# Service difficulty reports: N929AT

A list on [N929AT](https://openairdocs.org/aircraft/N929AT.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 187 reports

- [SDR DALA2026102105785](https://openairdocs.org/sdr/DALA2026102105785.md): Spar Cap · cracked · Oct 21, 2026 · N929AT · Boeing 717200 · Wing Spar
  > CRACK FOUND DURING INSPECTION OF LT WING REAR SPAR LOWER CAP AFT LEG, COMPLIED WITH ER/A 637410-14AD. (9540404) (AIRCRAFT GROUNDED).
- [SDR DALA2026102105787](https://openairdocs.org/sdr/DALA2026102105787.md): Spar · cracked · Oct 20, 2026 · N929AT · Boeing 717200 · Wing Spar
  > FOUND 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).
- [SDR DALA2026102105786](https://openairdocs.org/sdr/DALA2026102105786.md): Spar · cracked · Oct 20, 2026 · N929AT · Boeing 717200 · Wing Spar
  > FOUND CRACK AT LT WING REAR SPAR NEAR XRS = 164, COMPLIED WITH ER/A 637410-14AD. (1876109) (AIRCRAFT GROUNDED).
- [SDR DALA2026041402368](https://openairdocs.org/sdr/DALA2026041402368.md): Unknown · smoke · Apr 12, 2026 · N929AT · Boeing 717200 · Air Distribution System
  > SMOKE/FUMES IN CABIN. R & R D1- 80 CABIN HIGH LIMIT TEMP ANTICIPATOR IAW AMM 21-62 (1541379) (AIRCRAFT GROUNDED)
- [SDR DALA2026011600374](https://openairdocs.org/sdr/DALA2026011600374.md): Skin · cracked · Jan 13, 2026 · N929AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON SKIN FUSELAGE BTW L15R, BS 037 AT AFT FUSELAGE AREA. DAMAGED FUSELAGE AREA WAS REPAIRED PER PRI 631355-14 REV. (1399353)
- [SDR DALA2026011600376](https://openairdocs.org/sdr/DALA2026011600376.md): Skin · not reported · Jan 11, 2026 · N929AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DTA 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)
- [SDR DALA2026010500066](https://openairdocs.org/sdr/DALA2026010500066.md): Skin · corroded · Dec 31, 2025 · N929AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION 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)
- [SDR DALA2026010500065](https://openairdocs.org/sdr/DALA2026010500065.md): Skin · corroded · Dec 31, 2025 · N929AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION 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)
- [SDR DALA2025062504747](https://openairdocs.org/sdr/DALA2025062504747.md): Wire Splice · damaged · Jun 21, 2025 · N929AT · Boeing 717200 · Light System Wiring
  > EMERGENCY 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.
- [SDR DALA2025041502919](https://openairdocs.org/sdr/DALA2025041502919.md): Door · unsecure · Apr 15, 2025 · N929AT · Boeing 717200 · Doors
  > SHIP 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 RIG
- [SDR DALA2024120211376](https://openairdocs.org/sdr/DALA2024120211376.md): Light · inoperative · Nov 30, 2024 · N929AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY 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)
- [SDR DALA2024102910498](https://openairdocs.org/sdr/DALA2024102910498.md): Battery Pack · failed · Oct 29, 2024 · N929AT · Boeing 717200 · Emergency Lighting
  > THE 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)
- [SDR DALA2024092609433](https://openairdocs.org/sdr/DALA2024092609433.md): Connector · not seated · Sep 25, 2024 · N929AT · Boeing 717200 · Light System Wiring
  > THE 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 SE
- [SDR DALA2024061005955](https://openairdocs.org/sdr/DALA2024061005955.md): Battery Pack · inoperative · Jun 9, 2024 · N929AT · Boeing 717200 · Emergency Lighting
  > DURING 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)
- [SDR DALA2024050604958](https://openairdocs.org/sdr/DALA2024050604958.md): Heater · inoperative · May 3, 2024 · N929AT · Boeing 717200 · Windshield/Door Rain/Ice Removal
  > LT WINDSHIELD ARCING. WINDOW HEAT INOP. REPLACED LEFT FLIGHT COMPARTMENT WINDSHIELD PER B717 AMM 56-11-02 420-801. (LP #5893976)
- [SDR DALA2024010800318](https://openairdocs.org/sdr/DALA2024010800318.md): Unknown · unknown · Dec 2, 2023 · N929AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK 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 51-41-05-0
- [SDR DALA2024022002334](https://openairdocs.org/sdr/DALA2024022002334.md): Hinge Fitting · corroded · Dec 1, 2023 · N929AT · Boeing 717200 · Trailing Edge Flaps
  > CORROSION 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
- [SDR DALA2023120409898](https://openairdocs.org/sdr/DALA2023120409898.md): Unknown · unknown · Nov 30, 2023 · N929AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK 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)
- [SDR DALA2023112909799](https://openairdocs.org/sdr/DALA2023112909799.md): Unknown · unknown · Nov 28, 2023 · N929AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION 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)
- [SDR DALA2023112809761](https://openairdocs.org/sdr/DALA2023112809761.md): Unknown · unknown · Nov 28, 2023 · N929AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION 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)
- [SDR DALA2023112809752](https://openairdocs.org/sdr/DALA2023112809752.md): Unknown · unknown · Nov 26, 2023 · N929AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK 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)
- [SDR DALA2023112709725](https://openairdocs.org/sdr/DALA2023112709725.md): Unknown · unknown · Nov 25, 2023 · N929AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 #
- [SDR DALA2023112709720](https://openairdocs.org/sdr/DALA2023112709720.md): Unknown · unknown · Nov 23, 2023 · N929AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION 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 #007866
- [SDR DALA2023112709718](https://openairdocs.org/sdr/DALA2023112709718.md): Unknown · unknown · Nov 22, 2023 · N929AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK 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)
- [SDR DALA2023112209651](https://openairdocs.org/sdr/DALA2023112209651.md): Unknown · unknown · Nov 21, 2023 · N929AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK 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-
- [SDR DALA2023112209650](https://openairdocs.org/sdr/DALA2023112209650.md): Unknown · unknown · Nov 21, 2023 · N929AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK 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; TOGET
- [SDR DALA2023112109573](https://openairdocs.org/sdr/DALA2023112109573.md): Unknown · unknown · Nov 20, 2023 · N929AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK 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)
- [SDR DALA2023112009530](https://openairdocs.org/sdr/DALA2023112009530.md): Unknown · unknown · Nov 20, 2023 · N929AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK 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)
- [SDR DALA2023112009529](https://openairdocs.org/sdr/DALA2023112009529.md): Unknown · unknown · Nov 20, 2023 · N929AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS (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, 5
- [SDR DALA2023112009518](https://openairdocs.org/sdr/DALA2023112009518.md): Unknown · unknown · Nov 16, 2023 · N929AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK 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)
- [SDR DALA2023111509404](https://openairdocs.org/sdr/DALA2023111509404.md): Unknown · unknown · Nov 14, 2023 · N929AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS 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.
- [SDR DALA2023110809201](https://openairdocs.org/sdr/DALA2023110809201.md): Unknown · unknown · Nov 7, 2023 · N929AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK 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)
- [SDR DALA2023110709160](https://openairdocs.org/sdr/DALA2023110709160.md): Unknown · unknown · Nov 6, 2023 · N929AT · Boeing 717200 · Horizontal Stabilizer, Spar/Rib
  > CRACKS 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 AP
- [SDR DALA2023051803950](https://openairdocs.org/sdr/DALA2023051803950.md): Unknown · unknown · May 13, 2023 · N929AT · Boeing 717200 · Landing Gear System
  > SHIP 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
- [SDR DALA2023050203398](https://openairdocs.org/sdr/DALA2023050203398.md): Unknown · unknown · May 2, 2023 · N929AT · Boeing 717200 · Emergency Lighting
  > FOUND 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)
- [SDR DALA2023030201550](https://openairdocs.org/sdr/DALA2023030201550.md): None · none · Feb 23, 2023 · N929AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND 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 ER
- [SDR DALA2023022201320](https://openairdocs.org/sdr/DALA2023022201320.md): None · none · Feb 17, 2023 · N929AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > LONGERON 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)
- [SDR DALA2023021501182](https://openairdocs.org/sdr/DALA2023021501182.md): None · none · Feb 13, 2023 · N929AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AIRCRAFT 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)
- [SDR DALA2022110107062](https://openairdocs.org/sdr/DALA2022110107062.md): Unknown · faulted · Oct 10, 2022 · N929AT · Boeing 717200 · Emergency Lighting
  > UPON LANDING GEAR EXTENSION, ALL OF THE EMERGENCY EXIT LIGHTS EXTINGUISHED (WENT INOPERATIVE). MAINTENANCE OPERATIONALLY CHECKED THE EMERGENCY LIGHTS. ALL LIGHTS CHECKED GOOD. (LP #9580236)
- [SDR DALA2022080305324](https://openairdocs.org/sdr/DALA2022080305324.md): None · none · Jul 23, 2022 · N929AT · Boeing 717200 · Exterior Lighting
  > ---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
- [SDR DALA2022022401206](https://openairdocs.org/sdr/DALA2022022401206.md): None · none · Feb 24, 2022 · N929AT · Boeing 717200 · Emergency Lighting
  > THE 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)
- [SDR DALA2021110406788](https://openairdocs.org/sdr/DALA2021110406788.md): None · none · Oct 25, 2021 · N929AT · Boeing 717200 · Ailerons
  > CORROSION 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 SERVICE
- [SDR DALA2021102606617](https://openairdocs.org/sdr/DALA2021102606617.md): None · none · Oct 25, 2021 · N929AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION 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)
- [SDR DALA2021102606616](https://openairdocs.org/sdr/DALA2021102606616.md): None · none · Oct 25, 2021 · N929AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION 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 INSPECTIO
- [SDR DALA2021102606615](https://openairdocs.org/sdr/DALA2021102606615.md): None · none · Oct 25, 2021 · N929AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION 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 II
- [SDR DALA2021102606611](https://openairdocs.org/sdr/DALA2021102606611.md): None · none · Oct 23, 2021 · N929AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > LOOSE 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.
- [SDR DALA2021102606610](https://openairdocs.org/sdr/DALA2021102606610.md): None · none · Oct 23, 2021 · N929AT · Boeing 717200 · Fuselage Floor Panel
  > CARGO 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 5949
- [SDR DALA2021102606609](https://openairdocs.org/sdr/DALA2021102606609.md): None · none · Oct 23, 2021 · N929AT · Boeing 717200 · Fuselage Floor Panel
  > CARGO 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-
- [SDR DALA2023120710005](https://openairdocs.org/sdr/DALA2023120710005.md): Unknown · unknown · Oct 22, 2021 · N929AT · Boeing 717200 · Fuselage Main, Frame
  > FUSELAGE 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 0
- [SDR DALA2021101806407](https://openairdocs.org/sdr/DALA2021101806407.md): None · none · Oct 17, 2021 · N929AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION 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)

Next page: https://openairdocs.org/aircraft/N929AT/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N929AT/reports

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