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 UPS97821895Rib · crackedINSPECTION TYPE: C. LT WING L/E RIB AT STA XOLDI 6.225 IS CRACKED IN TWO PLACES ABOVE THE PNEUMATIC DUCT. REPAIRED IAW SRM 57-2-0.SDR UPS97821861Rib · crackedINSPECTION TYPE: C. LT WING L/E RIB AT STA XFS 448.581 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER, PER SRM 57-3-11 AND 51-1-21.SDR 9700389928Rib · crackedDURING PERIODIC CHECK, FOUND RIGHT WING TRAILING EDGE RIB CRACKED JUST ABOVE INBOARD BUTE DOOR. FABRICATED AND INSTALLED REPAIR ANGLE PER EA 99-112001.SDR TAOA019701Rib · crackedDURING D-CHECK, A 2 INCH CRACK AT 70.5 WING RIB UPPER CHORD RIGHT SIDE AT TWO MOST FORWARD HOLES, WERE FOUND DURING EDDY CURRENT INSPECTION. INSTALLED BOEING REPAIR KIT ON WING RIB UPPER CHORD RIGHT SIDE STATION 70.5 AS PER SERVICE BULLETING 727-57-0112 AND BSDR C2XA97IA016Rib · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING NOSE RIB NR 19 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE NOSE RIB USING AND ANGLE DOUBLER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR UPS97821827Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 360.25 IS CRACKED AT THE AFT UPPER EDGE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.SDR UPS97821826Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 366.5 IS CRACKED AT THE AFT UPPER EDGE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.SDR UPS97821825Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 329 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACKED AND REPAIRED PER SRM 57-2-0 FIG 2.SDR UPS97821824Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 316.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.SDR UPS97821822Rib · crackedINSPECTION TYPE: C. RT WING L/E RIB AT STA. XOLDI 6.225 CRACKED APPROX. 2.8 INCHES. REMOVED DAMAGED AREA PER SRM 57-2-0. FABRICATED FILLER, DOUBLER, AND INTERCOSTAL PER SRM 57-2-0 AND INSTALLED PER SRM 51-1-20D.SDR ABXA9700694Rib · crackedDURING C-CHECK, THE WING LEADING EDGE RIBS AT STA 418 AND 430 WERE FOUND CRACKED. THE RIBS WERE REPAIRED IAW DC9 SRM 51-30-5.SDR CALA9700038Rib · corrodedINSPECTION FOUND TOP RIB CHORD CORRODED AT LT WING LEADING EDGE, WS 614. THE RIB CHORD WAS REPAIRED IAW SRM 51-40-02, FIGURE 1.SDR MALA965250Rib · crackedDURING AN INSPECTION IN MSP, MAINTENANCE FOUND A 3.5 INCH CRACK IN THE RADIUS OF THE RT WING RIB LOWER ATTACH FLANGE P/N 27-31023. APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED A 6.5 INCH BY 3 INCH BY SDR MALA965249Rib · chafedDURING A SCHEDULED INSPECTION IN MSP, THE LEFT WS 27 AFT FLAP WELL RIB P/N 27-31080 WAS FOUND CHAFFED BY THE FLAP SWING LINK. BLENDED OUT CHAF DAMAGE AND INSTALLED A REPAIR DOUBLER AS PER EA 01-96132, AND LAR 92-MALA-107. (M)SDR MALA965245Rib · crackedDURING AN INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS 1INCH BY 1 INCH IN THE RADIUS OF THE LT WING RIB LOWER ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED A 6.5 INCH, SDR MALA965244Rib · crackedDURING AN INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS 2 INCH BY 1 INCH IN THE RADIUS OF THE RIGHT WING RIB LOWR ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED A 6.5 INCH, SDR MALA965243Rib · crackedDURING AN INSPECTION IN MSP, MAINTENANCE FOUND A 'X.0' CRACK IN THE RADIUS OF THE LT WING RIB LOWER ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED ADN INSTALLED A 'X.00' BY 3 INCH BY 1 ISDR MALA965242Rib · crackedDURING AN INSPECTION IN MSP, MAINTENANCE FOUND A 'X.0' CRACK IN THE RADIUS OF THE RT WING RIB LOWER ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATIONIS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED A 'X.0 BY 3 INCH BY 1 INCHSDR MALA965240Rib · crackedDURING AN INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS 1 INCH BY 1 INCH IN THE RADIUS OF THE LT WING RIB LOWER ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED AN APPROPRISDR MALA965239Rib · crackedDURING AN INSPECTION IN MSP, MAINTENANCE FOUND A 5 INCH CRACK IN THE RADIUS OF THE WING RIB LOWER ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED A 8.25 INCH BY 3 INCH BY 1 SDR 97ZZZX706Rib · corrodedFOUND HEAVY SURFACE CORROSION THROUGHOUT WING ASSEMBLY. INTERNAL PARTS OF WING WERE NOT PROTECTED FROM THE DAMAGING EFFECTS OF CORROSION DURING MANUFACTURE. REPLACED PART, CLEANED, TREATED, AND PRIMED WITH EPOXY PRIMER. RECOMMEND MANUFACTURE DO LIKEWISE.SDR 97ZZZX699Rib · corrodedFOUND HEAVY TO SEVERE CORROSION, POPPED RIVETS, THROUGHOUT WING. INTERNAL PARTS WERE NOT PRIMED DURING MANUFACTURE. REPLACED PART, CLEANED, TREATED, AND PRIMED WITH EPOXY PRIMER. RECOMMEND CESSNA DO LIKEWISE.SDR MALA965241Rib · crackedDURING AN INSPECTION IN MSP, FOUND TWO CRACKS IN THE RADIUS OF THE RT WING RIB LOWER ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED AN APPROPRIATE SIZED 3 INCH BY 1 INCH BYSDR CALA9700037Rib · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RIB CHORD AT RT WING NR 3 MAIN TANK, WS 670. THE RIB CHORD WAS REPAIRED IAW SB 57-2273.SDR CALA9700029Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN RIB TOP AREA OF LT WING INBOARD LEADING EDGE STA 628. THE RIB WAS REPAIRED IAW SRM 51-40-02.SDR COMA9610368Rib · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING RIB NR 1, CL RIB DAMAGED. REMOVED AND REPLACED IAW EMBRAER ENGINEERING DRAWING 120-44623.SDR CALA9601885Rib · crackedINSPECTION FOUND OUTBOARD WING TRAILING EDGE RIB, NR 3 FROM INBOARD END CRACKED .5 INCH AT FORWARD END UPPER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 2.SDR CALA9601882Rib · crackedINSPECTION FOUND A .5 INCH CRACK AT LOWER ATTACH BOLT HOLE IN INBOARD RIB OF RT WING NR 2 SLAT DRIVE TRACK. THE RIB WAS REPLACED IAW SRM 51-30-5.SDR 9627436608Rib · crackedDURING PERIODIC CHECK, FOUND SEVERAL CRACKS ON THE LEFT WING LEADING EDGE RIB. STOP DRILLED CRACKS, INSTALLED .100 REPAIR ANGLES, AND .160 REPAIR STRAP MADE FROM 7075-T6. REPAIR DONE PER EA 66-120602, SEC 1, MFG PART NUMBER 65B10151-601.SDR SCNA96443Rib · tornDURING HEAVY MAINTENANCE, FOUND TORN METAL ON THE LEFT HAND WING LEADING EDGE, INBOARD OF THE NUMBER 8 SLAT, INBOARD TRACK. INNER RIB REMOVED AND A NEW RIB FABRICATED PER DC10 BLUEPRINT AND INSTALLED PER 51-31-01 AND 51-33-01.SDR 96ZZZX6125Rib · crackedDISCOVERED BY CREW DURING POST-FLIGHT INSP, CAUSE AT THIS TIME IS UNDETERMINED. BOTH OUTER RIBS CRACKED, ON RT WING.SDR 96ZZZX6124Rib · crackedDISCOVERED BY CREW DURING POST-FLIGHT INSP, CAUSE AT THIS TIME IS UNDETERMINED. BOTH OUTER RIBS CRACKED, ON RT WING.SDR 97ZZZX443Rib · crackedDURING C/W AD 95 20-07 (SIDE BRACE STUD INSPECTION), IT WAS DISCOVERED THAT THE ADJACENT RIB (WS 49.25) WAS CRACKED IN THE LOWER PORTION OF THE RADIUS FOR THE FORWARD FLANGE. THE SIDE BRACE STUD BRACKET ASSEMBLY MOUNTS ON TOP OF THE RIB FLANGE MAKING INSPECTISDR 97ZZZX442Rib · crackedDURING C/W AD 95 20-07 (SIDE BRACE STUD INSPECTION), IT WAS DISCOVERED THAT THE ADJACENT RIB (WS 49.25) WAS CRACKED IN THE LOWER PORTION OF THE RADIUS FOR THE FORWARD FLANGE. THE SIDE BRACE STUD BRACKET ASSEMBLY MOUNTS ON TOP OF THE RIB FLANGE MAKING INSPECTISDR ABXA9700275Rib · crackedDURING C-CHECK, THE LEADING EDGE RIB INBOARD OF DE-ICE DUCT WAS FOUND CRACKED, NR AF-793. THE RIB WAS REPAIRED IAW DC9 SRM.SDR 97ZZZX692Rib · corrodedNOSE RIB CORRODED THROUGH AT STA 190 OF LT WING. AIRCRAFT WAS BASED IN FLORIDA WITH NO FACTORY PROTECTION OF PARTS INSIDE OF WINGS.SDR 97ZZZX686Rib · corrodedFOUND SURFACE TRAILING EDGE RIB'S CORRODED THROUGH IN RT WING. REPLACED PARTS WITH NEW CESSNA PARTS. PARTS NOT PROTECTEDY WITH PRIMER BY CESSNA.SDR 96ZZZX5971Rib Strap · misinstalledLEFT WING RIB AT WS 91 UPPER STRAP IS JOGGLED TO FIT BETWEEN SPAR AND RIB. ASSEMBLY AT FACTORY PUT STRAP ABOVE SPAR, CREATING A 0.050 INCH BUMP IN WING. SUBMITTER STATES CESSNA RESEARCHED AIRCRAFT BUILD RECORDS AND COULD NOT FIND ANYTHING SHOWING WHY THIS WASDR MALA965187Rib · dentedDURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT AFT FALSE WING RIB AT WS 39 DENTED AND CHAFED APPROX .025 IN FLANGE. COMPLETED REPAIR BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW AEROTECH DESIGNS EA01-96113 DATED NOV 4/96. (M)SDR EISA96213Rib · crackedDURING A SCHEDULED D-CHECK, FOUND IN THE RIB FLANGE LOWER RADIUS, LEFT WING STATION 656 ABOUT 12 INCHES FORWARD OF THE REAR SPAR. REPAIRED PER SB 727-57-127. (M)SDR EISA96204Rib · crackedDURING A SCHEDULED D-CHECK, FOUND A CRACK IN A CRACK IN THE RIB FLANGE UPPER RADIUS, LEFT WING STATION 546.5 ABOUT 11.5 INCH FORWARD OF THE AFT SPAR. REPAIRED PER SB 727-57-127. (M)SDR EISA96203Rib · crackedDURIGN A SCHEDULED D-CHECK, FUOND A CRACK IN A CRACK IN THE RIB FLANGE LOWER RADIUS, LEFT WING STATION 629 ABOUT 14 INCHES AFT OF THE FRONT SPAR. REPAIRED PER SB 727-57-127. (M)SDR EISA96202Rib · crackedDURING A SCHEDULED D-CHECK, FOUND A CRACK IN A CRACK IN THE RIB FLANGE LOWER RADIUS, RIGHT WING STATION 629 ABOUT 13 INCHES FORWARD OF THE REAR SPAR. REPAIRED PER SB 727-57-127. (M)SDR EISA96201Rib · crackedDURING A SCHEDULED D-CHECK, FOUND A CRACK IN A CRACK IN THE RIB FLANGE LOWER RADIUS, RIGHT WING STATION 629 ABOUT 14 INCHES AFT OF THE FRONT SPAR. REPAIRED PER SB 727-57-127. (M)SDR EISA96200Rib · crackedDURING A SCHEDULED D-CHECK, FOUND A CRACK IN A CRACK IN THE RIB FLANGE LOWER RADIUS, LEFT WING STATION 546.5 ABOUT 18 INCHES FORWARD OF THE AFT SPAR. REPAIRED PER SB 727-57-127. (M)SDR EISA96199Rib · crackedDURING A SCHEDULED D-CHECK, FOUND A CRACK IN A CRACK IN THE RIB FLANGE LOWER RADIUS, RIGHT WING STATION 601.50 ABOUT 14 INCHES FORWARD OF THE AFT SPAR. REPAIRED PER SB 727-57-127. (M)SDR EISA96198Rib · crackedDURING A SCHEDULED D-CHECK, FOUND A CRACK IN A RIB FLANGE LOWER RADIUS, LEFT WING STATION 601.5 ABOUT 14 INCHES FORWARD OF THE AFT SPAR. REPAIRED PER SB 727-57-127. (M)SDR 97ZZZM454Rib · chafedRIB ABOVE LEFT NR 1 FLAP TRACK IS CHAFED WHERE IT CONTACTS ACCESS PANEL 285FT. BLENDED AND REPROTECTED THE CHAFE MARK ON THE SIDE OF RIB 2 TRAILING EDGE EXTENSION PER FAX DJR/RJ1243-96 DATED OCT 31, 1996 AND SRM 51-20-11. GENERATED W/C TO C/W A DV INSPECTIONSDR 96ZZZX5655Canted Rib · crackedDURING A PHASE INSPECTION FOUND BOTH RT AND LT WING CANTED RIB TOP CAP CRACKED. CRACK STARTS AT AFT SIDE OF FWD WING SPAR AND RUNS AFT PARALLEL TO THE BEND RADIUS. STOP-DRILLED ENDS OF CRACKS PER CESSNA INSTRUCTIONS.SDR 96ZZZX5654Canted Rib · crackedDURING A PHASE INSPECTION FOUND BOTH RT AND LT WING CANTED RIB TOP CAP CRACKED. CRACK STARTS AT AFT SIDE OF FWD WING SPAR AND RUNS AFT PARALLEL TO THE BEND RADIUS. STOP-DRILLED ENDS OF CRACKS PER CESSNA INSTRUCTIONS.
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