# Service difficulty reports: N940AT

A list on [N940AT](https://openairdocs.org/aircraft/N940AT.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 · 243 reports

- [SDR DALA2026102005747](https://openairdocs.org/sdr/DALA2026102005747.md): Engine · failed · Oct 19, 2026 · N940AT · Boeing 717200 · Engine (Turbine/Turboprop)
  > DECLARED AN EMERGENCY AND DIVERTED TO BNA DUE TO RIGHT ENGINE FAILURE. INSPECTED RIGHT ENGINE CHIP DETECTOR AND FOUND METAL DEBRIS. R & R ENGINE #2 IAW AMDS JIC 7100-9901-02. (9521740) (AIRCRAFT GROUNDED).
- [SDR DALA2026101605699](https://openairdocs.org/sdr/DALA2026101605699.md): Wire · broken · Oct 16, 2026 · N940AT · Boeing 717200 · Light System Wiring
  > DURING SVC CHK FOUND OVERHEAD EMERGENCY LIGHT AT ROW 27/28 INOPERATIVE, BROKEN WIRE. WIRE PULLED OUT OF CONTACT AT CONNECTOR, STRIPPED WIRE TO APPROPRIATE DIMS AND RE-TERMINATED WIRE IAW B717 SWPM 20-31-00 AND WDM 33- 51-12. (9521732) (AIRCRAFT GROUNDED).
- [SDR DALA2026100605533](https://openairdocs.org/sdr/DALA2026100605533.md): Pump · faulted · Oct 4, 2026 · N940AT · Boeing 717200 · Hydraulic Pump (Electric/Engine), Main
  > THE FLIGHT RETURNED TO ATL DUE TO A RIGHT HYDRAULIC TEMP HIGH MESSAGE. MAINTENANCE REPLACED THE AUX PUMP, THE PTU, AND THE RUDDER HYDRAULIC SHUTOFF VALVE. ALSO REPLACED THE RUDDER HYDRAULIC ACTUATOR ASSEMBLY. SYSTEM OPERATES NORMAL AND PERFORMED ALL ADJUSTME
- [SDR DALA2026092505348](https://openairdocs.org/sdr/DALA2026092505348.md): Skin · cracked · Sep 24, 2026 · N940AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS WERE FOUND ON FUSELAGE SKIN AND INNER DOUBLER -39, BS 1022 BETWEEN LONGERONS 13-14R, COMPLIED WITH ER/A 577210-14. (1830070) (AIRCRAFT GROUNDED).
- [SDR DALA2026062903843](https://openairdocs.org/sdr/DALA2026062903843.md): Oxygen Mask · no test · Jun 27, 2026 · N940AT · Boeing 717200 · Crew Oxygen System
  > CAPT O2 MASK FAILED TEST. R & R FO'S CREW O2 MASK PER B717 AMM 35-23. (6545751) (AIRCRAFT GROUNDED).
- [SDR DALA2026060203341](https://openairdocs.org/sdr/DALA2026060203341.md): Skin · damaged · May 30, 2026 · N940AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > ELONGATED HOLES ON EXTERNAL FUSELAGE SKIN BTW STA Y=813-832 AND LONG 26LH. PERMANENT REPAIR AND PRI 634243-14 (1621845) (AIRCRAFT GROUNDED)
- [SDR DALA2026060203338](https://openairdocs.org/sdr/DALA2026060203338.md): Doubler · corroded · May 29, 2026 · N940AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON PRODUCTION DOUBLER BTW STA Y 813. FUSELAGE WAS REPLACED PER B717-200 SRM 51-41-05 (1620108) (AIRCRAFT GROUNDED)
- [SDR DALA2026051903062](https://openairdocs.org/sdr/DALA2026051903062.md): Pan · cracked · May 15, 2026 · N940AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON UPPER DOOR JAMB PAN AT LH FWD OVERWING EMERGENCY EXIT CUT OUT AT PAXCABIN. CRACK ON UPPER DOOR JAMB PAN AT LH FWD OVERWING EMERGENCY EXIT CUT OUT AT PAXCABIN WAS REPAIRED PER ER/ A 634007-14 REV ORIG. AND PRI 634007 REV 1. (1595786) (AIRCRAFT GROUND
- [SDR DALA2026051703031](https://openairdocs.org/sdr/DALA2026051703031.md): Support · corroded · May 14, 2026 · N940AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FILLET FAIRING SUPPORT ( UPPER/LOWER, FWD/AFT FACE) AT STA 832 BTW L29 AND L26 LH AND STA 832 BTW. CORROSION LEVEL 2, FILLET FAIRING SUPPORT (UPPER/LOWER, FWD/AFT FACE) AT STA 832 BTW L29 AND L26 LH AND STA 832 BTW L28 AND L26 RH AT AFT LOWER
- [SDR DALA2026051703028](https://openairdocs.org/sdr/DALA2026051703028.md): Frame · cracked · May 12, 2026 · N940AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1037 AND LONGERON 17L AT PASSENGER CABIN. CRACK ON FRAME STA Y=1037 AND LONGERON 17L WAS REPAIRED PER ER/A 633987-14 REV ORIG. AND PRI 633987-14 REV.1. (1590318) (AIRCRAFT GROUNDED)
- [SDR DALA2026051102943](https://openairdocs.org/sdr/DALA2026051102943.md): Longeron Splice · corroded · May 7, 2026 · N940AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON SPLICE (LONG 30) AT Y= 1009 ON AFT CARGO COMPARTMENT. DAMAGED AREA REPAIRED PER B717-200 SRM 51-41-05 (1581979) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502820](https://openairdocs.org/sdr/DALA2026050502820.md): Fuel Tank · cracked · May 2, 2026 · N940AT · Boeing 717200 · Fuel Storage
  > CRACK ON WEB FUEL TANK X=56 APROX STA Y =696 AT LH CENTRAL FUEL TANK. REPAIRED PER ER/A 633561-14AD (1573556) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502819](https://openairdocs.org/sdr/DALA2026050502819.md): Pan · cracked · May 1, 2026 · N940AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON OUTER PAN (UPPER EDGE) UNDER MID BRACKET (CUTOUT AREA STA Y972 APPROX) AT AFT CARGO COMPARTMENT DOOR. REPAIR PER ER/A 633588-14 (1573299) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502815](https://openairdocs.org/sdr/DALA2026050502815.md): Frame · cracked · Apr 29, 2026 · N940AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1037 ON LONGERON 17R AT CPAX. REPAIRED PER SRM 53-20-07 (1569682) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502813](https://openairdocs.org/sdr/DALA2026050502813.md): Hinge · corroded · Apr 29, 2026 · N940AT · Boeing 717200 · Trailing Edge Flaps
  > AFTER REMOVAL BOLT ON RH WING FLAP OUTBD HINGE PIVOT AREA BS 331.1 WAS FOUND CORROSION, TOOL MARKS, ELONGATED HOLES ON HOUSING ON INBD/OUTBD FACE AT RH WING. RT WING FLAP OTBD HINGE PIVOT AREA WAS REPAIRED PER PRI 633572-14 REV 1 AND ER/A 633572-14 (1569563)
- [SDR DALA2026042302605](https://openairdocs.org/sdr/DALA2026042302605.md): Pan · cracked · Apr 22, 2026 · N940AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON INNER PAN (AFT EDGE IN BEAM 2) AT FWD PASSENGER DOOR. REPAIRED PER B717-200 S.R.M. 52-10-02 (1557418) (AIRCRAFT GROUNDED)
- [SDR DALA2026042202562](https://openairdocs.org/sdr/DALA2026042202562.md): Cusp Web · damaged · Apr 20, 2026 · N940AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > LEFT FLOOR CUPS WEB AREA (UPPER/LOWER SURFACES) BTW STA 876 TO 884 WITH ORIGINAL THICKNESS IS 0.020 INCH AND MINIMUM REMAINING THICKNESS IS 0.008 INCH THEREFORE IT IS OUT LIMITS. REPAIRED PER B717- 200 SRM 53-00-55 (1554104) (AIRCRAFT GROUNDED)
- [SDR DALA2026042102511](https://openairdocs.org/sdr/DALA2026042102511.md): Floor Support · cracked · Apr 17, 2026 · N940AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL OF FLOOR STRUCTURE BTW STA Y= 1002 TO 1022 X=0 AT CPAX. REPAIRED PER B717-200 SRM 51-70-11 (1549483) (AIRCRAFT GROUNDED)
- [SDR DALA2026042902731](https://openairdocs.org/sdr/DALA2026042902731.md): Hinge Fitting · damaged · Apr 16, 2026 · N940AT · Boeing 717200 · Trailing Edge Flaps
  > FWD HINGE FITTING #3, XW=-333.148 / INBD A OUTBD LUG / ELONGATED HOLES AND CORROSION. ASSOCIATED ER/A 00-633572 (1559456) (AIRCRAFT GROUNDED)
- [SDR DALA2026042102509](https://openairdocs.org/sdr/DALA2026042102509.md): Skin · cracked · Apr 16, 2026 · N940AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL SKIN ON STA Y=1087 BTW LONG13L AND LONG14L AT AFT UPPER FUSELAGE. REPAIRED PER ER/A 633315- 14 (1548241) (AIRCRAFT GROUNDED)
- [SDR DALA2026042902732](https://openairdocs.org/sdr/DALA2026042902732.md): Spar Cap · corroded · Apr 14, 2026 · N940AT · Boeing 717200 · Horizontal Stabilizer, Spar/Rib
  > RH HORIZONTAL STABILIZER REAR SPAR LOWER CAP, HOLES #29 AND #30, XHR=-7.234 / CORROSION. RREPAIRED PER ER/A 00-633497. (1559543) (AIRCRAFT GROUNDED)
- [SDR DALA2026041702448](https://openairdocs.org/sdr/DALA2026041702448.md): Cusp Web · cracked · Apr 14, 2026 · N940AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON RH FLOOR CUPS WEB UNDER REPAIRED DOUBLER STA 343, X=-55.5 APROX AT PAX CABIN. DAMAGED AREA REMOVED AND INSTALLED PER B717-200 SRM 53-00-55. (1544260) (AIRCRAFT GROUNDED)
- [SDR DALA2026041702446](https://openairdocs.org/sdr/DALA2026041702446.md): Cusp Web · corroded · Apr 13, 2026 · N940AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH FLOOR CUPS WEB AREA (UPPER/ LOWER SURFACES) STA 229, BTW-X =55.5 -X=44.5 APROX AT PAX CABIN. REPAIRED PER B717-200 SRM 53-00-55 (1542943) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402365](https://openairdocs.org/sdr/DALA2026041402365.md): Cusp Web · cracked · Apr 12, 2026 · N940AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB BTW STA Y= 715/719 AND BTW STA X= 44/46 WING BOX AREA AT C. PAX. CUSP WEB BTW STA Y= 715/719 AND BTW STA X= 44/46 WING BOX AREA AT C. PAX WAS REPAIRED PER SRM 53-00-55-2R REPAIR 4 FIGURE 221. (1541206) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402342](https://openairdocs.org/sdr/DALA2026041402342.md): Web · corroded · Apr 9, 2026 · N940AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RT FLOOR CUPS WEB AREA (UPPER/ LOWER SURFACES) STA 256 BTW-X =55.5 -X=44.5 APROX AT PAX CABIN. REPAIRED IAW SRM 53-00-55-2R (1536178) (AIRCRAFT GROUNDED)
- [SDR DALA2026040802225](https://openairdocs.org/sdr/DALA2026040802225.md): Beam · cracked · Apr 6, 2026 · N940AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON BEAM NR 2 (AFT EDGE) ON L1 DOOR AT CPAX.. BEAM NR 2 (AFT EDGE) ON L1 DOOR AT CPAX WAS REPAIRED PER B717-200 S.R.M. 52-10-02 (1531786) (AIRCRAFT GROUNDED)
- [SDR DALA2025122309342](https://openairdocs.org/sdr/DALA2025122309342.md): Pressure Switch · faulted · Dec 20, 2025 · N940AT · Boeing 717200 · Fuel Pressure Sensor
  > ATB - RIGHT ENGINE SYSTEM FAIL MESSAGE ALONG WITH A RIGHT ENGINE FUEL FILTER MESSAGE ON CLIMB OUT. INSPECTED FILTERS WITH NO DEBRIS NOTED. BOTH HIGH AND LOW PRESSURE FILTERS REPLACED. FILTER DIFFERENTIAL PRESSURE SWITCH REPLACED. HIGH POWER RUN PERFORMED, OP
- [SDR DALA2025111808419](https://openairdocs.org/sdr/DALA2025111808419.md): Pin · missing · Nov 13, 2025 · N940AT · Boeing 717200 · Emergency Equipment
  > SPRING AND PIN MISSING FROM L1 GIRT BAR FLOOR FITTING (AFT ONE). REPLACED L1 CABIN EVACUATION SLIDE LATCH (AFT ONE) IAW CMM 25-60-02. (7585426)
- [SDR DALA2025040902755](https://openairdocs.org/sdr/DALA2025040902755.md): Skin · cracked · Apr 5, 2025 · N940AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE EXTERNAL SKIN LOCATED ON STA Y=1037 APROX BTW L=13R AND L=14R. SUMMARY OF NRC 00056: CRACK ON FUSELAGE EXTERNAL SKIN LOCATED ON STA Y=1037 APROX BTW L=13R AND L=14R WAS REPAIRED PER ER/A 625068-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND
- [SDR DALA2025040802701](https://openairdocs.org/sdr/DALA2025040802701.md): Fastener · loose · Apr 5, 2025 · N940AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK AND LOOSE FASTENERS (HI-LOCKS) ON EXTERNAL REPAIR DOUBLER ON STA Y=1022 AND BTW LONGERONS 13R/14R AT FUSELAGE WERE FOUND DURING REPETITIVE INSPECTION PER ER/A 577210-14 REV ORIGINAL SECTION II, STEP 1. SUMMARY OF NRC 00021: SKIN ON STA Y=1022 AND BTW LON
- [SDR DALA2025100807324](https://openairdocs.org/sdr/DALA2025100807324.md): Lug · corroded · Apr 4, 2025 · N940AT · Boeing 717200 · Elevator Structure
  > AFTER REMOVAL OF INBOARD AND OUTBOARD BUSHINGS OF HINGES LOCATED AT XE= 206 AND XE= 223, CORROSION WAS FOUND ON INBOARD AND OUTBOARD LUGS OF HINGE XE= 206, AND OUTBOARD LUG OF HINGE XE= 206. CORRECTIVE ACTION: CORROSION ON INBOARD AND OUTBOARD LUGS OF HINGE XE
- [SDR DALA2025033102353](https://openairdocs.org/sdr/DALA2025033102353.md): Longeron · cracked · Mar 29, 2025 · N940AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK LONGERON 4LH & STA Y=1152 AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00090: LONGERON 4LH BTW STA Y=1169 AND STA Y=1138 WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0883561)
- [SDR DALA2025033102347](https://openairdocs.org/sdr/DALA2025033102347.md): Skin · dented · Mar 26, 2025 · N940AT · Boeing 717200 · Cargo/Baggage Doors
  > SEVERAL DENTS ON EXTERNAL SKIN OF FWD CARGO DOOR. SUMMARY OF NRC 00025: EXTERNAL SKIN OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-00-01-2R PROCEDURE 8 REPAIR 8. PERFORM AN EXTERNAL GVI OF THE REPAIR DOUBLERS ON FWD CARGO DOOR EVERY C-CHECK PER B717-200
- [SDR DALA2025040802695](https://openairdocs.org/sdr/DALA2025040802695.md): Release Mech · out of adjust · Mar 22, 2025 · N940AT · Boeing 717200 · Aerodynamic Fairings
  > THE TAILCONE RELEASE MECHANISM CAM WAS FOUND TO BE INCORRECTLY ADJUSTED: PIN ALIGMENT IS MORE THAN 38.5. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00166: TAILCONE RELEASE MEC
- [SDR DALA2025032402185](https://openairdocs.org/sdr/DALA2025032402185.md): Intercostal · corroded · Mar 22, 2025 · N940AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTALS (2 EA) AND INTERNAL DOUBLER BTW STA Y=196/212 AND BTW LONGERONS 28R/29R AT E/E COMPARTMENT. SUMMARY OF NRC 00077: CORROSION LEVEL 2. REPAIR DOUBLER WAS REPLACED PER DWG 9923686-25 REV D, PER B717 SRM 51-41-02-0G AND 51-41-05-0G. CORRO
- [SDR DALA2024121011569](https://openairdocs.org/sdr/DALA2024121011569.md): Wire · damaged · Dec 9, 2024 · N940AT · Boeing 717200 · Light System Wiring
  > SHIP 9501 -ATB/FUME- THE FLIGHT CREW RETURNED THE AIRCRAFT TO ATL DUE TO AN ACRID BURNING SMELL IN THE CABIN. CORRECTIVE ACTION: MAINTENANCE REPAIRED DAMAGED WIRES AND RING TERMINALS AT THE SERVICE DOOR OVERHEAD LIGHT ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (L
- [SDR DALA2024120911540](https://openairdocs.org/sdr/DALA2024120911540.md): Power Supply · faulted · Dec 8, 2024 · N940AT · Boeing 717200 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS ARE INOPERATIVE NEAR FWD SERVICE DOOR. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY UNIT AT CANNON PLUG P1-259 PER B717 AMM 22-51. OPERATIONAL CHECK WAS GOOD. (LP #6556658)
- [SDR DALA2024120311396](https://openairdocs.org/sdr/DALA2024120311396.md): Service difficulty · Dec 1, 2024 · N940AT · Boeing 717200 · Landing Gear Position and Warning
  > SHIP 9501 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC GOING INTO ATL DUE TO "PSEU FAIL" MESSAGE AND THE RESULTANT FLAPS-UP LANDING AS PER THE QRH. CORRECTIVE ACTION: MAINTENANCE FOUND THE LEFT SLAT A SENSOR WIRES TO BE SHORTED TO GROUND. THE WIRE
- [SDR DALA2024120211377](https://openairdocs.org/sdr/DALA2024120211377.md): Sensor · inoperative · Nov 30, 2024 · N940AT · Boeing 717200 · Landing Gear Position and Warning
  > SHIP 9501 -MISC/DE- THE FLIGHT CREW DECLARED EMERGENCY WITH ATC INTO CHA DUE TO THE "PSEU FAIL" MESSAGE. A FLAPS-UP LANDING FOLLOWED PER THE QRH. CORRECTIVE ACTION: MAINTENANCE PERFORMED BITE OF THE PSEU WHICH RETURNED CODES 326029 (PSEU INTERNAL FAULT INTERMI
- [SDR DALA2024120911533](https://openairdocs.org/sdr/DALA2024120911533.md): None · none · Nov 21, 2024 · N940AT · Boeing 717200 · Standard Practices/Structures
  > -AD- ACCOMPLISH ER/A 539703-14AD REV A SEC II. ACCOMPLISH ER/A 539703-14AD REV A SEC II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-539703 ADDED FOR AC 9501. **REDEFFE
- [SDR DALA2024100709735](https://openairdocs.org/sdr/DALA2024100709735.md): Battery Pack · inoperative · Oct 7, 2024 · N940AT · Boeing 717200 · Emergency Lighting
  > THE OVERHEAD EMERGENCY EGRESS LIGHTS ARE INOPERATIVE FROM ROW 24 THROUGH TO ROW 29. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AT 25DEF (B5-231) PER B717 AMM 33-51. CHECK IS GOOD. (LP #6103393)
- [SDR DALA2024100709734](https://openairdocs.org/sdr/DALA2024100709734.md): Lens · missing · Oct 7, 2024 · N940AT · Boeing 717200 · Emergency Lighting
  > THE OVERHEAD EMERGENCY EXIT LIGHT DIFFUSER IS MISSING AT 25/26DEF. DEFERRED 25/26DEF OVERHEAD EMERGENCY EXIT LIGHT DIFFUSER PER NEF 33-51-02. DEFERRAL REMARKS NOTED. MAINTENANCE REPLACED THE MISSING COVER ASSEMBLY REF B717 AMM 33-51. THIS ACTION CLEARS NEF 33-
- [SDR DALA2024071006987](https://openairdocs.org/sdr/DALA2024071006987.md): Skin · punctured · Jul 7, 2024 · N940AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > ON WALKAROUND FOUND PUNCTURE IN SKIN AT STATION Y256 BETWEEN LONGERONS L18 AND L17. REMOVED THE PUNCTURED REPAIR SKIN AT FR 229-FR245 BETWEEN STGR L16L & L18L PER B717 SRM 51-40-02. C/W HFEC OF DAMAGED AREA. NO CRACK INDICATIONS. FABRICATED AND INSTALLED SKIN
- [SDR DALA2024040203984](https://openairdocs.org/sdr/DALA2024040203984.md): Connector · dirty · Mar 31, 2024 · N940AT · Boeing 717200 · Fuselage Main, Bulkhead Fuselage wiring
  > SHIP 9501 -MISC/DE- THE "TAILCONE UNLOCK" MASTER CAUTION ILLUMINATED THREE TIMES DURING FLIGHT. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED BY ATC FOR THE CREW. EWR MAINTENANCE CLEANED THE CONNECTOR PLUGS OF BOTH THE INTERNAL AND EXTERNAL TAILCONE
- [SDR DALA2024011000452](https://openairdocs.org/sdr/DALA2024011000452.md): Unknown · unknown · Jan 9, 2024 · N940AT · Boeing 717200 · Air Distribution System
  > SHIP 9501 -MISC/DE- AT 13K, THE F/A REPORTED A STRONG ELECTRICAL SMELL COMING FROM FORWARD GALLEY. COCKPIT FLIGHT CREW ALSO SMELLED IT AND DONNED O2 MASKS. SOON AFTER, IT WAS ALSO REPORTED TO BEING SMELLED IN THE TAIL AS WELL. ODOR WAS GONE BY 6K IN THE DECENT
- [SDR DALA2023112809768](https://openairdocs.org/sdr/DALA2023112809768.md): Unknown · unknown · Nov 28, 2023 · N940AT · Boeing 717200 · Passenger/Crew Doors
  > THE GATE AGENT COULD NOT OPEN THE MAIN CABIN DOOR. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE FOUND THE BRACKET, THAT THE DOOR HANDLE MOUNTS TO, WITH THREE BOLTS LOOSE AND ONE BO
- [SDR DALA2023051603854](https://openairdocs.org/sdr/DALA2023051603854.md): Unknown · unknown · May 13, 2023 · N940AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CORROSION ON AFT PRESSURE BULKHEAD FORWARD FACE LOWER SECTION STA Y=1053 BETWEEN LONGERON 27L AND 27R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00116: CORROSION LEVEL 2. CORROSION ON AFT PRESSURE BULKHEAD FORWARD FACE LOWER SECTION STA Y=1053 BETWEEN LONGERON 2
- [SDR DALA2023051103712](https://openairdocs.org/sdr/DALA2023051103712.md): Unknown · unknown · May 10, 2023 · N940AT · Boeing 717200 · Fuselage Main, Bulkhead
  > AFTER REMOVING DOUBLER, CORROSION WAS FOUND ON TEE CAP AFT PRESSURE GROUP BULKHEAD FORWARD FACE LOWER SECTION STA=1053 BTW LONGERON 25R AND 28R AFT CARGO COMPARTMENT. SUMMARY OF NRC 00181: CORROSION LEVEL II. TEE PRESURE DOME ON STA 1053 WAS REPLACED PER B717-
- [SDR DALA2023051003666](https://openairdocs.org/sdr/DALA2023051003666.md): Unknown · unknown · May 9, 2023 · N940AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON WEB AFT FACE LOWER SECTION STA Y=1053 BETWEEN LONGERON 28L AND 28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00115: CORROSION LEVEL II. WEBS #9915561-53 AND #9915561-3 WERE REPLACED PER DOUGLAS DWG 9915561 REV CG AND B717-200 SRM 51-41-02-0G AND 51
- [SDR DALA2023050903615](https://openairdocs.org/sdr/DALA2023050903615.md): Unknown · unknown · May 9, 2023 · N940AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION AT END LONGERON CLIPS STA 1032 (5 EA), 27RH, 28RH, 29RH, 28LH, AND 26RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00176: LEVEL CORROSION 2. END LONGERON CLIPS #26RH, #27RH, #28RH, AND #28LH WERE REPLACED PER B-717-200 SRM 51-40-08-0G AND END LONGERON

Next page: https://openairdocs.org/aircraft/N940AT/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 = 'N940AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N940AT/reports

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