# Service difficulty reports: N946AT

A list on [N946AT](https://openairdocs.org/aircraft/N946AT.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 6 · 270 reports

- [SDR DALA2026072704342](https://openairdocs.org/sdr/DALA2026072704342.md): Stop · out of adjust · Jul 24, 2026 · N946AT · Boeing 717200 · Passenger/Crew Doors
  > MAIN CABIN DOOR WOULD NOT CORRECTLY LATCH INTO GUST LOCK. READJUST DOOR LATCH MECH/RUBBER STOP IAW AMM 52-12 GUST LOCK ENGAGES/ DISENGAGES AS NORMAL. DOOR OPS CHK NORMAL. A/C OK FOR SVC. (8792584) AIRCRAFT GROUNDED.
- [SDR DALA2026041402345](https://openairdocs.org/sdr/DALA2026041402345.md): Skin · cracked · Apr 10, 2026 · N946AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > REF ERA 606161-14AD REV B STEP 4 OHEC INSP OF LEFT SIDE OF VERT STAB-5TH HOLE FROM BOTTOM HAS CRACK INDICATION. REPAIRED DAMAGE PER ER/A 606161-14AD (8672001) (AIRCRAFT GROUNDED)
- [SDR DALA2025101707595](https://openairdocs.org/sdr/DALA2025101707595.md): Spar Cap · cracked · Oct 15, 2025 · N946AT · Boeing 717200 · Vertical Stabilizer, Spar/Rib
  > SHIP 9506 CRACK WAS FOUND ON HOLE 6 HRS AT STA ZFS=51.267 APROX. FRONT SPAR CAP FORWARD FLANGE VERTICAL STABILIZER LH SIDE. CORRECTIVE ACTION: REPAIR ON FRONT SPAR CAP FORWARD FLANGE VERTICAL STABILIZER LH SIDE WAS PERFORMED PER PRI 606161-14 (1254228)
- [SDR DALA2025101707594](https://openairdocs.org/sdr/DALA2025101707594.md): Skin · damaged · Oct 13, 2025 · N946AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > FASTENERS (45 EA) ON VERTICAL STAB LEADING EDGE PREVIOUS REPAIR STA ZFS =52. CORRECTIVE ACTION: VERTICAL STAB LEADING EDGE REPAIR STA ZFS =52 WERE REMOVE AND INSTALL PER CARD 5530-01048-02 AND DVI WAS PERFORMED ON RH/LH VERTICAL STAB LEADING EDGE STRUCTURE SPL
- [SDR DALA2025101707591](https://openairdocs.org/sdr/DALA2025101707591.md): Service Panel · corroded · Oct 10, 2025 · N946AT · Boeing 717200 · Fuselage Main, Structure
  > SHIP 9506 CORROSION ON LOWER AREA OF LAVATORY SERVICE PANEL BTW TRAY-PANEL AND PREVIOUS REAPAIR INTERNAL FILLER. CORRECTIVE ACTION: REPAIRED PER ER/A 542102- 14 REV. (1245325)
- [SDR DALA2025101407521](https://openairdocs.org/sdr/DALA2025101407521.md): Vane · dented · Oct 7, 2025 · N946AT · Boeing 717200 · Trailing Edge Flaps
  > DISBOND OF 2.300IN X 3.100IN. ON DENT LOCATED AT LH AFT MOVABLE FLAP VANE, LOWER SURFACE. REPAIRED PER B717-200 SRM 57-53-01-2R (1239681)
- [SDR DALA2025101407519](https://openairdocs.org/sdr/DALA2025101407519.md): None · none · Oct 4, 2025 · N946AT · Boeing 717200 · Standard Practices/Structures
  > DTA ER/A 542233-14 REV D REPAIR MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 04-OCT-25. C/W ER/A 542233-14. (1245089)
- [SDR DALA2025030101574](https://openairdocs.org/sdr/DALA2025030101574.md): Transfer Valve · failed · Feb 27, 2025 · N946AT · Boeing 717200 · Landing Gear Retraction/Extension System
  > SHIP 9506-ATB- THE FLIGHT CREW PERFORMED AN AIR TURN BACK DUE TO A RIGHT HYDRAULIC SYSTEM FAILURE. AN EMERGENCY WAS DECLARED WITH ATC. THE LANDING WAS UNEVENTFUL EXCEPT FOR THE MAIN LANDING GEAR DOORS CONTACTING THE RUNWAY UPON ROLLOUT. CORRECTIVE ACTION: MAIN
- [SDR DALA2024121111611](https://openairdocs.org/sdr/DALA2024121111611.md): Unknown · not reported · Dec 4, 2024 · N946AT · Boeing 717200 · Standard Practices/Structures
  > -AD- MONITOR LOG REQUIRES PERMANENT REPAIR INSTRUCTIONS FOR ER/A 542233-14AD SECTION IV PRIOR TO 30-NOV-2025. CONTACT LIAISON ENGINEERING, DEP 555, FOR INSTRUCTIONS. DISCONTINUE REVENUE SERVICE ON OR PRIOR TO 30-NOV-25. PERMANENT REPAIR REQUIRED PER ERA 542233
- [SDR DALA2024120311391](https://openairdocs.org/sdr/DALA2024120311391.md): Bulkhead · abnormal · Nov 13, 2024 · N946AT · Boeing 717200 · Fuselage Main, Bulkhead
  > -AD- ACCOMPLISH ER/A 542233-14AD REV B SEC II. ACCOMPLISH ER/A 542233-14AD REV B SEC II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-542233 ADDED FOR AC 9506. ACCOMPLIS
- [SDR DALA2024081908281](https://openairdocs.org/sdr/DALA2024081908281.md): Splice · cracked · Aug 18, 2024 · N946AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > -AD- FOUND 2 CRACK INDICATIONS ON LEFT SIDE OF VERTICAL STAB BELOW SPLICE AT STA 2F552.267 WHILE PERFORMING BHEC PER AA 5530-01048 STEP 8 REF AD2018-10-08. HOLES ARE MARKED. AFTER SEPARATION OF LAYERS CONFRIMED CRACK INDICATIONS FROM FWD FLANGE LAYER REF AA553
- [SDR DALA2023102008639](https://openairdocs.org/sdr/DALA2023102008639.md): Unknown · unknown · Oct 19, 2023 · N946AT · Boeing 717200 · Escape Slide
  > INSPECTOR FOUND THE HALF HINGE INSTALLED WRONG ON THE TAIL EMERGENCY SLIDE COVER. 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 00212: HALF HINGE ON TAIL EMERGENCY SLIDE COVER WA
- [SDR DALA2023101808564](https://openairdocs.org/sdr/DALA2023101808564.md): Unknown · unknown · Oct 16, 2023 · N946AT · Boeing 717200 · Trailing Edge Flaps
  > SEVERAL DENTS ON LOWER SURFACE AT INB FWD MOVABLE FLAP VANE RH WING. SUMMARY OF NRC 00033: LOWER SURFACE AT INB FWD MOVABLE FLAP VANE RH WING WAS REPAIRED PER B717-200 SRM 51-70-02-0G PROCEDURE GENERAL IN REFERENCE TO B717-200 SRM 57-53-01-2R PROCEDURE 1 PAR 4
- [SDR DALA2023101608457](https://openairdocs.org/sdr/DALA2023101608457.md): Unknown · unknown · Oct 15, 2023 · N946AT · Boeing 717200 · Fuselage Main, Floor Beam
  > CRACK ON PAN IN BEAM 2 AND ON PAN BTW BEAM 7 TO 8 ON AFT SIDE OF PASSENGER DOOR L1. SUMMARY OF NRC 00095: PAN IN BEAM 2 AND PAN BTW BEAM 7 TO 8 AT AFT SIDE OF PASSENGER DOOR L1 WERE REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #0018804)
- [SDR DALA2023101608455](https://openairdocs.org/sdr/DALA2023101608455.md): Unknown · unknown · Oct 14, 2023 · N946AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON INTERCOSTAL BTW STA Y=927-946 ON LONGERON 29R. ALSO CORROSION ON INTERCOSTAL BTW STA 1022 TO 1037 AND LONGERON 30 AT AFT CARGO. SUMMARY OF NRC 00111: CORROSION LEVEL 2. INTERCOSTAL BTW STA Y=927-946 ON LONGERON 29 RH WAS REPLACED PER B717-200 SRM
- [SDR DALA2023101408448](https://openairdocs.org/sdr/DALA2023101408448.md): Unknown · unknown · Oct 14, 2023 · N946AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CORROSION ON AFT PRESSURE BULKHEAD FWD FACE LOWER AREA BTW LONG PROJECTION 28L TO 28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00116: CORROSION LEVEL 2. AFT PRESSURE BULKHEAD FWD FACE LOWER AREA BTW LONG PROJECTION 28L TO 28R AT AFT CARGO COMPARTMENT WAS REPAI
- [SDR DALA2023101408446](https://openairdocs.org/sdr/DALA2023101408446.md): Unknown · unknown · Oct 14, 2023 · N946AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON BEAM 6 AFT SIDE OF PASSENGER DOOR L1. SUMMARY OF NRC 00094: BEAM 6 AFT SIDE OF PASSENGER DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 12. (LP #0016617)
- [SDR DALA2023101408445](https://openairdocs.org/sdr/DALA2023101408445.md): Unknown · unknown · Oct 13, 2023 · N946AT · Boeing 717200 · Fuselage Main, Frame
  > HIDDEN CRACK ON FRAME WEB RH, AND ENLOGATED HOLES BTW LONGERON 27 RH TO LONGERON 28 RH, FROM STA 1053 (AFT CARGO). SUMMARY OF NRC 00184: CRACK AND ELOGATED HOLES ON FRAME WEB RH BTW LONGERON 27 RH TO LONGERON 28 RH FROM STA 1053 WERE REPAIRED PER B717-200 SRM
- [SDR DALA2023101408444](https://openairdocs.org/sdr/DALA2023101408444.md): Unknown · unknown · Oct 13, 2023 · N946AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 30 BTW FRAME STA 908 AND 1022.901 INCLUDING SPLICE (1 EA) AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00109: CORROSION LEVEL 2. LONGERON 30 BTW FRAME STA 908 AND 1022.901 INCLUDING SPLICE (1 EA) AT AFT CARGO COMPARTMENT WERE REPLACED PER B71
- [SDR DALA2023101408440](https://openairdocs.org/sdr/DALA2023101408440.md): Unknown · unknown · Oct 12, 2023 · N946AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON FWD REPAIR SPLICE AT LOWER DOOR JAMB AFT CARGO COMPARTMENT. SUMMARY OF NRC 00167: FWD PREVIOUS REPAIR SPLICE AT LOWER DOOR JAMB AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G, 51-41-02-0G, AND SRM 53-20-15-0G PROCEDURE REPAIR 7. (
- [SDR DALA2023052504151](https://openairdocs.org/sdr/DALA2023052504151.md): Unknown · unknown · May 25, 2023 · N946AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN AT THE AFT CABIN BULKHEAD DOOR IS INOPERATIVE. MAINTENANCE REPLACED THE BF-260 BATTERY PACK PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #4742276)
- [SDR DALA2023030201551](https://openairdocs.org/sdr/DALA2023030201551.md): None · none · Feb 28, 2023 · N946AT · Boeing 717200 · Cargo/Baggage Doors
  > FOUND DAMAGE AFT CARGO DOOR OPENING. AFT SIDE SEAL RETAINER SPLICE ANGLE CRACKED NEAR TEFLON GUIDE. REMOVED AFT DEPRESSOR SPLICE PER B717 SRM 53-20-15-2R-10. REPAIRED JAMB SEAL DEPRESSOR PER B717 SRM 53-20-15-2R-4. OK FOR SERVICE. (LP #9493774)
- [SDR DALA2023022701429](https://openairdocs.org/sdr/DALA2023022701429.md): None · none · Feb 27, 2023 · N946AT · Boeing 717200 · Emergency Lighting
  > THE R1 DOOR EMERGENCY INDENTIFIER SIGN LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY ASSEMBLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #9493766)
- [SDR DALA2023022701431](https://openairdocs.org/sdr/DALA2023022701431.md): None · none · Feb 25, 2023 · N946AT · Boeing 717200 · Vertical Stabilizer, Spar/Rib
  > FOUND 2 HOLES WITH CRACK INDICATIONS ON LH VERT STAB FRONT SPAR CAP FWD FLANGE, REF AA 5530-01048 AND AD 2018-10-08. REMOVED LH FASTENERS FROM VERT LEADING EDGE. REMOVED VERT LEADING EDGE PER B717 AMM 55-32-01. C/W BHEC OF SEPERATED LAYERS, FOUND CRACK INDICAT
- [SDR DALA2024121311699](https://openairdocs.org/sdr/DALA2024121311699.md): Skin · damaged · Feb 24, 2023 · N946AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > -AD- AMOC 606161-14AD - B717-200 VERTICAL STABILIZER LEADING EDGE SKIN ZFS 52.267 OVERSIZE HOLES. REPAIR APPROVAL IS LIMITED TO TWENTY-FOUR (24) MONTHS SERVICE FROM DATE OF APPROVAL ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CON
- [SDR DALA2022092806343](https://openairdocs.org/sdr/DALA2022092806343.md): None · none · Sep 27, 2022 · N946AT · Boeing 717200 · Emergency Lighting
  > DURING A SERVICE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS FOR ROWS 1-10, TO BE INOPERATIVE. THE BATTERY PACK B5-227 WAS REPLACED AND THE EMERGENCY LIGHTS RETURNED TO AN OPERATIONAL STATUS. (LP #9128785)
- [SDR DALA2022070504623](https://openairdocs.org/sdr/DALA2022070504623.md): None · none · Jul 2, 2022 · N946AT · Boeing 717200 · Emergency Lighting
  > ON SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS POWERED BY BATTERY PACK 135-119 WERE INOPERATIVE. REPLACED 135-119 AND APPLICABLE POWER SUPPY PER B717 AMM 33-51. (LP #8829612)
- [SDR DALA2022070504627](https://openairdocs.org/sdr/DALA2022070504627.md): None · none · Jul 2, 2022 · N946AT · Boeing 717200 · Emergency Lighting
  > ON SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS POWERED BY B5-231 WERE INOPERATIVE. REPLACED B5-231 AND APPLICABLE POWER SUPPY PER B717 AMM 33-51. (LP #8829616)
- [SDR DALA2022053103724](https://openairdocs.org/sdr/DALA2022053103724.md): Battery Pack · inoperative · May 28, 2022 · N946AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN FOR THE OVER WING EXIT WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE EXIT SIGN BATTERY PACK. OPERATIONAL CHECK IS NORMAL AT THIS TIME REF B717 AMM 33-51. (LP #8804889)
- [SDR DALA2022053103723](https://openairdocs.org/sdr/DALA2022053103723.md): Battery Pack · inoperative · May 28, 2022 · N946AT · Boeing 717200 · Emergency Lighting
  > THE FIRST CLASS EXIT SIGN WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK IS NORMAL AT THIS TIME REF B717 AMM 33-51. (LP #8804888)
- [SDR DALA2022040702384](https://openairdocs.org/sdr/DALA2022040702384.md): Sign · missing · Apr 6, 2022 · N946AT · Boeing 717200 · Emergency Lighting
  > SERVICE CHECK FOUND THAT THE EXIT SIGN IS MISSING AT 1R DOOR. MAINTENANCE REPLACED THE EXIT SIGN AT 1R DOOR PER B717 AMM 33-51. AIRCRAFT IS OK FOR SERVICE. (LP #8758656)
- [SDR DALA2021122908129](https://openairdocs.org/sdr/DALA2021122908129.md): None · none · Dec 21, 2021 · N946AT · Boeing 717200 · Wing, Control Surfaces
  > **THIS LOG REPLACES LOG 2010626.** DENTS LEFT UPPER FLAP MOVEABLE VANE. SUMMARY OF NRC 00049: LEFT UPPER FLAP MOVEABLE VANE WAS REPAIRED PER B-717-200 SRM 51-70-02-0G PROCEDURE GENERAL ON REFERENCE OF B-717-200 SRM 57-53-01-2R-1 PAR. 4. PERFORM DECAL INSP COND
- [SDR DALA2024040804187](https://openairdocs.org/sdr/DALA2024040804187.md): Vane · dented · Nov 8, 2021 · N946AT · Boeing 717200 · Trailing Edge Flaps
  > DENTS LEFT UPPER FLAP MOVEABLE VANE (AI). SUMMARY OF NRC 00049: LEFT UPPER FLAP MOVEABLE VANE WAS REPAIRED PER B-717-200 SRM 51-70-02-0G PROCEDURE GENERAL ON REFERENCE OF B-717-200 SRM 57-53-01-2R-1 PAR. 4. PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PE
- [SDR DALA2021110606828](https://openairdocs.org/sdr/DALA2021110606828.md): None · none · Nov 6, 2021 · N946AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON EXTERNAL FUSELAGE SKIN BTW STA 626 TO STA 690 AND BTW L-28L TO L-28R. SUMMARY OF NRC 00199: CORROSION LEVEL 2: AFTER BLENDING FOUND DAMGE TO BE OUT OF LIMITS. PERMANENT REPAIR WAS PERFORMED ON EXTERNAL FUSELAGE SKIN BTW STA 626 TO STA 690 AND BTW
- [SDR DALA2021110606827](https://openairdocs.org/sdr/DALA2021110606827.md): None · none · Oct 29, 2021 · N946AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > ACCOMPLISH VA 84027 MA AD IN CONJUNCTION WITH EM WORKCARD 5530-01048-02. ACCOMPLISH VA 84027 MA AD IN CONJUNCTION WITH EM WORKCARD 5530-01048-02. ASSOCIATED AA 5530-01048 ADDED FOR AC 9506. SUMMARY OF NRC 00224: VA 84027 MA AD WAS ACCOMPLISHED IN CONJUNTION WI
- [SDR DALA2021102606618](https://openairdocs.org/sdr/DALA2021102606618.md): None · none · Oct 26, 2021 · N946AT · Boeing 717200 · Ailerons
  > ELONGATED HOLE WAS FOUND ON RIB STA XA 390 (INBOARD SIDE) OF LEFT HAND WING AILERON STRUCTURE. SUMMARY OF NRC 00027: RIB STA XA 390 (INBOARD SIDE) OF LEFT HAND WING AILERON STRUCTURE WAS REPAIRED PER B717 SRM 57-00-00-2R. (LP #1996324)
- [SDR DALA2021051702719](https://openairdocs.org/sdr/DALA2021051702719.md): Battery Pack · inoperative · May 15, 2021 · N946AT · Boeing 717200 · Emergency Lighting
  > THE AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE ON ARRIVAL. MAINTENANCE REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK PER B717 AMM 3-51. (LP #7298548)
- [SDR DALA2021021000771](https://openairdocs.org/sdr/DALA2021021000771.md): Sign · detached · Feb 9, 2021 · N946AT · Boeing 717200 · Emergency Lighting
  > THE EXIT ROW SIGN ON THE AIRCRAFT LEFT IS DETACHED. MAINTENANCE REATTACHED THE SIGN. OPERATIONAL CHECK IS GOOD. (LP #7581138)
- [SDR DALA2021011100138](https://openairdocs.org/sdr/DALA2021011100138.md): Battery Pack · inoperative · Jan 11, 2021 · N946AT · Boeing 717200 · Emergency Lighting
  > THE INTERIOR OVERWING EXIT DOORS, AFT BOTTOM POSITION ON LEFT AND RIGHT SIDES, EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK BS-119, PER B717 AMM 33-51.
- [SDR DALA201910216015](https://openairdocs.org/sdr/DALA201910216015.md): Sign · broken · Oct 20, 2019 · N946AT · Boeing 717200 · Emergency Lighting
  > BROKEN ON OVER WING EMERGENCY EXIT SIGN (2 EA) (CPAX). SUMMARY OF NRC 00544: OVER WING EMERGENCY EXIT SIGNS (2 EA) P/N: BR9051-001 WERE REPLACED PER B717-200 AMM 33-51-05. (LP1323338)
- [SDR DALA2019101805973](https://openairdocs.org/sdr/DALA2019101805973.md): Frame · cracked · Oct 17, 2019 · N946AT · Boeing 717200 · Fuselage Main, Frame
  > INITIAL INSPECTION: CRACK ON CANTED FRAME STA Y=1225 7:00 O'CLOCK POSITION AT AFT ACCESSORY COMPARTMENT. CANTED FRAME STA Y=1225 7:00 O'CLOCK POSITION AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER ER/A 581847-14TR REV.ORIGINAL (SECTION I: PERMANENT REPAIR) AND
- [SDR DALA2019101705944](https://openairdocs.org/sdr/DALA2019101705944.md): Pan · cracked · Oct 16, 2019 · N946AT · Boeing 717200 · Cargo/Baggage Doors
  > INITIAL INSPECTION: CRACK ON PAN OF FWD CARGO DOOR INTERNAL STRUCTURE. SUMMARY OF NRC 00184 PAN OF FWD CARGO DOOR INTERNAL STRUCTURE WAS REPAIRED PER ETI -17-19-180 REV 6 AND ERA 582177-14 REV ORIGINAL SECTION I PERMANENT REPAIR. (LP1318513)
- [SDR DALA2019101705943](https://openairdocs.org/sdr/DALA2019101705943.md): Door Frame · cracked · Oct 16, 2019 · N946AT · Boeing 717200 · Fuselage Main, Structure
  > HIDDEN DAMAGED: IN REF NRC= 00103: CRACK ON LOWER DOOR JAMB BTW STA 994 STRINGERS 26 AND 27LH OF AFT CARGO COMPARTMENT. SUMMARY OF NRC 00639: LOWER DOOR JAMB BTW STA 994 STRINGERS 26 AND 27LH OF AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 582240- 14 REV.ORIGIN
- [SDR DALA2019101605930](https://openairdocs.org/sdr/DALA2019101605930.md): Cusp Web · canning · Oct 16, 2019 · N946AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: OIL CAN ON CUSP WEB BTW STA= 430 AND STA=445 LH SIDE CABIN PAX. SUMMARY OF NRC 00502: CUSP WEB BTW STA= 430 AND STA= 445 LH SIDE CABIN PAX WAS REPLACED PER B717-200 SRM 53-00-55-2R-4, SRM 51- 41-02-0G AND 51-41-05-0G. (LP1317341)
- [SDR DALA2019101505901](https://openairdocs.org/sdr/DALA2019101505901.md): Access Panel · corroded · Oct 15, 2019 · N946AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL STRUCTURE OF WATER WASTE ACCESS PANEL. WATER WASTE PANEL WAS REPLACED IAW SRM 51-41-02-0G AND SRM 51-41-05-0G AND DWG 5965767 REV. J.
- [SDR DALA2019101505900](https://openairdocs.org/sdr/DALA2019101505900.md): Frame · corroded · Oct 15, 2019 · N946AT · Boeing 717200 · Fuselage Main, Frame
  > FRAME CORRODED OUT OF LIMITS, BS 1022, LONGERON 27L TO 27R. THE FRAME 2 WAS REPAIRED PER SRM 53-20-07-2R-3.
- [SDR DALA2019101405887](https://openairdocs.org/sdr/DALA2019101405887.md): Longeron · corroded · Oct 14, 2019 · N946AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION LONGERON AT L=30 BTW Y=908/1037 AFT CARGO COMPARTMENT. (CORROSION LEVEL 2) LONGERON WAS REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 53-00-05-2R-2 REPAIR 2 FIGURE 201. (LP1314196)
- [SDR DALA2019101405888](https://openairdocs.org/sdr/DALA2019101405888.md): Wire · broken · Oct 13, 2019 · N946AT · Boeing 717200 · Aerodynamic Fairings
  > BROKEN WIRES ON LOCKING CABLE AT TAIL CONE EMERGENCY RELEASE SYSTEM STA Y=1225 CANT. CABLE AT TAIL CONE EMERGENCY RELEASE SYSTEM STA Y=1225 WAS REPLACED PER B717-200 AMM 20-00-02 AND WAS ADJUSTED PER B717-200 AMM 53-52-01-830-802.
- [SDR DALA2019101405886](https://openairdocs.org/sdr/DALA2019101405886.md): Door Frame · corroded · Oct 13, 2019 · N946AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON LOWER DOOR JAMB OF AFT COMPARTMENT CARGO. (CORROSION LEVEL 2) LOWER DOOR JAMB WAS REPLACED PER B717-200 SRM 53-20-15-2R-7 PROCEDURE 7 AND B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP1313860)
- [SDR DALA2019101205869](https://openairdocs.org/sdr/DALA2019101205869.md): Door Frame · cracked · Oct 12, 2019 · N946AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON FWD DOOR JAMB OF RH MLG. FWD DOOR JAMB OF RH MLG WAS REPAIRED PER ETI-17-19-186 REV. 2 AND ER/A 582048-14 REV. ORIGINAL. SECTION I: PERMANENT REPAIR.

Next page: https://openairdocs.org/aircraft/N946AT/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 = 'N946AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N946AT/reports

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