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 DALA2023041402962Unknown · unknownCORROSION ON FLOOR SUPPORT STA Y=194 BTW X=15 AND X=44. SUMMARY OF NRC 00524: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=194 BTW X=15 AND X=44 WAS REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 51-41-02-0G. (LP #2718337)Apr 13, 2023 · N891AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023041302909Unknown · unknownCORROSION ON FLOOR SUPPORT STA Y=200 BTW X=- 8 AND X=-44 AT PAX COMPARTMENT FLOOR STRUCTURE. (W1) SUMMARY OF NRC 00362: CORROSION LEVEL 2. FLOOR SUPPORT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2717156)Apr 13, 2023 · N891AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023041302908Unknown · unknownCORROSION ON FLOOR SUPPORT STA 200 AND X=-46 AT FLIGHT COMPARTMENT FLOOR STRUCTURE. (W1) SUMMARY OF NRC 00435: CORROSION LEVEL 2. FLOOR SUPPORT STA 200 AND X=-46 AT FLIGHT COMPARTMENT FLOOR STRUCTURE WAS REPLACE PER B717-200 SRM 51-41-05-0G AND SRM 51-41-02-0GApr 13, 2023 · N891AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023041302907Unknown · unknownCRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1076 AND BTW L13-RH TO L14-RH. SUMMARY OF NRC 00041: EXTERNAL FUSELAGE SKIN STA Y=1076 AND BTW L13-RH TO L14-RH WAS REPAIRED PER PRI 607016-14 REV 1 AND ER/A 607016-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #271666Apr 12, 2023 · N891AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023041302906Unknown · unknownIN REF 429: CORROSION OUT LIMITS ON RH CENTER SEAT TRACK BTW STA 899-970 AT PAX COMPARTMENT. SUMMARY OF NRC 00516: SEAT TRACK BTW STA 899-970 AT PAX COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-01-0G. (LP #2716662)Apr 12, 2023 · N891AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2023041302905Unknown · unknownCRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1087 AND BTW L13-RH TO L14-RH. SUMMARY OF NRC 00042: EXTERNAL FUSELAGE SKIN STA Y=1087 AND BTW L13-RH TO L14-RH WAS REPAIRED PER PRI 607016-14 REV 1 AND ER/A 607016-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #271652Apr 12, 2023 · N891AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023041202863Unknown · unknownCORROSION ON CUSP WEB (INNER AND UPPER SURFACE) BTW STA 503-522, BTW STA 541-560, ALSO BTW STA 598-617 AND BTW STA 617-636, X=-57 AT PAX COMPARTMENT. (CPAX) SUMMARY OF NRC 00390: CORROSION LEVEL 2. CUSP WEB (INNER AND UPPER SURFACE) BTW STA 503-522, BTW STA 54Apr 12, 2023 · N891AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025013000728Skin · crackedFUSELAGE SKIN Y=1037, L13R TO L14R HAS CRACK REPAIR & INSPECTIONS. ACCOMPLISH ER/A 606978-14 REV A SECTION II INSPECTION WITHIN EVERY 15,000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I REPAIR. ASSOCIATED ER/A 00-606978 ADDED FOR AC 9551. (LP #0786135)Apr 11, 2023 · N891AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023041302903Unknown · unknownIN REFERANCE TO AMDS 5352-4002: DURING INSTALLATION OF TAILCONE SLIDE, THE RESTRAINT STRAPS WERE FOUND MISSING. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF THE NRC 712: STRAP (2 EAS) WApr 11, 2023 · N954AT · Boeing 717200 · Escape SlideSDR DALA2023041202862Unknown · unknownCRACK ON CUSP WEB MEMBRANE (2EA) BTW STA Y636 AND Y655, LONGERONS 18L AND 18R AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00287: CRACK ON CUSP WEB MEMBRANE (2EA) BTW STA Y636 AND Y655 LONGERONS AND 18R AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 5Apr 11, 2023 · N970AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023041102800Unknown · unknownTHE LEFT AND RIGHT FORWARD OVER WING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY B5-121 ABOVE ROW 19E PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #9494080)Apr 11, 2023 · N942AT · Boeing 717200 · Emergency LightingSDR DALA2023041102801Unknown · unknownSHIP 9569 -GEAR/DE- THE CREW NOTED THE "GEAR DOOR OPEN" MESSAGE AFTER THE LANDING GEAR WAS EXTENDED ON APPROACH INTO CLT. THEY UTILIZED THE ALTERNATE GEAR EXTENSION METHOD AND DECLARED AN EMERGENCY WITH ATC. THE LANDING WAS UNEVENTFUL EXCEPT FOR THE MAIN LANDIApr 10, 2023 · N607AT · Boeing 717200 · Landing Gear Position and WarningSDR DALA2023041002745Unknown · unknownCORROSION ON FLOOR SUPPORT BTW STA Y=200 AND Y=223 X=15 AT PAX COMPARTMENT FLOOR STRUCTURE. (W1) SUMMARY OF NRC 00365: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=200 AND Y=223 X=15 AT PAX COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND B717-200 SRM 5Apr 10, 2023 · N891AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023041002744Unknown · unknownCRACK ON INTERCOSTAL BTW STA Y617 TO STA Y636 LONGERONS 18L AND 18R AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00291: INTERCOSTAL BTW STA Y617 TO STA Y636 LONGERONS 18L AND 18R AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1. Apr 8, 2023 · N970AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023041002743Unknown · unknownCORROSION ON CUSP WEBS INNER AND UPPER SURFACE (4EA) BTW STA Y=433 AND STA Y=503, X=-57 AT PAX COMPARTMENT. (CPAX) SUMMARY OF NRC 00398: CORROSION LEVEL 2. CUSP WEB BTW STA Y=389 TO Y=503, X=-57 AT PAX COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LPApr 7, 2023 · N891AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023041002742Unknown · unknownCRACK ON FWD PAN NEAR TO BEAM 1 OF AFT CARGO CAMPARTMENT DOOR. (C2) SUMMARY OF NRC 00639: FWD PAN NEAR TO BEAM 1 OF AFT CARGO CAMPARTMENT DOOR (C2) WAS REPAIRED PER ER/A 606786-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 606786-14 REV 2. (LP #2708762)Apr 7, 2023 · N954AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023041002741Unknown · unknownCORROSION ON WEB OF AFT CUT OUT DOOR JAMB LOWER SECTION AT ENTRY DOOR (L1). SUMMARY OF NRC 00408: CORROSION LEVEL 2. REPAIR ON WEB OF AFT CUT OUT DOOR JAMB LOWER SECTION AT ENTRY DOOR (L1) WAS PERFORMED PER PRI ER/A606769-14 REV. 0 AND ER/A 606769-14 REV. ORIGApr 7, 2023 · N954AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023041002740Unknown · unknownCRACK ON FRAME STA 1037 BTW LONGERON 17LH AT CABIN PAX. SUMMARY OF NRC 00443: FRAME STA 1037 BTW LONGERON 17LH AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 4. (LP #2708504)Apr 7, 2023 · N891AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023041002739Unknown · unknownSEVERAL CORROSION POINTS ON MEMBRANE BTW STA Y=155 AND Y=200 AND FROM X=-7 TO X=-44 AT PASSENGER COMPARTMENT FLOOR STRUCTURE. (W1). SUMMARY OF NRC 00358: CORROSION LEVEL 2. MEMBRANE BTW STA Y=155 AND Y=200 AND FROM X=-7 TO X=-44 WAS REPAIRED PER B717-200 SRM 5Apr 7, 2023 · N891AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023041002738Unknown · unknownCRACKED FRAME BTW BEAMS 4 AND 5 AT MAIN ENTRY DOOR. LOCATED JUST ON HANDLE HOUSING AREA. SUMMARY OF NRC 00075: FRAME (INTERCOSTAL) BTW BEAMS 4 AND 5 AT MAIN ENTRY DOOR ON HANDLE HOUSING AREA WAS FABRICATED AND REPLACED PER DWG 9955763 REV K AND B717-200 SRM 51Apr 6, 2023 · N954AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023041002737Unknown · unknownCRACKED BEAM #6 (CENTER SECTION) AT MAIN ENTRY DOOR. SUMMARY OF NRC 00077: BEAM #6 (CENTER SECTION) AT MAIN ENTRY DOOR WAS REPAIRED PER B717-200 SRM 51-70-11-2R REPAIR 1. (LP #2706615)Apr 6, 2023 · N954AT · Boeing 717200 · Fuselage Main, FrameSDR HALA2023040600017Unknown · unknownSUPPLEMENTAL SUBMISSION TO HALA2023040600016. CORRECTION OF AIRCRAFT MANUFACTURER FROM AIRBUS TO BOEING. AFTER GEAR EXTENSION "GEAR DOOR OPEN" APPEARED AND THEN CLEARED AFTER A FEW SECONDS. REMOVED AND REPLACED MAIN GEAR DOOR ASSY PER AMM 32-34-03. OPS CHECK GApr 5, 2023 · N475HA · Boeing 717200 · Landing Gear SystemSDR HALA2023040600016Unknown · unknownAFTER GEAR EXTENSION "GEAR DOOR OPEN" APPEARED AND THEN CLEARED AFTER A FEW SECONDS. REMOVED AND REPLACED MAIN GEAR DOOR ASSY PER AMM 32-34-03. OPS CHECK GOOD. LEAK CHECK OK. OK FOR SERVICE.Apr 5, 2023 · N475HA · Boeing 717200 · Landing Gear SystemSDR DALA2023040602681Unknown · unknownCORROSION ON CUSP ANGLE BTW STA Y=170 TO Y=203 AND X=-60 BELOW SERVICE DOOR SURROUND. SUMMARY OF NRC 00553: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=170 TO Y=203 AND X=-60 BELOW SERVICE DOOR SURROUND WAS REPAIRED PER PRI 606633-14 REV.2 AND ER/A 606633-14 REV. Apr 5, 2023 · N954AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023040602680Unknown · unknownCRACKS ON PAN (INNER STRUCTURE) APROX BEAM 3 & BEAM 4 BTW STA Y=408 & Y=427 AND BEAM 5, BTW STA Y=408 & Y=427 OF AT FWD CARGO DOOR COMPARTMENT. SUMMARY OF NRC 00212: PAN (INNER STRUCTURE) APROX BEAM 3 & BEAM 4 BTW STA Y=408 & Y=427 AND BEAM 5, BTW STA Y=408 & Apr 5, 2023 · N891AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023040602679Unknown · unknownCORROSION ON CUSP WEB BTW STA 927-946 AND ON STA 807 X-57. SUMMARY OF NRC 00522: CORROSION LEVEL 2. CUSP WEB BTW STA 927-946 AND ON STA 807 X-57 WAS REPAIRED PER B717-200 SRM 53-00-55 REPAIR 4. (LP #2705390)Apr 5, 2023 · N891AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023040602678Unknown · unknownIN REF NRC 00384: CORROSION ON LH CUSP WEB BTW STA 746 TO 756, 636 TO 642, X:57. SUMMARY OF NRC 00521: CORROSION LEVEL 2. CUSP WEB BTW STA 746 TO 756, 636 TO 642, X:57 WAS REPAIRED PER B717-200 SRM 53-00-55 REPAIR 4. (LP #2704179)Apr 4, 2023 · N891AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023040502675Unknown · undertorquedSECONDARY NRC, HIDDEN DAMAGE: CRACK ON CUSP WEB BTW STA Y=655-674 LH PASSENGER CABIN (CPAX). SUMMARY OF NRC 00490: CUSP WEB BTW STA Y=655-674 LH PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #2703902)Apr 4, 2023 · N891AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023040502677Unknown · unknownSECONDARY NRC IN REF AMDS 5530-01048-02: "AA 5530-01048" AND "AD 2018-10-08". LOOSE FASTENERS OF RH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267). SUMMARY OF NRC 00428: FASTENERS HOLES COUNTER SINK AND DIAMETER ON RH VERTICAL STABILIZER LEApr 4, 2023 · N970AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2023040502676Unknown · unknownSECONDARY NRC IN REF AMDS 5530-01048-02: "AA 5530-01048" AND "AD 2018-10-08". LOOSE FASTENERS OF LH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267). SUMMARY OF NRC 00427: FASTENERS HOLES COUNTER SINK AND DIAMETER ON LH VERTICAL STABILIZER LEApr 4, 2023 · N970AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2023041102799Unknown · unknownFUSELAGE EDGE SKIN DAMAGE. LOWER FORWARD CORNER OF AFT CARGO DOOR CUT OUT. COMPLIED WITH PRI 607567-14-AD- REV 0 AND REV 1. (LP #2700709)Apr 2, 2023 · N965AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023040502673Unknown · unknownFOWARD L/H MOUNT FOR G-7 GALLEY CORRODED. FOUND AFTER GALLEY DISPLACEMENT. SUMMARY SEE NRC 089-0001:0591-2001/002 00355: REPLACED FWD L/H MOUNT AT G-7 GALLEY PER B717 AMM 25-31-70. (LP #2698677)Apr 1, 2023 · N965AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023040402599Unknown · unknownCRACK ON PAN FWD UPPER SECTION AT L1 PASSENGER DOOR. SUMMARY OF NRC 00051: PAN ON FWD UPPER SECTION AT L1 PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R, REPAIR 3, PAR. 4, FIGURE 201. (LP #2698099)Apr 1, 2023 · N891AT · Boeing 717200 · Fuselage Floor PanelSDR HALA2023040100015Unknown · unknownOVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED OVERWING EMERGENCY LIGHTS BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD. OK FOR SERVICEApr 1, 2023 · N484HA · Boeing 717200 · Emergency LightingSDR HALA2023040100014Unknown · unknownWHILE CONDUCTING T/C 717-25-060-03-01, SLIDE DEPLOYMENT SYSTEM, THE SLIDE IS UNSERVICEABLE. REMOVED AND REPLACED FWD MAIN ENTRY DOOR ESCAPE SLIDE. REF. AMM 25-61-01. NO DEFECTS NOTED.Apr 1, 2023 · N475HA · Boeing 717200 · Cabin Equipment/FurnishingsSDR DALA2023040502674Unknown · unknownAFT CARGO DOOR FRAME STRUCK BY BELT LOADER IN MSP. REMOVED DAMAGE DOUBLER, DAMAGE CONTAINED. ACCOMPLISHED HFEC INSPECTION OF CUT-OUT IAW NDT SPM 06-10-01.01. NO CRACKS NOTED. REMOVED DAMAGE SEAL DEPRESSOR. DAMAGE CONTAINED. REPAIRED SKIN PER B717 SRM 53-20-15 Mar 31, 2023 · N934AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023040402598Unknown · unknownCRACK ON PAN (INNER STRUCTURE) APROX STA Y=370 & Y=389 BEAM 5 AT FWD CARGO DOOR. SUMMARY OF NRC 00213: PAN (INNER STRUCTURE) APROX STA Y=370 & Y=389 BEAM 5 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R, REPAIR 1, PAR. 6, FIG. 201. (LP #2697134)Mar 31, 2023 · N891AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023033102476Unknown · unknownAIRCRAFT 9513, AFTER TAILCONE SLIDE REMOVAL, IT WAS FOUND UNPACKED. CORRECTIVE ACTION: TAILCONE SLIDE WAS REMOVED P/N: D29984-213 S/N: 1539 PER AMM 25-61-02-000-801 AND SERVICEABLE TAILCONE SLIDE P/N: D29984-213 S/N: 1561RP WAS REPLACED. (LP 2695495)Mar 30, 2023 · N954AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2023040402601Unknown · unknownWHILE REMOVING CEILING PANELS MAINTENANCE FOUND A BROKEN EMERGENCY LIGHT WIRE. THE WIRE WAS REPAIRED PER SWPM 20-30. THE OPERATIONAL CHECK WAS GOOD. (LP #4025352)Mar 29, 2023 · N955AT · Boeing 717200 · Emergency LightingSDR DALA2023033102475Unknown · unknownAIRCRAFT 9571, INITIAL INSPECTION: BROKEN BRACKET INSIDE ACCESS PANEL NBR 530AF ON FLAP AT LH WING. CORRECTIVE ACTION: BRACKET INSIDE ACCESS PANEL NBR 530AF ON FLAP AT LH WING WERE REPLACED PER B-717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP 2694546)Mar 29, 2023 · N928AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2023033102474Unknown · unknownAIRCRAFT 9571, INITIAL INSPECTION: CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SECTION OF DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-04-0G, B717-200 SRM 51-41-02-0G, B717-200 SRM 51-41-05-0G. AND B717-2Mar 29, 2023 · N928AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023033102473Unknown · unknownAIRCRAFT 9551, INITIAL INSPECTION: CRACK ON INNER FITTING OF BEAM # 2 IN FWD EDGE AND BEAM # 3 ON FWD EDGE APPROX BTW STA Y=954 AND STA Y=964 AT AFT CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: INNER FITTING OF BEAM # 2 IN FWD EDGE AFT CARGO COMPARTMENT DOOR WASMar 29, 2023 · N891AT · Boeing 717200 · Fuselage Main, FrameSDR HALA2023032900012Unknown · unknownSUPPLEMENTAL SUBMISSION TO HALA2023032700011. RESOLUTION UPDATED. ENG L COMP STALL ON TAKE OFF ROLL BTB ALERT DISAPPEARED WHEN ENG IDLE. BORESCOPE PER AMM 72-00-00-200-801 FOUND HPC DAMAGE INSP 5895 REMOVED AND REPLACED L/H ENG PER W/O 245768 T/C E1128-717-72-Mar 28, 2023 · N490HA · Boeing 717200 · Powerplant SystemSDR DALA2023032902432Unknown · unknownAIRCRAFT 9513, CORROSION ON INTERCOSTAL STA 814 BTW LONGERON 24 LH TO 23LH AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: INTERCOSTAL STA 814 BTW LONGERON 24 LH TO 23LH AT AFT CARGO COMPARTMENT WAS REPLACE PER B717 SRM 51-41-05-0G. AND PER DRAWING 9971095 ITEM 5Mar 28, 2023 · N954AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023032802389Unknown · unknownAIRCRAFT 9513, CRACK ON OVERWING FRAME STA Y=674 LH SIDE AT WING BOX AREA. CORRECTIVE ACTION: OVERWING FRAME STA Y=674 LH WAS REPLACED PER CARD 5310-01436-03A. (LP 2691308)Mar 28, 2023 · N954AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023032802388Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CRACK 3EA S BTW STA 1087 AND 1076 ABOVE LONG 14 RH AT EXTERNAL FUSELAGE SKIN. CORRECTIVE ACTION: CRACK 3EA S BTW STA 1087 AND 1076 ABOVE LONG 14 RH WERE REPAIRED PER PRI 606376-14 REV. 1 AND ER/A 606376-14 REV. ORIGINAL SECTIMar 27, 2023 · N954AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR HALA2023032700011Unknown · unknownATO - L ENG COMPRESSOR STALL. NEED TO INSTALL ENG S/N 13105 TO REPAIR.Mar 27, 2023 · N490HA · Boeing 717200 · Powerplant SystemSDR DALA2023032702356Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CORROSION AT CUSP ANGLE LOWER SURFACE ON STA=560 TO STA =579 ON FWD CARGO COMPARTMENT RH SIDE. CORRECTIVE ACTION: CUSP ANGLE LOWER SURFACE ON STA =560 TO STA=579 ON FWD CARGO COMPARTMENT RH SIDE WAS REPAIRED PER B717 200 SRM Mar 27, 2023 · N954AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023032702355Unknown · unknownAIRCRAFT 9513, AFTER REMOVAL WEB BTW STA Y=200 TO 208 AND STRINGERS L13 TO L18 CORROSION WAS FOUND AT CUSP ANGLE AT STA Y-200 ON STRINGER L18. CORRECTIVE ACTION: CUSP ANGLE AT STA Y-200 ON STRINGER L18 WAS REPAIRED PER B717-200 SRM 53-00-55-2 REPAIR 3 PAR. 5. Mar 27, 2023 · N954AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023032602320Unknown · unknownAIRCRAFT 9525, ROWS 1-13 EMERGENCY LTS INOP. CORRECTIVE ACTION: REPLACED 2 EMERGENCY BATTERY PACK AT LOCATION 342R, AND 398R. (LP 4112094)Mar 25, 2023 · N966AT · Boeing 717200 · Emergency Lighting
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