# Service difficulty reports: N952AT

A list on [N952AT](https://openairdocs.org/aircraft/N952AT.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 · 251 reports

- [SDR DALA2026062503779](https://openairdocs.org/sdr/DALA2026062503779.md): Slide · no discrepancy · Jun 24, 2026 · N952AT · Boeing 717200 · Escape Slide
  > L1 DOOR SLIDE REMOVED FOR MTC REF AMDS W/C 2561-9004. INSTALLED L1 DOOR SLIDE PER AMDS WORK CARD 2561-9004. (8908875) (AIRCRAFT GROUNDED)
- [SDR DALA2026031801858](https://openairdocs.org/sdr/DALA2026031801858.md): Pan · cracked · Mar 12, 2026 · N952AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED WAS FOUND ON INNER PAN (FWD SIDE)Y 964 BEAM 4 ALSO CRACKED INNER PAN (AFT SIDE)Y 994 BEAM 5 AT AFT CARGO COMPARTMENT DOOR. REPAIRED PER ER/A 631760-14. (1491413)
- [SDR DALA2026031301747](https://openairdocs.org/sdr/DALA2026031301747.md): Access Panel · damaged · Mar 12, 2026 · N952AT · Boeing 717200 · Elevator, Plate/Skin
  > ELONGATED FASTENER HOLE ON ACCESS PANEL NBR:340UT AT RH ELEVATOR, AND ON 330ST AT LH ELEVATOR. REPAIRED PER ER/A NO. 631774-14 (1490586)
- [SDR DALA2026031301749](https://openairdocs.org/sdr/DALA2026031301749.md): Support Angle · cracked · Mar 10, 2026 · N952AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE SUPPORT STA Y=713 X=44 AT PAXCABIN WINGBOX AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 631793-14 (1488643)
- [SDR DALA2026031301746](https://openairdocs.org/sdr/DALA2026031301746.md): Frame Angle · cracked · Mar 10, 2026 · N952AT · Boeing 717200 · Fuselage Main, Frame
  > SHIP 9511 CRACK ON ANGLE OF FRAME STA 1153 AND BTW S1 TO S2L ALSO MISSING FASTENER ON SAME POSITION AFT ACCESSORY COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A 632751-14 REV. (1488330)
- [SDR DALA2026031001642](https://openairdocs.org/sdr/DALA2026031001642.md): Door Frame · cracked · Mar 7, 2026 · N952AT · Boeing 717200 · Fuselage Main, Structure
  > SHIP 9511 CRACK ON HOLE DOOR JAMB BTW STA Y=946 TO Y= 948 APROX LONG 28 RH BELOW TIE TRACK AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 51-70-10 (1484047)
- [SDR DALA2026030501524](https://openairdocs.org/sdr/DALA2026030501524.md): Longeron · corroded · Mar 3, 2026 · N952AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > AFTER REMOVING CORROSION ON LONGERON 30, BTW BS 1022 - 927 IN THE AFT CARGO BAY. REPLACED IAW SRM 51-41-02-0G AND SRM 51-41-05-0G. (1477180)
- [SDR DALA2026030201421](https://openairdocs.org/sdr/DALA2026030201421.md): Skin · cracked · Feb 26, 2026 · N952AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN STA Y = 1087 LONG 13 LH-14LH SIDE. REPAIR AND PRI 631743-14 (1469678)
- [SDR DALA2026030201420](https://openairdocs.org/sdr/DALA2026030201420.md): Hinge Fitting · corroded · Feb 26, 2026 · N952AT · Boeing 717200 · Trailing Edge Flaps
  > CORROSION WAS FOUND ON INB AND OUT HOLES (4EAS) UPPER AND LOWER HINGE FLAP ALSO ON SETTLEMENT AREA. REPAIRED PRI 631842-14 REV 2 AND ER/A 631842-14. (1469307)
- [SDR DALA2026030201417](https://openairdocs.org/sdr/DALA2026030201417.md): Skin · cracked · Feb 24, 2026 · N952AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN STA Y =1037 LONG 13 LH-14LH SIDE. REPAIRED PER PRI 631741-14 (1466248)
- [SDR DALA2026021801177](https://openairdocs.org/sdr/DALA2026021801177.md): Cusp Web · cracked · Feb 17, 2026 · N952AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AIRCRAFT 9511, CRACK WAS FOUND ON CUSP WEB AT X=-44 BTW BS 636 - 655 AT PAX CABIN. CRACKED ON CUSP WEB AT X=-44 BTW STA Y=636 - 655 AT PAX CABIN WAS REPAIRED PER SRM 53-00-55-2R, PROCEDURE 4, REPAIR 4, PAR 5 (19), FIGURE 221. (LP 1454694)
- [SDR DALA2026021801124](https://openairdocs.org/sdr/DALA2026021801124.md): Frame · cracked · Feb 15, 2026 · N952AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKS ON LT & RT FRAMES BS 1037 LONGERON 17. DAMAGED AREA REPAIRED IAW SRM 53-20-07 (1452565).
- [SDR DALA2026021801123](https://openairdocs.org/sdr/DALA2026021801123.md): Cusp Web · corroded · Feb 14, 2026 · N952AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORRODED CUSP WEB, BS 794 - 813, X= 55. DAMAGED AREA REPAIRED IAW SRM 53-20-07. (1451076).
- [SDR DALA2026021801122](https://openairdocs.org/sdr/DALA2026021801122.md): Cusp Web · corroded · Feb 13, 2026 · N952AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LT CUSP WEB BTW BS 380 - 389, BS 461 - 465, BS 503 - 522. DAMAGED AREA REPAIRED IAW SRM 53-20-07. (1449930).
- [SDR DALA2026021801121](https://openairdocs.org/sdr/DALA2026021801121.md): Floor Support · corroded · Feb 13, 2026 · N952AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS BTW BS 195, X= 18 - 22, BS 200, X=10 - 15, & BS 200, X=12 TO X=44. DAMAGED AREA REPAIRED IAW SRM 51-41-02. (1449816).
- [SDR DALA2026021801119](https://openairdocs.org/sdr/DALA2026021801119.md): Skin · cracked · Feb 13, 2026 · N952AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKED FUSELAGE SKIN, BTW LONGERONS 13 - 14R BS 1022. DAMAGED AREA REPAIRED IAW ER/A 631752-14. (1449591).
- [SDR DALA2026021801117](https://openairdocs.org/sdr/DALA2026021801117.md): Floor Support · corroded · Feb 12, 2026 · N952AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS BTW BS 60 - 200, X=56. DAMAGED AREA REPAIRED IAW SRM 51-41-05 (1448041).
- [SDR DALA2026021801116](https://openairdocs.org/sdr/DALA2026021801116.md): Web · cracked · Feb 11, 2026 · N952AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED LOWER WEB, BS 674, X= - 44.5, DAMAGED AREA REPAIRED IAW SRM 53-00-55. (1446890).
- [SDR DALA2026021801131](https://openairdocs.org/sdr/DALA2026021801131.md): Cusp Web · punctured · Feb 11, 2026 · N952AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > PUNCTURED CUSP WEB, BS 678, X=- 54. DAMAGED AREA REPAIRED IAW SRM 53-00-55. (1446439)
- [SDR DALA2026021801130](https://openairdocs.org/sdr/DALA2026021801130.md): Cusp Web · cracked · Feb 11, 2026 · N952AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED LOWER SURFACE OF RT CUPS WEB BS 219, 238, 654, 896, AND 942. DAMAGED AREA REPAIRED IAW SRM 53-00-55-2R (1446401).
- [SDR DALA2026021801125](https://openairdocs.org/sdr/DALA2026021801125.md): Hinge Fitting · damaged · Feb 10, 2026 · N952AT · Boeing 717200 · Trailing Edge Flaps
  > DAMAGED RT WING FLAP HINGE FITTING AT XW=251.68 28. DAMAGED AREA REPAIRED IAW ER/A 00-631842 (1445336).
- [SDR DALA2026020900907](https://openairdocs.org/sdr/DALA2026020900907.md): Vane · nicked · Feb 4, 2026 · N952AT · Boeing 717200 · Trailing Edge Flaps
  > INITIAL INSPECTION: NICKS (2EA) ON AFT FLAP MOVEABLE VANE LOWER SURFACE AT LT WING. REPAIRED IAW SRM 51-70-02, AND SRM 57-53-01 (1435960)
- [SDR DALA2026012700602](https://openairdocs.org/sdr/DALA2026012700602.md): Pan · cracked · Jan 25, 2026 · N952AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACKED OUTER PAN BS 370 BEAM 3 AT FWD CARGO DOOR. REPAIRED IAW SRM 52-30-02 (1418911)
- [SDR DALA2026012700601](https://openairdocs.org/sdr/DALA2026012700601.md): Cusp Web · cracked · Jan 21, 2026 · N952AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED LOWER SURFACE OF LT CUSP WEB, BS 258 - 814. REPAIRED IAW SRM 53-00-55. (1413152)
- [SDR DALA2025102407792](https://openairdocs.org/sdr/DALA2025102407792.md): Doubler · not reported · Oct 21, 2025 · N952AT · Boeing 717200 · Wing, Plate/Skin
  > EXISTING REPAIRS FOUND THAT IMPACTS INSPECTION ACCOMPLISHMENT. REPAIR INVESTIGATION REQUIRED PRIOR TO FURTHER FLIGHT. PERFORMED DOUBLER INSPECTION PER ERA 625837-14 AD (7976471)
- [SDR DALA2025082606325](https://openairdocs.org/sdr/DALA2025082606325.md): Fitting · leaking · Aug 22, 2025 · N952AT · Boeing 717200 · Fuel Storage
  > FUEL LEAK THROUGH FLAP HINGE BRACE FITTING ATTACHING FASTENERS AT LEFT WING STA XRS=164. LH WING AFT LOWER SKIN DOUBLER AT STA XRS= 164 WAS REPAIRED PER PRI 624486-14 (1157598)
- [SDR DALA2025082606324](https://openairdocs.org/sdr/DALA2025082606324.md): Skin · leaking · Aug 20, 2025 · N952AT · Boeing 717200 · Wing, Plate/Skin
  > RIGHT WING LOWER SKIN, XRS -164 AT FLAP BRACE FITTING FUEL LEAK TIME LIMITED REPAIR. REPAIRED RH LOWER WING SKIN PER ERA 625837-14AD REV ORIGINAL SECTION I TIME LIMITED REPAIR. REPETITIVE INSPECTION EVERY 90 DAYS FROM AUG 15 PER ERA 625837-14AD (1154482)
- [SDR DALA2025013000724](https://openairdocs.org/sdr/DALA2025013000724.md): Safety Pin · missing · Jan 29, 2025 · N952AT · Boeing 717200 · Escape Slide
  > MISSING SAFETY PIN OF SLIDE R1 DOOR. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF THE NRC 00084: SAFETY PIN WAS INSTALLED ON SLIDE R1 DOOR PER B717-200 AMM 25-61-03-000-801 STEP B.(
- [SDR DALA2025012900689](https://openairdocs.org/sdr/DALA2025012900689.md): Doubler · corroded · Jan 29, 2025 · N952AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON DOUBLER REPAIR, BTW PROJECTION LONGS 26/27RH AT AFT CARGO DOOR, FWD JAMB C2. SUMMARY OF NRC 00010: CORROSION LEVEL 2. DOUBLER REPAIR BTW PROJECTION LONGS 26/27RH AT AFT CARGO DOOR, FWD JAMB C2 WAS MANUFACTURED AND REPLACED PER B717-200 SRM 53-20-1
- [SDR DALA2024111911029](https://openairdocs.org/sdr/DALA2024111911029.md): Light · inoperative · Nov 17, 2024 · N952AT · Boeing 717200 · Emergency Lighting
  > THE CABIN CEILING MOUNTED EMERGENCY LIGHT AT 2AB IS INOPERATIVE. FORWARD TO MEL 33-51-01A. PLACARDS INSTALLED. ON 18NOV24 MAINTENANCE REPLACED THE 2AB CABIN CEILING STANBY LIGHTING ASSEMBLY PER B717 AMM 33-52. OPERATIONAL CHECK WAS GOOD. MCO AND PLACARD WERE R
- [SDR DALA2024072307417](https://openairdocs.org/sdr/DALA2024072307417.md): Power Supply · inoperative · Jul 23, 2024 · N952AT · Boeing 717200 · Emergency Lighting
  > PANELS 1-5 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY B5-227 BATTERY PER B717 AMM 33-51. (LP #6208532)
- [SDR DALA2024070506805](https://openairdocs.org/sdr/DALA2024070506805.md): Battery Pack · no test · Jul 4, 2024 · N952AT · Boeing 717200 · Emergency Lighting
  > AIRCRAFT 9511, DURING SVC CHECK FOUND MID CABIN EMER LIGHTS INOP.CORRECTIVE ACTION: REPLACED MID CABIN EMER LIGHTS BATTERY PACK. (LP 6209356)
- [SDR DALA2023031401852](https://openairdocs.org/sdr/DALA2023031401852.md): Unknown · unknown · Mar 12, 2023 · N952AT · Boeing 717200 · Trailing Edge Flaps
  > INTERFERENCE BETWEEN FITTING TO ATTACH RIGHT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PANEL 630AF AT RH WING FLAP INTERNAL STRUCTURE. SUMMARY OF NRC 00105: FITTING TO ATTACH RIGHT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS P
- [SDR DALA2023031401851](https://openairdocs.org/sdr/DALA2023031401851.md): Unknown · unknown · Mar 12, 2023 · N952AT · Boeing 717200 · Trailing Edge Flaps
  > INTERFERENCE BETWEEN FITTING TO ATTACH LEFT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PANEL 530AF AT LH WING FLAP INTERNAL STRUCTURE. SUMMARY OF NRC 00060: FITTING TO ATTACH LEFT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PAN
- [SDR DALA2023031401849](https://openairdocs.org/sdr/DALA2023031401849.md): Unknown · unknown · Mar 12, 2023 · N952AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION AT INTERNAL FUSELAGE SKIN ON STA Y=636 TO Y=655 BTW STR 29LH AND STR 29RH AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00189: CORROSION LEVEL 2. CORROSION AT INTERNAL FUSELAGE SKIN ON STA Y=636 TO Y=655 BTW STR 29LH AND STR 29RH AT FWD CARGO COMPARTMENT
- [SDR DALA2023031401846](https://openairdocs.org/sdr/DALA2023031401846.md): Unknown · unknown · Mar 10, 2023 · N952AT · Boeing 717200 · Fuselage Main, Frame
  > AFT SPLICE BTW L-28R TO L-28L REMOVAL, FOUND CRACK ON SPLICE FRAME AT STA 636. SUMMARY OF NRC 00244: SPLICE FRAME AT STA 636 WAS REPAIRED PER B-717-200 SRM 51-70-11-2R PROCEDURE 2 REPAIR 2. (LP #2664206)
- [SDR DALA2023030801720](https://openairdocs.org/sdr/DALA2023030801720.md): None · none · Mar 7, 2023 · N952AT · Boeing 717200 · Fuselage Floor Panel
  > AFTER DOOR ASSEMBLY, CORROSION WAS FOUND ON SETTLEMENT AREA AT DOOR PANEL P/N 5971074. SUMMARY OF NRC 0240: LEVEL CORROSION 2. (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON SETTLEMENT AREA AT DOOR PANEL. WAS MEASURED WITH AN ORIGINAL THICKNESS OF 0.090 IN. RE
- [SDR DALA2023030701661](https://openairdocs.org/sdr/DALA2023030701661.md): None · none · Mar 6, 2023 · N952AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ALONG LONGERON L30 FROM STA Y=900 TO Y=1022 AT AFT CARGO COMPARTMENT C2. SUMMARY OF NRC 00178: CORROSION LEVEL 2. NEW SECTION LONGERON L30 FROM STA Y=900 TO Y=1022 WAS INSTALLED PER B717-200 SRM 51- 41-05-0G. (LP #2658653)
- [SDR DALA2023030701660](https://openairdocs.org/sdr/DALA2023030701660.md): None · none · Mar 6, 2023 · N952AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERION 30 RH BTW STA Y=1031 TO STA Y=1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00195: CORROSION LEVEL 2. LONGERON SECTION 30 FROM STA Y=1022 TO Y=1053 AT AFT CARGO COMPARTMENT C2 WAS REPLACED PER B717-200 SRM 51-41-05-0G STEP 8. AND 51-41-0
- [SDR DALA2023030701658](https://openairdocs.org/sdr/DALA2023030701658.md): None · none · Mar 3, 2023 · N952AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN ON STA Y=1053 BTW STR 29 LH TO STR 29 RH AT AFT CARGO COMPARTMENT. CORROSION WAS FOUND ON PRODUCTION DOUBLER. SUMMARY OF NRC 00241: CORROSION LEVEL 2. DOUBLER ON STA 1053 BTW LONGERON 28RH TO 28LH WAS REPLACED PER B717 SRM 51-41-02-0
- [SDR DALA2023030301615](https://openairdocs.org/sdr/DALA2023030301615.md): None · none · Mar 2, 2023 · N952AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON FRAME CLIP ON AFT CARGO COMPARTMENT C2 STA Y=908 BTW LONG L30/L29. SUMMARY OF NRC 00174: CORROSION LEVEL 2. SECTION ON FRAME CLIP ON AFT CARGO COMPARTMENT C2 STA Y=908 BTW LONG L30/L29 WAS REPAIRED PER B717-200 SRM 53-00-06-2R-2. (LP #2652378)
- [SDR DALA2023030201554](https://openairdocs.org/sdr/DALA2023030201554.md): None · none · Mar 1, 2023 · N952AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON INTERCOSTAL AT STR 30 BTW STA Y=1022 TO STA Y=1037 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00193: CORROSION LEVEL 2. INTERCOSTAL AT STR 30 BTW STA Y=1022 TO STA Y=1037 WAS REPLACED PER B-717 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #2651008)
- [SDR DALA2023030201553](https://openairdocs.org/sdr/DALA2023030201553.md): None · none · Mar 1, 2023 · N952AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON FRAME CLIP AND SKIN ON AFT CARGO COMPARTMENT C2 STA Y=1022 BTW LONG L30. SUMMARY OF NRC 00182: CORROSION LEVEL 2. SECTION ON FRAME CLIP AFT CARGO COMPARTMENT C2 STA Y=1022 BTW LONG 29RH TO 29LH WAS REPAIRED PER B717-200 SRM 53-00-06-2R-2 FIG 201 A
- [SDR DALA2023022701428](https://openairdocs.org/sdr/DALA2023022701428.md): None · none · Feb 25, 2023 · N952AT · Boeing 717200 · Fuselage Floor Panel
  > CRACKED PAN ON AFT EDGE BELOW STOP FITTING #2 AT PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE. SUMMARY OF NRC 00235: PAN ON AFT EDGE BELOW STOP FITTING #2 AT PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #2644
- [SDR DALA2023022501420](https://openairdocs.org/sdr/DALA2023022501420.md): None · none · Feb 24, 2023 · N952AT · Boeing 717200 · Fuselage Floor Panel
  > CRACKED BEAM ON AFT SECTION BELOW STOP FITTING #2 AT PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE. SUMMARY OF NRC 00236: BEAM ON AFT SECTION BELOW STOP FITTING #2 AT PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 8. (
- [SDR DALA2023022201324](https://openairdocs.org/sdr/DALA2023022201324.md): None · none · Feb 21, 2023 · N952AT · Boeing 717200 · Fuselage Main, Frame
  > SECONDARY IN REF TO AMDS 5310-01436-01A: CRACK ON CUSP MEMBRANE WEB AT STA 674 L-18 LH. SUMMARY NRC 00198: CUSP MEMBRANE WEB AT STA 674 L-18 LH WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE 203. (LP #2637942)
- [SDR DALA2023022001258](https://openairdocs.org/sdr/DALA2023022001258.md): None · none · Feb 19, 2023 · N952AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON CUSP MEMBRANE WEB AT STA 696 L-18 LH. SUMMARY OF NRC 0209: CUSP MEMBRANE WEB WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE 203. (LP #2636060)
- [SDR DALA2022112307517](https://openairdocs.org/sdr/DALA2022112307517.md): Lens · missing · Nov 22, 2022 · N952AT · Boeing 717200 · Emergency Lighting
  > THE EXIT SIGN AT DOOR 1R IS MISSING. MAINTENANCE REPLACED THE MISSING LENS IAW B717 AMM 33-51. (LP #8566118)
- [SDR DALA2022062104328](https://openairdocs.org/sdr/DALA2022062104328.md): Battery Pack · inoperative · Jun 20, 2022 · N952AT · Boeing 717200 · Emergency Lighting
  > THE TAIL COMPARTMENT (CATWALK) AFT EMERGENCY CEILING LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK, B5-116, PER B-717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. (LP #8057681)
- [SDR DALA2022052003458](https://openairdocs.org/sdr/DALA2022052003458.md): Strip · missing · May 20, 2022 · N952AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY ESCAPE PATH LIGHTING STRIP AT ROW 19AB IS MISSING. MAINTENANCE INSTALLED A NEW EEPL INDIGO TAPE STRIP AND END CAPS. THE LUMINESCENT STRIP IS NOW OK FOR SERVICE. (LP #2243238)

Next page: https://openairdocs.org/aircraft/N952AT/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 = 'N952AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N952AT/reports

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