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 UPS99830780Doubler · crackedINSPECTION TYPE:C123, LT WING L/E LWR SKIN INTERNAL DOUBLER AT FS 336.75 WAS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED THE INTERNAL DOUBLER IAW DWG 5769589 AND SRM 51-1-20D & 51-1-21.SDR UPS99830772Doubler · crackedINSPECTION TYPE:C123, LT WING L/E LWR SKIN DOUBLER AT STA XFS 304.0 IS CRACKED FWD OF THE DOUBLER T/E. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D.SDR UPS99830771Angle · crackedINSPECTION TYPE:C123, LT WING LEADING EDGE I/B SIDE OF THE XS520.168 RIB, THE SLOT AFT BULKHEAD VERTICAL ANGLE IS CRACKED AT THE LWR END. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753297 AND SRM 51-1-20D.SDR UPS99230642Beam · corrodedINSPECTION TYPE:SI, LT MLG BEAM IS CORRODED AT NR 4 FLAP TRACK MOUNT BOLT HOLES. REMOVED CORROSION AND REPAIRED LG BEAM PER ER NR 99-6038.SDR DL72L992054Stiffner · crackedFOUND ON MV2 CK, L/E WING SPAR STIFFENER CRACKED AT THE NUMBER 7 SLAT O/B TRACK O/B SIDE. REPAIRED PER MM 57-20-21.SDR DL72L992053Stiffner · crackedFOUND ON MV2 CK INBD AND OUTBD SPAR STIFFENERS CRACKED AT THE NUMBER 7 SLAT I/B TRACK ON THE FWD WING SPAR. REPAIRED PER MM 57-20-21.SDR UPS99830774Doubler · crackedINSPECTION TYPE:C123, RT WING L/E AT FS 341.5, THE INTERNAL DOUBLER HAD A 7 INCH CRACK. REPAIRED THE DOUBLER IAW DH SK718-263.SDR UPS99230936Stiffner · corrodedINSPECTION TYPE:SI, WHILE WORKING CUST ID 997970, DISCOVERED RWS 185.30 VERTICAL STIFFENER CORRODED BEYOND ALLOWABLE LIMITS. REPLACEMENT OF STIFFENER WILL BE ACCOMPLISHED ON CUSTOMER ID 997970 PER SRM 51-30-2.SDR UPS99230935Stiffner · corrodedINSPECTION TYPE:SI, WHILE WORKING CUSTOMER CARD NR 997970, (WINGS 237) FOUND STIFFENER AT WS 173.25 CORRODED BEYOND ALLOWABLE LIMITS. REPLACEMENT OF STIFFENER WILL BE ACCOMPLISHED ON CUSTOMER ID 997970, PER SRM 51-30-2.SDR UPS99230634Stiffner · crackedINSPECTION TYPE:C RW VERTICAL STIFFENER ON FWD WEB JUST O/B OF 740 BOTTLE PIN IS CRACKED AT BOTTOM FASTENER. REMOVED STIFFENER, FABRICATED A NEW ONE, ALODINED AND PRIMED NEW STIFFENER. INSTALLED STIFFENER, ALL WORK ACCOMPLISHED IAW SRM 51-30-05, BOEING DRAWISDR DL72S992012Stiffener · cracked2 INCH VISIBLE CRACK IN VERT SPAR STIFFENER I/B SIDE OF O/B TRACK NR 3 L/E SLAT. REPAIRED PER MM 57-20-21 P 813.SDR ABXA9900695Fitting · crackedDURING C-CHECK, FOUND FITTING CRACKED AT LEFT WING SLAT DRIVE. REPLACED FITTING IAW ABX REA D957-33196.SDR DL76S992060Fitting · corrodedRT WING, I/B UNDERWING SIDE LOAD FITTING WAS FOUND WITH CORROSION DAMAGE IN THE BORE. REPAIR PER ER/A 333555-14 REV A.SDR CALA9901153Support · crackedINSPECTION FOUND A 2 CRACK INCH LT WING REAR SPAR WEB LOWER SUPPORT JUST O/B OF FLAP I/B HINGE, XRS 189. THE ANGLE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-10-4, 51-10-3, AND 51-30-2.SDR A6WA9900110Stiffener · crackedRIGHT WING UPPER WING STIFFENER OUTBOARD OF RIB 8 IS CRACKED AT FORWARD END. REPLACED RT WING UPPER WING STIFFENER AT THIS TIME OUTBOARD OF RIB 8 IAW BAE FAX NR REF DJR/RJ0630-98. (M)SDR A6WA9900109Stiffener · crackedRIGHT WING UPPER WING STIFFENER INBOARD OF RIB 9 IS CRACKED AT FORWARD END. REPLACED UPPER WING STIFFENER INBOARD OF RIB 9 AT THIS TIME IAW FAX REF DJR/RJ0630-98. (M)SDR 99ZZZX3943Beam · crackedRIGHT WING J-BEAM HAS APPROXIMATELY .3750 INCH CRACK ABOVE NR 8 SPOILER ACTUATOR. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER STATED DESIGN FLAW OR WING FLEX CAUSE OF CRACK.SDR 99ZZZX3939Stiffener · crackedONE INCH CRACK AT TOP OF STIFFENER INSIDE RIGHT WING LEADING EDGE AT INBOARD SIDE OF LEADING EDGE RIB WDL 92.0. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER SUGGESTED AREA SUBJECTED TO STRESS LOADS AND FLEX.SDR 99ZZZX3938Web · crackedLEFT WING LEADING EDGE LBL 92.0 WEB CRACKED 1.5 INCHES DOWN FROM TOP AFT VERTICAL STIFFENER. ACCESS 6302. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER SUGGESTED WING FLEX OR STRESS LOADS POSSIBLE CAUSE.SDR 99ZZZX3935Stiffener · crackedONE INCH CRACK AT TOP OF SECOND FROM AFT STIFFENER INSIDE RT WING LE AT INBOARD SIDE OF LEADING EDGE RIB WBL 92.0, ACCESS CUT-OUT 6402. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. AREA EXPOSED TO STRESS LOADS.SDR UPS99830570Flapwell · damagedINSPECTION TYPE:N/A, RT WING FLAPWELL DAMAGED BY FLAP ACT LINK FAILURE. *S/D* REF DMI D178387 INTERIM REPAIR TO RT WING AUX SPAR. TRANSFERRED TO NRC 626624 C/W REPAIR PER EO DC8-5720-11513-A. OK FOR A ONE TIME FLIGHT TO DHC FOR PERMANENT REPAIR.SDR DL72E992043Angle · crackedAT HMV, FOUND RT WING REAR SPAR LWR CHORD ANGLE IS CRACKED, O/B OF NR 5 FLAP TRACK. REMOVED CRACKED SECTION, FABRICATED NEW PER MM 57-55-0, AND INSTALLED.SDR A6WA9900108Stiffener · crackedLEFT WING UPPER TRAILING EDGE STIFFENER OUTBOARD OF RIB 8 IS CRACKED AT FORWARD END. REPAIRED LEFT WING UPPER TRAILING EDGE STIFFENER OUTBOARD OF RIB 8 IAW BAE FAX DJR/RJ0630-98. (M)SDR A6WA9900107Stiffener · crackedLEFT WING UPPER TRAILING EDGE STIFFENER OUTBOARD OF CENTER LIFT SPOILER JACK IS CRACKED AT FORWARD END. REPAIRED LEFT WING UPPER TRAILING EDGE STIFFENER OUTBOARD OF CENTER LIFT SPOILER JACK. WORK ACCOMPLISHED IAW BAE FAX REF JM/RJO317/97 AND FAX REF DJR/RJ06SDR A6WA9900106Stiffener · crackedUPPER TRAILING EDGE STIFFENER INBOARD OF NR 3 FLAP TRACK IS CRACKED AT FORWARD END, LEFT WING. REPLACED LEFT WING UPPER TRAILING EDGE STIFFENER INBOARD OF NR 3 FLAP TRACK. WORK ACCOMPLISHED IAW BAE SRM STD PRACTICES. (M)SDR USAA990927Stiffener · corrodedTPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 3 INCH AREA OF CORROSION, LOWER END OF STIFFENER, STATION 540, RBL 14.90. CORROSION LEVEL 1. INSTALLED REPAIR DOUBLER PER SRM 51-40-4 FIG 1.. (M)SDR 99T64R448EWAFlange · gougedFOUND DURING D-CHECK, FLANGE ON AFT SIDE OF OUTBOARD W/W AT WING AT WING STATION XRS 90.0 GOUGE APPROX .25 INCH IN DIAMETER. (M)SDR UPS99230612Te Wedge · corrodedINSPECTION TYPE:C, DURING REPAIR ON RT INBOARD MID FLAP DELAMINATION, CORROSION FOUND O N T/E WEDGE UPPER SURFACE. REPLACED MID FLAP IAW MM 27-51-23.SDR 2000ZZZM229Fitting · crackedDURING B-CHECK INSPECTION, FOUND 20 INCH CRACK AT LEFT INBOARD CANOE FITTING AT STATION 98. REPLACED FITTING AT LEFT CANOE IAW MM 27-27-7. (M)SDR UPS99230590Bracket · crackedINSPECTION TYPE:C RT WING, LWR FIXED TE PANEL SUPPORT BRACKET CRACKED AREA AT NR 8 SPOILER CENTER HINGE SUPPORT FITTING. BRACKET REMOVED AND REPLACED IAW SRM 51-10-3 SRM 51-20-1 SRM 51-30-2.SDR RRXA991629Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, RIGHT, RT OB FLAP AT STA X=410 FLAP SUPPORT FITTING LWR SURFACE UNDER FLAP TRACKS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW SDR RRXA991518Fitting · corrodedDURING A MAINTENANCE VISIT FOUND SPOTS OF CORROSION ON RT O/B FLAP AT STA X-410, FLAP SUPPORT FITTING LWR SURFACE UNDER FLAP TRACKS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW SDR DHL9980625CStrip · brokenAT C CHECK, LT WING UPPER EXTERIOR SURFACE CTR SPAR TRIM ANGLE BROKEN XRS 50. REMOVED DAMAGED STRIP AND FABRICATED NEW METAL STRIP FROM SAME MATERIAL IAW DC8 SRM 51-1-4 PAR 3. INSTALLED STRIP IAW DC8 SRM 51-1-15, PAR 2. N/R CARD NR 0711.SDR DLL14991925Stiffener · crackedTHE RBL 22.5 VERTICAL STIFFENER ON THE CENTER WING FRONT SPAR (FS 983) WAS FOUND WITH A TYPICAL CRACK EMANATING FROM A LIGHTENING HOLE IN THE STIFFENER WEB NEAR THE UPPER END. THE STIFFENER WAS REMOVED AND REPLACED WITH A NEW STIFFENER MANUFACTURED WITHOUSDR MWEA99549Web · crackedCRACK AT CENTERLINE FRAME LEFT SIDE OF FRAME WEB. MTC FABRICATED AND INSTALLED REPAIR.SDR TSAA9957416Beam · corrodedLEFT MLG BEAM CORRODED BEYOND LIMITS. REPLACED LEFT MLG BEAM (PERFORMED BY BOEING AOG TEAM). AIRCRAFT RETURNED TO SERVICE. (M)SDR P2EA99292Beam · crackedSJO - SPAN WISE BEAM NR 1 CRACKED AT STRINGER 9C BL 0. REPAIRED IAW COOPESA EO COO-3-57-520-99. (M)SDR UPS99830537Fitting · crackedINSPECTION TYPE:C3, RIGHT WING O/B AILERON ATTACH FITTING CRACKED (VERIFIED BY EDDY CURRENT INSP) AT LOWER MOUNT BOLT HOLES BELOW AILERON DAMPERS STA XW 693. INSTALLED NEW FITTING STA 693 AND TORQUED PER DC8 M/M 20-16-0 & 57-40- 00. REMOVED R/W O/B AILERON ASDR 20000515AP006Stiffener · crackedFOUND LEFT WING LEADING EDGE WBL 92 TOP OF CENTER STIFFENER CRACKED AT JOGGLE BELOW HI-LOCK THROUGH ACCESS 6302. REMOVED AND REPLACED CRACKED STIFFENER IAW SRM 51-30-2 PAGE 2. (M)SDR 20000515AP005Web · crackedFOUND LEFT WING LEADING EDGE WBL 92 WEB CRACKED 1.5 INCHES DOWN FROM TOP AFT VERTICAL STIFFENER. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBELR REPAIR IAW SRM 53-10-9 PAGE 19. (M)SDR UPS99830433Splice · crackedINSPECTION TYPE:C1, RT WING L/E SPLICE AT XFS 710 WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE SPLICE IAW SRM 57-3-3 AND 51-3-0.SDR UPS99830376Doubler · crackedINSPECTION TYPE:C1 RT WING L/E LWR SKIN INTERNAL DOUBLER AT XFS 336 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D AND 51-1-21.SDR DHL9972712CAngle · crackedAT C CHECK, LT WING COVE PANEL SUPPORT ROD ATTACH ANGLES CRACKED STA 568 OUTBD NR 2 SPOILER ACT. REPLACED LT WING COVE PANEL SUPPORT BRKT AT STA 568 O/B OF NR 2 SPOILER ACT PER B727 SRM 51-30-2 N/R 1464.SDR DHL9972704CBracket · crackedAT C CHECK, LT WING COVE PANEL SUPPORT ROD I/B OF NR 2 SPOILER ACT LOWER END SUPPORT BRACKET CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW B727 SRM 51-30-2 N/R 1465.SDR UPS99830547Intercostal · crackedINSPECTION TYPE:C3, LEFT WING, TRAILING EDGE STA 339, INTERCOSTAL CRACKED FITTING CHAFED OUT OF LIMITS. REMOVED INTERCOSTAL, FABRICATED AND INSTALLED INTERCOSTAL AND NEW SUPPORT FITTING (P/N 5707538-3) IAW DC8 SRM 57-5-1 & 51-1-21.SDR DHL9972711CBracked · crackedAT C CHECK, LT WING COVE PANEL SUPPORT ROD ATTACH BRACKET CRACKED I/B NR 3 SPOILER ACT. REPLACED SUPPORT ROD ATTACH BRACKET AT LT COVE I/B AT NR 3 SPOILER ACT PER B727 SRM 51-30-2 N/R 1469.SDR DHL9972705CBracket · crackedAT C CHECK, LT WING REAR SPAR CAVITY AREA WS 544.00 COVE PANEL LOWER SUPPORT BRACKET CRACKED. REMOVED AND REPLACED I/B AND O/B BRACKETS AT LT WING REAR SPAR WS 544.00 PER SRM 51-30-2 N/R 1421.SDR DHL9972703CSupport · crackedAT C CHECK, LT WING REAR SPAR CAVITY AREA WS 567.0 COVE PANEL LOWER SUPPORT CRACKET CRACKED. REPLACED COVE PANEL SUPPPORT BRKT AT WS 567.0 PER B727 SRM 51-30-2 N/R 1422.SDR DHL9972702CSupport · crackedAT C CHECK, LT WING REAR SPAR CAVITY AREA WS 499.0 COVE PANEL LOWER SUPPORT BRACKET CRACKED. REPLACED LT WING COVE PANEL SUPPORT BRACKET AT WS 499 PER B727 SRM 51-30-2 N/R 1423.SDR RRXA991657Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E AT STA XW 0.00, THE UPPER AFT L/E ATTACH ANGLE CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW MFG DWG 5613646 AND DC
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