JASC 5712
Service difficulty reports · 6,970
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 WRLA2009085Rib · crackedDURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON RIGHT WING FIXED L/E CAVITY XOS1025 - LOWER RIB CRACKED FROM FASTENERS AREA (REF EGAT N/R U50534). REPAIR THIS CRACKED RIB PER MD-11 SRM 57-00-01 VOL 1 FIG 10 REV 40. JOB COMPLETED AND CONDITION CHECK NORMALSDR DU4R2009337Panel · dentedDURING SCHEDULED INSP, FOUND LT HORIZ STAB L/E PNL 9150L HAD NUMEROUS HAIL DENTS.SDR WRLA2009078Doubler · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON DOUBLER OF RIGHT WING FIXED L/E CAVITY UPPER RIB AT STA XOS789 (REF EGAT N/R U05018). REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-358 REV 00, INSTSDR WRLA2009077Doubler · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON DOUBLER OF RIGHT WING FIXED L/E CAVITY UPPER RIB AT STA XOS667. REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-358 REV 00, INSTALLED THIS DOUBLER IAW SDR WRLA2009076Doubler · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON DOUBLER OF LT WING FIXED L/E CAVITY UPPER RIB AT STA XOS667. REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-355 REV 00, INSTALLED THIS DOUBLER IAW SRMSDR WRLA2009075Doubler · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON DOUBLER OF LT WING FIXED L/E CAVITY UPPER RIB AT STA XOS789. REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-357 REV 00, INSTALLED THIS DOUBLER IAW SRMSDR WRLA2009073Rib · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON LWR CHORD OF LT WING FIXED L/E NOSE CAVITY NEARBY FASTENER AT STA XOS546. REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-338 REV 00, INSTALLED THIS DOSDR IPXA09655175Stiffener · crackedINSPECTION TYPE:C WING CENTER SECTION FWD BULKHEAD VERTICAL STIFFENER FOUND CRACKED JUST AT RBL 10, WL 195. CRACK 3.75 INCH LENGTH. WING CTR SECTION FWD BULKHEAD STA 785.9 WL 195 RBL 10 VERTICAL STIFFENER REPAIRED AS PER HX RS R57-11-36287 REV B AND UPS EO BSDR FDEA200903171433Skin · wornLT WING FIX LEADING EDGE BTW SCREWJACK 3 AND SCREWJACK 4 WITH WEAR. FIX L/E REPAIRED AS PER EA 6-5710-127425.SDR SWAA091767Rib · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT WING LOWER CHORD CRACKED AT BS 135.5, BETWEEN STR 2R TO STR 3R. REPAIRED CHORD PER ACO.SDR SWAA091677Rib · crackedDURING SCHEDULED 20Y CHECK, FOUND LT WING LOWER CHORD CRACKED AT BS 135, BETWEEN STR 2L TO STR 3L. REPAIRED CHORD PER ACO.SDR UALA2009031200769Rib · crackedLT WING CHORD UPPER FLANGE CRACKED 2 INCHES AT WS 304. ASSEMBLED REPAIR PIECES AND INSTALLED RIB WITH REVISED EVA UA-EVA-72388A. ACCMP'D RIB INSP.SDR SWAA091482Rib · crackedDURING SCHEDULED SPV CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135, BETWEEN STR 3R TO STR 2R. REPAIRED CHORD PER ACO.SDR 2009FA0000181Rib · crackedDURING ANNUAL INSP, NUMEROUS CRACKED L/E RIBS WERE FOUND BETWEEN 66.3750 INCH TO 173.7500 INCH ON THE LT WING AND 86.6250 INCH TO 201 INCHES ON THE RT WING. THESE CRACKS WERE IN THE RIB BODY AND RAN ALONG THE UPPER SKIN ATTACH FLANGE. THE CRACKS STARTED AT TSDR FDEA200902280768Rib · crackedRT WING L/E FOUND CRACK ON INT RIB LOWER SIDE L/E. REPAIRED AREA IAW SRM 57-00-01, FIG 10, SHT 1, VOL I.SDR FDEA200902280767Rib · crackedRT WING L/E FOUND CRACK ON RIB LOWER INT L/E. REPAIRED AREA IAW SRM 57-00-01, FIG 10, SHT 1, VOL I.SDR CALA2009022700117Rib · wornRIGHT WING RIB ASSEMBLY BETWEEN NR 7 AND 8 SPOILER IS WORN AT UPPER TRAILING EDGE PANEL ATTACH POINT. REPAIRED PER ECRA 5750-03581.SDR LR7A2009030900017Rib · crackedDURING SCHEDULED C-8 CHECK PER JOB CARD HSP57119, FOUND RT CENTER WING AUX TANK COMPT RIB FOOT CAP CRACKED AT FS 522, CWS139R, WL256.5. REPAIRED IAW LAC MEA 382-57-09-008.SDR UALA2009021900561Rib · crackedRT WING RIB CHORD AT WBL 135.5 IS CRACKED AT AFT LOWER RIB CLIP. MAJOR REPAIR ACCOMPLISHED PER EA 080161 REV IR.SDR SWAA091045Rib · crackedDURING SCHEDULED 24Y CHECK, FOUND RT HORIZONTAL WING FLANGE RIB CRACKED AT WBL 135, BETWEEN STR 2R TO STR 3R. REPAIRED RIB PER ACO.SDR WRLA2009052Rib · crackedDURING C-CHECK IN TPE INSPECTION FOUND CRACK ON LT WING FIXED L/E PANEL RIB AT STA XORS 441. REPAIRED CRACK AREA IAW SRM 57-00-01 FIG 11 REV 40.SDR FDEA200901290397Rib · crackedLEFT WING LEADING EDGE COMPARTMENT CEILING UPPER SUPPORT RIB FOUND CRACKED AT APPROXIMATELY XORS 634 NEAR TO OUTBOARD SIDE OF NR 11 SLAT TRACK. REMOVED AS PER SRM 51-31-01 VOLUME II. RIB FABRICATED AS PER DRAWING ARB2923 AND INSTALLED AS PER SRM 51-31-01 VOLSDR NWAA09213224Rib · crackedDURING H-CHECK, FOUND CRACK ON RT WING RIB NR4 AT INBD FACE OF SKIN ATTACHMENT AREA BETWEEN STR 6 AND 7. REPAIRED IAW EA 32-211588. (K)SDR SWAA090473Rib · crackedDURING SCHEDULED 14Y CHECK, FOUND RT WING RIB CRACKED AT BS 135. REPAIRED RIB PER ACO.SDR FDEA200901160228Rib · crackedLEFT WING RIB 5 FWD ATTACHMENT FLANGE AT THE AFT SPAR HAS A CRACK INDICATION AT HOLE "K". STARTED REAMING HOLE "K" TO 0.816. COLD WORKED HOLE "K". FINAL REAMED HOLE "K" TO 843. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLED NEW FASTENER IAW EO 6-57SDR FDEA200901160227Rib · crackedLEFT WING RIB 5 FWD ATTACHMENT FLANGE AT THE AFT SPAR HAS A CRACK INDICATION AT HOLE "G". STARTED REAMING HOLE "G" TO 0.816. COLD WORKED HOLE "G" USING STDN 26-2-N TOOLING. FINAL REAMED HOLE "G" TO 843. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLESDR FDEA200901160220Rib · crackedRIGHT WING RIB 5 AT HOLE "N" HAS A CRACK INDICATION. STARTED REAMING HOLE TO 0.816. COLD WORKED HOLE USING STDN 26-2-N TOOLING. FINAL REAMED HOLE TO 0.844. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLED NEW FASTENER R570.40017.212 IAW EO 6-5710-1236SDR FDEA200901160219Rib · crackedRIGHT WING RIB 5 AT HOLE "J" HAS A CRACK INDICATION. STARTED REAMING HOLE TO 0.816. COLD WORKED HOLE "J" USING STDN 26-2-N TOOLING. FINAL REAMED HOLE TO 0.844. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLED NEW FASTENER R570.40017.206 IAW EO 6-5710-SDR SWAA090275Rib · crackedDURING SCHEDULED 16Y CHECK, FOUND LT WING FUEL TANK WING RIB LOWER CHORD CRACKED AT WBL 135, BETWEEN STR 2 TO STR 3. REPAIRED RIB PER ACO.SDR SWAA090274Rib · crackedDURING SCHEDULED 16Y CHECK, FOUND RT WING FUEL TANK WING RIB LOWER CHORD CRACKED AT WBL 135, BETWEEN STR 2 TO STR 3. REPAIRED RIB PER ACO.SDR FDEA200901120151Rib · crackedLEFT WING TIP RIB WY489 CRACKED REMOVED CRACKED RIB WY489.0 IAW SRM 51-40-21. FABRICATED NEW RIB ON TRAVELER NR T8/773917, BATCH NR 436186A1. INSTALLED RIB IAW SRM 51-40-21, AND 57-30-11.SDR FDEA200901050032Rib · crackedCOMPLY WITH EA 6-5710-123695. REWORKED HOLE TO 5.000". FABRICATED BUSHINGS "E" AND "F"; CAD PLATED BUSHINGS AND INSTALLED BUSHINGS "E" AND "F" IAW EA 6-5710-123695 "WINGS - AD2007-02-09 - WINGS GEAR RIB 5 FWD LUG BORE REWORK (RHS)".SDR UPS08M54243Rib · mismanufacturedINSPECTION TYPE:N/A MAJOR REPAIR- RT LWR WINGLET, RIB MISSING LIGHTENING. REPAIRED RIB AS PER MD11-5720-31667.SDR CA090107004Rib · cracked(CAN) DURING MX, RIB P/N 40423-06, WHICH RUNS THROUGH THE LT WW, WAS FOUND CRACKED THROUGH AT THE NARROWEST PART OF THE RIB AT THE TOP CENTER OF THE WW. THE WING SKIN IMMEDIATELY ABOVE AND ATTACHED TO THE RIB ALSO HAD A SMALL CRACK WHICH COINCIDED WITH THE RIBSDR FDEA200812225257Rib · crackedRT WING FIXED LEADING EDGE SLAT TRACK 16 INBD RIB FOUND CRACKED. RIB REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-35-01 VOLUME II AND SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR USAA2009011290065Rib · crackedNR 03-0528-8-0176/001 AND 6099288 - CRACK ON RT WING RIB LOWER CHORD WEB AT WBL 135.5. REPAIRED RT WING RIB LOWER CHORD WEB AT WBL 135.5 IAW EA NR 100777.SDR USAA2008121792254Rib · crackedCLT - Q5 - MAJOR REPAIR - RIGHT WING RIB WEB LOWER CHORD CRACKED AT WBL 135.5, 7 INCHES FORWARD OF AFT SPAR AT LOWER SKIN. REPAIRED RIGHT WING RIB WEB LOWER CHORD CRACKED AT WBL 135.5, IAW US AIRWAYS EA 100777.SDR FDEA200812125124Rib · crackedLT WING LEADING EDGE, FOUND CRACK AND RIVETS U/S ON ANGLE SUPPORT REFUEL PANEL. REPAIRED RIB IAW SRM57-00-01 VOL I, FIG 10, SHT 1,3,4.SDR SWIA200820632Rib · crackedSVC CHECK, RIGHT WING LEADING EDGE, INBOARD RIB ASSEMBLY IS CRACKED IN TWO PLACES. REPLACED PER SRM.SDR ASOA200801589Rib · crackedLT WING BATT RIB ASSY AT WS 53.60 IS CRACKED .800 INCH LONG JUST AFT OF TOP AFT FASTENER BEFORE THE RADIUS. COMPLIED WITH REPAIR TO LT BATT RIB AT WS 53.60 REPAIR IAW BOMBARDIER REO 601R-57-51-046.SDR FDEA200811264988Rib · crackedLEFT WING RIB 5; HOLE "O" HAS A CRACK INDICATION. COMPLIED WITH FEDEX EA 6-5710-123674, WINGS, AD 99-16-01 - EO 6-5710-7-5005, LT WING REAR SPAR, RIB 5 FITTING BOLT HOLE "G", "I", "M", AND "O".SDR FDEA200811264987Rib · crackedLEFT WING RIB 5; HOLE "M" HAS A CRACK INDICATION. COMPLIED WITH FEDEX EA 6-5710-123674, WINGS - AD 99-16-01 - E.O. 6-5710-7-5005, LT WING REAR SPAR, RIB 5 FITTING BOLT HOLE "G", "I", "M" AND "O". ORGINAL EA IS ATTACHED TO SNRM N00846.SDR FDEA200811264986Rib · crackedLEFT WING RIB 5; HOLE "I" HAS A CRACK INDICATION. COMPLIED WITH FEDEX EA 6-5710-123674 WINGS, AD 99-16-01 - EO 6-5710-7-5005, LT WING REAR SPAR, RIB 5 FITTING BOLT HOLE "G", "I", "M", AND "O". ORIGINAL EA ATTACHED TO SNRM N00846.SDR FDEA200811264985Rib · crackedLEFT WING RIB 5; HOLE "G" HAS A CRACK INDICATION. COMPLIED WITH FEDEX EA 6-5710-123674 WINGS - AD 99-16-01 - EO 6-5710-7-5005 - LT WING REAR SPAR, RIB 5 FITTING BOLT HOLE "G", "I", "M", AND "O". ORIGINAL EA ATTACHED TO SNRM N00846.SDR FDEA200811264980Rib · damagedRIGHT WING RIB 5; HOLE "E", THE EXISTING HOLE SIZE IS LARGER THAN THE FINAL HOLE SIZE CALLED OUT IN FEDEX EO 6-5710-7-5005 P1. COMPLIED WITH FEDEX EA 6-5710-123672, WINGS - AD 99-16-01 - EO 6-5710-7-5005, RT WING REAR SPAR MLG FWD PICK-UP FITTING BOLT "E".SDR WRLA2008096Rib · crackedCRACK- DURING BRIDGE CHECK + C4 CHECK, EGAT MECH FOUND LT WING FIXED L/E RIB CRACK ON FUELING PANEL OTBD LOWER SIDE AT XORS=538. REPAIRED CRACK AREA IAW ENGINEERING INSTRUCTION W2008A57B-1290 AND EI W2008A57B-1290 REV 01.SDR WRLA2008095Rib · crackedDURING BRIDGE CHK + C4 CHK, EGAT MECH FOUND LT WING FIXED LE INTERNAL SUPPORT RIB CRACK AT STA XORS=484. REPAIRED AREA IAW ENGINEERING INSTRUCTION W2008A57B-1288 REV 00 AND EI W2008A57B-1288 REV 01.SDR 08FDEA04968Rib · crackedLT WING L/E RIB LWR CHORD HAS 2 CRACKS AT 5 INCH AND 18 INCH FROM SPAR, FSS 122. REMOVED PNL 6301 TO FOM. FABRICATED ANGLE REF DWG 64-8342-19 DRILLED-UP, TREATED, PRIMED, AND INSTALLED ANGLE REF SRM 51-30-5, MM 51-20-021, MM 51-20-051, AND SRM 51-30-2. INSTSDR SWAA086473Rib · crackedDURING SCHEDULED 20Y CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 TO STR 3. REPAIRED RIB PER ACO.SDR CA081215005Rib · bent(CAN) DURING MAINTENANCE WALK AROUND ON AIRCRAFT, IT WAS FOUND THAT THE LT WING AT WS 244.45 HAS A SLIGHT BEND IN THE UPWARD DIRECTION APPROXIMATELY 1 INCH AS MEASURED FROM WS 244.45 TO WING TIP. FURTHER INVESTIGATION CARRIED OUT. AIRCRAFT DE-FUELED AND LT W
Back to JASC 5712