N989AT

Service difficulty reports · 198

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N989AT' AND registry_match = 'registration'
  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 DALA2026090404996Fairing · puncturedPUNCTURE ON TIP FAIRNG OF RT HORIZONTAL STAB. COMPLIED WITH ER/A 636479-14. (1793989) (AIRCRAFT GROUNDED).Sep 3, 2026 · N989AT · Boeing 717200 · Horizontal Stabilizer Miscellaneous StructureSDR DALA2026082404793Door Frame · crackedCRACK ON FWD UPPER CORNER OF GALLEY SERVICE DOOR CUTOUT IN BS Y=174.0 AND 3.5 INCHES FROM LONG 11 RH AT EXTERNAL FUSELAGE, REPAIRED DOOR CUTOUT PER B717-200 SRM 53-10-01-2R. (1773337) (AIRCRAFT GROUNDED).Aug 24, 2026 · N989AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2026082404791Frame · damagedELONGATED FRAME HOLE TO ATTACH AFT ROD OF LT AIR CONDITIONING PACK BS Y=1133 & LONG 9L AT AFT ACCESORY COMPARTMENT, REPAIRED FRAME HOLE IAW SRM 53-00-07-2R. (1772689) (AIRCRAFT GROUNDED).Aug 23, 2026 · N989AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2026082404788Vane · dentedSEVERAL DENTS ON LOWER SURFACE FWD MOVABLE FLAP VANE AT RT WING, FWD MOVABLE FLAP VANE AT RH WING WAS REPAIRED IAW SRM 57-53-01-2R. (1769283) (AIRCRAFT GROUNDED).Aug 21, 2026 · N989AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2026082404804Vane · crackedCRACK WAS FOUND ON AFT MOVABLE VANE IN FWD INBD FITTING AT RT WING, R & R AFT RT MOVABLE FLAP VANE UNDER AMDS 2000-2638. (1765421) (AIRCRFT GROUNDED).Aug 19, 2026 · N989AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2026032201929Anti-Skid Sys · faultedDUE TO RIGHT ANTISKID FAIL ON APPROACH ATL. CORRECTIVE ACTION: FAULTED #3 WHEEL SPEED TRANSDUCER. REPLACED SAME NO HELP. FOUND CONNECTOR P1-3700 PIN 1 AT TRANSDUCER DISCONNECTED. RE-TERMINATED WIRE. OPS CHECK GOOD. (LP 8356405)Mar 19, 2026 · N989AT · Boeing 717200 · Brake Anti-Skid SectionSDR DALA2025061104460Battery Pack · inoperativeAIRCRAFT 9527, MULTIPLE EMERGENCY LIGHTS INOP THROUGHOUT CABIN. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT BATTERY PACKS B5-227 AND B5-230 PER B717 AMM 33-51. OPS CHECK GOOD. (LP 6564077)Jun 10, 2025 · N989AT · Boeing 717200 · Emergency LightingSDR DALA2024120211375Light Sys · inoperativeDURING SERVICE NOTED THAT THE LH AND RH AFT OVERWING AND RH FWD OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY B5-119 REF B717 AMM 33-51. BOTH AFT OVER WING LIGHTS WORK BUT RH FWD STILL INOPERATIVE. FOUND GROUND LOOSE FOR L2-832. REDec 1, 2024 · N989AT · Boeing 717200 · Emergency LightingSDR DALA2024120911532Duct · temp repairCRACK ON RIGHT ENG BYPASS DUCT NEAR PRECOOLER INLET WAS TEMPORARILY REPAIRED. RE-INSPECTION REQUIRED PER ER/A 620571-14 REV ORIGINAL. REFER TO LOG #0580374 FOR PRIOR INSPECTION. SECTION 4 INSPECTION MUST BE ACCOMPLISHED BETWEEN 220 AND 180 FLIGHT CYCLES PER EROct 19, 2024 · N989AT · Boeing 717200 · Engine (Turbine/Turboprop)SDR DALA2024091809140Hinge · excess playFREEPLAY WAS FOUND ON RH WING FLAP OUTBD HINGE AREA. SUMMARY OF NRC 00781: RH WING FLAP OUTBD HINGE WAS REPAIRED PER ER/A 620752-14 REV ORIGINAL AND PRI 620752-14 REV 2 AND WAS INSTALLED PER B717-200 AMM 27-55-03 400-801. ASSOCIATED ER/A 14-620752 ADDED FOR ACSep 17, 2024 · N989AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024091809136Pan · crackedCRACK ON PAN FWD EDGE IN LOWER SIDE AT FWD CARGO COMPARTMENT DOOR. RE-WRITE REASON: TECHNICAL REFERENCE USED DOES NOT APPLY TO FWD CARGO COMPARTMENT. ALSO, AFTER DOUBLERS REMOVED CRACKS WERE FOUND ON PAN BTW BEAM 1 AND 2 AND ELONGATED HOLES ON INNER/OUTER PAN.Sep 17, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024091609051Pan · crackedCRACK ON AFT PAN WAS FOUND BTW BEAM 1 AND 2 AT AFT CARGO DOOR (REF NRC NBR 00640). SUMMARY OF NRC 00693: AFT INNER PAN BTW BEAM 1 AND 2 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 620224-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620224-14 REVSep 15, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024091609047Shear Tie · crackedFABRICATED PARTS IN REFERENCE NRC 00592 AND PRI 620225-14 REV 0. MANUFACTURE SHEAR CLIP (AFT ACCESS). CRACK WAS FOUND ON SHEAR CLIP IN REFERENCE NRC 00592: FABRICATE SHEAR CLIP PER PRI 620225-14 REV 4 AND ER/A 620225-14 REV OROGINAL, SECTION I PERMANENT REPAIRSep 12, 2024 · N989AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2024091308982Skin · crackedCRACK ON SKIN, SHEAR CLIP, AND SHEAR TIE OUTBOARD FASTENER AT STA Y=1152 AND LONG 2L ON AFT ACCESORY COMPARTMENT (IN REFERENCE TO ERA 95-520358-14 REV ORIGINAL FIGURE 4). SUMMARY OF NRC 00592: SHEAR TIE OUTBOARD FASTENER AT STA Y=1152 AND LONG 2L ON AFT ACCESOSep 12, 2024 · N989AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024091008881Frame · corrodedCORROSION ON FRAME BTW STA Y=1023 LONGERON 29L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00754: CORROSION LEVEL 2. CORROSION ON FRAME BTW STA Y=1023 LONGERON 29L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. (LP #0542411)Sep 6, 2024 · N989AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2026080404487Skin · corrodedCORROSION STABILIZERS RT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL BARREL NUT HOLE #11. REPAIRED PER ERA 620136-14. (0541097) AIRCRAFT WAS GROUNDED.Sep 5, 2024 · N989AT · Boeing 717200 · Horizontal Stabilizer, Plate/SkinSDR DALA2024090608757Access Panel · corrodedCORROSION INSIDE HOLE #33C LWR LH INSIDE ACCESS PANEL 350AB AT STABILIZER CENTER BOX. SUMMARY OF NRC 00399: CORROSION LEVEL 2. HOLE #33C LWR LH INSIDE ACCESS PANEL 350AB AT STABILIZER CENTER BOX WAS REPAIRED PER ER/A 620168-14 REV ORIGINAL, SECTION 1: PERMANENSep 5, 2024 · N989AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2024090608756Barrel Nut · corrodedCORROSION IN BARREL NUT HOLE #11RH AT HORIZONTAL STABILIZER IN REF NRC 00400. SUMMARY OF NRC 00649: CORROSION LEVEL 2. BARREL NUT HOLE #11RH AT HORIZONTAL STABILIZER WAS REPAIRED PER PRI 620136-14 REV 3 & ER/A 620136-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSep 5, 2024 · N989AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2024090308637Cusp Web · crackedCRACK ON CUSP WEB STA Y=645 X=44, Y=656 X=57, AND Y=633 X=44 AT LH PASSENGER CABIN (CPAX). SUMMARY OF NRC 00516: CUSP WEB STA Y=645 X=44, Y=656 X=57, AND Y=633 X=44 AT LH PASSENGER CABIN WERE FABRCATED AND REPAIRED PER DWG 9910151 REV CH, B717 SRM 51-70-10-2R Sep 2, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024090308636Former · crackedCRACK FORMER ON INTERNAL STRUCTURE BTW BEAM 4/5 FWD EDGE AT L1 DOOR. L1. SUMMARY OF NRC 00118: FORMER ON INTERNAL STRUCTURE BTW BEAM 4/5 FWD EDGE AT L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCEDURE 3, REPAIR 3. (LP #0533710)Sep 1, 2024 · N989AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2024090308635Pan · crackedCRACK ON AFT PAN INTERSECTION WITH BEAM #5, CRACK ON FWD PAN INTERSECTION WITH BEAM #3 , 3) CRACK ON FWD PAN INTERSECTION WITH BEAM #5 ON FWD CARGO DOOR. SUMMARY OF NRC 00132: AFT PAN INTERSECTION WITH BEAM #5, FWD PAN INTERSECTION WITH BEAM #3, AND FWD PAN INSep 1, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024083008600Cap · crackedCRACK ON CAP STA Y=1022 & LONG 7R ON PASSENGER CABIN. SUMMARY OF NRC 00554: CAP STA Y=1022 & LONG 7R ON PASSENGER CABIN WAS REPAIRED PER ERA 620017-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620017-14 REV 1. ASSOCIATED ER/A 14-620017 ADDED FOR AC 9527Aug 30, 2024 · N989AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024090408731Intercostal · crackedCRACK ON INTERCOSTAL 2 (EA) STA Y=1225 LONGERON 1 AT AFT ACCESORIES COMPARTMENT. SUMMARY OF NRC 00361: INTERCOSTAL 2 (EA) STA Y=1225 LONGERON 1 AT AFT ACCESORIES COMPARTMENT WERE REPLACED PER B717-200 SRM 51- 41-02-0G AND 51-42-05-0G AND SPRINGS WERE REMOVED AAug 29, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024083008598Longeron · crackedCRACK ON LONGERONS 06R, 05R, 04R, 03R STA Y=1022 ON PASSENGER CABIN. SUMMARY OF NRC 00553: LONGERONS 06R, 05R, 04R, 03R STA Y=1022 ON PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2. (LP #0527480)Aug 29, 2024 · N989AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024083008593Beam · crackedCRACK BEAM #1 AFT EDGE AT L1 DOOR PTAS. SUMMARY OF NRC 00320: BEAM #1 AFT EDGE AT L1 DOOR PTAS WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0526246)Aug 28, 2024 · N989AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024082808521Seat Track · crackedAIRCRAFT 9527, AFTER SEAT TRACK X = -44 BTW STA Y = 646 TO Y = 775 REMOVAL, CRACK ON HOLES AT WEB BTW STA 648 AND STA 650. CORRECTIVE ACTION: WEB BTW STA 648 AND STA 650 WAS REPAIRED PER B717 SRM 51-41-02-0G AND B717-200 SRM 51-70-10-2R-2. (LP 0524830)Aug 27, 2024 · N989AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024082508422Window Frame · crackedAIRCRAFT 9527, CRACK LH SLIDING WINDOW FRAME, JUST AFT UPPER CORNER OF INNER PLATE SKIN AT CREW CABIN. CPRRECTIVE ACTION: LH SLIDING WINDOW FRAME, JUST AFT UPPER CORNER OF INNER PLATE SKIN AT CREW CABIN WAS REPAIRED PER B717 SRM 56-10-02-2R-1. (LP 0519523)Aug 24, 2024 · N989AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024082408419Frame · crackedAIRCRAFT 9527, CRACKS ON FRAME STA Y=1037 AT INTERSECTION WITH LONGERONS 17L, 13L AND 12L ON PASSENGER CABIN. CORRECTIVE ACTION: FRAME STA Y=1037 AT INTERSECTION WITH LONGERONS 17L, 13L AND 12L ON PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEAug 23, 2024 · N989AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024082308414Cusp Web · crackedAIRCRAFT 9527, CRACK CUSP WEB MEMBRANE UNDER SEAT TRACK STA Y 660 X=-44 AT PAX CABIN. CORRECTIVE ACTION: CUSP WEB MEMBRANE UNDER SEAT TRACK STA Y 660 X=-44 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R-2 AND SRM 51-41-02-0G. (LP 0516434)Aug 22, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024082308413Cusp Web · crackedAIRCRAFT 9527, CRACK ON CUSP WEB STA Y=715 X=44 AT PASSENGER CABIN (CPAX). CORRECTIVE ACTION: CUSP WEB STA Y=715 X=44 AT PASSENGER CABIN (CPAX) REPAIRED PER B717-200 SRM 51-41-02-0G AND B717-200 SRM 51-70-10-2R-2 FIG. 201. (LP 0516174)Aug 22, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024082308411Window Frame · crackedAIRCRAFT 9527, CRACK ON RH WINDOWS RING PAN ON STA Y=737 UPPER FWD CORNER AND STA Y=889 LOWER FWD CORNER AT CPAX. CORRECTIVE ACTION: RH WINDOWS RING PAN ON STA Y=737 UPPER FWD CORNER AND STA Y=889 LOWER FWD CORNER AT CPAX WERE REPAIRED PER B717-200 SRM 56-20-0Aug 22, 2024 · N989AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024082208364Cusp Web · crackedAIRCRAFT 9527, CRACK ON CUSP WEB STA Y=813 X=54 AT LH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: CORROSION LEVEL 2, CUSP WEB STA Y=813 X=54 AT LH PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM. 53-00-55-2R PROCEDURE 4 FIG. 205. (LP 0514941)Aug 21, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024082208363Web · corrodedAIRCRAFT 9527, CORROSION ON RH WEB BTW STA Y=446 TO STA Y=465 AT CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2: RH WEB BTW STA Y=446 TO STA Y=465 AT CPAX WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. FIGURE 210. (LP 0514913)Aug 21, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024082208360Pan · crackedAIRCRAFT 9527, INITIAL INSPECTION: CRACK ON LH RING PAN (FWD/UPPER) STA Y= 484, (FWD/LOWER) STA Y=636, (AFT/UPPER) STA Y=851, (FWD/LOWER) STA Y= 851, (FWD/LOWER) STA Y=870, (FWD/LOWER) STA Y=908, (FWD/LOWER) STA Y=927, (FWD/UPPER/LOWER) STA Y= 946 AT CABIN PAXAug 21, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024082208359Web · corrodedAIRCRAFT 9527, CORROSION ON RH WEB BTW STA Y=448 TO STA Y=503 AT CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2: RH WEB BTW STA Y=448 TO STA Y=503 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 210. (LP 0514363)Aug 21, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024082208357Longeron · crackedAIRCRAFT 9527, CRACK ON LONGERON 4R STA Y=1152 AT AFT ACCESSORIES COMPARTMENT. CORRECTIVE ACTION: LONGERON 4R STA Y=1152 AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R. PROCEDURE 2. REPAIR 2 FIG. 201. (LP 0514325)Aug 21, 2024 · N989AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024082108332Structure · ground damageAIRCRAFT 9527, FWD CARGO DOOR SURROUND AFT SIDE HIT BY BELT LOADER. CORRECTIVE ACTION: PERMANENT REPAIR ON FWD CARGO DOOR SURROUND AFT SIDE HIT BY BELT LOADER WAS PERFORMED PER B717-200 SRM 53-20-15-2R, REPAIR 11, OPTION 1. PERFORMED VISUAL INSPECTION ON PERMAAug 20, 2024 · N989AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024082108330Web · crackedAIRCRAFT 9527, INITIAL INSPECTION: SEVERAL CRACKS BELOW INBD WEB RH APPROX BTW STA Y=715 TO STA Y=737 AT CPAX. CORRECTIVE ACTION: WEB RH APPROX BTW STA Y=715 TO STA Y=737 AT CPAX WAS REPAIRED PER B717-200 SRM 57-70-10-2R-2, PAR. 4 AND B717-200 SRM 51-41-02-0G.Aug 20, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024081908279Beam · crackedCRACK BEAM #6 MID SECTION JUST BY HARDWARE AREA AT L1 PASSENGER DOOR. PTAS. SUMMARY OF NRC 00321: CRACK BEAM #6 MID SECTION JUST BY HARDWARE AREA AT L1 PASSENGER DOOR WAS REPAIRED PER ER/A 559578-14MA REV ORIGINAL. ASSOCIATED ER/A 14-559578 ADDED FOR AC 9527. Aug 17, 2024 · N989AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2024081608211Cusp Web · crackedCRACK ON CUSP WEB STA Y=436 X=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00515: CUSP WEB STA Y=436 X=44 AT PASSENGER CABIN (CPAX) WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. (LP #0504361)Aug 15, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024081408111Longeron · crackedCRACK ON LONGERONS 07L, 06L, 05L, 04L, 03L STA Y=1022 AT PASSENGER CABIN. SUMMARY OF NRC 00552: (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON LONGERONS 07L, 06L, 05L, 04L, 03L STA Y=1022 AT PASSENGER CABIN, 1 CRACK WAS CONFIRMED ON LONG 6LH. PER DC-MD/BOEING NDTSAug 13, 2024 · N989AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024080807886Beam · crackedCRACK WAS FOUND ON AFT BEAM 3 AT PAN. SUMMARY OF NRC 00254: PAN AFT SIDE BEAM 3 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 3 REPAIR 3. (LP #0489872)Aug 7, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024072907549Hub Cap · missingSHIP 9527 -ATO- THE CREW SAFELY ABORTED THE TAKEOFF AT 65 KTS DUE TO RIGHT "ANTI-SKID FAIL" MESSAGE. CORRECTIVE ACTION: MAINTENANCE FOUND THE #4 MAIN GEAR HUBCAP AND CLAMP MISSING. THE HUBCAP AND CLAMP WERE REPLACED AND ALL ANTI-SKID RETURN TO SERVICE TESTS WEJul 26, 2024 · N989AT · Boeing 717200 · Brake Anti-Skid SectionSDR DALA2024071507165Spring · brokenSHIP 9527 -ATB/GEAR/DE- THE FLIGHT CREW RETURNED THE AIRCRAFT TO ATL DUE TO A RIGHT MAIN LANDING GEAR "DOOR UP AND LATCHED UNSAFE" INDICATION. ATC DECLARED AN EMERGENCY FOR THIS EVENT. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR UP AND LATCHED SENSOR SPRINJul 13, 2024 · N989AT · Boeing 717200 · Landing Gear Position and WarningSDR DALA2023102508761Unknown · unknownTHE CIRCUIT BEAKER Z26 WAS DISCOVERED OUT. FLIGHT CREW RESET IT ON DIRECTION OF MAINTENANCE. BREAKER VISIBLY SPARKED. BREAKER IS OUT AGAIN. MAINTENANCE FOUND WIRES CROSSED AT F/O SLIDING WINDOW. RETERMINATED WIRES AT SPLICE. BREAKER NOW OPERATES NORMALLY. WINDOct 20, 2023 · N989AT · Boeing 717200 · Windshield/Door Rain/Ice RemovalSDR DALA2023092807972Unknown · unknownCRACK ON SKIN ON STA Y=1133 AND BTW LONG 2R AND LONG 3R AT AFT FUSELAGE. SUMMARY OF NRC 00077: CRACK ON SKIN ON STA Y=1133 AND BTW LONG 2R AND LONG 3R AT AFT FUSELAGE WAS REPAIRED PER PRI 612145-14 REV 5 AND ER/A 612142-14AD REV ORIGINAL. SECTION I: PERMANENT Sep 27, 2023 · N989AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023092707955Unknown · unknownCRACK ON WEB (BELOW FLOOR BEAM) STA Y=696 AND X=56 LH ADJACENT TO FRAME. (WINGBOX AREA). SUMMARY OF NRC 00118: CRACK ON WEB (BELOW FLOOR BEAM) STA Y=696 AND X=56 LH ADJACENT TO FRAME WAS REPAIRED PER PRI 612213-14 REV 2 AND ER/A 612213-14 REV ORIGINAL SECTION Sep 26, 2023 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092707954Unknown · unknownCRACK ON LH CUSP WEB STA Y=696 X=54 AT PAX CABIN. SUMMARY OF NRC 00135: CUSP WEB FROM STA Y=655 TO STA Y=715 X=54 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2988642)Sep 26, 2023 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092707951Unknown · unknownCORROSION FOUND ON AFT CARGO LOWER DOOR JAMB BTW STA Y-954 TO Y-994 AND LONGERONS 27R AND 28R. SUMMARY OF NRC 0163: CORROSION LEVEL 2. LOWER DOOR JAMB WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 53-20-15-2R-7 REPAIR 7. (LP #2987631)Sep 26, 2023 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092607924Unknown · unknownCRACK ON EXTERNAL FUSELAGE SKIN BTW STA Y=1087 AND STR L14. SUMMARY OF NRC 00024: CRACK ON EXTERNAL FUSELAGE SKIN BTW STA Y=1087 AND STR L14 WAS REPAIRED PER ER/A 612108-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 612108-14 REV 2. REPETITIVE INSPECTIONSep 25, 2023 · N989AT · Boeing 717200 · Fuselage Main, Plate/Skin
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