Boeing 727-22C

Service difficulty reports · 2,328

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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 = '72722C'
  ORDER BY difficulty_date DESC"

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SDR 96FDEA01497Floor Beam · corrodedFLOOR BEAM AT STA 344 TOP SURFACE CORRODED FROM LBL 55 RBL 15. REMOVED DAMAGED SECTION OF UPPER CHORD, INSTALLED REPAIR CHORD AND ANGLES PER FEDEX SRD NR SR 27-53-007.Aug 27, 1996 · N113FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01496Floor Beam · crackedSTA 680 LBL 48 FLOOR BEAM IS CRACKED AROUND CORRODED FASTENER HOLE. REMOVED CORROSION PER 51-10-6, INSTALLED REPAIR PER SRM 53-10-8.Aug 27, 1996 · N113FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01495Floor Beam · corrodedSTA 680 BL 0 LBL 60 FLOOR BEAM IS HEAVY CORRODED BL 0 TO LBL 50 MEDIUM CORROSION 50 TO 60 LBL. REMOVED CORROSION PER 51-10-6 INSTALLED REPAIR PER SRM 53-10-8 FIG 8.Aug 27, 1996 · N113FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01430Skin · corrodedUPPER SURFACE CENTER WING SECTION, CENTER WING SKIN HAS HEAVY CORROSION AT LT AFT CORNER SECTION UNDER PRESS. SEAL TRACK APPROX 6 INCH AREA, THREE PLACES FS 850 TO 856. CORROSION REMOVED, DIGITAL THICKNESS CHECKED BY NDT, ORIG 184 TAKEN DOWN TO .068. REPAIRAug 21, 1996 · N107FE · Boeing 72722C · Wing, Plate/SkinSDR 96FDEA01428Angle · corrodedFLOOR BOARD SUPPORT ANGLE CORRODED AT STA 344 26 TO 45 LBL FLOOR BEAM. REMOVED CORROSION AND INSTALLED CAP STRIP REPAIR PER SRM 51-10-1.Aug 15, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01431Angle · corrodedCABIN INTERIOR, FS 1176 REINFORCEMENT CHORD ANGLE HAS HEAVY TO SEVERE CORROSION. FLOOR LEVEL BETWEEN BL 44 TO 46 LT. REMOVED DAMAGED PORTION OF CHORD ANGLE, INSTALLED NEW SECTION AND SPLICE DOUBLER PER E/A NR 7531028817.Aug 14, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01429Seat Track · corrodedCORROSION ON O/B OF TRACK STA 840 RBL 48. INSTALLED DOUBLER PER EA 7531028823.Aug 14, 1996 · N107FE · Boeing 72722C · Fuselage, Seat/Cargo Attach FittingsSDR 96FDEA01427Splice Plate · corrodedCORROSION UNDER WING TO FUSE SPLICE PLATE LT SIDE AFT CORNER OF TANK BS 870 LBL 70.5. CUT OUT CORROSION, INSTALLED REPAIR PER EA 7-5710-28845.Aug 14, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01361Doubler · crackedFOUND CRACK AT FWD ENTRY DOOR CUT OUT FRAME UPPER HINGE AREA. INSTALLED DOUBLER AS PER SRM 53-10-4 FIG 2.Aug 13, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01360Flange · corrosionNR0176, MAIN CARGO HAS CORR ON STR 5L STA 1148 TO 1166. REMOVED CORR SRM 51-10-6 OUT OF LIMITS, CUT REPAIR PARTS FOR INSIDE FLANGE REPAIR PER SRM 53-10-3.Aug 13, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA1359Doubler · crackedRT 870 INTERGRAL RIB FWD CRACKED FROM O/B HOLE TO EDGE. THE 2ND CRACK O/B OF O/B HOLE CRACKED FROM EDGE THROUGH RADIUS INTO AFT LWR HOLE OF O/B FLANGE. INSTALLED DOUBLER PER EZ 7-5310-28831.Aug 12, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01353Floor Beam · corrosionMAIN CARGO CORROSION ON FLOOR BEAM AT STA 312 LBL 19. INSTALLED AND COMPLETED FLOOR BEAM REPAIR STA 312 LBL 19 PER SRM 53-10-8.Aug 12, 1996 · N107FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01352Stringer · corrodedFORWARD CARGO BS 720 STR 23R HEAVY CORROSION INSIDE STRINGER ON LOWER LEG. REMOVED CORROSION AND INSTALLED STRINGER REPAIR PER SRM 53-10-3.Aug 12, 1996 · N107FE · Boeing 72722C · Fuselage Main, Longeron/StringerSDR 96FDEA01338Window Post · crackedCRACK AT F/O'S NR 1 WINDOW O/B POST AT UPPER CORNER. CRACK LENGTH VERIFIED BY NDT HFEC, CRACK WAS STOP DRILLED AND VERIFIED BY NDT HFEC REPAIR DOUBLER INSTALLED PER SRM 53-30-3.Aug 7, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01318Stringer · corrosionNR0440, FWD CARGO BS 720 STR 23R HEAVY CORROSION INSIDE STR ON LOWER LEG. *S/D* REMOVED CORROSION AND INSTALLED STRINGER REPAIR PER 53-10-3.Aug 4, 1996 · N107FE · Boeing 72722C · Fuselage Main, Longeron/StringerSDR 96FDEA01317Floor Beam · corrosionNR0436, FWD CARGO BS 600 BL 0 TO RBL 24 HEAVY CORROSION ON LOWER SIDE OF LOWER LEG OF MAIN CARGO FLOOR BEAM. *S/D* INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8.Aug 2, 1996 · N107FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01314Fitting · crackedSTR END FITTING CRACKED STA 740 STR 5R. REMOVED AND REPLACED STR END FITTING PER 51-10-01.Aug 2, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS96220754Rib · crackedINSPECTION TYPE-C, A PREVIOUS REPAIR WAS DISCOVERED TO THE RBL 70.5 RIB CHORD AT 135 760. HOWEVER, A CRACK HAD PROGRESSED SINCE THE ORIGINAL REPAIR INSTALLATION. REPAIR PER CARRIED OUT PER SB727-53-0112 (UPS EO 7275710-1271) WITH DEVIATIONS OUTLINED IN SRS EJul 31, 1996 · N941UP · Boeing 72722C · Wing, Rib/BulkheadSDR 96FDEA01322Skate Angle · corrosionNR0875 AND 0949, STA 294 TO 312 LT SIDE OF DOGHOUSE NOSE W/W BELOW FLOOR PANEL HAS CORROSION ON SKATE ANGLE LWR I/B SECTION OF TORQUE BOX NR0875. LT SKATE ANGLE AT STA 294.5 TO 298 HEAVY CORROSION ON VERTICAL SIDE OF SKATE ANGLE NR0949.Jul 31, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01321Skate Angle · corrosionNR0867 AND 0868, STA 294 RT SIDE OF DOGHOUSE BELOW FLOOR PANEL CORROSION IN LWR FWD CORNER BELOW NUT AND BEHIND SEALANT - NR0867 STA 294 R/H SIDE OF DOGHOUSE, BELOW FLOOR PANEL CORROSION ON ANGLE THAT ATTACHS TO DOGHOUSE LWR FWD AREA SKATE ANGLE NR0868. *Jul 31, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01320Splice Bolts · corrodedNR0879 STA 360 STR 26 LT AND RT SEVERAL SPLICE BOLTS ARE HEAVILY CORRODED AND NUTS FOR THE BOLTS ALSO CORRODED.Jul 31, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01319Spar Web · corrodedCTR FUEL TANK BAY 3, AFT SPAR WEB AT STA 870 BULGED, CRACKED AND CORRODED WITH POPPED RIVETS AT APPROX LBL 40 NEAR UPPER CHORD ANGLE. UPPER CHORD ANGLE HAS POPPED RIVETS IN THIS AREA ALSO.Jul 31, 1996 · N107FE · Boeing 72722C · Wing SparSDR UPS96220759Body Joint · corrodedINSPECTION TYPE-C, BOLTS IN PRODUCTION JOINT AT BS 360 FOUND CORRODED DURING STRUCTURAL SAMPLE BELOW STR 21L AND 21R. BOLTS REPLACED AS REQUIRED BETWEEN STR 21L AND 21R AT BS 360 AND TORQUED IAW MM 553-11-00 PG 601, CRACK IN HOLE AT BS 360 O/B OF STR 28R REPAJul 28, 1996 · N941UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS96220757Vert Stringer · crackedINSPECTION TYPE-C, VERT STRINGER FOUND CRACKED AT STR 13 TO 14 AT WS 686.5 LT. REPAIRED PER UPS EO B727-5710-0314-F.Jul 28, 1996 · N941UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS96220752Ribs · crackedINSPECTION TYPE-C, TWO HYDROPRESSED RIBS WERE FOUND CRACKED. CRACKED RIBS REPLACED WITH BUILT-UP RIBS, PER ABOVE EO O/S FASTENERS INSTALLED PER SRS EO 96-30-012.Jul 25, 1996 · N941UP · Boeing 72722C · Wing, Rib/BulkheadSDR RAAA96B2033Battery Pack · dischargedROW 7 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE.Jul 19, 1996 · N832RV · Boeing 72722C · Emergency LightingSDR RAAA96B2032Battery Pack · dischargedRIGHT SERVICE DOOR EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE.Jul 19, 1996 · N832RV · Boeing 72722C · Emergency LightingSDR UPS96220750Skin · corrodedINSPECTION TYPE-C, CORROSION AND DISBOND ON FUSELAGE SKIN AND DOUBLER BS 1183 TO 1080 BETWEEN S20R AND 26R. SKIN PANEL DERIVETED IAW SRM 51-30-02. SKIN PANEL AND DOUBLER INSPECTED USING LFEC IAW B727 NDT MANUAL, PART 6 51-00-00 FIG 5, MATERIAL LOSS OF 10 TO Jul 17, 1996 · N941UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS96220755Clamp Rings · corrodedINSPECTION TYPE-C, FRETTING SURFACE CORROION ON LT AND RT WING FUEL TANK DOOR CLAMP RINGS. FUEL TANK DOOR CLAMP RINGS REPLACED IAW MM 28-11.Jul 11, 1996 · N941UP · Boeing 72722C · Wing Miscellaneous StructureSDR UPS96220761Stringer · corrodedINSPECTION TYPE-D, STR 21R BS 460 TO 480. REPAIRED PER SRM 53-10-3.Jul 6, 1996 · N941UP · Boeing 72722C · Fuselage Main, Longeron/StringerSDR UPS96220758Doubler · crackedINSPECTION TYPE-C, FWD ENTRY DOOR CUTOUT HAS DOUBLER CRACK AT TOP FWD CORNER. REPAIR CARRIED OUT IAW EO B727-5330-1460 APPENDIX OPTION 1.Jul 6, 1996 · N941UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS96220746Frame · corrodedINSPECTION TYPE-C, CORROSION ON FRAME BS 600 ADJACENT TO STR 26L. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-01. FRAME REPAIRED IAW SRM 53-10-4 FIG 1.Jul 5, 1996 · N941UP · Boeing 72722C · Fuselage Main, FrameSDR UPS96220762Shear Tie · corrodedINSPECTION TYPE-D, SHEAR TIE CORRODED AND CRACKED ON ST 22L AT BS 328 LT SIDE. SHEAR TIE REPLACED SRM 53-10-2.Jul 4, 1996 · N941UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS96220756Skin · corrodedINSPECTION TYPE-C, LT O/B AILERON HAS SKIN BULGE ON TOP SKIN I/B END. RIVETS REMOVED FROM AILERON SKIN I/B END IAW SRM 51-30-2, AILERON HINGE ASSM FOUND CORRODED. REPLACED HINGE ASSM IAW DWG 65-2176 AILERON RIGGED IAW 27-10-00.Jul 4, 1996 · N941UP · Boeing 72722C · AileronsSDR UPS96220748Web · crackedINSPECTION TYPE-C, CRACK IN NOSE WHEEL WELL WEB, BS 292 RBL 30 WL 180 APPROX. HFEC CARRIED OUT TO CONFIRM CONTAINMENT OF CRACK BY STOPDRILL IAW B727 NDT MANUAL PART 6, 51-00-00 FIG 4, NO DEFECTS FOUND. REPAIR TO WEB IN NOSE WHEEL WELL CARRIED OUT IAW SRS EO Jul 4, 1996 · N941UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS96220753Skin · delaminationINSPECTION TYPE-C, DELAMINATION AT BS 1090 TO 1110 BETWEEN STR 11 AND 12 RT SIDE. FOKKER BOND INSP CARRIED OUT ON TWO SUSPECT AREAS OF METAL TO METAL DISBOND IAW B727 NDT MANUAL PART 4 51-40-00 FIG 1. BOTH AREAS INDICATE DISBONDING SKIN PANEL AND DOUBLER INSJul 3, 1996 · N941UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS96220751Skin · corrodedINSPECTION TYPE-C, CORROSION ON FUSELAGE SKIN BS 1085 BETWEEN STR 12L AND BL AREA PAINT STRIPPED IAW MM 51-20-1, AREA REINSPECTED FOUND TO BE CORRODED AND DAMAGED. SKIN AT BS 1080 TO 1160 BETWEEN S10L & S14L DERIVETED IAW SRM 51-30-2, SKIN PANEL REPAIRED IAW Jul 3, 1996 · N941UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS96220749Skin · corrodedINSPECTION TYPE-C, CORROSION BETWEEN FUSELAGE SKIN AND S17L, BS 1183. REMOVED SKIN PANEL, REPAIRED IAW SRS EO 96-30-015.Jul 3, 1996 · N941UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS96220747Skin · corrodedINSPECTION TYPE-C, CORROSION BETWEEN FUSELAGE SKIN AND FRAME AT BS 1183 BETWEEN 58L AND 59L. AREA PAINT STRIPPED IAW MM 51-20-1, FASTENERS REMOVED IAW SRM 51-30- 2, AREA BETWEEN BS 1183 AND 1166 BETWEEN 510L AND 58L INSPECTED IAW B7 27 NDT MANUAL 51-00-00 FIGJul 3, 1996 · N941UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS96220745Bottle Pin · corrodedINSPECTION TYPE-C, SLIGHT SURFACE CORROSION ON INNER SURFACE OF LT REAR BOTTLE PIN. NEW BOTTLE PIN INSTALLED IAW MM 57-41-01.Jul 3, 1996 · N941UP · Boeing 72722C · Wing, Fuselage Attach FittingsSDR RAAAB296031Battery Pack · dischargedRIGHT AFT OVERWING EXIT EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X)Jul 1, 1996 · N832RV · Boeing 72722C · Emergency LightingSDR UPS96220572Frame · crackedINSPECTION TYPE SI, RT 870 FORGING SPLICE AT STR 9 HAS 5 CRACKED HOLES AND ONE 2 TO 3 INCH CRACK IN RADIUS OF AFT FLANGE. REPAIRED BS 870 FORGING BY REMOVING DAMAGED SECTION AND SPLICING A NEW SECTION IN PLACE IAW B727-5310-3057 AND B727-5310-8080A.Jun 29, 1996 · N929UP · Boeing 72722C · Fuselage Main, FrameSDR UPS96220571Frame · crackedINSPECTION TYPE SI, LT 870 FORGING STR 9 HAS ONE CRACKED HOLE AND CRACK IN RADIUS ON FWD FLANGE. INSTALLED EXTERNAL DOUBLERS AND REPAIRED IAW EO B727-5310-3057E AND EO B727-5310-8080A.Jun 29, 1996 · N929UP · Boeing 72722C · Fuselage Main, FrameSDR UPS96220576Floor · corrodedINSPECTION TYPE SI, CORROSION ON FLOOR STA 209 TO 231 LBL 6 TO 18 WL 208. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED FLOOR PANEL PER SRM 51-40-2, 51-10-2 MM 51-20-151, SRM 51-30-02.Jun 28, 1996 · N929UP · Boeing 72722C · Fuselage Floor PanelSDR UPS96220575Floor Beam · corrodedINSPECTION TYPE SI, CORROSION ON FLOOR BEAM BOTTOM SIDE OF UPPER FLANGE AT NUTCLIP HOLES STA 680 WL 207.5 LBL 5, 29, 33, 35 RBL 4, 37, 59, 60, AREAS MARKED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, REPAIRED PER EO 96-2363.Jun 28, 1996 · N929UP · Boeing 72722C · Fuselage Main, Floor BeamSDR UPS96220574Floor Beam · corrodedINSPECTION TYPE SI, DOUBLE HOLES IN LOWER FLANGE OF THE 1110 FLOOR BEAM LBL 19 RBL 45 WL 201. DURING REMOVAL OF CEILING SUPPORT FOUND FLOOR BEAM TO BE CORRODED OUT OF LIMITS PER SRM 53-10-01. REPAIRED PER EO 96-2357.Jun 28, 1996 · N929UP · Boeing 72722C · Fuselage Main, Floor BeamSDR UPS96220573Floor Beam · corrodedINSPECTION TYPE SI, CORROSION AT NUTPLATES IN FLOOR BEAM BOTTOM SIDE OF UPPER FLANGE STA 640 WL 207.5 LBL 38 AREAS MARKED. FOUND FLOOR BEAM AT BS 640 LBL 38 TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FLOOR BEAM AT BS 640 LBL 38 PER UPS EO 727-53-1780.Jun 28, 1996 · N929UP · Boeing 72722C · Fuselage Main, Floor BeamSDR RAAAB196011Skin · crackedDURING SCHEDULED S1 INSPECTION PER CARD S1-11101, FOUND 2 ADJACENT CRACKS EMANATING FROM HI-LOCK FASTENERS IN NOSE W/W UPPER SKIN BS 259.5, LBL 21 AND 22. REPAIRED PER SRM 53-10-9. (M)Jun 28, 1996 · N831RV · Boeing 72722C · Fuselage Main, Plate/SkinSDR RAAAB196010Skin · crackedDURING SCHEDULED S1 INSPECTION PER CARD S1-11101, FOUND 2 ADJACENT CRACKS EMANATING FROM HI-LOCK FASTENERS IN NOSE W/W UPPER SKIN BS 259.5, RBL 21 AND 22. REPAIRED PER SRM 53-10-9. (M)Jun 28, 1996 · N831RV · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS96220535Frame · corrodedINSPECTION TYPE SI, FOUND CORROSION ON FRAME AT BS 304 WL 175 LBL 44. CLEANED AND REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER EO 96-2371.Jun 27, 1996 · N929UP · Boeing 72722C · Fuselage Main, Frame
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