# Service difficulty reports: N896AT

A list on [N896AT](https://openairdocs.org/aircraft/N896AT.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 2 · 93 reports

- [SDR DALA2026081404656](https://openairdocs.org/sdr/DALA2026081404656.md): Skin · ground damage · Aug 13, 2026 · N896AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > RAMP STRUCK BOTTOM OF AIRCRAFT WITH HOSE REEL, CREATING DENT, COMPLIED WITH ER/A 636316-16. (9606506) (AIRCRAFT GROUNDED).
- [SDR DALA2026072704341](https://openairdocs.org/sdr/DALA2026072704341.md): Light · inoperative · Jul 25, 2026 · N896AT · Boeing 717200 · Emergency Lighting
  > LT & RT EXT EMERGENCY LIGHT INOP. R & R R2-273 PER B717 33-51-11. BOTH EMERGENCY LIGHTS OPS CK NORMAL AT THIS TIME OK FOR SVC. (9124825) AIRCRAFT GROUNDED.
- [SDR DALA2026040102117](https://openairdocs.org/sdr/DALA2026040102117.md): Compressor · stalled · Mar 30, 2026 · N896AT · Boeing 717200 · Turbine Engine Compressor Section
  > CREW REJECTED TAKEOFF AT 70 KNOTS DUE TO RIGHT ENGINE COMPRESSOR STALL. PERFORMED BORESCOPE INSPECTION OF RIGHT ENGINE AND FOUND MULTIPLE HPC BLADES DAMAGED. REPLACED RIGHT ENGINE AND RETURNED TO SERVICE.(8306458)
- [SDR DALA2025020300804](https://openairdocs.org/sdr/DALA2025020300804.md): Computer · faulted · Jan 31, 2025 · N896AT · Boeing 717200 · Rudder Control System
  > SHIP 9556 -MISC/DE- THE FLIGHT CREW NOTICED THAT THE AIRCRAFT WAS FLYING UNCOORDINATED DURING THE DESCENT AND THEN THEY RECEIVED "RUDDER RESTRICTED" MESSAGE ON APPROACH. AN EMERGENCY WAS THEN DECLARED WITH ATC. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MA
- [SDR DALA2025012000464](https://openairdocs.org/sdr/DALA2025012000464.md): Skin · corroded · Jan 17, 2025 · N896AT · Boeing 717200 · Wing, Plate/Skin
  > -AD- CORROSION ON UPPER SKIN BTW XRS 360 TO XRS 380 AT LH WING. SUMMARY OF NRC 0015: CORROSION LEVEL 2. CORROSION ON UPPER SKIN BTW XRS 360 TO XRS 380 AT LH WING WAS REAPAIRED PER PRI 623423-14 REV 2 AND ERA 623423-14AD REV ORIGINAL. ASSOCIATED ER/A 14-623423
- [SDR DALA2025011400312](https://openairdocs.org/sdr/DALA2025011400312.md): Skin · nicked · Jan 13, 2025 · N896AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > NICK BETWEEN STA 994 AND STGR 24-26 RH AT EXTERNAL FUSELAGE SKIN. SUMMARY OF NRC 00007: EXTERNAL SKIN BETWEEN STA 994 AND STGR 24-26 RH WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 12, REPAIR 12. PERFORM INITIAL GENERAL VISUAL INSPECTION AT 8,000 CYCLES
- [SDR DALA2023102408719](https://openairdocs.org/sdr/DALA2023102408719.md): Unknown · unknown · Oct 23, 2023 · N896AT · Boeing 717200 · Emergency Lighting
  > ROW 21 BOTH L/H AND R/H OVERWING EXIT SIGNS (LOWER) ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IAW B717 AMM 33-51 AT LOCATION B5-1119. OPERATIONAL CHECK WAS GOOD. (LP #4615512)
- [SDR DALA2023052204054](https://openairdocs.org/sdr/DALA2023052204054.md): Unknown · unknown · May 20, 2023 · N896AT · Boeing 717200 · Emergency Lighting
  > THE FLIGHT ATTENDANT NOTED THAT THE EMERGENCY EXIT COVER DIFFUSER LENS WAS DAMAGED AT LOCATION 603. MAINTENANCE RESECURED THE EMERGENCY EXIT COVER LIGHT LENS OVER AISLE AT ROW 20 AS REQUIRED. NO DEFECTS NOTED. (LP #2776663)
- [SDR DALA2023021401120](https://openairdocs.org/sdr/DALA2023021401120.md): Unknown · unknown · Feb 8, 2023 · N896AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON RH TIE TRACK UPPER SURFACES FROM STA Y=900 TO Y=954. SUMMARY OF NRC 0556: CORROSION LEVEL 2. TIE TRACK RH ON STA Y=900 TO Y=954 WAS REPLACED PER B717-200 SRM 51-41-08-0G, 51-41-02 -0G, AND 51-41-01-0G. (LP #2620761)
- [SDR DALA2023021401117](https://openairdocs.org/sdr/DALA2023021401117.md): Unknown · unknown · Feb 8, 2023 · N896AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > SECONDARY IN REFERENCE NRC 496: CORROSION ON LH TIE TRACK UPPER SURFACES FRON STA Y=900 TO Y=1028. SUMMARY OF NRC 00555: CORROSION LEVEL 2. TIE TRACK SECTION FROM Y=900 TO Y=1028 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-01-0G. (LP #2620158)
- [SDR DALA2023013100773](https://openairdocs.org/sdr/DALA2023013100773.md): Tab · debonded · Jan 28, 2023 · N896AT · Boeing 717200 · Aileron Tabs
  > IN REF TO NRC 00041, DISBONDED AREA WAS FOUND ON DENT #1 WITH A MEASURE OF 0.500 IN LENGTH X 0.500 IN WIDTH AT AILERON CONTROL TAB OUTBOARD UPPER FACE AT LH WING. SUMMARY OF NRC 00195: AILERON CONTROL TAB OUTBOARD UPPER FACE AT LH WING WAS REPAIRED AND WEIGHT
- [SDR DALA2023012400524](https://openairdocs.org/sdr/DALA2023012400524.md): Access Panel · corroded · Jan 20, 2023 · N896AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK HOLE OF LH WING ACCESS PLATE NBR 520CB REF NRC 417. SUMMARY NRC 00506: CORROSION LEVEL 2. FUEL ACCESS PLATE NBR 520CB AT LH WING WAS REPAIRED PER B717-200 SRM 57-10- 01-2R PROCEDURE 2 PAR. 5 CONDITION II. (LP #2591579)
- [SDR DALA2023012000436](https://openairdocs.org/sdr/DALA2023012000436.md): Beam · cracked · Jan 19, 2023 · N896AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON BEAM NBR 7 AFT SECTION AT MAIN ENTRANCE DOOR. SUMMARY OF NRC 00106: CRACKED BEAM NBR 7 AFT SECTION AT MAIN ENTRANCE DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R-13. (LP #2590277)
- [SDR DALA2023011900387](https://openairdocs.org/sdr/DALA2023011900387.md): Beam · cracked · Jan 18, 2023 · N896AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON BEAM NR 1 AFT SECTION AT MAIN ENTRANCE DOOR. BEAM NR 1 AFT SECTION AT MAIN ENTRANCE DOOR WAS REPAIRED IAW SRM 52-10-02-2R-7.
- [SDR DALA2023011900386](https://openairdocs.org/sdr/DALA2023011900386.md): Pan · cracked · Jan 18, 2023 · N896AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON UPPER PAN AT STA 197.750 & BEAM #1 OF FWD PASSENGER ENTRANCEN DOOR. UPPER PAN AT STA 197.750 & BEAM #1 OF FWD PASSENGER ENTRANCEN DOOR WAS REPAIRED IAW SRM 52-10-02- 2R PROCEDURE 3 REPAIR 3.
- [SDR DALA2023011800365](https://openairdocs.org/sdr/DALA2023011800365.md): Cusp Web · cracked · Jan 17, 2023 · N896AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > DURING REMOVAL OF RH CUSP WEB, DVI WAS PERFORMED AND 3 CRACKS WERE FOUND (EAS). A CRACK AT HOLE OF FASTENER AT CUSP WEB STA 656, A CRACK ON EDGE OF CUSP WEB STA 657, AND CRACK AT HOLE OF FASTENER AT CUSP WEB STA 694 PAX CABIN FLOOR. CUSP WEB BS 656 TO 657 WAS
- [SDR DALA2023011600311](https://openairdocs.org/sdr/DALA2023011600311.md): Cusp Web · cracked · Jan 14, 2023 · N896AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB ON STA 229 AT BL 46R AT PAX CABIN. SUMMARY OF NRC 00258: CUSP WEB ON STA 229 AT BL 46R WAS REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 2. (LP #2582373)
- [SDR DALA2023011600308](https://openairdocs.org/sdr/DALA2023011600308.md): Diaphragm · corroded · Jan 12, 2023 · N896AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON DIAPHRAGM STA=192 AND STA=187 RBL=44 ARE OUT OF LIMITS IN REF NRC 00325. SUMMARY OF NRC 00451: LEVEL CORROSION 2. DIAPHRAGM STA=192 AND STA =187 RBL=44 WAS REPAIRED PER B717-200 SRM 53-00-00-1A PAR 4.B.(2). FIG. 102.
- [SDR DALA2022092806344](https://openairdocs.org/sdr/DALA2022092806344.md): None · none · Sep 28, 2022 · N896AT · Boeing 717200 · Emergency Lighting
  > DURING A SERVICE CHECK, THE AFT GROUP OF EMERGENCY LIGHTS WAS DISCOVERED TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY B5-260 REF B717 AMM 33-51. THEY ALSO REPLACED THE MIDDLE EMERGENCY LIGHT ON THE TAILCONE CATWALK REF B717 AMM 33-51. (
- [SDR DALA2022092806342](https://openairdocs.org/sdr/DALA2022092806342.md): None · none · Sep 25, 2022 · N896AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS BATTERY WAS DISCOVERED TO BE DISCHARGED. MAINTENANCE REPLACED THE POWER SUPPLY AT THE EMERGENCY LIGHT BATTERY PER B717 AMM 33-51. AIRCRAFT READY FOR SERVICE. TESTS OK. (LP #8940315)
- [SDR DALA2022033102152](https://openairdocs.org/sdr/DALA2022033102152.md): None · none · Mar 30, 2022 · N896AT · Boeing 737 · Emergency Lighting
  > MAINTENANCE FOUND THAT THE AFT CABIN EXIT IDENTIFIER FAILED TO ILLUMINATE DURING THE SERVICE CHECK. TROUBLE SHOOTING PER WD 33-51-12 FOUND THE EMERGENCY LIGHT BATTERY PACK WAS INOPERATIVE. THE BATTERY PACK WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS
- [SDR DALA2022012500495](https://openairdocs.org/sdr/DALA2022012500495.md): None · none · Jan 22, 2022 · N896AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN STA Y=1133 AND ABOVE LONGERON 2R. SUMMARY OF NRC 00057: CRACK ON FUSELAGE SKIN STA Y=1133 AND ABOVE LONGERON 2R WAS REPAIRED PER ETI-17-22-001 REV. 3 AND ER/A 596558-14AD SECTION I. PERMANENT REPAIR REPAIR APPROVAL IS LIMITED TO 60,000 F
- [SDR DALA2022011700299](https://openairdocs.org/sdr/DALA2022011700299.md): None · none · Jan 17, 2022 · N896AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON PAN BTW STA Y=954 TO Y=994 AT AFT CARGO DOOR JAMB. SUMMARY OF NRC 00008: CORROSION LEVEL 2, PAN BTW STA Y=954 TO Y= 994 AT AFT CARGO DOOR JAMB WAS REPAIRED PER B717 SRM 53-20-15-2R REPAIR 7. (LP #2088850)
- [SDR DALA2022011700298](https://openairdocs.org/sdr/DALA2022011700298.md): None · none · Jan 15, 2022 · N896AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN STA Y=1022 BTW LONGERON 7L AND 8L. SUMMARY OF NRC 00056: CRACK ON FUSELAGE SKIN STA Y=1022 BTW LONGERON 7L AND 8L WAS REPAIRED PER B717-200 SRM 53-03-01-2R, REPAIR 1 STEP 6 PAR G, FIG 20. REQUIRES VISUAL REPETITIVE (8,000 CYCLES) INSPECT
- [SDR DALA2021060403067](https://openairdocs.org/sdr/DALA2021060403067.md): Battery Pack · inoperative · Jun 2, 2021 · N896AT · Boeing 717200 · Emergency Lighting
  > FOUND EMERGENCY LIGHT BATTERY INOPERATIVE IN FIRST CLASS. MAINTENANCE REPLACED THE FORWARD EMERGENCY LIGHTS BATTERIES (2) REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7462600)
- [SDR DALA2021042902460](https://openairdocs.org/sdr/DALA2021042902460.md): Sliding Window · failed · Apr 27, 2021 · N896AT · Boeing 717200 · Flight Compartment Windows
  > WHILE ATTEMPTING TO CLEAN THE WINDOWS, MAINTENANCE DETERMINED THAT THE COPILOTS SLIDING WINDOW WILL NOT UNLOCK AND OPEN. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE UPPER RETAINER SPRING WAS
- [SDR DALA2021012200455](https://openairdocs.org/sdr/DALA2021012200455.md): Cover · missing · Oct 3, 2020 · N896AT · Boeing 717200 · Nacelle/Pylon, Main Frame
  > THE INBOARD COWL HOIST COVER IS MISSING ON LEFT ENGINE. CONTRACT MAINTENANCE FORWARDED THE DISCREPANCY TO NEF 71- 10-02. COWL HOIST SCREW COULD NOT BE INSTALLED, PER AIPC 71-11-05-10 ITEM 95. OK TO CONTINUE. ATL 22JAN21 THE NR 1 ENGINE WAS CHANGED WITH A N
- [SDR DALA2020030201516](https://openairdocs.org/sdr/DALA2020030201516.md): Power Supply · inoperative · Mar 1, 2020 · N896AT · Boeing 717200 · Emergency Lighting
  > THE EXTERIOR EMERGENCY LIGHTS REMAIN ON WHEN THE AIRCRAFT IS SHUTDOWN. MAINTENANCE REPLACED THE POWER SUPPLY AND RELAY PER B717 AMM 33-51. THE OPERATIONAL CHGECK WAS GOOD. (LP #1511748)
- [SDR DALA2020021801207](https://openairdocs.org/sdr/DALA2020021801207.md): Windshield Wiper · broken · Feb 13, 2020 · N896AT · Boeing 717200 · Windshield/Door Rain/Ice Removal
  > THE CAPTAIN SIDE WIPER ARM BROKE OFF ON TOUCH DOWN (22L) AT JFK. MAINTENANCE REPLACED THE CAPTAIN SIDE WINDSHIELD WIPER IN REF B717 AMM 30-43. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT IS OK FOR SERVICE. (LP #6954789)
- [SDR DALA2019110506386](https://openairdocs.org/sdr/DALA2019110506386.md): Release Cable · worn · Nov 2, 2019 · N896AT · Boeing 717200 · Aerodynamic Fairings
  > KEVLAR RELEASE CABLE IS WORN IN THE TAILCONE. REMOVED WORN KEVLAR RELEASE CABLE, INSTALLED NEW KEVLAR RELEASE CABLE, WITH COMPLETION OF KEVLAR CABLE ON AMDS CARD #5352-2001. (LP #1343143)
- [SDR DALA2019110506385](https://openairdocs.org/sdr/DALA2019110506385.md): Bracket · worn · Nov 2, 2019 · N896AT · Boeing 717200 · Aerodynamic Fairings
  > THE TAILCONE KEVLAR CABLE SPRING BRACKET ON THE RIGHT SIDE IS WORN. MAINTENANCE REPLACED THE TAIL CONE KEVLAR CABLE SPRING BRACKET WITH A NEW BRACKET. (LP #1343012)
- [SDR DALA2019090905217](https://openairdocs.org/sdr/DALA2019090905217.md): Light · inoperative · Sep 6, 2019 · N896AT · Boeing 717200 · Emergency Lighting
  > WHILE PERFORMING SERVICE CHECK FOUND 2ND FROM FORWARD EMERGENCY ESCAPE PATH LIGHT ABOVE TAIL CATWALK INOPERATIVE. MAINTENANCE REPAIRED THE WIRE PER SWPM 20 AND THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #9875618)
- [SDR DALA2019073104498](https://openairdocs.org/sdr/DALA2019073104498.md): Door · missing · Jul 21, 2019 · N896AT · Boeing 717200 · Fluid Service Doors
  > POTABLE WATER DOOR MISSING. REF LP 5476442. (LP #5476460)
- [SDR 2019F00176](https://openairdocs.org/sdr/2019F00176.md): Spoiler · delaminated · Mar 29, 2019 · N896AT · Boeing 717200 · Spoilers
  > DELAMINATED LT INBOARD SPOILER.
- [SDR DALA2018031301682](https://openairdocs.org/sdr/DALA2018031301682.md): Slide · damaged · Mar 9, 2018 · N896AT · Boeing 717200 · Escape Slide
  > THE OUT OF PLACE INFLATION CABLE PIN WAS ALSO MISSING VALVE LOCK PIN ON L1 DOOR SLIDE. THE DOOR SLIDE WAS REMOVED AND REPLACED IAW AMM 25-61-01.
- [SDR DALA2018031001597](https://openairdocs.org/sdr/DALA2018031001597.md): Vane · debonded · Mar 9, 2018 · N896AT · Boeing 717200 · Trailing Edge Flaps
  > DISBONDED AREA OF 2"X2" ON RT AFT MOVEABLE VANE LOWER SURFACE. THE VANE LOWER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R, PROCEDURE 1, REPAIR 1, PARAGRAPH 4, FIGURE 201.
- [SDR DALA2018031001596](https://openairdocs.org/sdr/DALA2018031001596.md): Skin · debonded · Mar 9, 2018 · N896AT · Boeing 717200 · Spoilers
  > DISBONDED AREA OF 1.5"X 1.5" ON RH INBD SPOILER LWR SURFACE. THE SPOILER LOWER SURFACE WAS REPAIRED IAW SRM 51-70-02-2R-3.
- [SDR DALA2018030701456](https://openairdocs.org/sdr/DALA2018030701456.md): Frame · cracked · Mar 7, 2018 · N896AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED FRAME, BS 1225, BETWEEN 6 AND 7 HRS. THE FRAME WAS REPLACED IAW SRM 51-41-02 AND 51-40-08.
- [SDR DALA2018030601405](https://openairdocs.org/sdr/DALA2018030601405.md): Channel · cracked · Mar 6, 2018 · N896AT · Boeing 717200 · Fuselage Floor Panel
  > CRACKED CHANNELS OF FLOOR PANEL 222AFF AND FLOOR PANEL P/N 9952521U187. PERMANENT REPAIR. FLOOR PANEL 222AFF AND FLOOR PANEL P/N 9952521U187 WERE REPAIRED PER SRM 53-20-50-2R FIG 102. INSPECTION WAS ACCOMPLISHED ON FLOORS PANELS 222AFF AND P/N 9952521U187. NO
- [SDR DALA2018021400883](https://openairdocs.org/sdr/DALA2018021400883.md): Wire · shorted · Feb 14, 2018 · N896AT · Boeing 717200 · Flight Control System Wiring
  > DURING SLAT RETRACTION, AFTER TAKEOFF RECEIVED A PSEU FAIL CAUTION INDICATION. DURING APPROACH, EXTENSION OF SLATS, DOWN ARROW STAYED ON, THOUGH INTERMITTENT. PERFORMED A NO FLAP, NO SLAT LANDING IAW QRH. REPLACED THE LT SLAT A SENSOR D1-65 IAW AMM 27-84 W
- [SDR DALA2017112908380](https://openairdocs.org/sdr/DALA2017112908380.md): Fms · malfunctioned · Nov 16, 2017 · N896AT · Boeing 717200 · Flight Management Computing Hardware System
  > THE CREW DECLARED AN EMERGENCY ON APPROACH AFTER THE LOSS OF FMS GUIDED FLIGHT PLAN. MAINTENANCE FOUND BOTH VIA NR 1 & 2 DATA BUSS FAULT CODES 344343 AND 344344. REPLACED BOTH VIA NR 1 AND 2 IN ACCORDANCE WITH THE AMM. ALL TESTS NORMAL AND THE AIRCRAFT HAS R
- [SDR DALA2016121509877](https://openairdocs.org/sdr/DALA2016121509877.md): Engine · overheated · Dec 9, 2016 · N896AT · Boeing 717200 · Engine (Turbine/Turboprop)
  > THE CREW DIVERTED, FOLLOWING AN OVERHEAT OF THE LEFT ENGINE BEARING AND ASSOCIATED ROLLBACK. THE ENGINE WAS REPLACED.
- [SDR DALA2016031501940](https://openairdocs.org/sdr/DALA2016031501940.md): Fuel Tank · corroded · Mar 14, 2016 · N896AT · Boeing 717200 · Fuel Storage
  > LEFT CTR WING TANK UPPER SURFACE, BS 706 SKIN EXFOLIATED. REPAIRED IAW PRI 543588-14, REV 3 AND ER/A 543588, REV A.
- [SDR DALA2016031301880](https://openairdocs.org/sdr/DALA2016031301880.md): Cusp Web · damaged · Mar 8, 2016 · N896AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > LT CUSP WEB HAS MULTIPLE DEFECTS FROM BS 157 TO BS 1022. REPAIRED MULTIPLE DEFECTS IN LT CUSP WEB FROM BS 157 TO BS 1022 IAW SRM 53-00-55, REPAIR 4, DEPTH GAUGE USED, SN ABXF593.
- [SDR DALA2015081204916](https://openairdocs.org/sdr/DALA2015081204916.md): Battery Pack · inoperative · Aug 12, 2015 · N896AT · Boeing 717200 · Emergency Lighting
  > LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED OVERWING EMERGENCY EXIT LIGHT BATTERY.
- [SDR DALA2015060803628](https://openairdocs.org/sdr/DALA2015060803628.md): Spring · out of adjust · Jun 7, 2015 · N896AT · Boeing 717200 · Landing Gear Retraction/Extension System
  > DECLARED AN EMERGENCY BECAUSE THE NOSE GEAR DID NOT EXTEND USING NORMAL PROCEDURES. THE ALTERNATE GEAR EXTENSION WAS SUCCESSFUL AND THE FLIGHT CREW HAD A 3 GREEN INDICATIONS PRIOR TO AN UNEVENTFUL LANDING. THE ACFT WAS MAINTENANCE FERRIED FOR REPAIR. MAINTEN
- [SDR DALA2015051803313](https://openairdocs.org/sdr/DALA2015051803313.md): Battery Pack · inoperative · May 18, 2015 · N896AT · Boeing 717200 · Emergency Lighting
  > DURING SERVICE CHECK, EMERGENCY LIGHTS ABOVE FWD F/A SEAT AND CEILING WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AMM 33-51 AND CHECKS WERE GOOD.
- [SDR DALA2015031602168](https://openairdocs.org/sdr/DALA2015031602168.md): Warning Light · false activation · Mar 15, 2015 · N896AT · Boeing 717200 · Hydraulic System, Main
  > DURING LANDING GEAR EXTENSION, RT HYD QUANTITY LOW MESSAGE DISPLAYED. QUANTITY OF RIGHT HYD SYSTEM WAS INDICATING 3.5 AND HELD THERE WITH 3,000 PSI PRESSURE. DECLARED AN EMERGENCY, LANDED UNEVENTFULLY AND TAXIED NORNALLY TO THE GATE. MAINTENANCE DISCOVERED N
- [SDR DALA2015030901994](https://openairdocs.org/sdr/DALA2015030901994.md): Frame · cracked · Mar 8, 2015 · N896AT · Boeing 717200 · Fuselage Main, Frame
  > FOUND LT OVERWING FRAME STA 715 HAS CRACK INDICATION THE LENGTH IS GREATER THAN.125. VERIFIED CRACK IAW NDT SPM 06-10-01.001 WIP QC1965. REPLACED LT STA 715 OVERWING FRAME IAW WC 5310-01436-03A. LP 1852707.
- [SDR DALA2014102005637](https://openairdocs.org/sdr/DALA2014102005637.md): Battery Pack · inoperative · Oct 17, 2014 · N896AT · Boeing 717200 · Emergency Lighting
  > DURING CABIN CHECK, FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE IN FWD GALLEY AND FWD AISLE CEILING PANEL. FOUND BATTERY PACK AT B5-259 POWER SUPPLY AT FAULT. REPLACED BATTERY PACK IAW AMM 33-51. OPS CKS NORMAL IAW AMM 33-51.

Next page: https://openairdocs.org/aircraft/N896AT/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 = 'N896AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N896AT/reports

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