JASC 5712
Service difficulty reports · 6,959
Reports filed under 5712 · Wing, Rib/Bulkhead, 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 = '5712' 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 = '5712' 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 EE4Y2024032219622Rib · corrodedDURING THE STRUCTURAL INSPECTION PER ALLEGIANT TASK CARD 572179-01-1-002 RELATED TO MPD TASK 572179-01, IT WAS FOUND AT RH WING REAR SPAR AREA THE RIBLET J WITH CORROSION. SINCE THAT THE MENTIONED RIBLETS HAVE DEEP CORROSION, THEY WILL BE REPLACED BY NEW ONES.SDR EE4Y2024032219621Rib · corrodedDURING THE STRUCTURAL INSPECTION PER ALLEGIANT TASK CARD 572179-01-1-002 RELATED TO MPD TASK 572179-01, IT WAS FOUND AT RH WING REAR SPAR AREA THE RIBLET E WITH CORROSION. SINCE THAT THE MENTIONED RIBLETS HAVE DEEP CORROSION, THEY WILL BE REPLACED BY NEW ONES.SDR CALA2024040200935Rib · crackedDURING INSPECTION OF ACCESS PANEL 541DB, IT WAS A CRACKED RIB AT POSITION RIB 13 AND BETWEEN STGR 4/5 ON LH SIDE. THE JACKING OF THE AC FULLY ACCOMPLISHED AS PER ECRA#0711-01085 INSTRUCTIONS AND FULLY ACCOMPLISHED RIB#13 WEB REPLACEMENT AS PER ECRA#5220-03391.SDR FDEA202403150438Rib · gougedLH WING SPOILER #6 ACTUATOR INBD JACK RIB LOWER HOLE GOUGE ACCOMPLISHED THE CAT.A REINFORCEMENT REPAIR AT LH WING #6 SPOILER JACK RIB STA SP1X 31.675, THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5740- T0378536 P1, SEQ NO:1164, TITLESDR SWAA2024031462367Rib · damagedRIGHT WING DEFLECTION CONTROL RIB UPPER TAB IS BROKEN/SEPARATED<[01] PERFORMED HFEC IAW BOEING NDT MANUAL PART 6 51-00-00 PROCEDURE 23 IN COMPLIANCE WITH SRM 57-51-02-2R-3 REPAIR 3 - WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB CRACK DAMAGSDR IPXA2024040221180Rib · crackedZONE 513 LT WING, FWD WING ROOT STA71/RIB2 LEADING EDGE RIB HAS A CRACK. INSTALLED REINFORCED ANGLE P/N: A5724199320200 AT FWD WING ROOT RH RIB 2. IAW SRM 51-40-21.SDR VNAA202404150005Rib · crackedCRACK ON MACHINED RIB LEADING EDGE SS57.16 AT RIGHT WING. CRACK ON MACHINED RIB LEADING EDGE SS57.16 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-240 REV --SDR VNAA202404090011Rib · corrodedCORROSION ON WINGLET LOWER CLOSING RIB AT RH WINGLET CORROSION ON WINGLET LOWER CLOSING RIB AT RH WINGLET WAS REPAIRED PER REO 690-57-31-229 REV. --SDR VNAA202404150008Rib · crackedAFTER INTERNAL ZONAL INSPECTION, CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING WAS REPAIRED PER REO 690-57-51-339 REV.--SDR VNAA202404150006Rib · crackedCRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-338 REV --SDR IXXA2024030401Rib · mismarkedRH WING, OUTBOARD TRAILING EDGE, FWD OF OUTBOARD EDGE OF OUTBOARD AILERON, FLANGE HAS DRILL START/STRIKESDR IXXA2023030401Rib · mechanic errorRH WING, OUTBOARD TRAILING EDGE, FWD OF OUTBOARD EDGE OF OUTBOARD AILERON, FLANGE HAS DRILL STRIKESDR VNAA202404090006Rib · crackedAFTER ACCESS PANEL 521BL REMOVAL , CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING. LH INBOARD FIXED L/E RIB AT STA 57.16 WAS REPAIRED PER REO 690-57-41-420 REV. --SDR VNAA202404080016Rib · elongatedELONGATED HOLES ON LH INBOARD FIXED L/E MACHINED RIB AT SLAT STA. 57.16, PERFORM PERM REPAIR IAW ENGINEERING DISPOSITION.L LH INBOARD FIXED L/E RIB AT STA 57.16 WAS REPAIRED PER REO 690-57-41-420 REV. --SDR SWIA20240425224Rib · cracked* R/H WING FIXED LEADING EDGE RIB AT SS57.16 HAS A CRACK IN THE UPPER ATTACH FLANGE NEAR THE FRONT SPAR, MARKED. (C-CHECK RO 4/24/2024) REPAIRED R/H WING FIXED LEADING EDGE RIB CRACK IN THE UPPER ATTACH FLANGE NEAR THE FRONT SPAR AT SS57.16 REF. REO 670-57SDR REXA2024080600637Rib · crackedFLS 36 RIB AFT R/H HAS A CRACK REQUIRES REPLACEMENT LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE RIB, AFT, INB, FLAT, P/N CC670-14163-2, IAW CRJ-900 SRM 51-42-06-001-001-A01.SDR ABXA2024021900639Rib · gougedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, GOUGE DAMAGE WAS FOUND ON THE RH WING L/E RIB AT OFSS 427. THE POST-BLEND MEASUREMENT HAS MATERIAL REMAINING OF 0.025" AND 0.029" FROM INITIAL THICKNESS OF 0.060". THAT'S LESS THAN 50% REMAINING. THE ALLOWABLE PSDR VNAA202403230010Rib · crackedAFTER ACCESS PANEL 521BL REMOVAL, CRACK ON MACHINED RIB LEADING EDGE SS 57.16 AT LEFT WING. (SM). MACHINED RIB LEADING EDGE SS 57.16 AT LEFT WING. (SM) WAS REPAIRED PER REO 690-57-41-240. REV. --SDR SWIA20240308214Rib · damagedDAMAGE FOUND ON LH WING FWD CLOSING RIB P/N 601R10854-29 AT WS389.00 IS OUT OF LIMITS AND CLASSIFIED TO BE A MAJOR REPAIR.INITIATED FORM M-337.SEE CP 27816132 FOR ORIGINAL DISCREPANCY. FILED CLOSEDREMOVED AND REPLACED LH WING FWD CLOSING RIB AT WS389.00 IAW SDR HNAA2024022700141Rib · crackedE017252 POSSIBLE CRACKS ON RH WING RIB 21. FABRICATED AND DRILLED DOUBLER, FILLER, AND SHIM AND INSTALLED REPAIR OF R/H WING RIB 21 IAW EMB 145 SRM 57-50-07 ITEM 4 FIG 203 AND EO1-57-24-0130SDR VNA2024F00002Rib · crackedAFTER ACCESS PANEL 621BR REMOVAL, CRACK ON MACHINED RIB LEADING EDGE SS 57.16 AT RIGHT WING. CRACK ON MACHINED RIB LEADING EDGE SS 57.16 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-240. REV. - -SDR VNAA202402290020Rib · crackedAFTER ACCESS PANEL 521BL REMOVAL TO SLAT LUBRICATION, CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING. MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING WAS REPAIRED PER REO 690-57-41-240 REV - -SDR VNAA202402050019Rib · crackedCRACK WAS FOUND ON RIB LEADING EDGE SS57.16 AT RH WING. RIB LEADING EDGE SS57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV - -SDR SWAA2024022649057Rib · wornLEFT WING DEFLECTION CONTROL RIB JUST O/B OF I/B AFT FLAP WORN.<[01] REMOVED I/B AND O/B SERRATED PLATES PER SRM 51-40-02.;[02] REMOVED DAMAGE ON LEFT WING DEFLECTION CONTROL RIB TAB PER SRM 57-51-02-2R-4.;[03] REMOVED DAMAGE ON LEFT WING FIXED TRAILING EDGE SSDR VNAA20240212009Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 AT LH WING. RIB LEADING EDGE SS57.16 AT LH WING WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01SDR AALA202403216448Rib · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION AND DAMAGE FOUND ON RIGHT WING, RIGHT HAND MAIN LANDING GEAR AFT SUPPORT RIB FORWARD LUG AFT FACE. MAINTENANCE REPAIRED SUPPORT RIB PER EA 351093ASDR SWAA2024022047374Rib · crackedLEFT WING TRAILING EDGE RIB IS CRACKED AT DEFLECTION RIB PANEL .<[01] RIB WAS REPLACED ON NR TTG8Q00R8TCV LINE #1207;[02] VERIFIED RIB WAS REPLACED ON NR TTG8Q00R8TCV LINE #1207SDR AALA202401308534Rib · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT WING AILERON CLOSURE RIB AT RWS 1263.60. REPAIRED RIB PER EA 350837 AND EO 5720D009.SDR YENA2024012900125Rib · crackedDURING HEAVY MAINTENANCE: CRACK ON RIB 22 AT FIXED LEADING EDGE LH WING ; (RESOLVED ON W/O: 1267464 TASKCARD: NR-00126) REF TOMX W/O# 2452 N/R 00131. CRACK AT RIB ON RIB 22 AT FIXED LEADING EDGE LH WING WAS REPAIRED PER ETI-190-23-741 REV. 3, ETD2023-190-03249SDR YENA2024012900123Rib · corrodedDURING HEAVY MAINTENANCE: AFTER NUT PLATES REMOVAL ON THE RH WING RIB 42. CORROSION WAS FOUND ; (RESOLVED ON W/O: 1267464 TASKCARD: NR-00128) REF TOMX W/O# 2452 N/R 00432. CORROSION ON RIB 42 OF RH WING WAS REMOVED AND EVALUATED OUT OF LIMITS THEREFORE WAS REPSDR YENA2024012900122Rib · corrodedDURING HEAVY MAINTENANCE: AFTER NUT PLATES REMOVAL ON THE RH WING RIB 42. CORROSION WAS FOUND ; (RESOLVED ON W/O: 1267464 TASKCARD: NR-00128) REF TOMX W/O# 2452 N/R 00432. CORROSION ON RIB 42 OF RH WING WAS REMOVED AND EVALUATED OUT OF LIMITS THEREFORE WAS REPSDR YENA2024012900114Rib · crackedDURING HEAVY MAINTENANCE: WINGS / LH WING / FIXED LEADING EDGE / RIB 22 / CRACK - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR).SDR AALA202401300911Rib · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT WING AILERON CLOSURE RIB AT LWS 1263.60. REPAIRED RIB PER EA 350837 AND EO 5720D009.SDR FDEA202401250166Rib · corrodedRH #3 SPOILER JACK RIB I/B UPPER BORE FOUND CORROSION ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #3 SPOILER JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377948 P1, SEQ NO:636, MAJOR REPAIR.SDR VNAA202402290022Rib · crackedCRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING WAS REPAIRED PER REO 690-57-51-322 REV.--SDR VNAA202402290021Rib · crackedCRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-323 REV.--SDR VNAA202402290019Rib · crackedAFTER ACCESS PANEL 621BR REMOVAL TO SLAT LUBRICATION, CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING. CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-240 REV - -SDR IXXA2024030601Rib · gougedLH WING INTERNAL RIB 28 INBD FACING WEB SURFACE IS GOUGED IN LINE WITH STRINGER L-9 VIEWED THROUGH ACCESS HOLE 541TBSDR SWAA2024021248664Rib · crackedCRACK ON INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB AT RT WING 2024-67274<[01] TOOL USED: EDDY CURRENT EQUIPMENT. P/N: NORTEC 600D. S/N: 200048001. DUE DATE: 01-MAY-24.;[02] REPAIRED INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB AT RT WING IAW B73SDR EE4Y2024011619219Rib · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 572112-01-1-001 LH WING RIBLET E CORRODED WAS FOUND. DUE TO FLIGHT BY WIRE CABLES PASSING THROUGH THE RIBLET E AND THE AMOUNT OF WORK TO REMOVE THEM, AIRBUS WAS CONTACTED FR ALTERNATIVE METHOD OF INSTALLATION. AIRBUSSDR FDEA202401150167Rib · gougedRH #5 SPOILER JACK RIB O/B LOWER BORE FOUND GOUGE ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #5 SPOILER JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377951 P1, SEQ NO:637, TITLE:WINGS-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIB AT STA ABX184.625-BEAM ATTACHMENT HSDR VNAA202401220011Rib · damagedPERM REPAIR BEFORE 20,826.13 FH - TAPE APPLIED - LH FIXED LE SKIN PANEL 521BL AND RIB WITHIN 800 FH FROM IR (BEFORE 20,826.13 FH), REPLACE OR REPAIR THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. RIB WAS REPAIRED PER REO 690-57-41-408 REV. -- ANSDR IPXA2024012202767Rib · cracked**SUPPLEMENTAL SDR**FAULT- CRACK - WEB, RH WING BL 255.692 FXD TE RIB. (REPAIR) C/W REVIEWSDR DALA2024010900349Unknown · unknownSHIP 3120 ELONGATED HOLE LOWER SURFACE AT CUT OUT BTW RIB17 TO RIB18 FUEL TANK O N LH WING. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON LOWER SURFACE AT CUT OUT BTW RIB17 TO RIB18 FUEL TANK ON LH WING AS PER A319 SRM 57-21-11-300-002. (0141860)SDR IPXA2024010802767Unknown · unknown*SDR FILED OPEN* FAULT- CRACK - WEB, RH WING BL 255.692 FXD TE RIB. (REPLACE) OK TO WORKSDR VNAA202401040028Rib · crackedCRACK WAS FOUND ON RIB LEADING EDGE SS57.16 AT RH WING. STEP 1 TO STEP 4 WAS PERFORMED PER REO 690-57-41-240 REV. -- AND DUE ADYACENT CRACK WAS FOUND RIB LEADING EDGE SS57.16 AT RH WING WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 , CRJ900 SRM 51-42-21-00SDR VNAA202401040027Rib · crackedCRACK WAS FOUND ON RIB LEADING EDGE SS57.16 AT LH WING. STEP 1 TO STEP 4 WAS PERFORMED PER REO 690-57-41-240 REV. -- AND DUE ADYACENT CRACK WAS FOUND RIB LEADING EDGE SS57.16 AT LH WING WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 , CRJ900 SRM 51-42-21-00SDR SWAA2024011134472Rib · crackedRIGHT WING TRAILING EDGE; UPPER O/B FASTENER OF DEFLECTION CONTROL RIB IS CRACKED (MARKED)<[01] REMOVED AND REPLACE TRANSVERSE WEB COMMON TO DEFLECTION CONTROL RIB IAW SRM 51-40-02 AND AIPC 57-50-00-36A.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MESDR SWAA2024012932494Rib · crackedRH WING T/E RIGHT ABOVE #2 ENGINE AFT FAIRING TIP THERE IS A RIB CRACKED AT THE BOTTOM BOLT ATTACHMENT HOLE. DOT 82-002.<[01] THIS N/R WAS ACCOMPLISHED ON N/R: TTG8Q00Q7JM0.;[02] VERIFIED STEP 1SDR VNAA202401210008Rib · crackedAFTER INTERNAL ZONAL INSPECTION, CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-319 REV. --
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