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 P2EA99064Web · crackedSJO - RIGHT WHEEL WELL SKIN CRACKED AT BS 663, RBL 42, WL 195. DEFECT SIZE, AVERAGE LENGTH 2 INCHES. REPAIRED CENTER WING SECTION SPAR VERTICAL PRESSURE WEB BETWEEN RBL 37 AND RBL 52, BS 663 FROM WL 190 TO WL 202 PER BOEING FAX COO-SJO-990036RR DATED 1-12-99SDR DHL9971227CDoubler · misrepairedAT C-CHECK, LEFT WING PANEL NR 8405 HAS PREVIOUS REPAIR COMING LOOSE. INSTALLED BONDING REPAIR PER SRM 51-20-3, 17 X 5.SDR DHL9971213CTip · crackedAT C-CHECK, LEFT WING TIP CRACKED AND POPPED RIVETS AT UPPER TRAILING EDGE I/B SEAM. STOP DRILLED CRACKS, HFEC, INSTALLED DOUBLER REPAIR PER SRM 57-20-5, 4 X 6.SDR CALA9900055Tip · crackedLEFT WING LOWER WING TIP SURFACE HAS .5 INCH LONG HOLE WORK THROUGH AND .5625 INCH CRACK. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 57-30-2.SDR CALA9900054Angle · crackedRIGHT WING I/B OF I/B AILERON ANGLE IS CRACKED (.5) LOCATED ABOVE JACK SCREW AREA. REMOVED FASTENERS, FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-30-2 AND 57-20-4.SDR CALA9900052Tip · crackedRIGHT WING TIP AT LOWER SURFACE AFT OF MOUNT SCREWS HAS A 1 INCH LONG CRACK. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-2 AND 51-30-2.SDR CALA9900051Angle · crackedA 2.875 PIECE OF ANGLE BROKEN OFF AT TOP OF LEFT WING JUST FWD OF O/B AILERON L/E AT I/B END. REMOVED FASTENERS AND DAMAGED T ANGLE. FABRICATED AND INSTALLED NEW T ANGLE PER SRM 51-30-2 AND 57-10-7.SDR UPS99228431Web · crackedINSPECTION TYPE-C, LT WING NR 4 LE SLAT AND O/B ACTUATOR WEB CRACKED. CRACK STOP DRILLED IAW SRM 51-10-1 AND REPAIRED IAW SRM 57-50-3.SDR P2EA99063Angle · crackedSJO - RIGHT WING SPAR VERTICAL ANGLE CRACKED AT FSS 268. DEFECT SIZE, LENGTH .5 INCH. REPLACED FRONT SPAR VERTICAL ANGLE AT FSS 268 PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2, PAGE 5. (M)SDR DHL9971219CAngle · crackedAT C-CHECK, LEFT WING COVE PANEL SUPPORT ANGLES ARE CRACKED AT STA 573. REMOVED SUPPORT ANGLES AND REPLACED PER SRM 51-30-2.SDR DHL9971218CAngle · crackedAT C-CHECK, LEADING EDGE COVE PANEL SUPPORT ANGLE IS CRACKED JUST BELOW NR 3 SPOILER O/B HINGE. REMOVED AND INSTALLED ANGLE PER SRM 57-50-1.SDR DHL9971217CAngle · crackedAT C-CHECK, LEFT WING T/E COVE PANEL SUPPORT ANGLE IS CRACKED JUST I/B OF NR 3 SPOILER ACTUATOR STA 497. REMOVED AND INSTALLED SUPPORT ANGLE PER SRM 57-50-1.SDR DHL9971216CAngle · crackedAT C-CHECK, LEFT WING T/E COVE PANEL SUPPORT ANGLE IS CRACKED JUST BELOW NR 4 SPOILER I/B HINGE. REMOVED AND REPLACED COVE PANEL SUPPORT ANGLE PER SRM 51-30-2.SDR ASOA99021Angle · crackedDURING INSPECTION, FOUND LEFT AND RIGHT WING RIB 17, SPAR ANGLE CRACKED. MCN MAINTENANCE REPAIRED WING SPAR IAW ASA EO120-57-0067, REF DATA EAC FAX SST-0216/99, SST-2447/98 AND SRM 51-00-00. (M)SDR UPS99828658Angle · crackedINSPECTION TYPE-C123, RT WING L/E LOWER T-CAP FLANGE, STA XRS505 ANGLE CRACKED. REMOVED DAMAGE FROM FLANGE FAB DOUBLER FOR REPAIR IAW DAC DRAWING NR R08570014. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER IAW DC8 SRM 51-3-0.SDR UPS99828472Doubler · crackedINSPECTION TYPE:C3, RT WING L/E LWR SKIN AT STA XFS341.5, THE T/E INTERNAL DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 57-3-0 FIG 7.SDR UPS99828390Doubler · crackedINSPECTION TYPE:C3, RT WING L/E, INBD SKIN DOUBLER AT XFS 571 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D AND 51-1-21.SDR UPS99828389Doubler · crackedINSPECTION TYPE:C3, RT WING L/E, LWR T/E DOUBLER AT XFS 598 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 57-1-20D, 51-1-21.SDR UPS99828383Angle · crackedINSPECTION TYPE:C3, RT WING L/E INBD SIDE OF THE XS 520.168 RIB, THE VERTICAL ANGLE IS CRACKED AT THE LWR END. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297 AND SRM 51-1-20D.SDR UPS99828382Doubler · crackedINSPECTION TYPE:C3 RT. WING L/E, LWR SKIN INTERNAL DOUBLER, AT THE L/E OF THE NR 3 PYLON CUTOUT IS CRACKED. STOP DRILLED CRACK AND REPIARED IAW SRM 57-2-1A FIG 2.SDR 99T64R014Fitting · corrodedRIGHT W/W LONGERON FITTING STATION 920 CORRODED ABOVE LANDING GEAR UPLOCK CYLINDER. REMOVED CORRODED FITTING AND REPLACED WITH NEW FITTING PER SRM 57-3-2 AND SRM 51-1-20 UNDER WO NR 1310. (M)SDR 99T64R012Nut Plate · missingMISSING FASTENERS RIGHT WING LEADING EDGE. OPENED HOLES TO .260 DIAMETER AND INSTALLED NAS 1670 PER EO DRAWING NR 98-058 ON 8110-3 DATED 12/13/98 UNDER WO NR 1308. (M)SDR 99T64R011Nut Plate · missingMISSING FASTENERS LEFT WING LEADING EDGE SECTION. OPEN HOLES TO .260 DIAMETER AND INSTALLED NAS 1670 PER EO DRAWING NR 98-057 ON 8110-3 DATED 12/13/98 UNDER WO 1308. (M)SDR 99T64R008Angle · corrodedCENTER FUEL TANK TOP SIDE AT STATION 857 UNDER NR 4 FLOOR PANEL SURFACE CORROSION AFT TANK ANGLE. REMOVED CORROSION, FLAP PEEN BLENDED AREA PROTECT REWORKED AREA PER EO DRAWING NR 98-025 ON 8110-3 DATED 10/27/98 WO 1308. (M)SDR UPS99828566Intercostal · crackedINSPECTION TYPE-C3, LT WING L/E, I/B OF THE I/B SLOT, STA XFS 196, THE INTERCOSTAL WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE INTERCOSTAL IAW DWG 5769859 AND SRM 51-1-20D.SDR UPS99828381Angle · crackedINSPECTION TYPE:C3 LT OTBD STUB WING INBD RIB, THE VERTICAL SLOT ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753297 AND SRM 51-1-20D.SDR AT9900088Angle · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND LEFT WING INBOARD FLAP ATTACHED ANGLE AND SPAR CAP AT STA 137.50 AND REAR SPAR ATTACHED ANGLE AT STA 149 CORRODED. REMOVED NECESSARY FASTENERS IN ORDER TO GAIN ACCESS, CLEANED CORROSION, FABRICATED RIB, DOUBLER, ASDR A6WA9900023Bolt · brokenFRAME 29 LEFT AND RIGHT BOTTOM BOLT OF WING ATTACHMENT BRACKET HEAD APPEARS TO BE BROKEN. REMOVED BOLT, CLEANED AND INSPECTED HOLE, PREP, ALODINE, PRIMED AND INSTALLED NEW BOLT AND NUT IAW FAX DJR/RJ0022/96 AND DJR/RJ0721-96. WITCO BOND WILL BE APPLIED ON WOSDR UPS99828659Angle · crackedINSPECTION TYPE-C123, LT WING LOWER LEADING EDGE I/B STA XWO ANGLE CRACKED AT O/B END OF ANGLE. FAB DOUBLER IAW 57-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-21. INSTALLED DOUBLERS IAW DC8 SRM 51-1-20D.SDR ASOA99003Angle · crackedDURING INSPECTION FOUND LEFT WING, RIB 17, SPAR ANGLE CRACKED. MCN MAINTENANCE REPAIRED WING SPAR IAW ASA EO120-57-0066, REFERENCE DATA EAC FAX SST-2447/98 AND SRM 51-00-00. (M)SDR ABXA9900096Web · crackedCRACKED WEB GUSSETT INSIDE RIGHT WING LEADING EDGE BETWEEN PANELS 519C AND 520A ABOVE ANTI-ICE VALVE. REPAIRED IAW DC8 SRM 51-3-0.SDR AALA990023Angle · damagedDURING C-CHECK, GOUGE FOUND IN REINFORCEMENT ANGLE, OUTBOARD SIDE OF FUSELAGE ABOVE WING STATION 760.95. ANGLE REMOVED AND REPLACED. (M)SDR UPS99828721Fitting · crackedINSPECTION TYPE:C RT WING STA 410 FLAP HINGE CANOE FITTING SIDE BRACE FITTINGS, 2EA ARE CRACKED. REMOVED AND REPLACED FITTINGS IAW SRM 51-3-0.SDR UPS99828373Fitting · crackedLT WING STA 410 FLAP CANOE INBD SIDE BRACE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.SDR AT9900133Splice · crackedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND LEFT WING STA XOS 290.0 LEADING EDGE SKIN SPLICE CRACKED. REMOVED AND REPLACED SPLICE PLATE, FABRICATED SPLICE PLATE, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-2 AND RES NR 99199.SDR UPS99828410Angle · crackedINSPECTION TYPE-C, RT WING L/E INBOARD SIDE OF THE XS 250.089 RIB, THE VERTICAL ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753293 AND SRM 51-1-20D.SDR QXEA9900171Strip · chafedPDX - .25 INCH CHAFE MARK ON FORWARD END OF LOWER CENTER TO OUTER WING JOINT STRIP. REPAIRED IAW HORIZON AIR EA 4-57-202.SDR UPS99828408Doubler · corrodedINSPECTION TYPE-C, RT WING L/E AT ACCESS PANEL 519B, THE INTERNAL DOUBLER HAS MODERATE EXFOLIATION CORROSION. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 3641256 AND SRM 51-1-20D AND 51-1-21.SDR MWEA981186Doubler · misdrilled2 HOLES WERE MISDRILLED ON THE LEFT MAIN GEAR UPPER SUPPORT DOUBLER. FABRICATED AND INSTALLED REPAIR BUSINGS INSTALLED NOMINAL FASTENERS.SDR ABXA9801198Clip · crackedDURING C-CHECK, FOUND CRACKED SHEAR CLIP AT RIGHT WING STATION XRS 69.00 AT AFT BOTTOM. REPLACED SHEAR CLIP IAW DC9 SRM 51-10-04.SDR 99ZZZX417Doubler · crackedA PREVIOUSLY INSTALLED REPAIR DOUBLER CRACKED AT THE LOWER BOLT OF THE RIGHT DRAG STRUT ATTACH FITTING. CRACK APPEARS TO BE FROM IMPROPER INSTALLATION OF REPAIR DOUBLER.SDR C2XA98IA519Fitting · wornIAH - DURING C-CHECK INSPECTION, THE RIGHT WING SPAR LOWR FITTING AT RIB 18 WAS FOUND TO HAVE AN ELONGATED FLAP PANEL MOUNT HOLE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FITTING IAW THE ATR 42-320 SRM 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURNSDR 99ZZZX281Washer · wrong partUPON INSPECTION OF THE WING ATTACH A-BOLT, NOTED THE WASHER LISTED IN THE PARTS MANUAL, AN 960-C616, PAGE I-53-2, IS INCORRECT IN SIZE AND WILL ALLOW THE BOLT TO PULL THROUGH THE ATTACH BRACKET. THE PROPER BOLT, P/N MS 16212-13, WAS OBTAINED THROUGH DIAMOND ASDR COMA9810284Support · crackedRIGHT WING SKIN SUPPORT NR 37 AT RIB NR 9 CRACKED. REPLACED SKIN SUPPORT.SDR COMA9810283Support · crackedRIGHT WING SKIN SUPPORT NR 30 AT RIB 6 CRACKED. REPLACED SKIN SUPPORT.SDR COMA9810279Support · crackedWING SKIN SUPPORT CRACKED. REPLACED SKIN SUPPORT.SDR COMA9810281Support · brokenDURING FUEL LEAK REPAIR, FOUND SKIN SUPPORT BROKEN IN THE RIGHT WING, RIB 16, BOTTOM CENTER. REPLACED SKIN SUPPORT.SDR RRXA99981Flange · damagedDURING A MAINTENANCE VISIT, FOUND OVERSIZED HOLES IN AFT UPPER SPAR FLANGE ON RIGHT WING BETWEEN XRS= 436.500 AND XRS = 456.563. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. OVERSIZED HOLES APPROVED IAW FAA APPROVESDR DL72L982508Stiffener · crackedREF SHIP 512 TPA LTR CHK D-1 12-07-98, L/E SPAR STIFFENER CRACKED AT NR 6 SLAT I/B TRACK I/B STIFFENER. REPLACED PER MM 57-20-21.SDR QXEA9801896Angle · crackedPDX - RIGHT WING LOWER CONNECTION ANGLE AT MAIN LANDING GEAR BRACKET TO REAR SPAR IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-05.
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