# Service difficulty reports: N938AT

A list on [N938AT](https://openairdocs.org/aircraft/N938AT.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 3 · 150 reports

- [SDR DALA2026100705545](https://openairdocs.org/sdr/DALA2026100705545.md): Flap · damaged · Oct 6, 2026 · N938AT · Boeing 717200 · Trailing Edge Flaps
  > FOUND DAMAGE ON LEFT TRAILING EDGE FLAP, INSTALLED PERMANENT REPAIR PER B717 SRM 57-00-01-02A. (9483579) (AIRCRAFT GROUNDED).
- [SDR DALA2026071404143](https://openairdocs.org/sdr/DALA2026071404143.md): Display · faulted · Jul 13, 2026 · N938AT · Boeing 717200 · Central Display
  > DIVERTED TO BWI DUE TO SYSTEM DISPLAY CONTROL PANEL FAULTS. REPLACED EFIS DISPLAY SELECT PANEL IAW AMM 31-62-01. OPS CHKD GOOD. (8290442) (AIRCRAFT GROUNDED)
- [SDR DALA2026070803992](https://openairdocs.org/sdr/DALA2026070803992.md): Lamp · inoperative · Jul 7, 2026 · N938AT · Boeing 717200 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-11. (8290423) (AIRCRAFT GROUNDED).
- [SDR DALA2026012200495](https://openairdocs.org/sdr/DALA2026012200495.md): Unknown · vibration · Jan 20, 2026 · N938AT · Boeing 717200 · Fuselage Structure (General)
  > DIVERTED TO SYR DUE TO AIRFRAME VIBRATIONS IN FLIGHT. PERFORMED AIRFRAME VIBRATION INSPECTION PER AMM. PERFORMED IDLE ENGINE RUN WITH BOTH VIBRATION INDICATIONS WITHIN LIMITS. OPS CHECKS NORMAL.(7787876)
- [SDR DALA2026012200494](https://openairdocs.org/sdr/DALA2026012200494.md): Battery Pack · inoperative · Jan 16, 2026 · N938AT · Boeing 717200 · Emergency Lighting
  > NUMEROUSE EMERGENCY CEILING LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK B5-231 AND OPS CHECKED GOOD IAW BN717 AMM 33-21. (8406044)
- [SDR DALA2025111808426](https://openairdocs.org/sdr/DALA2025111808426.md): Module · inoperative · Nov 13, 2025 · N938AT · Boeing 717200 · Fuel Quantity Indicator
  > DIVERTED TO MSN DUE TO FUEL QUANTITY INOPERATIVE. REPLACED ELECTRONIC MODULE. OPS CHECK NORMAL.(1301584)
- [SDR DALA2025070805069](https://openairdocs.org/sdr/DALA2025070805069.md): Valve · binding · Jul 7, 2025 · N938AT · Boeing 717200 · Air Distribution System
  > SHIP 9561 -ATB- DUE TO CLT DUE TO SMOKE IN THE CABIN COMING FROM FWD GALLEY AREA. SMOKE DISSIPATED AND EMERGENCY WAS DECLARED. CORRECTIVE ACTION: FOUND BUFFER AIR VALVE BINDING. REPLACED SAME. OPS CHECKS GOOD.
- [SDR DALA2025043003320](https://openairdocs.org/sdr/DALA2025043003320.md): Battery Pack · inoperative · Apr 29, 2025 · N938AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY LIGHTS (3 EA) LOCATED AT CEILING PANEL IN FRONT OF FWD LAVATORY, EXIT SIGN AT TOP OF COW 1 AND ABOVE THE SERVICE DOOR DOES NOT OPERATE. THE POWER ASSEMBLY BATTERY PACK WAS REPLACED PER B717-200 AMM 33-51-04. TEST OK. (LP #6915838)
- [SDR DALA2025042403189](https://openairdocs.org/sdr/DALA2025042403189.md): Skin · worn · Apr 22, 2025 · N938AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > WEAR ON SKIN BTW STA Y=994 L24R TO L26R (AFT EDGE CUT OUT) AT AFT CARGO DOOR. WORN SKIN BTW STA Y=994 L24R TO L26R (AFT EDGE CUT OUT) AT AFT CARGO DOOR WAS REPAIRED PER PRI 625059-14 REV 7 AND ER/A 625059-14 REV ORIGINAL SECTION I: PERMANENT REPAIR.
- [SDR DALA2025041602959](https://openairdocs.org/sdr/DALA2025041602959.md): Doubler · cracked · Apr 15, 2025 · N938AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK FOUND ON INTERNAL DOUBLER AT STA Y=1178 CANT LONGERON 17RH AT AFT ACCESSORIES COMPARTMENT. SUMMARY OF NRC 00686: INTERNAL CAP DOUBLER AT STA Y=1178 CANT LONGERON 17RH AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 RE
- [SDR DALA2025041202832](https://openairdocs.org/sdr/DALA2025041202832.md): Longeron · cracked · Apr 12, 2025 · N938AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK WAS FOUND BTW STA Y=1178 APPROX IN LONG 17R AT AFT FUSELAGE. SUMMARY OF NRC 00660: CRACK BTW STA Y=1178 APPROX IN LONG 17R AT AFT FUSELAGE WAS REPAIRED PER ERA 625404-14 REV ORIGINAL SECTION 1: PERMANENT REPAIR. ASSOCIATED ER/A 14-625404 ADDED FOR AC 956
- [SDR DALA2025041202830](https://openairdocs.org/sdr/DALA2025041202830.md): Access Panel · corroded · Apr 11, 2025 · N938AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION OUT OF LIMITS ON COUNTERSINKS OF ACCESS PANELS: 520CB (3 HOLES), 520DB (4 HOLES), 520FT (6 HOLES), 620GB (3 HOLES), 620FT (2 HOLES), AND 620DT (3 HOLES) PER B717-200 SRM 57-10-01-2R PROCEDURE 2. SUMMARY OF NRC 00631: CORROSION LEVEL 2. ACCESS PANELS:
- [SDR DALA2025040802704](https://openairdocs.org/sdr/DALA2025040802704.md): Cargo Track · corroded · Apr 8, 2025 · N938AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > DUE TO CORRISION REWORK, (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON SIDE TIE TRACK BTW L27L TO L28L AND STA=900 LH TO STA=1022 LH AFT CARGO COMPARTMENT. WITH AN ORIGINAL THICKNESS OF 0.060IN, AND MINIMUN REMAINING THICKNESS OF 0.027IN. THE AREA REWORKED IS
- [SDR DALA2025040802702](https://openairdocs.org/sdr/DALA2025040802702.md): Frame · corroded · Apr 5, 2025 · N938AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME STA Y=870 L29L TO L29R. ORIGINAL THICKNESS IS 0.063IN AND MINIMUM REMAINING THICKNESS IS 0.029IN THEREFORE AREA IS OUT OF LIMITS PER B717-200 SRM 53-00-00-1A PAR 4C (2) FIG 103. SUMMARY OF NRC 00663: CORROSION LEVEL 2. FRAME STA Y=870 L29L T
- [SDR DALA2025040802700](https://openairdocs.org/sdr/DALA2025040802700.md): Skin · corroded · Apr 5, 2025 · N938AT · Boeing 717200 · Horizontal Stabilizer, Plate/Skin
  > CORROSION ON BARREL NUT HOLE #28 AT HORIZONTAL STABILIZER UPPER SURFACE LH SIDE (CENTER SECTION). (EHV). SUMMARY OF NRC 00383: CORROSION LEVEL 2. BARREL NUT HOLE #28 AT HORIZONTAL STABILIZER UPPER SURFACE LH SIDE WAS REPAIRED PER PRI 624982-14 REV 1 & ER/A 624
- [SDR DALA2025040802698](https://openairdocs.org/sdr/DALA2025040802698.md): Pan · corroded · Apr 4, 2025 · N938AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION AROUND DOOR JAMB PAN OF AFT CARGO COMPARMENT BTW L=25R/28R. SUMMARY OF NRC 00305: CORROSION LEVEL 2. DOOR JAMB PAN OF AFT CARGO COMPARMENT BTW L=25R/28R WAS REPLACED AND INSTALLED PER B717 SRM 53-20-15-2R-7 REPAIR 7. (LP #0896016)
- [SDR DALA2025040402565](https://openairdocs.org/sdr/DALA2025040402565.md): Frame · cracked · Apr 3, 2025 · N938AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=465 BTW L-25R AND L-27R AT FWD CARGO COMPARTMENT. (CCD). SUMMARY OF NRC 00149: CRACK ON FRAME STA Y=465 BTW L-25R AND L-27R AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20 -07-2R PROCEDURE 3 REPAIR 3. PERFORM VISUAL INITIAL IN
- [SDR DALA2025040402564](https://openairdocs.org/sdr/DALA2025040402564.md): Longeron · corroded · Apr 3, 2025 · N938AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION OUT LIMITS, IN REFERENCE TO NRC 00163: CORROSION ON LONGERON BTW STA Y=956 TO STA Y=964 L30 AT AFT CARGO COMPARTMENT WITH ORIGINAL THICKNESS IS 0.125IN AND MINIMUM REMAINING THICKNESS IS 0.055IN, THEREFORE AREA IS OUT OF LIMITS PER B717-200 SRM 53-00
- [SDR DALA2025040302495](https://openairdocs.org/sdr/DALA2025040302495.md): Angle · corroded · Apr 2, 2025 · N938AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE OF AFT CARGO DOOR JAMB AREA BTW STA Y=956 AND LONGERON 27R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00300: CORROSION LEVEL 2. ANGLE OF AFT CARGO DOOR JAMB AREA BTW STA Y=956 AND LONGERON 27R AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLE
- [SDR DALA2025040302493](https://openairdocs.org/sdr/DALA2025040302493.md): Strap · cracked · Apr 2, 2025 · N938AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKED STRAP STA Y 1178 CANT UPPER CHORD, PROJECTION LONG 2 RH AT AFT ACCESORY COMPARTMENT. INITIAL INSPECTION: PERFORM DECAL CONDITION INSPECTION EVERY C-CHECK PER TOPP MANUAL 30-10-70 PAR I PAGE 14. LOG PAGE FOR CRACKED STRAP STA Y 1178 CANT UPPER CHORD, PR
- [SDR DALA2025033102352](https://openairdocs.org/sdr/DALA2025033102352.md): Skin · cracked · Mar 28, 2025 · N938AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON SKIN AT STA Y=1076 AND LONG 14R ON AFT FUSELAGE. SUMMARY OF NRC 00035: CRACK ON SKIN AT STA Y=1076 AND LONG 14R ON AFT FUSELAGE WAS REPAIRED PER PRI 624820-14 REV 3 AND ER/A 624820-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. PERFORM GVI EVERY 24 MONT
- [SDR DALA2025033102350](https://openairdocs.org/sdr/DALA2025033102350.md): Skin · cracked · Mar 28, 2025 · N938AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK EVIDENCE ON FUSELAGE SKIN LOCATED AT Y=1087 AND L-14L. SUMMARY OF NRC 00444: CRACK EVIDENCE ON FUSELAGE SKIN LOCATED AT Y=1087 AND L-14L WAS REPAIRED PER PRI 625028-14 REV 1 AND ER/A 625028-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. PERFORM GENERAL VIS
- [SDR DALA2025032402191](https://openairdocs.org/sdr/DALA2025032402191.md): Skin · dented · Mar 23, 2025 · N938AT · Boeing 717200 · Trailing Edge Flaps
  > DENT ON UPPER MID AREA NEAR L/E AT LH WING FWD MOVABLE VANE. SUMMARY OF NRC 00554: AREA DAMAGE WAS REPAIRED ON UPPER MID AREA NEAR L/E AT LH WING FWD MOVABLE VANE PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR 4. (LP #0873498)
- [SDR DALA2025032402189](https://openairdocs.org/sdr/DALA2025032402189.md): Pan · cracked · Mar 22, 2025 · N938AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACKED PAN ON AFT EDGE OF AFT CARGO COMPARMENT DOOR BTW BEAM 1-2. SUMMARY OF NRC 00096: PAN ON AFT EDGE OF AFT CARGO COMPARMENT DOOR BTW BEAM 1-2 WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 8 FIGURE 202, 51-41-02-0G PROCEDURE GENERAL, AND 51-41-05-0G. (L
- [SDR DALA2025032402188](https://openairdocs.org/sdr/DALA2025032402188.md): Beam · cracked · Mar 22, 2025 · N938AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON BEAM #8 AFT SIDE AT PASSENGER DOOR. SUMMARY OF NRC 00083: BEAM #8 AFT SIDE AT PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 14 PAR 6. (LP #0871639)
- [SDR DALA2025032402187](https://openairdocs.org/sdr/DALA2025032402187.md): Pan · cracked · Mar 22, 2025 · N938AT · Boeing 717200 · Cargo/Baggage Doors
  > A CRACK WAS FOUND ON THE #2 INNER PAN AT AFT EDGE OF THE FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC 00598: INNER PAN ON AFT EDGE BEAM #2 AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R-3 PROCEDURE 3 REPAIR 3. (LP #0871599)
- [SDR DALA2025032402186](https://openairdocs.org/sdr/DALA2025032402186.md): Door Frame · cracked · Mar 22, 2025 · N938AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON BEAM #1 AFT EDGE AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00290: BEAM #1 AFT EDGE AT PASSENGER ENTRANCE DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0871550)
- [SDR DALA2025032102134](https://openairdocs.org/sdr/DALA2025032102134.md): Frame · cracked · Mar 21, 2025 · N938AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK OF 0.093 IN LENGTH WAS FOUND ON THE UPPER RADIUS OF FRAME TAB ON THE OVERWING FRAME AT STA Y=696.000 RH. (IN REF CARD 5310-01436-04D, JOB #090-0004, STEP 10). SUMMARY OF NRC 00281: FRAME TAB ON THE OVERWING FRAME AT STA Y= 696.000 RH WAS REPAIRED PER CAR
- [SDR DALA2025032102132](https://openairdocs.org/sdr/DALA2025032102132.md): Cusp Web · cracked · Mar 20, 2025 · N938AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB BTW STA Y=655 TO STA Y=670 LH SIDE AT CABIN PASSENGER. SUMMARY OF NRC 00338: CRACK ON CUSP WEB BTW STA Y=655 TO STA Y=670 LH SIDE AT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53- 00-55-2R PROCEDURE 4 REPAIR 4 FIGURE 203. (LP #0868343)
- [SDR DALA2025032002096](https://openairdocs.org/sdr/DALA2025032002096.md): Frame · cracked · Mar 19, 2025 · N938AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1037 LONG 17L AT PASSENGER CABIN. SUMMARY OF NRC 00360: CRACK ON FRAME STA Y=1037 LONG 17L AT PASSENGER CABIN WAS REPAIRED PER B717-200 53-20-07-2R REPAIR 4. (LP #0866910)
- [SDR DALA2025032002094](https://openairdocs.org/sdr/DALA2025032002094.md): Cusp Web · damaged · Mar 19, 2025 · N938AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE ON CUSP WEB LH BTW STA Y=696 X=56 AT CABIN PASSENGER. SUMMARY OF NRC 00339: ELONGATED HOLE ON CUSP WEB LH BTW STA Y=696 X=56 AT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REP 4. (LP #0866724)
- [SDR DALA2025031902063](https://openairdocs.org/sdr/DALA2025031902063.md): Cusp Web · cracked · Mar 18, 2025 · N938AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB RH SIDE BTW STA Y=674 X-56 AT CABIN PASSENGER. SUMMARY OF NRC 00330: CRACK ON CUSP WEB RH SIDE BTW STA Y=674 X-56 AT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4, PAR 5, FIG 223, AND FIG 226. (LP #0864855)
- [SDR DALA2025031702029](https://openairdocs.org/sdr/DALA2025031702029.md): Frame · cracked · Mar 16, 2025 · N938AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1037 LONG 17R AT PASSENGER CABIN. SUMMARY OF NRC 00361: FRAME STA Y=1037 LONG 17R AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0861190)
- [SDR DALA2025031702025](https://openairdocs.org/sdr/DALA2025031702025.md): Longeron · cracked · Mar 14, 2025 · N938AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON INTERNAL AREA OF LONGERON 7R, 8R, 5R, STA Y=1022 AT PASSENGER CABIN. SUMMARY OF NRC 00363: LONGERON 8R, 5R, STA Y=1022 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2 AND LONGERON 7R NO DAMAGE WAS FOUND PER DC-MD/BOEING NDTSPM P
- [SDR DALA2025031702022](https://openairdocs.org/sdr/DALA2025031702022.md): Seat Track · corroded · Mar 14, 2025 · N938AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SEAT TRACK STA Y=236-238 -X=22 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00398: CORROSION LEVEL 2. CORROSION ON RH SEAT TRACK STA Y=236-238 -X=22 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-20-52-2R. PROC 1, REPAIR 1. (LP #
- [SDR DALA2025031401969](https://openairdocs.org/sdr/DALA2025031401969.md): Longeron · cracked · Mar 13, 2025 · N938AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON INTERNAL AREA OF LONGERON 5L STA Y=1022 AT PASSENGER CABIN. SUMMARY OF NRC 00432: CRACK ON INTERNAL AREA OF LONGERON 5L STA Y=1022 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0856135)
- [SDR DALA2024042604730](https://openairdocs.org/sdr/DALA2024042604730.md): Cover · missing · Apr 24, 2024 · N938AT · Boeing 717200 · Emergency Lighting
  > THE CABIN CEILING EMERGENCY STANDBY LIGHT LENS COVER IS MISSING AT SEAT ROW 3. MAINTENANCE FORWARDED IT TO NEF 33-21-02. CABIN LIGHT LENS MISSING SEAT ROW 3. (LP #0309494)
- [SDR DALA2024010500149](https://openairdocs.org/sdr/DALA2024010500149.md): Unknown · unknown · Jan 5, 2024 · N938AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS FROM ROW 1 TO ROW 13 CEILING LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AT B5-227 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #5006827)
- [SDR DALA2023102008641](https://openairdocs.org/sdr/DALA2023102008641.md): Unknown · unknown · Oct 19, 2023 · N938AT · Boeing 717200 · Emergency Lighting
  > THE LOWER EMERGENCY LIGHTS ARE INOPERATIVE AT THE AFT EMERGENCY EXIT. MAINTENANCE REPLACED THE BATTERY (B5-119) PER B717 AMM 33-51-04. ALL EMERGENCY LIGHT OPERATIONAL CHECKS ARE GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4620011)
- [SDR DALA2023062305084](https://openairdocs.org/sdr/DALA2023062305084.md): Unknown · unknown · Jun 22, 2023 · N938AT · Boeing 717200 · Emergency Lighting
  > ON A SERVICE CHECK, THE SIDE PAX DOOR EMERGENCY EXIT LIGHT AND SERVICE DOOR SIDE EMERGENCY EXIT LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY B5-118 AND THE BATTERY ASSEMBLY IAW B717 AMM 33-51. (LP #4798653)
- [SDR DALA2023052004046](https://openairdocs.org/sdr/DALA2023052004046.md): Unknown · unknown · May 19, 2023 · N938AT · Boeing 717200 · Emergency Lighting
  > MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS IN THE CABIN AT STA 715-737R TO BE INOPERATIVE. THE EMERGENCY LIGHTS BATTERY SUPPLY (B5-230) WAS REPLACED. OPERATIONAL CHECK WAS GOOD. (LP #4774723)
- [SDR DALA2022090405925](https://openairdocs.org/sdr/DALA2022090405925.md): None · none · Sep 4, 2022 · N938AT · Boeing 717200 · Emergency Lighting
  > AIRCRAFT 9561, EXIT LOCATOR SIGN FWD/AFT FACING DOES NOT ILLUMINATE. LIGHTED SIGN IS LOCATED ON CEILING OF CABIN BETWEEN OVER-WING EMERGENCY EXITS. CORECTIVE ACTION: REPLACED EMERGENCY LIGHTS BATTERY ASSY (LP 9147282)
- [SDR DALA2022041202525](https://openairdocs.org/sdr/DALA2022041202525.md): None · none · Apr 10, 2022 · N938AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY LIGHTS AT LOWER AFT OVERWING DOOR ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7883681)
- [SDR DALA2022010300010](https://openairdocs.org/sdr/DALA2022010300010.md): None · none · Dec 31, 2021 · N938AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > HIDDEN DAMAGE DURING THE DOUBLER REMOVE PROCESS. WEB DAMAGE WAS FOUND ON LEFT HAND SIDE, LOCATED ON INTECECTION STA 674 AND STGR 18LH. SUMMARY OF NRC 00175: WEB ON STA 674 LH WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. (LP #2071146)
- [SDR DALA2021112407218](https://openairdocs.org/sdr/DALA2021112407218.md): None · none · Nov 24, 2021 · N938AT · Boeing 717200 · Emergency Lighting
  > THERE ARE MULTIPLE CABIN EMERGENCY ESCAPE LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK B5-121 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT IS OK FOR SERVICE. (LP #8141196)
- [SDR DALA2020111303714](https://openairdocs.org/sdr/DALA2020111303714.md): Battery Pack · inoperative · Nov 13, 2020 · N938AT · Boeing 717200 · Emergency Lighting
  > DURING A SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT CEILING PANELS 11, 12, AND 13 WERE INOPERATIVE. THE BATTERY PACK, B5-231, WAS REPLACED, PER B717 WDM 33-51-12. OPERATIONAL CHECK WAS SATISFACTORY. THE AIRCRAFT IS OK FOR SERVICE.
- [SDR DALA2020031301823](https://openairdocs.org/sdr/DALA2020031301823.md): Pump · malfunctioned · Mar 13, 2020 · N938AT · Boeing 717200 · Hydraulic Pump (Electric/Engine), Main
  > ACCORDING TO THE AOS REPORT, EMERGENCY DECLARED - HYD R TEMP HI MESSAGE AFTER T/O. R&R RT ENG EDP PER B717 AMM 29-11. OPS AND LEAK CHK OK. ODI PAPERWORK C/W. PUMP, HYD, ENG 95-2911-9-0001 S/N 00019. (LP6906554)
- [SDR 2020F00283](https://openairdocs.org/sdr/2020F00283.md): Skin · delaminated · Jan 31, 2020 · N938AT · Boeing 717200 · Spoilers
  > NON ROUTINE CHECK, UPPER AND LOWER SKINS OF THE RT WING SPOILER WAS DELAMINATED.
- [SDR DALA2024012401104](https://openairdocs.org/sdr/DALA2024012401104.md): Skin · dented · Jan 8, 2020 · N938AT · Boeing 717200 · Trailing Edge Flaps
  > DENT INSPECTION RHS AFT MOVABLE VANE, UPPER SKIN - QTY 6. #5) APPROX 25" FROM O/B EDGE & 4.5" FROM T/E. 5) DENT DIMENSIONS WIDTH 1.3" X DEPTH 0.024" APPROX 25" FROM O/B EDGE & 4.5" FROM T/E. IAW B717 SRM 57-53-01 AD 1 ACCOMPLISH DVI AND TAP TEST FOR POSSIBLE D
- [SDR DALA2019121807399](https://openairdocs.org/sdr/DALA2019121807399.md): Skin · corroded · Dec 17, 2019 · N938AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CORRODED INTERNALLY AT CUTOUT FOR DRAIN MAST IN FLOOR OF E/E COMPARTMENT. EXTERNAL FILLET SEALER AROUND MAST SHOWS CORROSION PROTRUSION ALSO. NRC 001-0223:2570-2002/002 00076: (CORROSION LEVEL 2), REPLACED DOUBLER REF BOEING DWG #9923686. (LP #14

Next page: https://openairdocs.org/aircraft/N938AT/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 = 'N938AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N938AT/reports

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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.