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 UPS08854023Rib · crackedINSPECTION TYPE:SP LT WING OUTBOARD LEADING EDGE INBOARD SECTION HAS CRACKED UPPER RIB ABOVE PNL 520A XFS 476. INSTALLED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-20D, 57-3-3 FIG 6 SHT 2.SDR UPS08854026Rib · crackedINSPECTION TYPE:SP LT WING OUTBOARD LEADING EDGE INBOARD SECTION HAS CRACKED UPPER RIB ABOVE PANEL 579B XFS 584. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-20D, 57-2-0 FIG 002 SHT 2.SDR UPS08854025Rib · crackedINSPECTION TYPE:SP LT WING OUTBOARD L/E INBOARD SECTION HAS CRACKED UPPER RIB ABOVE ACCESS PANEL 519A XFS 692. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-20D, 57-3-3 FIG 006, 57-2-0 FIG 002.SDR KCSA081587Rib · crackedLT WING RIB LOWER CHORD CRACKED AT WS 1516, 35 INCHES AFT OF FRONT SPAR.SDR KCSA081585Rib · crackedLT WING RIB LOWER CHORD CRACKED AT WS 1516, 23 INCHES AFT OF FRONT SPAR.SDR 08FDEA04837Rib · corrodedLT GEAR RIB 5, CORROSION FOUND UPON REMOVAL OF BUSH E AND F. A REPAIR IN ACCORDANCE WITH EA 6-5710-126452 WAS ACCOMPLISHED.SDR 08FDEA04843Rib · corrodedN16 MLG RT GEAR RIB 5, LUG WITH CORROSION UPON REMOVAL OF BUSHES E AND F. THE LUG BORE AND FACES WERE REPAIRED AS PER FEDEX EA 6-5710-126457.SDR 08FDEA04819Rib · crackedA86-2470, RT WING LE RIB UPPER CHORD IS CRACKED AT EXISTING REPAIR FSS 119, 8 INCHES-18 INCHES FROM SPAR (MKD). INSTALLED AND FABRICATED RT WING LE UPPER CHORD AND SPLICE AT FSS 119. REFS BOEING DWG 64-08342-20, SRM 51-40-03, SRM 51-30-02. TREATED AND PRIMESDR 08FDEA04817Rib · crackedRT WING L/E RIB UPPER CHORD HAS SEVERAL CRACKS ALONG EXISTING REPAIRS AT 9 INCHES-20 INCHES FROM SPAR, FSS 122. REMOVED REPAIR, FABRICATED REPAIR DOUBLER REF SRM 51-40-3 FIG 1. INSTALLED RT WING LF RIB CHORD REPAIR REF SRM 51-40-3 FIG 1. THIS IS CLASSIFIED SDR 08FDEA04816Rib · crackedRT WING L/E RIB UPPER CHORD HAS SEVERAL CRACKS ALONG EXISTING REPAIRS AT 9 INCHES-20 INCHES FROM SPAR, FSS 122. REMOVED REPAIR, FABRICATED REPAIR DOUBLER REF SRM 51-40-3 FIG 1. INSTALLED RT WING LF RIB CHORD REPAIR REF SRM 51-40-3 FIG 1. THIS IS CLASSIFIED SDR 08FDEA04801Rib · crackedRT WING LE RIB LWR CHORD IS CRACKED IS CRACKED FSS 119, 4 INCHES-18 INCHES FROM SPAR VERIFIED MATERIAL ID FOR REPAIR ANGLE AND FILLER. CUT OUT DAMAGE. FABRICATED REPAIR ANGLE AND FILLER. LOCATED, DRILLED AND TRIMMED REPAIR ANGLE. HEAT TREATED REPAIR ANGLE.SDR UPS08M53927Attach Fitting · crackedINSPECTION TYPE:1C LT WING AT STA XORS 562 FIXED L/E RIB ATTACH STRAP CRACKED. REMOVED, FABRICATED, AND INSTALLED STRAP IAW MD11 SRM 51-33-01 AND DWG ARB3954.SDR ASOA200801478Rib · crackedRT WING BAT WEB AT FS 53.6 CRACKED BETWEEN 2 FASTENERS. REPAIRED RT WING BAT WEB AT WS 53.6 IAW REO 601R-57-51-0046. C/W ASA ECTC REO 601R-57-51-046. SUPPLEMENTAL-SDR CLOSED 11/17/2008.SDR ASOA200801476Rib · crackedLT BATTERY RIB ASSY AT WS 53.60 IS CRACKED AROUND A FASTENER. TRIMMED AWAY DAMAGE FROM LT BATTERY RIB. REMOVED NUT PLATES AND FABRICATED ALL REPAIR PARTS. ALL WORK PERFORMED IAW BOMBARDIER AEROSPACE REO 601R-57-51-046 STEPS 1-4 REPAIR 2. REPAIR ITEMS REQUISDR 08FDEA04693Rib · crackedLEFT WING OTBD L/E NR 4 SLAT S/N BN605, 2 CRACKED INTERNAL BRACKET TABS ON AFT WEB BELOW EACH SIDE OF ACTUATOR BOLT HEAD AND NUT. REPLACED 2 CRACKED RIBS REF SRM 51-30-02 PG 1-5. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA04666Rib · crackedLT WING LE RIB LWR CHORD IS CRACKED FSS 119, 17 INCH FROM SPAR REMOVED CRACKED AREA OF RIB FLANGE, FABRICATED AND INSTALLED REPAIR ANGLE REF SRM 51-40-3 FIG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR SWIA200820915Rib · crackedC-CHECK, LEFT OUTBOARD WING OUTBOARD OF NACELLE, RIB NR 16 LOWER CLIP CRACKED. REPLACED PER SRM.SDR 2008FA0000707Spar Cap · corrodedDURING ANNUAL INSPECTION, SEVERE INNER GRANULAR CORROSION WAS FOUND IN THE RIGHT WING, MAIN UPPER SPAR CAP AT THE AFT PORTION OF THE T-CAP, IN THE VICINITY OF THE WHEEL WELL IN PARTICULAR THE LOCATION OF WHEEL SPIN OFF. DURING TIME, CAUSED DAMAGE TO THE POINTSDR UPS08853898Rib · crackedINSPECTION TYPE:SV REPAIR EFN 700200001086 REQUIRES EVALUATION AND DISPOSITION ORIGINAL N RC 145820 RT WING L/E STA XRS 6.22 LOWER RIB IS CRACKED. NO REPAIR AT STATION STA XRS 6.22 REPAIR IS AT XAS 62.2 FOUND REPAIR TO HAVE BEEN ACCP IAW DC8 SRM 57-02-00-0.SDR 2008UALA06224Rib · crackedLT WING O/B LEADING EDGE CAVITY LWR RIB FWD END CRACKED AT OFSS 547. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED DOUBLER TRIMMED DAMAGE AND INSTALLED DOUBLER.SDR 2008UALA06223Rib · crackedLT WING O/B LEADING EDGE CAVITY, LWR RIB FWD END CRACKED AT OFSS 688. MAJOR REPAIR ACCOMPLISHED. REMOVED RIB, INSTALLED NEW RIB AND LOWER STRUT.SDR UPS08M53718Rib · crackedINSPECTION TYPE:1C DURING OK TO INSTALL RT WING LOWER WINGLET FOUND CRACK ON RIB. REMOVED AND REPLACED RIB IAW SRM, 51-35-01, 51-33-01 VOL 2 PG 37 TABLE 12.SDR USAA920082025Rib · crackedCLT Q3 MAJOR REPAIR NR 03C40557004/001 RT WING INTERIOR RIB 135.5 LOWER CHORD CRACKED AT LOWER AFT END. REPAIRED RT WING INTERIOR RIB 135.5 LOWER CHORD IAW US AIRWAYS EA NR 100733 AND US AIRWAYS TYPICAL REPAIR NR 57-25-20.SDR 08FDEA04366Rib · crackedLEFT WING UPPER L/E PANEL 517 CT HAS 2 CRACKED RIBS. REMOVED 2EA CRACKED RIBS IAW SRM 51-35-01 & SRM 51-33-01; VOL II. & FABRICATED IAW DWG ARB 2407; REV "G". ALODINED & PRIMED IAW SRM 51-21-01; PGS 21 - 24; VOL II. INSTALED IAW DWG ARB 2407; REV "G"SDR KCSA081530Rib · crackedLEFT WING L/E RIB CRACKED AT FWD END AT FS 415.SDR KCSA081529Rib · crackedLT WING L/E RIB CRACKED AT AFT END, AT THE WING FRONT SPAR FSS 415.SDR UPS08853675Rib · crackedINSPECTION TYPE:SV RT WING OUTBOARD L/E LOWER RIB CRACKED AT XFS 835. STOP DRILLED CRACK IAW SRM 57-2-0 DC8. MANUF AND INSTALLED REPAIR IAW DC8 SRM 51-1-8AND SRM DC8 SRM 51-01-20D-0.SDR UPS08853673Rib · crackedINSPECTION TYPE:SV RT WING L/E LOWER RIB CRACKED AT XFS 829. STOP DRILLED CRACK IAW SRM 57-2-0 DC8. FABBED AND INSTALLED REPAIR IAW DC8 SRM 51-03-00-0, AND SRM 51-01-20D-0 DC8.SDR UPS08M53600Rib · crackedINSPECTION TYPE:1C RT WING FIXED L/E RIB XOS 1113 CRACKED LWR AFT END. STOP DRILLED, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 57-00-01 FIG 3, VOL 1 57-00-1 PG 9, SRM VOL 2. 51-21-01 PG 1, VOL 2, 51-33-01 PG 29.SDR UPS08853728Rib · crackedINSPECTION TYPE:SV EVALUATE AND DISPOSITION EFN 70219911059 ORIGINAL NRC 188671 RIB CRACKED AT OUTBOARD FORWARD CORNER OF ACCESS PANEL 522B. REPAIRED IAW 57-02-00 PG 1 FIG 002.SDR UPS08853550Rib · crackedINSPECTION TYPE:SV EVALUATION OF N/R 535858 LT WING L/E REPAIR BETWEEN NR 1 AND 2 PYLONS TENTH RIB FROM INBOARD END IS CRACKED. REPAIR WAS ACCOMPLISHED IAW DC8 SRM 57-2-0 SHEET 2 OF 2.SDR UPS08853551Rib · crackedINSPECTION TYPE:SV EVALUATION OF N/R 534213 RIGHT HAND LEADING EDGE AT STA XFS 804.00 UPPER LEFT RIB HAS A CRACK AFT END. REPAIR IS ACCOMPLISHED IAW DC8 SRM 57-2-0 FIG 2.SDR 08FDEA03890Rib · chafedFOUND CHAFING MARKS IN RT WING STRUCTURE RIB 27-28, IN AREA OF NACA DOOR. REPAIR PERFORMED BY POLISHING THE DAMAGED STRUCTURE TO SMOOTH CONTOUR, CUT OUT DAMAGED STRUTURE AND INSTALLING A REPAIR ANGLE AT NACA DOOR SURROUND REAR STIFFENER IAW RAS BAE10076602008SDR 08FDEA03864Rib · crackedLEFT WING, LEADING EDGE COMPARTMENT RIB AT XOS 1003 FOUND CRACK. REMOVED AND REPLACED WITH NEW RIB AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR DL757081266Rib · damagedLT WING RIB 25 LOWER SKIN PANEL RIB CHORD HAS SHORT EDGE MARGIN ON UPPER ROW OF FAST HOLES. REPAIR C/W PER ERA 470544-14 REV O AND APB DWG 757-3250 REV B.SDR 08FDEA03751Rib · crackedRIGHT WING TIP INTERIOR CRACKED WBL 624. REMOVED WING TIP IAW B727 MM 57-20-001-4. REMOVED WING TIP RIB IAW B727 SRM 51-30-2. LOCATED AND DRILLED NEW RIB IAW B727 SRM 51-30-5. INSTALLED NEW RIB IAW B727 SRM 51-30-2 AND REINSTALLED WING TIP IAW B727 MM 57-2SDR 08FDEA03706Rib · chafedFOUND CHAFING MARKS ON LT WING, LEADING EDGE RIB, BETWEEN RIB 1-5 REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS, NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1007859/2008 ISS.A , APPROVED BY EA 6-5741-123061.SDR 08FDEA03672Rib · chafedFOUND CHAFING MARKS ON RT WING TRAILING EDGE AREA ON RIB FOR ASA ATTACHMENT. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS , PERFORM NDT FOR CRACK FREE CONDITION IAW. RAS/BAE/1007863/2008 ISS.A , APPROVED BY EA 6-5751-123063SDR 08FDEA03671Rib · chafedFOUND CHAFING MARKS ON LH WING TRAILING EDGE AREA ON RIB FOR ASA ATTACHMENT. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS , PERFORM NDT FOR CRACK FREE CONDITION IAW. RAS/BAE/1007863/2008 ISS.A , APPROVED BY EA 6-5751-123063SDR 08FDEA03623Rib · crackedLEFT WING T/E STRUCTURE VERTICAL WEB IS CRACKED AT THE INBOARD FWD CORNER OF THE INBOARD FLAP. REMOVED & REPLACED THE CRACKED WEB (ANGLE) IN REF TO DC/MD-10 SRM 51-35-01; VOL II & IN REF TO DAC DWG AUB 7203; REV "BA".SDR 08FDEA03470Rib · chafedFOUND CHAFING MARKS ON LT WING TRAILING EDGE STRUCTURE RIB 6A-6B. REPAIR PERFORMED BY REWORK OF CHAFING MARK AT RIB 6A AND NDT FOR CRACK FREE CONDITION AND REWORK CHAFING MARK AT INTERMEDIATE RIB WITH INSTALLING A NEW RUBBING PLATE IAW RAS/BAE/1007587/2008 SDR UPS08M53160Rib · crackedINSPECTION TYPE:1C LT WING FIXED L/E SUPPORT RIB FOUND CRACKED AT SING STA XORS 683. REMOVED, FABRICATED, AND INSTALLED RIB IAW MD-11 SRM 51-33-01, DWG ARB3954, AND MD-11 SRM 51-21-01.SDR 08FDEA03397Rib · crackedRIGHT WING INBD FLAP NOSE RIB NR 5 IS CRACKED AT RIVET HOLE. FABRICATED REPAIR DOUBLER REF SRM 57-50-00; PG 204. ALODINED AND PRIMED REF AMM 51-22-00-0; PG 1. INSTALLED REF SRM 51-40-21; PG 7.SDR UPS08M53097Rib · crackedINSPECTION TYPE:2C LEFT WING FIXED L/E RIB XFS 1024 CRACKED ON AFT SIDE BETWEEN FASTENERS. REMOVED, FABRICATED, AND INSTALLED RIB IAW MD-11 SRM 51-33-01 AND DWG ARB2920.SDR UPS08M53111Rib · crackedINSPECTION TYPE:C LT WING L/E CAVITY AT 15 INCHES I/B OF SLAT TRACK NR 9, RIB SUSPECT CRACK. HFEC CARRIED OUT IAW NDT SPM REV13 PART 06-10-01.001 AND CRACK CONFIRM APPROX 3.75 INCH LONG. DAMAGE RIB REMOVED, NEW RIB FABRICATED & REPLACED AS PER SRM 51-31-01 VSDR UPS08M53103Rib · crackedINSPECTION TYPE:C RT WING LOWER WINGLET FWD RIB FOUND CRACKED AS MARKED. CRACKED RIB REMOVED PER SRM 51-31-01 V2 R40. NEW RIB FAB PER BOEING DRWG ARB7774 USING MATL 7075-0-0.040". RIB HEAT TREATED TO T6 PER DPS7.00-1 HARDNESS VALUE OBTAINED HRB80.1 PER DPS1SDR UPS08M53102Rib · crackedINSPECTION TYPE:C LT WING LOWER WINGLET FWD RIB FOUND CRACKED AS MARKED. CRACKED REMOVED PER SRM 51-31-01 V2 R40. NEW RIB FAB PER BOEING DRAWING ARB7774 USING MATL 7075-0-0.040". RIB HEAT TREATED TO T6 PER DPS7.001 HARDNESS HRB80.1 PER DPS1.053. NEW RIB HOSDR UPS08M52914Rib · crackedINSPECTION TYPE-1C, LT WING LE RIB FWD OF XORS 917 CRACKED ON AFT END, REMOVED, FABRICATED, AND INSTALLED RIB IAW MD-11 SRM 51-31-01, DWG ARB2920, SAA TRAVELER 80538380001, AND MD-11 SRM 51-35-01.SDR 08FDEA02943Rib · crackedLEFT WING L/E INTERIOR RIB IS CRACKED AT STA XFS 580. REMOVED CRACKED RIB IAW DC/MD-10 SRM 51-35-01, 51-33-01; VOL II. MATERIAL ID FOR THE RIB IS 7075-0, 0.063, PO 613435.3. FABRICATED IAW DAC DWG ARB 1162, REV "S". ALODINED AND PRIMED IAW DC/MD-10 SRM 5SDR 08FDEA02928Rib · crackedLEFT WING L/E INTERIOR RIB IS CRACKED AT THE STOP DRILL AT APPROX WING STA 683 (INBD OF THE NR 5 SLAT CENTER TRACK).
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