Boeing 717-200

Service difficulty reports · 18,771

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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 = '717200'
  ORDER BY difficulty_date DESC"

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SDR DALA2019071304236Skin · corrodedSEVERAL CORROSION POINTS ON FUSELAGE SKIN BTW STA Y=794 TO Y=851 BTW LONG 26L TO 26R AT FILLET PANELS AREA IN REF 5315-2001. (FUS). NRC 00420: CORROSION LEVEL 2, AREA WAS REPAIRED PER ER/A 579396-14 REV ORIGINAL SECTION I AND SECTION II. ASSOCIATED ER/A 00-579Jul 12, 2019 · N948AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019071304235Splice · corrodedCORROSION ON SPLICE BTW LONG 26L TO 26R AT STA Y=815 AT FILLET PANELS AREA IN REF 5315-2001. (FUS). NRC 00421: CORROSION LEVEL 2, AREA WAS REPAIRED PER ER/A 579396-14 REV ORIGINAL SECTION I AND SECTION II. ASSOCIATED ER/A 00-579396 ADDED FOR AC 9508. (LP #1168Jul 12, 2019 · N948AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019071304234Window Frame · crackedCRACK ON FRAME OF CLEAR VIEW WINDOW LT, UPPER AFT CORNER. (CPIL). NRC 00527: CRACK WAS REPAIRED PER SRM 56-10-02-2R-1 REPAIR 1 FIG.201, PERFORM LEAK CHECK PRESSURIZATION PER AMM 21-30-00 780-801. NO LEAKS WERE FOUND. (LP #1168010)Jul 12, 2019 · N948AT · Boeing 717200 · Flight Compartment WindowsSDR DALA2019071804288Cover · missingTHE EMERGENCY EXIT SIGN COVER IS LOOSE AT LOCATION: 6.2 INTERIOR. UPON ARRIVAL MAINTENANCE DISCOVERED THAT THE EMERGENCY EXIT SIGN COVER WAS MISSING. THE EXIT SIGN COVER WAS REINSTALLED AND THE OPERATIONAL CHECK WAS GOOD PER AMM 25-60. (LP #1167004)Jul 11, 2019 · N974AT · Boeing 717200 · Emergency LightingSDR DALA2019071604249Tray · dirtySHIP 9585 - THE CREW ABORTED THE TAKE-OFF AT 110 KNOTS FOR A "TAKEOFF CONFIGURATION" WARNING DUE TO STAB TRIM. ALSO THE ENGINE DISPLAY BLANKED FOR 4 SECONDS. CORRECTIVE ACTION: MAINTENANCE FOUND DUST IN BOTH OF THE VIA COMPUTER TRAYS. THE TRAYS WERE CLEANED ANJul 10, 2019 · N985AT · Boeing 717200 · Central DisplaySDR DALA2019071104151Floor Panel · delaminatedPARTS RACKS: DELAMINATED FLOOR PANEL NR 221DF ON PAX CABIN. SUMMARY OF NRC 00665: FLOOR PANEL NR 221DF WAS FABRICATE REPLACED AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP1165057)Jul 10, 2019 · N944AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2019071104150Finger Doubler · corrodedINITIAL INSPECTION. CORROSION ON FINGER DOUBLER BTW STA Y: 585 TO Y: 570, S26L AT FWD CARGO COMPARMENT. FINGER DOUBLER WAS REPLACED PER SRM 51-00-07-0G, PAR. 5. CORROSION LEVEL 2. (LP1164589)Jul 10, 2019 · N944AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019071104149Frame · crackedINITIAL INSPECTION: CRACK ON FRAME STA 1225 CANT BTW 3/4 O CLOCK POSITION AT AFT FUSELAGE. SUMMARY: OF NRC 00412 AREA WAS REPAIRED PER ER/A 579525-14 REV. ORIGINAL AND ETI-17-19-118 REV 2 ( PERMANENT REPAIR). (LP1164569)Jul 10, 2019 · N948AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019071004146Power Supply · inoperativeDURING SERVICE CHECK FOUND EMERGENCY LIGHT FROM ROW 23-29 IN OP. REMOVED AND REPLACED BATTERY POWER SUPPLY PER AMM 33-51 AND OPS CHECK GOOD. A/C OK FOR SERVICE. (LP5973324)Jul 10, 2019 · N985AT · Boeing 717200 · Emergency LightingSDR DALA2019071004145Coalescer Bag · dirtyAFTER SELECTING APU BLEED AIR ON WITH BOTH LEFT OR RIGHT PACK ON, FUEL ODOR IN AIRCRAFT , DISSIPATED AFTER A FEW MINUTES. STARTED ODI PREVENTION -AMM 2172. INSPECTED APU - RAN PAKS FOUND NO CONTAMINATION AT APU COMPARTMENT OR THE INLET. PER FIM 49-50-00-810-80Jul 9, 2019 · N979AT · Boeing 717200 · Humidity Control SystemSDR DALA2019071004144Light · unsecureEMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE LOCATIONS:19B. SECURED LIGHTING STRIP. OK FOR SVC. REF AMM 33-51. (LP1162517)Jul 9, 2019 · N979AT · Boeing 717200 · Emergency LightingSDR DALA2019071004142Cusp Web · crackedAWR: HIDDEN DISCREPANCY: IN REF NRC 568: CRACK ON LT CUSP WEB BTW STA 446 AND 465 PASSENGER CABIN. SUMMARY OF NRC S/N 00656: CRACK ON LT CUSP WEB BTW STA 446 AND 465 PASSENGER CABIN WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 215. (LP1163685)Jul 9, 2019 · N944AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019071004141Longeron · crackedINITIAL INSPECTION: CRACK LONGERON NR 6L IN STA Y=1022. LONGERON NR 6L IN STA Y=1022 WAS REPAIRED PER SRM 53-00-05-2R-2 FIG. 201. (LP1162983)Jul 9, 2019 · N944AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019071004140Longeron · crackedINITIAL INSPECTION: CRACK LONGERON NR 6R IN STA Y=1022. LONGERON N 6R IN STA Y=1022 WAS REPAIRED PER SRM 53-00-05-2R-2 FIG. 201. (LP1162729)Jul 9, 2019 · N944AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019071004139Hinge · crackedINITIAL INSPECTION: CRACK ON INBD FLAP FAIRING HINGE AT STA. XRS =137. 750 AT LT WING. (AI). INB FLAP HINGE FAIRING WAS REPLACED SERVICEABLE PN: 5912150-509 PER DWG 5910134 AND AMM 20-50-01-911-801 TOOL USED P/N TE25AC S/N 1049 DUE DATE 21/AUG/19. (LP1163426)Jul 9, 2019 · N948AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2019070904113Access Panel · corrodedPART RACKS: CORROSION ON COUNTERSUNK AREA ON FUEL ACCESS PLATES NR 520DT AND 520GB. CORROSION LEVEL 2. FUEL ACCESS PLATES NR 520DT AND 520GB WERE REPLACED AND VERIFIED PER IPC 57-22-01-01 ITEM 015 AND IPC 57-23-01-01 ITEM 345. (LP1161708)Jul 8, 2019 · N948AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019070904112Skin · crackedAWR IN REFERENCE MON 2071758 : A CRACK WAS FOUND ON DENT # 10 AT RT AFTER MOVABLE VANE LOWER SKIN (AD). SUMMARY OF THIS N.R.C. 00747": IN REFERENCE MON 2071758 CRACK IN DENT NO. 10 (LOCATION: 25" OF INBD EDGE AND 14" OF T/E) WAS REPAIRED AT LOWER SKIN AFT MOVAJul 8, 2019 · N948AT · Boeing 717200 · Trailing Edge FlapsSDR HALA2019090500370Attach Angle · crackedLT LOWER WING TO FUSELAGE ATTACH ANGLE FOUND CRACKED AROUND ONE FASTENER HOLE. ANGLE IS LOCATED AT STA 661 BETWEEN L-22L AND L-21L. TRIMED OUT CRACK AS REQUIRED. ACCOMPLISHED A SURFACE HFEC INSPECTION PER NDT SPM PART 06-10--01.001. NO CRACKS FOUND. ACCOMPLISJul 7, 2019 · N491HA · Boeing 717200 · Wing, Fuselage Attach FittingsSDR HALA2019090500367Splice Angle · crackedLEFT WING T/E 4981366-1 SPLICE ANGLE CRACKED FWD OF INBD SPOILER. REMOVED AND REPLACED ANGLE, 4981366-1 PER DWG 59Y2156. PRIMED AND PAINTED AREA PER SRM 51-22-01.Jul 7, 2019 · N491HA · Boeing 717200 · Wing Miscellaneous StructureSDR HALA2019090500366Spar · corrodedLEFT WING REAR SPAR LOWER TANG SERVER CORROSION STATION 360. 366 (M) 0/B OF 0/B FLAP HINGE. TRIMMED OUT CORRODED FLANGE AT XRS 360 TO 366. PERFORMED HIGH FREQUENCY EDDY CURRENT(HFEC) INSPECTION FOR THE FLANGE AND OPEN HOLES IN THE EFFECTIVE AREA, NO CRACKS FOJul 7, 2019 · N491HA · Boeing 717200 · Wing SparSDR DALA2019070804078Release Cable · brokenINITIAL INSPECTION: BROKEN STRANDS ON CONTROL CABLE (LT MIDDLE) OF TAIL CONE EMERGENCY RELEASE SYSTEM. BROKEN STRANDS ON CONTROL CABLE (LT MIDDLE) OF TAIL CONE EMERGENCY RELEASE SYSTEM WAS REPLACED PER AMM 53-52-01-830-802. OPERATIONAL TEST WAS PERFORMED PER AJul 7, 2019 · N948AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2019070804077Access Panel · corrodedPART RACKS: CORROCION ON COUNTERSINK AREA ON FUEL ACCESS PLATE NBR 620DT AND 620DB. CORROSION LEVEL 2. FUEL ACCESS PLATE NR 620DT AND 620DB WERE REPLACED PER SRM 57-10-01-2R REPAIR 2 PAR.5C CONDITION III TABLE 201, VERIFIED PER IPC 57-22-01-01 ITEM 020 AND IPCJul 7, 2019 · N948AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019070804076Access Panel · damagedPART RACKS: ELONGATED HOLES ON FUEL ACCESS PLATES NBR 141AL AND 520CB. ACCESS PLATES NBR 141AL AND 520CB WERE REPLACED AND VERIFIED PER IPC 57-22-01-01 ITEM 015, IPC 57-23-01-01 ITEM 465J. (LP1160237)Jul 7, 2019 · N948AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019070804075Splice · corrodedAWR IN REF MON/9508/049-MON, 95 REP, L.P. 2070042: CORROSION ON PREVIOUS REPAIR SPLICE LOWER AREA OF AFT CARGO COMPARTMENT. LEVEL 2. PREVIOUS REPAIR SPLICE LOWER AREA WERE REPLACED OF AFT CARGO COMPARTMENT PER SRM 53-20-15-2R-7, SRM 51-41-04-0G AND SRM 51-41-0Jul 7, 2019 · N948AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019070804080Battery Pack · dischargedEMERGENCY EXIT SIGNS INOPERATIVE. EXIT LIGHTS FLASHING. T/S AS PER FIM 33-50; ALLOW SUFFICIENT TIME FOR BATTERY PACKS TO RE-CHARGE OPS CHECK NORMAL OK FOR SERVICE. (LP1157653)Jul 6, 2019 · N995AT · Boeing 717200 · Emergency LightingSDR DALA2019070704062Cargo Track · corrodedINITIAL INSPECTION: CORROSION ON LT TIE TRACK, BTW STA:915 TO STA:1020 AT AFT CARGO COMPARTMENT. SUMMARY: OF NRC.00359 CORROSION LEVEL 2. LT TIE TRACK, WAS REPLACED BTW STA:915 TO STA:1020 AT AFT CARGO COMPARTMENT PER SRM 51-41-05-0G AND SRM 51-41-01-0G. (LP11Jul 6, 2019 · N948AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019070704061Access Panel · corrodedOUT OF LIMITS - CORROSION IN ACCESS 520FT, 520GB, 520DT, 520CT, 520CB AND CENTER FUEL TANK UPPER ACCES PANNEL, SETTLEMENT AREA AND COUNTERSINK HOLES. AT FUEL TANK (AI). ALL PANELS WERE REPLACED. (LP1157907)Jul 6, 2019 · N943AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019070704060Access Panel · corrodedOUT OF LIMITS- CORROSION IN ACCESS 620 CB, 620AT AND 620 DT SETTLEMENT AREA AND COUNTERSINK HOLES. AT FUEL TANK (AD). ACCES PANEL 620CB WAS REPLACED AND PART NUMBER WAS VERIFIED PER IPC 57-23-01-01 (SHEET 6) (ITEM 465J) AND ACCES PANNEL 620AT AND 620DT WERE REJul 6, 2019 · N943AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019070604056Frame · corrodedCORROSION ON FRAME STA:1022 BTW STGR:27L AND STGR:28R AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2. FRAME WAS REPAIRED PER SRM 53-20-07-2R-3 REPAIR 3 CONFIGURATION -7005. PERFORM VISUAL INSPECTION INITIAL 25,000 CYCLES AND REPETITIVE 6,500 CYCLES PER SRM 53-20-Jul 6, 2019 · N948AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019070604059Cargo Track · corrodedINITIAL INSPECTION: CORROSION ON TIE TRACK BTW STA:994 TO STA: 1020 AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2.TIE TRACK RT BTW STA:994 TO STA:1020 AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 53-20-51-0I-7 AND 51-41-01-0G. (LP1156952)Jul 6, 2019 · N948AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019070604055Hinge Bracket · corrodedAWR, HIDDEN CORROSION (IN REF NRC S/N 00283): CORROSION WAS FOUND ON ELEVATOR HINGE BRACKET HOLES AT RT HORIZONTAL STABILIZER STA XHS=104, 158, 204 AND 2. CORROSION ON ELEVATOR HINGE BRACKET HOLES AT RT HORIZONTAL STABILIZER STA XHS=104, 158, 204 AND 225 (EHV)Jul 6, 2019 · N943AT · Boeing 717200 · Elevator StructureSDR DALA2019070604054Longeron · corrodedINITIAL INSPECTION: SEVERAL CORROSION ON LONGERON L30 FROM STA 889 TO STA 1053 AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2 CORROSION ON LONGERON 30 BTW STA Y=894-1076 WAS REMOVED PER SRM 51-10-04-0G PAR 26 (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR.5 FIG 3Jul 5, 2019 · N943AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019070604053Cap · crackedINITIAL INSPECTION: CRACK ON CAP AT BULKHEAD STA. 1022 LONGERON 7R. CRACK ON CAP AT BULKHEAD STA. 1022 LONGERON 7 RH WAS REPAIRED PER ETI-17-19-090 REV ORG. AND ERA 579434-14 REV. ORIG. (LP1156275)Jul 5, 2019 · N948AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2019070604052Skin · crackedINITIAL INSPECTION: CRACK SKIN ON EXTERNAL AREA OF HOLD LOCK AND OPENING LEVER AT PASSENGER DOOR FWD ENTRANCE. SKIN ON EXTERNAL AREA OF OPENING LEVER WAS REPAIRED PER ER/A 579458-14 REV. ORIGINAL AND ETI-17-19-094 REV. 3. (LP1156212)Jul 5, 2019 · N948AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2019070604051Intercostal · crackedINITIAL INSPECTION CRACKED INTERCOSTAL ON STA Y=184 BTW BEAM 4 AND 5 AT PASSENGER DOOR FWD ENTRANCE. INTERCOSTAL ON STA Y=184 BTW BEAM 4 AND 5 WAS REPLACED PER DWG 9955763 REVISION M, SRM 51-41-02- 0G AND 51-41-05-0G. (LP1156196)Jul 5, 2019 · N948AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019070604050Housing · wornAWR,HIDDEN WEAR: WEAR ON HOUSING OF HOLD LOCK AND OPENING LEVER AT PASSENGER DOOR FWD ENTRANCE. HOUSING OF HOLD LOCK AND OPENING LEVER WAS REPLACED PER SRM 51-41-02-0G. (LP1156264)Jul 5, 2019 · N948AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2019070504041Battery · dischargedEMERGENCY EXIT MARKERS @ L1, L2, AND OVERWING EXIT DOORS INOP. R/R BATTERIES PER AMM 33-51. OP'S CHECK GOOD. (LP5742980)Jul 5, 2019 · N988AT · Boeing 717200 · Emergency LightingSDR DALA2019070504043Pushrod · corrodedINITIAL INSPECTION: CORROSION ON PUSH ROD OF HOOK AT RUDDER THROW LIMITER. PUSH ROD OF HOOK AT RUDDER THROW LIMITER WAS REPLACED, ADJUSTED AND TESTED PER AMM 27-26-01-000-801, AMM 27-26-01-400-801 AND 2720-2003. (LP1154990)Jul 4, 2019 · N948AT · Boeing 717200 · Rudder Control SystemSDR DALA2019070504040Fastener · damagedINITIAL INSPECTION: DAMAGED INTERNAL HARDWARE ON LEVER OF THE TAIL CONE JETTISON MECHANISM AT RT LOWER CORNER OF THE TAILCONE CUTOUT. NEW HARDWARE ON LEVER OF THE TAIL CONE JETTISON MECHANISM AT RT LOWER CORNER OF THE TAILCONE WERE INSTALLED PER AMM TAILCONE AJul 4, 2019 · N943AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2019070504039Torque Tube · corrodedINITIAL INSPECTION: CORROSION ON RUDDER CONTROL TAB TORQUE TUBE IN REF 2720-2004 JOB #001-0259. RUDDER CONTROL TAB TORQUE TUBE WERE REPLACED FOR NEW P/N:3917927-1 AND WAS INSTALLED PER 2720-2004 JOB# 001-0259. (LP1155397)Jul 4, 2019 · N948AT · Boeing 717200 · Rudder Tab Control SystemSDR DALA2019070504038Skin · dentedSEVERAL DENTS ( 7 EAS ) ON RH WING AILERON CONTROL TAP UPPER SKIN BTW STATION XAC=3.5 TO XAC=48.2. RT AILERON CONTROL TAB UPPER SKIN DENT 7 WAS REPAIRED PER SRM 51-70-02-2R PROCEDURE 6 REPAIR 6. TAP TEST INSPECTION WAS PERFORMED AFTER REPAIR AND NO DISBONDS WEJul 4, 2019 · N943AT · Boeing 717200 · Aileron TabsSDR DALA2019070504037Skin · crackedINITIAL INSPECTION: CRACK ON FUSELAGE SKIN AT STA Y=1087 BTW LONG 13L TO 14L. PERMANENT REPAIR WAS PERFORMED ON FUSELAGE SKIN AT STA Y=1087 BTW LONG 13L TO 14L PER ERA 579428-14 REV. ORG. SECTION I AND ETI 17-19-081 REV. 5. REPETITIVE INSPECTION WITHIN EVERY CJul 4, 2019 · N948AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019070504024Skin · crackedINITIAL INSPECTION: CRACK ON FUSELAGE SKIN AT STA Y=1073 LONG 14L. PERMANENT REPAIR WAS PERFORMED ON FUSELAGE SKIN AT STA Y=1073 LONG 14L PER ERA 579428-14 REV. ORG. SECTION I AND ETI 17-19-081 REV. 5. REPETITIVE INSPECTION WITHIN EVERY C CK (NOT TO EXCEED 24 Jul 4, 2019 · N948AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019070504023Skin · crackedINITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA. 1087.060, LONGERON 14R SIDE. PERMANENT REPAIR FUSELAGE SKIN STA. 1087. LONGERON 14R WAS PERFORMED PER ERA 579432-14 REV. ORG. AND ETI 17-19-088 REV. 2 AND PERFORM A GVI WITHIN EVERY CCK (NOT TO EXCEED 24 MONTHS) Jul 4, 2019 · N948AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019070504042Bearing · corrodedINITIAL INSPECTION: RUSTED BEARING ON RUDDER DRIVE SECTOR AT AFT ACCESORIES COMPARTMENT IN REF 2720-2003. RUDDER DRIVE SECTOR AT AFT ACCESSORIES COMPARTMENT WAS REPLACED PER AMM 27-21-02. AND RUDDER CONTROL CABLES SYSTEM WAS ADJUSTED UNDER 2720-2004 JOB#001-02Jul 3, 2019 · N948AT · Boeing 717200 · Rudder StructureSDR DALA2019070404035Handle · out of adjustAWR: DURING CHECK OF THE TAILCONE RELEASE SYSTEM, TAILCONE WAS NO RELEASED WITH "EMERGENCY OPERATING HANDLE" OF THE PASSENGER AFT ENTRANCE DOOR PER 5352-2001, STEP 2. NRC 00534 EMERGENCY OPERATING HANDLE OF THE PASSENGER AFT ENTRANCE DOOR WAS ADJUSTED AND TESTJul 3, 2019 · N943AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2019070404034Skin · crackedINITIAL INSPECTION CRACK ON SKIN AND CHANNEL MAIN LANDING GEAR DOOR RT. INNER SKIN AT RH MAIN LANDING GEAR DOOR WAS REPAIRED PER ER/A 579454-14 REVISION ORIGINAL SECTION I AND ETI-17-19-093 REVISION 3. REPETITIVE INSPECTION WITHIN EVERY 3,000 CYCLES AFTER SECTJul 3, 2019 · N948AT · Boeing 717200 · Landing Gear DoorsSDR DALA2019070404033Skin · crackedINITIAL INSPECTION: CRACKED FUSELAGE SKIN STA Y=97 ON NLG DOOR CUT OUT LT AFT HINGE DOOR. SUMMARY IN REF OF NRC 00039 AREA WAS REPAIRED PER SRM 53-10-01-2R-11, SRM 51-41-02-0G AND 51-41-05-0G. (LP1153816)Jul 3, 2019 · N943AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019070404032Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME STA:889 AND STR:26L AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2, FRAME STA:889 AND STR: 26L WAS REPAIRED PER SRM 53-20-07-2R PROCEDURE 3, FIGURE 201 (SHEET 7). MAINTENANCE REQUIREMENTS ARE THE FOLLOWING. PERFORM VISUAL INJul 3, 2019 · N948AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019070404031Skin · corrodedINITIAL INSPECTION: CORROSION ON FUSELAGE SKIN BTW STA Y= 1022 - 1035 AND LONG 23L - 26L. CORROSION LEVEL 2 IN REF OF NRC 00063 AREA WAS REPAIRED PER ER/A 578990-14 REV ORIGINAL AND ETI-17-19-085 REV 3. TIME CONTROLLED ITEMS: ACCOMPLISH SECTION II: REPETITIVE Jul 3, 2019 · N943AT · Boeing 717200 · Fuselage Main, Plate/Skin
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