JASC 5714

Service difficulty reports · 1,451

Reports filed under 5714 · Wing, Center Box, 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 = '5714'
  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.

SDR 07FDEA01624Skin · corrodedCORROSION AT CENTER WING BOX TOP SKIN AT TRACK 5-6 LT ON C46.2-47, 5-6 RT ON C47 REPAIR PERFORMED BY BLEND OUT AND OVERSIZING IAW EA 6-5710-99188 AND RAS/43898/038/2006 ISS. AApr 26, 2007 · N809FD · Airbus A310324SDR 07FDEA01612Structure · misrepairedDEVIATIONS DURING EMBODIMENT OF SB A310-57-2047 REV 2, SEVERAL HOLES WERE FOUND WITH DAMAGES: HOLE 63 RT (MISDRILLED PILOT HOLE), HOLE 35A, 42 RT (TOOLING MARK), HOLE 18LH (TOOLING MARK). REPAIR PERFORMED BY REAM UP THE HOLES IAW EA 6-5710-99209 AND RAS/04423Apr 26, 2007 · N809FD · Airbus A310324SDR 07FDEA01610Skin · corrodedCORROSION ON CENTER WING BOX TOP SKIN TRACK 4-5 LT, C 42-47; TRACK 3-4 LT, C46.1-47; TRACK 2-3 RT, C47; TRACK 4-5, C47; TRACK 4 RT, C40 REPAIR PERFORMED BY BLEND OUT CORROSION AND INSTALLING OVERSIZE FASTENER IN ALL AREA AND IN ADDITION INSTALLING A REPAIR DOUApr 26, 2007 · N809FD · Airbus A310324SDR KCSA071147Spar · corrodedVAPOR SEAL BULGING ON WING CENTER SECTION REAR SPAR WEB ADJACENT TO LOWER SPAR VERT FLANGE AT RBL 104 STA 980.Apr 13, 2007 · N701CK · Boeing 747236BSDR 07FDEA01455Skin · wornELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM OF LT WING SKIN. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW. EA 6-5720-101304 AND RAS/BAE/1002914/2006 ISSUE (A).Apr 12, 2007 · N810FD · Airbus A310SDR KCSA071132Skin · corrodedCENTER WING SECTION UPPER SKIN PANEL CORRODED AT BS 1238, RBL 90.Apr 9, 2007 · N701CK · Boeing 747236BSDR SWAA071752Web · crackedDURING SCHEDULED C2 CHECK, FOUND WING CENTER SECTION WEB CRACKED BS 610, LBL 40.875. REPAIRED WEB PER SWA EA.Apr 6, 2007 · N307SW · Boeing 7373H4SDR 07FDEA00957Frame · crackedDEVIATIONS DURING ACCOMPLISHMENT OF SB A310-57-2035 REV.8 AT INTERNAL ANGLE OF CENTER WING BOX. REPAIR PERFORMED BY OVERSIZING AFFECTED HOLES IAW EA 6-5710-103421 AND RAS/048070/031/2006 ISSUE "A".Mar 16, 2007 · N813FD · Airbus A310324SDR 07FDEA00956Frame · crackedDEVIATIONS DURING ACCOMPLISHMENT OF SB A310-57-2035 REV 8 AT INTERNAL ANGLE OF CENTER WING BOX. REPAIR PERFORMED BY OVERSIZING AFFECTED HOLES IAW EA 6-5710-103421 AND RAS/048070/031/2006 ISSUE "A".Mar 16, 2007 · N813FD · Airbus A310324SDR 07FDEA00810Skin · inoperativeELONGATED HOLES IN PYLON SUPPORT BRACKET AND BOTTOM SKIN, RT WING. REPAIR PERFORMED IAW AI-INSTRUCTION: R571-50532 ISSUE "A" AND EA 6-5720-106407.Mar 14, 2007 · N748FD · Airbus A300B4622RSDR 07FDEA00763Skin · corrodedFOUND UPPER CARGO COMPARTMENT, CENTER WING TANK UPPER SKIN CORRODED AT STA 1229, RBL 75. COMPLIED WITH FEDEX EA 1-5720-109840, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Mar 12, 2007 · N597FE · Doug MD11FSDR 07FDEA00762Skin · corrodedFOUND UPPER CARGO COMPARTMENT, CENTER WING UPPER SKIN CORRODED AT STA 1229, RBL 98. COMPLIED WITH FEDEX EA 1-5720-109840. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6- 2-100.Mar 12, 2007 · N597FE · Doug MD11FSDR UIEA200700115Skin · corrodedFOUND BS 1240 LBL 99 WING CENTER SECTION SKIN CORRODED. CORROSION REMOVED PER SRM 51-10-01. AREA HFEC INSPECTED AND FLAT PEENED. REPAIR DOUBLER WERE FABRICATED AND INSTALLED PER 8100-9.Mar 2, 2007 · N524MC · Boeing 7472D7BSDR UPS07449489Skin · corrodedINSPECTION TYPE:C M/D BS 1210-1220 LBL 97 WING CTR SECTION TOP SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.043 X .5 X 2 INCHES EXCEED SRM LIMIT. M/D BS 1210-1220 LBL 97 WING CTR SECTION TOP SKIN REPAIRED AS PER RS R57-14-35765 AND UPS EO B747-5730-15819.Feb 15, 2007 · N683UP · Boeing 747121SDR UPS07449435Stiffener · corrodedINSPECTION TYPE:C RIGHT WING RIGHT WLG WW CTR SECTION REAR SPAR STIFFENER BS 1241 AT RBL 85 30 INCHES BELOW CEILING FOUND CORRODED. CORROSION BLEND OUT 0.150 X .5 X 5 INCH EXCEED SRM LIMIT. RIGHT WING RIGHT WLG W/W CTR SECTION REAR SPAR STIFFENER AT BS 1241 Feb 12, 2007 · N683UP · Boeing 747121SDR TRAX200700166Angle · crackedRIGHT WING BOX AT FR 28 ANGLE BEHIND FACE PLACED CRACKED. NEW SHEETMETAL BENT INSTALLED IAW SRM 51-25-01 AT FR28 WING BOX. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SR663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01.Feb 1, 2007 · N633AS · Aerosp ATR72SDR 06FDEA04099Frame · unknownUPON DETAILED SPECIAL INSP (SDET) OF CENTER WING BOX LOWER SKIN BETWEEN FRAME 40/41AND 47/48 LT SIDE AT FRAME 44.2 OB MOST FWD HOLE SHOWS POSITIVE INDICATION DUE TO A BUSHING INSTALLED IN THE HOLE COMPLIED WITH EA 6-5710-106250 PT1.Nov 23, 2006 · N449FE · Airbus A310222SDR 06FDEA04043Support · corroded4 AREAS OF CORROSION AROUND FASTENERS ON HORIZONTAL LOWER SURFACE OF STRINGER SUPPORT STRAP AT FS 40 STRG 1 C/W FEDEX EA6-5730-105024.Nov 19, 2006 · N449FE · Airbus A310222SDR 06FDEA04042Support · corroded13 AREAS OF CORROSION AROUND FASTENERS ON HORIZONTAL LOWER SURFACE OF STRINGER SUPPORT STRAP AT FRAME 40 STRINGER 3R C/W FEDEX EA6-5730-105024.Nov 19, 2006 · N449FE · Airbus A310222SDR 06FDEA04040Spar · corroded33 AREAS OF CORROSION AROUND FASTENERS ALONG FS 40 AT CTR WING TANK LOWER SPAR CHORD BETWEEN STRINGER 1 AND 5R (EXTERNAL OF TANK) C/W FEDEX EA6-5730-105024.Nov 19, 2006 · N449FE · Airbus A310SDR IXXA06SMN375SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND WING CENTER SECTION FITTING CRACKED AT STATION 759.000 RBL-24. REMOVED FITTING. CLEANED TREATED AND PRIMED AREA. INSTALLED FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-1-8B, AND DC8 SRM 51-3-1.Nov 17, 2006 · N799AL · Doug DC862FSDR ARWA20061103Fitting · corrodedDURING AN "A" CHECK, THE FOLLOWING WAS FOUND; RT MAIN LANDING GEAR WHEEL WELL STATION 1381; SLANT PANEL PRESSURE BULKHEAD CAP ANGLE/STRUCTURAL FRAME HAS CORROSION ON BOTH INBOARD AND OUTBOARD LOWER CORNERS; WING CENTER SECTION REAR SPAR JOINT WITH RT PANEL, THNov 15, 2006 · N68041 · Doug DC1010SDR ARWA20061102Frame · corrodedDURING AN "A" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LT MAIN LANDING WHEEL WELL AT STATION 1381; SLANT PANEL PRESSURE BULKHEAD SHIMS INSTALLED AROUND CAP ANGLE/STRUCTURAL FRAME ARE DISPLACED DUE TO PRESENT CORROSION AND BROKEN RIVETS; FRAME STRUCTURE INBOANov 15, 2006 · N68041 · Doug DC1010SDR UPS06448141Skin · corrodedINSPECTION TYPE:C M/D WING CTR SECTION UPPER SKIN CORROSION REVEAL AFTER PAINT STRIPPED AT ITEM 8,10,18A,18B,18D AND 19 PER BOEING ATTACHMENT. M/D WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35608 AND R57-14-35609 AND ENGINEERING FILE Sep 4, 2006 · N682UP · Boeing 747121SDR UPS06448166Skin · corrodedBS 1126-1130 LBL103-107 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.074" BY 4" BY 4" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35586 AND UPS ENGINEERING FILE NUMBER 747-57-20114.Aug 17, 2006 · N682UP · Boeing 747121SDR UPS06448165Skin · corrodedINSPECTION TYPE:C M/D BS1140 LBL106-108 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.028" BY 1" BY 3" EXCEED SRM LIMIT. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND 51-10-02 ORIGINAL THICKNESS .0445" BLEND OUT DEPTH 0.028Aug 17, 2006 · N682UP · Boeing 747121SDR UPS06448142Skin · corrodedINSPECTION TYPE:C M/D BS1238-1240 RBL16-19 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.182" BY 2" BY 6" EXCEED SRM LIMIT. BS 1238-1240 RBL16-19 WING CTR SECTION UPPER SURFACE SKIN REPAIRED AS PER RS R57-14-35607 AND UPS EO B747-5730-Aug 17, 2006 · N682UP · Boeing 747121SDR UPS06448140Skin · corrodedINSPECTION TYPE:C M/D BS 1161-1164 LBL101-104 WING CTR SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.043" BY 3" BY 4" EXCEED SRM LIMIT. BS 1161-1164 LBL101-104 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35581 AND UPAug 17, 2006 · N682UP · Boeing 747121SDR UPS06448137Skin · corrodedBS 1050-1054 RBL116-122 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.079" BY 4" BY 6" EXCEED SRM LIMIT. BS 1050-1054 RBL116-122 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35590 AND UPS ENGINEERING FILE NUMBAug 17, 2006 · N682UP · Boeing 747121SDR UPS06448134Skin · corrodedBS 1240 LBL60-66 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.063" BY 2" BY 2" EXCEED SRM LIMIT. BS 1240 LBL60-66 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35592 AND UPS ENGINEERING FILE NUMBER 747-57-2010Aug 17, 2006 · N682UP · Boeing 747121SDR UPS06448133Skin · corrodedBS 1080 LBL93 TO 96 WING CTR SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.073" BY 4" BY 4" EXCEED SRM LIMIT. BS 1080 LBL 93 TO 96 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35579 AND UPS ENGINEERING FILE NUMBER 747Aug 17, 2006 · N682UP · Boeing 747121SDR UPS06448111Skin · corrodedBS 1140-1146 LBL11-14 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.064" BY 4" BY 6" EXCEED SRM LIMIT. BS 1140-1146 LBL11-14 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35593 AND UPS ENGINEERING FILE NUMBER 7Aug 17, 2006 · N682UP · Boeing 747121SDR UPS06448110Skin · corrodedBS 1140-1143 RBL 29-32 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.085" BY 2" BY 5" EXCEED SRM LIMIT. BS 1140-1143 RBL 29-32 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35604 AND UPS ENGINEERING FILE NUMBERAug 17, 2006 · N682UP · Boeing 747121SDR UPS06448109Skin · corrodedBS 1237-1240 LBL68-74 WING CTR SECTION UPPER SKIN CORROSION. CORROSION BLEND OUT 0.045" BY 3" BY 4" EXCEED SRM LIMIT. BS 1237-1240 LBL68-74 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35592 AND UPS ENGINEERING FILE NUMBER 747-57-20108Aug 17, 2006 · N682UP · Boeing 747121SDR UPS06448107Skin · corrodedBS 1186-1214 RBL 54-56 WING CTR SECTION UPPER SKIN CORROSION. CORROSION BLEND OUT 0.034' BY 1.5" BY 10" EXCEED SRM LIMIT. BS 1186-1214 RBL 54-56 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35594 FIG 7 AND UPS ENGINEERING FILE NUMBER 7Aug 17, 2006 · N682UP · Boeing 747121SDR UPS06448106Skin · corrodedBS 1185-1187 LBL31-33 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.056" BY 2" BY 3" EXCEED SRM LIMIT. BS 1185-1187 LBL31-33 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35594 FIG 3 AND UPS ENGINEERING FILE NUMBEAug 17, 2006 · N682UP · Boeing 747121SDR UPS06448104Skin · corrodedBS 1195 LBL71-73 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.037" BY 3" BY 3" EXCEED SRM LIMIT. BS 1195 LBL71-73 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35576 AND UPS ENGINEERING FILE NUMBER 747-57-2009Aug 17, 2006 · N682UP · Boeing 747121SDR UPS06448103Skin · corrodedBS 1193 LBL100 TO 103 WING CTR SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.047" BY 2" BY 3" EXCEED SRM LIMIT. BS 1193 LBL100 TO 103 WING CTR SECTION UPPER SKIN REPAIRED AS PER RS R57-14-35597 AND UPS ENGINEERING FILE NUMBER 747-57-20104.Aug 17, 2006 · N682UP · Boeing 747121SDR UPS06448101Skin · corrodedINSPECTION TYPE:C M/D BS1235-1238 RBL57-59 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.071" BY 2" BY 4" EXCEED SRM LIMIT. M/D BS 1235-1238 RBL57-59 WING CTR SECTION UPPER CORRODED AREA REPAIRED AS PER RS R57-14-35587 AND UPS ENGINEERAug 17, 2006 · N682UP · Boeing 747121SDR UPS06448154Skin · corrodedINSPECTION TYPE:C M/D BS 1182 TO BS 1188 RBL 75 TO 83 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.059" BY 2" BY 6" EXCEED SRM LIMIT. M/D BS 1175 TO 1198 RBL75 WCS UPPER SKIN REPAIRED AS PER RS R57-14-35616 AND UPS ENGINEERING FILE NUAug 16, 2006 · N682UP · Boeing 747121SDR UPS06448152Skin · corrodedINSPECTION TYPE:C M/D BS 1168-1170 LBL31-33 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.054" BY 3" BY 8" EXCEED SRM LIMIT. M/D BS 1168-1170 LBL31-33 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35594 FIG 2 AAug 16, 2006 · N682UP · Boeing 747121SDR UPS06448149Skin · corrodedINSPECTION TYPE:C M/D BS 1118 TO 1120 RBL70 TO 72 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.055" BY 3.5" BY 5" EXCEED SRM LIMIT. M/D BS 1118 TO 1120 RBL 70 TO 72 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-3Aug 16, 2006 · N682UP · Boeing 747121SDR UPS06448147Skin · corrodedINSPECTION TYPE:C M/D BS1156-1160 RBL106-108 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.067" BY 2.5" BY 5" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35602 AND UPS EO B747-5730-25246-A.Aug 16, 2006 · N682UP · Boeing 747121SDR UPS06448144Skin · corrodedBS 1185-1195 RBL87-91 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.041" BY 6" BY 10" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35603 AND UPS ENGINEERING FILE NUMBER 747-57-20115.Aug 16, 2006 · N682UP · Boeing 747121SDR UPS06448138Skin · corrodedINSPECTION TYPE:C M/D BS 1155 RBL 92 TO 96 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.079" BY 4" BY 4" EXCEED SRM LIMIT. M/D BS 1155 RBL 92 TO 96 WING CTR SECTION UPPER SURFACE SKIN REPAIRED AS PER RS 57-14-35602 REFER NRC6353 FOR WAug 16, 2006 · N682UP · Boeing 747121SDR UPS06448131Skin · corrodedINSPECTION TYPE:C M/D BS 1140 TO 1142 RBL106 TO 108 WING CENTER SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.044" BY 2" BY 4" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35594 FIG 6 AND UPS ENGINEERING FILE NUMBER 747-57-20100.Aug 16, 2006 · N682UP · Boeing 747121SDR UPS06448112Skin · corrodedBS 1138 TO 1144 LBL9-11 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.064" BY 2" BY 2" EXCEED SRM LIMIT. BS 118 - 1144 LBL9-11 WING CTR SECTION UPPER SKIN REPAIRED AS PER RS R57-14-35593 AND UPS ENGINEERING FILE NUMBER 747-57-20107.Aug 16, 2006 · N682UP · Boeing 747121SDR UPS06448108Skin · corrodedBS 1208-1212 LBL9-13 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.041" BY 2" BY 10" EXCEED SRM LIMIT. BS 1208-1212 LBL9-13 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35594 FIG 5 AND UPS ENGINEERING FILE NUMAug 16, 2006 · N682UP · Boeing 747121SDR UPS06448132Skin · corrodedINSPECTION TYPE:C M/D BS1140 LBL 55 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.159" BY 3" BY 4" EXCEED SRM LIMIT. BS 1140 LBL 55 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35596 AND UPS ENGINEERING FILE NUAug 15, 2006 · N682UP · Boeing 747121SDR UPS06448102Skin · corrodedBS 1100 LBL85 WING CTR SECTION UPPER SKIN FOUND CORRODED. CORROSION BLEND OUT 0.067" BY 4" BY 5.5" EXCEED SRM LIMIT. BS 1100 LBL85 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35578 AND UPS ENGINEERING FILE NUMBER 747-57-20110.Aug 15, 2006 · N682UP · Boeing 747121
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