Boeing 747-121

Service difficulty reports · 3,030

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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 aircraft_model_key = '747121'
  ORDER BY difficulty_date DESC"

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SDR UPS06447921Fitting · corrodedM/D BS860 LBL55 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.026" BY 1/2" BY 3" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447920Fitting · corrodedM/D BS 978 RBL28 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.027" BY 0.5" BY 2" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447919Fitting · corrodedM/D BS980 RBL83 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.021" BY 1" BY 2" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447916Fitting · corrodedM/D BS 802 LBL27 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.043" BY 1" BY 3" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447915Fitting · corrodedM/D BS 900 LBL55 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.039" BY 1/2" BY 2" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447913Seat Track · corrodedM/D BS 759 LBL75 SEAT TRACK LT FLANGE CORROSION. CORROSION BLEND OUT 0.021" BY 1/2" BY 1" EXCEED SRM LIMIT. M/D BS 750 TO BS 830 LBL 75 TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447906Skin · crackedINSPECTION TYPE-C, AFT CARGO DOOR CUTOUT FWD DR HINGE 2EA HOLES CRACK AT FUSELAGE SKIN CRACK LENGTH : .0625 INCH AND 0.040 INCH. AFT CARGO DOOR CUTOUT FWD DOOR HINGE AREA. DOUBLERS REMOVED AND INSTALLED IAW SRM 51-30-02 FROM CRACKED SHIM REPLACED ONLY IAW SRMAug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS06447902Seat Track · corrodedINSPECTION TYPE-C M/D BS 896 LBL 33 SEAT TRACK RT FLANGE CORROSION. CORROSION BLEND OUT 0.022 INCH X .5 INCH X 2 INCH EXCEED SRM LIMIT. M/D BS890 TO BS1000 LBL33 TRACK REPAIRED IAW SRM 53-10-05 FIG 1A.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447888Channel · corrodedINSPECTION TYPE-C M/D BS787 LBL11-RBL11 HAT SECTION AFT FLANGE CORROSION. CORROSION BLEND OUT 0.022 INCH X .8750 X 3 INCH EXCEED SRM LIMIT. HAT SECTION REPLACED IAW SRM 51-10-01 PG9. P/N:BAC1510-335-7075T6511.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06447852Skin · crackedINSPECTION TYPE:C EMP - BS2656 FUSELAGE EXTERNAL SKIN SURFACE FOUND DENT MARK AT STR3L-5L, CRACK LENGTH 3/16". SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS06447845Stringer · damagedINSPECTION TYPE:C M/D BS 434 TO BS 440 RT S27AR TO S28AR FASTENER HOLES FOUND OVAL. BS 434 TO BS 440 STR 27AR AND STR 28AR STRINGER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR 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 747121 · Wing, Center BoxSDR 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 747121 · Wing, Center BoxSDR UPS06448150Skin · corrodedBS 1138 TO 1142 RBL 85-98 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.128" BY 3.5" BY 6" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35617 AND UPS EO B747-5710-25225-A.Aug 16, 2006 · N682UP · Boeing 747121 · Wing, Plate/SkinSDR 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 747121 · Wing, Center BoxSDR UPS06448148Floor Support · corrodedBS 1220-1260 LBL55 FLOOR SUPPORT UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.087" BY 1.5" BY 10" EXCEED SRM LIMIT. M/D BS 1220-1260 LBL55 FLOOR SUPPORT REPAIRED AS PER RS R53-45-35575 AND UPS ENGINEERING FILE NUMBER 747-53-20335.Aug 16, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR 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 747121 · Wing, Center BoxSDR 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 747121 · Wing, Center BoxSDR 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 747121 · Wing, Center BoxSDR 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 747121 · Wing, Center BoxSDR 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 747121 · Wing, Center BoxSDR 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 747121 · Wing, Center BoxSDR UPS06448055Floorbeam · corrodedBS 1020 LBL 25 FLOORBEAM UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.041" BY 2" BY 2". FLOORBEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 REFER NRC 6539 FOR WORKING DETAIL.Aug 16, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06448053Floorbeam · corrodedBS 1220 LBL 83-95 FLOORBEAM UPPER TEE UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.046" BY 1.5" BY 10". BS 1220 LBL 75-95 FLOORBEAM UPPER TEE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 16, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06447989Web · crackedINSPECTION TYPE-C M/D BS1154-1160 RBL11 SEAT TRACK SUPPORT WEB LWR AREA CRACK. CRACK LENGTH 3.7500. M/D BS1140-1200 RBL11 SEAT TRACK SUPPORT WEB REPLACED AND INSTALLED IAW SRM 51-10-01 PG9 AND 51-30-02.Aug 16, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06447938Support · corrodedINSPECTION TYPE:C FX AIR CONDITIONING BAY FAIRING SUPPORT FLOATING NUT AT SURFACE FOUND SURFACE CORROSION AT STA 1045 RBL 10 TO RBL 57. CORROSION BLEND OUT 0.029" BY 1/2" BY 20" EXCEED SRM LIMIT. FX BS 1045 BL0 - RBL57 FAIRING SUPPORT REPAIRED AS PER SRM 51-Aug 16, 2006 · N682UP · Boeing 747121 · Aerodynamic FairingsSDR UPS06447926Support · corrodedINSPECTION TYPE:C FX FRONT BODY FAIRING SUPPORT LOWER SURFACE CORROSION AT STA983 LBL20 TO RBL10. CORROSION BLEND OUT 0.025" X 1/2" X 10" EXCEED SRM LIMIT. FX BS983 LBL22 TO RBL33 BODY FAIRING SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.Aug 16, 2006 · N682UP · Boeing 747121 · Aerodynamic FairingsSDR UPS06447917Fitting · corrodedM/D BS 682 LBL15 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.017" BY 1.5" BY 3" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.Aug 16, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447914Support · corrodedFX AIR CONDITIONING BAY FAIRING SUPPORT FLOATING NUT AT SURFACE FOUND CORROSION AT STA 1013 TO 1017 O/B SIDE. CORROSION BLEND OUT 0.050" BY 1/2" BY 8" EXCEED SRM LIMIT. FX BS1005-1018 RBL75 FAIRING SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.Aug 16, 2006 · N682UP · Boeing 747121 · Aerodynamic FairingsSDR UPS06447884Seat Track · corrodedINSPECTION TYPE-C M/D BS990-1000 LBL33 SEAT TRACK IB FLANGE FOUND COR. CORROSION BLEND OUT 0.020 INCH X .5 INCH X 1 INCH EXCEED SRM LIMIT. M/D BS890-1000 LBL33 TRACK REPAIRED IAW SRM 53-10-05 FIG 1A REFER NRC 6587 FOR WORKING DETAIL.Aug 16, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447883Seat Track · corrodedINSPECTION TYPE-C M/D BS980-1000 LBL33 SEAT TRACK OB FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.033 INCH X .8750 INCH X 2 INCH EXCEED SRM LIMIT. M/D BS890 TO 1000 LBL33 TRACK REPAIRED IAW SRM 53-10-05 FIG 1A REFER NRC 6587 FOR WORKING DETAIL.Aug 16, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447838Pressure Panel · crackedINSPECTION TYPE:C NWW RT SIDEWALL PANEL BETWEEN BS 300-320 2 LOCATIONS CRACK FOUND ON WEB. CRACK ON BS305 APPROX 3/8" AND ON BS 313 APPROX 1/2" IN LENGTH. NWW RT SIDEWALL PANEL BETWEEN BS300-320 WL160 AREA REPAIRED AS PER SRM 53-10-04 FIG 116. REPEAT INSPECAug 16, 2006 · N682UP · Boeing 747121 · Fuselage Main, BulkheadSDR UPS06448084Seat Track · crackedBS 520 RBL8 SEAT TRACK CRACK, CRACK LENGTH 4" AND 0.75" RESP. BS 520 RBL98 SEAT TRACK REPAIRED AS PER RS R53-25-35572 AND UPS ENGINEERING FILE NUMBER 747-53-20330.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448139Frame · crackedINSPECTION TYPE:C U/D LT BS 340 UPPER DECK FLOORBEAM UPPER TEE AND FRAME ATTACHMENT AREA 1 FASTENER HOLE FOUND CRACK AT FRAME WEB, CRACK LENGTH 0.060". U/D LT BS 340 UPPER DECK FLOORBEAM UPPER TEE ATTACHED FRAME REPAIRED AS PER RS R53-12-35567. CONTINUED INSAug 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, FrameSDR UPS06448136Floorbeam · crackedINSPECTION TYPE:C U/D LT BS340 UPPER DECK FLOORBEAM UPPER TEE AND FRAME ATTACHMENT AREA 1 FASTENER HOLE FOUND CRACK AT STRAP, CRACK LENGTH 0.060". LT BS 340 FLOORBEAM UPPER TEE CRACKED STRAP REPLACED AS PER RS R53-12-35567. REPEAT INSPECTION IS REQUIRED AS PAug 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR 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 747121 · Wing, Center BoxSDR UPS06448129Floorbeam · crackedINSPECTION TYPE:C U/D RT BS 340 UPPER DECK FLOORBEAM UPPER TEE AND FRAME ATTACHMENT AREA 2 FASTENER HOLE FOUND CRACK AT FRAME WEB, CRACK LENGTH .060". U/D RT BS 340 UPPER DECK FLOORBEAM UPPER TEE ATTACHED FRAME REPAIRED AS PER RS R53-12-35567. CONTINUE INSPEAug 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06448128Floorbeam · damagedINSPECTION TYPE:C U/D RT BS 340 UPPER DECK FLOORBEAM UPPER TEE AND FRAME ATTACHMENT AREA 1 FASTENER HOLE FOUND TEE AT FRAME SPLICE. U/D RT BS 340 FLOORBEAM TEE ATTACHED FRAME SPLICE AT STR 13A AREA REPLACED AS PER RS R53-12-35567. CONTINUED INSPECTION IS REQAug 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06448123Skin · crackedINSPECTION TYPE:C FWD CARGO DOOR CUTOUT FWD DOOR HINGE 1 HOLE CRACK AT FUSELAGE SKIN RUNNING UP APPROX 0.030". SKIN REPAIRED AS PER RS R53-21-35571. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-21-35571 AND UPS B747-5320-25077-A.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS06448118Door Frame · crackedINSPECTION TYPE:C FWD CARGO DOOR CUTOUT AFT DOOR HINGE FOUND 1 FASTENER HOLE CRACKED AT FRAME AT 4 O`CLOCK POSITION APPROX 0.030 LONG. REPAIRED AS PER RS R53-25-35580 AND UPS EO B747-5330-25123-AAug 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR 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 · Wing, Center BoxSDR UPS06448039Floorbeam · damagedRT BS 360 UPPER DECK FLOORBEAM UPPER SECTION VERTICAL FLANGE AREA 3EA FASTENER HOLES FOUND OVAL AT STRAP AS MARKED. U/D RT BS 360 UPPER DECK FLOORBEAM UPPER SECTION VERTICAL FLANGE ATTACHED STRAP REPLACED AS PER RS R53-15-35573. REPEAT INSPECTION IS REQUIREDAug 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06447975Floorbeam · crackedBS 980 LBL55 FLOORBEAM UPPER TEE FOUND CRACKED, CRACK LENGTH 3/8". BS 980 LBL20 TO LBL70 FLOORBEAM UPPER CHORD REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06447880Seat Track · crackedBS 641 RBL 75 SEAT TRACK CRACK, CRACK LENGTH 3/8". BS 640 TO BS 670 RBL75 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447879Seat Track · crackedBS 520 RBL90 SEAT TRACK CRACK, CRACK LENGTH 1/2". BS 480 TO BS 530 RBL90 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447878Seat Track · crackedBS 636-640 RBL75 SEAT TRACK CRACK, CRACK LENGTH 7/16". BS 610 TO BS 640 RBL75 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447927Fitting · corrodedBS 521 RBL14-20 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.022" BY 1/2" BY 3" EXCEED SRM LIMIT. TIE DOWN FTG ATTACH PLATE REPLACED AS PER SRM 51-10-01 PG 9.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447925Splice Plate · crackedNWW LT AFT CORNER BS 400 S44L INTERNAL SPLICE PLATE FOUND CRACK FROM FWD EDGE AND RUNNING AFT UNDERNEATH BH CHORD, CRACK LENGTH 3/4". NWW LT AFT CORNER BS400 STR 44L INTERNAL SPLICE PLATE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06447924Splice Plate · crackedNWW RT AFT CORNER BS 400 S44R INTERNAL SPLICE PLATE FOUND CRACK FROM FWD EDGE AND RUNNING AFT AND RUNNING O/B UNDERNEATH BH CHORD, CRACK LENGTH 1/2". NWW RT AFT CORNER BS400 STR 44R INTERNAL SPLICE PLATE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06447918Fitting · corrodedM/D BS 681 RBL15 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.042" BY 1.5" BY 2" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach Fittings
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