# Service difficulty reports: N996AT

A list on [N996AT](https://openairdocs.org/aircraft/N996AT.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 5 · 203 reports

- [SDR DALA2026061603618](https://openairdocs.org/sdr/DALA2026061603618.md): Battery Pack · inoperative · Jun 16, 2026 · N996AT · Boeing 717200 · Emergency Lighting
  > AIRCRAFT 9542, AFT EMERGENCY EXIT SIGN AND TAIL COMP EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY BATTERY PACK B5-260 IAW AMM 33-51. TEST OK. (LP 8630750 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026052903251](https://openairdocs.org/sdr/DALA2026052903251.md): Doubler · gouged · May 25, 2026 · N996AT · Boeing 717200 · Wing, Plate/Skin
  > GOUGES (2 EAS) ON FIXED LEADING EDGE PREVIOS REPAIR DOUBLER BTW XOS 384.0 TO XOS 386.0 APPROX AT RT WING. REPAIRED PER PRI 634250-14 (1611243) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502827](https://openairdocs.org/sdr/DALA2026050502827.md): Slide · wrong part · May 2, 2026 · N996AT · Boeing 717200 · Escape Slide
  > TARP WRONG INSTALLED ON TAIL CONE SLIDE DEPLOYMENT AT AFT ACCESSORIES COMPARTMENT. REPLACED AT TAIL CONE SLIDE (1573474) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502816](https://openairdocs.org/sdr/DALA2026050502816.md): Skin · cracked · May 1, 2026 · N996AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL FUSELAGE SKIN BS Y= 1076 BTW LONG 13RH & 14RH. CORRECTIVE ACTION: REPAIR AND PRI 633992-14 (1571512) (AIRCRAFT GROUNDED)
- [SDR DALA2026042102513](https://openairdocs.org/sdr/DALA2026042102513.md): Spar Cap · mechanic error · Apr 13, 2026 · N996AT · Boeing 717200 · Wing Spar
  > RIGHT WING, TRAILING EDGE LOWER SPAR CAP MISDRILLED HOLES. REPAIRED PER ERA 608531-14. (1542895) (AIRCRAFT GROUNDED)
- [SDR DALA2026031701819](https://openairdocs.org/sdr/DALA2026031701819.md): Engine · bird ingestion · Mar 14, 2026 · N996AT · Boeing 717200 · Engine (Turbine/Turboprop)
  > IFSD - APPROXIMATELY 13 MINUTES FROM LANDING IN STL, BIRD STRIKE RIGHT ENGINE WITH VIBES. CREW PERFORMED IFSD. REPLACED #2 ENGINE.
- [SDR DALA2026021901204](https://openairdocs.org/sdr/DALA2026021901204.md): Power Supply · inoperative · Feb 15, 2026 · N996AT · Boeing 717200 · Emergency Lighting
  > AIRCRAFT 9542, AFT WALKWAY EMERG. LIGHTS INOP. FOUND BATTERY POWER SUPPLY FAULTY AT B5-260 REMOVED AND REPLACED POWER SUPPLY PER B717 AMM 33-51. OPS CHECKS GOOD. (LP 8281713)
- [SDR DALA2024102110285](https://openairdocs.org/sdr/DALA2024102110285.md): Battery · malfunctioned · Oct 19, 2024 · N996AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ON TOP OF TAILCONE IS INTERMITTENTLY FLASHING. MAINTENANCE REPLACED THE BATTERY AND BATTERY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. AIRCRAFT OK FOR SERVICE. (LP #6449074)
- [SDR DALA2024072507458](https://openairdocs.org/sdr/DALA2024072507458.md): Power Supply · inoperative · Jul 24, 2024 · N996AT · Boeing 717200 · Emergency Lighting
  > INTERIOR OVERWING EMERGENCY LIGHT LEFT & RIGHT LOWER LIGHTS ARE INOPERATIVE. REPLACED POWER SUPPLY PER B717 AMM 33-51 AT LOCATION B5-119. OPERATIONAL CHECK OK. (LP #6208055)
- [SDR DALA2024051305135](https://openairdocs.org/sdr/DALA2024051305135.md): Pump · leaking · May 12, 2024 · N996AT · Boeing 717200 · Hydraulic Pump (Electric/Engine), Main
  > SHIP 9542 -HYD/DE- LOSS OF RIGHT HYDRAULIC SYSTEM ON APPROACH REQUIRING A MANUAL GEAR EXTENSION. CORRECTIVE ACTION: MAINTENANCE DETERMINED THAT THE HYDRAULIC REVERSABLE PUMP (PTU) WAS LEAKING INTERNALLY AND REPLACED IT ALONG WITH THE RIGHT SYSTEM RESERVOIR. (L
- [SDR DALA2024042304666](https://openairdocs.org/sdr/DALA2024042304666.md): Not Reported · corroded · Apr 22, 2024 · N996AT · Boeing 717200 · Horizontal Stabilizer Structure
  > -AD- CORRORION WAS FOUND ON LH HORIZ STAB BARREL NUT HOLE #26. SUMMARY OF NRC 00719: CORROSION LEVEL 2. LH HORIZ STAB BARREL NUT HOLE #26 WAS REPAIRED PER ER/A 616773-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 616773-14 REV 1. ASSOCIATED ER/A 14-616
- [SDR DALA2024042204626](https://openairdocs.org/sdr/DALA2024042204626.md): Skin · damaged · Apr 21, 2024 · N996AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > -AD- CRACK ON SKIN DRILL FOUND. SUMMARY OF NRC 00852: FUSELAGE SKIN STA 1133 BTW L1-L3LH WAS REPAIRED PER ER/A 617266-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617266-14 REV 5. ASSOCIATED ER/A 14-617266 ADDED FOR AC 9542. (LP #0305492)
- [SDR DALA2024042204623](https://openairdocs.org/sdr/DALA2024042204623.md): Unknown · cracked · Apr 21, 2024 · N996AT · Boeing 717200 · Horizontal Stabilizer Structure
  > CRACK ON LOWER MATING SURFACE BTW ACCESS 330XB AND ELEVATOR LEADING EDGE STA XE=171 AT RH ELEVATOR. SUMMARY OF NRC 00385: LOWER MATING SURFACE BTW ACCESS 330XB AND ELEVATOR LEADING EDGE STA XE=171 OF RH ELEVATOR WAS REPAIRED PER ER/A 616815-14 REV ORIGINAL SEC
- [SDR DALA2024042204621](https://openairdocs.org/sdr/DALA2024042204621.md): Spar Cap · damaged · Apr 19, 2024 · N996AT · Boeing 717200 · Wing Spar
  > PERFORM PERMANENT REPAIR ON RH WING TRAILING EDGE LOWER SPAR CAP DUE TO MISDRILLED HOLES WITH TIME LIMITED REPAIR. SUMMARY OF NRC 00856: RH WING TRAILING EDGE LOWER SPAR CAP WAS REPAIRED PER PRI 608531-14 REV 1 AND ERA #608531-14 REV C. SECTION II: TIME LIMITE
- [SDR DALA2024041804527](https://openairdocs.org/sdr/DALA2024041804527.md): Vane · debonded · Apr 16, 2024 · N996AT · Boeing 717200 · Trailing Edge Flaps
  > SEVEN DISBONDS WERE FOUND ON LH AFT MOVABLE VANE LOWER SKIN, 1) LENGTH 1.550IN AND WIDTH 1.125IN, 2) LENGTH 1.000IN AND WIDTH 0.850IN, 3) LENGTH 1.250IN AND WIDTH 0.850IN, 4) LENGTH 1.250IN AND WIDTH 1.250IN, 5) LENGTH 1.250IN AND WIDTH 1.250IN, 6) LENGTH 1.37
- [SDR DALA2024041804526](https://openairdocs.org/sdr/DALA2024041804526.md): Guide Vane · damaged · Apr 15, 2024 · N996AT · Boeing 717200 · Trailing Edge Flaps
  > DAMAGE T DURING TEST OF FLIGHT SPOILER ACTUATOR. FLAPS WAS RETRACTED AND RH FLAP GUIDE VANE WAS DENTED WITH INDB FLAP INGE SUPPORT BRACKET (HINGE FAIRING REMOVAL). SUMMARY OF NRC 00077: RH FLAP GUIDE VANE WAS REPAIRED PER PRI 616775-14 REV 2 AND ER/A 616775-14
- [SDR DALA2024041504426](https://openairdocs.org/sdr/DALA2024041504426.md): Beam · cracked · Apr 13, 2024 · N996AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON BEAM #5 NEAR TO AFT HINGE AT FWD CARGO COMPARTMENT DOOR C1. SUMMARY OF NRC 00221: BEAM #5 NEAR TO AFT HINGE AT FWD CARGO COMPARTMENT DOOR C1 WAS REPAIRED PER PRI 616929-14 REV 1 AND ERA 616929-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER
- [SDR DALA2024041504421](https://openairdocs.org/sdr/DALA2024041504421.md): Angle · corroded · Apr 13, 2024 · N996AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND IN ANGLE OVER CENTER WING UPPER SKIN STA Y=748 X=0. SUMMARY OF NRC 00803: CORROSION LEVEL 2. CORROSION IN ANGLE OVER CENTER WING UPPER SKIN STA Y=748 X=0 WAS REPAIRED PER PRI 616932-14 REV 4 AND ER/A 616932-14 REV ORIGINAL SECTION I: PERMAN
- [SDR DALA2024041504423](https://openairdocs.org/sdr/DALA2024041504423.md): Frame · damaged · Apr 12, 2024 · N996AT · Boeing 717200 · Fuselage Main, Frame
  > ELONGATE HOLES AND WRONG DRILLED ON FRAME STA Y=994 BTW LONGERONS 26RH/27RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00674: FRAME STA Y=994 BTW LONGERONS 26RH/27RH AT AFT CARGO COMPARTMEN WAS REPAIRED PER PRI 616818-14 REV 2 AND ERA 616818-14 REV ORIGINAL, SEC
- [SDR DALA2024041204361](https://openairdocs.org/sdr/DALA2024041204361.md): Pan · corroded · Apr 11, 2024 · N996AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER PAN AREA AT AFT CARGO DOOR JAMB. SUMMARY OF NRC 0070: CORROSION LEVEL 2. LOWER PAN AREA AT AFT CARGO DOOR JAMB WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G AND WAS REPAIRED PER B717-200 SRM 53-00-15-2R PROCEDURE 1. (LP #0289228)
- [SDR DALA2024041204360](https://openairdocs.org/sdr/DALA2024041204360.md): Doubler · corroded · Apr 11, 2024 · N996AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL PRODUCTION DOUBLER BTW PAN AND FUSELAGE SKIN AT AFT CARGO COMPARTMENT LOWER DOOR JAMB. SUMMARY OF NRC 0273: CORROSION LEVEL 2. INTERNAL PRODUCTION DOUBLER BTW PAN AND FUSELAGE SKIN AT AFT CARGO COMPARTMENT LOWER DOOR JAMB WAS REPAIRED PER
- [SDR DALA2024041004262](https://openairdocs.org/sdr/DALA2024041004262.md): Skin · cracked · Apr 9, 2024 · N996AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL FUSELAGE SKIN LOCATED Y=1022 BETWEEN L-9L AND L-8L. SUMMARY OF NRC 00496: CRACK ON EXTERNAL FUSELAGE SKIN LOCATED Y=1022 BETWEEN L-9L AND L-8L WAS REPAIRED PER PRI 616777-14 REV 1 AND ERA 616777-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR.
- [SDR DALA2024041004263](https://openairdocs.org/sdr/DALA2024041004263.md): Screw · damaged · Apr 8, 2024 · N996AT · Boeing 717200 · Horizontal Stabilizer Structure
  > AD - BURRS WERE FOUND ON THE THREADS OF THE ACME SCREW AT THE HORIZONTAL STABILIZER. SUMMARY NRC 00437: HORIZONTAL STABILIZER JACKSCREW ASSEMBLY WAS REPLACED UNDER AMDS 2740-01114-05. (LP #0282538)
- [SDR DALA2024040504135](https://openairdocs.org/sdr/DALA2024040504135.md): Skin · dented · Apr 4, 2024 · N996AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DENT ON EXTERNAL FUSELAGE SKIN STA Y=588 AND LONG 30 ABOVE BUTT SPLICE. SUMMARY OF NRC 00338: DENT ON EXTERNAL FUSELAGE SKIN STA Y=588 AND LONG 30 ABOVE BUTT SPLICE WAS REPAIRED PER PRI 616805-14 REV 1 AND ER/A 616805-14 REV ORIG. SECTION I. ACCOMPLISH SECTION
- [SDR DALA2024040404051](https://openairdocs.org/sdr/DALA2024040404051.md): Web · corroded · Apr 4, 2024 · N996AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON L1 DOOR JAMB WEB STA Y=200-207, BTW LONG 17LH-18LH. SUMMARY OF NRC 00651: CORROSION LEVEL 2. CORROSION ON L1 DOOR JAMB WEB STA Y=200-207, BTW LONG 17LH-18LH WAS REPAIRED PER PRI 616779-14 REV 1 AND ER/A 616779-14 REV ORIGINAL SECTION I: PERMANENT
- [SDR DALA2024040103937](https://openairdocs.org/sdr/DALA2024040103937.md): Longeron · corroded · Mar 30, 2024 · N996AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION WAS FOUND ON LONGERON 22LH FROM STA 1017/STA 1049 AND LONGERON ENDS 22LH AND 24 LH STA 1053. ALSO CORROSION ON SHIMS OF LONGERONS 22LH, 23LH, AND 24LH BTW STA 1037-1042 AND FILLERS AT STA 1053 AND STR 21LH/STR 23LH AT AFT CARGO COMPARTMENT (C2). SUMM
- [SDR DALA2024040504132](https://openairdocs.org/sdr/DALA2024040504132.md): Longeron · out of limits · Mar 29, 2024 · N996AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > THICKNESS MEASUREMENT WAS ACCOMPLISHED ON LONGERON L-23L BETWEEN Y=994 AT AFT CARGO COMPARTMENT. ORIGINAL THICKNESS IS 0.080 IN. REMAINING THICKNESS IS 0.043 IN. THEREFORE, IT IS OUT OF LIMITS. SUMMARY OF NRC 829: ON LONGERON L-23L BETWEEN Y=994 AT AFT CARGO W
- [SDR DALA2025103107967](https://openairdocs.org/sdr/DALA2025103107967.md): Tab · corroded · Mar 28, 2024 · N996AT · Boeing 717200 · Rudder, Tab Structure
  > CORROSION ON SKIN LT & RT SIDE AT RUDDER TAB. REPLACED BY SERVICIABLE RUDDER CONTROL TAB (0266679).
- [SDR DALA2024040103934](https://openairdocs.org/sdr/DALA2024040103934.md): Floor Support · corroded · Mar 28, 2024 · N996AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH FLOOR SUPPORT BTW STA 200-214 AND X=-56 PAX CABIN (W1). SUMMARY OF NRC 00464: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 200-214 AND X=-56 PAX CABIN WAS REPLACED AND INSTALLED PER B717-200 SRM 51-41-08-0G AND 51-41-01-0G. (LP #0267742)
- [SDR DALA2024032703842](https://openairdocs.org/sdr/DALA2024032703842.md): Pan · cracked · Mar 27, 2024 · N996AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS ON PAN FWD END OF BEAM 5 AND BEAM 3 AT FWD CARGO COMPARTMENT DOOR C1. SUMMARY OF NRC 00222: DAMAGED SECTIONS OF PAN FWD END OF BEAM 5 AND BEAM 3 AT FWD CARGO COMPARTMENT DOOR C1 WERE REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #02641
- [SDR DALA2024032703841](https://openairdocs.org/sdr/DALA2024032703841.md): Floor Support · corroded · Mar 27, 2024 · N996AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON L/R FLOOR SUPPORTS BTW STA 160-200 AT X=7 AND X=-7 PAX CABIN (W1). SUMMARY OF NRC 00468: CORROSION LEVEL 2. L/R FLOOR SUPPORTS BTW STA 160-200 AT X=7 AND X=-7 PAX CABIN (W1) WERE REPLACED PER B717-200 SRM 51-41-01-0G. (LP #0264025)
- [SDR DALA2024032703838](https://openairdocs.org/sdr/DALA2024032703838.md): Window Frame · cracked · Mar 25, 2024 · N996AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK WAS FOUND ON FRAME ON UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00802: UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1 PAR 5 FIG 201 OPTION 2 FLAG NOTE E AND F. (LP #0262080)
- [SDR DALA2024032203636](https://openairdocs.org/sdr/DALA2024032203636.md): Frame · corroded · Mar 22, 2024 · N996AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION WAS FOUND ON PREVIOUS REPAIR SPLICES AND FRAME, STA Y=927 LONGERON 29LH TO 29RH AT AFT CARGO COMPARMENT. SUMMARY OF NRC S/N 00339: CORROSION LEVEL 2. FRAME STA Y=927 LONGERON 29LH TO 29RH AT AFT CARGO COMPARMENT CORROSION WAS REMOVED PER B717-200 51-
- [SDR DALA2024032203634](https://openairdocs.org/sdr/DALA2024032203634.md): Beam · cracked · Mar 21, 2024 · N996AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CRACK ON BEAM 1 LH EDGE AT AFT CABIN PRESSURE BULKHEAD. SUMMARY OF NRC 00097: WEB WAS REPLACED PER B717-200 SRM 51-41-05-0G, 51-41-02-0G, AND DWG 9915565 REV BD. (LP #0256085)
- [SDR DALA2024032203630](https://openairdocs.org/sdr/DALA2024032203630.md): Cusp Web · cracked · Mar 21, 2024 · N996AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON RH CUSP WEB STA X=-56 TO -60 AND Y=1012 AT PASSENGER CABIN. SUMMARY OF NRC 00514: RH CUSP WEB STA X=-56 TO -60 AND Y=1012 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R. (LP #0255600)
- [SDR DALA2024032103590](https://openairdocs.org/sdr/DALA2024032103590.md): Longeron · cracked · Mar 20, 2024 · N996AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 17LH STA 1022 PAX CABIN. SUMMARY OF NRC 00352: LONGERON 17LH STA 1022 PAX CABIN WAS REPAIRED PER B717 SRM 53-00-05-2R. (LP #0254278)
- [SDR DALA2024032103589](https://openairdocs.org/sdr/DALA2024032103589.md): Frame · cracked · Mar 20, 2024 · N996AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED LH FRAME STA 1037 AT LONG 17LH PAX CABIN. SUMMARY OF NRC 00449: LH FRAME STA 1037 AT LONG 17LH PAX CABIN WAS REPAIRED PER B717 SRM 53-20-07-2R PROCEDURE 4. (LP #0254275)
- [SDR DALA2024032103588](https://openairdocs.org/sdr/DALA2024032103588.md): Longeron · cracked · Mar 20, 2024 · N996AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 17RH STA 1022 PAX CABIN. SUMMARY OF NRC 00353: LONGERON 17RH STA 1022 PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #0254033)
- [SDR DALA2024032103587](https://openairdocs.org/sdr/DALA2024032103587.md): Doubler · corroded · Mar 20, 2024 · N996AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON FWD AND AFT PREVIOUS REPAIR DOUBLER OF FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 0069: CORROSION LEVEL 2. FWD AND AFT DOUBLERS OF FWD CARGO COMPARTMENT DOOR JAMB WERE REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 6 PAR. 5. (LP #0253957)
- [SDR DALA2024032103585](https://openairdocs.org/sdr/DALA2024032103585.md): Pan · cracked · Mar 19, 2024 · N996AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON SPLICE AND PAN NEAR TO AFT TORQUE TUBE AREA AT FWD CARGO COMPARTMENT DOOR C1. SUMMARY OF NRC 00219: SPLICE (REPAIR DOUBLER) NEAR TO AFT TORQUE TUBE AREA AT FWD CARGO COMPARTMENT DOOR C1 WAS REPLACED PER B717-200 SRM 52-30-02-2R PROCEDURE 4 REPAIR 4. (
- [SDR DALA2024032103578](https://openairdocs.org/sdr/DALA2024032103578.md): Skin · dented · Mar 17, 2024 · N996AT · Boeing 717200 · Trailing Edge Flaps
  > DENTS OUT LIMITS WERE FOUND ON REVALUATION DENTS OF LOWER SKIN FWR MOVABLE VANE FLAP AT LH WING. SUMMARY OF NRC 00659: PERMANENT REPAIR WAS PERFORMED ON FWD MOVABLE FLAP VANE (LOWER SKIN) OF LH WING PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR 4. (LP
- [SDR DALA2024032103572](https://openairdocs.org/sdr/DALA2024032103572.md): Cusp Web · corroded · Mar 15, 2024 · N996AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP WEB BTW STA X=-56 TO -60 STA 568 (BELOW) AT PASSENGER CABIN. SUMMARY OF NRC 00749: CORROSION LEVEL 2. RH CUSP WEB BTW STA X=- 56 TO -60 STA 568 (BELOW) AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIGURE 215. (LP #0246687
- [SDR DALA2024032103571](https://openairdocs.org/sdr/DALA2024032103571.md): Cusp Web · cracked · Mar 15, 2024 · N996AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON RH CUSP WEB STA X=-56 TO -60 AND Y=660 AT PASSENGER CABIN. SUMMARY OF NRC 00513: RH SECTION CUSP WEB WAS FABRICATED AND REPAIRED ON STA X=-56 TO -60 AND Y=660 AT PASSENGER CABIN PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, FIGURE 223. (LP #0246
- [SDR DALA2024032103570](https://openairdocs.org/sdr/DALA2024032103570.md): Cusp Web · cracked · Mar 15, 2024 · N996AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON RH CUSP WEB STA X=-56 AND Y=636-655 ALSO CORROSION AND MISSING FASTENERS AT PASSENGER CABIN. SUMMARY OF NRC 00512: CORROSION LEVEL 2. RH CUSP WEB STA X=-56 AND Y=636-655 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR
- [SDR DALA2024030803186](https://openairdocs.org/sdr/DALA2024030803186.md): Release Cable · out of limits · Mar 4, 2024 · N996AT · Boeing 717200 · Aerodynamic Fairings
  > THE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS TORN BEYOND ALLOWABLE LIMITS. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE TAILCONE JETTISON KEVLAR CABLE REF
- [SDR DALA2022110807208](https://openairdocs.org/sdr/DALA2022110807208.md): None · none · Nov 7, 2022 · N996AT · Boeing 717200 · Emergency Lighting
  > ON THE SERVICE CHECK, FOUND AFT F/A JUMPSEAT CEILING EMERGENCY LIGHT OUT AND EXIT SIGN NEAR FLOOR WITH LAMPS OUT. MAINTENANCE RELAMPED THE CEILING EMERGENCY LIGHT AT AFT F/A JUMPSEAT AND EXIT SIGN AT SAME LOCATION NEAR FLOOR PER B717 AMM 33-51. OPERATIONAL TES
- [SDR DALA2022110807206](https://openairdocs.org/sdr/DALA2022110807206.md): None · none · Nov 7, 2022 · N996AT · Boeing 717200 · Emergency Lighting
  > ON SERVICE CHECK, FOUND BOTH AFT OVERWING EMERGENCY EXIT SIGNS WITH MULTIPLE LAMPS OUT. MAINTENANCE RELAMPED BOTH OF THE OVER WING EMERGENCY EXIT LOWER SIGNS PER B717 AMM 33- 51. OPERATIONAL TEST OK. (LP #9705710)
- [SDR DALA2022091906175](https://openairdocs.org/sdr/DALA2022091906175.md): None · none · Sep 18, 2022 · N996AT · Boeing 717200 · Emergency Lighting
  > DURING SERVICE CHECK THE RIGHT HAND EMERGENCY LIGHTS IN THE FIRST CLASS ROWS WAS DISCOVERED TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY AND POWER SUPPLY (STA 39A) PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVI
- [SDR DALA2022060103808](https://openairdocs.org/sdr/DALA2022060103808.md): Lens · missing · May 31, 2022 · N996AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT ROW 29. MAINTENANCE REPLACED THE MISSING AFT COVER PER B717 AMM 33-51. OK FOR SERVICE. (LP #2258245)
- [SDR DALA2022060103809](https://openairdocs.org/sdr/DALA2022060103809.md): Pseu · fault message · May 28, 2022 · N996AT · Boeing 717200 · Landing Gear Position and Warning
  > SHIP 9542 - THE FLIGHT CREW DECLARED AN EMERGENCY DURING APPROACH DUE TO A PSEU FAILURE MESSAGE. A GO-AROUND WAS PERFORMED, THE QRH WAS COMPLIED WITH, AND THE SUBSEQUENT LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE PSEU. (LP #8812192)

Next page: https://openairdocs.org/aircraft/N996AT/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 = 'N996AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N996AT/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.