# Service difficulty reports: N959AT

A list on [N959AT](https://openairdocs.org/aircraft/N959AT.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 · 213 reports

- [SDR DALA2026080604548](https://openairdocs.org/sdr/DALA2026080604548.md): Lanyard · broken · Aug 5, 2026 · N959AT · Boeing 717200 · Emergency Equipment
  > L1 DOOR SLIDE BUSTLE TO GIRT BAR LANYARD BROKEN, REPLACED L1 DOOR SLIDE LANYARD IAW AMM 25-61. (8497882) (AIRCRAFT GROUNDED).
- [SDR DALA2026062103689](https://openairdocs.org/sdr/DALA2026062103689.md): Light · detached · Jun 20, 2026 · N959AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY FLOOR LIGHT STRIP EXTENDING FROM ROW 14-17 ON THE RIGHT SIDE CAME OFF. SECURED EMERGENCY FLOOR LIGHT STRIP. OK FOR SVC. (LP 8878887 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051102945](https://openairdocs.org/sdr/DALA2026051102945.md): None · none · May 6, 2026 · N959AT · Boeing 717200 · Standard Practices/Structures
  > INSTALL ESA ANTENNA, REPAIRED REF B717 ERA 681787-14. (8673211) (AIRCRAFT GROUNDED)
- [SDR DALA2026031901912](https://openairdocs.org/sdr/DALA2026031901912.md): Carbon Seal · leaking · Mar 16, 2026 · N959AT · Boeing 717200 · APU Oil System
  > AIRCRAFT 9518, STRONG DIRTY SOCK ODOR COMING FROM PACK 2. FOUND APU TO BE LEAKING THROUGH CARBON SEAL PER B717 AMM 49-00. REPLACED APU. (LP 8237910)
- [SDR DALA2025091606818](https://openairdocs.org/sdr/DALA2025091606818.md): Hinge Fitting · corroded · Sep 11, 2025 · N959AT · Boeing 717200 · Elevator Structure
  > RT ELEVATOR GEARED TAB INBD CRANK FITTING-HINGE HAS SIGNS OF CORROSION ON HARDWARE AND PUSH ROD END HAS SIDE TO SIDE PLAY. REPLACED HARDWARE REF B717 AMM 27-31-05 (1193806)
- [SDR DALA2025060704357](https://openairdocs.org/sdr/DALA2025060704357.md): Light · detached · Jun 2, 2025 · N959AT · Boeing 717200 · Emergency Lighting
  > AIRCRAFT 9518, EMERGENCY EXIT LIGHT HANGING DOWN ROW 19. CORRECTIVE ACTION: SECURED LIGHT ASSY REF B717 AMM 33-51. (LP 7263518)
- [SDR DALA2025060604337](https://openairdocs.org/sdr/DALA2025060604337.md): Repair · not reported · May 29, 2025 · N959AT · Boeing 717200 · Wing Spar
  > SHIP 9518 EXISTING REPAIR FOUND. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. CORRECTIVE ACTION: REPAIRED PER ER/A 14-621443 (0994030)
- [SDR DALA2025060604336](https://openairdocs.org/sdr/DALA2025060604336.md): Repair · not reported · May 29, 2025 · N959AT · Boeing 717200 · Wing Spar
  > SHIP 9518 EXISTING REPAIRS FOUND. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. CORRECTIVE ACTION: REPAIRED PER ERA 621388-14AD (0994041)
- [SDR DALA2025052203934](https://openairdocs.org/sdr/DALA2025052203934.md): None · none · May 16, 2025 · N959AT · Boeing 717200 · Standard Practices/Structures
  > SHIP 9518 ACCOMPLISH ERA 624994-14 KA1717 STRUCTURAL SHIMMING FOR HUGHES WIFI INSTALLATION, CORRECTIVE ACTION: COMPLIED WITH ERA 624994-14 REV. (0969673)
- [SDR DALA2025051403727](https://openairdocs.org/sdr/DALA2025051403727.md): Spar Cap · cracked · May 9, 2025 · N959AT · Boeing 717200 · Wing Spar
  > DUE TO CRACK IN RH WING REAR AFT SPAR LOWER CAP, COMPLY WITH PRI 621388-14. CRACKED SPAR CAP REPLACED ON PRI 621388-14 REVS 0 THRU 22. COMPARED PRI 621388-14 REVS 0 THRU 22 AND ERA 621388-14 REV ORIG. ALL ITEMS MATCH. COMPLIED WITH ERA 621388-14 REV ORIG. ALL
- [SDR DALA2025051203682](https://openairdocs.org/sdr/DALA2025051203682.md): Battery · no test · May 9, 2025 · N959AT · Boeing 717200 · Emergency Lighting
  > DURING TESTING FOUND 1EA LIGHT IN CEILING AT AFT EXIT / FA SEAT AREA TO BE INOPERATIVE. REPLACED BATTERY AT B5-116. NOW LIGHT TEST GOOD REF B717 AMM 33-51-00. (LP #0957765)
- [SDR DALA2025051403726](https://openairdocs.org/sdr/DALA2025051403726.md): Spar Cap · cracked · May 8, 2025 · N959AT · Boeing 717200 · Wing Spar
  > DUE TO CRACK IN LH WING LOWER SPAR CAP, COMPLY WITH PRI 621443-14. CRACKED SPAR CAP REPLACED ON PRI 621443-14 REVS 0 THRU 24. COMPARED PRI 621443-14 REVS 0 THRU 24 WITH ERA 621443-14 REV A. ALL ITEMS MATCH. COMPLIED WITH ERA 621443-14 REV A. ALL RII ITEMS C/W.
- [SDR DALA2024040504130](https://openairdocs.org/sdr/DALA2024040504130.md): Nut · out of limits · Apr 3, 2024 · N959AT · Boeing 717200 · Flight Control System
  > AD -- DURING FUNCTIONAL TEST OF THE TRIM ACME SCREW AND NUT FOUND DIMENSION BG IS OUT OF LIMIT. UNSAFTIED TURNBUCKLE CONNECTING CABLES 130B TO 130A AND CABLE TURNBUCKLE TO 129B AND 129A. BROKE SAFTEY WIRE ON STOP BOLT (AB) PER B717 AMM 27-40-00 FIGURES 504 AND
- [SDR DALA2024040504131](https://openairdocs.org/sdr/DALA2024040504131.md): Support · cracked · Apr 1, 2024 · N959AT · Boeing 717200 · Stabilizer Control System
  > AD -- DURING JACK SCREW LUBE, CYCLED HORIZ STAB FULL NOSE UP, SUPPORT ASSY CONTACTED STOP AND CRACKED. REMOVED HORIZONTAL STABILIZER ACTUATOR ASSEMBLY AND REPLACED JACKSCREW FOR HORIZONTAL STAB PER B717 AMDS WORKCARD 2740-0114-05. ALL RII TASK COMPLETE. (LP #5
- [SDR DALA2024020801685](https://openairdocs.org/sdr/DALA2024020801685.md): Cover · misaligned · Feb 7, 2024 · N959AT · Boeing 717200 · Emergency Lighting
  > DURING SERVICE CHECK, THE CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE WITH C/B A11 PULLED. MAINTENANCE FOUND F/A PANEL SWITCH COVER MISALIGNED, CAUSING SWITCH TO NOT GO TO OFF POSITION FULLY. ADJUSTED SWITCH COVER AND OPERATIONAL CHECK WAS GOOD PER B717 AMM 33
- [SDR DALA2024020601581](https://openairdocs.org/sdr/DALA2024020601581.md): Holder · shorted · Feb 4, 2024 · N959AT · Boeing 717200 · Light System Wiring
  > SHIP 9518 -SMKE- THE FLIGHT CREW REPORTED VISIBLE SMOKE FROM THE CAPTAIN SIDE CLIPBOARD LIGHT. THE SMOKE STOPPED AFTER ABOUT 10 SECONDS. THE QRH WAS COMPLIED WITH AND THE CREW CONTACTED MAINTENANCE TO PULL THE CIRCUIT BREAKERS. THE FLIGHT CONTINUED TO THE SCHE
- [SDR DALA2024012601172](https://openairdocs.org/sdr/DALA2024012601172.md): Light · sparks · Jan 24, 2024 · N959AT · Boeing 717200 · Flight Compartment Lighting
  > AFTER TAKEOFF ON RWY 6 IN BHM, AT APPROX 600 FT, CAPTAIN SIDE MAP LIGHT SPARKED AND BEGAN TO SMOKE. THE CIRCUIT BREAKER W29 TRIPPED AND FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE PUSHED C/B IN AND BOTH LIGHT WORKED ON CAPTAIN AND FIRST OFFICER SIDE
- [SDR DALA2023100408162](https://openairdocs.org/sdr/DALA2023100408162.md): Unknown · unknown · Sep 29, 2023 · N959AT · Boeing 717200 · Hydraulic Pump (Electric/Engine), Main
  > SHIP 9518 -DE- THE CREW DECLARED AN EMERGENCY DUE TO INTERMITTENT RIGHT HYDRAULIC PUMP FAIL MESSAGE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE SWITCH. (LP #4594298)
- [SDR DALA2023081606668](https://openairdocs.org/sdr/DALA2023081606668.md): Unknown · unknown · Aug 12, 2023 · N959AT · Boeing 717200 · Passenger Compartment Equipment
  > AD RELATED, MISSING TO PERFORM STEP 14 A (2) AND 22 A (2) OF 2521-01701-01B-TRIPLE TOURIST CLASS SEATS, B717 - MODIFY; SECTION 01. SUMMARY OF NRC 00520: STEP 14 A (2) AND 22 A (2) OF 2521-01701- 01B-TRIPLE TOURIST CLASS SEATS, B717 - MODIFY; SECTION 01 WERE PE
- [SDR DALA2023081606667](https://openairdocs.org/sdr/DALA2023081606667.md): Unknown · unknown · Aug 12, 2023 · N959AT · Boeing 717200 · Passenger Compartment Equipment
  > AD RELATED, MISSING TO PERFORM TORQUE OF TRIPLE TOURIST CLASS SEATS. SUMMARY OF NRC 00518: STEP 8J OF 2521-01701-01B-TRIPLE TOURIST CLASS SEATS, B717 - MODIFY; SECTION 01 WAS PERFORMED PER TRIPLE TOURIST CLASS SEATS, B717 - MODIFY; SECTION 01 STEP 8.J.(1) AND
- [SDR DALA2023081606666](https://openairdocs.org/sdr/DALA2023081606666.md): Unknown · unknown · Aug 12, 2023 · N959AT · Boeing 717200 · Passenger Compartment Equipment
  > AD RELATED, MISSING TO PERFORM STEP 14 A (2), 21 A (2) AND 34 A (2) OF 2521-01701-01A-SINGLE AND DOUBLE TOURIST CLASS SEATS, B717 - MODIFY; SECTION 01. SUMMARY OF NRC 00521: STEP 14 A (2), 21 A (2), AND 34 A (2) OF 2521-01701-01A-SINGLE AND DOUBLE TOURIST CLAS
- [SDR DALA2023080706365](https://openairdocs.org/sdr/DALA2023080706365.md): Unknown · unknown · Aug 4, 2023 · N959AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > NICKS ON DOUBLER REPAIR BTW STA Y=996 TO Y=1002. SUMMARY OF NRC 099: 2ND. DOUBLER WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 10 FIGURE 202. PERFORM VISUAL INSPECTION EACH 8000 CYCLES PER B 717-200 SRM 53-20-15-2R PROCEDURE 10 PAR 7 TABLE 202. (LP #290
- [SDR DALA2023080706364](https://openairdocs.org/sdr/DALA2023080706364.md): Unknown · unknown · Aug 4, 2023 · N959AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON WEB INSIDE STRUCTURE AFT EMERGENCY DOOR AT CABIN PAX. SUMMARY OF NRC 0170: WEB INSIDE STRUCTURE AFT EMERGENCY DOOR AT CABIN PAX WAS REPAIRED PER B-717-200 SRM 55-00-00-2R REPAIR 1 FIG 201. (LP #2901626)
- [SDR DALA2023080306278](https://openairdocs.org/sdr/DALA2023080306278.md): Unknown · unknown · Aug 2, 2023 · N959AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON WEB ON X=-44 STA Y=160 AND X=54 BTW STA Y=160 AND STA Y=180 AT FWD PAX CABIN FLOOR. SUMMARY OF NRC 00179: CORROSION LEVEL 2. WEB ON X=-44 STA Y=160 AND X=54 BTW STA Y=160 AND STA Y=180 AT FWD PAX CABIN FLOOR WERE REPAIRED PER B717-200 SRM 51-70-10
- [SDR DALA2023080106211](https://openairdocs.org/sdr/DALA2023080106211.md): Unknown · unknown · Jul 31, 2023 · N959AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON GENERATION FLOOR ACCESS PANELS 221SF, 222EF, 221NF, 222AWF, AND 222SF. SUMMARY OF NRC 00283: CORROSION LEVEL 2. FLOOR ACCESS PANELS 222EF AND 222SF WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2, FLOOR PANELS 221SF AND 221NF WERE F
- [SDR DALA2023080106210](https://openairdocs.org/sdr/DALA2023080106210.md): Unknown · unknown · Jul 31, 2023 · N959AT · Boeing 717200 · Trailing Edge Flaps
  > DISBOND ON RH CENTER FIXED VANE, UPPER SURFACE OF 0.700IN LENGTH X 0.600IN WIDTH AT DENT #1, (53.25" FROM IB EDGE, 5" FROM TE) IN REF MON JOB 032-0001 LOG 1549344. SUMMARY OF NRC 00407: RH CENTER FIXED VANE, UPPER SURFACE WAS REPAIRED PER B717-200 SRM 57-53-01
- [SDR DALA2023080106201](https://openairdocs.org/sdr/DALA2023080106201.md): Unknown · unknown · Jul 29, 2023 · N959AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR PANEL 211AMF AT COCKPIT. SUMMARY OF NRC 00299: CORROSION LEVEL 2. PANEL (SKIN) OF FLOOR PANEL 211AMF AT COCKPIT WAS FABRICATED AND REPLACED PER DWG 9957826 REV AA, B717-200 SRM 51-20-05-0G AND 51-41-02-0G. (LP #2891380)
- [SDR DALA2023080106200](https://openairdocs.org/sdr/DALA2023080106200.md): Unknown · unknown · Jul 28, 2023 · N959AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME BTW STA Y=1037 AND LONG 17LH AT AFT PAX CABIN. SUMMARY OF NRC 00289: FRAME BTW STA Y=1037 AND LONG 17LH AT AFT PAX CABIN WAS REPAIRED PER B717 SRM-53-20-07-2R-4 (PERMANENT REPAIR). (LP #2890030)
- [SDR DALA2023072806113](https://openairdocs.org/sdr/DALA2023072806113.md): Unknown · unknown · Jul 28, 2023 · N959AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH CTR SEAT TRACK FROM STA Y=216 TO STA Y=245 AT FWD PAX CABIN FLOOR. SUMMARY OF NRC 0174: CORROSION LEVEL 2. SECTION SEAT TRACK FROM STA Y=200 TO STA Y=245 AT FWD PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-01-0G PAR 6 AND 51-41-05-0G PAR 8. (L
- [SDR DALA2023072806110](https://openairdocs.org/sdr/DALA2023072806110.md): Unknown · unknown · Jul 27, 2023 · N959AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FITTINGS (2 EA) OF FWD SERVICE DOOR JAMB AT FWD PAX CABIN FLOOR. SUMMARY OF NRC 0180: CORROSION LEVEL 2. FITTINGS (2 EA) WERE REPLACED PER B717-200 SRM 51-41-02-0G. (LP #2887630)
- [SDR DALA2023072606037](https://openairdocs.org/sdr/DALA2023072606037.md): Unknown · unknown · Jul 24, 2023 · N959AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LH CUSP MEMBRANE (WEB) STA 832 TO STA 870. SUMMARY OF NRC 0438: CORROSION LEVEL 2. CUSP MEMBRANE WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE 209 AND 210. (LP #2883139)
- [SDR DALA2023072505981](https://openairdocs.org/sdr/DALA2023072505981.md): Unknown · unknown · Jul 23, 2023 · N959AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKED FRAME CLIP STA Y=715 LH SIDE AT UNDERWING CANTED KEEL INTERNAL STRUCTURE. SUMMARY OF NRC 0197: FRAME CLIP STA Y=715 LH SIDE AT UNDERWING CANTED KEEL INTERNAL STRUCTURE WAS REPAIRED PER B-717-200 SRM 51-70-11-2R PROCEDURE 1 PAR 4 C FIG 201 DETAIL A-A. (
- [SDR DALA2023072105923](https://openairdocs.org/sdr/DALA2023072105923.md): Unknown · unknown · Jul 20, 2023 · N959AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKS ON RH WINDOW PANS ON STA Y=238 FWD UP CORNER, STA Y=294 FWD UP CORNER, STA Y=370 FWD UPPER CORNER, STA Y=636 FWD LOWER CORNER, STA Y=851 AFT LOWER CORNER, AND STA Y=870 AFT LOWER CORNER AT PAX CABIN. SUMMARY OF NRC 292: ON RH WINDOW PANS ON STA Y=238 FW
- [SDR DALA2023071705781](https://openairdocs.org/sdr/DALA2023071705781.md): Unknown · unknown · Jul 16, 2023 · N959AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON PLATE IN STA Y=1053 BTW LONGERONS 29R-29L AT AFT BULKHEAD AT AFT CARGO COMPARMENT. SUMMARY OF NRC 203: LEVEL CORROSION 2. DOUBLER (PLATE) WAS REPLACED PER B-717-200 SRM 51-41-05-0G AND PER DGW 5910130-61 REV "ET". (LP #2869463)
- [SDR DALA2023071705780](https://openairdocs.org/sdr/DALA2023071705780.md): Unknown · unknown · Jul 16, 2023 · N959AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP MEMBRANE LOWER SURFACE ON STA Y=645 AND X=-44 AT CPAX. SUMMARY OF NRC 421: CUSP MEMBRANE LOWER SURFACE ON STA Y=645 AND X=-44 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE 203 AND (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS
- [SDR DALA2020022601416](https://openairdocs.org/sdr/DALA2020022601416.md): Battery Pack · inoperative · Feb 25, 2020 · N959AT · Boeing 717200 · Emergency Lighting
  > REAR AIRCRAFT, ABOVE JUMPSEAT, THE EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND POWER SUPPLY PER AMM 33-51-03. OPERATIONAL CHECK IS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #6396492)
- [SDR DALA2020011400239](https://openairdocs.org/sdr/DALA2020011400239.md): Power Supply · inoperative · Jan 13, 2020 · N959AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY OVER WING EXIT SIGN IS INOPERATIVE AT B20DC. MAINTENANCE REPLACED THE POWER SUPPLY, EMERGENCY BATTERY AT 20DC, RIGHT HAND AFT EMERGENCY EXIT PER AMM 33-51-06. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE.
- [SDR DALA2019120507056](https://openairdocs.org/sdr/DALA2019120507056.md): Battery Pack · inoperative · Dec 5, 2019 · N959AT · Boeing 717200 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS IN REAR TAIL CONE ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK, B5-116, IN THE AFT RIGHT LAVATORY. THE OVERHEAD EMERGENCY LIGHTS IN THE REAR TAIL CONE RETURNED TO NORMAL OPERATION. (LP #6607840)
- [SDR DALA2019120206971](https://openairdocs.org/sdr/DALA2019120206971.md): Power Supply · malfunctioned · Nov 27, 2019 · N959AT · Boeing 717200 · Emergency Lighting
  > THE AFT CATWALK AND AFT EMERGENCY EXIT DOORWAY LIGHTS ARE FLICKERING ON AND OFF. MAINTENANCE REPLACED THE AFT CATWALK EMERGENCY POWER SUPPLY IAW B717 AMM 33-51-03. OPERATIONAL TEST WAS GOOD. (LP #6607820)
- [SDR DALA2019092305439](https://openairdocs.org/sdr/DALA2019092305439.md): Battery · discharged · Sep 21, 2019 · N959AT · Boeing 717200 · Emergency Lighting
  > UPON ARRIVAL AT THE GATE IN ATL, THE AFT EMERGENCY EXIT LIGHT WAS FLASHING. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY. OPERATIONAL CHECK WAS GOOD PER AMM 33-51. (LP #5966954)
- [SDR DALA2019091805389](https://openairdocs.org/sdr/DALA2019091805389.md): Lug · corroded · Sep 18, 2019 · N959AT · Boeing 717200 · Fuselage, Landing Gear Attach Fittings
  > CORROSION FOUND ON RT FWD AND AFT FACES OF THE RHS FIXED BRACE ATTACH LUG. REPAIRED PER ER/A 581446-14 REV ORIGINAL. ASSOCIATED ER/A 14-581446 ADDED FOR AC 9518. (LP #1276499)
- [SDR DALA2019091805387](https://openairdocs.org/sdr/DALA2019091805387.md): Lug · corroded · Sep 18, 2019 · N959AT · Boeing 717200 · Fuselage, Landing Gear Attach Fittings
  > CORROSION FOUND ON LT FWD AND AFT FACES OF THE LHS FIXED BRACE ATTACH LUG. REPAIRED PER ER/A 581445-14 REV ORIGINAL. ASSOCIATED ER/A 14-581445 ADDED FOR AC 9518. (LP #1276502)
- [SDR DALA2019060603431](https://openairdocs.org/sdr/DALA2019060603431.md): Power Supply · malfunctioned · Jun 5, 2019 · N959AT · Boeing 717200 · Emergency Lighting
  > EXIT LIGHT OVER TAILCONE EXIT AND AIRCRAFT RIGHT STANDBY EMERGENCY LIGHT FLICKER INTERMITTENTLY DURING ALL PHASES OF FLIGHT. MAINTENANCE RE-SET AFT POWER PACK AND THE FLICKER CEASED. OPERATIONAL CHECK WAS GOOD REF B717 AMM 33-51. (LP #6285367)
- [SDR DALA20190221082](https://openairdocs.org/sdr/DALA20190221082.md): Power Supply · inoperative · Feb 20, 2019 · N959AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN IS INOPERATIVE AT LOCATIONS:102. MAINTENANCE FOUND THE AFT LIGHT AND ESCAPE SECTION EMERGENCY LIGHT POWER PACK TO BE INOPERATIVE. THE POWER SUPPLY WAS REPLACED IAW B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS RETURNED
- [SDR DALA2019020410715](https://openairdocs.org/sdr/DALA2019020410715.md): Cover · damaged · Jan 31, 2019 · N959AT · Boeing 717200 · Escape Slide
  > THE TAIL-CONE SLIDE COVER HAS A BROKEN CLIP FOR THE RELEASE CABLE. MAINTENANCE INSTALLED A NEW CLIP. (LP #0926413)
- [SDR DALA2018100305847](https://openairdocs.org/sdr/DALA2018100305847.md): Power Supply · defective · Oct 3, 2018 · N959AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN ABOVE THE DOOR TO THE AFT ACCESSORY COMPARTMENT IS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY BASE AND THE LIGHT RETURNED TO NORMAL OPERATION. (LP #5111438)
- [SDR DALA2016081906087](https://openairdocs.org/sdr/DALA2016081906087.md): Skin · damaged · Aug 18, 2016 · N959AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STAB RIGHT SIDE BELOW AND FORWARD OF LOWER RIGHT VOR ANTENNA SEVERAL SCREWS PULLED THROUGH SKIN. REPAIR WAS ACCOMPLISHED IAW ER/A 549263-14AD REV. ORIGINAL.
- [SDR DALA2016081806070](https://openairdocs.org/sdr/DALA2016081806070.md): Skin · gouged · Aug 17, 2016 · N959AT · Boeing 717200 · Wing, Plate/Skin
  > GOUGES ON RIGHT WING FIXED LE BETWEEN XIS 83.5, XIS 90 AND XIS 120. GOUGES WERE BLENDED IAW SRM 57-00-00 FIG 103. BHEC INSPECTION WAS ACCOMPLISHED ON DRILLED HOLES, HOLE 2, CRACKS WERE FOUND IAW ETI-17-16-109. REPAIRED IAW ETI-17-16-109 REV 2 AND ER/A 5492
- [SDR DALA2016081706042](https://openairdocs.org/sdr/DALA2016081706042.md): Access Panel · corroded · Aug 17, 2016 · N959AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON COUTERSINKS AT FUEL TANK ACCESS NR 520JB, SM. CORROSION OF COUNTERSINK WAS REMOVED IAW SRM 51-10-04. REWORKED AREAS WERE MEASURED AND MAX DIAMETER ALLOWABLE IS 0.532" AND 5 ADJACENT HOLES OUT OF LIMITS WERE FOUND. MAX DIAMETER MEASURED IS 0.557
- [SDR DALA2016081706041](https://openairdocs.org/sdr/DALA2016081706041.md): Access Panel · corroded · Aug 17, 2016 · N959AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON COURTERSINKS AT FUEL TANK ACCESS NR 520EB, SM. CORROSION OF COUNTERSINKS WAS REMOVED IAW SRM 51-10-04. REWORKED AREAS WERE MEASURED AND MAX DIAMETER ALLOWABLE IS 0.532" AND 3 ADJACENT HOLES OUT OF LIMITS WERE FOUND, MAX DIAMETER MEASURED IS 0.56

Next page: https://openairdocs.org/aircraft/N959AT/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 = 'N959AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N959AT/reports

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