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.

SDR ASOA05412Rib · crackedDURING A C-CHECK IN MCN, THE LEFT BATTERY RIB AT THE UPPER CORNER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT BATTRY RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-039A. (M)May 8, 2005 · N867AS · Cndair CL6002B19SDR UPS05844485Rib · crackedINSPECTION TYPE: C3, LT WING L/E AT XFS 385.000 LWR RIB CRACKED 2 INCHES LONG MIDDLE OF RIB. FABRICATED AND INSTALLED RIB FORMER AND 2 EA REPAIR ANGLES IAW DWG 5769603, SRM 51-3-2, 57-2-1 AND 51-3-2.May 5, 2005 · N808UP · Doug DC873FSDR UPS05844479Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED XFS 316.000. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2, 51-1-21, 51-1-20D AND 51-1-15.May 5, 2005 · N808UP · Doug DC873FSDR VTZA200500069Rib · crackedLEFT BATT RIB IS CRACKED 1.5 INCH.May 5, 2005 · N625BR · Cndair CL6002B19SDR VTZA200500068Rib · crackedRIGHT BATT RIB IS CRACKED .750 INCH BETWEEN THE ATTACHING FASTENERS.May 5, 2005 · N625BR · Cndair CL6002B19SDR UPS05844498Rib · crackedINSPECTION TYPE:C3 LEFT WING L/E UPPER RIB CRACKED AT STA XFS 438. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA REPAIR ANGLE DOUBLERS IAW SRM 53-02-00 FIG 001B, 51-1-21.May 4, 2005 · N808UP · Doug DC873FSDR UPS05844497Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 408. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2, 51-1-20D AND DWG 5770375.May 4, 2005 · N808UP · Doug DC873FSDR UPS05844491Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 385.250. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS 2 EA IAW SRM 57-2-0 FIG 018, 51-1-20D, 51-1-15 AND DWG 5770087.May 4, 2005 · N808UP · Doug DC873FSDR UPS05844494Rib · crackedINSPECTION TYPE: C3, LEFT WING L/E UPPER RIB CRACKED 1 INCH LONG AT XFS 828.500. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-2-0 FIG 1B, 57-2-0 FIG 2B, AND DWG'S 5769470-45, 576947U.May 3, 2005 · N808UP · Doug DC873FSDR UPS05844488Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 822.500 .5 INCH LONG. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2 -0, 57-2-0 FIG 2, 51-1-20D, 51-1-21 AND DWG 5769470.May 3, 2005 · N808UP · Doug DC873FSDR UPS05844484Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED .25 INCH LONG AT XFS 809. STOP DRILLED CRACK AND FABRICATED INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.May 3, 2005 · N808UP · Doug DC873FSDR UPS05844471Rib · crackedINSPECTION TYPE:C3 LT WING L/E UPPER RIB CRACKED 1/4 INCH LONG AT XFS779. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER IAW SRM 57-2-0 FIG 2, DWG 5769470-29 AND SRM 51-1-20D,51-1-21 AND 51-1-15.May 3, 2005 · N808UP · Doug DC873FSDR COMA0560288Rib · crackedCRACK FOUND TO BATT RIB ASSEMBLY AT WS 53.60. REPAIRED IAW REO 601R-57-51-046.May 3, 2005 · N708CA · Cndair CL6002B19SDR IXXA05SMN17SRib · crackedLT NR 1 STUB WING FORMER CRACKED, STA XFS 526.000. PERFORMED MAJOR REPAIR IAW DWG 9753247. REMOVED CRACKED RIB IAW DC-8 SRM 54-1-0 PAGE 1, DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW RIB IAW DWG 9753297, DC-8 SRM. DPS 369-4 REV AM. PEApr 29, 2005 · N828BX · Doug DC871FSDR SWAA051246Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SWA ACO.Apr 27, 2005 · N509SW · Boeing 7375H4SDR SWAA051227Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SWA ACO.Apr 26, 2005 · N509SW · Boeing 7375H4SDR 05FDEA01117Rib · crackedLEFT WING LOWER SURFACE T/E SKIN HAS INDICATION OF CRACK RIB 11 AT PANEL 581 AB. REPAIRED IAW EA 6-5710-87138.Apr 25, 2005 · N402FE · Airbus A310203SDR 05FDEA01115Rib · crackedTOP OF RIGHT WING AT RIB 20 SKIN JOINT I/B SIDE OF SPLICE HAS 4 FASTENERS SHOWING CRACK INDICATION USING NDT METHOD. REMOVED CRACKS IAW EA 6-5720--87800.Apr 25, 2005 · N402FE · Airbus A310203SDR SWIA200515659Rib · crackedRIGHT WING WHEEL BIN AREA; FORWARD BATTERY ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-57-51-046.Apr 24, 2005 · N594SW · Cndair CL6002B19SDR SWIA200515658Rib · crackedLEFT WING WHEEL BIN AREA; FORWARD BATTERY ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601-57-51-046.Apr 24, 2005 · N594SW · Cndair CL6002B19SDR 05FDEA01105Rib · crackedLT WING LEADING EDGE CAVITY BETWEEN SLAT TRACK NR 17 AND NR 18 FOUND WITH RIB FLANGE CRACKED. FABRICATED AS PER DRAWING NR: ARB2920. RIBS PN ARB2920-41 AND ARB2920-47. REMOVED AND REPLACED IAW SRM 51-35-01 VOLUME II.Apr 23, 2005 · N617FE · Doug MD11SDR 05FDEA01104Rib · crackedRT WING LEADING EDGE CAVITY RIB BETWEEN SLAT TRACK NR 16 AND NR 17 FOUND CRACKED AT EDGE. FABRICATED IAW DRAWING NR: ARB2920. RIB REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II.Apr 23, 2005 · N617FE · Doug MD11SDR 05FDEA01103Rib · crackedLT WING LEADING EDGE CAVITY BETWEEN SLAT TRACK NR 16 AND 17, FOUND RIB FLANGE CRACKED. FABRICATED AS PER DRAWING NR ARB2920. RIB REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II.Apr 23, 2005 · N617FE · Doug MD11SDR COMA0560268Rib · crackedLEFT AND RIGHT HAND BATTERY RIB CRACKED. REPAIRED IAW REO 601R-57-51-046.Apr 20, 2005 · N981CA · Cndair CL6002B19SDR DHL2005807500Frame · crackedNR 1 LT STUB WING FORMER CRACK 0.500, STA XW 540.000. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. PERFORMED STOP HOLE AND FABRICATED REINFORCING ANGLE (ALCLAD 7075-T6 0.063) IAW SRM 57-2-0. CLEANED, TREATED AND PRIMED REINFORCING ANGLE AND AREA IAW SRM 51-1-8Apr 19, 2005 · N807DH · Doug DC873FSDR UPS05844436Rib · crackedINSPECTION TYPE: C1, RT WING L/E UPPER RIB CRACKED 1 INCH LONG AT XFS 841.25. REPAIRED IAW DC-8 SRM 57-3-3 AND SRM 51-1-21.Apr 19, 2005 · N880UP · Doug DC873FSDR SWAA051160Rib · crackedDURING SCHEDULED 1/4D CHECK, FOUND LT WING RIB CHORD CRACKED AT WBL 135.5, FWD OF AFT SPAR. REPAIRED RIB PER SWA EA.Apr 19, 2005 · N333SW · Boeing 7373H4SDR SWIA200515730Rib · crackedRIGHT MLG WHEEL WELL BATTERY RIB CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R-57-51-046.Apr 14, 2005 · N905SW · Cndair CL6002B19SDR SWIA200515729Rib · crackedLEFT MLG WHEEL WELL BATTERY RIB CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED DOUBLER IAW CRJ200 REO 601R-57-51-046 TYPE 1 REPAIR.Apr 14, 2005 · N905SW · Cndair CL6002B19SDR DHL2005807503Frame · crackedRIGHT WING INBOARD L/E UPPER FORMER 0.250 CRACK, STA XFS 207.500. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. PERFORMED STOP HOLE AND FABRICATED REINFORCING ANGLE (AL7075T6 0.050) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND REINFORCING ANGLE Apr 14, 2005 · N807DH · Doug DC873FSDR 2005FA0000512Rib · crackedWING MID-CORD RIB JUST FORWARD OF THE OB AILERON HINGE, FOUND CRACKED WHERE IT IS RIVETED TO THE REAR SPAR. BOTH LT AND RT SIDES SAME. THIS IS NOT EASY TO SEE DUE TO THE POSITION OF THE EXISTING INSPECTION HOLES BUT CAN BE SEEN IF YOU ARE LOOKING FOR IT. SBApr 14, 2005 · N6124Y · Ayres STRT34SDR DHL2005783512Rib · crackedNR 5 SLAT INTERIOR AT ACTUATOR ATTACHMENT INB RIB CRACK NOTED WS 410. REMOVED NR 5 LE SLAT ACTUATOR ASSY IAW 727 MM 27-81-32 AND 27-81-11. REMOVED CRACKED U-CHANNEL IAW 727 SRM 51-30-2 AND FABBED NEW FROM 2024T3 .071 PONR 9002193 DIM.15 INCH BY 3 1/8 INCH IAApr 13, 2005 · N783DH · Boeing 727227SDR AU510001625Rib · cracked(AUS) RIB LOCATED IN CENTER OF RT WHEEL WELL CRACKED. (CASA NR 510001625)Apr 6, 2005 · Piper PA31350SDR ASOA05315Rib · crackedDURING A C-CHECK, THE LT BATT RIB ASSY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT BATT RIB ASSY AT WS 53.60 IAW EO. (K)Apr 6, 2005 · N820AS · Cndair CL6002B19SDR UPS05844277Rib · crackedC1 LT WING OB LEADING EDGE UPPER RIB CRACKED 6 INCH OB OF IB END. REPAIRED RIB IAW SRM 57-02-00-0.Apr 4, 2005 · N810UP · Doug DC873FSDR UPS05844273Rib · crackedC1 LT WING OB LEADING EDGE UPPER RIB CRACKED 12 INCH OB OF IB END. REPAIRED BY STOP DRILLING AND INSTALLING REPAIR ANGLE IAW SRM 57-2-0.Apr 4, 2005 · N810UP · Doug DC873FSDR 2005FA0000607Rib · crackedDURING SCHEDULED ANNUAL INSPECTION, FOUND LT WING BATT RIB AFT ANGLE AT IB MLG DOOR AFT ATTACH POINT CRACKED. HAVE NOTED SIMILAR CRACKING IN OTHER LOW-TIME RAC MODEL 58 AIRCRAFT. CRACKING SEEMS TO BE RELATED TO INSTALLATION OF MACHINED ALUMINUM DOORS THAT REApr 1, 2005 · N128WS · Beech 58SDR 2005FA0000549Rib · crackedSINCE OUR FLEET OF SIX PIPER ARROWS WERE ALL FOUND TO HAVE CRACKED RIBS IN THE SAME LOCATION (FOUND DURING ROUTINE INSPECTION / SDRS WERE SENT IN) WE DETERMINED TO INSPECT OUR FLEET OF TEN SEMINOLES. THE BASIC WING STRUCTURE IS DESIGNED THE SAME. WE FOUND SIMar 31, 2005 · N925ER · Piper PA44180SDR 2005FA0000547Rib · crackedSINCE OUR FLEET OF SIX PIPER ARROWS WERE ALL FOUND TO HAVE CRACKED RIBS IN THE SAME LOCATION (FOUND DURING ROUTINE INSPECTION / SDRS WERE SENT IN) WE DETERMINED TO INSPECT OUR FLEET OF TEN SEMINOLES. THE BASIC WING STRUCTURE IS DESIGNED THE SAME. WE FOUND SIMar 31, 2005 · N928ER · Piper PA44180SDR 2005FA0000562Rib · crackedSINCE OUR FLEET OF SIX PIPER ARROWS WERE ALL FOUND TO HAVE CRACKED RIBS IN THE SAME LOCATION (FOUND DURING ROUTINE INSPECTION / SDRS WERE SENT IN) WE DETERMINED TO INSPECT OUR FLEET OF TEN SEMINOLES. THE BASIC WING STRUCTURE IS DESIGNED THE SAME. WE FOUND SIMar 31, 2005 · N923ER · Piper PA44180SDR 2005FA0000532Rib · crackedSINCE OUR FLEET WERE ALL FOUND TO HAVE CRACKED RIBS IN THE SAME LOCATION (FOUND DURING ROUTINE INSPECTION / SDRS WERE SENT IN). THE CRACKS ARE FOUND IN THE RIB, ADJACENT TO THE LANDING GEAR TRUSS BRACKET (WHICH MUST BE REMOVED TO PROPERLY SEE THE CRACK). IN Mar 31, 2005 · N921ER · Piper PA44180SDR UPS05844375Rib · crackedINSPECTION TYPE: C1, RT WING L/E UPPER RIB CRACKED .25 INCH LONG AT STA XW 754. REPAIRED BY STOP DRILLING AND INSTALLING REPAIR ANGLE IAW SRM 51-1-21, 51-1-20D AND 57-2-0.Mar 30, 2005 · N810UP · Doug DC873FSDR 2005FA0000451Rib · crackedSINCE FLEET OF SIX PIPER ARROWS WERE ALL FOUND TO HAVE CRACKED RIBS IN THE SAME LOCATION, FOUND DURING ROUTINE INSPECTION. SDRS WERE SENT. DETERMINED TO INSPECT FLEET OF TEN SEMINOLES. THE BASIC WING STRUCTURE IS DESIGNED THE SAME. FOUND SIMILAR CRACKS IN Mar 28, 2005 · N931ER · Piper PA44180SDR 05FDEA00649Rib · crackedRT WING NR 16 SLAT TRACK INBOARD RIB FOUND CRACKED. REMOVED AND REPLACED WITH NEW RIB AS PER SRM 51-33-01 VOLUME II.Mar 27, 2005 · N616FE · Doug MD11SDR 05FDEA00648Rib · crackedLT WING NR 16 SLAT TRACK INBOARD RIB FOUND CRACKED. REMOVED AND REPLACED WITH NEW RIB IAW SRM 51-33-01 VOLUME II.Mar 27, 2005 · N616FE · Doug MD11SDR USAA050390Rib · crackedCLT - Q6 - RIB, (1.5 AND .3750 INCH) CRACK; H WING, ROB AT WS 505 UPPER FLANGE RADIUS 20 INCH FROM L/E OF RIB. INSTALLED REPAIR DOUBLER IAW EA. (K)Mar 24, 2005 · N442US · Boeing 7374B7SDR 2005FA0000556Rib · crackedDURING A VISUAL INSPECTION, A SMALL CRACK WAS FOUND IN THE RT NOSE RIB P/N-62021-005 AND -004. A MORE THOROUGH INSPECTION REVEALED THAT AN ADDITIONAL CRACK, MUCH LARGER (ABOUT 4 IN LONG), WAS FOUND ON THE RIB P/N-78475-009 AND -008. THESE RIBS ARE INCLUDED IMar 22, 2005 · N708ER · Piper PA28R201SDR 2005FA0000428Rib · crackedDURING A VISUAL INSPECTION, A SMALL CRACK WAS FOUND IN THE RT NOSE RIB P/N-62021-005 AND -004. A MORE THOROUGH INSPECTION REVEALED THAT AN ADDITIONAL CRACK, MUCH LARGER (ABOUT4 INCHES LONG), WAS FOUND ON THE RIB P/N-78475-009 AND -008. THESE RIBS ARE INCLUDED Mar 22, 2005 · N706ER · Piper PA28R201SDR 2005FA0000581Rib · crackedDURING A VISUAL INSPECTION, A SMALL CRACK WAS FOUND IN THE RT NOSE RIB. A MORE THOROUGH INSPECTION REVEALED THAT AN ADDITIONAL CRACK, MUCH LARGER (ABOUT 4 INCHES LONG), WAS FOUND ON THE RIB. THESE RIBS ARE INCLUDED IN THE MOUNTING ASSEMBLY FOR THE BRACKET(MAIMar 22, 2005 · N703ER · Piper PA28R201SDR 2005FA0000555Rib · crackedDURING A VISUAL INSP, A SMALL CRACK WAS FOUND IN THE RT NOSE RIB P/N-62021-005 AND -004. A MORE THOROUGH INSPECTION REVEALED THAT AN ADDITIONAL CRACK, MUCH LARGER (ABOUT 4 INCH LONG), WAS FOUND ON THE RIB P/N-78475-009 AND -008. THESE RIBS ARE INCLUDED IN THE Mar 21, 2005 · N492B · Piper PA28R201
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