# Service difficulty reports: N603AT

A list on [N603AT](https://openairdocs.org/aircraft/N603AT.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 · 223 reports

- [SDR DALA2026093005423](https://openairdocs.org/sdr/DALA2026093005423.md): Skin · damaged · Sep 26, 2026 · N603AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND DAMAGE AFT OF AFT CARGO DOOR OPENING, COMPLIED WITH ER/A 637189-14. (9197562) (AIRCRAFT GROUNDED).
- [SDR DALA2026071304128](https://openairdocs.org/sdr/DALA2026071304128.md): Tail Cone · damaged · Jul 10, 2026 · N603AT · Boeing 717200 · Aerodynamic Fairings
  > TAIL CONE HAS MULTIPLE LIGHTNING STRIKES BEYOND ALLOWABLE LIMITS. REPLACED TAIL CONE IAW AMDS W/C 5352-4013. (9204003) (AIRCRAFT GROUNDED)
- [SDR DALA2026052103104](https://openairdocs.org/sdr/DALA2026052103104.md): Control Valve · faulted · May 18, 2026 · N603AT · Boeing 717200 · Trailing Edge Flap Control System
  > UFC/DE- TRAILING EDGE FLAPS LOCKED OUT ON APPROACH. LEADING EDGE SLATS EXTENDED NORMALLY. FOUND FLAP CONTROL VALVE CONTROL ROD BOLT BROKEN/MISSING. REPLACED SAME. OPS CHECK GOOD. (8360108) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402371](https://openairdocs.org/sdr/DALA2026041402371.md): None · none · Apr 9, 2026 · N603AT · Boeing 717200 · Standard Practices/Structures
  > DURING ACCOMPLISHMENT OF ERA 633150-14AD PRI REV 0 STEP 15 FOUND 7 EA UNINSPECTABLE HOLES IN UPPER MLG SUPPORT DOUBLER AND TE PANEL LE. HOLES ARE NUMBERED UNK 1-7. COMPLIED WITH ERA 633274-14 (1536155) (AIRCRAFT GROUNDED)
- [SDR DALA2025092907058](https://openairdocs.org/sdr/DALA2025092907058.md): Spar · cracked · Sep 24, 2025 · N603AT · Boeing 717200 · Wing Spar
  > WHILE PERFORMING AMDS 5720-01103-01B. INSPECTION FOUND A CRACK AT APPROX STA XRS= 170REAR SPAR. COMPLIED WITH ER/A- 628659-14AD REV. ORIGINAL (1215975)
- [SDR DALA2025110708140](https://openairdocs.org/sdr/DALA2025110708140.md): None · none · Sep 23, 2025 · N603AT · Boeing 717200 · Standard Practices/Structures
  > SHIP 9594 ER/A 628659-14AD REV ORIGINAL REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. CORRECTIVE ACTION: COMPLIED WITH ERA 628659-14AD REV ORIGINAL REP INSPECTION II. (1215579)
- [SDR DALA2025081806161](https://openairdocs.org/sdr/DALA2025081806161.md): Repair · out of position · Aug 14, 2025 · N603AT · Boeing 717200 · Wing, Plate/Skin
  > EXISTING REPAIR FOUND THAT IMPACTS INSPECTION ACCOMPLISHMENT. REPAIR INVESTIGATION REQUIRED PRIOR TO FURTHER FLIGHT. FOUND AT RT WING REAR SPAR INSPECTION AREA DURING ACCOMPLISHMENT OF AA EM 5720-01103. REPAIR PER ER/A 624368-14AD (1143045)
- [SDR DALA2025081806160](https://openairdocs.org/sdr/DALA2025081806160.md): Structure · chafed · Aug 14, 2025 · N603AT · Boeing 717200 · Wing Main, Frame Structure
  > NUMBER 2 LT SLAT ATTACH POINT INSPECTION, SLAT DRIVE TRACK NR 5 CHAFED WING STRUCTURE ON INBD AT EDGE. REPAIRED ERA 628327-14 REV. (1143308)
- [SDR DALA2025031301960](https://openairdocs.org/sdr/DALA2025031301960.md): Skin · corroded · Mar 12, 2025 · N603AT · Boeing 717200 · Wing, Plate/Skin
  > -AD- CORROSION FOUND DURING INSPECTION OF RH WING AFT LOWER SKIN. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT PER INSPECTION FC5720-01103. SUMMARY SEE NRC 004-0001:5720-01103- 01B/001 00001: COMPLIED WITH PRI 624368-14AD REV 0, PR
- [SDR DALA2025100807322](https://openairdocs.org/sdr/DALA2025100807322.md): Skin · corroded · Mar 10, 2025 · N603AT · Boeing 717200 · Trailing Edge Flaps
  > EXFOLIATING CORROSION FOUND ON RIGHT WING REAR SPAR LOWER CAP AT APPROXIMATELY STATION XRS=164. (6925752)
- [SDR DALA2025031101893](https://openairdocs.org/sdr/DALA2025031101893.md): Hinge Fitting · corroded · Mar 9, 2025 · N603AT · Boeing 717200 · Trailing Edge Flaps
  > RIGHT WING INBOARD FLAP HINGE FITTING LOWER OUTBOARD STUD ON AFT SPAR HAS HEAVY RUST/PITTING. SUMMARY SEE NRC 004-0001:5720-01103-01B/006 00006: CORROSION LEVEL 2. REPLACED 4 EA MOUNTING STUDS PER B717 AMM 57-55-25-300-801. (LP #0849083)
- [SDR DALA2025010700131](https://openairdocs.org/sdr/DALA2025010700131.md): Power Supply · no test · Jan 5, 2025 · N603AT · Boeing 717200 · Emergency Lighting
  > THE AFT EMERGENCY EXIT DOORS OVERWING LIGHTS, LT AND RT, ARE NOT COMING ON WHEN TESTED AT ROW 20. MAINTENANCE REPLACED THE B5-119 EMERGENCY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6967194)
- [SDR DALA2024071807234](https://openairdocs.org/sdr/DALA2024071807234.md): Light · malfunctioned · Jul 17, 2024 · N603AT · Boeing 717200 · Emergency Lighting
  > EXTERIOR EMERGENCY ILLUMINATION SYSTEM LEFT AFT WING EXTERIOR EMERGENCY LIGHT STAYING ON. LEFT WING EMERGENCY ILLUMINATION WAS FOUND ON DURING PRE-FLIGHT. RELAMEPED WING EMERGENCY LIGHT. REPLACED EMERGENCY LIGHT BATTERY PACK & RELAY PER B717 33-50 (B5-125 & R2
- [SDR DALA2024032103580](https://openairdocs.org/sdr/DALA2024032103580.md): Battery Pack · inoperative · Mar 17, 2024 · N603AT · Boeing 717200 · Emergency Lighting
  > FOUND LEFT AND RIGHT AFT EMERGENCY EXIT DOOR LOCATOR SIGNS INOPERATIVE AT THE AFT OVERWING DOORS. MAINTENANCE REPLACED THE EMERGENCY BATTERY (B5-115) POWER SUPPLY PER B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #5333890)
- [SDR DALA2024010300074](https://openairdocs.org/sdr/DALA2024010300074.md): Relay · unknown · Jan 3, 2024 · N603AT · Boeing 717200 · Emergency Lighting
  > THE OVERWING ESCAPE PATH LIGHTING IS ON WITH THE SWITCH IN ARM POSITION. MAINTENANCE FOUND THAT THE OVERWING EMERGENCY LIGHTS REMAINED ILLUMINATED WITH SWITCH IN OFF POSITION TOO. THE RELAY R2-273, WAS REPLACED PER B717 SWPM 20-20. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA2023112009532](https://openairdocs.org/sdr/DALA2023112009532.md): Unknown · unknown · Nov 19, 2023 · N603AT · Boeing 717200 · Emergency Lighting
  > THE EXTERIOR EMERGENCY LIGHTS STAY ON WHEN SWITCH IS PLACED IN "ARM" POSITION. MAINTENANCE RESET THE EMERGENCY LIGHTS SYSTEM. PERFORMED AN OPERATIONAL CHECK IAW FIM B717 33-50 AND THE EEPL SYSTEM TESTED NORMAL. (LP #4996206)
- [SDR DALA2023090507198](https://openairdocs.org/sdr/DALA2023090507198.md): Unknown · unknown · Sep 3, 2023 · N603AT · Boeing 717200 · Emergency Lighting
  > THE OVERWING EXIT EXTERIOR LIGHTS ARE ON WITH THE SWITCH IN ARM POSITION. MAINTENANCE REPLACED THE OVERWING EMERGENCY POWER SUPPLY PER B717 AMM 33-51. ALL OPERATIONAL CHECKS WERE NORMAL. OK FOR SERVICE. (LP #4617678)
- [SDR DALA2023080406301](https://openairdocs.org/sdr/DALA2023080406301.md): Unknown · unknown · Aug 4, 2023 · N603AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON AFT BULKHEAD DOOR JAMB (UPPER AREA) STA Y=1060 PROJECTION LONGERON 1 AT AFT PAX CABIN. SUMMARY OF NRC 00286: AFT BULKHEAD DOOR JAMB (UPPER AREA) STA Y=1060 PROJECTION LONGERON 1 AT AFT PAX CABIN WAS REPAIRED PER ER/A 610327-14 REV ORIGINAL SECTION I:
- [SDR DALA2023080406300](https://openairdocs.org/sdr/DALA2023080406300.md): Unknown · unknown · Aug 3, 2023 · N603AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL SKIN BTW STA 655 TO 658 AND LONG 29LH TO 29RH BILGE AREA AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00611: CORROSION LEVEL 2. CORROSION ON INTERNAL SKIN BTW STA 655 TO 658 AND LONG 29LH TO 29RH BILGE AREA AT FWD CARGO COMPARTMENT WAS REPAIR
- [SDR DALA2023080306284](https://openairdocs.org/sdr/DALA2023080306284.md): Unknown · unknown · Aug 2, 2023 · N603AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL DOUBLER BTW LOWER DOOR JAMB AND EXTERNAL SKIN FROM STA Y 954 TO 994 AT AFT CARGO. IN REF NRC0337. C2. SUMMARY OF NRC 00664: CORROSION LEVEL 2. CORROSION ON INTERNAL DOUBLER BTW LOWER DOOR JAMB AND EXTERNAL SKIN FROM STA Y 954 TO 994 AT AF
- [SDR DALA2023080306282](https://openairdocs.org/sdr/DALA2023080306282.md): Unknown · unknown · Aug 2, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER JAMB PAN INTERNAL AND EXTERNAL STRUCTURE STA 946 TO STA 1002 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00337: DOOR JAMB WAS REPLACED PER B717-200 SRM 51 -41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #2898062)
- [SDR DALA2023080306277](https://openairdocs.org/sdr/DALA2023080306277.md): Unknown · unknown · Aug 2, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS (4 EA) ON STA 466, STA 426, STA 371, AND STA 332 BTW LONG 28RH AND 28LH BILGE AREA AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00317: LEVEL CORROSION 2. FLOOR SUPPORTS (4 EA) ON STA 466, STA 426, STA 371, AND STA 332 BTW LONG 28RH AND
- [SDR DALA2023072806114](https://openairdocs.org/sdr/DALA2023072806114.md): Unknown · unknown · Jul 28, 2023 · N603AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON TIE TRACK LH SIDE STA 813 TO STA 1022 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00306: CORROSION LEVEL 2. TIE TRACK LH SIDE STA 813 TO STA 1022 AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER DWG 5936663, B717-200 SRM 51-40-04-0G AND 51-41-05-0
- [SDR DALA2023072706098](https://openairdocs.org/sdr/DALA2023072706098.md): Unknown · unknown · Jul 27, 2023 · N603AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME STA 870 AND LONGERON L30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00645: CORROSION LEVEL 2. FRAME STA 870 AND LONGERON L30 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. (LP #2886682)
- [SDR DALA2023072606038](https://openairdocs.org/sdr/DALA2023072606038.md): Unknown · unknown · Jul 25, 2023 · N603AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKS (3 EA) ON INTERNAL STRUCTURE BEAM #3 STA 370 AND BEAM #5 STA 370, STA 427 AT FWD CARGO DOOR. SUMMARY OF NRC 00264: CRACKS (3 EA) ON INTERNAL STRUCTURE BEAM #3 STA 370 AND BEAM #5 STA 370, STA 427 AT FWD CARGO DOOR WERE REPAIRED PER B717-200 SRM 52-30-02
- [SDR DALA2023072505982](https://openairdocs.org/sdr/DALA2023072505982.md): Unknown · unknown · Jul 23, 2023 · N603AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON PRODUCTION DOUBLER OF INNER FUSELAGE SKIN DRAIN STA 1007 BTW L30 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00300: CORROSION LEVEL 2. DOUBLER OF INNER FUSELAGE SKIN DRAIN STA 1007 BTW L30 AT AFT CARGO COMPARTMENT (C2) WERE FABRICATED PER DWG 59
- [SDR DALA2023072505980](https://openairdocs.org/sdr/DALA2023072505980.md): Unknown · unknown · Jul 23, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK WAS FOUND ON RH CUSP MEMBRANE WEB BTW STA 579 TO 598 AT PAX CABIN. SUMMARY OF NRC 00630: RH CUSP MEMBRANE WEB BTW STA 579 TO 598 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4, FIG 226, 51-41-02-0G, AND 51-41-05-0G PAR 10. (LP #2880836
- [SDR DALA2023072505979](https://openairdocs.org/sdr/DALA2023072505979.md): Unknown · unknown · Jul 23, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR MEMBRANE WAS FOUND BTW STA Y 813-832 AND X=-44 TO X=-54 AT PAX CABIN. SUMMARY OF NRC 00648: FLOOR MEMBRANE BTW STA Y 813-832 AND X=-44 TO X=-54 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 PAR 5 FIG 221. (LP #2880828)
- [SDR DALA2023072505977](https://openairdocs.org/sdr/DALA2023072505977.md): Unknown · unknown · Jul 21, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT BTW -X 45 FROM STA 157 TO 200 (W1). SUMMARY OF NRC 00643: CORROSION LEVEL 2. FLOOR SUPPORT BTW -X 45 FROM STA 157 TO 200 (W1) WAS REPLACED PER DWG 9936534 REV BW, DWG S2929169, B717-200 SRM 51-41-02-0G, AND 51-41-05-0G. (LP #2877366)
- [SDR DALA2023072505976](https://openairdocs.org/sdr/DALA2023072505976.md): Unknown · unknown · Jul 21, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT (1 EA) BTW X 55 AND STA 200-204.5 WAS MEASURED WITH AN ORIGINAL THICKNESS OF 0.063 IN. MAXIMUM MATERIAL REMOVED IS 0.030 IN AND THEREFORE ALL AREAS REWORKED ARE OUT OF LIMITS PER B717-200 SRM 53-00-00-1A, PROCEDURE ALLOWABLE DAMAGE G
- [SDR DALA2023072105929](https://openairdocs.org/sdr/DALA2023072105929.md): Unknown · unknown · Jul 20, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR FITTING ON AFT BULKHEAD BTW STA Y=1060 AND X=-22 AT AFT PAX CABIN. SUMMARY OF NRC 00374: CORROSION LEVEL 2. FLOOR FITTING ON AFT BULKHEAD BTW STA Y=1060 AND X=-22 WAS REPLACED PER B717 SRM 51-41-05-0G. (LP #2876410)
- [SDR DALA2023072105928](https://openairdocs.org/sdr/DALA2023072105928.md): Unknown · unknown · Jul 20, 2023 · N603AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK, X-44 BTW STA 200-205 AT PAX CABIN. SUMMARY OF NRC 00369: CORROSION LEVEL 2. SEAT TRACK, X-44 BTW STA 200 TO 264 WAS REPLACED PER B717 SRM 51-41-05-0G PAR 8 AND SRM 51-41-01-0G PROCEDURE GENERAL. (LP #2876390)
- [SDR DALA2023072105925](https://openairdocs.org/sdr/DALA2023072105925.md): Unknown · unknown · Jul 20, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON GUSSET WITH NP: 3925389-1 UNDER VENTRAL DOOR STA Y=1065 AND X=18 AT CABIN PAX. SUMMARY OF NRC 00442: CORROSION LEVEL 2. GUSSET WITH NP: 3925389-1 UNDER VENTRAL DOOR STA Y=1065 AND X=18 WAS REPLACED PER B717 SRM 51-41-05-0G. (LP #2875094)
- [SDR DALA2023072105924](https://openairdocs.org/sdr/DALA2023072105924.md): Unknown · unknown · Jul 20, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BTW X=13 TO 38.5 BTW STA Y=180 AT W1 AREA, IS CORRODED OUT OF LIMITS IN CABIN PAX. SUMMARY OF NRC 00638: CORROSION LEVEL 2. FLOOR SUPPORT BTW X=13 TO 38.5 BTW STA Y=180 AT PAX CABIN WAS REPLACED PER B717 SRM 51-41-02-0G PAR 4. (LP #2875085)
- [SDR DALA2023071705783](https://openairdocs.org/sdr/DALA2023071705783.md): Unknown · unknown · Jul 17, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON LH CUSP MEMBRANE WEB (2 EA) BTW STA 655 TO 695 AT CABIN PAX. SUMMARY OF NRC 00356: CRACK ON LH CUSP MEMBRANE WEB (2 EA) BTW STA 655 TO 695 AT CABIN PAX WERE REPAIRED PER B717 SRM-53-00-55-2R-4 REPAIR 4 PAR 5 FIGURE 203 AND 204. (LP #2869967)
- [SDR DALA2023071705779](https://openairdocs.org/sdr/DALA2023071705779.md): Unknown · unknown · Jul 16, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS ON LH MEMBRANE WEB UPPER, LOWER SURFACE BTW STA 463 TO STA 466 AT PAX CABIN IN REF NRC 0353. SUMMARY OF NRC 00657: CORROSION LEVEL 2. CORROSION OUT OF LIMITS ON LH MEMBRANE WEB UPPER/LOWER SURFACE BTW STA 463 TO STA 466 AT PAX CABIN WAS
- [SDR DALA2023071705776](https://openairdocs.org/sdr/DALA2023071705776.md): Unknown · unknown · Jul 15, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL FROM STA Y=1002 TO STA Y=1022 AND X=0 AT PAX CABIN. SUMMARY OF NRC 00438: INTERCOSTAL FROM STA Y=1002 TO STA Y=1022 AND X=0 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1 PAR 4 FIGURE 201 AND 51-41-05-0G. (LP #
- [SDR DALA2023071705775](https://openairdocs.org/sdr/DALA2023071705775.md): Unknown · unknown · Jul 14, 2023 · N603AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION OUT OF LIMIT ON FLOOR SUPPORTS (2 EA) LH SIDE FROM STA Y=1022 TO STA Y=1053 AND X=44, AND FROM STA Y=1022 TO STA Y=1053 AND X=53.5 AT CABIN PAX. (W2) IN REF NRC 0441. SUMMARY OF NRC 00622: FLOOR SUPPORTS (2 EA) LH SIDE FROM STA Y=1022 TO STA Y=1053 A
- [SDR DALA2023071305678](https://openairdocs.org/sdr/DALA2023071305678.md): Unknown · unknown · Jul 12, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED CUSP WEB BTW STA 658 TO STA 664 RH SIDE AT PAX CABIN. SUMMARY OF NRC 00399: CUSP WEB BTW STA 658 TO STA 664 RH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (LP #2862517)
- [SDR DALA2023071205662](https://openairdocs.org/sdr/DALA2023071205662.md): Unknown · unknown · Jul 9, 2023 · N603AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CORROSION ON BULKHEAD STA 1053 BTW L28R/L28L AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00314: CORROSION LEVEL 2. BULKHEAD DOUBLER STA 1053 BTW L28R/L28L AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2856373)
- [SDR DALA2020031801918](https://openairdocs.org/sdr/DALA2020031801918.md): Light · inoperative · Mar 18, 2020 · N603AT · Boeing 717200 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS IN CABIN CEILING ARE INOPERATIVE. MAINTENANCE RELAMPED THEM IAW B717 AMM 33-51. (LP #6674820)
- [SDR DALA2018123197452](https://openairdocs.org/sdr/DALA2018123197452.md): Power Supply · malfunctioned · Dec 28, 2018 · N603AT · Boeing 717200 · Emergency Lighting
  > THE AFT BULKHEAD EMERGENCY DOOR EXIT SIGN IS INOPERATIVE AND THE MID CABIN OVERHEAD AISLE EMERGENCY EXIT LIGHT IS ALSO INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLIES FOR AFT AND MID EMERGENCY LIGHTS IAW B717 AMM 33-50. OPERATIONAL CHECK WAS GOOD AND THE
- [SDR DALA2018110606495](https://openairdocs.org/sdr/DALA2018110606495.md): Battery Pack · shorted · Nov 3, 2018 · N603AT · Boeing 717200 · Emergency Lighting
  > ON SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT LIGHTS FOR BOTH LEFT AND RIGHT FORWARD FLOOR LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND THAT BATTERY PACK ASSEMBLY B5-119 HAD INTERNAL SHORT. BATTERY PACK B5-119 WAS REPLACED. THE EMERGENCY LIGHTS NOW
- [SDR DALA2018101506043](https://openairdocs.org/sdr/DALA2018101506043.md): Lens · unsecure · Oct 14, 2018 · N603AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT AT DOOR 1L HAS A DAMAGED DIFFUSER LENS ON THE EXIT SIGN AND THE COVER FALLS OFF. MAINTENANCE REPLACED THE LIGHT COVER ABOVE DOOR 1L AND INSTALLED A NEW DIFFUSER. CHECKS ARE GOOD. (LP 0784436)
- [SDR DALA2018101105975](https://openairdocs.org/sdr/DALA2018101105975.md): Light · inoperative · Oct 11, 2018 · N603AT · Boeing 717200 · Emergency Lighting
  > 8 EMERGENCY LIGHTS INOP AISLE OVHD DURING SVC CK. RELAMPED INOP LTS, NO HELP. FOUND 3 BULBS BURNT OUT. RELAMPED. OPS CKD PER AMM 33-52-00. ALL LIGHTS WORK. OK FOR SERVICE.
- [SDR DALA2018082085142](https://openairdocs.org/sdr/DALA2018082085142.md): Door Frame · corroded · Aug 17, 2018 · N603AT · Boeing 717200 · Fuselage Main, Structure
  > SEVERAL AREAS ON THE FORWARD LOWER CARGO DOOR FRAME HAD SIGNS OF CORROSION. REPLACED THE FWD CARGO DOOR LOWER FRAME PAN IAW SRM 53-20-15-2R, REPAIR 6.
- [SDR DALA2018081605102](https://openairdocs.org/sdr/DALA2018081605102.md): Cam · cocked · Aug 15, 2018 · N603AT · Boeing 717200 · Aerodynamic Fairings
  > TAILONE RELEASE CAM TAB WAS CLOCKED INCORRECTLY. ADJUSTED THE RELEASE CAM IAW AMM 53-52-03.
- [SDR DALA2018041802584](https://openairdocs.org/sdr/DALA2018041802584.md): Bracket · damaged · Apr 17, 2018 · N603AT · Boeing 717200 · Emergency Lighting
  > FOUND THE EMERGENCY LIGHT BATTERY PACK BRACKET TO BE DAMAGED. MAINTENANCE REPLACED THE EMERGENCY LIGHTS POWER SUPPLY PER AMM 33-51. OPERATIONAL CHECK WAS NORMAL.
- [SDR DALA2018040202116](https://openairdocs.org/sdr/DALA2018040202116.md): Lens · missing · Mar 30, 2018 · N603AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT SIGN LENS MISSING IN THE FIRST CLASS CABIN. MAINTENANCE INSTALLED THE LENS. THE AIRCRAFT IS OK FOR SERVICE.
- [SDR DALA2018032601906](https://openairdocs.org/sdr/DALA2018032601906.md): Battery Pack · inoperative · Mar 24, 2018 · N603AT · Boeing 717200 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND BOTH AFT OVERWING EXIT HATCH LOWER EXIT SIGNS INOPERATIVE. MAINTENANCE FOUND BATTERY PACK TO BE BAD. REPLACED THE BATTERY PACK ASSEMBLY B5-119. THE EMERGENCY LIGHTS TEST NORMAL IAW AMM 33-51.

Next page: https://openairdocs.org/aircraft/N603AT/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 = 'N603AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N603AT/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.