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 ABXA9701531Doubler · corrodedCENTER WING DOUBLER AT STATION 759 CORRODED AT CENTER SPLICE. REPAIRED IAW ABX REA D857-20452MR AND DC8 SRM 51-1-9.SDR 97FDEA00697Chord · crackedNR 0706 036 STA-PAE - CORROSION (C53-224-05) CRACK IN RT 70.85 PLUS CHORD IS CRACKED ON UPPER VERTICAL FLANGE IN RADIUS FROM BS 760 TO 770, WL 201, RBL 70.5 LONG CRACK REPAIR REQUIRED PER S/B 727-57-0112 REV 5. REPAIRED CRACK IN RT 70.8 PLUS CHORD PER EA 7-5SDR UPS97824567Te Box · crackedINSPECTION TYPE-N/A, CRACK IN TRAILING EDGE BOX INBD TO OUTBD WHEEL WELL. DEFERRED AS D138752 PER MMOC AND PER EO DC8-5720-9758-A PERMANENT REPAIR TO BE ACCOMPLISHED NEXT B OR BEFORE.SDR GAIA9752Fitting · corrodedDURING C-1 INSPECTION CORROSION WAS FOUND AT LEFT WING STATION 15, LOWER AFT ATTACH FITTING. THE DEFECTIVE ATTACH FITTING WAS REMOVED AND A NEW ATTACH FITTING INSTALLED IAW GD 600 (240D) SB NR 57-4A AND GENERAL DYNAMICS CV SRM 1-12-5. AIRCRAFT RETURNED TO SESDR 97ZZZX4511Pan · crackedDURING REPLACEMENT OF PAN UNDER WING WALK IN THE GEAR WELL, RIB WAS FOUND CRACKED. THE WING WAS REMOVED AND FOUND SEVERAL WING ATTACHMENT BOLTS CORRODED. BOLTS AND SPECIAL WASHERS NOT IN PROPER LOCATIONS PER PA28 MM. (WING ATTACH). NO SHIMS AT EITHER WING SSDR 97ZZZX4506Rivets · defectiveDURING REPLACEMENT OF PAN UNDER WING WALK IN THE GEAR WELL, RIB WAS FOUND CRACKED. THE WING WAS REMOVED AND FOUND SEVERAL WING ATTACHMENT BOLTS CORRODED. BOLTS AND SPECIAL WASHERS NOT IN PROPER LOCATIONS PER PA28 MM. (WING ATTACH). NO SHIMS AT EITHER WING SSDR EIAA970214Tee · crackedMZJ - DURING C-CHECK INSPECTION, DISCOVERED A CRACKED AND BROKEN UPPER T-CHORD ON THE LEFT AND RIGHT WING TRAILING EDGE BEAM WBL 235.2. REPAIRED USING FABRICATED SPLICES IAW EVEGREEN INT'L AIRLINE ECRA 480-57-066-2. (X)SDR ABXA9701694Intercostal · crackedRIGHT HAND L/E XW 163.75 HAS A CRACK ON UPPER INTERCOSTAL EXTENDING FROM FASTENER HOLE TO THE END OF PART. REPAIRED IAW DC-8 SRM 57-3-3.SDR RRXA97278Fitting · chafedDURING A MAINTENANCE VISIT, FOUND LEFT WING STA XW 98, FLAP CANOE FITTING HAD SEVERAL CHAFED AND GOUGED AREAS, REPAIR BLENDED-OUT BEYOND DC-8 SRM LIMITATIONS. *S/D* THE BLEND-OUT SHOWN IN FIGURE 1 AND 2 OF REO-03692 ARE ACCEPTABLE FOR STRENGTH PER DAC ACTIONSDR DHL9780771CBracket · crackedRT WING FLAP HINGE SUPPORT BRACKET AT STA 339. STOP DRILL ON CRACK AND FABRICATED REPAIR ANGLE IAW SRM 51-1-0. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED REPAIR ANGLE IAW SRM 51-1-0. INSTALLED FASTENERS IAW SRM 51-1-21.SDR UPS97824600Fitting · crackedINSPECTION TYPE-C, WING BOX VERT FITTING CRACKED F/S 923 LBL 68. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.SDR TWAA9804108Screws · brokenMCI - DURING C-CHECK MAINTENANCE, FOUND RT WING LOWER TRAPEZOIDAL PANEL OUTBOARD OF MAIN GEAR TRI-WING SCREWS BROKEN LOOSE AT FORWARD OUTBOARD END. INSTALLED DOUBLER PER SRM 51-40-2 AND FASTENER PR SRM 51-30-3. (M)SDR 97ZZZX4273Doubler · crackedTHE WING WALK SKIN WAS FOUND TO SAG WHEN STEPPED ON. INVESTIGATION REVEALED THE REINFORCEMENT DOUBLER RIVETED TO THE UNDERSIDE OF THE WING WALK SKIN WAS CRACKED ALL ALONG THE BUTT RIB AREA.SDR 97ZZZX4264Bulkhead · crackedFOUND BULKHEAD CRACKED. SUBMITTER STATED MOST LIKELY FROM FATIGUE. CRACK STARTED IN COMPOUND BEND AND HAD NOT YET MADE IT TO THE EDGE. SUBMITTER STATED THE BULKHEAD IS MADE OF TOO LIGHT OF MATERIAL AND SUGGESTS CESSNA MAKE A REPLACEMENT BULKHEAD OUT OF HEAVSDR UPS97824579Angle · crackedINSPECTION TYPE-C, L/WING L/E UPPER ANGLE CLIP AT STA XOLD 6.225 CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 57-3-0, DWG 5769948.SDR ABXA9701502Fixed Vane · delaminatedDURING C-CHECK, FOUND THE CENTER FIXED VANE TOP SIDE DELAMINATED. REPLACED VANE IAW DC9 MM 27-51-3.SDR UPS97424495Fitting · crackedINSPECTION TYPE-C, CENTER WING TANK FOUND FITTING CRACKED AT LOWER SPAR CHORD, LBL 78. REPLACED FITTING AT NAC STA 1000, IN CENTERWING AT LOWER SPAR CHORD LBL 78 ACC SRM 51-30-02.SDR DL72W971822Stiffener · crackedFOUND DURING A-1 LETTER CHECK, 1.5 INCH CRACK L/E SPAR STIFFENER AT NR 2 SLAT I/B TRACK ROLLER BOX I/B SIDE. REPAIRED PER M/M 57-20-21.SDR SCNA97315Bolt · crackedDURING INSPECTION IN ACCORDANCE WITH AD 96-06-08 AND DC-10 SERVICE BULLETIN 57-126, REV 1, THE BOLT LOCATED IN THE NUMBER 2 POSITION OF THE LEFT WING MILKSTOOL FITTING, (P/N 71658-18-58), WAS FOUND TO HAVE CRACK INDICATIONS. THE BOLT WAS REPLACED WITH (P/N 8SDR CKSA97535Stiffener · corrodedDURING CPCP CHECK INSPECTION, FOUND AFT SPAR VERTICAL STIFFENER CORRODED AT WS 170 LOWER CHORD. REMOVED CORROSION IAW B727 SRM 51-10-6. CORROSION FOUND OUT OF LIMITS IAW B727 SRM 51-10-1. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-40-4. CORROSION TASK CARD NSDR 98ZZZM73Tip · crackedRIGHT WING TIP FAIRING PANEL CRACKED 2 PLACES. ALSO, REQUIRES REINFORCEMENT PER EO E96/008/634 BLOCK 9. REPAIRED 2 CRACKS IN RIGHT WING TIP FAIRING IAW AW 57-20-9412-06. C/W EO E96/008/634 BLK 9.SDR 97ZZZX4609Screw · missingLOOSE PANEL ON WING FLAP PULLEY COVER. RETURNED TO ANC, MADE UNEVENTFUL LANDING. REPLACED COVER SCREWS. NO OTHER DAMAGE NOTED.SDR ABXA9701717Clip · crackedRIGHT HAND WING L/E AT STA XOLDI 6.225, THE UPPER ATTACH CLIP IS CRACKED IN HALF. FABRICATED AND INSTALLED CLIP IAW DWG 5769589 AND DC-8 SRM 51-1-20 AND 51-1-8.SDR ABXA9701530Vane · delaminatedDURING C-CHECK, FOUND RT OUTBOARD FIXED VANE DELAMINATED. REPLACED RT OUTBOARD FIXED VANE IAW DC-9 MM 27-51-3.SDR CALA9701477Angle · crackedANGLE CRACKED THROUGH 7 FASTENERS INSIDE AT BOTOM OF RIGHT WING LEADING EDGE RIB AT WBL 92.0 INBOARD AND AFT OF NR 4 LEADING EDGE FLAP AREA. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-10-6 AND 51-10-1.SDR RAAA97B1010Support · brokenDURING SCHEDULED RIGHT MAIN LANDING GEAR CHANGE FOUND WS 304 REAR SPAR MAIN LANDING GEAR BEAM SUPPORT BOLT SAFETY LUG BROKEN. REPAIRED PER S/B 727-57-153.SDR RAAA97B1009Support · crackedDURING SCHEDULED RIGHT MAIN LANDING GEAR CHANGE FOUND WS 224.5 AFT REAR SPAR LANDING GEAR TRUNNION SUPPORT CRACKED AT OUTBD LOWER FWD BOLT HOLE APPROX .4 IN. USING HFEC CHANGED AFT REAR SPAR LANDING GEAR TRUNNION SUPPORT PER SRM 51-10-1.SDR RAAA97B1008Support · crackedDURING SCHEDULED LEFT MAIN LANDING GEAR CHANGE FOUND WS 224.5 AFT REAR SPAR LANDING GEAR TRUNNION SUPPORT CRACKED AT INBD AND OUTBD LOWER BOLT HOLES APPROX .6 IN. USING HFEC CHANGED AFT REAR SPAR LANDING GEAR TRUNNION SUPPORT PER SRM 51-10-1.SDR ABXA9705128Vane · delaminatedDURING C-CHECK, FOUND LEFT WING NR 2 FIXED VANE DELAMINATED ON UPPER SURFACE. REPLACED NR 2 FIXED VANE IAW DC-9 MM 27-51-3.SDR 98ZZZM26Stiffener · crackedLEFT WING TRAILING EDGE SHROUD TOP SKIN STIFFENER BETWEEN RIBS 5 AND 6 IS CRACKED AT FWD ADN BRACKET AT ITS AFT END IS CRACKED ON ITS LOWER FLANGE. REPAIRED LT WING TRAILING EDGE SHROUD TOP SKIN STIFFENER BETWEEN RIBS 5 AND 6 IAW BAE FAX REF GCR/0754-97 DATEDSDR 98ZZZM25Bracket · crackedLEFT WING INBOARD LIFT SPOILER OUTBOARD HINGE RIB HAS A BRACKET FOR SECURING HYD LINES THATS CRACKED, RIB 5 LT. REPLACED ANGLE P/N HC932H0211-000 ON LEFT WING INBOARD LIFT SPOILER OUTBOARD HINGE RIB SECURING HYD LINES. (M)SDR 98ZZZM24Bracket · crackedLEFT WING TRAILING EDGE SHROUD AREA, BOTTOM SKIN STIFFENER BRACKET CRACKED ON FLANGE AFT BETWEEN RIBS 8 AND 9. REPLACED STIFFENER BRACKET ON LEFT WING TRAILING EDGE SHROUD AREA BOTTOM SKIN. ALL WORK ACCOMPLISHED IAW BAE SRM AND STD PRACTICES. (M)SDR 98ZZZM23Bracket · crackedLT WING TRAILING EDGE SHROUD AREA AT INBOARD LIFT SPOILER JACK RIB, THERE IS A BRACKET THAT SECURES HYD LINE THATS CRACKED. REMOVED BRACKET, REPAIRED BRACKET BY WELDING IAW BAE FAX REPAIR REF DJH/RJ0737-97 DATED 10-02-97 AND FOUND UNIT SERVICEABLE. INSTALLEDSDR UPS97824552Angle · crackedINSPECTION TYPE-C, FOUND LEADING EDGE ATTACH ANGLE CRACKED AT INBD END OF LEADING EDGE EXTENSION ABOVE NR 1 PYLON. REMOVED CRACKED ANGLE, FABRICATED, DRILLED, TREATED, PRIMED AND INSTALLED ATTACH ANGLE IAW DC8 SRM 57-2-0, 51-1-8, 51-1-21, 51-3-0.SDR 98ZZZM27Stiffener · crackedRIGHT WING TE TOP SKIN STIFFENER CRACKED AT FWD END, INBOARD OF RIB NR 9. REPLACED RIGHT WING TRAILING EDGE TOP SKIN STIFFENER INBOARD OF RIB NR 9. (M)SDR ABXA9701479Clip · crackedRT WING L/E STA XDLDI 6.225, THE UPPER INTERCOASTAL ATTACH CLIP IS CRACKED. REPLACED CLIP IAW SRM 51-1-4 AND INSTALLED IAW SRM 51-1-20D.SDR UPS97224487Bracket · crackedINSPECTION TYPE-C, T-BRACKET FWD OF NR 7 SPOILER PANEL UPPER SKIN ON T/E OF WING BROKEN. REPLACED BRACKET IAW SRM 51-30-2.SDR UPS97824556Angle · crackedINSPECTION TYPE-C, FOUND LT WING INBD SLOT PANEL, OTBD SPLICE PAN ANGLE CRACKED AT AFT END, STA XW 223. REMOVED CRACKED PAN ANGLE, DRILLED, TREATED, PRIMED AND INSTALL NEW PAN ANGLE IAW DC8 SRM 57-1-0, 51-1-8, 51-1-21.SDR UPS97824444Angle · crackedINSPECTION TYPE-C, FOUND LT WING INBD FLAP OTBD LOWER INTERCONNECT PANEL ATTACH ANGLE CRACKED AT AFT END STA XW138. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0, 51-1-20D, 51-1-8.SDR 98ZZZM379Fairing · crackedLEFT WING TIP FAIRING AT RIB 20 FALSE RIB IS CRACKED. REPAIRED IAW BAE SRM 51-71-11 FIG 2. (M)SDR 98ZZZM378Jobolts · damagedPERFORM RIL HC571H9033 LT WING RIB 0. REMOVED AND REPLACED JO-BOLT FASTENERS AT LEFT SIDE RIB 0 IAW HC571H9033. SEE W/C 82103/75 FOR REPORT AND SIZES USED. (M)SDR 98ZZZM377Jobolts · damagedPERFORM RIL HC571H9033 RT WING RIB 0. INSTALLED JOBOLTS TO RIB 0 RT SIDE. (M)SDR 98ZZZM376Jobolts · damagedPERFORM RIL HC571H9033 RT WING RIB 2 INBOARD. INSTALLED JOBOLTS TO INSIDE PORTION OF RIB 2 RT SIDE. INSTALLED JOBOLTS TO INSIDE PORTION OR RIB 2 RT SIDE. (M)SDR 98ZZZM375Jobolts · damagedPERFORM RIL HC571H9033 RT WING RIB 2 OUTBOARD. INSTALLED JOB0LTS TO OUTBOARD RIB 2 RIGHT WING PER RIL HC57 1H9033. (M)SDR 97FDEA00605Chord · corrodedCORROSION (C53-132-02 1/2) WING CENTER SECTION UPPER REAR SPAR CHORD BS 870, LBL 70 TO RBL 70, WL 188.SDR 97FDEA00604Chord · corrodedCORROSION (C53-132-02 1/2) WING CENTER SECTION LOWER REAR SPAR CHORD VERTICAL LEG BS 870, LBL 10 TO RBL 10, WL 164.SDR 97ZZZX4515Casting · crackedMAIN LANDING GEAR SUPPORT STRUCTURE, LT AND RT, MLG WHEELWELL - CRACKS ARE OCCURRING IN THE RIBS, PN 0822175-79, -74, CENTER RIB WEB, ORIGINATING AT UPPER AFT CORNER OF THE CUT-OUT HOLE (WHERE THE OPERATING PUSH/PULL ROD PASSES THROUGH) PROPAGATING TOWARDS TOPSDR 97ZZZX4514Casting · crackedMAIN LANDING GEAR SUPPORT STRUCTURE, LT AND RT, MLG WHEELWELL - CRACKS ARE OCCURRING IN THE RIBS, PN 0822175-79, -74, CENTER RIB WEB, ORIGINATING AT UPPER AFT CORNER OF THE CUT-OUT HOLE (WHERE THE OPERATING PUSH/PULL ROD PASSES THROUGH) PROPAGATING TOWARDS TOPSDR 97ZZZX4306Cord · failedDURING INSP, LOOSE FABRIC WAS FOUND ON TOP RT INBD SECT OF TOP WING (NO FABRIC TORN). SUCTION CUP WAS ABLE TO LIFT FABRIC FROM WING RIBS, BOTH TOP AND BOTTOM. A FABRIC PUNCH TEST WAS COMPLETED AND FOUND FABRIC OK. UNDER SUPERVISION OF THE FAA, TOP WING FABRSDR CALA9701375Beam · crackedINSPECTION FOUND A .365 INCH AND .625 INCH CRACK IN RT WING UPPER TRAILING EDGE AFT OF MLG SUPPORT BEAM AT UPPER INBOARD CORNER OF NR 8 SPOILER ACTUATOR LINKAGE CASTING, WS 232. THE CRACKS WERE ROUTED OUT. REPAIR STRAPS WERE FABRICATED AND INSTALLED IAW ECRA
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