Boeing 727-227

Service difficulty reports · 5,082

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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 aircraft_model_key = '727227'
  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 C8GA20090260Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STR 27R STA 710 IS CORRODED. REMOVED DAMAGED SECTION OF STR AND FABRICATED NEW FROM BAC1498-144 7075 T6 DIM 20.5". INSTALLED STR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR C8GA200900259Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STA 560-570, STR 27L IS CORRODED. FLOORBEAM SPLICE PLATE IS CRACKED. REMOVED DAMAGED SECTION OF STR DIM 18.25" FABRICATED NEW STR FROM BAC1498-147 DIM 18.25" .090". FABRICATED 2 SPLICES 13.25" X 10" BAC 1Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR C8GA200900258Floorbeam · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STA 660, STR 17L FLOORBEAM SPLICE PLATE IS CRACKED. REMOVED CRACKED SPLICE PLATE AND FABRICATED NEW FROM 2024 T3 .125" DIM 18" X 9". INSTALLED SPLICE PLATE, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TOJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Floor BeamSDR C8GA200900257Floorbeam · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STA 680, STR 17L FLOORBEAM IS CRACKED. REMOVED DAMAGED SECTION . HFEC FORT CONTAINMENT, FABRICATED FILLER FROM 7075 T6 .090" DIM 5.5" X 7.2 AND REINSTALL SPLICE PLATE. NO OTHER DEFECTS WERE NOTED. ACFT WASJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Floor BeamSDR C8GA200900256Failsafe · gougedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE FAIL SAFE IS GOUGED AT STA 540, STR 25L. FABRICATED NEW FAIL SAFE CHORD FROM BAC 1490-2763 .090" DIM 8.75" X 1.75". INSTALLED CHORD, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, StructureSDR C8GA20090255Web · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE WEB IS CRACKED AT STA 500, STR 27L. REMOVED AND REPLACE WEB, FABRICATED FROM 7075 T6 .050" DIM 5.875" X 4. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Miscellaneous StructureSDR C8GA20090254Stringer · misrepairedWHILE IN HEAVY MX PERFORMING INSP STR SPLICE WAS FOUND TO BE NO-COMPLIANT AT BS 950E +5 - 969 STR 28R. REMOVED REPAIR AND FABRICATED NEW STR FROM 65-58387-2 DIM 60" FABRICATED SPLICE, INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR C8GA20090253Skin · damagedWHILE IN HEAVY MX PERFORMING DENT AND REPAIR MAPPING EXISTING EXTERNAL FUSELAGE REPAIR AT BS 1180 BETWEEN STR 19L- 20L IS NON COMPLIANT. REMOVED REPAIR AND FABRICATED NEW DOUBLER FROM 2024 T3 .063" DIM 6" X 9". INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Plate/SkinSDR C8GA20090252Skin · damagedWHILE IN HEAVY MX PERFORMING DENT AND REPAIR MAPPING EXISTING EXTERNAL FUSELAGE REPAIR AT BS 1151 BETWEEN STR 18L- 20L IS NON COMPLIANT. REMOVED REPAIR AND FABRICATED NEW DOUBLER FROM 2024 T3 .063" DIM 13" X 13.5". INSTALLED REPAIR, NO OTHER DEFECTS NOTED. Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Plate/SkinSDR C8GA20090251Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STA 740 STR 24R HAS CORROSION. REMOVED DAMAGED SECTION DIM 11", FABRICATED NEW STR FROM BAC 1498-142 DIM 11" AND SPLICE REPAIR FROM BAC 1498-132 DIM 13.6". INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. ACJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR C8GA20090250Skin · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE FWD CARGO, STA 680 STR 26R HAS CORROSION. REMOVED DAMAGED SECTION DIM 3.0625 X 2.625" FABRICATED DOUBLER FROM 2024 T3 .080" DIM 9.125" X 9.625" FILLER FROM 2024 T3 .071" DIM 10.4375" X 7 & 2024 T3 .063" Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Plate/SkinSDR C8GA20090249Rib · bentWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE FWD CARGO, MOD RIB AT FWD OF STATION 640 IS BENT ON STR 25L. REMOVED DAMAGED SECTION AND FABRICATED ANGLE FROM 2024 T4. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Miscellaneous StructureSDR C8GA20090248Frame · bentWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE FWD CARGO, TOP OF FRAME 500 IS BENT BETWEEN STR 25L AND 24L. REMOVED DAMAGED SECTION DIM 1.250" X 1" FABRICATED REPAIR SPLICE FROM AE 727-1-041-11 DIM 9.6". INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTEDJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, FrameSDR C8GA20090247Spar · defectiveREMOVED AND REPLACED LT ELEVATOR REAR SPAR AND SUPPORT FITTINGS TO COMPLY WITH SB 727-55-0089 NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Jul 31, 2009 · N89427 · Boeing 727227 · Elevator, Spar/RibSDR C8GA20090246Floorbeam · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE FLOOR BEAM CAP TRIM AT BS 700 STR 17L IS CRACKED. REMOVED CRACK, HFEC FOR CONTAINMENT AND FABRICATED ANGLES FRO 7075-0 .100" HEAT TREATED TO T6, DIM 10.750" X 2.250" 2 EA. INSTALLED ANGLES, NO OTHER DEFJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Floor BeamSDR C8GA20090245Web · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE NR 3 ENGINE NOSE COWL INTERIOR WEB IS CRACKED AT THE 7 O'CLOCK POSITION. REMOVED WEB AND FABRICATED NEW FROM 2024 T3 .032" DIM 13" X 36". INSTALLED WEB, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TJul 31, 2009 · N89427 · Boeing 727227 · Engine Air Intake SystemSDR C8GA20090244Rub Strip · delaminatedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE RT OTBD FOREFLAP RUB STRIP IS DISBONDED OTBD OF INBD TRACK. REMOVED DAMAGE DIM 21" X 4" FABRICATED FILLER FROM 2024 T3 .016" DOUBLER 2024 T3 .016" DIM 24" X 5.5" INSTALLED HOT BOND REPAIR, NO OTHER DEFJul 31, 2009 · N89427 · Boeing 727227 · Trailing Edge FlapsSDR C8GA20090243Rub Strip · delaminatedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT OTBD FOREFLAP RUB STRIP IS DISBONDED. REMOVED DAMAGE FROM T/E DIM 13.5" X 5" FABRICATED FILLER FROM 2024 T3 .016" DIM 16.5" X 6.5" INSTALLED HOT BOND REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETJul 31, 2009 · N89427 · Boeing 727227 · Trailing Edge FlapsSDR C8GA20090242Skin · delaminatedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT INBD AFT FLAP T/E DELAMINATED. REMOVED DELAMINATION DIM 3" X 7" FABRICATED DOUBLER FROM 2024 T3 .020" DIM 4.5" X 10. INSTALLED HOT BOND REPAIR. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVIJul 31, 2009 · N89427 · Boeing 727227 · Trailing Edge FlapsSDR C8GA20090241Doubler · gougedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT INBD FOREFLAP OTBD L/E REPAIR IS GOUGED. REMOVED PREVIOUS REPAIR, FABRICATED DOUBLER FROM2024 T3 .063" DIM 14" X 4.875" FILLER 2024 T3 .050" DIM 14" X 4.5". NO OTHER DEFECTS WERE NOTED. ACFT WAS RETJul 31, 2009 · N89427 · Boeing 727227 · Trailing Edge FlapsSDR C8GA20090240Hinge · crackedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE MAIN CARGO DOOR HINGE HAS 7 HINGE LOBES CRACKED AT BS 620. REMOVED AND REPLACED HINGE SEGMENTS. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Jul 31, 2009 · N89427 · Boeing 727227 · Cargo/Baggage DoorsSDR C8GA20090239Skin · bulgedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE FUSELAGE SKIN HAS A BULGE AT BS 1118 ALONG STR 27L. REMOVED DAMAGED AREA DIM 4.9" X 1.250" FABRICATED DOUBLER FROM 2024 T3 .063" DIM 14.375" X 7.375" FILLER FROM 2024 T3 .050" DIM 4.9" X 1.250". INSTALLJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Plate/SkinSDR C8GA20090238Skin · dentedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE FUSELAGE SKIN IS DENTED AT BS 1043 BETWEEN STR 21L-22L. REMOVED DAMAGE DIM .750" FABRICATED DOUBLER FROM 2024 T 3 .063" DIM 4.5" AND FILLER FROM SAME DIM .750". INSTALLED REPAIR, NO OTHER DEFECTS WERE NJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Plate/SkinSDR C8GA20090237Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE FUSELAGE SKIN HAS A BULGE FWD AT BS 1183 BETWEEN STR 29R-28R. CUT OUT DAMAGED STR DIM 8.75 FABRICATED NEW STR FROM BAC 1498-147 7075 T62 DIM 8.875", SPLICE FROM BAC 1498-131 7075 T62 DIM 10.0625". INSTAJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR C8GA20090236Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE FUSELAGE SKIN HAS A BULGE BETWEEN 470-480 STR 28L. REMOVED STR SECTION FROM BS 450-480. FABRICATED STR FROM BAC 1498-138 7075 T6 DIM 28.750". INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR C8GA20090235Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE FUSELAGE SKIN JUST AFT OF EXISTING REPAIR LOCATED AT BS 680 STR 28R HAS A BULGE. REMOVED EXISTING STR SPLICE CUT OUT CORROSION DIM 3" AT BS 670 STR 28R. FABRICATED REPAIR SPLICE FROM 7075-0 DIM 12" X 4Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR C8GA20090233Skin · delaminatedWHILE IN HEAVY CHECK PERFORMING INSP IT WAS NOTED THAT THE RT INBD MID FLAP T/E HAS DELAMINATION. REMOVED DAMAGED SKIN DIM 5" X 4". FABRICATED FILLER FROM 2024 T3 .016" AND DOUBLER FROM 2024 T3 .020 DIM 8" X 4". INSTALLED HOT BOND REPAIR, NO OTHER DEFECTS WEJul 31, 2009 · N89427 · Boeing 727227 · Trailing Edge FlapsSDR C8GA20090232Skin · crackedWHILE IN HEAVY MX PERFORMING INSPECTIONS IT WAS NOTED THAT THE NR 3 SLAT INBD TRACK L/E CRACKED. STOP DRILLED CRACK, PERFORMED HFEC FOR VERIFICATION OF CRACK CONTAINMENT. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. AJul 31, 2009 · N89427 · Boeing 727227 · Leading Edge DevicesSDR C8GA20090231Skin · crackedWHILE IN HEAVY MX PERFORMING INSPECTIONS, IT WAS NOTED THAT THE NR 3 SLAT OTBD TRACK L/E CRACKED. STOP DRILLED CRACK, PERFORMED HFEC FOR VERIFICATION OF CRACK CONTAINMENT. FABRICATED REPAIR DOUBLER FROM .063" 2024 T3 DIM 10.5" X 9.250" AND FILLER FROM .063" Jul 31, 2009 · N89427 · Boeing 727227 · Leading Edge DevicesSDR C8GA20090230Skin · crackedWHILE IN HEAVY MX PERFORMING INSPECTIONS, IT WAS NOTED THAT THE NR 3 SPOILER HINGE CUTOUT IS CRACKED. STOP DRILLED CRACK, PERFORMED HFEC FOR VERIFICATION OF CRACK CONTAINMENT. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAJul 31, 2009 · N89427 · Boeing 727227 · SpoilersSDR C8GA20090227Skin · crackedWHILE IN HEAVY MX INSP, IT WAS NOTED THAT THE NR4 SPOILER, NR2 HINGE CUTOUT IS CRACKED. STOP DRILLED CRACK, PERFORMED HFEC FOR CRACK CONTAINMENT. FABRICATED DOUBLER REPAIR FROM 7075 T6 DIN 6.5" X 4.25" .071, FILLER FROM 7075 T6 DIM 3" X .75". INSTALLED REPAJul 31, 2009 · N89427 · Boeing 727227 · SpoilersSDR C8GA20090228Stringer · crackedWHILE IN HEAVY MX INSP, IT WAS NOTED THAT STRINGER 18A IS CRACKED AT BS 910-940. DAMAGED SECTION OF STRINGER WAS REMOVED. FABRICATED NEW STRINGER FROM 65-58488-25,REPAIR ANGLES, FILLERS AND SHIMS. INSTALLED STRINGER AND SPLICE REPAIR. NO OTHER DEFECTS NOTEDJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR C8GA20090227AAngle · crackedWHILE IN HEAVY MX INSP IT WAS NOTED THAT THE NR1 K FLAP ACTUATOR INBD MOUNT ANGLE IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE FROM 2024 T3 DIM 8" X 3.5" .063", DOUBLER FROM 2024 T3 DIM 4.875" X 2" .125". INSTALLED REPAIR, NO OTHER DEFECTS WERE NOJul 31, 2009 · N89427 · Boeing 727227 · Leading Edge DevicesSDR C8GA20090226Door · corrodedWHILE IN HEAVY MX INSP, CORROSION WAS NOTED AT THE AFT LAVATORY SERVICE DOOR STA 1183, STR 22L. REMOVED AFT DOOR SERVICE PANEL, REMOVED CORROSION FROM INTERNAL DOUBLER. FABRICATED TIPPLER FROM 7075 T6 DIM 20" X 20" .071", DOUBLER FROM 2024 T3 DIM 8" X 27" .02Jul 31, 2009 · N89427 · Boeing 727227 · Fluid Service DoorsSDR C8GA20090225Doubler · noneWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE EXISTING REPAIR AT BS 1223 AND 1242 RT AFT FUSELAGE REQUIRES PERMANENT REPAIR. EXISTING REPAIR WAS REMOVED, FABRICATED DOUBLER. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVIJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Plate/SkinSDR C8GA20090224Skin · dentedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION A DENT WAS NOTED ON THE HORIZONTAL STAB LEADING EDGE. DAMAGED AREA WAS CUT OUT. FABRICATED DOUBLER, & FILLER . INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.Jul 31, 2009 · N89427 · Boeing 727227 · Horizontal Stabilizer, Plate/SkinSDR C8GA20090223AFrame · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION A CRACK WAS NOTED IN THE FRAME ATT BS 720F AT STRINGER 16R APPROX 5" LONG. CUT OUT DAMAGED PORTION DIM 5" X 2.5". FABRICATED REPAIR PARTS (ANGLE)FROM 7075-T6 DIM 15" X 5.5", FRAME FROM 7075-0 .080" DIM 15" X 7".Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, FrameSDR C8GA20090222Floorbeam · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE MAIN CABIN FLOORBEAM AT BS 990 UPPER FLANGE IS CORRODED BETWEEN RBL 45-70. CORROSION FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS. INSTALLED REPAIR PART, NO OTHEJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Floor BeamSDR C8GA20090221Stringer · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT STRINGER 26L STATION 680 +12 HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGED AREA APPROX DIM 23.25" FABRICATED STRINGER REPAIR FROM BAC 1498-143 7075 T62 DIM 23.25", BAC 14Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR C8GA20090224ASkin · crackedWHILE IN INSP, IT WAS NOTED THAT THE LT INBD AFT FLAP UPPER SKIN AT HINGE IS CRACKED. STOP DRILLED CRACK, HFEC FOR CRACK CONTAINMENT AND FABRICATED DOUBLER. INSTALLED DOUBLER, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Jul 31, 2009 · N89427 · Boeing 727227 · Trailing Edge FlapsSDR C8GA20090222AStringer Splice · corrodedWHILE IN INSP, IT WAS NOTED THAT THE SPLICE AT STR 26L AT BS 680 IS CORRODED. REMOVED STR SPLICE, FABRICATED SPLICE, HEAT TREATED TO T6. INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR C8GA20090221ASkin · corrodedWHILE IN INSP, IT WAS NOTED THAT THE SKIN AT STR 26L AT BS 680 IS CORRODED. CUT OUT UPPER SKIN, . FABRICATED REPAIR DOUBLER, FILLER, INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Jul 31, 2009 · N89427 · Boeing 727227 · Wing, Plate/SkinSDR C8GA20090220Floorbeam · corrodedWHILE IN INSPECTION, IT WAS NOTED THAT THE FLOORBEAM AT BS 1130 RBL 50 IS CORRODED. REMOVED CORROSION, CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED FILLER FROM 7075 T6 DIM 1.5 INCH X 1.25 INCH .160 INCH, STRAP 7075 T6 1 INCH X 10 INCH .160 INCH, STRAP 707Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Floor BeamSDR C8GA20090219Spar · corrodedWHILE IN HEAVY MX INSP, IT WAS NOTED THAT RT WING FRONT SPAR WEB IS CORRODED. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER FROM 2024 T3 DIM 10 INCHES X 12 INCHES .160 INCH. INSTALLED DOUBLER REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVIJul 31, 2009 · N89427 · Boeing 727227 · Wing SparSDR C8GA20090218Stringer · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT STRINGER 26R B.S. 530 IS CORRODED. CORROSION FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGED AREA DIM 25" FABRICATED NEW STRINGER FROM BAC 1498-131 7075 T6 DIM 15.25" X 10.375. INSTALLED NEW STRIJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR C8GA20090217Stringer Splice · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT STRINGER SPLICE AT 26R B.S. 480 IS CORRODED. CORROSION FOUND TO BE OUT OF LIMITS, FABRICATED NEW SPLICE FROM 7075 T6 DIM 14" X 47" .050". INSTALLED SPLICE, NO OTHER DEFECTS NOTED. AIRCRAFT WJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR C8GA20090216Skin · misrepairedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE EXISTING REPAIR ON THE NR 6 SLAT I/B EDGE IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER. INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT RETURNED TO SERVICE.Jul 31, 2009 · N89427 · Boeing 727227 · Leading Edge DevicesSDR C8GA20090215Shear Tie · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE LOWER FLANGE OF SHEAR TIE AT B.S. 720, BL 0 IS CORRODED. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED SHEAR TIE "L" ANGLE, FABRICATED NEW ANGLE. INSTALLED ANGLE, NO OTHER DEFECTS WERE NOTEJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Internal Mounting StructureSDR C8GA20090214Intercostal · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT AT BS 620 STRINGER 23R, INTERCOSTAL CRACKED. REMOVED CRACKED INTERCOSTAL FABRICATED NEW INTERCOSTAL, HEAT TREATED TO T6. INSTALLED INTERCOSTAL, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Miscellaneous StructureSDR C8GA20090213Skin · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE SKIN BELOW STRINGER 27R B.S. 1050-1100 IS CORRODED. REMOVED CORROSION, CORROSION FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA AND PERFORMED NDT WITH NO DEFECTS NOTED. FABRICATED DOUBLERJul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Plate/Skin
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