# Service difficulty reports: N964AT

A list on [N964AT](https://openairdocs.org/aircraft/N964AT.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 6 · 264 reports

- [SDR DALA2026031001645](https://openairdocs.org/sdr/DALA2026031001645.md): Not Reported · not reported · Mar 8, 2026 · N964AT · Boeing 717200 · Standard Practices/Structures
  > SHIP 9523 ERA 632996-14 ISSUED FOR REPAIR TO STA 207-218,L L17-18RH. CORRECTIVE ACTION: REPAIRED PER ERA 632996-14. (1485115)
- [SDR DALA2026031001641](https://openairdocs.org/sdr/DALA2026031001641.md): Skin · cracked · Mar 6, 2026 · N964AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > SHIP 9523 CRACKS (2EAS) ON UPPER EXTERNAL FUSELAGE SKIN APPROX Y=1087 BTW LONG 13R-14R. CORRECTIVE ACTION: REPAIRED PER ER/A 632448-14 (1482120)
- [SDR DALA2026031001640](https://openairdocs.org/sdr/DALA2026031001640.md): Frame · cracked · Mar 6, 2026 · N964AT · Boeing 717200 · Fuselage Main, Frame
  > SHIP 9523 CRACKED FRAME AND FRAME CLIP BTW STA 1152 BTW L=1/2R AT AFT ACCESORY COMPARMENT. CORRECTIVE ACTION: PERMANENT REPAIR AND PER PRI 632524-14 REV 1. (1481299)
- [SDR DALA2026031001646](https://openairdocs.org/sdr/DALA2026031001646.md): Skin · damaged · Mar 5, 2026 · N964AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > SHIP 9523 ERA 632448-14 ISSUED FOR REPAIRS TO STA 1087 AND 1076 L13R TO L1 4R FUSELAGE SKIN. CORRECTIVE ACTION: ASSOCIATED ER/A 00-632448 (1480632)
- [SDR DALA2026030501526](https://openairdocs.org/sdr/DALA2026030501526.md): Hinge Fitting · corroded · Mar 3, 2026 · N964AT · Boeing 717200 · Trailing Edge Flaps
  > CORROSION ON LOWER OTBD ATTACH POINT STUD AND MIDDLE FLAP HINGE FITTING STA Y XRS 267 APPROX AT RT WING. REPLACED PER SERVICEABLE CENTER WING FLAP HINGE FITTING RH PER B717-200 AMM 57-55-25. (1476470)
- [SDR DALA2026030201424](https://openairdocs.org/sdr/DALA2026030201424.md): Skin · cracked · Feb 28, 2026 · N964AT · Boeing 717200 · Wing, Plate/Skin
  > CRACKS (2 EA) ON INTERNAL SKIN OF INBRD BUTE DOOR (OUTBOARD EDGE) AT RH WING. CORRECTIVE ACTION: REPAIR ASSOCIATED ER/A 14-618696 (1472759)
- [SDR DALA2026022501337](https://openairdocs.org/sdr/DALA2026022501337.md): Bulkhead · nicked · Feb 21, 2026 · N964AT · Boeing 717200 · Fuselage Main, Bulkhead
  > NICK ON FWD BULKHEAD BTW STA Y=37 AND X=10 AT NOSE GEAR WHEEL WELL. DAMAGED AREA REPAIRED PER B717-200 SRM 51-00-00 (1460835)
- [SDR DALA2025072005441](https://openairdocs.org/sdr/DALA2025072005441.md): Transceiver · faulted · Jul 19, 2025 · N964AT · Boeing 717200 · Ground Proximity System
  > SHIP 9523-ATO- ABORTED TAKE-OFF DUE TO RECEIVING A STICK PUSHER FAIL MESSAGE. CORRECTIVE ACTION: MAINTENANCE REPLACED BOTH RADIO ALTIMETER TRANSCEIVERS AND PERFORMED ALL APPLICABLE RETURN TO SERVICE TESTS. (LP 7808224)
- [SDR DALA2024123112106](https://openairdocs.org/sdr/DALA2024123112106.md): None · none · Dec 10, 2024 · N964AT · Boeing 717200 · Standard Practices/Structures
  > -AD- OVERWEIGHT LANDING. LW - 110.1. MAX 110.0. VERTICAL SPEED AT TOUCHDOWN ~ 50 FT/MN. WT EXITING RUNWAY INDICATED 109.8. PERFORMED B717 AMM 05-51-04 210-801 A-1 CHECK INSP FOR HARD OR OVERWEIGHT LANDING. FLOW CHART FIGURE 602 USED FOR OVERWEIGHT LANDING ONLY
- [SDR DALA2024032803863](https://openairdocs.org/sdr/DALA2024032803863.md): Warning Message · false indication · Mar 27, 2024 · N964AT · Boeing 717200 · Landing Gear Position and Warning
  > SHIP 9523 -MISC/DE- ON CLIMB OUT, AT APPROXIMATELY 5,000 FEET, THE "PSEU FAIL" MESSAGE ILLUMINATED. THE QRH WAS COMPLIED WITH, AND AN EMERGENCY WAS DECLARED WITH ATC DUE TO THE PSEU FAILURE. THE PSEU RETURNED TO NORMAL ON DESCENT AND THE LANDING WAS UNEVENTFUL
- [SDR DALA2024020601578](https://openairdocs.org/sdr/DALA2024020601578.md): Spar · cracked · Feb 5, 2024 · N964AT · Boeing 717200 · Wing Spar
  > CRACK ON REAR SPAR LOWER SECTION LH WING AT XRS=214.000. SUMMARY OF NRC 00651: REAR SPAR LOWER SECTION LH WING AT XRS=214.000 WAS REPAIRED PER ERA 615443-14AD REV ORIGINAL. SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-615443 ADDED FOR AC 9523. (LP #0188635)
- [SDR DALA2024020601573](https://openairdocs.org/sdr/DALA2024020601573.md): Pan · cracked · Feb 3, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED PAN AND FITTING ON BEAM #4 FWD STOP FITTING AREA AT AFT CARGO DOOR. SUMMARY OF NRC 00156: FITTING REPLACED PER B717-200 SRM 51-41-03-0G, 51-41-01-0G, AND 51-41-05-0G. PAN BEAM #4 FWD STOP FITTING AREA AT AFT CARGO DOOR WAS REPAIRED PER PRI 614439-14 RE
- [SDR DALA2024020301511](https://openairdocs.org/sdr/DALA2024020301511.md): Pan · cracked · Feb 2, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED PAN AND FITTING ON BEAM #4 AFT STOP FITTING AREA AT AFT CARGO DOOR. SUMMARY OF NRC 00154: FITTING WAS FABRICATED PER DWG 3914025 REV C AND PAN ON BEAM #4 AFT STOP FITTING AREA AT AFT CARGO DOOR WAS REPAIRED PER PRI 614439-14 REV 6 AND ERA 614439-14 REV
- [SDR DALA2024020101447](https://openairdocs.org/sdr/DALA2024020101447.md): Frame · cracked · Feb 1, 2024 · N964AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME FORMER STA 1133 AND LONGERON 2LH AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00146: FRAME FORMER STA 1133 AND LONGERON 2LH AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R REPAIR 1 EXAMPLE A. (LP #0181239)
- [SDR DALA2024020101446](https://openairdocs.org/sdr/DALA2024020101446.md): Angle · corroded · Feb 1, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND ON LH UPPER CUSP ANGLE (LOWER SKIN) BTW STA Y=200 TO Y=226 FROM X=56 TO X=60 AT PAX CABIN. SUMMARY OF NRC 00571: CORROSION LEVEL 2. LH UPPER CUSP ANGLE (LOWER SKIN) BTW STA Y=200 TO Y=226 FROM X=56 TO X=60 AT PAX CABIN WAS REPAIRED PER B717
- [SDR DALA2024020301505](https://openairdocs.org/sdr/DALA2024020301505.md): Web · cracked · Jan 31, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS ON INTERNAL STRUCTURE (WEB) BTW STA Y=1053, -X14 Y53, AND X14 Y53 AT EMERGENCY EXIT DOOR. SUMMARY OF NRC 00255: INTERNAL STRUCTURE (WEB) BTW STA Y=1053, -X14 Y53, AND X14 Y53 AT EMERGENCY EXIT DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G PROCEDURE GEN
- [SDR DALA2024013101412](https://openairdocs.org/sdr/DALA2024013101412.md): Angle · corroded · Jan 31, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD LOWER ANGLE OF DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00168: CORROSION LEVEL 2. FWD LOWER ANGLE OF DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7. (LP #0179772)
- [SDR DALA2024013001358](https://openairdocs.org/sdr/DALA2024013001358.md): Cargo Track · corroded · Jan 29, 2024 · N964AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR TRACK LH STA Y=889, AFT CARGO WAS REMOVED AND REMAINDER TRACK IS OUT OF LIMITS. SUMMARY OF NRC 00648: CORROSION LEVEL 2. FLOOR TRACK LH STA Y=889, AFT CARGO WAS REPAIRED B717-200 SRM 53-20-52-2R PROCEDURE 4 FIG 201. (LP #0178275)
- [SDR DALA2024013001356](https://openairdocs.org/sdr/DALA2024013001356.md): Pan · cracked · Jan 29, 2024 · N964AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON INNER PAN, SETTLEMENT AREA OF STOP FITTING #2 AT FWD SIDE OF FWD CARGO DOOR. SUMMARY OF NRC 00239: INNER PAN, SETTLEMENT AREA OF STOP FITTING #2 AT FWD SIDE OF FWD CARGO DOOR WERE REPAIRED PER PRI 614520-14 REV 5 AND ERA 614520-14 REV ORIGINAL SECTION
- [SDR DALA2024012901231](https://openairdocs.org/sdr/DALA2024012901231.md): Longeron Splice · corroded · Jan 28, 2024 · N964AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON SPLICE 24L BTW STA Y=889 AND STA Y=908 IN REFERENCE TO NRC 00644. SUMMARY OF NRC 00650: CORROSION LEVEL 2. SPLICE ON LONGERON 24L BTW STA Y=889 AND STA Y=908 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0176297)
- [SDR DALA2024012901227](https://openairdocs.org/sdr/DALA2024012901227.md): Cusp Web · corroded · Jan 27, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LH CUSP WEB UPPER AND LOWER BTW STA Y=200 TO Y=294 FROM X=53 TO X=60 AT PAX CAB. SUMMARY OF NRC 00361: CORROSION LEVEL 2. LH CUSP WEB UPPER AND LOWER BTW STA Y=200 TO Y=294 FROM X=53 TO X=60 AT PAX CAB WAS FABRICATED AND REPLACED PER DWG 9936535-3
- [SDR DALA2024012901226](https://openairdocs.org/sdr/DALA2024012901226.md): Web · corroded · Jan 27, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB (UPPER SURFACE) BTW STA 160-200 AND X=44.5 TO X=55 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00409: CORROSION LEVEL 2. WEB (UPPER SURFACE) BTW STA 160-200 AND X=44.5 TO X=55 AT PAX CABIN FLOOR STRUCTURE WAS FABRICATED AND REPLACED PER B717
- [SDR DALA2024012901225](https://openairdocs.org/sdr/DALA2024012901225.md): Floor Support · corroded · Jan 27, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT (1 EA) (UPPER/ LOWER SURFACE) BTW STA 186-195 ON X=52.5 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00408: CORROSION LEVEL 2. FLOOR SUPPORT (1 EA) (UPPER/LOWER SURFACE) BTW STA 186-195 ON X=52.5 AT PAX CABIN FLOOR STRUCTURE WAS REPL
- [SDR DALA2024012901224](https://openairdocs.org/sdr/DALA2024012901224.md): Floor Support · corroded · Jan 27, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS (UPPER/LOWER SURFACE) BTW STA 160-200 ON X=44.5 (1 EA) AND X=55 (1 EA) AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 407: CORROSION LEVEL 2. FLOOR SUPPORTS (UPPER/LOWER SURFACE) BTW STA 160-200 ON X=44.5 (1 EA) AND X=55 (1 EA) AT PAX
- [SDR DALA2024012901223](https://openairdocs.org/sdr/DALA2024012901223.md): Stringer Splice · corroded · Jan 27, 2024 · N964AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON PREVIOUS REPAIR SPLICE AT STA Y=908 BTW LONG 26L AND LONG 27L IN AFT CARGO COMPARTMENT. SUMMARY OF NRC 00647: CORORSION LEVEL 2. SPLICE OF STA Y=908 BTW LONG 26L AND LONG 27L WAS REPLACED PER B717-200 DGW 9971183 REV 'J'. (LP #0174281)
- [SDR DALA2024012901222](https://openairdocs.org/sdr/DALA2024012901222.md): Doubler · corroded · Jan 27, 2024 · N964AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON PREVIOUS REPAIR DOUBLER BTW STA 844-859 AND LONGERONS 28L-28R AT EXTERNAL FUSSELAGE SKIN. SUMMARY OF NRC 00395: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER BTW STA 844-859 AND LONGERONS 28L-28R AT EXTERNAL FUSSELAGE SKIN WAS REPLACED PER B717 SRM 5
- [SDR DALA2024012901221](https://openairdocs.org/sdr/DALA2024012901221.md): Floor Support · corroded · Jan 27, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT (UPPER/LOWER SURFACE) BTW STA 148-200 BTW X=-5 TO X=-9 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00413: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 148-200 BTW X=-5 TO X=-9 AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER B717-200 SRM 5
- [SDR DALA2024012901220](https://openairdocs.org/sdr/DALA2024012901220.md): Angle · corroded · Jan 26, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND ON LH/LOWER CUSP ANGLE BTW STA Y=180 AND X=56 LH, PAX CABIN. SUMMARY OF NRC 00611: CORROSION LEVEL 2. CUSP ANGLE ON LH/LOWER CUSP ANGLE BTW STA Y=180 AND X=56 LH WAS REPAIRED PER B717 SRM 53-00-55-2R-3. (LP #0173416)
- [SDR DALA2024013101411](https://openairdocs.org/sdr/DALA2024013101411.md): Skin · damaged · Jan 25, 2024 · N964AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > FASTENER HOLES AND COUNTERSINKS ARE ELONGATED OUT OF LIMITS ON 1/4 FASTENERS ROW AT VERT STAB FIX LE. ALSO, ON VERT STAB REMOVABLE LE STA ZFS=52.267 REF SERVICE GENERAL DRAWING SG95550001. SUMMARY OF NRC 00538: FASTENER HOLES AND COUNTERSINKS AT VERT STAB FIX
- [SDR DALA2024012401101](https://openairdocs.org/sdr/DALA2024012401101.md): Seat Track · corroded · Jan 24, 2024 · N964AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK X=-44.5 BTW STA 200-219 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00403: SEAT TRACK SECTION X=-44.5 BTW STA 200-246 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED OFF PER B717-200 SRM 53-20-52-2R PROCEDURE 5. (LP #0169174)
- [SDR DALA2024012401100](https://openairdocs.org/sdr/DALA2024012401100.md): Skin · damaged · Jan 24, 2024 · N964AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CREASES WERE FOUND ON REPAIR SKIN SECTION OVER THE FRAME STA 256 BTW LONG 17LH-18LH PER B717 SRM 53-00-01-02 REPAIR 6 PAR. 7. SUMMARY OF NRC 00270: SKIN SECTION OVER THE FRAME STA 256 BTW LONG 17LH-18LH WAS REPAIRED PER B717-200 SRM 53-00-01-2R REP 6. SPECIFIC
- [SDR DALA2024012301009](https://openairdocs.org/sdr/DALA2024012301009.md): Skin · gouged · Jan 23, 2024 · N964AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > GOUGE AND DENT ON FUSELAGE SKIN AT STA 237 BTW LONG 18L-19L. SUMMARY OF NRC 00615: FUSELAGE SKIN AT STA 237 BTW LONG 18L-19L WAS PERMANENT REPAIRED PER B717-200 SRM 53-02-01-2R-1 FIG 202. THE PERMANENT REPAIR SPECIFIED MAINTENANCE REQUIREMENTS ARE A VISUAL INS
- [SDR DALA2024012301008](https://openairdocs.org/sdr/DALA2024012301008.md): Web · cracked · Jan 20, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > WEB CRACKED FORWARD OF CANTED FRAME 1200 AT 2 O-CLOCK POSITION. SUMMARY OF NRC 00599: WEB FORWARD OF CANTED FRAME 1200 AT 2 O-CLOCK POSITION WAS REPAIRED PER ERA 537343-14MA REV B SECTION II. ASSOCIATED ERA 14-537343 ADDED FOR AC 9523. (LP #0162948)
- [SDR DALA2024012301007](https://openairdocs.org/sdr/DALA2024012301007.md): Web · cracked · Jan 20, 2024 · N964AT · Boeing 717200 · Fuselage Main, Frame
  > WEB CRACKED FORWARD OF CANTED FRAME 1200 AT 10 O-CLOCK POSITION. SUMMARY OF NRC 00598: WEB FORWARD OF CANTED FRAME 1200 AT 10 O-CLOCK POSITION WAS REPAIRED PER ERA 537343-14MA REV B SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-537343 ADDED FOR AC 9523. (LP #
- [SDR DALA2024012200905](https://openairdocs.org/sdr/DALA2024012200905.md): Web · punctured · Jan 20, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > PUNCTURES (2 EA) ON WEB BTW STA 160-200 AND X=-44.4 TO X=-54 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00415: WEB BTW STA 160-200 AND X=-44.4 TO X=-54 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-10-2R. (LP #0163433)
- [SDR DALA2024012200902](https://openairdocs.org/sdr/DALA2024012200902.md): Floor Support · corroded · Jan 19, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT (UPPER/LOWER SURFACE) BTW STA 148-200 BTW X=5 TO X=9 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00412: CORROSION LEVEL 2. FLOOR SUPPORT (UPPER/ LOWER SURFACE) BTW STA 148-200 BTW X=5 TO X=9 AT PAX CABIN FLOOR STRUCTURE WAS REPLACED
- [SDR DALA2024011900810](https://openairdocs.org/sdr/DALA2024011900810.md): Cusp Web · cracked · Jan 19, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON RH CUSP WEB BTW STA 218-237 AND X=-44 TO X=-60 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00397: RH CUSP WEB BTW STA 218-237 AND X=-44 TO X=-60 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4. (LP #0161271)
- [SDR DALA2024011900805](https://openairdocs.org/sdr/DALA2024011900805.md): Floorbeam · corroded · Jan 18, 2024 · N964AT · Boeing 717200 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR SUPPORTS AT W1 AREA STA 200 BTW X=7 AND X=-44 IN REF TO NRC 00401. SUMMARY OF NRC 00539: CORROSION LEVEL 2. FLOOR SUPPORTS WERE REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0160759)
- [SDR DALA2024011500577](https://openairdocs.org/sdr/DALA2024011500577.md): Unknown · unknown · Jan 14, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON LH CUSP WEB LOWER BTW STA Y=294 TO Y=313 FROM X=45 AT PAX CAB. SUMMARY: LH CUSP WEB LOWER BTW STA Y=294 TO Y=313 FROM X=45 AT PAX CAB WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #0154369)
- [SDR DALA2024011500576](https://openairdocs.org/sdr/DALA2024011500576.md): Unknown · unknown · Jan 14, 2024 · N964AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK OF 0.125 IN ON UPPER RADIUS OF THE FRAME TAB OVERWING FRAME AT STA Y=674.000 LH (REF CARD 5310-01436-04B). SUMMARY OF NRC 00205: OVERWING FRAME AT STA Y=674.000 LH (REF CARD 5310-01436-04B) WAS REPLACED PER B717-200 SRM 51-41-05-0G PAR 8 AND AMDS 5310-01
- [SDR DALA2024010900327](https://openairdocs.org/sdr/DALA2024010900327.md): Unknown · unknown · Jan 8, 2024 · N964AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON CABIN FLOOR SUPPORT BTW STA Y=1022 TO Y=1053 X=44 AT CPAX. SUMMARYOF NRC 00600: CORROSION LEVEL II. FLOOR SUPPORT BTW STA Y=1022 TO Y=1053 X=44 AT CPAX WAS REPLACED PER B717-200 SRM 51-41-05-0G PAR 8 AND DWG 9981477-15 REV L. (LP #0145572)
- [SDR DALA2024010900326](https://openairdocs.org/sdr/DALA2024010900326.md): Unknown · unknown · Jan 8, 2024 · N964AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA 1037 LONG 17 RH AT PAX CABIN. SUMMARY OF NRC 00289: FRAME STA 1037 LONG 17 RH AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #0144771)
- [SDR DALA2024010900325](https://openairdocs.org/sdr/DALA2024010900325.md): Unknown · unknown · Jan 7, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON RH CUSP MEMBRANE ON STA Y=716 AND X=-44 AT PAX CABIN. SUMMARY OF NRC 00445: RH CUSP MEMBRANE ON STA Y=716 AND X=-44 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROC 2 PAR 4. (LP #0144067)
- [SDR DALA2024010900324](https://openairdocs.org/sdr/DALA2024010900324.md): Unknown · unknown · Jan 7, 2024 · N964AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SKIN LOWER SURFACE BTW STA 389 AND X=-58 AT FWD CARGO DOOR JAMB AREA. SUMMARY OF NRC 00203: CORROSION LEVEL 2. FLOOR SKIN LOWER SURFACE BTW STA 389 AND X=-58 AT FWD CARGO DOOR JAMB AREA WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4. (
- [SDR DALA2024010800319](https://openairdocs.org/sdr/DALA2024010800319.md): Unknown · unknown · Jan 4, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON RH CUSP MEMBRANE ON STA Y=813 AND X =-44 AT PAX CABIN. SUMMARY OF NRC 00446: RH CUSP MEMBRANE ON STA Y=813 AND X=-44 AT PAX CABIN WAS REPAIRED PER B717 SRM-53-00-55-2R-4. (LP #0138861)
- [SDR DALA2024010210753](https://openairdocs.org/sdr/DALA2024010210753.md): Unknown · unknown · Dec 30, 2023 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > TOOL MARK ON CUSP MEMBRANE (INTERNAL SIDE) ON STA Y=916 AND X=-56 AT PAX CABIN. SUMMARY OF NRC 00448: CUSP MEMBRANE (INTERNAL SIDE) ON STA Y=916 AND X=-56 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 208. (LP #0132552)
- [SDR DALA2023122410541](https://openairdocs.org/sdr/DALA2023122410541.md): Unknown · unknown · Dec 22, 2023 · N964AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON INTERNAL STRUCTURE APROX BTW STA 370 AND L-19R AT FWD CARGO DOOR. SUMMARY OF NRC 00136: INTERNAL STRUCTURE APROX BTW STA 370 AND L-19R AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0122246)
- [SDR DALA2023092107773](https://openairdocs.org/sdr/DALA2023092107773.md): Unknown · unknown · Sep 21, 2023 · N964AT · Boeing 717200 · Hydraulic System, Main
  > SHIP 9523 -HYD/DE- THE CREW RECEIVED A "HYD R QTY LOW" MESSAGE AT TOP OF CLIMB. THEY WERE UNABLE TO REPRESSURIZE THE SYSTEM. THE QRH WAS COMPLIED WITH AND PERFORMED THE ALTERNATE GEAR EXTENSION (DUE TO A RIGHT HYDRAULIC SYSTEM LOW QUANTITY). AN EMERGENCY WAS D
- [SDR DALA2022121308025](https://openairdocs.org/sdr/DALA2022121308025.md): Power Supply · inoperative · Dec 9, 2022 · N964AT · Boeing 717200 · Exterior Lighting
  > THE EXTERIOR EMERGENCY LIGHTS IN THE AFT FUSELAGE WILL NOT EXTINGUISH. MAINTENANCE REPLACED THE AFT EXTERIOR EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT IS OK FOR SERVICE. (LP #9017959)
- [SDR DALA2022100406443](https://openairdocs.org/sdr/DALA2022100406443.md): None · none · Oct 1, 2022 · N964AT · Boeing 717200 · Emergency Lighting
  > THE LOWER AFT OVERWING EXIT DOOR LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-119 PER B717 AMM 33-51. OPERATIONAL CHECK IS NOW GOOD. (LP #8954064)

Next page: https://openairdocs.org/aircraft/N964AT/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 = 'N964AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N964AT/reports

---
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.