# Service difficulty reports: N982AT

A list on [N982AT](https://openairdocs.org/aircraft/N982AT.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 · 202 reports

- [SDR DALA2026101305627](https://openairdocs.org/sdr/DALA2026101305627.md): Battery Pack · inoperative · Oct 12, 2026 · N982AT · Boeing 717200 · Emergency Lighting
  > EXTERIOR EMERGENCY ILLUMINATION SYSTEM. INSTALLED NEW BATTERY IN POWER SUPPLY, B5-125, REF B717 AMM 33-51. OPS CK GOOD. (9456246) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026101305628](https://openairdocs.org/sdr/DALA2026101305628.md): Battery Pack · inoperative · Oct 11, 2026 · N982AT · Boeing 717200 · Emergency Lighting
  > TAIL COMP EMERG PATHWAY AND AFT DOOR EXIT LIGHTS INOP. REMOVED AND REPLACE EMERG LIGHT BATTERY ASSEMBLY B5-260 PER B717 AMM 33-51. (9456237) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026100605532](https://openairdocs.org/sdr/DALA2026100605532.md): Sign · detached · Oct 5, 2026 · N982AT · Boeing 717200 · Emergency Lighting
  > EXIT SIGN HANGING BY WIRES. FOUND LIGHT ASSY DAMGED UNABLE TO SECURE. REMOVED AND REPLACED EMERGENCY EXIT SIGN (FWD) PER AMM 33-51 OPS CHECK GOOD. (9456216) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026090805038](https://openairdocs.org/sdr/DALA2026090805038.md): Indication Sys · faulted · Sep 6, 2026 · N982AT · Boeing 717200 · Engine Indicating System
  > RTO- DISCONTINUED TAKE OFF AT THROTTLE UP IN ATL DUE TO AMBER XXS ON BOTH N1 AND N2 VIBE INDICATIONS. CREW RESET C/B AND DATA RETURNED. TROUBLESHOT PER B717 FIM 77-31. PERFORMED EVEM BITE. NO CURRENT OR PREVIOUS FAULTS FOUND. EVEM RTS PASS PER B717 AMM 77-31
- [SDR DALA2026081204642](https://openairdocs.org/sdr/DALA2026081204642.md): Battery · inoperative · Aug 11, 2026 · N982AT · Boeing 717200 · Emergency Lighting
  > BATTERY FOR EXTERIOR EMERGENCY LIGHTS NEEDS REPLACING. R & R OVERWING EMERGENCY EVACUATION BATTERY IAW AMM 33-51-06. OPS CHECKED GOOD. (8804496) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026070103876](https://openairdocs.org/sdr/DALA2026070103876.md): Proximity Sensor · out of adjust · Jun 29, 2026 · N982AT · Boeing 717200 · Door Warning System
  > AFT BULKHEAD DOOR WARNING ANNUNCIATION SYSTEMS, PERFORMED ADJUSTMENT OF AFT B/H DOOR PROX SENSOR IAW B717 AMM 52 -70/803. (1672780) (AICRAFT GROUNDED).
- [SDR DALA2026062503780](https://openairdocs.org/sdr/DALA2026062503780.md): Battery Pack · inoperative · Jun 24, 2026 · N982AT · Boeing 717200 · Emergency Lighting
  > LT & RT WING EMERGENCY LIGHT INOPERATIVE. R & R WING EMERGEMCY LIGHT BATTERY PER AMM 33-51. OPS CHKD GOOD OK FOR SVC. (8873908) (AIRCRAFT GROUNDED)
- [SDR DALA2026033002079](https://openairdocs.org/sdr/DALA2026033002079.md): Angle · cracked · Mar 25, 2026 · N982AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE, BS 1178, ABOVE LT PYLON, EXTERNAL FUSELAGE. REPAIRED IAW ER/A 633070-14. (1511986)
- [SDR DALA2026032501992](https://openairdocs.org/sdr/DALA2026032501992.md): None · none · Mar 24, 2026 · N982AT · Boeing 717200 · Standard Practices/Structures
  > ERA 633129-14 SECTION I ISSUED FOR REPAIR TO BS 1076, L14R SKIN FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH ERA 633129-14 (1510528)
- [SDR DALA2026032501991](https://openairdocs.org/sdr/DALA2026032501991.md): Skin · cracked · Mar 24, 2026 · N982AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL FUSELAGE SKIN BTW BS 1076, LONGERONS 13-14 RT. REPAIRED PER ER/A 633129-14 (1510684)
- [SDR DALA2026032401967](https://openairdocs.org/sdr/DALA2026032401967.md): Frame · cracked · Mar 19, 2026 · N982AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK WAS FOUND IN OVERWING FRAME TAB Y= 696 RH SIDE AT PAX CABIN. CORRECTIVE ACTION: OVERWING FRAME TAB Y= 696 RH SIDE AT PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-02-0G, SRM 51-41-05 (1502762)
- [SDR DALA2026030501525](https://openairdocs.org/sdr/DALA2026030501525.md): Bracket · loose · Mar 3, 2026 · N982AT · Boeing 717200 · Fuselage Main, Attach Fittings
  > ATO- CREW ABORTED TAKEOFF AT 20 KTS FOR AN AFT BULKHEAD DOOR WARNING. MAINTENANCE FOUND AFT CABIN BULKHEAD DOOR SENSOR BRACKET LOOSE AND RESECURED.(1477597)
- [SDR DALA2025111108262](https://openairdocs.org/sdr/DALA2025111108262.md): Proximity Sensor · faulted · Nov 7, 2025 · N982AT · Boeing 717200 · Door Warning System
  > AFT BULKHEAD DOOR CAUTION MESSAGE ON TAXI OUT FOR TAKEOFF. T/S PER FIM 52-70-00-810-809 CHECK PSEU SENSOR. CLEAN AND ADJUST PROX SENSOR PER B717 AMM 52-70 (7521980)
- [SDR DALA2025081806159](https://openairdocs.org/sdr/DALA2025081806159.md): Proximity Sensor · faulted · Aug 12, 2025 · N982AT · Boeing 717200 · Door Warning System
  > ABORTED TAKEOFF APPROX. 35KTS DUE TO AFT CABIN BULKHEAD DOOR INDICATION. REPLACED BULKHEAD DOOR PROX SENSOR. OK FOR SERVICE.(1140292)
- [SDR DALA2025071005217](https://openairdocs.org/sdr/DALA2025071005217.md): Battery Pack · inoperative · Jul 9, 2025 · N982AT · Boeing 717200 · Emergency Lighting
  > AIRCRAFT 9549, BOTH EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. CORRECTIVE ACTION: REPLACED OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY PER B717 AMM 33-51. OPS CHECK GOOD. (LP 7315329)
- [SDR DALA2024032503740](https://openairdocs.org/sdr/DALA2024032503740.md): Power Supply · inoperative · Mar 23, 2024 · N982AT · Boeing 717200 · Emergency Lighting
  > DURING CHECK OF THE EXTERIOR LIGHTS, LH/RH EMERGENCY LIGHTS WERE INOPERATIVE. SUMMARY OF NRC 00959: OVERWING EMERGENCY EVACUATION LIGHTS BATTERY POWER SUPPLY WAS REPLACED WITH A SERVICEABLE ONE PER B717 AMM 33-51-06. (LP #0258403)
- [SDR DALA2024032303703](https://openairdocs.org/sdr/DALA2024032303703.md): Skin · cracked · Mar 22, 2024 · N982AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS ON SKIN WERE FOUND AFTER REMOVAL STOP FITTING ON AFT EDGE BEAM 2 APROX. SUMMARY OF NRC 00531: SKIN ON AFT EDGE BEAM 2 APROX WAS REPAIRED PER PRI 615938-14 REV 1 AND ERA 615938-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-615938 ADDED FOR A
- [SDR DALA2024032203632](https://openairdocs.org/sdr/DALA2024032203632.md): Skin · cracked · Mar 21, 2024 · N982AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS ON FUSELAGE SKIN (2 EA) ON STA Y1154 BTW L3 LH AND L3 RH (UPPER SECTION) AT FUSELAGE. SUMMARY OF NRC 00072: FUSELAGE SKIN ON STA Y1154 BTW L3 LH AND L3 RH (UPPER SECTION) WAS REPAIRED PER ERA 615858-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPETITIV
- [SDR DALA2024032103586](https://openairdocs.org/sdr/DALA2024032103586.md): Skin · worn · Mar 20, 2024 · N982AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > WEAR ON EXTERNAL FUSELAGE SKIN STA Y=994 BTW LONGERON 25R/L26R. SUMMARY OF NRC 00018: EXTERNAL FUSELAGE SKIN STA Y=994 BTW LONGERON 25R/L26R WAS REPAIRED PER ERA 577681-14 REV B SECTION II: PERMANENT REPAIR AND PRI 577681-14 REV 1 PART C. REPAIR APPROVAL IS LI
- [SDR DALA2024032103575](https://openairdocs.org/sdr/DALA2024032103575.md): Fitting · worn · Mar 16, 2024 · N982AT · Boeing 717200 · Wing, Attach Fittings
  > WEAR ON TRACK FITTING SUPPORT OF SETTLEMENT AREA OF INBD SPOILER STA XTE 162 AND OTBD SPOILER XTE 341. SUMMARY OF NRC 00134: FITTING SUPPORT OF SETTLEMENT AREA OF INBD SPOILER STA XTE 162 WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G
- [SDR DALA2024031203224](https://openairdocs.org/sdr/DALA2024031203224.md): Floor Support · corroded · Mar 11, 2024 · N982AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT STA Y=160 TO Y=200 X= 6, Y=180 BTW -X=10 TO -X=43, Y= 200 BTW -X=46 TO -X=50 AND Y=200 BTW X=5 TO -X=5 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00681: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=160 TO Y=200 X= 6, Y=180 BTW -X=10 TO -
- [SDR DALA2024030803180](https://openairdocs.org/sdr/DALA2024030803180.md): Pan · cracked · Mar 7, 2024 · N982AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON L1 DOOR PANE FWD SIDE BTW #1 BEAM AND UPPER EDGE STA 168. SUMMARY OF NRC 00704: L1 DOOR PAN FWD SIDE BTW #1 BEAM AND UPPER EDGE STA 168 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. (LP #0234210)
- [SDR DALA2024030503009](https://openairdocs.org/sdr/DALA2024030503009.md): Frame · cracked · Mar 5, 2024 · N982AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME CLIP STA Y=908 BTW LONG 28L AND 28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00241: CORROSION LEVEL 2. FRAME CLIP STA Y=908 BTW LONG 28L AND 28R AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0230532
- [SDR DALA2025103107962](https://openairdocs.org/sdr/DALA2025103107962.md): Vane · corroded · Mar 3, 2024 · N982AT · Boeing 717200 · Trailing Edge Flaps
  > CORROSION ON LOWER SKIN OF OUTBD FLAP VANE AT RT WING. OTBD FLAP VANE AT RT WING WAS REPLACED BY ONE SERVICEABLE OTBD FLAP VANE (0228760).
- [SDR DALA2024031103220](https://openairdocs.org/sdr/DALA2024031103220.md): Skin · damaged · Feb 29, 2024 · N982AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN RH WINDOW BELT AT STA 446-465, WINDOW 12 LOWER FWD CORNER HAS A LIGHTNING STRIKE. REPAIRED FUSELAGE SKIN RH WINDOW BELT AT STA 446-465, WINDOW 12 LOWER FWD CORNER PER ERA 596251-14AD REV A SECTION III TIME LIMITED REPAIR. REPETITIVELY INSPECT THE
- [SDR DALA2024022902793](https://openairdocs.org/sdr/DALA2024022902793.md): Doubler · cracked · Feb 28, 2024 · N982AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON HANDLE DOUBLER STA Y=396 AT FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC: 00120. HANDLE DOUBLER STA Y=396 AT FWD CARGO COMPARMENT DOOR WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 52-30-01-2R PROCEDURE 1 REPAIR 1. (LP #0222418)
- [SDR DALA2024022802764](https://openairdocs.org/sdr/DALA2024022802764.md): Strip · corroded · Feb 27, 2024 · N982AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON STRIP BESIDE RH TIE TRACK BTW STA 332 TO 370 FWD CARGO COMPARTMENT. SUMMARY OF NRC 00625: CORROSION LEVEL 2. STRIP BESIDE RH TIE TRACK BTW STA 332 TO 370 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-08-0G. (LP #0221234)
- [SDR DALA2024022002323](https://openairdocs.org/sdr/DALA2024022002323.md): Cusp Web · cracked · Feb 17, 2024 · N982AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK WAS FOUND AT CUSP MEMBRANE (LWR SKIN) BTW STA Y=218 AND X=60 APPROX PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00678: CUSP MEMBRANE (LWR SKIN) BTW STA Y=218 AND X=60 APPROX WAS REPAIRED PER B-717 SRM 53-00-55-2R-4 FIG.215. (LP #0206279)
- [SDR DALA2024021602272](https://openairdocs.org/sdr/DALA2024021602272.md): Cusp Web · cracked · Feb 16, 2024 · N982AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON RH CUSP WEB (LOWER SURFACE) STA Y=672 X=- 57 AT PASSENGER CABIN. SUMMARY OF NRC 00527: RH CUSP WEB STA Y=672 X=- 57 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND AFTER T
- [SDR DALA2024021602271](https://openairdocs.org/sdr/DALA2024021602271.md): Cusp Web · cracked · Feb 16, 2024 · N982AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON RH CUSP WEB STA Y=245 X=-60 AT PASSENGER CABIN. SUMMARY OF NRC 00518: RH CUSP WEB STA Y=245 X=-60 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ALONG THE CUT OUT EDGES, NO CRACKS WERE FOUND PER
- [SDR DALA2024021602270](https://openairdocs.org/sdr/DALA2024021602270.md): Doubler · corroded · Feb 16, 2024 · N982AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON RH PREVIOUS REPAIR DOUBLERS STA Y=451-464 AND Y=479 (LOWER SURFACE) X=-60 AT PASSENGER CABIN. SUMMARY OF NRC 00524: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER STA Y=451-464 AND Y=479 (LOWER SURFACE) X=- 60 AT PASSENGER CABIN WAS REPLACED PER B717-
- [SDR DALA2023020600883](https://openairdocs.org/sdr/DALA2023020600883.md): Not Reported · not reported · Feb 4, 2023 · N982AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS AT THE LOWER AFT, LT AND RT OVERWING EMERGENCY DOORS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY B5-119 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4138625)
- [SDR DALA2022080205279](https://openairdocs.org/sdr/DALA2022080205279.md): Bulkhead · damaged · Jul 28, 2022 · N982AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DURING EXTENSION AND RETRACTION OF NLG RETRACT ACTUATOR PER STEP 22 FOLLOWING GEAR MAINTENANCE, THE ACTUATOR CONTACTED THE REAR WHEELWELL BULKHEAD CAUSING DAMAGE. NRC 005-0003:3221-4001/013 00035; REPAIRED IAW ER/A 601048-14 REV. ORIG AND PER PRI 601048-14 REV
- [SDR DALA2022072605122](https://openairdocs.org/sdr/DALA2022072605122.md): None · none · Jul 22, 2022 · N982AT · Boeing 717200 · Fuselage, Landing Gear Attach Fittings
  > L/H O/B FIXED STRUT MOUNT HAS CORROSION AND TOOLING MARKS ON OUTBOARD/AFT MOUNT HOLE SURFACE. SUMMARY SEE NRC 004-0003: 3211-4003/001 00022 COMPLIED WITH PRI 600942-14 REV. 0, PRI 600942-14 REV 1, AND FINAL ER/A 600942-14 REV ORIGINAL. (LP #2331305)
- [SDR DALA2022072605123](https://openairdocs.org/sdr/DALA2022072605123.md): None · none · Jul 22, 2022 · N982AT · Boeing 717200 · Fuselage, Landing Gear Attach Fittings
  > L/H O/B FIXED STRUT MOUNT HAS CORROSION ON OUTBOARD/FWD MOUNT HOLE SURFACE. SUMMARY SEE NRC 004-0003: 3211-4003/002 00023 COMPLIED WITH PRI 600942-14 REV. 0, PRI 600942-14 REV 1, AND FINAL ER/A 600942-14 REV ORIGINAL. (LP #2331304)
- [SDR DALA2022072605121](https://openairdocs.org/sdr/DALA2022072605121.md): None · none · Jul 21, 2022 · N982AT · Boeing 717200 · Fuselage, Landing Gear Attach Fittings
  > RIGHT MLG ATTACH FITTING CHAFED AND CORRODED WHERE FIXED STRUT MOUNTS. -M- SUMMARY SEE NRC 008-0003: 3211-4004/001 00018 PRI 600916-14 REV. 0 PRI 600916-14 REV. 1 AND FINAL ER/A 600916-14 REV. ORIGINAL HAVE BEEN COMPLIED WITH. (LP #2330440)
- [SDR DALA2022050603161](https://openairdocs.org/sdr/DALA2022050603161.md): Cable Assy · broken · May 5, 2022 · N982AT · Boeing 717200 · Escape Slide
  > TAIL CONE SLIDE PACK CABLE RETAINER BROKEN. THIS ITEM IS RII PER TOPP 40-30-05 QC5146. REPLACED CABLE RETAINER PER SAFRAN CMM 25-66-20 QC 5270. (LP #8745178)
- [SDR DALA2022030201329](https://openairdocs.org/sdr/DALA2022030201329.md): None · none · Mar 2, 2022 · N982AT · Boeing 717200 · Emergency Lighting
  > THE AFT LEFT & RIGHT EMERGENCY EXIT OVERWING THRESHOLD LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-230 PER B717 AMM 33-51-04. THE EMERGENCY EXIT LIGHTS NOW OPERATE NORMALLY. (LP #8262534)
- [SDR DALA2022010700123](https://openairdocs.org/sdr/DALA2022010700123.md): Floor Support · corroded · Jan 6, 2022 · N982AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT UNDER FLOOR PANEL 221AF FOUND CORRODED. MAINTENANCE REPLACED SUPPORT PER BOEING DWG 9936534, AND B717 SRM 51-40-02. (LP #2076902)
- [SDR DALA2022010600093](https://openairdocs.org/sdr/DALA2022010600093.md): None · none · Jan 5, 2022 · N982AT · Boeing 717200 · Emergency Lighting
  > THE RIGHT HAND GALLEY CABIN EMERGENCY EXIT SIGN LIGHT HAS BROKEN WIRES. -M- SUMMARY SEE NRC 001-0010:2500-2647/113 00431: REPAIRED WIRES PER REF B717 SWPM 20-10-03. OPERATIONAL CHECK WAS GOOD. (LP #2076170)
- [SDR DALA2022010600091](https://openairdocs.org/sdr/DALA2022010600091.md): None · none · Jan 3, 2022 · N982AT · Boeing 717200 · Fuselage Floor Panel
  > AFT CARGO. FLOOR BOARD SUPPORT/FORMER CORRODED AT STA 973 STRINGERS 29 AND 30 ATTACH POINTS, 6 INCHES FWD OF ANTENNA DOUBLER. (M) FLOOR BOARD SUPPORT/FORMER AT STA 973 STRINGERS 29 AND 30 ATTACH POINTS, 6 INCHES FWD OF ANTENNA DOUBLER FOUND CRACK, FOUND TO BE
- [SDR DALA2022010400050](https://openairdocs.org/sdr/DALA2022010400050.md): None · none · Jan 2, 2022 · N982AT · Boeing 717200 · Fuselage Floor Panel
  > FLOOR BEAM CRACKED AT STATION Y=737 RH OVERWING FRAME ATTACH POINT. REPLACED FLOOR BEAM PER B717 SRM 51-40-02. (LP #2072760)
- [SDR DALA2022010400049](https://openairdocs.org/sdr/DALA2022010400049.md): None · none · Jan 2, 2022 · N982AT · Boeing 717200 · Fuselage Floor Panel
  > FLOOR BEAM CRACKED AT STATION Y=737 LH OVERWING FRAME ATTACH POINT. MAINTENANCE REPLACED FLOOR BEAM PER B717 SRM 51-40-02. (LP #2072758)
- [SDR DALA2024031103213](https://openairdocs.org/sdr/DALA2024031103213.md): Skin · damaged · Dec 28, 2021 · N982AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > RH FUSELAGE WINDOW BELT WINDOW #12 AT STA 446-465 HAD A LIGHTNING STRIKE. FOLLOW ON ACTION REQUIRED. ERA 596251-14 ISSUED. FOLLOW ON ACTION REQUIRED SECT I TBA DURING C-CHK VISIT IN MSP DEC2021. SECT II HFEC INSPECTIONS TBA AT EVERY 24 MONTH INTERVALS AFTER SE
- [SDR DALA2021081004559](https://openairdocs.org/sdr/DALA2021081004559.md): Battery Pack · failed · Aug 9, 2021 · N982AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS FAILED TO ILLUMINATE WHEN SWITCHED ON. MAINTENANCE REPLACED THE BATTERY PACK REF B717 AMM 35-31-03. OPERATIONAL CHECK WAS GOOD. (LP #7374989)
- [SDR DALA2020083182882](https://openairdocs.org/sdr/DALA2020083182882.md): Thermoswitch · failed · Aug 27, 2020 · N982AT · Boeing 717200 · Windshield/Door Rain/Ice Removal
  > ON TAXI-IN, WHEN ATTEMPTING TO OPEN A FOGGED-UP WINDOW WITH WINDSHIELD ANTI-FOG SELECTED ON, THE WINDOW JAMMED ON THE CAPT HEADSET CAUSING A SHORT. THE RESULT WAS A LOUD BUZZ AND A FIREBALL THAT QUICKLY EXTINGUISHED. THE CB Z-26 ALSO TRIPPED. MAINTENANCE PULLE
- [SDR DALA2019100705770](https://openairdocs.org/sdr/DALA2019100705770.md): Relay · malfunctioned · Oct 4, 2019 · N982AT · Boeing 717200 · Emergency Lighting
  > THE CABIN EMERGENCY LIGHTS FLICKER WHILE IN ARMED POSITION VERY OCCASSIONALY. MAINTENANCE REPLACED THE RELAY R2-5133 PER B717 WDM 24-51-01. OPERATIONAL CHECK WAS GOOD. NOTED NO DEFECTS.
- [SDR DALA2018082705269](https://openairdocs.org/sdr/DALA2018082705269.md): Battery Pack · no test · Aug 27, 2018 · N982AT · Boeing 717200 · Emergency Lighting
  > MAINTENANCE FOUND THAT THE FWD EMERGENCY LIGHTS FAILED DURING A SERVICE CHECK TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51. OPS CHECKED NORMAL. AIRCRAFT OK FOR SERVICE.
- [SDR DALA2018082005144](https://openairdocs.org/sdr/DALA2018082005144.md): Lens · missing · Aug 18, 2018 · N982AT · Boeing 717200 · Emergency Lighting
  > THE R1 DOOR EXIT SIGN LENS WAS MISSING. MAINTENANCE INSTALLED A NEW EXIT SIGN LENS IAW AMM 33-51.
- [SDR DALA2018061103926](https://openairdocs.org/sdr/DALA2018061103926.md): Wire · disconnected · Jun 9, 2018 · N982AT · Boeing 717200 · Light System Wiring
  > ONE EMERGENCY LIGHT WAS OUT IN THE TAIL COMPARTMENT. MAINTENANCE FOUND A DISCONNECTED WIRE AND CONNECTED IT. OPS CHECKED GOOD.

Next page: https://openairdocs.org/aircraft/N982AT/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 = 'N982AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N982AT/reports

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