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 DALA2020022801532Skin · damaged(AIRCRAFT 5649, L/P 1507783) RH ENGINE DRAG FITTING HOLES FOUND INDICATIONS ION HOLE NUMBER 5 IN TOP SKIN AT 12 O'CLOCK POSITION. CORRECTIVE ACTION: COMPLIED WITH ERA 584953-14AD REV ORIGINAL ON RH ENGINE DRAG FITTING ON HOLE NUMBER 5 SKIN AND FITTING.SDR DALA2020022801531Skin · damaged(AIRCRAFT 5649, L/P 1507777) RH ENGINE DRAG FITTING HOLES FOUND INDICATIONS IN HOLE NUMBER 2 WITH (2) INDICATIONS IN TOP SKIN AT 3 OCLOCK AND 9 OCLOCK POSITIONS. CORRECTIVE ACTION: COMPLIED WITH ERA 584953-14AD REV ORIGINAL ON RH ENGINE DRAG FITTING ON HOLE NUSDR FDEA2020022870433Skin · crackedL/H WING TIP AFT - LOWER SURFACE BETWEEN ACCESS PANEL#528CB AND AFT POSITION LIGHT - 2 CRACKS EMINATING FROM FASTENER HOLE, CRACKS CONFIRMED AND ENDS. PERFORMED A PERMANENT REPAIR IN ACCORDANCE TO SRM VOLUME I CHAPETER 57-00-01 FIGURE 4 (SHEET 2).SDR R61A2020031320399Skin · crackedWHILE IN HEAVY CHECK-MAJOR REPAIR- DISCOVERED RH WING UPPER SKIN HAS SMOKING RIVETS AND SIGNS OF A CRACK AT THE #3 SPOILER INBD ATTACH FITTING AS MARKED. REMOVED DAMAGE AT THE RH WING UPPER SKIN, AT THE #3 SPOILER INBD ATTACH FITTING, BY CUTTING OUT CRACK. FSDR FDEA202002280392Skin · cracked01 EA CRACK INDICATION FOUND APPROXIMATELY 0.1Ï¿½ IN LENGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING FIXED LEADING EDGE SLAT TRACK #10 INBOARD CUTOUT ( CORNER #13) AT XOS 657. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGSDR DALA2020022701529Skin · damaged(AIRCRAFT 5649, L/P 585015) L/H ENGINE DRAG FITTING/SKIN HOLE #4 HAS INDICATION ON FORWARD SIDE OF HOLE BELOW SHIM. CORRECTIVE ACTION: COMPLIED WITH ER/A 585015-14AD REV ORIGINAL ON L/H ENGINE DRAG FITTING/SKIN HOLE #4.SDR DALA2020022701528Skin · damaged(AIRCRAFT 5649, L/P 1506444) L/H ENGINE DRAG FITTING/SKIN HOLE #3 HAS INDICATIONS ON FORWARD SIDE OF HOLE JUST ABOVE & BELOW SHIM. CORRECTIVE ACTION: COMPLIED WITH ER/A 585015-14AD REV ORIGINAL ON L/H ENGINE DRAG FITTING/SKIN HOLE #3.SDR FDEA202002260393Skin · cracked02 EA CRACK INDICATION FOUND APPROXIMATELY 0.3Ï¿½ & 0.1Ï¿½ IN LENGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING FIXED LEADING EDGE SLAT DOOR INBOARD CORNER ( CORNER #5) AT XOS 490. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING ESDR SWIA2020040349895Access Panel · nickedL/H WING LOWER PLANK ACCESS HOLE 540EB HAS NICK (C-CHECK) RO 4/2/2020 REMOVED DAMAGE, RESTORED FINISH IAW BOMB CRJ-200 REO LEAK CHECK ACCOMPLISHED ON AAR W.O 1018283 ZONE 5000 ITEM 0002 S/N 7665261SDR SIMA20200224010None · crackedLEFT WING TIP SPAR 1 CRACKED INSIDE ACCESS PANEL 551AB.-C/A-COMPLETE:REMOVED AND REPLACED LEFT WING TIP IAW EMB 175 AMM 57-30-00. SEE WIPS AND TASKS FOR DETAILS.SDR SIMA20200224009None · crackedRIGHT WING TIP SPAR 1 CRACKED INSIDE ACCESS PANEL 651AB.-C/A-COMPLETE:REMOVED AND REPLACED RIGHT WING TIP IAW EMB 175 AMM 57-30-00. SEE WIPS AND TASKS FOR DETAILSSDR FDEA202002240375Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY AT XOS 667 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING LEADING EDGE CAVITY AT XOS 667 BEADED DOUBLER AREA AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202002240377Doubler · crackedRIGHT HAND WING LEADING EDGE CAVITY AT STATION XOS 667 DOUBLER CRACKED. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB 3954 REVISION K. INSTALLED FABRICATED DOUBLER AT RIGHT HAND WING LEADING EDGE CAVITY AT STSDR FDEA202002240374Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY AT STATION XOS 789 DOUBLER CRACKED. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB 3954 REVISION K. INSTALLED FABRICATED DOUBLER AT LEFT HAND WING LEADING EDGE CAVITY AT STATSDR FDEA2020022420370Skin · corrodedL/H WING LOWER SKIN T/E OUTBRD AT RIB 28, INSIDE PANEL 590BB UPPER SKIN CORRODED (STREAMER) L/H WING LOWER SKIN T/E OUTBRD AT RIB28 REPAIRED PER FDX EA 6-5720-T0352251 P1; TITLED: WING-SECONDARY WING STRCT-LW UPPER SKIN,TRAILING EDGE OVERHANG, RIB 24- 29,SDR K11A2020042833101Skin · corrodedLEFT WING SKIN CORROSION WBL 15SDR SWIA2020033049514Skin · crackedRH WING PLANK ACCESS HOLE FOR PANEL 650BB IS CRACKED ON INNER EDGE. (C-CHECK) RO 3/26/2020 BLENDED CORROSION AT RH WING PLANK ACCESS HOLE 650BB REF BOMBARDIER REO, REO. ROTO PEENED AND RESTORED FINISH. ALL CHECKS GOOD. COMPLETED TASK CARD, WEIGHT CHANGESDR DALA2020022501411Access Panel · corrodedSHIP 3820 RT. WING - TANK PLATE HOLES 632PB, 632MB AND 632GB - LWR FLANGE IS CORRODED. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0008:5700-2615/001 00284 TREATED AREAS AND COMPLETED REPAIRS REF B737 SRM 57-20-01 -2R PROCEDURE 1 REPAIR 1.SDR DALA2023019200424Stringer · damagedDURING INSPECTION PER WC 5724-01010-41A, EM 5724-01010, AD 2018- 11-14, A CRACK WAS FOUND IN A HOLE AT THE END OF STRINGER L-6.5. CORRECTIVE ACTION: ER/A 585070-14AD REVISED TO REV. A. ACCOMPLISH ER/A 585070-14AD REV A SECTION II INSPECTIONS.SDR SWIA2020050150435Fastener · corrodedDAMAGED/ CORRODED HARDWARE ON PANEL 698MT, RT WING T/E. REF. CAMP# 20511101 (C-CHECK) RO 4/30/2020 REPLACED CORRODED/DAMAGED HARDWARE AND REINSTALLED PANEL 698MT IAW CRJ 200 SRM AND AMM.SDR SWIA2020050150434Fastener · corrodedDAMAGED/ CORRODED HARDWARE ON PANEL 698LT, RT WING T/E. REF. CAMP# 20511067 (C-CHECK) RO 4/30/2020 REPLACED DAMAGED AND CORRODED HARDWARE AND REINSTALLED PANEL 698LT IAW CRJ 200 SRM AND AMM.SDR SWIA2020050150433Fastener · corrodedDAMAGED/ CORRODED HARDWARE ON PANEL 698KT, RT WING T/E. REF. CAMP#20511065 (C-CHECK) RO 4/30/2020 REPLACED DAMAGED/CORRODED HARDWARE AND REINSTALLED PANEL 698KT IAW CRJ 200 SRM AND AMM.SDR SWIA2020050150432Fastener · corrodedDAMAGED/ CORRODED HARDWARE ON PANEL 698AB, RT WING T/E. REF. CAMP# 20511061 (C-CHECK) RO 4/30/2020 REPLACED DAMAGED/ CORRODED HARDWARE AND INSTALLED PANEL 698AB IAW CRJ 200 AMMSDR SWIA2020040649942Panel · chafedPANEL 599BB CHAFED (C-CHECK) RO 4/3/2020 PANEL 599BB BLENDED AND FOUND TO BE BEYOND LIMITS OF SRM; SEE CONTINUATION SHEET FOR DETAILS. PANEL 599BB REPLACED WITH NEW PN CC670-13056-3, LOCATED/DRILLED PER SRM. PANEL INSTALLED ON TRANS # 20446669.SDR ABXA2020030520042Panel · corrodedLH WING FUEKL TANK PANEL 533AB CORRODED. AIRCRAFT WAS GROUNDED.SDR FDEA202002200360Skin · crackedRIGHT WING TRAILING EDGE LOWER PANEL BETWEEN #8 AND #9 SPOILERS CRACKED. REPAIRED PANEL PER B757 SRM 57-51-01-2R.SDR REXA2020030200266Access Panel · gouged"DAMAGE T. DURING LH WING FUEL ACCESS PANEL INSTALL, GOUGE WAS FOUND ON ACCESS PANEL 551FB.
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"SUMMARY: FUEL ACCESS PANEL 551FB AT LH WING WAS REPLACED PER CRJ900 AMM 28-11-01. SDR GTIA2020021985021Skin · corrodedCORROSION FOUND ON LH WING TOP SKIN AT STATION 3059 O/B OF WX3622. RAF-01 OPENED. REF LTPR 5000973409-0010-REVIEWED NR#5000973409-0010 AND HAS BEEN ACCCOMPLISHED AS PER EO 5721-2002 ATTACHED TO J.O 1003097008-0010, REPAIR R572-58998 ISSUE F PERFORMED AND RDASRSDR C77A202002170006Skin · gougedDURING BASIC CHECK AT EAMS, GOUGE DAMAGE WAS DISCOVERED ON THE LH WING FIXED
LEADING EDGE SKIN (P/N 170-31031-021) OF AIRCRAFT 207AN BETWEEN RIB 1 AND RIB 4.
REFERENCE ETD2020-170-004771-A FIGURES 1 AND 2 FOR THE DAMAGE LOCATION AND
DIMENSIONS. THE DAMAGE ESDR SWIA2020030549037Skin · damagedWING FUEL TANK PANEL 640BB WING PLANK LANDING HAS AREAS OF PITTING (C CHECK) RO 3/2/2020 C/W REPAIR OF RH WING PLANK FUEL ACCESS LANDING LOWER (640BB) IAW REO. BLEND WAS FOUND OUTSIDE OF CRITICAL AREA. ORIGINAL .186, REMOVED .002, REMAINING .184 NO FURTHERSDR SWIA2020030549036Skin · damagedWING FUEL TANK PANEL 540BB WING PLANK LANDING HAS AREAS OF PITTING (C CHECK) RO 3/2/2020 C/W REPAIR OF LH WING PLANK FUEL ACCESS LANDING LOWER (504BB) IAW REO. BLENDOUT WAS OUTSIDE OF THE CRITICAL AREA WITH A REMAINING THICKNESS OF .188. FOUND TO BE WITHISDR R61A202003010305Skin · cracked** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** LH WING SLAT TRACK #5 CUTOUT CRACKED. REPAIRED AREA IAW ETD2020-170-005412. AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.SDR 2020FA0000161Skin · corrodedCORROSION DAMAGE WAS FOUND AT 5 SITES ON THE RH WING UPPER SKIN FROM CWS 363.9 TO 378.71. REFERENCE FAA FORM 8100-9 FIELD REPAIR FR-750-0201-7656 REV -, DATED 2/6/2020.SDR C77A202002170004Skin · gougedDURING BASIC CHECK AT EAMS, GOUGE DAMAGE WAS DISCOVERED ON THE RH WING FIXED LEADING EDGE SKIN (P/N 170-31031-022) OF AIRCRAFT 207AN BETWEEN RIB 1 AND RIB 2. REFERENCE ETD2020-170-004755 FIGURES 1 AND 2 FOR THE DAMAGE LOCATION AND DIMENSIONS. THE DAMAGE EXCEEDSDR C77A202002170001Skin · crackedTHIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH SB 170-57-0072 PART II, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION THAT CONSISTS OF REPLACING THE CURRENT RH WING TIP SPAR 1 (P/N 171-16231-002 OR 171-16231-004) WITH A NEW, REDESIGNED SPAR 1 (P/N 171-171-22480-40SDR SWIA2020040850050Skin Panel · damagedD: DAMAGE TO LH WINGLET OUTBOARD SKIN PANEL. COMPLIED WITH TEMPORARY REPAIR PER REO, PERMANENT REPAIR DUE WITHIN 5750 FH PER REV A OF REO. PERMANENT REPAIR DUE BY TAT 31330.1 C: MCI RA# 41829 NOTE: BUILT MX CODE TO TRACK 800 FLT HRS REINSP ***** DO NOT SDR IPXA2020031353136Doubler · wornINSPECTION TYPE:2CR/H WING FIXED L/E SKIN REPAIR DOUBLER HAS DEEP WEAR BETWEEN STA. XIS= 163.4 AND 164.972.REMOVED, INSPECTED AND REPLACED R/H WING FIXED L/E SKIN REPAIR DOUBLER BETWEEN STA. XIS= 163.4 TO 164.972 IAW VT-SAA EA 011-5740-01-A8035 REV. I/R AND UPSDR F3LA2020021850010Tip Cap · damagedSUPPLEMENT: 03/05/2020: R&R LEFT WING TIP ASSEMBLY PN D5735690300001, SN 11543-REF AMM 57-31-23-PB401. REMOVED AND REPLACED LH WING SLAT #5 PN D5746095000600, SN SA8202, IAW AMM27-84-67-PB401, REF NR 121228, WO401588 FOR CORRECTIVE ACTION. SIGNIFICANT DAMAGE TSDR F3LA2020021850011Tip Cap · damaged03/05/2020 SUPPLEMENT: REMOVED DAMAGED R/H WING TIP AND INSTALLED SERVICEABLE R/H WINGTIP IAW AMM 57-31-21-PB401. REMOVED PN D5735052101951A, SN 13572. REMOVED AND REPLACED R/H WINGTIP FENCH IAW AMM 57-31-22-PB401, PN D5735120000300A. SIGNIFICANT DAMAGE TO RH SDR IPXA2020031353131Filler · corrodedINSPECTION TYPE:2CLT WING T/E PANEL HAS BULGE FWD OF I/B AILERON.REPAIRED CORRODED LT WING T/E SPACER FILLER BETWEEN XORS 414 TO XORS 420 IAW VT-SAA EA 011-5700-01-A8051 REV. IR AND UPS EO MD11-5710-75648-A. (MINOR)SDR IPXA2020030352713Skin · corrodedINSPECTION TYPE:2CL/H WING UPPER FWD. SKIN HAS CORROSION BETWEEN STA. XORS,=222.65 TO 230.6.REPAIRED CORRODED L/H WING UPPER FWD. SKIN BETWEEN STA. XORS.= 222.65 TO 230.6 IAW VT-SAA EA 011-5730-01-A8038 REV. I/R AND UPS EO MD11-5730-75670-A. (MINOR)SDR IPXA2020030252619Doubler · crackedINSPECTION TYPE:2CLT WING FIXED L/E SKIN SPLICE DOUBLER AT XOS 789 IS CRACKED.REMOVED AND REPLACED CRACKED LT WING FIXED L/E SPLICE DOUBLER AT XOS 789 IAW MD-11 SRM 51-33-01. (MINOR)SDR IPXA2020022875553Landing · crackedINSPECTION TYPE:2CL/H WING FIXED L/E LOWER STRINGER (PANEL LANDING) IS CRACKED AT STA. XOS.= 906.5607.REPAIRED CRACKED L/H WING FIXED L/E LOWER STRINGER AT STA. XOS.= 906.5607 IAW SRM 57-40-03 REPAIR 1 FIG. 201. (MAJOR)SDR IPXA2020022435378Skin · crackedINSPECTION TYPE:2CL/H WING L/E LOWER SKIN IS CRACKED AT STA. XOS= 776.REPAIRED CRACKED L/H WING L/E LOWER SKIN AT STA. XOS.= 776 IAW SRM 57-40-02 REPAIR 7 FIG. 201. (MAJOR)SDR DALA2020022041275Skin · damagedFOUND RHW LOWER SKIN STRINGER L-6.5 HOLE NO.2 DIAMETER BEFORE OVERSIZING 0.515", THE HOLE OUT OF LIMIT. REPAIRED PER ERA 5844524-14. (LP 41489069)SDR YENA2020021840180Skin · corrodedDURING HEAVY MAINTENANCE, REF AEROMAN W/O 2020-12/1 WCC 2020-42262, CORROSION ON TOP SKIN, LOWER SURFACE, TRAILING EDGE, REAR SPAR, RIB 16 PLUS 20 INCHES ON LH WINGL; REF AEROMAN W/O 2020-12/1, WCC 2020-42262, EVALUATED EXISTING REWORK LOCATED RIB 16 + 20, TOPSDR SWIA2020032649388Skin · damaged* LH WING €“ RADIUS OF LANDING FOR PANEL 550HB HAS SIGNS OF PITTING IN MULTIPLE LOCATIONS AROUND PERIPHERY. (C-CHECK) RO 3/25/2020 REPAIRED L/H WING LANDING FOR ACCESS PANEL 550HB REF REO SEE. CONTINUATION CARD FOR DETAILSSDR SWIA2020032649387Skin · damaged* LH WING €“ LANDING FOR ACCESS PANEL 540BB HAS PITTING (AREA MARKED). (C-CHECK) RO 3/25/2020 REPAIRED L/H WING ACCESS PANEL CUTOUT AT 540BB REF REO. SEE CONTINUATION CARD FOR DETAILSSDR CALA2020021600425Skin · crackedLH INBD DIAGONAL BRACE FITTING HAS 2 FASTENER HOLE CRACK INDICATIONS MARKED. REF: AAR N/R 9756230 SEE ECRA 5720-03163 L/H WING UPPER SKIN, FWD DRAG FITTINGS, AND SHIM REPLACEMENT INTERIM REPAIR. ON OR BEFORE JAN 23 2022 OR THE ACCUMULATION OF 21975 TOTAL FLT CSDR CALA2020021600424Skin · crackedLH DRAG BRACE FITTING SKIN HAS FASTENER HOLE CRACK INDICATION AT FASTENERS 5, 9, 14, 17 & 18. REF. A EE ECRA 5720-03163 L/H WING UPPER SKIN, FWD DRAG FITTINGS, AND SHIM REPLACEMENT INTERIM REPAIR. ON OR BEFORE JAN 23 2022 OR THE ACCUMULATION OF 21,975 TOTAL A/
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