N929AT

Service difficulty reports · 187

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 = 'N929AT' 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 DALA2026102105785Spar Cap · crackedCRACK FOUND DURING INSPECTION OF LT WING REAR SPAR LOWER CAP AFT LEG, COMPLIED WITH ER/A 637410-14AD. (9540404) (AIRCRAFT GROUNDED).Oct 21, 2026 · N929AT · Boeing 717200 · Wing SparSDR DALA2026102105787Spar · crackedFOUND CRACK EXTENDING AFT FROM ONE OF THE IB BUTE DOOR ATTACH LOCATIONS IN THE AFT FLANGE OF THE LOWER REAR SPAR CHORD, COMPLIED WITH ER/A 637410-14AD. (1876126) (AIRCRAFT GROUNDED).Oct 20, 2026 · N929AT · Boeing 717200 · Wing SparSDR DALA2026102105786Spar · crackedFOUND CRACK AT LT WING REAR SPAR NEAR XRS = 164, COMPLIED WITH ER/A 637410-14AD. (1876109) (AIRCRAFT GROUNDED).Oct 20, 2026 · N929AT · Boeing 717200 · Wing SparSDR DALA2026041402368Unknown · smokeSMOKE/FUMES IN CABIN. R & R D1- 80 CABIN HIGH LIMIT TEMP ANTICIPATOR IAW AMM 21-62 (1541379) (AIRCRAFT GROUNDED)Apr 12, 2026 · N929AT · Boeing 717200 · Air Distribution SystemSDR DALA2026011600374Skin · crackedCRACK ON SKIN FUSELAGE BTW L15R, BS 037 AT AFT FUSELAGE AREA. DAMAGED FUSELAGE AREA WAS REPAIRED PER PRI 631355-14 REV. (1399353)Jan 13, 2026 · N929AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026011600376Skin · not reportedDTA ER/A 631355-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 11-JAN-26. CONTACT LIAISON ENGINEERING. REPAIRED PER ER/A 00-631355. (1398745)Jan 11, 2026 · N929AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026010500066Skin · corrodedCORROSION ON FUSELAGE SKIN AREA BELOW FILLET PANEL RUBSTRIP UPPER SECTION BTW STA Y= 760 TO Y= 800. CORROSION ON FUSELAGE SKIN WAS ATTENDED PER SRM 51-10-04 (1378771)Dec 31, 2025 · N929AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026010500065Skin · corrodedCORROSION ON FUSELAGE SKIN( AREA UNDER FILLET PANELS) Y=590 BTW LONG 24RH, Y=615 BTW LONG 23RH-25RH, Y=901 BTW LONG 25LH-26LH , Y=586-590 LONG 24 RH , Y=588 TO Y=598 LONG 22RH-23RH. CORROSION WAS REMOVED PER BOEING 717 SRM 51- 10-04. (1378734)Dec 31, 2025 · N929AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025062504747Wire Splice · damagedEMERGENCY ESCAPE PATH MARKING SYSTEM LIGHTS INOP AT 12C AND 27C CEILING. INSP AND FOUND DAMAGED SPLICES R5-6720 @ LIGHT L2-746 & R5-6722 @ LIGHT L2-771. REPLACED SPLICES PER B717 SWPM 20-10 & WDM 33-51 -12. MEL AND PLACARD REMOVED.Jun 21, 2025 · N929AT · Boeing 717200 · Light System WiringSDR DALA2025041502919Door · unsecureSHIP 9570 -ATB/DE- AIRCRAFT HAD AN UNCOMMANDED HEAVY ROLL IN FLIGHT DURING CLIMB AFTER TAKEOFF. THE CREW DECLARED AN EMERGENCY WITH ATC AND RETURNED THE AIRCRAFT BACK TO ATL, LANDING UNEVENTFULLY. CORRECTIVE ACTION: UPON ARRIVAL, MAINTENANCE FOUND THAT THE RIGApr 15, 2025 · N929AT · Boeing 717200 · DoorsSDR DALA2024120211376Light · inoperativeEMERGENCY LIGHTS ABOVE ROWS 24-27 ARE INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY (B5-231) AND OPERATIONAL CHECK WAS GOOD IAW B717 AMM 33-51. (LP #6585094)Nov 30, 2024 · N929AT · Boeing 717200 · Emergency LightingSDR DALA2024102910498Battery Pack · failedTHE EMERGENCY LIGHTS AT LOCATION SEAT ROW 20 ARE INOPERATIVE. MAINTENANCE FOUND THAT THE BATTERY PACK AT LOCATION B5-230 WAS BAD. THE BATTERY AT LOCATION B5-230 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6658874)Oct 29, 2024 · N929AT · Boeing 717200 · Emergency LightingSDR DALA2024092609433Connector · not seatedTHE AFT EMERGENCY CEILING LIGHT REMAINED ON IN THE ARM POSITION. MAINTENANCE RESEATED THE CANNON PLUG ON THE AFT CABIN EMERGENCY LIGHT BATTERY IAW B717 AMM 33-51. PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. ALL LIGHTS OPERATE NORMALLY. OK FOR SESep 25, 2024 · N929AT · Boeing 717200 · Light System WiringSDR DALA2024061005955Battery Pack · inoperativeDURING SVC CHK FOUND R FWD AND L FWD OVERWING EXIT IDENTIFIER INOPERATIVE. T/S PER B717 WD 33-51-14, FOUND BATTERY PACK B5-118 INOPERATIVE. REPLACED BATTERY PACK PER B717 AMM 33-51, OPERATIONAL CHECK WAS GOOD. (LP #5958700)Jun 9, 2024 · N929AT · Boeing 717200 · Emergency LightingSDR DALA2024050604958Heater · inoperativeLT WINDSHIELD ARCING. WINDOW HEAT INOP. REPLACED LEFT FLIGHT COMPARTMENT WINDSHIELD PER B717 AMM 56-11-02 420-801. (LP #5893976)May 3, 2024 · N929AT · Boeing 717200 · Windshield/Door Rain/Ice RemovalSDR DALA2024010800318Unknown · unknownCRACK ON WEB (2 EA) X=11.5, Z=54 AND -X=11.5, Z=54 APPROX AT AFT CABIN BULKHEAD DOOR (CPAX). SUMMARY OF NRC 00095: WEB (2 EA) X=11.5, Z=54 AND -X=11.5, Z=54 APPROX AT AFT CABIN BULKHEAD DOOR (CPAX) WAS REPLACED PER B717-200 SRM 51-41-02-0G PAR 4 AND 51-41-05-0Dec 2, 2023 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024022002334Hinge Fitting · corrodedCORROSION WAS FOUND ON BOLTS HOUSING AT FLAP HINGE FITTING #3 AND #2. (AI). SUMMARY OF NRC 00366: LH CENTER WING FLAP HINGE FITTING WAS REPLACED PER B717-200 AMM 57-55-25 AND LH INBD WING FLAP HINGE FITTING WAS REPLACED PER B 717-200 AMM 57-55-25 AND OUTBOARD Dec 1, 2023 · N929AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2023120409898Unknown · unknownCRACK WAS FOUND ON OUTER AND INNER PAN IN LOWER AREA STA Y=974 AT AFT CARGO DOOR. SUMMARY OF NRC 00469 AFT CARGO DOOR WAS REMOVED PER B717-200 AMM 52-31-01 AND SERVICEABLE AFT DOOR WAS INSTALLED UNDER AMDS 5231-4004. (LP #0088352)Nov 30, 2023 · N929AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2023112909799Unknown · unknownCORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00053: CORROSION LEVEL 2. LOWER DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7, 51-41-02-0G, AND 51-41-05-0G. (LP #0085760)Nov 28, 2023 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112809761Unknown · unknownCORROSION ON RH CUSP ANGLE BTW STA 195 TO STA 205 AT CPAX. SUMMARY OF NRC 00308: CORROSION LEVEL 2. RH CUSP ANGLE BTW STA 195 TO STA 205 AT CPAX WAS REPAIRED PER ER/A 613282-14 REV ORGINAL, SECTION 1 PERMANENT REPAIR. (LP #0084908)Nov 28, 2023 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112809752Unknown · unknownCRACK ON WEB STA Y=200 X=-44 AT PASSENGER CABIN (W1). SUMMARY OF NRC 00507: WEB STA Y=200 X=-44 AT PASSENGER CABIN (W1) WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2, REPAIR 2 AND SRM 51-41-08-0G PAR 7 A. (LP #0081861)Nov 26, 2023 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112709725Unknown · unknownCORROSION WAS FOUND ON SEAT TRACK BTW STA 208 TO STA 218, X=-54 (RH) AT CPAX. SUMMARY OF NRC 00483: CORROSION LEVEL 2. SEAT TRACK BTW STA 208 TO STA 218, X=-54 (RH) AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5, REPAIR 5, AND 51-41-01-0G. (LP #Nov 25, 2023 · N929AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2023112709720Unknown · unknownCORROSION ON PREVIOUS REPAIR OF RH CUSP MEMBRANE BTW STA 200 TO STA 229 AT CPAX. SUMMARY OF NRC 00236: CORROSION LEVEL 2. PREVIOUS REPAIR OF RH CUSP MEMBRANE BTW STA 200 TO STA 229 AT CPAX WAS REPLACED PER B717 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1. (LP #007866Nov 23, 2023 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112709718Unknown · unknownCRACK ON L2L STA 1144 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00192: LONGERON ON L2 STA 1144 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R, PROCEDURE 2. (LP #0077910)Nov 22, 2023 · N929AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023112209651Unknown · unknownCRACK ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=674.000 RH OF 1.500 IN (REF. CARD 5310-01436-01D). SUMMARY OF NRC 00188: FRAME TAB OF THE OVERWING FRAME AT STA Y=674.000 RH WAS REPLACED PER B717-200 SRM 51-41-05-0G AND B717-200 SRM 51-41-Nov 21, 2023 · N929AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023112209650Unknown · unknownCRACK ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=696.000 RH OF 1.500 IN (REF. CARD 5310-01436-01D). SUMMARY OF NRC 00189: FRAME TAB OF THE OVERWING FRAME AT STA Y=696.000 WAS REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 51-41-02-0G; TOGETNov 21, 2023 · N929AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023112109573Unknown · unknownCRACK ON FRAME BTW L7L AND STA Y1022 AT INTERNAL AFT FUSELAGE. SUMMARY OF NRC 00252: FRAME BTW L7L AND STA Y1022 AT INTERNAL AFT FUSELAGE WAS REPAIRED PER ERA 613218-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #0074650)Nov 20, 2023 · N929AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023112009530Unknown · unknownCRACK ON FLOOR SUPPORT OF ACCESS PANEL 211PF AT COCKPIT. SUMMARY OF NRC 00290: FLOOR SUPPORT OF ACCESS PANEL 211PF AT COCKPIT WAS REPAIRED PER B717 SRM 53-00-00-2R PROCEDURE 1. (LP #0073479)Nov 20, 2023 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112009529Unknown · unknownCRACKS (2 EA) ON EXTERNAL FUSELAGE SKIN ON PREVIOUS REPAIR AREA, BTW STA 503-522 AND BTW LONG 27RH AND 29RH. SUMMARY OF NRC 00505: EXTERNAL FUSELAGE SKIN BTW STA 503-522 AND BTW LONG 27RH AND 29RH WAS REPAIRED PER B717-200 SRM 53-03-01-2R FIGURE 205 SHEET 1, 5Nov 20, 2023 · N929AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023112009518Unknown · unknownCRACK WAS FOUND ON THE CONTRAFRAME STRUCTURE OF THE AFT CABIN BULKHEAD DOOR. SUMMARY OF NRC 00362: COUNTERFRAME STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1. (LP #0068675)Nov 16, 2023 · N929AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023111509404Unknown · unknownCRACKS ON PAN AFT UPPER CORNER AT FWD CARGO DOOR. SUMMARY OF NRC 00130: PAN AFT UPPER CORNER AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1.Nov 14, 2023 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023110809201Unknown · unknownCRACK ON FRAME STA 1037 L17L AT PAX CABIN. SUMMARY OF NRC 00201: FRAME STA 1037 L17L AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-41-05-0G PAR 8 AND 53-20-07-2R PROCEDURE 4. (LP #0054034)Nov 7, 2023 · N929AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023110709160Unknown · unknownCRACKS WERE GENERATED AROUND FASTENER HOLES OF REAR SPAR WEB ON INTERNAL FACE OF LEFT HORIZONTAL STABILIZER AT STA XHS 177 APPROX, DURING REMOVAL OF FASTENERS. SUMMARY OF NRC 00372: REAR SPAR WEB ON INTERNAL FACE OF LEFT HORIZONTAL STABILIZER AT STA XHS 177 APNov 6, 2023 · N929AT · Boeing 717200 · Horizontal Stabilizer, Spar/RibSDR DALA2023051803950Unknown · unknownSHIP 9570 -ATO- THE PILOT ABORTED THE TAKEOFF AT 100 KTS DUE TO THE AIRCRAFT DRIFTING LEFT OF CENTER LINE. CORRECTIVE ACTION: MAINTENANCE PERFORMED A HIGH ENERGY STOP INSPECTION AND ACCOMPLISHED CHECKS OF ALL OF THE FLIGHT CONTROLS. NO DEFECTS WERE FOUND. (LP May 13, 2023 · N929AT · Boeing 717200 · Landing Gear SystemSDR DALA2023050203398Unknown · unknownFOUND MID CABIN OVERHEAD EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY EMERGENCY EXIT LIGHT BATTERY IAW B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. (LP #4773170)May 2, 2023 · N929AT · Boeing 717200 · Emergency LightingSDR DALA2023030201550None · noneFOUND SKIN DAMAGE AT C-2 DOORWAY JAMB EDGE AT DOOR CUT OUT SURROUND AREA BELOW DOOR STOP #2. SUMMARY SEE NRC 003-0001:0514-2001/003 00003: COMPLIED WITH ER/A PRI 606111-14 REV'S "0","1","2","3" AND ALL REPAIR INSTRUCTIONAL STEPS ARE COMPLETED, ENSURED FINAL ERFeb 23, 2023 · N929AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023022201320None · noneLONGERON TEMPORARY REPAIR INSTALLED AT 25R BETWEEN STA 1022 AND STA 1042. COMPLIED WITH LONGERON SPLICE REPAIR PER B717 SRM 53-00-05-2R REPAIR 2 LONGERON REPAIR. A/C WAS DAMAGED BY BELTLOADER ON 13FEB22, REF LOG PAGE 9046786. (LP #2633018)Feb 17, 2023 · N929AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023021501182None · noneAIRCRAFT FUSELAGE DAMAGED BY BELT LOADER STA 1002 STR 25R. C/W FUSELAGE TEMPORARY SKIN REPAIR STA 1002 STR 25R PER ERA 605962-14 REV A SECTION 1. RII C/W. ASSOCIATED ER/A 14-605962 ADDED FOR AC 9570. (LP #9046786)Feb 13, 2023 · N929AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2022110107062Unknown · faultedUPON LANDING GEAR EXTENSION, ALL OF THE EMERGENCY EXIT LIGHTS EXTINGUISHED (WENT INOPERATIVE). MAINTENANCE OPERATIONALLY CHECKED THE EMERGENCY LIGHTS. ALL LIGHTS CHECKED GOOD. (LP #9580236)Oct 10, 2022 · N929AT · Boeing 717200 · Emergency LightingSDR DALA2022080305324None · none---SUPPLEMENTAL INFORMATION: ATL 10AUG22 INSTALLED LEFT LOGO LIGHT PER B717 AMM 33-41. OPS CHECK GOOD. THIS CLEARS CDL. PLACARDS REMOVED. M PROCEDURES REVERSED. --- THE LEFT LOGO LIGHT IS MISSING FROM THE AIRCRAFT. *** CONTRACT MAINTENANCE EVENT - OCM: 250470 Jul 23, 2022 · N929AT · Boeing 717200 · Exterior LightingSDR DALA2022022401206None · noneTHE AFT EMERGENCY OVERWING DOOR EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER B717 AMM 33-51-04. OPERATIONAL CHECKS IS NOW GOOD. (LP #8542605)Feb 24, 2022 · N929AT · Boeing 717200 · Emergency LightingSDR DALA2021110406788None · noneCORROSION ON UPPER SKIN OF LH AILERON (INBOARD AREA). SUMMARY NRC #00213: CORROSION ON UPPER SKIN OF LH AILERON (INBOARD AREA) WAS TREATED. THE AREA REWORKED IS OUT OF LIMITS PER B717 SRM 57-00-00-1A. THE AILERON WAS REMOVED PER B717 AMM 27-10-01 AND A SERVICEOct 25, 2021 · N929AT · Boeing 717200 · AileronsSDR DALA2021102606617None · noneCORROSION ON LOWER DOOR JAMB PAN BTW STA 954 -994 AT AFT CARGO COMPARMTENT. SUMMARY OF NRC 00067: CORROSION LEVEL 2, LOWER DOOR JAMB PAN BTW STA 954-994 AT AFT CARGO COMPARMTENT WAS REPAIRED PER B717 SRM 53-20-15-2R. PROCEDURE 7. REPAIR 7. (LP #1995219)Oct 25, 2021 · N929AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2021102606616None · noneCORROSION ON FRAME AT STA Y=927 AND L-30, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00222: CORROSION LEVEL 2, FRAME AT STA Y=927 AND L-30 WAS REPAIRED PER B-717-200 SRM 53-20-07-2R REPAIR 3 AND ER/ A 594977-14 REV. ORIGINAL. ACCOMPLISH SECTION II INITIAL INSPECTIOOct 25, 2021 · N929AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2021102606615None · noneCORROSION ON FRAME AT STA Y=908 AND L-29L TO L-29R, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00189: CORROSION LEVEL 2 FRAME AT STA Y=908 AND L-29L TO L-29R WAS REPAIRED PER B-717-200 SRM 53-20-07-2R REPAIR 3 AND ER/A 594972-14 REV. ORIGINAL. ACCOMPLISH SECTION IIOct 25, 2021 · N929AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2021102606611None · noneLOOSE FASTENER ON CLIP STA Y=1152 AND LONG 1L AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00249: PERMANENT REPAIR WAS PERFORMED ON CLIP STA Y=1152 AND LONG 1L AT AFT ACCESSORY COMPARTMENT PER ETI-17-21- 017 REV. 2 AND ER/A 594962-14 REV. ORIGINAL, SECTION I. Oct 23, 2021 · N929AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2021102606610None · noneCARGO DOOR JAMB WEB WAS FOUND CRACKED ON FRAME AT STA Y=954 AND BETWEEN L-29R TO L-27R, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00220: FRAME AT STA Y=954 AND BETWEEN L-29R TO L- 27R, AFT CARGO COMPARTMENT WAS REPAIRED PER ETI-17-21-026 REV. ORIGINAL AND ERA 5949Oct 23, 2021 · N929AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2021102606609None · noneCARGO DOOR JAMB WEB WAS FOUND CRACKED ON INTERCOSTAL AT STA Y=974 AND BETWEEN L-29R TO L-28R, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00221: REPAIR WAS PERFOMED ON INTERCOSTAL AT STA Y=974 AND BETWEEN L-29R TO L-28R, AFT CARGO COMPARTMENT. PER B717 SRM 51-70-11-Oct 23, 2021 · N929AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023120710005Unknown · unknownFUSELAGE FRAMES STA 954.0 BETWEEN L- 28R & L-29R IS CRACKED. REPAIR PER SECTION I IS TIME LIMITED AND REQUIRES REPLACEMENT WITH SECTION II PERMANENT REPAIR. ACCOMPLISH ER/A 594963-14, SECTION II PERMANENT REPAIR WITHIN 24 MONTHS FROM 19OCT21. ASSOCIATED ER/A 0Oct 22, 2021 · N929AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2021101806407None · noneCORROSION ON LONGERON L-29L AT STA Y=946 AND Y=954, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00244: CORROSION LEVEL 2, LONGERON L-29L AT STA Y=946 AND Y=954 AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R. (LP #1986109)Oct 17, 2021 · N929AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
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