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 UPS97822662Angle · crackedINSPECTION TYPE:D, RT WING L/E O/B OF NR 4 AFT FILL VALVE, SLOT ISLAND MOUNT ANGLE IS CRACKED PAST STOP DRILL. REMOVED, FABRICATED, AND REPLACED IAW SRM 53-1-0.SDR UPS97822601Splice Doubler · crackedINSPECTION TYPE-D, RT WING L/E SECTION BTWN PYLONS AT STA XOLDI 6.225, SPLICE DOUBLER HAS SEVERAL FATIGUE CRACKS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5769891 AND SRM 57-3-3.SDR UPS97822593Intercostal · crackedINSPECTION TYPE-D, RT WING L/E SECTION BETWEEN PYLONS, BLEED AIR DUCT SUPPORT INTERCOSTAL O/B OF O/B UNDER-WING FUELING ADAPTER IS CRACKED ON THE O/B AFT END. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER, AND INSTALLED IAW SRM 57-2-0, 51-1-21, 5SDR HALA9722Doubler · corrodedHNL - MODERATE CORROSION ON LOWER MLG DOUBLER STATION 105 (MIDDLE OF DOUBLER, INBOARD AREA). REMOVED CORROSION, CLEANED AND TREATED PER SRM 57-10-3. REPAIRED PER HAL 105. (M)SDR COMA9710194Angle · crackedON 2C TASK 5720-651-01I, THE RIGHT WING LOWER SKIN SUPPORT ANGLE, AT RIB 16, BETWEEN STRINGERS 8 AND 10, WAS FOUND CRACKED. THE ANGLE WAS REPLACED PER SRM CHAP 51 STANDARD PRACTICES.SDR COMA9710193Angle · crackedON 2C TASK 5720-622-01I, THE RIGHT WING LOWER SKIN SUPPORT ANGLE WAS FOUND CRACKED AT RIB 8, BETWEEN STRINGERS 10 AND 11. THE ANGLE WAS REPLACED PER SRM CHAP 51 STANDARD PRACTICES.SDR 97ZZZX3053Rivets · looseATW - RT NR 3 FLAP CANOE INBOARD OPERATING STRUT RIVETS LOOSE. REPLACED LOOSE RIVETS IAW FAX'S DJR/RJ0296-97 AND DJR/RJ0638-96.SDR MWEA97223Trap Panel · crackedDURING C-CHECK, TRAPEZOID AFT FLANGE SHOWING SIGNS OF CRACKS. MAINTENANCE REMOVED AND INSTALLED ANGLE REPAIR IAE SRM 57-09 FIG 7A.SDR CKSA97168Flange · damagedDURING C-1 CHECK INSPECTION, FOUND LEFT HAND WING LOWER ACCESS PANEL FLANGE DAMAGED OUTBOARD MAIN LANDING GEAR DOOR. REPAIRED LEFT HAND WING LOWER ACCESS PANEL FLANGE IAW SKETCH AIA/E/2509 EA 97-013A. C-1 CHECK INSPECTION WORK CARD NUMBER 1002. NON-ROUTINE SDR CKSA97134Stiffener · crackedDURING C-1 CHECK INSPECTION, FOUND RIGHT HAND WING FRONT SPAR HAS A STIFFENER BRACKET CRACKED (AT BOTTOM) AT XFS522 INBOARD NR 4 ENGINE. REMOVED AND REPLACED RIGHT HAND WING FRONT SPAR STIFFENER AT XFS522 INBOARD NR 4 ENGINE IAW DC8 SRM 51-1-0 AND 51-1-20D. SDR CKSA97059Angle · corrodedDURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION, CENTER WING FRAME ANGLE UNDER RIGHT HAND INBOARD DOG HOUSE DOOR. REPAIRED IAW SKETCH AIA/E/2375. CORROSION TASK CARD NUMBER 227L/R-0551. NON-ROUTINE TASK CARD NUMBER 82428.SDR CKSA97047Web · crackedDURING CPCP CHECK INSPECTION, FOUND STA 680 FRONT SPAR OF WING BOX IN MID ELECTRONICS BAY HAS CRACKED WEB. REPAIRED PRESSURE BULKHEAD STA 680 IAW DC8 SRM 53-2-5 FIGURE 13. CORROSION TASK CARD NUMBER 2000-0551. NON-ROUTINE TASK CARD NUMBER 82897.SDR CKSA97034Angle · crackedDURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION RIGHT HAND FS 781.50 FLOORBEAM WEB CENTER WING ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW DC8 SRM 51-1-20D. CORROSION TASK CARD NUMBER 2000-0551. NON-ROUTINE TASK CARD NUMBER 82830.SDR CKSA97032Angle · corrodedDURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION LEFT OUTBOARD DOG HOUSE LOWER ANGLE CORRODED. REMOVED AND REPLACED ANGLE IAW SRM 51-1-8, 51-1-0, 51-1-20, 51-1-21, 51-1-4. CORROSION TASK CARD NUMBER 5700-0551. NON-ROUTINE TASK CARD NUMBER 83104.SDR RRXA97081Web · wornDURING A MAINTENANCE VISIT, FOUND RIGHT EXHAUST GATE INBD WEB AND UPPER ATTACH ANGLE WORN OUT OF LIMITATIONS. REMOVED ATTACH ANGLE AND WORN WEB. FABRICATED NEW WEB AND ATTACH ANGLE REPAIR AND INSTALLED IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH CO7-R23. SDR DHL9771285DClip · crackedDURING D-CHECK, FOUND SHEAR TIE CLIP CRACKED AT RADIUS AT UPPER END OF FORWARD SPAR CAP WEB VERTICAL STIFFENER AT RBL 25. REPLACED TIE CLIP AS PER SRM 51-10-1 AT WING CENTER SECTION FORWARD SPAR WEB.SDR DL72S970513Stiffener · crackedFOUND ON B1 LETTER CK, 1.5 INCH CRACK VERTICAL STIFFENER WING FRONT SPAR AT NR 7 SLAT INBD TRACK. REPAIRED PER MM 57-20-21.SDR DL72S970512Stiffener · crackedFOUND ON B1 LETTER CK, 1.25 INCH CRACK IN L/E SPAR STIFFENER INBD TRACK INBD RIB NR 4 SLAT. REPAIRED PER MM 57-20-21.SDR DL72S970511Stiffener · crackedFOUND ON B1 LETTER CK, 1 INCH CRACK IN L/E SPAR STIFFENER AT O/B TRACK INBD RIB NR 3 SLAT. REPAIRED PER MM 57-20-21.SDR MWEA97206Doubler · corrodedDURING INSPECTION, STA XFS 410 INBD 4 SLAT DRIVE TRACK RT WING LWR CAP FOUND CORRODED. MAINTENANCE REPAIRED IAW DAC TEL SVC-MSP-0119/PPS 01-31-97 AND SRM 57-09 FIG 18.SDR MWEA97196Bracket · corrodedDURING INSPECTION, STA 128 FWD SPAR LT WING LWR BRACKET EXFOLIATED. MAINTENANCE REPLACED IAW SRM 57-01.SDR MWEA97143Bracket · corrodedDURING INSPECTION, FOUND LT WING FWD FACE SPAR ANTI-ICE DUCT LWR MNT BRACK AT STA XIS 111, HEAVY CORRODED. MAINTENANCE REMOVED AND REPLACED BRACKET IAW SRM 57-01.SDR MWEA97142Strap · corrodedDURING INSPECTION, LT WING FWD FACE FRONT SPAR LWR CAP FWD TANG STRAP AT STA XIS 109 TO 132 HAS MOD CORROSION. MAINTENANCE REMOVED AND REPLACED STRAP.SDR ABXA9700342Angle · crackedDURING C INSPECTION, FOUND A RIGHT WING LEADING EDGE RIB ATTACH ANGLE CRACKED, AT NR 7 SLAT TRACK. REPAIRED RIB ATTACH ANGLE IAW DC-9 SRM CHAPTER 57-09 FIGURE 19.SDR 97UAL900216Closeout Panel · crackedA 3 VERTICAL CRACK WAS FOUND IN A FIBERGLASS CLOSEOUT PANEL AT BS 1241 CANTED PRESSURE DECK AREA IN RT WING WHEEL WELL. THE CRACK RUNS AMONG THE THREE UPPERMOST FASTENERS AT THE INBOARD EDGE VERTICAL ATTACHMENT OF THE PANEL AT RBL 98.58. THE CRACK WAS FOUNDSDR EISA97063Angle · crackedWING CENTER SECTION INTERIOR STATION 740, 'L' ANGLE AT TOP OF VERTICAL BEAM CRACKED IN RADIUS, RBL 12. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-1. (M)SDR EISA97062Stiffener · crackedWING CENTER SECTION INTERIOR STATIO 740, VERTICAL BEAM CRACKED IN RADIUS, RBL 8. FABRICATED AND INSTALLED NEW VERTICAL BEAM PER SRM 51-10-1 AND 51-30-2. (M)SDR EISA97061Angle · crackedWING CENTER SECTION INTERIOR FS 740, ANGLE ON TOP OF VERTICAL BEAM CRACKED IN RADIUS AT LBL 20. FABRICATED AND INSTALLED NEW 'L' ANGLE PER SRM 51-10-1. (M)SDR DHL9771286DAngle · crackedDURING D-CHECK, THE LEFT WING FRONT SPAR RIB ATTACH ANGLE WAS FOUND CRACKED. REPLACED RIB ANGLE, FIRST OUTBOARD OF BOTTLE PIN FITTING PER BOEING SRM 51-30-2.SDR ABXA9700349Web · crackedDURING C INSPECTION, FOUND THE RIGHT WING TRAILING EDGE AFT VERTICAL WEB CRACKED AT RIGHT OUTBOARD SPOILER REACTION ARM. REPAIRED CRACK IAW DC-9 SRM CHAPTER 57-01, FIGURE 3 SHEET 2.SDR EISA97047Angle · crackedLEFT WING UNDER PANEL 6401, 3RD AFT VERTICAL ANGLE CRACKED AT LOWER FASTENER APPROXIMATELY WS 92.8. FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-2. (M)SDR DHL9771260DAngle · crackedAT D-CHECK, INBOARD LT WING LEADING EDGE INNER RIB ANGLE AT WBL 92.8 CRACKED IN 6 PLACES AT LEADING EDGE TAI BOX. CUT OUT DAMAGED SECTION, HFEC AREAS, REPAIRED RIB ANGLES PER SRM 51-40-3, 1 BY 1 BY 7.SDR HALA9745Doubler · corrodedLEFT WING FLAP NR 4 LEADING EDGE CAP INBOARD AND OUTBOARD ATTACH FITTINGS HAVE CORROSION, LEVEL 2 LEFT WING XRS 232. REMOVED BRACKETS, REMOVED CORROSION AND TREATED, BRACKET MATERIAL LOSS IN LIMITS PER SRM 57-01 FIG 1 INSTALLED NEW CAP DOUBLERS PER SRM 51-30-SDR CALA9700366Support · crackedINSPECTION FOUND A 2 INCH CRACK IN RT WING FLAP WELL UPPER TRAILING EDGE PANEL SUPPORT JUST AFT OF AFT SPAR AT STA RSS 446.94. THE T-CHANNEL WAS REMOVED AND A NEW CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-7.SDR 97ZZZM676Doubler · corrodedLEFT WING FLAP NR 4 LEADING EDGE CAP INBOARD AND OUTBOARD ATTACH FITTINGS HAVE CORROSION, LEVEL 2 LEFT WING XRS 232. REMOVED BRACKETS, REMOVED CORROSION AND TREATED, BRACKET MATERIAL LOSS IN LIMITS PER SRM 57-01 FIG 1 INSTALLED NEW CAP DOUBLERS PER SRM 51-30-SDR UPS97822341Angle · crackedINSPECTION TYPE-D, LT STUB WING L/E ABOVE NR 1 ENG PYLON INBD ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW DWG 9753297, SRM 57-3-1 AND 51-1-21.SDR 9704769948Trap Fitting · crackedDURING PERIODIC CHECK, FOUND CRACK IN LEFT TRAPEZOIDAL FITTING IN LEFT WHEEL WELL BETWEEN 5TH AND 6TH BOLT FROM FORWARD END. INSTALLED REPAIR FITTINGS PER SRM 57-09 AND EA 99-112215.SDR CALA9700479Angle · corrodedINSPECTION FOUND RT WING AFT ATTACH ANGLE CORRODED UNDER PANEL NR 641JB. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 57-22-01, 51-10-00 AND 51-31-01.SDR P5CA9700369Stiffener · crackedCRACKED STIFFENER INSIDE LEADING EDGE OF LEFT WING AT INBOARD END OF INTERCOASTAL AT WS 270. FABRICATED AND INSTALLED STIFFENER PER BAC SRM 51-40-03.SDR 97ZZZX1148Rib Reinforcment · hangs gearUPON RETRACTION OF THE GEAR, THE BRAKE CALIPER FITTING P/N 754-857 OVERCENTERED INTO THE RIB CUT OUT AND THE GEAR WOULD NOT COME DOWN UPON EXTENSION. THE PILOT HAD TO 'G' LOAD THE AIRCRAFT AND EXTEND THE GEAR SIMULTANEOUSLY TO GET THE LEFT GEAR TO EXTEND. BOSDR UPS97223083Beam · corrodedINSPECTION TYPE:D, CORROSION IN BORE OF O/B HOLE ON L/GEAR BEAM FOR NR 5 FLAP TRACK ATTACHMENT. CORROSION REMOVED FROM HOLE PER SRM 51-40-6.SDR RRXA97057AAttach Angle · wornDURING A MAINTENANCE VISIT, FOUND RIGHT SIDE WING FLAP EXHAUST GATE HAD EXCESSIVE PLAY. AFTER REMOVAL, FOUND FWD UPPER ATTACHMENT BOLT HOLE FOR INBD ATTACHMENT POINT WORN BEYOND LIMITS AND INBD WEB AND UPPER ATTACHMENT ANGLE WORN. AWAITING ON ZANTOP AND COTNSDR CA970226043Rib Cap · cracked(CAN) CENTRE WING STA 178.8 R/H INBOARD UPPER RIB CAP FITTING CRACKED AT UPPER FORWARD TRUSS MOUNT ATTACHMENT HOLE. REPLACED.SDR CA970226042Sword Fitting · cracked(CAN) R/H WING OWS 303 SWORD FITTING CRACKED. REPLACED.SDR DHL9771287DClip · crackedDURING D-CHECK, THE SHEAR TIE CLIP AT THE RADIUS, UPPER END OF FORWARD SPAR WEB VERTICAL STIFFENER AT LBL 25 WAS FOUND CRACKED. REPLACED TIE CLIP PER BOEING SRM 51-10-1.SDR 9704229958Fitting · crackedDURING H-CHECK, FOUND CRACK IN LOWER AFT SKIN TO RIB ATTACH FITTING AT RWS 111.5 INBOARD SIDE. REPLACED FITTING PER SRM 51-30-5.SDR 9704219958Fitting · crackedDURING H-CHECK, FOUND CRACK IN LOWER AFT SKIN TO RIB ATTACH FITTING AT RWS 111.5 OUTBOARD SIDE. REPLACED FITTING PER SRM 51-30-5.SDR CALA9700307Bracket · crackedINSPECTION FOUND A .375 INCH CRACK IN LT WING LEADING EDGE RIB LOWER ATTACH BRACKET AT STA XRS 289, TWO RIBS INBOARD OF NR 9 SLAT TRACK. THE ATTACH BRACKET WAS REPLACED IAW SRM 51-30-2.SDR CALA9700304Bracket · crackedINSPECTION FOUND A 3 INCH CRACK IN LT WING LEADING EDGE RIB LOWER ATTACH BRACKET AND DOUBLER AT STA XRS 164, BETWEEN NR 5 AND NR 6 SLAT TRACKS. A REPAIR ANGLE AND DOUBLER WERE FABRICATED AND INSTALLED IAW ECRA 5710-01645.SDR P5CA9700320Stiffener · corrodedLEVEL 1 CORROSION ON RIGHT WING REAR SPAR VERTICAL STIFFENER OUTBOARD OF NR 3 ENGINE. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02.
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