# Service difficulty reports: N994AT

A list on [N994AT](https://openairdocs.org/aircraft/N994AT.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 · 192 reports

- [SDR DALA2026092105262](https://openairdocs.org/sdr/DALA2026092105262.md): Annunciator · inoperative · Sep 21, 2026 · N994AT · Boeing 717200 · Door Warning System
  > R1 DOOR WARNING ANNUNCIATION INOP. T/S PER B717 FRMFIM 52-70-00-810-809, PERFORMED PSEU BITE TEST, TEST PASSED, NO DEFECTS NOTED. PSEU SENSOR READOUT OK. (1823746) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026082604840](https://openairdocs.org/sdr/DALA2026082604840.md): Skin · cracked · Aug 26, 2026 · N994AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKED ON EXTERNAL FUSELAGE SKIN ON BS 1086 BTW LONG 13L AND 14L, COMPLIED WITH ER/A 636457-14. (1777167) (AIRCRAFT GROUNDED).
- [SDR DALA2026082604839](https://openairdocs.org/sdr/DALA2026082604839.md): Skin · cracked · Aug 26, 2026 · N994AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS ON EXTERNAL FUSELAGE SKIN ON BS 1076 BTW LONG 13L AND 14L, COMPLIED WITH ER/A 636463-14. (1777154) (AIRCRAFT GROUNDED).
- [SDR DALA2026082604842](https://openairdocs.org/sdr/DALA2026082604842.md): Skin · cracked · Aug 25, 2026 · N994AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS WERE FOUND AFFECTING THE FUSELAGE SKIN AT APPROXIMATELY BS 1087.060, BTW LONGERONS 13 & 14, COMPLIED WITH ER/A 636457-14. (1776557) (AIRCRAFT GROUNDED).
- [SDR DALA2026082604841](https://openairdocs.org/sdr/DALA2026082604841.md): Skin · cracked · Aug 25, 2026 · N994AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS WERE FOUND AFFECTING THE FUSELAGE SKIN AT APPROX BS 1076, BTW LONGERONS 13L & 14L, COMPLIED WITH ER/A 636463-14. (1776432) (AIRCRAFT GROUNDED).
- [SDR DALA2026082404792](https://openairdocs.org/sdr/DALA2026082404792.md): Skin · cracked · Aug 23, 2026 · N994AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL FUSELAGE SKIN STA Y= 1037 BTW LONG 13L AND 14L, COMPLIED WITH ER/A 636303-14. (1773110) (AIRCRAFT GROUNDED).
- [SDR DALA2026082404790](https://openairdocs.org/sdr/DALA2026082404790.md): Lanyard · torn · Aug 23, 2026 · N994AT · Boeing 717200 · Emergency Equipment
  > TORN LANYARD OF R1 DOOR EMERGENCY SLIDE. R & R LANYARD OF R1 DOOR EMERGENCY SLIDE IAW AIPC 25-61- 03-01. (1771710) (AIRCRAFT GROUNDED).
- [SDR DALA2026082404794](https://openairdocs.org/sdr/DALA2026082404794.md): Skin · cracked · Aug 21, 2026 · N994AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS WERE FOUND AFFECTING THE FUSELAGE SKIN AT BS Y=1037, BETWEEN THE L-13L AND L-14L, COMPLIED WITH ER/A 636303-14. (1772642) (AIRCRAFT GROUNDED).
- [SDR DALA2026082404789](https://openairdocs.org/sdr/DALA2026082404789.md): Door Frame · cracked · Aug 21, 2026 · N994AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON LOWER JAMB AT Y=391 APPROX. ON FWD CARGO DOOR CUTOUT, R & R LOWER JAMB IAW SRM 51-41-02-0G AND SRM 51-41-05-0G. (1769464) (AIRCRAFT GROUNDED).
- [SDR DALA2026082104769](https://openairdocs.org/sdr/DALA2026082104769.md): Frame · cracked · Aug 20, 2026 · N994AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON CAP STA Y=1178 CANT AND LONG 17L AT AFT FUSELAGE COMPARTMENT, COMPLIED WITH ER/A 636312-14. (1767796) (AIRCRAFT GROUNDED).
- [SDR DALA2026082004758](https://openairdocs.org/sdr/DALA2026082004758.md): Channel · cracked · Aug 20, 2026 · N994AT · Boeing 717200 · Landing Gear Doors
  > CRACKED CORNER OF AFT ZEE CHANNELS Y=799, -X=10.5 AT THE RT MLG INBD DOOR, COMPLIED WITH ER/A 619191-14TR. (1766358) (AIRCRAFT GROUNDED).
- [SDR DALA2026082004756](https://openairdocs.org/sdr/DALA2026082004756.md): Scuff Plate · corroded · Aug 19, 2026 · N994AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FOUND CORROSION LVL 2 ON ANGLE (2EAS) AT FWD CARGO SCUFF PLATE, R & R THE SCUFF PLATE IAW SRM 53-20- 15-2R. (1765931) (AIRCRAFT GROUNDED).
- [SDR DALA2026081704699](https://openairdocs.org/sdr/DALA2026081704699.md): Ferrule · cracked · Aug 16, 2026 · N994AT · Boeing 717200 · Fuselage Floor Panel
  > CRACK AND MISSING FERRULES ON CARGO COMPARTMENT FLOOR PANEL, COMPLIED WITH ER/A 591778-14TR. (1759040) (AIRCRAFT GROUNDED).
- [SDR DALA2026081704698](https://openairdocs.org/sdr/DALA2026081704698.md): Floor Panel · cracked · Aug 16, 2026 · N994AT · Boeing 717200 · Fuselage Floor Panel
  > CRACKED FLOOR PANEL 121RF ON FWD CARGO COMPARTMENT, CORRECTIVE ACTION: COMPLIED WITH ER/A 00-591778. (1759039) (AIRCRAFT GROUNDED).
- [SDR DALA2026081704696](https://openairdocs.org/sdr/DALA2026081704696.md): Vane · debonded · Aug 16, 2026 · N994AT · Boeing 717200 · Trailing Edge Flaps
  > DISBOND WAS FOUND OF 6.500IN X 3.500IN (LENGTH / WIDTH) ON RT FWD MOVABLE FLAP VANE AT 20IN OF IB AND 5IN TE, RT FWD MOVABLE FLAP VANE WAS REPAIRED IAW SRM 51-70-02-0G AND SRM 57-53-01-2R-1. (1760027) (AIRCRAFT GROUNDED).
- [SDR DALA2025092406976](https://openairdocs.org/sdr/DALA2025092406976.md): Limiter · damaged · Sep 23, 2025 · N994AT · Boeing 717200 · Wing Structure
  > ON WAKEUP FOUND SPEED TAPE ON RH VORTILON. DAMAGE WITHIN LIMITER PER EAA 570743-14MA REV B APPLIED TEMP REPAIR. WILL NEED PERMINENT REPAIR WITHIN 100 FLIGHT HOURS.(7372557)
- [SDR DALA2024112611222](https://openairdocs.org/sdr/DALA2024112611222.md): Pan · cracked · Nov 22, 2024 · N994AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON FWD INNER PAN BTW STA 954 BEAM 3 APPROX AT AFT CARGO DOOR. SUMMARY OF NRC 00086: AFT CARGO DOOR WAS REPLACED WITH A SERVICEABLE AFT CARGO DOOR AND PART NUMBER WAS VERIFIED PER B717-200 AIPC 52-33-01-01 ITEM 130J AND IS INSTALLED UNDER AMDS 5231-4004.
- [SDR DALA2024112211134](https://openairdocs.org/sdr/DALA2024112211134.md): Pan · cracked · Nov 22, 2024 · N994AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INNER PAN FWD EDGE IN BEAM #5 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00325: INNER PAN FWD EDGE IN BEAM #5 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA 621747-14, REV ORIGINAL. ASSOCIATED ER/A 14-621747 ADDED FOR AC 9539. (LP #0671941)
- [SDR DALA2024111911024](https://openairdocs.org/sdr/DALA2024111911024.md): Skin · cracked · Nov 15, 2024 · N994AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUS SKIN BTW STA 1037 AND 1053 LONGERON 15R. SUMMARY OF NRC 0053: FUS SKIN BTW STA 1037 AND 1053 LONGERON 15R WAS REPAIRED PER ER/A 621624-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. MAINTENANCE REQUIREMENTS WERE VERIFIED AND THE FOLLOWING ACTIONS AR
- [SDR DALA2024111210889](https://openairdocs.org/sdr/DALA2024111210889.md): Door Frame · corroded · Nov 12, 2024 · N994AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON DOOR JAM BTW STA Y-954 TO 994 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00076: CORROSION LEVEL 2. CORROSION ON DOOR JAM BTW STA Y-954 TO 994 AT AFT CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROC 7 REPAIR 7. (LP #0655665)
- [SDR DALA2024111210886](https://openairdocs.org/sdr/DALA2024111210886.md): Vane · dented · Nov 11, 2024 · N994AT · Boeing 717200 · Trailing Edge Flaps
  > DENTS: 2, 3, 4, 5, AND 6 BTW XF89 AND XF95 (10 TO 13.5 INCHES FROM T.E.) ON RH AFT MOVABLE FLAP VANE WERE FOUND OUT OF LIMITS BY DISTANCE BTWN OTHER DAMAGES. SUMMARY OF NRC 00628: DENTS: 2, 3, 4, 5, AND 6 BTW XF89 AND XF95 (10 TO 13.5 INCHES FROM T.E.) ON RH A
- [SDR DALA2024111110805](https://openairdocs.org/sdr/DALA2024111110805.md): Access Panel · corroded · Nov 10, 2024 · N994AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON ACCESS PANEL 5971074 -1 BTW STA Y=636 TO STA Y=655 L29L TO L29R AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00616: CORROSION LEVEL 2. ACCESS PANEL 5971074-1 BTW STA Y=636 TO STA Y=655 L29L TO L29R AT FWD CARGO COMPARTMENT WAS REPLACED PER B717-200 SR
- [SDR DALA2024111110804](https://openairdocs.org/sdr/DALA2024111110804.md): Doubler · corroded · Nov 10, 2024 · N994AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND ON DOUBLER AT E/E COMPARTMENT ON INTERNAL FUSELAGE SKIN PANEL STA Y=215 TO STA Y=221 BTW LONGERON 28R AND 29R. SUMMARY OF NRC 00626: CORROSION LEVEL 2. DOUBLER ON INTERNAL FUSELAGE SKIN PANEL STA Y=215 TO STA Y=221 BTW LONGERON 28R AND 29R
- [SDR DALA2024111110803](https://openairdocs.org/sdr/DALA2024111110803.md): Vane · dented · Nov 9, 2024 · N994AT · Boeing 717200 · Trailing Edge Flaps
  > DENTS OUT OF LIMITS: 8, 12, 19, 22, AND 24 BTW STA XF95 AND XF103 (4 TO 7 INCHES FROM T.E.) ON UPPER SURFACE AT LH AFT MOVABLE VANE AT LH WING. SUMMARY OF NRC 00618: IN REFERENCE TO NRC 00501 DENTS OUT OF LIMITS: 8, 12, 19, 22, AND 24 BTW STA XF95 AND XF103 (4
- [SDR DALA2024111110802](https://openairdocs.org/sdr/DALA2024111110802.md): Vane · dented · Nov 9, 2024 · N994AT · Boeing 717200 · Trailing Edge Flaps
  > DENT #1 (1EA) OUT OF LIMITS UPPER SURFACE RH FWD MOVEABLE FLAP VANE. DISTANCE TO AFT EDGE 6.650, DISTANCE OF OUTER EDGE 34.900 RH WING. SUMMARY OF NRC 00620: ON REF NRC 00503 DENT #1 (1EA) OUT OF LIMITS UPPER SURFACE RH FWD MOVEABLE FLAP VANE DISTANCE TO AFT E
- [SDR DALA2024110810727](https://openairdocs.org/sdr/DALA2024110810727.md): Skin · gouged · Nov 8, 2024 · N994AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > GOUGE ON EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE. SUMMARY OF NRC 00092: EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE WAS REPAIRED PER B717-200 SRM 53-03-01-2R PROCEDURE 1, REPAIR 1 PAR 6.A. FIG 202. PERFORM A VISUAL INSPECTION EVERY
- [SDR DALA2024110410591](https://openairdocs.org/sdr/DALA2024110410591.md): Hinge · worn · Nov 4, 2024 · N994AT · Boeing 717200 · Passenger Compartment Equipment
  > WEAR ON DOBLER AND FLIGHT ATTENDANT SEAT HINGES OF AFT CABIN BULKHEAD VENTRAL DOOR. AND WEAR ON UPPER / LWR SIDE FITTING (7 EA) 0F AFT CABIN BULKHEAD VENTRAL DOOR. SUMMARY OF NRC-00452: UPPER / LWR SIDE FITTINGS (7 EA) AND FLIGHT ATTENDANT SEAT HINGES WERE BLE
- [SDR DALA2024110410590](https://openairdocs.org/sdr/DALA2024110410590.md): Skin · gouged · Nov 3, 2024 · N994AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > GOUGE ON EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE. SUMMARY OF NRC 00092: EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE WAS REPAIRED PER B717-200 SRM 53-03-01-2R PROCEDURE 1, REPAIR 1 PAR 6.A, FIG 202. (LP #0642594)
- [SDR DALA2024110410589](https://openairdocs.org/sdr/DALA2024110410589.md): Frame · cracked · Nov 1, 2024 · N994AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON MAIN FRAME BTW STA Y=1037 AND L17L AT AFT CABIN PASSENGER. SUMMARY OF NRC 00433: MAIN FRAME BTW STA Y=1037 AND L17L AT AFT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0639803)
- [SDR DALA2024110110567](https://openairdocs.org/sdr/DALA2024110110567.md): Web · cracked · Oct 31, 2024 · N994AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON WEB BTW STA Y=674 AND -X=45 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00380: WEB BTW STA Y=674 AND -X=45 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. FIGURE 217. -PERFORM DECAL INSPECTION CONDITION EVERY "C" C
- [SDR DALA2024110110566](https://openairdocs.org/sdr/DALA2024110110566.md): Longeron · cracked · Oct 31, 2024 · N994AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON BTW STA Y=1022 AND L6L AT AFT CABIN PASSENGER. SUMMARY OF NRC 00434: LONGERON BTW STA Y=1022 AND L6L AT AFT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0637160)
- [SDR DALA2024103110527](https://openairdocs.org/sdr/DALA2024103110527.md): Pan · cracked · Oct 30, 2024 · N994AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK WAS FOUND ON INNER PAN AFT EDGE BTW BEAM 1 AND BEAM 2 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00486: INNER PAN AFT EDGE BTW BEAM 1 AND BEAM 2 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 8. (LP #0636755)
- [SDR DALA2024103110526](https://openairdocs.org/sdr/DALA2024103110526.md): Skin · cracked · Oct 30, 2024 · N994AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON SKIN ON CUTOUT OF RH SLIDING WINDOW AT COCKPIT (UPPER AFT CORNER). SUMMARY OF NRC 00355: SKIN ON CUTOUT OF RH SLIDING WINDOW AT COCKPIT (UPPER AFT CORNER) WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1 PAR 5 FIGURE 201. (LP #0636659)
- [SDR DALA2024103010504](https://openairdocs.org/sdr/DALA2024103010504.md): Web · cracked · Oct 29, 2024 · N994AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED WEB BTW STA Y=696 AND X=45 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00432: WEB BTW STA Y=696 AND X=45 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 FIGURE 204. PERFORM A GENERAL VISUAL INSPECTION EVERY C-CHECK P
- [SDR DALA2024103010503](https://openairdocs.org/sdr/DALA2024103010503.md): Beam · cracked · Oct 29, 2024 · N994AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON BEAM #1 AFT SECTION AT FWD PASSENGER DOOR. SUMMARY OF NRC 00266: BEAM #1 AFT SECTION AT FWD PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0634844)
- [SDR DALA2024103010499](https://openairdocs.org/sdr/DALA2024103010499.md): Web · cracked · Oct 25, 2024 · N994AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON WEB BTW STA Y=674 AND X=45 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00378: WEB BTW STA Y=674 AND X=45 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55 2R PROCEDURE 4, REPAIR 4, FIGURE 217. (LP #0627536)
- [SDR DALA2024031203222](https://openairdocs.org/sdr/DALA2024031203222.md): Intercostal · cracked · Mar 8, 2024 · N994AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL LH STA Y=1224 CANT 12 O'CLOCK AT AFT ACCESORY COMPARMENT. SUMMARY OF NRC 00078: INTERCOSTAL LH STA Y=1224 CANT 12 O'CLOCK AT AFT ACCESSORY COMPARMENT WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G. SPRING ON RUDDER STOP ASSEMBLY WAS
- [SDR DALA2024030503008](https://openairdocs.org/sdr/DALA2024030503008.md): Frame · cracked · Mar 5, 2024 · N994AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON CLIP FRAME STA 1116 BTW LONG 15RH AND 16 RH AT AFT ACCESSORY COMPARMENT. SUMMARY OF NRC 00087: CLIP FRAME STA 1116 BTW LONG 15RH AND 16 RH AT AFT ACCESSORY COMPARTMENT WAS REPLACED PER B717 SRM 51-41-05-0G. (LP #0230455)
- [SDR DALA2024030503007](https://openairdocs.org/sdr/DALA2024030503007.md): Frame · cracked · Mar 5, 2024 · N994AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON CLIP FRAME STA 1116 BTW LONG 15LH AND 16LH AT AFT ACCESSORY COMPARMENT. SUMMARY OF NRC 00084: CLIP FRAME STA 1116 BTW LONG 15LH AND 16LH AT AFT ACCESSORY COMPARTMENT WAS REPLACED PER B717 SRM 51- 41-05-0G. (LP #0230453)
- [SDR DALA2023120810062](https://openairdocs.org/sdr/DALA2023120810062.md): Unknown · unknown · Dec 7, 2023 · N994AT · Boeing 717200 · Passenger/Crew Doors
  > RAMP REPORTS DENT ON LOWER LEFT CORNER OF L1 DOOR OUTER SKIN. INSPECTED IAW B717 SRM 53-01-01-1A PROC 3, DENT MEASURES 2 X 0.125 X 0.342. DENT IS OUT OF LIMITS IAW SRM. PERFORMED PRESSUIZATION OF A/C PER B717 AMM 21-30, FOUND LEAK OUT OF DAMAGE LOCATION. INSPE
- [SDR DALA2023090507199](https://openairdocs.org/sdr/DALA2023090507199.md): Unknown · unknown · Sep 4, 2023 · N994AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT JUST AFT OF GALLEY. MAINTENANCE INSTALLED THE EMERGENCY EXIT SIGN COVER BETWEEN ROW 1 SEATS REF B717 AIPC 33-51-18-05. LIGHTS CHECK GOOD. (LP #2952421)
- [SDR DALA2023022201328](https://openairdocs.org/sdr/DALA2023022201328.md): None · none · Dec 2, 2022 · N994AT · Boeing 717200 · Wing, Plate/Skin
  > PDA. LH WING SKIN ASSY STA XFS 70.812-196.236 MISSING. FWD TO MON PER ER/A 604219-14 REV ORIGINAL. C/W SECTION 1. PERMANENT REPAIR TO BE ACCOMPLISHED IN 90 DAYS. C/W PERMANENT REPAIR ON ERA 604219-14 REV. ORIGINAL. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT
- [SDR DALA2022021500948](https://openairdocs.org/sdr/DALA2022021500948.md): None · none · Feb 11, 2022 · N994AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > LH VERTICAL STAB LE, CRACK INDICATION IN 4TH HOLE UP FROM SLICE AT STA ZFS 52.267. FOUND DURING OPEN HOLE INSPECTION REF AMDS 5530-01048-02-ET STEP 8 AND AD 2018-10-08. -M-. SUMMARY SEE NRC 069-0001:5530-01048-02/002 00420: REPAIRED PER PRI 597048-14 REV 0 THR
- [SDR DALA2022021500947](https://openairdocs.org/sdr/DALA2022021500947.md): None · none · Feb 9, 2022 · N994AT · Boeing 717200 · Aerodynamic Fairings
  > TAILCONE EMERGENCY RELEASE; LEFT LOWER LATCH LEVER CABLE IS FRAYED AT UPPER PULLY AREA. -M- SUMMARY SEE NRC 001-0317:5353-2001/001 00453: REPLACED, RIGGED, AND SAFETIED CABLE REF B717 AMM 53-52-01. OPERATIONALS CHECK WAS GOOD. (LP #2115930)
- [SDR DALA2022021500946](https://openairdocs.org/sdr/DALA2022021500946.md): None · none · Feb 9, 2022 · N994AT · Boeing 717200 · Aerodynamic Fairings
  > TAILCONE R/H SIDE LATCH LEVER REQUIRES RIG ADJUSTMENT TO TOP OF SLOT PER B717 AMM 53-52-01 830-802 STEP E.1.AG. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0138:5352-4002/002
- [SDR DALA2019091205278](https://openairdocs.org/sdr/DALA2019091205278.md): Door Frame · corroded · Sep 11, 2019 · N994AT · Boeing 717200 · Fuselage Main, Structure
  > AFT CARGO LOWER DOOR JAMB CORRODED (MARKED). NRC 001-0302:5231-2002/001 00013: REPAIRED REF SRM 53-20-15-2R PROC 7. (LP #1266353)
- [SDR DALA2018112706854](https://openairdocs.org/sdr/DALA2018112706854.md): Transceiver · malfunctioned · Nov 26, 2018 · N994AT · Boeing 717200 · Wind Shear Detection System
  > SHIP 9539 - ATO - AT 105 KNOTS DUE TO PREDICTIVE WINDSHEAR WARNING AT 95-100KNOTS. SUSPECT A FALSE WARNING AS OTHER DEPARTURES AND ARRIVALS REPORTED GOOD FLIGHT CONDITIONS WITHOUT WINDSHEAR. CORRECTIVE ACTION: TROUBLESHOT PER FIM. REPLACED WEATHER RADAR TRANSC
- [SDR DALA2018111906671](https://openairdocs.org/sdr/DALA2018111906671.md): Battery Pack · inoperative · Nov 19, 2018 · N994AT · Boeing 717200 · Emergency Lighting
  > DURING THE SERVICE CHECK, MAINTENANCE FOUND THE AFT LEFT LOWER EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY FOR THE AFT LEFT LOWER EMERGENCY EXIT SIGN PER B717 AMM 33-55. (LP #5088722)
- [SDR DALA2017111508130](https://openairdocs.org/sdr/DALA2017111508130.md): Longeron · cracked · Nov 14, 2017 · N994AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 16L, BS 1022. THE LONGERON WAS REPAIRED IAW ER/A 562376-14, REV ORIGINAL, AND ETI-17-17-223, REV 3.
- [SDR DALA2017111408092](https://openairdocs.org/sdr/DALA2017111408092.md): Angle · corroded · Nov 14, 2017 · N994AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RT CUSP ANGLE BELOW OF R1 DOOR JAMB BTW Y=168-207 AT PAX CABIN. CORROSION LEVEL 2. RT CUSP ANGLE BELOW OF R1 DOOR JAMB BTW Y=168-207 AT PAX CABIN WAS REPAIRED (PERMANENT REPAIR) PER ER/A 562367-14 REV ORIGINAL AND ETI-17-17-214 REV 3.

Next page: https://openairdocs.org/aircraft/N994AT/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 = 'N994AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N994AT/reports

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