N924AT

Service difficulty reports · 174

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 = 'N924AT' 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 DALA2026070303894Warning Message · activatedFT BULKHEAD DOOR WARNNING ANNUNCIATION, COMPLIED WITH ER/A 635445-14. (1663962) (AIRCRAFT GROUNDED).Jun 24, 2026 · N924AT · Boeing 717200 · Door Warning SystemSDR DALA2026031901911Tire · damagedDUE TO RT NLG TIRE LOOSING TREAD CAP COUSED DENT ON RT SIDE JUST AFT OF FS 110 BETWEEN FS28R AND FS29R. CUT AND REMOVED DAMAGED AREA PER B717 SRM 53-03-01-2R-1 FIG 211 FABRICATED FILLER AND REPAIR DOUBLER, PER B717SRM 53-03-01-2R-1. (LP 1494857)Mar 14, 2026 · N924AT · Boeing 717200 · TireSDR DALA2026031701821Tire · separatedRETURNED TO ATL DUE TO RIGHT NLG TIRE RECAP SEPARATION ON TAKEOFF. DECLARED EMERGENCY AND LANDED SAFELY. REPLACED NOSE LANDING GEAR WHEEL ASSY.Mar 14, 2026 · N924AT · Boeing 717200 · TireSDR DALA2026031801859Cap · separatedDUE TO RT NLG TIRE LOOSING TREAD CAP CAUSED DENT ON RT SIDE JUST AFT OF FS110 BETWEEN FS28R AND FS29R. REPAIR PER B717 SRM 53-03-01-2R-1 (1494824)Mar 14, 2026 · N924AT · Boeing 717200 · TireSDR DALA2026020900918Blades · damagedRTO- APPROXIMATELY 25 KNOTS DUE TO A LT ENGINE COMPRESSOR STALL MESSAGE ALONG WITH AN AUDIBLE STALL. PERFORMED BORESCOPE INSPECTION OF LT ENGINE AND FOUND MULTIPLE HPC BLADES DAMAGED. REPLACED LEFT ENGINE. OPS CHECK NORMAL. (8428118)Feb 2, 2026 · N924AT · Boeing 717200 · Turbine Engine Compressor SectionSDR DALA2025122909453Acm · seizedSHIP 9575 FUME EVENT ON DESCENT. ACM WAS FOUND SEIZED, REPLACED RT ACM AND BOTH COALESCER BAG ASSY. (8047459)Dec 22, 2025 · N924AT · Boeing 717200 · Cabin Cooling SystemSDR DALA2025111908461Battery Pack · inoperativeAFT OVER WING EXIT LIGHTS OUT ON BOTH SIDES OF A/C. T/S PER B717 FIM 33-50-00-201 R/R BATTERY ASSY P/N 803949-1 PER B717 AMM 33-51-03 (6532441)Nov 19, 2025 · N924AT · Boeing 717200 · Emergency LightingSDR DALA2025110708145Door · out of adjustSHIP 9575 AFT BULKHEAD DOOR CAUTION MESSAGE ON DECENT 26000 AND CLEARED AT 7000, REAPPEARED ON LANDING. CORRECTIVE ACTION: T/S PER B717 FIM 52-70 TASK 809. FOUND "A CABIN DR" AT 86%/NEAR ADJUSTMENT RECCOMMENDED. (7816676)Nov 2, 2025 · N924AT · Boeing 717200 · DoorsSDR DALA2025110708142Proximity Sensor · faultedSHIP 9575 AFT BULKHEAD DOOR MESSAGE ILLUMINATED ON DECENT THROUGH FL180- 8000 CAME ON AGAIN DUREING APPROACH. CORRECTIVE ACTION: REMOVED AND REPLACED AFT CABIN DOOR PROX SENSOR PER B717 AMM 52- 70. (7816682)Nov 2, 2025 · N924AT · Boeing 717200 · Door Warning SystemSDR DALA2025110708148Latch · dirtySHIP 9575 1L DOOR GRIT BAR VERY DIFFICULT TO ARM SLIDE. CORRECTIVE ACTION: FOUND BOTH 1L DOOR RETENTION LATCHES STICKY AND DIRTY. CLEANED AND VERIFIED NORMAL OPERATION REF B717 AMM 25-61. (7816646)Oct 28, 2025 · N924AT · Boeing 717200 · Emergency EquipmentSDR DALA2025103107968Hinge Fitting · excess playRT WING FLAP O/B HINGE HAS EXCESSIVE PLAY. REPAIRED PER ERA/PRI 629650-14 REV. A (1274899).Oct 27, 2025 · N924AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2025063004852Brace · not reportedSHIP 9575 LH WING BRACE FITTING BEING REPLACED. CORRECTIVE ACTION: BRACE FITTING INSTALLED ON ERA622844-14AD (1047886)Jun 26, 2025 · N924AT · Boeing 717200 · Wing Main, Frame StructureSDR DALA2025063004855None · noneSHIP 9575 DTE, 624256-14AD. CORRECTIVE ACTION: ACCOMPLISH DTE FOR ERA 622844-14AD (1033944)Jun 19, 2025 · N924AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025062604791Inspection · noneSHIP 9575 AMOC, ERA 624259-14AD. CORRECTIVE ACTION: CURRENT AMOC APPROVAL IS LIMITED TO 24 MONTHS. ADDITIONAL ERA REVISION IS REQUIRED FOR AMOC APPROVAL BEYOND 17-JUN-2027 FOR ERA 624259-14AD (1033908)Jun 19, 2025 · N924AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024110510646Frame · damagedR/H FRAME ON STATION Y1133 DAMAGED NEAR LONGERON R8. REMOVED DAMAGED FRAME REF B717 SRM 53-20-07-2R PROCEDURE 1. FABRICATED, ALODINE, PRIMED, AND PAINTED REPAIR FRAME SPLICE PARTS FOR SPLICE R4-R5 LONGERON. FRAME GOES DOWN TO PRODUCTION SPLICE RIGHT PER B717 SOct 31, 2024 · N924AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024102410343Longeron · damagedLONGERON R8 AT STATION Y1133 DAMAGED. REMOVED DAMAGED R8 LONGERON 16.5 INCHES OF MATERAL SURROUNDING Y1133 REF 53-00-05-2R PROCEDURE 2. PERFORMED DAMAGE CONTAMENT HFEC IAW MDC93K0393-NDT SPM. NO FURTHER DAMAGE FOUND. FABRICATED, PAINTED, AND INSTALLED R8 REPAIOct 23, 2024 · N924AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024061606116Fire Detector · false indicationSHIP 9575 -ATB/DE- AS THE AIRCRAFT CLIMBED OUT ON DEPARTURE, THE APU FIRE WARNING (LEVEL 2) ACCOMPANIED BY THE MASTER CAUTION, ALL ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND RETURNED THE AIRCRAFT BACK TO DTW. THE LANDING WAS UNEVENTFUL AND ARFF SCANNED THJun 15, 2024 · N924AT · Boeing 717200 · Fire DetectionSDR DALA2024040504133Skin · crackedAD -- OPEN HOLE HFEC (BHEC) INDICATED CRACK 2 FASTENER HOLES BELOW EXISTING DOUBLER ON RT VERT L/E. MARKED. FOUND ON STEP 12 OF AA 5530-01048 AD 2018-10-08. SEPERATED EXTERIOR LATERS ON R/H VERT STAB FRONT SPAR CAP PER AA 5530-01048-02 STEP 13. PERFORMED OPEN Mar 29, 2024 · N924AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2024011800752Battery Pack · no testDURING SERVICE CHECK FOUND AFT OVER WING (RT/LT) EMERGENCY DOOR EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY AT STA 726 AND STA 803 IAW B717 AMM 33-51-03. PERFORMED OPERATIONAL CHECK IAW B717 AMM 33-51-03. OPERATIONAL CHJan 18, 2024 · N924AT · Boeing 717200 · Emergency LightingSDR DALA2023121910405Unknown · unknownDURING A SERVICE CHECK, MAINTENANCE FOUND THAT THE LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. THE EMERGENCY BATTERY PACK B5-230 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5549256)Dec 19, 2023 · N924AT · Boeing 717200 · Emergency LightingSDR DALA2023112009514Unknown · unknownWHILE WORKING AD TASK CARD 2540-01288-01, NOTED FWD LAV & AFT RT LAV WASTE RECEPTACLE FLAPPER DOORS WILL NOT FULLY CLOSE. ADJUSTED SPRING TENSION ON BOTH SPRINGS OF AFT LAV FLAPPER DOOR AND REPLACED BROKEN SPRING IN FWD LAV FLAPPER DOOR PER B717 AMM 25-40. OPENov 15, 2023 · N924AT · Boeing 717200 · Waste Disposal SystemSDR DALA2023110108979Unknown · unknownTHE EMERGENCY EXIT LIGHT COVER OVER ROW 29 FELL OFF. MAINTENANCE REPLACED THE EXIT LIGHT LENS. (LP #4997060)Oct 31, 2023 · N924AT · Boeing 717200 · Emergency LightingSDR DALA2023071205659Unknown · unknownAFTER REMOVAL OF THE RECHARGEABLE BATTERY ASSEMBLY, THE RECEPTACLE PINS WERE FOUND DAMAGED. THE OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REMOVED PER B717-200 AMM 33-51-06 000-801. SUMMARY OF NRC 00257: THE OVERWING EMERGENCY EVACUATION BATTERY POJul 8, 2023 · N924AT · Boeing 717200 · Emergency LightingSDR DALA2023070605439Unknown · unknownCORROSION ON FLOOR SUPPORT BELOW ACCESORY COMPARMENT DOOR BTW LBL16 AND RBL16 STA 1053. SUMMARY OF NRC 00367: CORROSION LEVEL 2. FLOOR SUPPORT BELOW ACCESORY COMPARMENT DOOR BTW LBL16 AND RBL16 STA 1053 WAS REPAIRED PER PRI 609849-14 REV 0 AND REV 1 AND ERA 60Jul 5, 2023 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023070505394Unknown · unknownCORROSION ON CUSP ANGLE (LWR SURFACE AREA) BTW STA Y=200 AND X=55 TO X=60 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00633: CORROSION LEVEL 2. CUSP ANGLE (LWR SURFACE AREA) BTW STA Y=200 AND X=55 TO X=60 AT PASSENGER CABIN FLOOR STRUCTURE WAS REPAIRED Jul 4, 2023 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023070405372Unknown · unknownCRACK ON MEMBRANE (LWR SEAT TRACK AREA) IN STA Y=220 AND X=55 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00648: MEMBARANE WAS REPLACED PER B717-200 SRM 53-00-55-0R PROCEDURE 4 REPAIR 4 AND 53-20-51-0I PROCEDURE 1. (LP #2847901)Jul 3, 2023 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023070405371Unknown · unknownDURING REMOVAL OF FLOOR SUPPORT, CRACK AND CORROSION ON CUSP WEB Y=199 TO Y=160 X54 (CPAX) WAS FOUND. SUMMARY OF NRC 00598: CORROSION LEVEL 2. CUSP WEB WAS REPAIRED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2847871)Jul 3, 2023 · N924AT · Boeing 717200 · Fuselage Structure (General)SDR DALA2023070405369Unknown · unknownCORROSION ON FLOOR SUPPORT OF MAIN ENTRANCE DOOR FROM STA Y=162 TO STA Y=194 & LBL 54 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00381: CORROSION LEVEL 2. SUPPORT WAS FABRICATED AND REPLACED PER DWG S00074, B-717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #284750Jul 3, 2023 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024022002335Hinge Fitting · corrodedCORROSION ON INBD/OUTBD ATTACHMENT POINTS OF CENTER WING FLAP HINGE FITTING STA 251.6 AT LH WING REAR SPAR. SUMMARY OF NRC 00167: CENTER WING FLAP HINGE FITTING STA 251.6 AT LH WING REAR SPAR WAS REPLACED PER B717 AMM 57-55-25. LEVEL N/A BECAUSE IS NOT A PRIMAJul 2, 2023 · N924AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2023070305302Unknown · unknownCRACK ON FRAME STA 1037 BTW LONGERON 17 LH AT CABIN. SUMMARY OF NRC 00239: FRAME STA 1037 BTW LONGERON 17 LH AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 4. (LP #2844142)Jul 1, 2023 · N924AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023063005262Unknown · unknownFLOOR PAN BTW RBL 43 AND LBL 0 BTW STA Y=160 AND STA Y=193 AT CPAX CABIN WAS FOUND WITH CORROSION DAMAGE OUT OF LIMITS PER B717-200 SRM 53-00-00-1A ALLOWABLE DAMAGE GENERAL PARAGRAPH 4. C. FIGURE 103 AND DC-MD/BOEING NDT SPM PART 4 FIG 9. (REFERENCE TO NRC 211Jun 29, 2023 · N924AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023063005259Unknown · unknownCORROSION ON FLOOR FITTING BTW STA Y=218 AND RBL 9 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00614: CORROSION LEVEL 2. FLOOR FITTING BTW STA Y=218 AND RBL 9 AT PASSENGER CABIN STRUCTURE WAS FABRICATED AND INSTALLED PER DWG 5968021 REV AND B717-200 SRM 51-41Jun 29, 2023 · N924AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023062805190Unknown · unknownCORROSION ON CUSP ANGLE FROM STA Y=168 TO STA Y=218 AND -X=54 TO -X=60 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00452: CUSP ANGLE FROM STA Y=168 TO STA Y=218 AND -X=54 TO -X=60 WAS REPAIRED PER PRI 608991-14 REV 2 AND ER/A 608991-14 REV ORIGINAL SECTJun 28, 2023 · N924AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023062705156Unknown · unknownCORROSION FOUND ON MENBRANE STA Y=200 TO STA Y=218 AND X=60 TO X=22 AT PASSENGER CABIN. SUMMARY OF NRC 00645: CORROSION LEVEL 2. MEMBRANE STA Y=200 TO STA Y=218 AND X=60 TO X=22 WAS FABRICATED AND REPLACED PER DWG 9936535-3 REV CS. (LP #2831368)Jun 23, 2023 · N924AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023062705154Unknown · unknownCORROSION ON SEAT TRACK X=-44 BTW STA 197- 217, OUT OF LIMIT. SUMMARY OF NRC 00606: CORROSION LEVEL 2. SECTION OF SEAT TRACK X=- 44 BTW STA 197-217 WAS REPLACED AND INSTALLED PER B717-200 SRM 51-40-02-0G AND 51-41-01-0G. (LP #2830727)Jun 23, 2023 · N924AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2023062705153Unknown · unknownCORROSION ON RH SEAT TRACK X-22 BTW STA Y=197 TO STA Y=266 AT PAX CABIN WAS MEASURED WITH AN ORIGINAL THICKNESS OF 0.100 IN. REMAINING THICKNESS IS 0.050 IN. THEREFORE, AREA IT IS OUT OF LIMITS PER B717-200 SRM 53-20-52-1A ALLOWABLE DAMAGE 1 PARAGRAPH 4. C. FIJun 23, 2023 · N924AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2023062705152Unknown · unknownCORROSION ON FLOOR SUPPORTS (2EA) STA Y:148 APPROX BTW -X:22 TO -X:56 AT CABIN PAX. SUMMARY OF NRC 00473: CORROSION LEVEL 2. FLOOR SUPPORT (1EA) STA Y:148 APPROX -X:56 AT CABIN PAX WAS REPLACED AND INSTALLED PER DWG 9936533 REV. CM AND B717-200 SRM 51-41-02-0GJun 23, 2023 · N924AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023062205058Unknown · unknownCORROSION ON FLOOR SUPPORT BTW LBL 5 AND RBL 5 STA Y=193 AT CPAX CABIN. SUMMARY OF NRC 00212: CORROSION LEVEL 2. FLOOR SUPPORT BTW LBL 5 AND RBL 5 STA Y=193 AT CPAX CABIN WAS REPLACED AND INSTALLED PER B717-200 SRM 51-41-05-0G. (LP #2828746)Jun 22, 2023 · N924AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023062205057Unknown · unknownSEVERAL AREAS OF CORROSION ON FLOOR TRACKS (2 EA) BTW LBL 8 AND RBL 8 BTW STA Y=148 AND STA Y=193 AT CPAX CABIN. SUMMARY OF NRC 00210: CORROSION LEVEL 2. FLOOR TRACKS (2 EA) BTW LBL 8 AND RBL 8 BTW STA Y=148 AND STA Y=193 AT CPAX CABIN WERE REPLACED AND INSTALJun 22, 2023 · N924AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2023062205055Unknown · unknownCORROSION ON FLOOR FITTING RBL11 STA Y=157 AT CPAX CABIN. SUMMARY OF NRC 00214: CORROSION LEVEL 2. FLOOR FITTING RBL11 STA Y=157 AT CPAX CABIN WAS REPLACED AND INSTALLED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2827439)Jun 21, 2023 · N924AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023062005002Unknown · unknownCORROSION ON FLOOR SUPPORT BTW L28R TO L28L STA 332 AT FWD CARGO COMPARTMENT C-1. SUMMARY OF NRC 00447: FLOOR SUPPORT BTW L28R TO L28L STA 332 AT FWD CARGO COMPARTMENT C-1 WAS REPLACED PER B717-200 SRM 51-40-02 -0G AND 51-41-02-0G. (LP #2824613)Jun 19, 2023 · N924AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023061904972Unknown · unknownCRACK ON INNER SURFACE OF CUSP WEB MEMBRANE LH STA Y=655. SUMMARY OF NRC 00223: CUSP WEB MEMBRANE LH STA Y=655 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2822605)Jun 18, 2023 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023061904971Unknown · unknownSEVERAL AREAS OF CORROSION ON FLOOR SUPPORT BTW RBL 9 AND RBL 39 STA Y=193 AT CPAX CABIN. SUMMARY OF NRC 00213: CORROSION LEVEL 2. FLOOR SUPPORT BTW RBL 9 AND RBL 39 STA Y=193 WAS REPLACE AND INSTALLED PER DWG S2929169 REV B AND B717-200 SRM 51-41-05-0G. (LP #Jun 18, 2023 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023061904967Unknown · unknownCORROSION ON GUSSET BELOW AFT ACCESSORY COMPARMENT DOOR RBL 15 STA Y=1072 AT CPAX CABIN. SUMMARY OF NRC 00378: CORROSION LEVEL 2. GUSSET BELOW AFT ACCESSORY COMPARMENT DOOR RBL 15 STA Y=1072 AT CPAX CABIN WAS REPLACED PER DWG 3925389 REV A AND B717-200 SRM 51-Jun 17, 2023 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023061904966Unknown · unknownCORROSION ON FLOOR SUPPORT BTW RBL 0 TO RBL 15 STA Y=237 AT CPAX CABIN. SUMMARY OF NRC 00218: CORROSION LEVEL 2. FLOOR SUPPORT BTW RBL 0 TO RBL 15 STA Y=237 AT CPAX CABIN WAS REPLACED PER DWG S2932222 REV A AND B717-200 SRM 51-41-02-0G. (LP #2820357)Jun 17, 2023 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023061904963Unknown · unknownCORROSION ON LH CUPS WEB IN STA Y=503 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00567: CORROSION LEVEL 2. LH CUPS WEB IN STA Y=503 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG 219. (LP #2819734)Jun 16, 2023 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023061904961Unknown · unknownCRACK ON LOWER SKIN AT CUSP WEB MEMBRANE STA 634. SUMMARY OF NRC 00149: LOWER SKIN AT CUSP WEB MEMBRANE STA 634 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG.221. (LP #2819538)Jun 16, 2023 · N924AT · Boeing 717200 · Fuselage Structure (General)SDR DALA2023061604904Unknown · unknownCORROSION ON LH CUSP WEB IN STA Y=364 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00566: CORROSION LEVEL 2. LH CUSP WEB IN STA Y=364 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 215. (LP #2818952)Jun 16, 2023 · N924AT · Boeing 717200 · Fuselage Structure (General)SDR DALA2023061504878Unknown · unknownCORROSION ON UPPER SIDE AND LOWER SIDE OF CUSP WEB BTW STA Y=200 TO STA Y=220 AT PASSENGER CABIN. SUMMARY OF NRC 00203: CORROSION LEVEL 2. CUSP WEB BTW STA Y=200 TO STA Y=220 AT PASSENGER CABIN WAS REPLACED PER DWG #9936535 REV CS AND B717-200 SRM 51-41-02-0G.Jun 14, 2023 · N924AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023061304793Unknown · unknownCORROSION ON FLOOR SUPPORT BTW L28R TO L28L STA 375 AT FWD CARGO COMPARTMENT C-1. SUMMARY CORROSION LEVEL 2. FLOOR SUPPORT BTW L28R TO L28L STA 375 AT FWD CARGO COMPARTMENT C-1 WAS REPLACED PER B717-200 SRM 51-40-02-0G. (LP #2809951)Jun 10, 2023 · N924AT · Boeing 717200 · Fuselage Floor Panel
Back to N924AT