# Service difficulty reports: N995AT

A list on [N995AT](https://openairdocs.org/aircraft/N995AT.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 · 158 reports

- [SDR DALA2026092405328](https://openairdocs.org/sdr/DALA2026092405328.md): Skin · damaged · Sep 24, 2026 · N995AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND DAMAGE TO AFT CARGO DOOR CUTOUT AFT SKIN EDGE, COMPLIED WITH ER/A 637149-14. (9115046) (AIRCRAFT GROUNDED).
- [SDR DALA2025111808418](https://openairdocs.org/sdr/DALA2025111808418.md): Cover · detached · Nov 12, 2025 · N995AT · Boeing 717200 · Escape Slide
  > DURING SERVICE CHECK WALK AROUND, TAIL CONE SLIDE COVER WAS COMPLETELY UNLATCHED AND COVER WAS FULLY TO THE REAR. RESECURED CONTAINER ASSY LATCH IAW CMM 25-66-20, ALSO REF AMM 25-61. PER TOPP 40-30-05 APP J ABLE TO RESECURE AND NOT CONSIDERED RII EVENT. (7982
- [SDR DALA2025100807328](https://openairdocs.org/sdr/DALA2025100807328.md): Skin · damaged · Sep 26, 2025 · N995AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > SHIP 9540 DUE ER/A 628896-14 REV. ORIG. SECTION II PERMANENT REPAIR INSTRUCTION FOR RIGHT SIDE FUSELAGE SKIN DAMAGED AT STA. 237"- STA. 294". COMPLIED WITH PERMANENT REPAIR PER B717-200 SRM 53-00-01 (1219111)
- [SDR DALA2025091606811](https://openairdocs.org/sdr/DALA2025091606811.md): Stringer · damaged · Sep 9, 2025 · N995AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > STRINGER 27R DAMAGED BS 237 - 282. REPAIR SPLICE IAW SRM 53-00-05 (1190061).
- [SDR DALA2025091606810](https://openairdocs.org/sdr/DALA2025091606810.md): Stringer · damaged · Sep 9, 2025 · N995AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R DAMAGED BETWEEN BS 226 - 282. REPAIRED PER B717 SRM 53-00- 05-2R. (1190030)
- [SDR DALA2025091606809](https://openairdocs.org/sdr/DALA2025091606809.md): Frame · damaged · Sep 9, 2025 · N995AT · Boeing 717200 · Fuselage Main, Frame
  > FS 256 FRAME DAMAGED BETWEEN STR 25 RT-28 RT. REMOVED DAMAGED FRAME SECTION PER B717 SRM 53-20-07-2R (1189997)
- [SDR DALA2025100807325](https://openairdocs.org/sdr/DALA2025100807325.md): Access Panel · out of limits · Jan 22, 2025 · N995AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > ELONGATED HOLES (11 EA) WERE FOUND ON ACCESS PANEL OF LIGHT ASSY MB LOWER ARE OUT OF LIMITS PER DWG 5925039 REV. F. HOLES OUT OF LIMITS WERE REPAIRED PER ER/A 623283-14 REV. (0773037)
- [SDR DALA2025012400583](https://openairdocs.org/sdr/DALA2025012400583.md): Light · inoperative · Jan 22, 2025 · N995AT · Boeing 717200 · Emergency Lighting
  > THE EXTERIOR EMERGENCY LIGHT DOESN'T TURN ON. THE OVERWING EMERGENCY LIGHT WAS REPLACED PER B717-200 AMM 33-51-05. ALL TEST OK. (LP #6552182)
- [SDR DALA2025012100470](https://openairdocs.org/sdr/DALA2025012100470.md): Doubler · worn · Jan 20, 2025 · N995AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > WEAR ON REPAIR DOUBLER BTW STA Y=954 L24R TO L27R AT EXTERNAL FUSELAGE. SUMMARY OF NRC 00011: PREVIOUS REPAIR DOUBLER BTW STA Y=954 L24R TO L27R AT EXTERNAL FUSELAGE WAS REPLACED PER PRI 562383-14 REV 3 AND ERA 562383-14 REV B SECTION III: PERMANENT REPAIR. PE
- [SDR DALA2025012100469](https://openairdocs.org/sdr/DALA2025012100469.md): Frame · bent · Jan 20, 2025 · N995AT · Boeing 717200 · Fuselage Main, Frame
  > BENT FRAME STA Y=465 BTW LONG 26L AND LONG 27L AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00279: FRAME STA Y=465 BTW LONG 26L AND LONG 27L AT FWD CARGO COMPARTMENT WAS REPAIRED PER PRI 623357-14 REV 2 AND ERA 623357-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR.
- [SDR DALA2025012000465](https://openairdocs.org/sdr/DALA2025012000465.md): Door Frame · corroded · Jan 17, 2025 · N995AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON CARGO DOOR JAMB BTW STA Y=954 TO Y=988 AND LONGERON 28R (LOWER SIDE) AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00154: CORROSION LEVEL 2. CARGO DOOR JAMB CORROSION BTW STA Y=954 TO Y=988 AND LONGERON 28R (LOWER SIDE) AT AFT CARGO COMPARTMENT WAS REP
- [SDR DALA2025012000463](https://openairdocs.org/sdr/DALA2025012000463.md): Pan · cracked · Jan 15, 2025 · N995AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS ON PAN OF INTERNAL STRUCTURE AT AFT EDGE OF AFT CARGO COMPARMENT DOOR BTW BEAM 2/3 AND BTW BEAM 4/5. ALSO ON FWD EDGE BTW BEAM 3/4. SUMMARY OF NRC 00135: AFT CARGO COMPARMENT DOOR WAS REMOVED AND A SERVICEALBE AFT CARGO COMPARMENT DOOR WAS INSTALLED PER
- [SDR DALA2025011600359](https://openairdocs.org/sdr/DALA2025011600359.md): Beam · cracked · Jan 15, 2025 · N995AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON BEAM 6 APROX STA Y=180 AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00256: BEAM 6 APROX STA Y=180 AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIRED PER ER/A: 623355-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 623355-14 REV 0. ASSOCIATED ER/A 14-6
- [SDR DALA2025011300273](https://openairdocs.org/sdr/DALA2025011300273.md): Longeron · corroded · Jan 11, 2025 · N995AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 29L BTW STA Y=946 TO Y=1007 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00651: CORROSION LEVEL 2. LONGERON 29L BTW STA Y=946 TO Y=1007 AT AFT CARGO COMPARMENT WAS REPAIRED DUE CORROSION PER B717-200 SRM 53-00-05-2R REPAIR 3 PAR 4. (1) FIGURE
- [SDR DALA2025011300271](https://openairdocs.org/sdr/DALA2025011300271.md): Frame · cracked · Jan 10, 2025 · N995AT · Boeing 717200 · Fuselage Main, Frame
  > -AD- CRACK ON UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=715 LH WAS FOUND IN REF TASK CARD 5310-01436-04B JOB #079-0002, STEP 13. SUMMARY OF NRC 00397: FRAME WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G UNDER AMDS 5310-01436-03A.
- [SDR DALA2025011300269](https://openairdocs.org/sdr/DALA2025011300269.md): Doubler · damaged · Jan 9, 2025 · N995AT · Boeing 717200 · Wing, Plate/Skin
  > WEAR AND GOUGES ON PREVIOUS REPAIR DOUBLER OF FIXED LEADING EDGE PANEL ON XIS=120 AT RH WING. SUMMARY OF NRC 00057: PREVIOUS REPAIR DOUBLER OF FIXED LEADING EDGE PANEL ON XIS=120 AT RH WING WAS REPLACED PER B717-200 SRM 57-40-01-2R REPAIR 7 FIG 202, 51-41-05-0
- [SDR DALA2025011300266](https://openairdocs.org/sdr/DALA2025011300266.md): Floor Support · corroded · Jan 9, 2025 · N995AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS OF STA 157-210 -X=45, STA 256 -X=44-24L, STA 174-176 BTW -X=10- 49, STA 200-157 X=10, STA 200-157 -X=10, STA 157-200 BTW X=44, STA 200 BTW X=44-42, AND STA 200-203 BTW -X=5 TO -X=43 AT PAX CABIN. SUMMARY OF NRC 00671: CORROSION LEVE
- [SDR DALA2025011300274](https://openairdocs.org/sdr/DALA2025011300274.md): Skin · dented · Jan 9, 2025 · N995AT · Boeing 717200 · Trailing Edge Flaps
  > DENT #4, XF=89.250" DAE=13.500"; DENT #5, XF=86.500" DAE=11.500"; DENT#6. XF=88.375" DAE=14"; AND DENT#26, XF=81.250" DAE=4.500" WERE FOUND OUT OF LIMITS ON LOWER SURFACE ON AFT MOVABLE FLAP VANE AT RH WING. SUMMARY OF NRC 00592: RIGHT WING AFT MOVABLE FLAP VA
- [SDR DALA2025010900178](https://openairdocs.org/sdr/DALA2025010900178.md): Cusp Web · cracked · Jan 8, 2025 · N995AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB STA Y:715 X:60 IN PAX CABIN. SUMMARY OF NRC 00567: CUSP WEB STA Y:715 X:60 IN PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4, FIG 223 AND DWG 9910151-5. (LP #0752185)
- [SDR DALA2024123112104](https://openairdocs.org/sdr/DALA2024123112104.md): Floor Support · corroded · Dec 30, 2024 · N995AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS (3 EA), FROM STA Y=1022 TO STA Y=1063 ON X=44, X=52, AND X=-44 AT AFT PAX CABIN FLOOR. SUMMARY OF NRC 00459: CORROSION LEVEL 2. FLOOR SUPPORTS (3 EA), FROM STA Y=1022 TO STA Y=1063 ON X=44, X=52, AND X=-44 AT AFT PAX CABIN FLOOR WER
- [SDR DALA2024123112103](https://openairdocs.org/sdr/DALA2024123112103.md): Cusp Web · cracked · Dec 30, 2024 · N995AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB (LOWER SIDE) BTW X=47 AND STA 591 AT CPAX. SUMMARY OF NRC 00467: CUSP WEB (LOWER SIDE) BTW X=47 AND STA 591 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 221 AND 51-41-02-0G. (LP #0736473)
- [SDR DALA2024123012067](https://openairdocs.org/sdr/DALA2024123012067.md): Pan · cracked · Dec 29, 2024 · N995AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON OUTER PAN AT FWD EDGE ON BEAM #3 WAS FOUND AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00405: CRACK ON OUTER PAN AT FWD EDGE ON BEAM #3 AT FWD CARGO DOOR COMPARTMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0734792)
- [SDR DALA2024123012066](https://openairdocs.org/sdr/DALA2024123012066.md): Vane · dented · Dec 27, 2024 · N995AT · Boeing 717200 · Trailing Edge Flaps
  > SEVERAL DENTS ON LOWER SKIN LH AFT MOVEABLE FLAP VANE. SUMMARY OF NRC 00250: DENTS (8 EA) ON LOWER SKIN LH AFT MOVABLE FLAP VANE WERE EVALUATED AND DENTS #1 TO #7 ARE OUT OF LIMITS PER B717-200 SRM 57-53-01-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 3. A. AND WERE
- [SDR DALA2024122712034](https://openairdocs.org/sdr/DALA2024122712034.md): Pan · cracked · Dec 27, 2024 · N995AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON PAN OF FWD AND AFT EDGE AT FWD CARGO DOOR BELOW BEAM 5. SUMMARY OF NRC-00143: PAN OF FWD AND AFT EDGE AT FWD CARGO DOOR BELOW BEAM 5 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0730599)
- [SDR DALA2024123012065](https://openairdocs.org/sdr/DALA2024123012065.md): Seat Track · corroded · Dec 24, 2024 · N995AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH INB SEAT TRACK (X=22) ON STA Y=200-205 AT CPAX. SUMMARY OF NRC 00482: CORROSION LEVEL 2. CORROSION AT LH INB SEAT TRACK (X=22) ON STA Y=200-205 AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #0726955)
- [SDR DALA2024122712031](https://openairdocs.org/sdr/DALA2024122712031.md): Beam · cracked · Dec 24, 2024 · N995AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON BEAM #1 APROX STA Y=190 AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00255: BEAM #1 APROX STA Y=190 AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0726863)
- [SDR DALA2024122311961](https://openairdocs.org/sdr/DALA2024122311961.md): Pan · cracked · Dec 19, 2024 · N995AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INNER PAN AT FWD EDGE BTW BEAM 1 AND 2 WAS FOUND ON AFT CARGO DOOR. SUMMARY OF NRC 00442: OUTER PAN FWD EDGE BTW BEAM 1 AND 2 WAS BLENDED OUT AND MEASURED AS FOLLOW: MINIOR DAMAGED TO SKIN EDGE NO MORE THAN 0.380" DEEP: BLEND OUT IS 0.125". REWORK ARE
- [SDR DALA2024121911828](https://openairdocs.org/sdr/DALA2024121911828.md): Cover · broken · Dec 19, 2024 · N995AT · Boeing 717200 · Aerodynamic Fairings
  > BROKEN PLASTIC COVER OF TAIL CONE EXTENSION PULL LEVER AFT ACCESORIES COMPARTMENT. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC: 00326 PLASTIC COVER OF TAIL CONE EXTENSION PULL
- [SDR DALA2024060605812](https://openairdocs.org/sdr/DALA2024060605812.md): Stringer · corroded · Jun 6, 2024 · N995AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION AT APPROX STATION 1053 ON STRINGER 26. RIVETS POPPED WITH SKIN PROTRUDING. REMOVED STR END FITTING AT STR 26 STA 1053 FOUND TO BE 100% LOSS. OUT OF LIMITS. INSPECTED AREA AFTER END FITTING REMOVAL, NO ADDITIONAL CORROSION FOUND. LOCATED, DRILLED, ALO
- [SDR DALA2024042304670](https://openairdocs.org/sdr/DALA2024042304670.md): Bearing · faulted · Apr 20, 2024 · N995AT · Boeing 717200 · Passenger/Crew Doors
  > THE GATE AGENT REPORTS THAT THE 1L DOOR WAS HARD TO OPEN. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REMOVED 1L DOOR LINER, FOUND ROLLER BEARING NOT FALLING INTO DOOR HANDLE DETE
- [SDR DALA2024021502204](https://openairdocs.org/sdr/DALA2024021502204.md): Battery · inoperative · Feb 15, 2024 · N995AT · Boeing 717200 · Emergency Lighting
  > THE TAIL CONE AREA EMERGENCY LIGHTS WERE DISCOVERED TO BE INOPERATIVE. MAINTENANCE FOUND THE BATTERY ASSEMBLY B5-260 BAD. BATTERY ASSEMBLY B5-260 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. (LP #5412733)
- [SDR DALA2023082206831](https://openairdocs.org/sdr/DALA2023082206831.md): Unknown · unknown · Aug 18, 2023 · N995AT · Boeing 717200 · Emergency Lighting
  > EXIT SIGN (RIGHT) AT ROW 19 KNOCKED DOWN. MAINTENANCE FOUND THE EMERGENCY SIGN COVERS KNOCKED OFF, RESECURED THEM AS REQUIRED. THE AIRCRAFT IS OK FOR SERVICE. (LP #4391072)
- [SDR DALA2022032101833](https://openairdocs.org/sdr/DALA2022032101833.md): Not Reported · not reported · Mar 18, 2022 · N995AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING ABOVE SEAT 01B IN THE CABIN. MAINTENANCE RE-SECURED THE EMERGENCY "EXIT" LENS AT 01B AS REQUIRED. THE AIRCRAFT IS OK FOR SERVICE. (LP #2161790)
- [SDR DALA2021102706652](https://openairdocs.org/sdr/DALA2021102706652.md): None · none · Oct 24, 2021 · N995AT · Boeing 717200 · Aerodynamic Fairings
  > VAULT DOOR TAILCONE RELEASE PUSH-PULL CABLE TEFLON SHEATHING TORN AT RELEASE BLOCK STA 1212 AND AT THE 8 0'CLOCK POSITION. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE DEP
- [SDR DALA2021102606614](https://openairdocs.org/sdr/DALA2021102606614.md): None · none · Oct 24, 2021 · N995AT · Boeing 717200 · Fuselage Floor Panel
  > FWD CARGO DOOR JAMB AREA HAS AREAS OF CHIPPED PAINT, LIGHT CORROSION, AND NO GRAY PAINT AS PER SRM 53-00-15 REPAIR 1 FROM HALFWAY UP JAMB FWD AND AFT SIDES AND LOWER JAMB AREA. SUMMARY SEE NRC 065-0009:5300-2007/001 00348: REPAIRED PER B717 SRM 53-20-15-2R PRO
- [SDR DALA2021102606613](https://openairdocs.org/sdr/DALA2021102606613.md): None · none · Oct 24, 2021 · N995AT · Boeing 717200 · Flight Compartment Windows
  > RIGHT SIDE AFT COCKPIT WINDOW HAS HEAVY SCRATCHES ON EXTERIOR. SUMMARY SEE NRC 001-0305:5610-2001/002 00062: REPLACED RT SIDE AFT COCKPIT WINDOW PER B717 AMM 56-13-01. (LP #1994394)
- [SDR DALA2021102606612](https://openairdocs.org/sdr/DALA2021102606612.md): None · none · Oct 24, 2021 · N995AT · Boeing 717200 · Passenger Compartment Windows
  > RIGHT HAND SIDE PASSENGER WINDOW #30 IS FADED. SUMMARY SEE NRC 001-0308:5620-2001/004 00008: REPLACED WINDOW PER B717 AMM 56-20-01. (LP #1994391)
- [SDR DALA2021050302490](https://openairdocs.org/sdr/DALA2021050302490.md): Battery Pack · inoperative · May 2, 2021 · N995AT · Boeing 717200 · Emergency Lighting
  > THE MAIN CABIN MAIN DOOR TOP EMR LIGHT OUT. R & R THE BATTERY PACK B5-123 PER AMM 33-51. OPS CHECK GOOD.
- [SDR DALA2020112303834](https://openairdocs.org/sdr/DALA2020112303834.md): Lamp · wrong part · Nov 22, 2020 · N995AT · Boeing 717200 · Emergency Lighting
  > BOTH AFT OVERWING EXIT SIGNS ARE INOPERATIVE. MAINTENANCE FOUND THE WRONG LAMPS INSTALLED. COMPLETED RE-LAMP AND OPERATIONAL CHECK WAS GOOD, PER B717 AMM 33-51. OK FOR SERVICE.
- [SDR DALA2019070804080](https://openairdocs.org/sdr/DALA2019070804080.md): Battery Pack · discharged · Jul 6, 2019 · N995AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT SIGNS INOPERATIVE. EXIT LIGHTS FLASHING. T/S AS PER FIM 33-50; ALLOW SUFFICIENT TIME FOR BATTERY PACKS TO RE-CHARGE OPS CHECK NORMAL OK FOR SERVICE. (LP1157653)
- [SDR DALA2018051503374](https://openairdocs.org/sdr/DALA2018051503374.md): Computer · malfunctioned · May 8, 2018 · N995AT · Boeing 717200 · Autopilot Computer
  > THE CREW ABORTED THE TAKE-OFF AT 120 KNOTS AFTER THE "STAB TRIM" AURAL WARNING SOUNDED. THE STAB TRIM WAS SET WITHIN THE GREEN BOX AT 4.4 PRIOR TO THE TAKE-OFF ROLL. THE AIRCRAFT TAXIED BACK TO THE GATE. CORRECTIVE ACTION: MAINTENANCE HAS REPLACED THE FCC PER
- [SDR DALA2017112808353](https://openairdocs.org/sdr/DALA2017112808353.md): Skin · cracked · Nov 27, 2017 · N995AT · Boeing 717200 · Wing, Plate/Skin
  > CRACK ON INBOARD RT WING BUTE DOOR. INNER SKIN WAS REPLACED PER DWG 5919571 REV BG AND SRM 51-41-02.
- [SDR DALA2017112608328](https://openairdocs.org/sdr/DALA2017112608328.md): Skin · damaged · Nov 26, 2017 · N995AT · Boeing 717200 · Trailing Edge Flaps
  > ELONGATED SCREW HOLES AT LOWER SKIN. THE SKIN DOUBLER WAS REPLACED IAW SRM 51-41-01, AND DWG 5919571, REV BG.
- [SDR DALA2017112608327](https://openairdocs.org/sdr/DALA2017112608327.md): Cusp Web · cracked · Nov 25, 2017 · N995AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON THE RT CUSP WEB BETWEEN BS 650 - 655, RBL 54 TO 60. THE CUSP WEB WAS REPAIRED IAW ER/A 562407-14, REV ORIGINAL AND ETI 17-17-243, REV 2.
- [SDR DALA2017112508326](https://openairdocs.org/sdr/DALA2017112508326.md): Doubler · corroded · Nov 24, 2017 · N995AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON THE AFT CARGO BAY PRODUCTION DOUBLER IN THE JAMB AREA BETWEEN BS 965 - 979, LONGERONS 27 - 28R.
- [SDR DALA2017112408325](https://openairdocs.org/sdr/DALA2017112408325.md): Skin · cracked · Nov 23, 2017 · N995AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > CRACK ON VERTICAL STABILIZER SKIN. THE SKIN WAS REPLACED IAW SRM 51-41-02 0G, 51-40-05 0G, AND DWG 5936143, REV AS.
- [SDR DALA2017112408324](https://openairdocs.org/sdr/DALA2017112408324.md): Cargo Track · corroded · Nov 23, 2017 · N995AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON THE CARGO TRACK BS 892 TO 954 IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01, 51-41-05, AND 51-41-02.
- [SDR DALA2017112408323](https://openairdocs.org/sdr/DALA2017112408323.md): Cargo Track · corroded · Nov 23, 2017 · N995AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON THE CARGO TRACK BS 994 TO 1022, IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01.
- [SDR DALA2017112408322](https://openairdocs.org/sdr/DALA2017112408322.md): Cargo Track · corroded · Nov 23, 2017 · N995AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON CARGO TRACK BS 813 TO 1022 LT SIDE IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01, AND 51-41-05.
- [SDR DALA2017112408321](https://openairdocs.org/sdr/DALA2017112408321.md): Stiffener · cracked · Nov 23, 2017 · N995AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CRACKED STIFFENER AT THE 12 HR POSITION, ON AFT CABIN PRESSURE BULKHEAD. THE STIFFENER WAS REPLACED IAW DWG 9915562, REV P, AND SRM 51-41-05.

Next page: https://openairdocs.org/aircraft/N995AT/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 = 'N995AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N995AT/reports

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