# Service difficulty reports: N928AT

A list on [N928AT](https://openairdocs.org/aircraft/N928AT.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 · 161 reports

- [SDR DALA2026102605886](https://openairdocs.org/sdr/DALA2026102605886.md): Skin · damaged · Oct 23, 2026 · N928AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE DAMAGE AT BS 860 BETWEEN LONGERONS 1 AND 2R, COMPLIED WITH ER/A 637656-14AD. (1881336) (AIRCRAFT GROUNDED).
- [SDR DALA2026102605882](https://openairdocs.org/sdr/DALA2026102605882.md): Skin · damaged · Oct 23, 2026 · N928AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE FOUND INSIDE THE ESA STC AREA, COMPLIED WITH ER/A 637656-14AD. (1881585) (AIRCRAFT GROUNDED).
- [SDR DALA2026083104911](https://openairdocs.org/sdr/DALA2026083104911.md): Switch · loose · Aug 30, 2026 · N928AT · Boeing 717200 · Aerodynamic Fairings
  > TAIL CONE EXIT TOGGLE SWITCH/LATCH LOOSE. CORRECTIVE ACTION: RESECURED AND ADJUSTED HARDWARE PER B717 AMM 52-22, NO OHTER FAULTS NOTED A/C OK TO CONT IN SVC. (9488400) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026082504809](https://openairdocs.org/sdr/DALA2026082504809.md): Skin · cracked · Aug 24, 2026 · N928AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS WERE FOUND AFFECTING THE FUSELAGE SKIN AT STA Y=1037 BETWEEN THE L-13L AND L-14L, COMPLIED WITH ER/A 624765-14. (1774752) (AIRCRAFT GROUNDED).
- [SDR DALA2026070803991](https://openairdocs.org/sdr/DALA2026070803991.md): Coalescer Bag · odor · Jul 7, 2026 · N928AT · Boeing 717200 · Humidity Control System
  > BURNING ELECTRICAL ODOR FROM FWD CARGO COMPARTMENT, R & R COELESCER BAGS PER B717 AMM 21-54. (1687018) (AIRCRAFT GROUNDED).
- [SDR DALA2026052803227](https://openairdocs.org/sdr/DALA2026052803227.md): Slide · detached · May 23, 2026 · N928AT · Boeing 717200 · Escape Slide
  > UPON ARRIVAL & OPENING 1L DOOR, EMERGENCY SLIDE SEPARATED FROM DOOR & FELL INTO JET BRIDGE. SLIDE DID NOT DEPLOY. REINSTALLED L1 DOOR SLIDE IAW B717 AMM 25-61. AC OK FOR SVC. (8235878) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502822](https://openairdocs.org/sdr/DALA2026050502822.md): Door Frame · cracked · May 3, 2026 · N928AT · Boeing 717200 · Fuselage Main, Structure
  > AFTER REMOVAL STOP FITTING CRACK WAS FOUND ON OUTER PAN AFT EDGE BEAM 4 AT AFT CARGO COMPARMENT DOOR. REPAIRED PER ERA 633375-14 (1576138) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502821](https://openairdocs.org/sdr/DALA2026050502821.md): Frame · cracked · May 2, 2026 · N928AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON CANTED FRAME AT Y=1200 AND PROJECTION. REPAIRED PER SRM 51-70-11-2R (1574671) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502814](https://openairdocs.org/sdr/DALA2026050502814.md): Support Angle · cracked · Apr 29, 2026 · N928AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE SUPPORT (FWD BULKHEAD) BTW STA Y= 816 AND LONGERON 30 AT AFT CARGO COMPARTMENT. CRACK ON ANGLE SUPPORT (FWD BULKHEAD) BTW STA Y= 816 AND LONGERON 30 AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 53-00-00 (1569678) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502812](https://openairdocs.org/sdr/DALA2026050502812.md): Intercostal · corroded · Apr 29, 2026 · N928AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BTW STA Y=1022.091 TO Y=1037 AND L30 AT AFT CARGO COMPARTMENT. REPAIRED PER SRM 51-41-02-0G AND B717-200 SRM 51-41-05. (1568910) (AIRCRAFT GROUNDED)
- [SDR DALA2026042902729](https://openairdocs.org/sdr/DALA2026042902729.md): Seat Track · cracked · Apr 27, 2026 · N928AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 9571 AFTER REMOVE OF THE CUSP WEB, SEAT TRACK WAS FOUND WHIT CRACK. CORRECTIVE ACTION: SEAT TRACK WHIT CRACK WAS REPAIRED PER B717-200 SRM 53-20-52 (1566030) (AIRCRAFT GROUNDED)
- [SDR DALA2026042902728](https://openairdocs.org/sdr/DALA2026042902728.md): Cusp Web · cracked · Apr 27, 2026 · N928AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9571 CRACK ON RH CUSP WEB BTW STA Y= 617 TO Y=636, Y=636 TO Y=655 AND Y=656 TO Y=674. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55 (1565636) (AIRCRAFT GROUNDED)
- [SDR DALA2026042902727](https://openairdocs.org/sdr/DALA2026042902727.md): Cusp Web · cracked · Apr 26, 2026 · N928AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9571 CRACK ON CUSP WEB BTW STA Y=655 AND X= 56 AT PASSENGER CABIN. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 AND SRM 51-41-02-0G AND SRM 51-41-05 (1564249) (AIRCRAFT GROUNDED)
- [SDR DALA2026042902726](https://openairdocs.org/sdr/DALA2026042902726.md): Cusp Web · cracked · Apr 25, 2026 · N928AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9571 CRACK AND MISSING MATERIAL ON RH CUSP WEB AT STA 460 X=56 AT CPAX. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55 (1561674) (AIRCRAFT GROUNDED)
- [SDR DALA2026042902725](https://openairdocs.org/sdr/DALA2026042902725.md): Cusp Web · cracked · Apr 25, 2026 · N928AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9571 CORROSION ON RH CUSP WEB LOWER AREA BTW STA 218 AND 228, X=54 AT CPAX. CORRECTIVE ACTION: REPAIRED PER 717-200 SRM 51-41-05-0G AND SRM 51-40-02. (1561481) (AIRCRAFT GROUNDED)
- [SDR DALA2026042902724](https://openairdocs.org/sdr/DALA2026042902724.md): Cusp Web · cracked · Apr 25, 2026 · N928AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSB WEB BTW STA Y= 715 TO STA Y= 737 AND X=44. REPAIRED PER B717-200 SRM 53-00-55 (1561470) (AIRCRAFT GROUNDED)
- [SDR DALA2026042302604](https://openairdocs.org/sdr/DALA2026042302604.md): Frame · cracked · Apr 22, 2026 · N928AT · Boeing 717200 · Fuselage Main, Frame
  > INITIAL INSPECTION: CRACK ON CAP IN FRAME Y=1022 AND L 7R AT CPAX. REPAIR AND PRI 633416-14 (1557376) (AIRCRAFT GROUNDED)
- [SDR DALA2026042302603](https://openairdocs.org/sdr/DALA2026042302603.md): Web · corroded · Apr 22, 2026 · N928AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB BTW STA Y=180, STA Y=200, X =54 AND X=44.5 AT CPAX. REPAIRED PER B717-200 SRM 51-70-10 (1557318) (AIRCRAFT GROUNDED)
- [SDR DALA2026042202563](https://openairdocs.org/sdr/DALA2026042202563.md): Web · cracked · Apr 20, 2026 · N928AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CORNER AT LOWER WEB STA Y= 219 X= 55. REPAIRED PER B717-200 SRM 51-70-10 (1554629) (AIRCRAFT GROUNDED)
- [SDR DALA2026042202561](https://openairdocs.org/sdr/DALA2026042202561.md): Floor Support · corroded · Apr 19, 2026 · N928AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT ON X=44.5 BTW STA Y= 148 AND STA Y=200 AT CPAX. REPAIRED PER SRM 51-41-02-0G AND B717-200 SRM 51-41- 05. (1551876) (AIRCRAFT GROUNDED)
- [SDR DALA2026042202560](https://openairdocs.org/sdr/DALA2026042202560.md): Intercostal · cracked · Apr 18, 2026 · N928AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9571 CRACK ON INTERCOSTAL ON UPPER AFT CORNER ALSO CRACK NEAR FASTENERS ON CLIP IN THE SAME INTERCOSTAL X=0 ON STA Y=1022 AT CPAX. REPAIRED PER B717-200 SRM 53-00-00 (1550325) (AIRCRAFT GROUNDED)
- [SDR DALA2026041702447](https://openairdocs.org/sdr/DALA2026041702447.md): Cusp Web · cracked · Apr 13, 2026 · N928AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AFTER CRACK REMOVAL ON CUSP WEB STA Y=655-684 RH SIDE, AT PASSENGER COMPARTMENT. REPAIRED PER B717-200 SRM 53-00-55 (1542990) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402367](https://openairdocs.org/sdr/DALA2026041402367.md): Frame · cracked · Apr 12, 2026 · N928AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME BS 1037 AND L17R. REPAIRED PER SRM 53-20-07 (1541418) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402346](https://openairdocs.org/sdr/DALA2026041402346.md): Longeron · cracked · Apr 10, 2026 · N928AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON RH #17, RH #8 AND RH #6 STA Y=1022 AT CPAX. REPAIRED PER SRM 53-00-05 (1538208) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402344](https://openairdocs.org/sdr/DALA2026041402344.md): Skin · dented · Apr 10, 2026 · N928AT · Boeing 717200 · Rudder, Plate/Skin
  > DENTS 2E/A ON LH EXTERNAL SKIN OF RUDDER ZR 42. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 51-70-13-2R-1. (1536804) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402343](https://openairdocs.org/sdr/DALA2026041402343.md): Skin · cracked · Apr 9, 2026 · N928AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL FUSELAGE SKIN BS 1037 BTW LONG 13 RT & 14 RT. REPAIRED PER PRI 633254-14 REV. 2 AND ER/A 633254-14 (1536512) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402348](https://openairdocs.org/sdr/DALA2026041402348.md): Hinge Fitting · corroded · Apr 7, 2026 · N928AT · Boeing 717200 · Trailing Edge Flaps
  > CORROSION ON CENTER FLAP HINGE FITTING (OUTB/ LOWER HOLE AND STUD) STA XRS 260.000 APROX AT LH WING. CORRECTIVE ACTION: FITTING WAS REMOVED PER B717-200 AMM 57-55-25 (1532955) (AIRCRAFT GROUNDED)
- [SDR DALA2026041302317](https://openairdocs.org/sdr/DALA2026041302317.md): Floor Support · corroded · Apr 6, 2026 · N928AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9571 CORROSION ON FLOOR SUPPORT APPROX STA Y=180 BTW X=44.5 AND X=15 AT CPAX. DAMAGED AREA REPAIRED PER DWG 9936534-43 AND B717-200 SRM 51-41-02 (1531523) (AIRCRAFT GROUNDED).
- [SDR DALA2026033002083](https://openairdocs.org/sdr/DALA2026033002083.md): Beam · cracked · Mar 29, 2026 · N928AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACKED OUTER PAN, FWD EDGE, BEAM NR 5 AT THE FWD CARGO DOOR. THE BEAM WAS REPAIRED IAW SRM 52-30-02. (1518647)
- [SDR DALA2026033002082](https://openairdocs.org/sdr/DALA2026033002082.md): Pan · cracked · Mar 29, 2026 · N928AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACKED OUTER PAN, FWD EDGE, BEAM NR 3 IN THE FWD CARGO DOOR. THE CARGO DOOR WAS REPAIRED IAW SRM 52-30-02. (1518642)
- [SDR DALA2026033002081](https://openairdocs.org/sdr/DALA2026033002081.md): Longeron · cracked · Mar 29, 2026 · N928AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 8L, BS 1022. CRACKED LONGERON 8L WAS REPAIRED IAW SRM 53-00-05, (1518640)
- [SDR DALA2026031001647](https://openairdocs.org/sdr/DALA2026031001647.md): Controller · faulted · Mar 6, 2026 · N928AT · Boeing 717200 · Trailing Edge Flap Control System
  > SHIP 9571-ATB- RETURNED TO ATL DUE TO A FLAP/SLAT DISAGREE MESSAGE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE #2 FCC DUE TO ERRATIC SENSOR READOUTS. COMPLIED WITH NO-GO MSI AND RETURNED TO SERVICE.(8112258)
- [SDR DALA2025031001823](https://openairdocs.org/sdr/DALA2025031001823.md): Skin · cracked · Mar 10, 2025 · N928AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK EVIDENCE ON FUSELAGE SKIN LOCATED ON STA Y=1037 AND L-14L. SUMMARY OF NRC 0180: AREA WAS REPAIRED ON FUSELAGE SKIN LOCATED ON STA Y=1037 AND L-14L PER PRI 624765-14 REV 2 AND PER ER/A 624765-14 REV ORIG SECTION I. REPAIR APPROVAL IS LIMITED TO 24 MONTHS
- [SDR DALA2025031001822](https://openairdocs.org/sdr/DALA2025031001822.md): Elec Connector · damaged · Mar 8, 2025 · N928AT · Boeing 717200 · Light System Wiring
  > THE EMERGENCY LIGHT DOES NOT TURN ON IN THE AFT ACCESSORY VENTRAL WALKWAY. SUMMARY OF NRC 00219: CONNECTOR P1-260 OF BATTERY PACK B5-250 AND CONNECTOR P1-116 OF BATTERY PACK B5-116 WAS CONNECTED CORRECTLY PER B717 WDM 33-51-11 AND PERFORMED TEST PER B717 AMM 3
- [SDR DALA2025031001819](https://openairdocs.org/sdr/DALA2025031001819.md): Frame · cracked · Mar 7, 2025 · N928AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1037 LONG 17 LH. SUMMARY OF NRC 00189: FRAME STA Y=1037 LONG 17 LH WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0845545)
- [SDR DALA2025030401649](https://openairdocs.org/sdr/DALA2025030401649.md): Skin · worn · Mar 3, 2025 · N928AT · Boeing 717200 · Passenger/Crew Doors
  > WEAR ON EXTERNAL SKIN, NEAR CUT OUT OF HOOK, AT PASSENGER DOOR L1. SUMMARY OF NRC 00036: DAMAGE ON EXTERNAL SKIN, NEAR CUT OUT OF HOOK, AT PASSENGER DOOR L1 WAS REPAIRED PER ER/A 624489-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 624489-14 REV 1. ASSOC
- [SDR DALA2025030301648](https://openairdocs.org/sdr/DALA2025030301648.md): Pan · corroded · Mar 1, 2025 · N928AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO DOOR JAMB PAN BTW LONG 24RH TO LONG 27RH (NEW SECTION AND PRODUCTION SECTION OF PAN). SUMMARY OF NRC 00118: CORROSION LEVEL 2. CARGO DOOR JAMB PAN STA 954 LONG 28 LH AND STA 986 BTW LONG 28 RH WAS REPAIRED PER B717-200 SRM 53-20-15-2R RE
- [SDR DALA2025022101361](https://openairdocs.org/sdr/DALA2025022101361.md): Fastener · loose · Feb 19, 2025 · N928AT · Boeing 717200 · Vertical Stabilizer
  > -AD- LOOSE FASTENERS OF RH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267) WERE FOUND IN REFERENCE TO AMDS 5530-01048-02 STEP 3 "AA 5530-01048" AND "AD 2018-10-08". SUMMARY OF NRC 00058: FASTENERS (5 EA) OF RH VERTICAL STABILIZER LEADING EDG
- [SDR DALA2024071006986](https://openairdocs.org/sdr/DALA2024071006986.md): Battery · inoperative · Jul 8, 2024 · N928AT · Boeing 717200 · Emergency Lighting
  > ON SERVICE CHECK FOUND OVERWING EMERGENCY EVACUATION LIGHTS NOT ILLUMINATING. REPLACED OVERWING EMERGENCY EVACUATION LIGHT BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. LIGHTS NOW ILLUMINATE CORRECTLY. (LP #6026764)
- [SDR DALA2024042404676](https://openairdocs.org/sdr/DALA2024042404676.md): Lens · missing · Apr 24, 2024 · N928AT · Boeing 717200 · Emergency Lighting
  > THE CABIN CREW NOTED THAT THE AFT TAIL COMPT EMERGENCY EXIT LIGHT LENS IS MISSING. MAINTENANCE INSTALLED THE MISSING LIGHT COVER AT AFT TAIL OF AIRCRAFT. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #5829167)
- [SDR DALA2023042603245](https://openairdocs.org/sdr/DALA2023042603245.md): Unknown · unknown · Apr 24, 2023 · N928AT · Boeing 717200 · Service Doors
  > PARTS DEPARTED AICRAFT. GROUND CREW FOUND AIRCRAFT PANEL ACCESS DOOR MISSING. MAINTENANCE REPLACED THE GROUND AIR PANEL ACCESS DOOR. TOP/3998-23 (LP #4027955)
- [SDR DALA2023042503244](https://openairdocs.org/sdr/DALA2023042503244.md): Unknown · unknown · Apr 22, 2023 · N928AT · Boeing 717200 · Flight Compartment Windows
  > ARCING LIGHT WITH ASSOCIATED SMELL AND NOISE FROM BEHIND TRIM FORWARD OF F/O CLEARVIEW WINDOW. CBZ24 PULLED R/H WINDSHIELD ANTI-ICE FOR TROUBLESHOOTING NA 2375451. REMOVED R1 WINDSHIELD IAW B717 56-11-02. PERFORMED TERMINAL BLOCK REPLACEMENT PER ERA 608256-14
- [SDR DALA2023033102475](https://openairdocs.org/sdr/DALA2023033102475.md): Unknown · unknown · Mar 29, 2023 · N928AT · Boeing 717200 · Trailing Edge Flaps
  > AIRCRAFT 9571, INITIAL INSPECTION: BROKEN BRACKET INSIDE ACCESS PANEL NBR 530AF ON FLAP AT LH WING. CORRECTIVE ACTION: BRACKET INSIDE ACCESS PANEL NBR 530AF ON FLAP AT LH WING WERE REPLACED PER B-717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP 2694546)
- [SDR DALA2023033102474](https://openairdocs.org/sdr/DALA2023033102474.md): Unknown · unknown · Mar 29, 2023 · N928AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9571, INITIAL INSPECTION: CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SECTION OF DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-04-0G, B717-200 SRM 51-41-02-0G, B717-200 SRM 51-41-05-0G. AND B717-2
- [SDR DALA2023032602317](https://openairdocs.org/sdr/DALA2023032602317.md): Unknown · unknown · Mar 25, 2023 · N928AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9571, CORROSION AT SLIDE SUPPORTS LOCATED AT RBL 53 BETWEEN STA-163 AND STA-186. CORRECTIVE ACTION: NEW SUPPORTS (2EAS) WERE REPLACED PER B717-200 SRM 51-41-01-0G PAR 6. (LP 2686865)
- [SDR DALA2023032602315](https://openairdocs.org/sdr/DALA2023032602315.md): Unknown · unknown · Mar 24, 2023 · N928AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9571, DURING OK TO TREAT RH WING BOX AREA WITH CIC, CRACKED CUSP MEMBRANE WEB WAS FOUND ON STA Y= 715-720 X=-44 AT PASSENGER CABIN FLOOR STRUCTURE. CORRECTIVE ACTION: CUSP MEMBRANE WEB ON STA Y= 715-720 X=-44 AT PASSENGER CABIN FLOOR STRUCTURE WAS REP
- [SDR DALA2023030801721](https://openairdocs.org/sdr/DALA2023030801721.md): None · none · Mar 4, 2023 · N928AT · Boeing 717200 · Hydraulic System, Main
  > SHIP 9571 -HYD/DE- THE FLIGHT CREW DECLARED AN EMERGENCY INTO ATL DUE TO THE "RIGHT HYDRAULIC LOW-PRESSURE" MESSAGE. THE ALTERNATE GEAR EXTENSION PROCEDURES WERE UTILIZED, AND THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT HYDRAU
- [SDR DALA2023011000173](https://openairdocs.org/sdr/DALA2023011000173.md): Light · miswired · Jan 9, 2023 · N928AT · Boeing 717200 · Light System Wiring
  > FOUND EMERGENCY LIGHT FLOOD LIGHT AT R1 DOOR INOPERATIVE. FOUND POWER WIRE FOR EMERGENCY LIGHT IN WRONG TERMINAL. RE-CONFIGURED PER WDM 33-51-12. ALSO FOUND POWER SUPLY BAD AND REPLACED IT PER B717 AMM 33-51. (B5-235) EMERGENCY LIGHT OPERATION IS NOW NORMAL. (
- [SDR DALA2022061704243](https://openairdocs.org/sdr/DALA2022061704243.md): Hub Cap · missing · Jun 13, 2022 · N928AT · Boeing 717200 · Brake Anti-Skid Section
  > ON LANDING IN KGRR, GOT "ANTI-SKID L FAIL" MESSAGE. ON SD BRAKES WERE NOT APPLIED UNTIL ABOUT 75 KNOTS ON LANDING ROLL. *** CONTRACT MAINTENANCE EVENT - OCM: 248846 *** FOUND LT INBD HUBCAP MISSING. INSTALLED NEW HUBCAP ASSY REF B717 AMM 32-41. C/W RTS CK OF A
- [SDR DALA2020021801205](https://openairdocs.org/sdr/DALA2020021801205.md): Sign · inoperative · Feb 18, 2020 · N928AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN IS INOPERATIVE AT 603. EXIT PLACARD MISSING ON CEILING EXIT SIGN AT WINDOW EXITS. MAINTENANCE FOUND THE MISSING EXIT SIGN LENS AND REINSTALLED IT IN SERVICEABLE CONDITION. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS NOW OK FOR SERVICE. (LP

Next page: https://openairdocs.org/aircraft/N928AT/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 = 'N928AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N928AT/reports

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