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 ABXA000379Web · crackedLEFT WING TRAILING EDGE WEB, FORWARD OF AILERON, CRACKED APPROXIMATELY TWO INCHES FROM OUTBOARD EDGE.SDR RRXA003014Bracket · brokenDURING A MAINTENANCE VISIT FOUND A BROKEN BRACKET ON THE LT WING L/E WING LOWER L/E AT STA XFS 622, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DCSDR UPS00433745Cap · crackedINSPECTION TYPE:C, RT WING - TRAILING EDGE SUPPORT BEAM UPPER CAP DEEP CORROSION AND A LONG CRACK WERE FOUND AT THE UPPER AFT FLANGE OF THE UPPER CHORD. REPAIR ACCOMPLISHED PER IAI EO 89310 AND AS APPROVED BY FAA-8110-3 FORM. THE CHORD AT WBL 360 TRIMMED OUSDR DHL200070960DFitting · damagedRT WING FRONT SPAR TERMINAL FITTING CRACKED IN BOTTLE PIN HOLE (APPROX 3 IN CRACK) VERIFIED BY HFEC. REMOVED LEADING EDGE PER SRM 51-30-2. REMOVED WIRING AS PER M/M 27-82-00. REMOVED FUEL LINE S PER M/M 28-22-0. PLACED A/C IN JIG POSITION PER SRM 51-50-1 ASDR AU000557Strut · corroded(AUS) LEFT WING STRUT CORRODED IN AN AREA LOCATED APPROXIMATELY 355.6 MM (14 INCHES) OUTBOARD FROM THE LOWER ATTACHMENT FITTING ON THE AFT WEB. FOUND DURING INSPECTION IAW AD/DHC6/58 AND SB 6-474. (X)SDR AT0000366Fitting · gougedFOUND LEFT WING LEADING EDGE GOUGED AT CENTER RIB FITTING. BLENDED OUT GOUGE AND REPAIRED IAW REO-L00228.SDR ABXA000334Stiffener · crackedREAR SPAR STIFFENER WAS CRACKED AT STATION XRS 313. REPLACED STIFFENER IAW DC9 SRM 51-30-5.SDR AU000607Spar · failed(AUS) PORT WING SPAR FAILED IN COMPRESSION AT DIHEDRAL ''CRANK''. REAR UPPER SPAR BOOM FAILED IN BOX SPAR AT TWO POINTS: VERTICAL PLY FACE OF BOX SPAR FAILED AT OUTER FAILURE, AND UPPER PLY FACE FAILED AT NEXT INBOARD RIB.SDR DHL200070956DAngle · crackedLT WING LEADING EDGE CAVITY VERTICAL SUPPORT ANGLES FOR THE NR 3 SLAT I/B TRACK SUPPORT RIBS ARE CRACKED. LOCATED AT FRONT SPAR. REMOVED FUEL LINE TO GAIN ACCSES PER M/M 28-22-131. REMOVED HYD LINES FOR ACCSESS PER M/M 29-00. REMOVED VERT SUPPORTS PER SRM SDR DHL200070922CWeb · crackedLEFT WING WEB CRACKED AT UPPER I/B AFT SIDE WBL 273.3. STOP DRILLED CRACK PER SRM 51-10-1. INSPECTED WITH HFEC PER NDT M/M 6-51-000, CONFIRMED NO CRACK PAST STOP DRILL. INSTALLED DOUBLER REPAIR PER SRM 51-40-2. TREATED AND PRIMED AREA PER SRM 51-10-2.SDR DL72W001268Stiffener · crackedSPAR STIFFENER CRACKED I/B OF I/B TRACK NR 2 SLAT. REPLACED STIFFENER PER MM 57-20-21.SDR DL72W001267Stiffener · crackedNR 7 SLAT I/B TRACK I/B SPAR STIFFENER FOUND CRACKED. DURING E-1 LETTER CHECK.SDR QXEA0001951Bracket · crackedPDX- CRACK IN WING REAR SPAR BRACKET AT OUTBOARD BOLT. REPAIRED IAW FOKKER SRM 57-02-09, PAGE 5.SDR QXEA0002056Angle · corrodedPDX- RIB 1700 LEFT HAND CONNECTION ANGLE CORROSION BY 20TH BOLT AFT FROM FRONT IN WING CENTER SECTION. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5.SDR QXEA0002055Angle · corrodedRIB 1700 LEFT HAND CONNECTION ANGLE CORROSION BY 17TH BOLT AFT FROM FRONT IN WING CENTER SECTION. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5.SDR QXEA0002054Angle · corrodedPDX- RIB 1700 LEFT HAND LOWER CONNECTION ANGLE CORROSION BY 13TH AND 14TH BOLTS FROM FRONT IN WING CENTER SECTION. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5.SDR QXEA0002053Angle · corrodedPDX- RIB 1700 LEFT HAND LOWER CONNECTION ANGLE CORROSION BY 6, 7, AND 9 BOLTS FROM FRONT IN WING CENTER SECTION. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5.SDR QXEA0002052Angle · corrodedPDX- RIB 1700 LEFT HAND CONNECTOR ANGLE CORROSION NEAR 2ND BOLT FROM FRONT IN WING CENTER SECTION. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5.SDR QXEA0002051Fitting · corrodedPDX- CORROSION AROUND BOLT HEAD/WASHER UPPER REAR SPAR END FITTING. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5.SDR RRXA003013Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE ATTACH CLIP ON THE LT WING CTR L/E MIDDLE OF L/E AT SPLICE TOP SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1SDR RRXA003011Doubler · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SPLICE ON THE LT WING CTR L/E MIDDLE OF L/E DOUBLER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW SDR RRXA003005Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CTR L/E #4 RIB I/B BOTTOM OF L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51SDR GAIA00380Angle · crackedDURING ROUTINE C-CHECK, FOUND A CRACK IN THE FORWARD UPPER HOLE IN THE UPPER VERTICAL FLANGE OF THE WING TO BODY RIB FITTING UPPER CHORD AT RIGHT BS 760.95. COMPLIED WITH BOEING 727 SB 727-57-0112 REV 5. INSTALLED SUPPORT ANGLE IAW BOEING 727 SB 57-0112 AND SDR QXEA0002040Rivet · misinstalledPDX- RIVET INSTALLED IN CLEAT WITHOUT PROPER GAUGE DISTANCE IN AFT INBOARD OF STRUT BAY STATION 1877. REPAIRED IAW FOKKER SRM 57-22-02, PAGE 19 AND SRM 51-30-02, AND SRM 51-31-01.SDR RRXA002719Nut Plate · missingDURING A MAINTENANCE VISIT FOUND A BROKEN NUT PLATE ON THE RIGHT O/B SLOT UPPER SIDE SCREW AT STA XS 515, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW EO NR 00-107 WITH APPROVED 8SDR RRXA003016Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CHANNEL NUT PLATES ON THE LT L/E ABOVE NR 1 PYLON ANGLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, ALODINED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-SDR RRXA003003Doubler · crackedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE LT WING L/E O/B OF #2 PYLON L/E DOUBLER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, ALODINED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW SDR RRXA003002Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN LOWER SPAR CAP, WEB AND SKIN LOWER ON LEFT WING AT STA XFS 576, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPASDR ABXA000358Door · delaminatedLEFT BUTE DOOR NR 1502 WAS DELAMINATED. REPLACED BUTE DOOR.SDR COMA0010220Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-244-01I, THE RIGHT WING ATTACH ANGLE FOR FAIRING 194 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #1226-21, IR, 7/6/99.SDR COMA0010208Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-243-01I, THE LEFT WING ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #1226-21, REV IR, 7/6/99.SDR 20001204AP009Web · corrodedMAIN CABIN SHEAR WEB FLOOR SHOWING CORROSION ON SURFACE FROM BS 1150 TO 1183 LBL 18 AND EXFOLITIVE CORROSION ON PLATE ATTACHED (REINFORCEMENT). REMOVED DAMAGED AREAS AND FABRICATED DOUBLER AND FILLER IAW SRM 51-40-2 PAGE 1. TREATED, PRIMED AND INSTALLED IAW SDR 20001204AP007Angle · crackedR/W REAR SPAR LOWER ANGLE SECTION CRACKED AT HOLE POINT, AFT SECTION OF MLG (LOWER AREA OF NR 8 SPOILER ACTUATOR). STOP DRILLED CRACK IAW SRM 51-10-1 PAGE 4 AT R/W REAR SPAR LOWER ANGLE BELOW NR 8 SPOILER FABRICATED ANGLE. TREATED WITH ALODINE AND PRIMER ANDSDR 20001204AP006Web · crackedRT WING AFT SECTION OF MLG (REAR SPAR) AT ATTACHED FITTING AREA, WEB SHOWING TWO CRACKS ON SURFACE AND LITTLE FORMED ANGLE CRACKED. FABRICATED NEW SECTION WEB AS PER SAMPLE AT RW SPAR AFT SECTION OF MLG REAR SPAR. TREATED WITH ALODINE AND PRIMED. INSTALLED SDR 20001204AP005Intercostal · crackedLEFT WING INBOARD AFT OF MAIN LANDING GEAR ATTACHED FITTING HAS INTERCOSTAL CRACKED. STOP DRILLED CRACK IAW SRM 51-10-1 PAGE 4. FABRICATED ANGLE IAW SRM 51-40-4 PAGE 10. TREATED PRIMED AND INSTALLED REPAIR WITH FASTENERS IAW SRM 51-40-4 PAGE 10. (M)SDR 20001204AP004Intercostal · crackedRIGHT WING INBOARD AFT OF MAIN LANDING GEAR ATTACHED FITTING HAS INTERCOSTAL CRACKED. STOP DRILLED CRACK IAW SRM 51-10-1 PAGE 1. FABRICATED ANGLE IAW SRM 51-40-4 PAGE 10. TREATED AND PRIMED, INSTALLED REPAIR IAW 51-40-4 PAGE 10. (M)SDR UPS00832993Intercostal · crackedINSPECTION TYPE: C123 RT WING L/E. LOWER INTERCOSTAL IS CRACKED AT XFS 341 REMOVED, FABRICATED, AND REPLACED INTERCOSTAL I.A.W. DWG. 5769589,AND SRM. 51-1-20DSDR DL72K001193Stiffener · crackedRT WING REAR SPAR STIFFENER , WS 543.68 THE RT WING REAR SPAR WAS FOUND WITH A CRACKED STIFFENER AT WS 543.68. THE DAMAGED STIFFENER WAS REMOVED AND A NEW STIFFENER INSTALLED WITH A STRUCTURAL SHIM PER ER/A 377615-14, REV A.SDR 00FDEA00399Support Bracket · crackedSNRM 0338 RT WING PANEL SUPPORT FOR PANEL NR 618GB WAS CRACKED, LOCATED APPROX 4 INCHES OB OF SLAT DRIVE MECH ACCESS PANEL. R&R PER SRM 51-31-01.SDR UPS00833195Angle · crackedINSPECTION TYPE: C1, LT WING L/E VERTICLE ANGLE AT XS 250 IS CRACKED. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG. 5769515, AND SRM. 51-1-20DSDR UPS00833021Angle · crackedINSPECTION TYPE:C123, RIGHT WING LEADING EDGE I/B SUPPORT ANGLE IS CRACKED AT XFS -23.75. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5769646 AND SRM 51-1-20D.SDR COMA0010170Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-243-01I, THE LEFT WING UPPER SURFACE ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, REV IR, 7-6-SDR COMA0010169Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-244-01I, THE RIGHT WING UPPER SURFACE ATTACH ANGLE FOR FAIRING 194 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, REV SDR TWAA0009703Door · crackedDURING CHECK-C MAINT ON THE RT WING, THE I/B BUTTE DOOR 1602C HAD A CRACK AT SCREW HOLE. STOP DRILLED CRACK, MADE DOUBLER 0.032 TITANIUM PER SRM 57-01. EDDY CURRENT INSP PER 51-00-03 WITH CRACK CONTAINED.SDR DL72S001153Angle · crackedFOUND AT F-1 LETTER CHECK, NR 8 SLAT ACT I/B AND O/B SUPPORT DOUBLERS CRACKED. REPAIRED PER MM 57-20-21.SDR DL72S001152Stiffener · crackedFOUND AT F-1 LETTER CHECK, NR 7 O/B SLAT TRACK I/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21.SDR COMA0060497Angle · crackedTHE LEFT HAND WING SPOILER NUT PLATE ANGLE ASSEMBLY IS DAMAGED. REPAIRED LEFT HAND WING SPOILER NUT PLATE ANGLE ASSEMBLY BY REMOVING AND REPLACING DAMAGED ANGLE ASSEMBLY IAW WVAC EO 601R-57-1380.SDR UPS00833039Intercostal · crackedINSPECTION TYPE:C123, LEFT WING L/E INTERCOSTAL IS CRACKED BETWEEN XFS 195 - 201. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5769859 AND SRM 51-1-20D, 51-1-21.SDR UPS00832938Angle · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER SUPPORT ANGLE IS CRACKED AT XRS 2 FRONT SPAR. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 4776168 AND SRM 51-1-20D.SDR UPS00833391Mount · damagedINSPECTION TYPE:C123, SEVERAL TANK MOUNTING BOLT HOLES ARE ELONGATED ALONG THE UPPER FWD MOST O/B END OF THE LEFT WING L/E TANK. MATL ID 2024-0 .090 PO NR 328799 IAW DC8 SRM 57-2-1. FABBED REPAIR DOUBLER IAW DC8-5720-7767 HEAT TREATED IAW TPS-1003 REV A DRIL
Back to JASC 5720