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 07FDEA02091Rib · crackedRIGHT RIB CHORD UPPER VERTICAL FLANGE HOLE AT STATION 760.95. LOWER FWD HOLE (B), RELEVANT CRACK INDICATION NOTED AT THE 9 O`CLOCK POSITION LOOKING I/B. MADE TEMPORARY REPAIR PER ENGINEERING AND AIRCRAFT WAS FERRIED TO VENDOR FOR PERMANENT REPAIR.SDR UPS07849952Rib · crackedINSPECTION TYPE:C3 RIGHT OUTBOARD LEADING EDGE LWR RIB CRACKED AT XFS 634. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 EA. REPAIR ANGLES IAW 57-02-0 FIG 02, 51-1-20D.SDR UPS07849948Rib · crackedINSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT STA XFS 722. STOP DRILLED CRACKED RIB AT STA XFS 722 IAW SRM 57-02-00. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XFS 722 IAW SRM 57-02-00 FIG 2.SDR UPS07849947Rib · crackedINSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT STA XFS 634. STOP DRILLED CRACKED RIB AT STA XFS 634 IAW SRM 57-03-03-0. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XFS 634 IAW SRM 57-02-00 FIG 2.SDR UPS07849944Rib · crackedINSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT STA XFS 672. STOP DRILLED CRACKED RIB AT STA XFS 672 IAW SRM 57-02-00. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XFS 672 IAW SRM 57-2-0 FIG 2.SDR UPS07849943Rib · crackedINSPECTION TYPE:C2 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT STA XFS 616. STOP DRILLED CRACKED RIB AT STA XFS 616 IAW SRM 57-02-00. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XFS 616 IAW SRM 57-02-00 FIG 2.SDR DHL2007803528Rib · crackedNR 4 STUB WING RIB CRACKED STA XOLDO 67.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00364-001, DOUGLAS DWG NR 9753297. REMOVED CRACKED RIB IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED SDR CALA0700289Vapor Barrier · crackedINSPECTION FOUND FIVE CRACKS IN THE RT WHEEL WELL FORWARD BULKHEAD (WING CENTER SECTION AFT SPAR VAPOR BARRIER). THREE OF THE CRACKS WERE LOCATED AT THE B-SYSTEM RETURN FILTER, ONE AT RBL 45, AND ONE AT RBL 25. THE VAPOR BARRIER WAS REMOVED AND REPLACED IAW SDR QXEA200700896Rib · damagedC4 PDX - RIGHT WING COVE RIB UNDER INBOARD SPOILER HAS MISDRILLED RIVET HOLE ON BOTTOM FLANGE AT WS YW 285. REPAIRED IAW RD8/4-57-811 AD SRM 51-42-05.SDR 07FDEA02001Rib · crackedRT WING LOWER RIB CHORD HAS 2 CRACKED LUGS CRACKS EXTEND ABOVE HORIZONTAL FLANGE OF CHORD. REPAIRED IAW SRM 57-20-00 FIG 21 SHT 1 VOL 1.SDR DLM88070646Rib · brokenBROKEN RIB IN LT FIXED L/E AT STA XFS=218. RIB REMOVED IAW SRM 51-30-2. RIB AND DOUBLER INSTALLED IAW SRM 51-06B FIG 17 N/R T0056247.SDR ABXA070215Rib · corrodedCORROSION WS 564, RIGHT WING LEADING EDGE PANEL SUPPORT/RIB. REPLACED STRUT RIB IAW B767 SRM 51-40-02.SDR ABXA070214Rib · corrodedCORROSION WS 720, RIGHT WING LEADING EDGE LOWER PANEL SUPPORT/RIB. REPLACED STRUT RIB IAW B767 SRM 51-40-02.SDR 2007UALA01556Stiffener · crackedWHEEL WELL FWD BULKHEAD HAS CRACKED STIFFENER JUST FWD OF AILERON BELLCRANK SHAFT. MAJOR REPAIR: MAJOR REPAIR ACCOMPLISHED. REPAIRED PER MM57-12-96, REPAIR NUMBER 3.SDR UPS07M50204Rib · crackedINSPECTION TYPE:C RIGHT SLAT TRACK 16 STRUCTURE I/B RIB CRACKED. CRACKED RIB 16 AT RIGHT WING REMOVED PER SRM 51-31-01 V2 R38. ATTACHMENT HOLES XFERRED ONTO NEW RIB PER DOUGLAS DWG ARB2873. FASTENER HOLES PICKED UP PER SRM 51-31-01 V2 R38. REWORKED AREA RESDR UPS07M50203Rib · crackedINSPECTION TYPE:C LEFT SLAT TRACK 16 STRUCTURE I/B RIB CRACKED. CRACKED RIB 16 AT LEFT WING REMOVED PER SRM 51-31-01 V2. ATTACHMENT HOLES T XFERRED ONTO NEW RIB PER DOUGLAS DWG ARB2873. FASTENER HOLES PICKED UP PER SRM 51-31-01 V2 R38. REWORKED AREA REPROTSDR 07FDEA01782Rib · crackedCOMPLY WITH EA 7-5710-102035 WINGS (AD 90-06-09 AND (94-07-08) MAIN FRAME -RIB REPAIR EO 7-5710-7-2308. COMPLIED WITH EA 7-5710-102035 WINGS (AD 90-06-09 AND AD 94-07-08)MAIN FRAME-RIB UPPER CHORD REPAIR EO 7-5710-7-2308 PART 2.SDR 07FDEA01781Rib · crackedRT WINGS, RIB AT BL 70-5 FASTENER INSP DURING "B" CHECK CRACK INDICATION WITNESSED BETWEEN BOTH HOLES AND BEYOND. HOLES SHOWN ON FIGURE 1 OF EO 7-5710-7-2308 PT1R. REPAIRED IAW EO 7-5710-7-2308 PT1 AND PT2 AND EA 7-5710-102035 REF WRI 57-10/0313.SDR 07FDEA01766Rib · damagedCOMPLY WITH E.A. 7-5710-110741-WING (AD 90-06-09:94- 87-08;98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. COMPLIED WITH EA 7-5710-110741 WING (AD90-06-09-94-0 7-08, 98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. COMPLIED WITH EA 5710-110741 WSDR CALA0700251Bulkhead · crackedINSPECTION FOUND THE RIGHT WHEEL WELL FORWARD BULKHEAD (WING CENTER SECTION AFT SPAR VAPOR BARRIER) CRACKED. THERE WERE TWO CRACKS MEASURING 12.75 INCHES AND 8 INCHES. THE VAPOR BARRIER WAS REMOVED AND REPLACED IAW ECRA 5710-02116.SDR USAA070359Rib · crackedRT WING RIB 6 AT AFT APERTURE REFUEL PIPE ATTACHMENT FASTENERS. TEMPORARY REPAIR PER EA 98639. DEFECT SIZE: LESS THAN 1"SDR SWIA200718418Rib · crackedLEFT INBOARD LEADING EDGE RIB IS CRACKED, DISCOVERED AT C-CHECK. REPLACED RIB IAW EMB 120 SRM 51-10-02 PG 2 SECT 2B AND 51-40-02.SDR SWIA200718417Rib · crackedRIGHT INBOARD LEADING EDGE RIB IS CRACKED, DISCOVERED AT C-CHECK. REPLACED RIB IAW EMB 120 SRM 51-10-02 PG 2 SECT 2B AND 51-40-02.SDR UPS07849742Rib · crackedINSPECTION TYPE:C3 LEFT WING CENTER L/E UPPER RIB CRACKED AT XFS 484. STOP DRILLED CRACK IAW SRM 57-02-00. FABRICATED AND INSTALLED 2 DOUBLERS IAW SRM 57-02-00, 51-1-21, AND 51-1-20D.SDR UPS07849741Rib · crackedINSPECTION TYPE:C3 LEFT WING CENTER RIB CRACKED AT XFS 409. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-02-00 51-1-21, AND 51-1-20D.SDR 07FDEA01646Rib · crackedRIGHT WING LEADING EDGE PERFORMANCE FILLET OUTBOARD RIB FOUND CRACKED. [SUP 05-16-07] RIB REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR USAA070329Rib · crackedFOUND CRACK, LOWER CHORD OF LT WBL 135.5 INSPAR RIB. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS PER EA 98574, DEFECT SIZE: .05".SDR USAA070330Rib · crackedFOUND CRACKED LOWER CHORD RT WBL 135.5 INSPAR RIB. INSTALLED REPAIR PARTS PER EA 98573, DEFECT SIZE: .05.SDR UPS07849738Rib · crackedINSPECTION TYPE:C3 LT WING OUTBD L/E RIB CRACKED AT STA XFS 609. NDT VERIFIED CRACK TERMINATES AT FASTNER HOLE IAW NDSPM 06-10-01-001. FABRICATED AND INSTALLED REPAIR ANGLE AT L/WING L/E RIB STA XFS 609 IAW SRM 57-03-03 FIG 6.SDR UPS07849737Rib · crackedINSPECTION TYPE:C3 LT WING OUTBD L/E RIB CRACKED AT XFS 591. NDT VERIFIED CRACK ENDS AT FASTENER HOLE IAW NDSPM 06-10-01-001. FABRICATED AND INSTALLED REPAIR ANGLE AT LT WING OUTBD L/E STA XFS 591 IAW SRM 57-03-03 FIG 6.SDR UPS07849722Rib · crackedINSPECTION TYPE:C3 LT WING OB LE RIB CRACKED AT XFS 804. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 57-02-00, 51-01-21 AND 51-1-20D.SDR UPS07849721Rib · crackedINSPECTION TYPE:C3 LT WING OB LE CRACKED AT XFS 876. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SRM 57-02-00, 51-1-21 AND 51-1-20D.SDR UPS07849720Rib · crackedC3 LT WING OB LE RIB CRACKED AT XFS 798. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SRM 57-07-00, 57-02-00, 51-1-21 AND 51-1-20D.SDR UPS07M50125Rib · crackedINSPECTION TYPE:C RIGHT WING L/E SLAT TRACK NR 16 I/B SUPPORT RIB FOUND CRACK. RIGHT WING L/E SLAT TRACK NR 16 ATTACHING PARTS & WIRE HARNESS REMOVED. NR 16 CRACK I/B SUPPORT RIB REMOVED. HOLES TRANSFERRED TO NEW NR 16 RIB ASSY. RIGHT WING L/E SLAT TRACK NSDR UPS07M50074Rib · deformedINSPECTION TYPE:C RT WING LOWER SURFACE FIXED L/E COMPARTMENT BETWEEN STA XOS 657 AND XO S 714 APPROX FOUND 04 SUPPORT RIB DEFORMED. 4 SUPPORT DEFORMED RIBS REMOVED. NEW SUPPORT RIBS FAB PER DWG ARB2924-8, ARB2924-6, ARB2924-4 AND ARB2930-16. RIBS HEAT TREASDR 07FDEA01527Rib · crackedCOMPLY WITH EA 7-5710-102033 WINGS (AD 90-06-09 AND AD 94-07-08) MAIN FRAME - RIB REPAIR EO 7-5710-7-2308 PART 2. COMPLIED WITH EA 7-5710-102033 (AD90-06-09 AND AD 94-07-08) RIB REPAIR EO 7-5710-7-2308 PART 2.SDR UIEA200700187Rib · crackedRHW NR 23 VC FLAP I/B ARM ROTARY ATT RIB AT OLES 1278 I/B FACE FOUND CRACKED AT "D" HOLE FWD STIFFENER AREA. CRACKED RIB "D" HOLE REPAIRED AS PER BOEING MSG 1-308409234-2.SDR 07FDEA01321Rib · crackedRT WING L/E INTERNAL ZONE FOUND 1 CRACK 0.75" LONG ON RIB. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1 VOL 1.SDR 07FDEA01319Rib · crackedRT WING L/E INT ZONE FOUND 1 CRACK 0.50" LONG, ON RIB WITH OLD REPAIR. REMOVED OLD REPAIR, AND PERFORMED NEW REPAIR IAW SRM 57-20-00 FIGURE 1 VOL 1.SDR ABXA070131Rib · crackedLEFT LEADING EDGE RIB HAD CRACKED DOUBLER 2ND RIB INBOARD OF NR 11 TRACK. REPAIRED RIB IAW REA D957-55597.SDR 07FDEA01191Rib · mismanufacturedEDGE MARGIN TO SHORT FOR TEMPORARY REPAIR ON RIB 5 IAW DR 426 REPAIR PERFORMED BY INSTALLATION ADDITIONAL FASTENER IAW EA 6-5710-108975 AND RAS/BAE/1004080/2006 A.SDR MLJ2007F00000Bulkhead · crackedWHILE AC WAS IN FOR AN ANNUAL INSPECTION, A CRACK WAS FOUND IN THE REAR MOUNT BULKHEAD ON THE RT MAIN TANK. THE CRACK WAS APPROX 1.5 INCH LONG AND LOCATED IN THE UPPER IB RADIUS OF THE WEBBING, NOT THE FLANGE. THE CRACK DID NOT ORIGINATE FROM AN EDGE OR A HOSDR 07FDEA01140Rib · crackedCRACK WAS FOUND ON MLG RIB 5 RT WING INTERIM REPAIR PERFORMED IAW, DRAWING R572-40265 AND APPROVED BY EA 6-5710-108975 AND RAS/BAE/1004080/2006 ISS.ASDR USAA070223Rib · crackedLEFT WING IN WBL 135.5 RIB UPPER CHORD ABOUT 6 INCHES FWD OF REAR SPAR. SPLICED IN REPAIR ANGLE & DOUBLERS PER EA 98495, DEFECT SIZE: 0.5 INCH.SDR 07FDEA00946Rib · chafedKRUEGER BOX RT, DAMAGED REPAIR, ABRASION IN AN SUPPORT FLANGE OF RIB 2B. REPAIR WAS PERFORMED BY BLEND OUT.SDR 07FDEA00854Rib · crackedFOLDING NOSE LT INTERNAL RIB CRACKED. REPAIR WAS PERFORMED IAW EA 6-5710-106358 AND SB A300-57-6067.SDR USAA070196Rib · crackedLEFT WING, WBL 235.5 IN SPAR RIB, LOWER CHORD BETWEEN STRINGERS 2 & 3 CRACKED. CUT OUT CRACKED SECTION OF LOWER CHORD, FAB'D & INSTALLED REPAIR FILLERS & TEE PER EA 98492, DEFECT SIZE: 0.6 INCH.SDR ABXA070092Rib · crackedLEFT WING XRS 164, RIB FITTING CRACKED. REMOVED AND REPLACED RIB AT LEFT WING XRS 164 IAW DC9 SRM.SDR WRLA2007049Rib · crackedDURING C-04 CHECK IN TPE, FOUND RT WING FIXED LEADING EDGE SLAT TRACK RIB R16 CRACK .5 INCH XORS:885. REPLACED RIB AND FASTENERS PER MD-11 SRM 51-33-01 VOL.II REV.38.SDR UPS07849431Rib · crackedINSPECTION TYPE:C3 LEFT WING OUTBOARD LWR RIB CRACKED AT XFS 790. CRACK TERMINATES AT FASTENER HOLE PER HFEC INSP NDTSPM 06-10-01-001 FABRICATED AND INSTALLED REPAIR DOUBLERS AND ANGLES AT LEFT WING OUTBOARD LEADING EDGE STA XFS 790 IAW SRM 57-03-03 FIG 7, AN
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