDR JR2R20240224138Skin · chafedLH WING FIXED LEADING EDGE AT #1 PYLON CHAFED. REPAIREDSDR JR2R20240224139Skin · chafedRH WING FIXED LEADING EDGE AT #2 PYLON CHAFED. REPAIREDSDR 2024FA0000867Stiffener · crackedR/H WING I/B FWD LOWER SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEWSDR DALA2024022602684Skin · corrodedSHIP 5641 MULTIPLE AREAS OF BUBBLING PAINT ON L/H WING UPPER SURFACE IN WALKWAY. AREAS MARKED. CORRECTIVE ACTION: C/W ER/A 523968-14 REV A ON R/H WING UPPER SURFACE IN WALKWAY AREA. (0215225)SDR DALA2024022602683Skin · corrodedSHIP 5641 2EA. BUBBLING AREAS FOUND ON R/H WING UPPER SURFACE IN WALKWAY. AREAS ARE MARKED. CORRECTIVE ACTION: C/W ER/A 523967-14 REV A AT R/H WING UPPER SURFACE WALKWAY AREA. (0215056)SDR UIEA2024022100109Skin · corrodedLH WINGLET WEB SKIN (STA ZERO) CORROSION EVIDENCE(<P>LH WINGLET RIB 1 WEB SURFACE (STA ZERO) WAS REPAIRED PER CMA-TLS 24-0107-07B & CMA-TLS 24-0107-12B. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024022100110Skin · corrodedRH WINGLET WEB SKIN (STA ZERO) EVIDENCE OF CORROSION(<P>RH WINGLET RIB 1 WEB SURFACE (STA ZERO) WAS REPAIRED PER CMA-TLS 24-0105-03B. NO FURTHER DEFECTS NOTED.</P>)SDR R61A2024030300094Skin · corrodedDURING HEAVY CHECK MAINTENANCE FOUND RH WING TRAILING EDGE RIB 11 FOUND TO HAVE A CRACK ON THE UPPER SKIN PANEL. RH WING TRAILING EDGE RIB 11 CRACK ON THE UPPER SKIN PANEL REPAIRED IAW ETD2024-170-009342. HFEC CARRIED OUT WITH NO DEFECTS NOTED.SDR R61A2024031000105Skin · crackedR/H WING FLE SKIN TOP SIDE SLAT TRACK #5 CUTOUT BETWEEN L/E RIB19-L/E RIB220 FOUND CRACK. R/H WING FLE SKIN TOP SIDE, SLAT TRACK #5 CUTOUT BETWEEN L/E RIB19-L/E RIB20 HAS BEEN REPAIRED IAW ERJ-170-SRM 57-49-01.SDR R61A2024031000104Skin · crackedL/H WING FLE SKIN TOP SIDE, SLAT TRACK#5 CUTOUT BETWEEN L/E RIB19-L/E RIB20 FOUND CRACKED. LH WING FLE SKIN TOP SIDE, SLAT TRACK#5 CUTOUT BETWEEN L/E RIB19-L/E RIB20 HAS BEEN REPAIRED IAW ERJ-170-SRM 57-49-01.SDR SWAA2024031453580Panel · elongatedRIGHT WING T/E PANEL 661BB HAS ELONGATED HOLE. MARKED WITH DOT.<[01] REPAIRED RIGHT WING T/E PANEL 661BB; AS PER SRM 51-70-04-2R-9; MATERIAL USED PO#1608196 AND PO#2040614;[02] VERIFIED STEP 1.SDR F3LA2024021800023Access Panel · missingAIRCRAFT GROUNDED DUE TO THE FOLLOWING ISSUE - REFERENCE LP259071, ITEM 1. PANEL MISSING FROM TOP OF RIGHT WING DIRECTLY ABOVE ENGINE PYLON (621BT) ARRIVED IN SEA AT 0918, UPON TAXI INTO THE GATE, A PASSENGER POINTED OUT THAT PANEL 621BT LEADING EDGE ACCESS PASDR HNAA2024030400170Nut Plate · corroded00125 WING LOWER SKIN ACCESS HOLE FOR 6532AB INTERNAL NUTPLATE RING IS CORRODED. REMOVED CORRODED RING ASSY AND INSTALLED NEW SERVICABLE NUTPLATE MOUNTING RING ASSY P/N 145-67342-402 IAW EMB145 SRM 51-40-02SDR CALA2024021900461Skin · crackedR/W FIXED L/E BEHIND NO 8 SLAT IS CRACKED / MISSING MATERIAL AT RIVET HEAD (MARKED 7285) DAMAGE BEHIND THE #8 SLAT FOUND TO BE CRACK FREE ON THE LE FIXED WING. ACCOMPLISHED A REPAIR IAW SRM 51-70-08 PARA 4C AND 4G.SDR DALA2026011200295Skin · noneREPAIR TO RT WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 598799-14AD REV A. (WINGS / OUTER WING / RHS UKPPER SKIN AT FWD DRAG FITTINGS, HOLES 3, 4, 5, 13 & 16 / CORROSION / AMOC 22-151). REF ERA 598799-14AD. (0SDR BAGA202402200008Skin · crackedDURNING THE HEAVY CHECK INSPECTION OF N190BZ, ZONAL INSPECTION CARDS FOUND L/H WING T/E LOWER SKIN CRACKED AT RIB 10. REPAIR SIGNED OFF ON 2/12/2024 AS A MAJOR REPAIR. AIRCRAFT WAS RETURNED TO SERVICE ON 2/16/2024.SDR BAGA202402200007Skin · crackedDURNING THE HEAVY CHECK INSPECTION OF N190BZ, ZONAL INSPECTION CARDS FOUND RH WING T/E LOWER SKIN CRACKED AT RIB 10. REPAIR SIGNED OFF ON 2/12/2024 AS A MAJOR REPAIR. AIRCRAFT WAS RETURNED TO SERVICE ON 2/16/2024.SDR BAGA2024021900006Skin · crackedDURNING THE HEAVY CHECK INSPECTION OF N190BZ, ZONAL INSPECTION CARDS FOUND L/H WING T/E LOWER SKIN CRACKED AT RIB 10. REPAIR SIGNED OFF ON 2/16/2024 AS A MAJOR REPAIR. AIRCRAFT WAS RETURNED TO SERVICE ON 2/16/2024.SDR BAGA0220242190005Skin · crackedDURNING THE HEAVY CHECK INSPECTION OF N190BZ, ZONAL INSPECTION CARDS FOUND RH WING T/E LOWER SKIN CRACKED AT RIB 10. REPAIR SIGNED OFF ON 2/16/2024 AS A MAJOR REPAIR. AIRCRAFT WAS RETURNED TO SERVICE ON 2/16/2024.SDR ABXA2024021900640Skin Panel · corrodedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED THAT THE RH OUTBOARD FLAP UPPER SKIN PANEL, LOWER SKIN IS DELAMINATED. AFTER REMOVING THE DIS-BONDED SKIN, THE SIZE OF THE DAMAGE IS 70.4-INCH BY 8.10 INCHES. THE SRM 57-53-01, REPAIR L DIRESDR ABXA2024021900638Skin Panel · corrodedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, CORROSION WAS REMOVED FROM THE RIGHT WING UPPER SKIN, PANEL NO. 1, UPPER SURFACE FROM AROUND THE FUEL PORT CUTOUT LOCATED AT APPROXIMATELY WS 785.2 AND BETWEEN STRINGERS U15-U16. ORIGINAL THICKNESS PER DRAWING 1SDR ABXA2024021960037Skin Panel · corrodedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, CORROSION WAS REMOVED FROM THE LEFT WING UPPER SKIN, PANEL NO. 1, UPPER SURFACE FROM AROUND THE FUEL PORT CUTOUT LOCATED AT APPROXIMATELY WS 785.2 AND BETWEEN STRINGERS U15-U16. ORIGINAL THICKNESS PER DRAWING 11SDR ABXA2034021900636Skin Panel · corrodedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED CORROSION DAMAGE ON LH WING UPPER SKIN PANEL NO.L, APPROX. AT WBL105 (112T3101-5), STRINGER U4-U5. DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51-10-02. PLANE XXXII, INITIAL 0.210" SDR ABXA2024021900635Skin Panel · corrodedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED CORROSION DAMAGE ON LH WING UPPER SKIN PANEL NO.L, APPROX. AT WBL105 (112T3101-5). DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51-10-02 WITH MEASURED MATERIAL REMAINING OF 0.159 INCSDR ABXA2024021900634Skin Panel · damagedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED CORROSION DAMAGE ON LH WING UPPER SKIN PANEL NO.1, APPROX. AT WBL105 (112T3101-5), STRINGER UL-U3. DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51-10-02 WITH MEASURED MATERIAL REMAINSDR ABXA2024021900633Skin · corrodedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, CORROSION DAMAGE WAS FOUND ON THE LH WING SKIN PANEL NO. 1, TRAILING EDGE OVERHANG AT APPROXIMATELY WS 230.00. THE DAMAGE WAS REMOVED BY BLENDING, HOWEVER, THE BLEND DEPTH WAS FOUND TO BE OUT OF THE B767-200 SRMSDR SWAA2024031452815Angle · crackedRIGHT WING FIXED T/E PANEL JUST AFT OF THE PYLON ATTACH ANGLE CRACKED JUST IB OF DEFLECTION RIB. MARKED<[01] REMOVED AND REPLACED RIGHT WING FIXED T/E ATTACH ANGLE JUST AFT OF PYLON AND I/B OF DEFLECTION RIB IAW SRM 51 -40-02-0G-0 PARA. 4.;[02] VERIFIED COMPLESDR AALA202402151587Skin Panel · wornAIRCRAFT WAS GROUNDED: RIGHT WING BOTTOM SKIN PANEL #3 HYDRAULIC LINE PASS THROUGH AREA WORN DUE TO THE HYDRAULIC LINES CHAFFING BETWEEN WING RIBS 7 AND 8 AT #2 ENGINE PLYON STATION 5723. REPAIRED SKIN PANEL PER EA 349469A.SDR AALA202404150573Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 10 PLUS 3 INCHES. REPAIRED SKIN PANEL PER EA 351787.SDR HALA2026090300194Skin · corrodedDURING PERFORMING A 3 YEAR CHECK AT SIAEP, AN OF INSPECTION AS PER B321-ZL-500-02-1, CORROSION WAS FOUND ON THE LT WING BOTTOM SKIN PANEL 2 BETWEEN RIBS 24-25. AFTER DAMAGE ASSESSMENT AS PER SRM 57-21-11-283-014, CONTACT WITH AIRBUS IS REQUIRED SINCE THE BLENDSDR AALA202404155702Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL UPPER SURFACE BETWEEN RIBS 8 AND 9. REPAIRED SKIN PANEL PER EA 351780.SDR SWAA2024031451921Access Panel · corrodedCORROSION ON PLATE ACCESS PANEL 653BB IB MIDFLAP AT RT WING 2024-121697<[01] REPLACED PLATE ACCESS PANEL 653BB IB MIDFLAP AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[02] TASK COMPLETEDSDR 2024FA0000145Skin · crackedR/H WING FWD WING WALK CRACKED AROUND CORRUGATED SKIN. REPLACED SKIN ASSY WITH NEW
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