JASC 5720
Service difficulty reports · 13,638
Reports filed under 5720 · Wing Miscellaneous Structure, 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 = '5720' 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 = '5720' 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 CALA9701724Bracket · crackedINSPECTION FOUND A 6 INCH CRACK IN RT INBOARD HINGE LOWER BULLET ATTACH BRACKET ON RT OUTBOARD FLAP. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 57-52-01 AND 51-21-01.SDR 97UAL900880Support · brokenON WALKAROUND, FOUND FAIRING SUPPORT ROD BRACKET (115W2266-5) FOR RIGHT HAND TRAILING EDGE ASSEMBLY LOWER INBOARD FIXED FAIRING BROKEN. THE SUPPORT BEAM (115W2214-2) WAS ALSO DAMAGED. *S/D* ACCOMPLISHED INTERIM REPAIR UNTIL REPLACEMENT PARTS AVAILABLE FROM SDR DL72W972558Stiffener · crackedA 1.5 INCH CRACK_IN SPAR STIFFENER LOCATED OUTBD SIDE OF NR 6 SLAT INBD TRACK. REPAIRED PER MM 57-20-21.SDR DL72S972627Beam · crackedRT WING SPOILER SUPPORT BEAM CRACKED IN O/B BOLT HOLE FOR NR 5 FLAP TRACK. REMOVED DAMAGED SECTION OF SPOILER BEAM PER M/M 57-55-0 FIG 805. REMOVED SUPPORT BETWEEN SPOILERS 7 AND 8. FABRICATED EXTRUDED CHORD IAW M/M 57-55-0 PG 810. DRILLED CHORD, DOUBLER TSDR 98ZZZX610Nutplate · crackedDURING AN INSPECTION OF THE AIRCRAFT, THE LEFT LEADING EDGE WING ROOT FAIRING WAS REMOVED TO PERFORM MAINTENANCE. A 2.50 INCH CRACK WAS FOUND FROM ONE OF THE RIVETS WHICH HOLD THE NUTPLATE IN PLACE FOR THE WING ROOT FAIRING IN THE PRESSURE VESSEL AREA. CRACKSDR AALA972528Trap Panel · corrodedTUL - THE INBOARD BARREL NUT HOLE FOR THE SIDE BRACE ATTACHMENT TO THE TRAPEZOIDAL PANEL IS CORRODED (IN THE TRAPEZOIDAL PANEL). HOLES REWORKED PER ESO 7349 DATED 12-11-97. FABRICATED AND INSTALLED BUSHING PER SRM 57-20-00. (X)SDR AALA972527Trap Panel · corrodedTUL - THE INBOARD BOLT HOLE FOR THE TRAPEZOIDAL PANEL ATTACHMENT TO THE SIDE BRACE IS CORRODED (IN THE TRAPEZOIDAL PANEL). HOLES WERE REWORKED PER ESO 7349 DATED 12-11-97. FABRICATED AND INSTALLED BUSHING PER SRM 57-20-00. TST: 67,144.30 HOURS. CYCLES: 2SDR AALA972275Trap Panel · corrodedTUL - THE OUTBOARD BOLT HOLE FOR THE SIDE BRACE ATTACHMENT TO THE TRAPEZOIDAL PANEL IS CORRODED (IN THE TRAPEZOIDAL PANEL). BORED TO 1.3215 INCH TO REMOVE CORROSION PER SRM 57-20-00, FABRICATED AND INSTALLED BUSHING PER SRM 57-20-00. (X)SDR AALA972274Trap Panel · corrodedTUL - THE OUTBOARD BARREL NUT HOLE IN THE TRAPEZOIDAL PANEL FOR THE SIDE BRACE TO TRAPEZOIDAL PANEL ATTACHMENT IS CORRODED. REMOVED CORROSION IN BORE PER SRM 57-20-00 (SIZE BORED TO 2.244), FABRICATED AND INSTALLED BUSHING PER SRM 57-20-00. TST: 67,144.30 HSDR AALA972270Trap Panel · pittedTUL - BOTTOM FAYING SURFACE OF TRAPEZOIDAL PANEL PITTED. REMOVED .018 INCH FROM FAYING SURFACE TO REMOVE CORROSION PER SRM 57-20-00, PAGE 05, NOV 1, '89. TREATED PRIMED AND INSTALLED SHIM AND RETORQUED PER DR 329432. TST: 67,144.30 HOURS. CYCLES, 25,370. SDR UPS97825293Clip · crackedINSPECTION TYPE-C/CK, RIB TO STRINGER CLIP CRACKED NR 4 MAIN OUTBOARD. REMOVED AND REPLACED CLIP IAW DC8 SRM 51-1-24 AND 51-1-20D. ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51-1-8.SDR AU971445Flap Shroud · corroded(AUS) LH AND RH WINGS CONTAINED CORROSION IN AREAS OF FLAP SHROUDS AND REAR BAYS.SDR AALA972232Web · crackedTUL - WEB CRACKED UNDER NR 7 SPOILER ACTUATOR CASTING, TWO PLACES. REMOVED DAMAGED SECTION OF WEB AND INSTALLED WEB REPAIR PER BOEING SERVIEC BULLETIN 727-57-158. (M)SDR AALA972229Stiffener · crackedTUL - INSPAR STIFFENER UPPER NR 10 CRACKED AT STATION 686.50 LT WING TANK. STOP DRILLED CRACK INSTALLED DOUBLER PER BOEING SB 727-57A159. (M)SDR 98ZZZX1221Stiffener · crackedATW - RIGHT WING TOP T/E SKIN STIFFENER CRACKED AT FWD END JUST INBD OF RIB NR 8. REPAIRED STIFFENER, REF FAX JM/RJ0317/97, AND JM/RJ0818-97.SDR 98ZZZM372Stiffener · crackedRT WING TOP TE SKIN STIFFENER CRACKED AT FWD END BETWEEN RIBS 8/9, JUST OUTBOARD OF RIB 8. REPAIRED CRACKED STIFFENER IAW FAX NR'S JM/RJO317/97 AND NR JM/RJO818-97. (M)SDR 98ZZZM369Stiffener · crackedLT WING, TRAILING EDGE AND SHROUD UPPER SKIN STIFFENER IS CRACKED AT FORWARD END IN AREA BETWEEN WING RIBS 7 AND 8. REPAIRED STIFFENER REF FAX JM/RJ0818-97. (M)SDR 98ZZZM365Stiffener · crackedRT WING TOP TE SKIN STIFFENER CRACKED AT FWD END AT RIB NR 9, JUST INBOARD OF RIB 9. REPAIRED CRACKED STIFFENER IAW FAX NR'S JM/RJ0317/97 AND NR JM/RJO317/97 AND NR JM/RJO818-97. (M)SDR UPS97825277Fitting · crackedINSPECTION TYPE-C/CK, STRINGER ATTACH FITTING ON AFT SIDE OF 1ST STRINGER FWD OF REAR SPAR AT XRS 74 CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-24 AND 51-1-20D, ALODINED AND PRIMED AS REQUIRED PER DC8 SRM 51-1-8.SDR MZZA97304Beam · crackedKUL - NRC: 813821 - SPOILER SUPPORT BEAM, LOWER CHORD, FOUND CRACKED. FABRICATED DOUBLER IAW SRM 51-40-4, FIG 1, ALODINED AND PRIMED PER SRM 51-10-2. CARRIED OUT REPAIR IAW SRM 51-40-4. INSTALLED FASTENERS IAW SRM 51-30-2, AND PL, REF DRAWING NR 65-24966. SDR UPS97825104Tripler · crackedINSPECTION TYPE-SP, RT WING L/E AT STA XOLDI 6.225 THE LWR INTERNAL TRIPLER IS CRACKED. REMOVED CRACKED TRIPLER, FABRICATED, AND INSTALLED REPLACEMENT TRIPLER IAW SRM 57-3-3 AND 51-1-21.SDR ABXA9701927Channel · crackedCANTED WEB CHANNEL HAS CRACK IN NR 4 ALT TANK, AT RT WING STA 508.977. REPAIRED IAW DWG 56 1326 AND DC8 SRM 51-1-21.SDR ABXA9701885Channel · crackedCANTED WEB CHANNEL HAS CRACK AT NR 4 ALT TANK, AT RT WING STA 508.977. REPAIRED IAW SRM 51-1-21 AND DWG 56-1326.SDR 98ZZZX1224Angle · crackedATW - RT WING T/E LOWER SKIN STIFFENER AFT TAG ANGLE CRACKED BETWEEN RIBS 3 AND 4. REPLACED ANGLE.SDR 98ZZZX1223Angle · crackedRT WING T/E LOWER SKIN STIFFENER AFT TAG ANGLE CRACKED AT RIB NR 4. REPLACED ANGLE.SDR 98ZZZX1222Angle · crackedATW - RT WING T/E LOWER SKIN STIFFENERS AFT TAG ANGLE CRACKED BETWEEN RIBS 5 AND 6. REPLACED ANGLE.SDR UPS97825109Intercostal · crackedINSPECTION TYPE-SP, RT WING L/E INBD SIDE OF THE STA XOLDI 6.225 RIB, FWD OF THE PNEU DUCT THE INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-1-21 AND DWG 5769589.SDR CALA9701616Bracket · crackedINSPECTION FOUND A .75 INCH CRACK IN UPPER RIB TO STRINGER CLIP/BRACKET JUST AFT OF TANK ACCESS 634 AT INBOARD RIB, STA XORS 402. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-31-1.SDR 98ZZZX1226Bolts · looseATW - AIR WISC EO E92/083/657 RECC ATTACH BOLTS AND NUTS ON RT SIDE, A, B, C, D ARE LOOSE ON THE REAR SPAR ROOT ATTACHMENT FITTING AT WING RIB 2. REPLACED FASTENERS IAW BAE REPAIR INSTRUCTIONS HC53H9043. BOLTS A, C, D ORIG SIZE. BOLT B FIRST OVERSIZE, RESEASDR UPS97825311Fitting · crackedINSPECTION TYPE-C, CRACK IN FITTING AT XRS 74.9, 1ST FITTING AFT OF FWD SPAR AT BLKH TO FWD SPAR ATTACH. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.SDR 98ZZZX1231Bracket · crackedATW - LT WING BRACKET FOR HYD LINES THAT PASS THROUGH THE AFT END OF THE SPOILER HINGE RIB AT WING RIB NR 5 IS CRACKED. REPLACED BRACKET.SDR 98ZZZX1213Jobolts · damagedREPLACED JOBOLTS ON RT WING CENTER TANK RIB 2 INBOARD PER RIL HC571H9033. PERFORMED RIL HC571H9033 TO RIB 2 INBD CENTER TANK. REPLACED JOBOLTS WITH MRL FASTENERS.SDR UPS97824953Doubler · crackedINSPECTION TYPE-C, LT WING L/E INNER DOUBLER CRACKED JUST AFT AND INBD OF O/B SLOT DOOR. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE DOUBLER IAW SRM 51-1-20D AND DWG 5769891.SDR HALA9700250T-Cap · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON T-CAP HORIZONTALLY LEG STATION 58.5 RIGHT FWD TO AFT SPAR. BLENDED OUT DAMAGE, HFEC INSPECTED WITH NO DEFECTS NOTED, RESTORED FINISH, ACTION DER APPROVED PERMANENT REPAIR. (M)SDR 98ZZZX1212Jobolts · damagedJOBOLTS ON RIGHT CENTER TANK RIB ZERO NEED TO BE REPLACED PER RIL HC571H9033. C/W RIL HC571H9033 RT CENTER TANK RIB ZERO REPLACING OF JOBOLTS.SDR 98ZZZX1211Jobolts · damagedATW - PERFORMED RIL HC571H9033 LT CENTER TANK RIB ZERO (JOBOLTS). C/W RIL 571H9033 TP; LT SIDE RIB ZERO. REPLACEMENT OF JOBOLTS WITH MRL FASTENERS.SDR 98ZZZX1198Jobolts · damagedATW - PERFORMED RIL HC571H9033 LT RIB 2 INBD (JOBOLTS). PERFORMED RIL HC571H9033 LT RIB 2 INBD (CENTERTANK) SIDE. REPLACEMENT OF JOBOLTS WITH MRL FASTENERS.SDR 98ZZZM367Jobolts · damagedPERFORM RIL HC571H9033 LT RIB 2 OUTBOARD. PERFORMED RIL HC571H9033 TO LEFT RIB 2 OUTBOARD (WING TANK) SIDE. REPLACEMENT OF JOBOLTS WITH MRL FASTENERS. (M)SDR RRXA97305Doubler · damagedDURING A MAINTENANCE VISIT, FOUND RIGHT WING LOWER MAIN LANDING GEAR SUPPORT DOUBLER (P/N 5753736-1) HAD LARGE COUNTERSUNKS AND 3 KNIFE EDGE HOLES. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED DOUBLER REPAIR IAW FAA DER APPROVED ENGINEERING SKETCHSDR RRXA97295Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND RIGHT WING FLAP CANOE FITTING GOUGED BEYOND LIMITATIONS IAW DC-8 SRM AND DAC DWG 5614372 AT XW 98. *S/D* ALSO, FOUND CORROSION DAMAGE TO WING FLAP CANOE FITTING BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED AND TREATED CORROSIONSDR CALA9701574Strap · corrodedINSPECTION FOUND LT WING UPPER SURFACE FILLER STRAP CORRODED ABOVE REAR SPAR AT XORS 417. REPAIRED IAW ECRA 5710-01840.SDR 98ZZZX1230Shroud · crackedATW - LT WING UPPER TRAILING EDGE SHROUD LOWER LIP HAS A 2 INCH CRACK IN IT IN AREA BETWEEN WING RIBS 5 AND 6. REF: W/C NR 5042 FOR SHEET METAL FORMING AND HEAT TREATING TO 2024T-81 SPEC. REPAIRED IAW FAX DJR/RJ0192-97 ISS 2.SDR 98ZZZX1204Rib · brokenSMALL ALUMINUM BRACKET AT RT WING TIP RIB 20 BROKEN TAB, BRACKET IS USED FOR CONDUIT TUBE AT FLUX VALVE WIRING. FABRICATED BRACKET PER DRAWING HC923H0759 AND REPLACED BRACKET AT RIB 20 IAW BAE 146 SRM.SDR UPS97825040Fitting · crackedINSPECTION TYPE-C, LT WING UPPER STRINGER END FITTING CRACKED JUST AFT OF MLG ACTUATOR. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.SDR UPS97824987Strap · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS597.508 THE UPPER RIB TIE STRAP IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT STRAP IAW SRM 51-1-21 AND DWG 5655441.SDR UPS97425029Clip · crackedINSPECTION TYPE-C, FOUND CLIP CRACKED ON LE RIB TO FRONT SPAR UP CHORD AT ILES 543.93. REPLACED CLIP IN ACC WITH SRM 51-30-02 AND DWG 65B15969.SDR ABXA9701765Angle · corrodedCANTED WING BOX SHEAR WEB L-ANGLE CORRODED AT STA 857 FROM C/L TO RBL 15. REPAIRED IAW ABX D853-19085MR.SDR UPS97225145Tie Point · crackedINSPECTION TYPE-D, TANK LACING POINT ON REAR WALL STA 870 OF CENTER FUEL TANK CRACKED. TIE POINT IS SECOND FROM O/B ON RIGHT SIDE OF TANK REAR WALL. REMOVED AND INSTALLED TIE POINT IAW SRM 51-30-1.SDR UPS97225144Vert Stiffener · crackedINSPECTION TYPE-D, CRACK AT TOP END OF VERTICAL STIFFENER NR 4 FROM O/B ON LT SIDE ON SPANWISE BEAM NR 1 STA 820 APPROX SECOND BAY OF CENTER TANK. REPAIRED IAW SRM 51-40-4 FIG 1.SDR ABXA9701755Fitting · crackedRT WING STR NR 8 END FITTING AT XRS 408 IS CRACKED. REPLACED RT WING UPPER STRINGER NR 8 FITTING IAW DWG 5616894 AND DC8 SRM 51-1-20D.
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