# Service difficulty reports: N915AT

A list on [N915AT](https://openairdocs.org/aircraft/N915AT.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 · 197 reports

- [SDR DALA2026091805212](https://openairdocs.org/sdr/DALA2026091805212.md): Battery Pack · inoperative · Sep 17, 2026 · N915AT · Boeing 717200 · Emergency Lighting
  > LT & RT OVERWING FWD EMERGENCY EXIT DOOR LIGHTS ARE INOP, R/R EMERGENCY POWER SUPPLY BATTERY PACK FOR FWD OVERWING EXIT PER B717 AMM 53-51-03. (9484062) (AIRCRAFT GROUNDED).
- [SDR DALA2026072004261](https://openairdocs.org/sdr/DALA2026072004261.md): Girt Bar · dirty · Jul 17, 2026 · N915AT · Boeing 717200 · Emergency Equipment
  > GIRT BARS DIRTY AND HARD TO ARM. INSPECTED BARS & OPS CHECK OF LATCHES GOOD IAW AMM 25-61. (8826616) AIRCRAFT GROUNDED.
- [SDR DALA2026021801128](https://openairdocs.org/sdr/DALA2026021801128.md): Battery · discharged · Feb 10, 2026 · N915AT · Boeing 717200 · Emergency Lighting
  > AFT OVERWING EXIT ROW LIGHTS INOPERATIVE. RESET BATTERY AND LET RECHARGE FOR FEW HOURS, OPS CHECKED GOOD IAW AMM 33-51 (8111544).
- [SDR DALA2026010509565](https://openairdocs.org/sdr/DALA2026010509565.md): Warning Message · false activation · Dec 27, 2025 · N915AT · Boeing 717200 · Central Warning
  > ATO, ABORTED TAKE-OFF AT 60KTS DUE TO A STABILIZER CONFIGURATION MESSAGE. MAINTENANCE PERFORMED A HORIZONTAL STABILIZER CHECK, THE SYS OPS PROPERLY, AND AIRCRAFT WAS RETURNED TO SERVICE.(8144086)
- [SDR DALA2025121009020](https://openairdocs.org/sdr/DALA2025121009020.md): Door Frame · damaged · Dec 6, 2025 · N915AT · Boeing 717200 · Fuselage Main, Structure
  > AFT CARGO DOOR FRAME STATION 944 - FOUND PLUG RIVET UNDER SPLICE PLATE REMOVED FOR REPAIR. REPAIRED PER ER/A 630377-14 REV. ORIG. (1338586)
- [SDR DALA2025121009019](https://openairdocs.org/sdr/DALA2025121009019.md): Threshold · corroded · Dec 5, 2025 · N915AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION IN THRESHOLD PAN SEVERAL LOCATIONS. CORROSION DAMAGE SPLICE REPAIR - CHECKED AND REPLACED HI-SHEAR FASTENERS REF: B717-200 SRM 51-41-04 (1336682)
- [SDR DALA2025101407520](https://openairdocs.org/sdr/DALA2025101407520.md): Spar · corroded · Oct 3, 2025 · N915AT · Boeing 717200 · Wing Spar
  > WORKING PRI 629584-14 REV 0, REV1, REV 2, REV 3, AND ERA 629584- 14AD REV ORIG. LT REAR SPAR XRS 179 CORROSION. ACCOMPLISHED PRI 629584-14AD REV 3 LT WING REAR SPAR XRS 179 REPAIR. SFAR 88 AND CDCCL REQUIREMENTS C.W. (1232961)
- [SDR DALA2025043003322](https://openairdocs.org/sdr/DALA2025043003322.md): Holder · sparks · Apr 29, 2025 · N915AT · Boeing 717200 · Flight Compartment Lighting
  > WHILE MOVING CAPT NOTE PAD HOLDER HAD SPARKS BEHIND THE HOLDER & ALL MAP LIGHTS WENT OUT. ALSO, CIRCUIT BREAKER W29 TRIPPED. MAINTENANCE REPAIRED BARE WIRES PER B717 SWPM 20-10-03. NO FURTHER ISSUES. OPERATIONAL CHECK WAS NORMAL ON CHART HOLDER. (LP #7237748)
- [SDR DALA2024110410592](https://openairdocs.org/sdr/DALA2024110410592.md): Battery Pack · inoperative · Nov 3, 2024 · N915AT · Boeing 717200 · Emergency Lighting
  > BOTH AFT OVERWING LOWER SIDE WALL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-119 PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. (LP #6342840)
- [SDR DALA2024091909180](https://openairdocs.org/sdr/DALA2024091909180.md): Pseu · failed · Sep 19, 2024 · N915AT · Boeing 717200 · Landing Gear Position and Warning
  > SHIP 9580 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO A "PSEU FAIL" MESSAGE. THE QRH WAS COMPLIED WITH AND THE LANDING GEAR POSITION INDICATIONS WERE NORMAL FOLLOWING GEAR EXTENSION FOR LANDING. HOWEVER, THE LEADING EDGE SLATS FAILED TO EXTEND RESUL
- [SDR DALA2023120710011](https://openairdocs.org/sdr/DALA2023120710011.md): Unknown · unknown · Dec 5, 2023 · N915AT · Boeing 717200 · Landing Gear Position and Warning
  > SHIP 9580 -ATB/DE- FUNCTIONAL CHECK FLIGHT. SECOND ATTEMPT. THE CREW RETURNED TO THE DEPARTURE FIELD AFTER THE LANDING GEAR MALFUNCTIONED. NORMAL GEAR RETRACTION ON TAKEOFF. FCF CHECKLIST REQUIRED GEAR EXTENSION INFLIGHT; WHEN RETRACTING, CREW RECEIVED A RED "
- [SDR DALA2023120710010](https://openairdocs.org/sdr/DALA2023120710010.md): Unknown · unknown · Dec 4, 2023 · N915AT · Boeing 717200 · Landing Gear Position and Warning
  > SHIP 9580 -ATB/DE- FUNCTIONAL CHECK FLIGHT. THE CREW RETURNED TO THE DEPARTURE FIELD AFTER THE LANDING GEAR FAILED TO RETRACT PROPERLY. GEAR RETRACTION SHORTLY AFTER TAKEOFF PRODUCED A RED "RIGHT GEAR UNSAFE" INDICATION. QRH 14.18 WAS COMPLIED WITH. LOWERING T
- [SDR DALA2023120409901](https://openairdocs.org/sdr/DALA2023120409901.md): Unknown · unknown · Dec 2, 2023 · N915AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACKS ON OUTER PAN (3 EA) ON STOP FITTING AREA (AFT EDGE) AT AFT CARGO DOOR. SUMMARY OF NRC 0072: CRACKS OUTER PAN ON STOP FITTINGS AREA (AFT EDGE) AT AFT CARGO DOOR WERE REPAIRED PER ERA 613600-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 613600-14 REV
- [SDR DALA2023120109873](https://openairdocs.org/sdr/DALA2023120109873.md): Unknown · unknown · Nov 30, 2023 · N915AT · Boeing 717200 · Fuselage Internal Mounting Structure
  > CORROSION FRAMES CLIP STA=927 STGR 29RH TO STGR 28LH AT AFT CARGO COMPARTMENT C2 (ON REFERENCE NRC 0139). SUMMARY OF NRC 00493: CORROSION LEVEL 2. FRAME CLIP STA=927 STGR 29RH TO STGR 28LH AT AFT CARGO COMPARTMENT C2 WAS FABRICATED PER DWG 9915524 REV P AND RE
- [SDR DALA2023112809755](https://openairdocs.org/sdr/DALA2023112809755.md): Unknown · unknown · Nov 27, 2023 · N915AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON L2L AND STA Y 1133 AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00496: LONGERON L2L AND STA Y 1133 AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER B717-200 SRM-53-00-05-2R-2 PAR 5, FIG 201. (LP #0083405)
- [SDR DALA2023112709722](https://openairdocs.org/sdr/DALA2023112709722.md): Unknown · unknown · Nov 24, 2023 · N915AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON DOOR JAMB STA Y 954 TO STA Y 994 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00058: CORROSION LEVEL 2. DOOR JAMB STA Y 954 TO STA Y 994 AT AFT CARGO COMPARTMENT (C2) WAS REPAIRED PER B717-200 SRM 53-20-15 2R PROCEDURE 7. (LP #0079727)
- [SDR DALA2024022102373](https://openairdocs.org/sdr/DALA2024022102373.md): Trunnion · corroded · Nov 23, 2023 · N915AT · Boeing 717200 · Fuselage, Landing Gear Attach Fittings
  > WEAR AND CORROSION ON FIXED STRUT MLG ATTACH FITTING AND BUSHING ALSO (TRAPEZOIDAL PANEL) AND BUSHING AT RH MLG IN REF AMDS 3211-4004 STEP 4. SUMMARY OF NRC 00434: CORROSION LEVEL 1. WEAR AND CORROSION ON FIXED STRUT MLG ATTACH FITTING AND BUSHING ALSO (TRAPEZ
- [SDR DALA2023111609439](https://openairdocs.org/sdr/DALA2023111609439.md): Unknown · unknown · Nov 15, 2023 · N915AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON DOOR JAMB STA Y 370 TO STA Y 424 AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00057: CORROSION LEVEL 2. DOOR JAMB AT FWD CARGO COMPARTMENT (C1) WAS REPAIRED PER SRM 53-20-15-2R PROCEDURE 6 REPAIR 6 PAR 6 FIG 201 AND 51-41-02-0G. (LP #0067222)
- [SDR DALA2023111409348](https://openairdocs.org/sdr/DALA2023111409348.md): Unknown · unknown · Nov 13, 2023 · N915AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT FROM STA Y=160 TO STA Y=200 AND X=56 AT LOWER SIDE OF FWD PASSENGER DOOR JAMB. SUMMARY OF NRC 00254: CORROSION LEVEL 2. FLOOR SUPPORT FROM STA Y=160 TO STA Y=200 AND X=56 AT LOWER SIDE OF FWD PASSENGER DOOR JAMB WAS REPLACED PER DWG
- [SDR DALA2023110809202](https://openairdocs.org/sdr/DALA2023110809202.md): Unknown · unknown · Nov 8, 2023 · N915AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB (LOWER SURFACE) BTW STA Y=1022-1037 -X=57 TO -X=60 AT RH WEB PAX CABIN. SUMMARY OF NRC 00291: CORROSION LEVEL 2. WEB (LOWER SURFACE) BTW STA Y=1022-1037 -X=57 TO -X=60 AT RH WEB PAX CABIN WAS REPLACED PER DWG 9981474 REV K AND PER B717-200 SRM
- [SDR DALA2023101408450](https://openairdocs.org/sdr/DALA2023101408450.md): Unknown · unknown · Oct 13, 2023 · N915AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ASSEMBLY ABOVE R1 DOOR HANDLE, BR9051-001, IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE R1 DOOR. OPERATIONAL CHECK WAS GOOD. (LP #7217465)
- [SDR DALA2023101408449](https://openairdocs.org/sdr/DALA2023101408449.md): Unknown · unknown · Oct 13, 2023 · N915AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHT BATTERY CHARGER AT STA 332 - 351 PANEL P1-118 EIN B5-118 IS DEFECTIVE REF B717 33-51-14. MAINTENANCE REPLACED THE EMERGENCY LIGHT CHARGER AT STA 332 REF B717 WDM 33-51- 14. (LP #7217464)
- [SDR DALA2019061103495](https://openairdocs.org/sdr/DALA2019061103495.md): Skin · dented · Jun 10, 2019 · N915AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DENTS ON FUSELAGE SKIN AT STA 427 BETWEEN LONGERON 27L AND 29L. ACCOMPLISHED PERMANENT REPAIR REF PRI #578768-14, REV. 1 AND ER/A #578768 -14 REV. ORIGINAL. REQUIRED INSPECTION COMPLETE QC1981. (LP #1116346)
- [SDR DALA201906113489](https://openairdocs.org/sdr/DALA201906113489.md): Skin · dented · Jun 9, 2019 · N915AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN AT STA 524 TO 527 1" BELOW LONG 26L LAP SEAM. PER B717 SRM 53-01-01-1A-3 CONDITION 5 DENT IS OUT OF LIMITS. REMOVED DAMAGE 1" X 3" PER B717 SRM 53-03-01-2R-1 FIG. 110 SHEET 3. FUSELAGE SKIN MISDRILLED AT STA 520 ON LONG 26L, REMOVED DAMAG
- [SDR DALA2019010200009](https://openairdocs.org/sdr/DALA2019010200009.md): Terminal · broken · Dec 31, 2018 · N915AT · Boeing 717200 · Light System Wiring
  > THE AFT WALKWAY EMERGENCY LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A WIRE TERMINAL BROKEN. THE WIRE TERMINAL WAS REPAIRED PER SWPM CHAPTER 20. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #5521308)
- [SDR DALA2018120547036](https://openairdocs.org/sdr/DALA2018120547036.md): Seal · missing · Dec 3, 2018 · N915AT · Boeing 717200 · Leading Edge Devices
  > LEFT WING INBOARD SLAT MISSING ABOUT 9.5" OF SEAL. MISSING SEAL STARTS AT 30 IN. FROM MOST INBD EDGE OF SEAL ON LT WING #1 SLAT. FWD TO CDL 57-48-01. SDR REPORTED DUE TO POSSIBILITY THAT PART MAY HAVE DEPARTED THE AIRCRAFT DURING FLIGHT. (LP4252114)
- [SDR DALA2018092005668](https://openairdocs.org/sdr/DALA2018092005668.md): Warning System · false activation · Sep 19, 2018 · N915AT · Boeing 717200 · Stabilizer Position Indicating
  > THE CREW ABORTED THE TAKEOFF AFTER 110 KNOTS FOLLOWING AN AURAL STABILIZER MOTION WARNING AND AN ILLUMINATED RED "STAB TRIM" MESSAGE. MAINTENANCE VERIFIED THAT NO FAULTS WERE RECORDED IN THE VERSATILE INTEGRATED AVIONICS SYSTEMS 1 OR 2. BOTH VIA 1 AND 2 WERE R
- [SDR DALA2018091805645](https://openairdocs.org/sdr/DALA2018091805645.md): Light · unknown · Sep 15, 2018 · N915AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY SEAT MOUNTED LIGHTING DAMAGED AND INOPERATIVE. MAINTENANCE REINSTALLED THE EMERGENCY LIGHT AT 28B.
- [SDR DALA2017022101389](https://openairdocs.org/sdr/DALA2017022101389.md): Light · inoperative · Feb 21, 2017 · N915AT · Boeing 717200 · Emergency Lighting
  > DURING A LINE CHECK, MAINTENANCE FOUND THAT THE RIGHT WING EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK.
- [SDR DALA2016061904762](https://openairdocs.org/sdr/DALA2016061904762.md): Web · damaged · Jun 18, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > TOOL MARK ON WEB STA Y=674 BETWEEN LONGERON 11RT TO 10RT AND LONGERON 14RT TO 15RT AT CPAX, SM, CARD 6, ZONE 201. WEB WAS REPAIR IAW ER/A 547802-14, REV ORIGINAL AND ETI 17-16-064, SRM 51-40-08, 51-20-09 AND 51-10-04, PAR 15/21.
- [SDR DALA2016061604672](https://openairdocs.org/sdr/DALA2016061604672.md): Strap · cracked · Jun 15, 2016 · N915AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON FWD STRAP AT BEAM NR 6 L1 PASSEGER DOOR. STRAP WAS REPLACED IAW SRM 51-41-02, 51-41-05, 51-40-08, 51-10-04 PAR 15 AND 21, AND DWG 9955750, REV. U. CRACK LENGTH.500".
- [SDR DALA2016061604671](https://openairdocs.org/sdr/DALA2016061604671.md): Angle · corroded · Jun 15, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP ANGLE AT LBL 60 BETWEEN BS 157 AND 218. DUE TO EXCESSIVE DAMAGE BY CORROSION. CUSP ANGLE WAS REPAIRED IAW ETI 17-16-054, REV 1 AND ER/A 547810-14, REV ORIGINAL.
- [SDR DALA2016061504667](https://openairdocs.org/sdr/DALA2016061504667.md): Structure · bent · Jun 14, 2016 · N915AT · Boeing 717200 · Passenger/Crew Doors
  > BEND ON FWD/AFT LOWER CORNER AT EXTERNAL SURFACE PASSENGER L1 DOOR. LOWER CORNER AT EXTENAL SURFACE PASSENGER ENTRANCE DOOR WAS REPAIRED IAW SRM 52-10-01, FIG 201, REP 2. WEIGHT IS 1.52 LB. RII INSPECTOR EVP 200801883 TECHOPS.
- [SDR DALA2016061504666](https://openairdocs.org/sdr/DALA2016061504666.md): Doubler · cracked · Jun 14, 2016 · N915AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON DOUBLER FWD/AFT END AT BEAM NR 1 L1 DOOR. FWD/AFT END AT BEAM NR 1 WERE REPIRED IAW SRM 52-10-02, FIG 201, REPAIR 7. CRACKS LONG.656 AND.468".
- [SDR DALA2016061504665](https://openairdocs.org/sdr/DALA2016061504665.md): Doubler · cracked · Jun 14, 2016 · N915AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON DOUBLER AFT END AT BEAM NR 7 L1 DOOR. AFT END AT BEAM NR 7 WAS REPAIRED IAW SRM 52-10-02, FIG 201, REPAIR 13. CRACK LONG 0.812".
- [SDR DALA2016061504664](https://openairdocs.org/sdr/DALA2016061504664.md): Doubler · worn · Jun 14, 2016 · N915AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > WEAR ON DOUBLER PRODUCTION AT INNER RT PAN A SIDE LOWER HINGE AFT EMERGENCY EXIT. DOUBLER PRODUCTION WAS REPAIRED IAW SRM 52-10-02, FIG 201, REP 16. MEASURE: OT IS 0.050" AND REMAINING THICKNESS IS 0.028". THEREFORE OUT LIMITS. EQ: DIGITAL ULTRASONIC THICK
- [SDR DALA2016061504662](https://openairdocs.org/sdr/DALA2016061504662.md): Skin · cracked · Jun 14, 2016 · N915AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKED FUSELAGE SKIN ON CUTOUT OF RT/LT NLG AFT DOOR AFT HINGE. SKIN WAS REPLACED IAW SRM 53-10-01, 51-41-02, 51-41-05, 51-10-3 P. 21, 15.
- [SDR DALA2016061404601](https://openairdocs.org/sdr/DALA2016061404601.md): Cargo Track · corroded · Jun 13, 2016 · N915AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT CARGO TRACK UPPER & LOWER SURFACE BETWEEN BS 900-954. DUE TO EXCESSIVE DAMAGE, CARGO TRACK SECTION WAS REPLACED IAW SRM 51-41-05 AND 51-41-02.
- [SDR DALA2016061404600](https://openairdocs.org/sdr/DALA2016061404600.md): Angle · cracked · Jun 13, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE OF WING BOX FLOOR STRUCTURE BS 712 TO 714 X -20 AND Z -8. ANGLE WAS REPLACED IAW SRM 51-41-02 AND SRM 51-41-05 AND DWG 5910464, REV "DE" ITEM 24.
- [SDR DALA2016061404599](https://openairdocs.org/sdr/DALA2016061404599.md): Access Panel · corroded · Jun 13, 2016 · N915AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520EB AT LT WING. CORROSION ON COUNTERSINK OF ACCESS DOOR 520EB WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.545", 0.555", AND 0.540" AND WAS REP
- [SDR DALA2016061304548](https://openairdocs.org/sdr/DALA2016061304548.md): Longeron · corroded · Jun 12, 2016 · N915AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 29 LT BELOW OF SPLICE BS 960 IN AFT CARGO COMPARTMENT. DAMAGE ON SECTION LONGERON WAS REMOVED AND WAS REPAIRED IAW SRM 51-10-04 AND 53-20-05, FIG 201.
- [SDR DALA2016061304547](https://openairdocs.org/sdr/DALA2016061304547.md): Access Panel · corroded · Jun 12, 2016 · N915AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620EB AT RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS 620EB WERE REMOVED AND FOUND OUT LIMITS WITH 3 ADVANCED HOLES.545,.549,.544 THEREFORE WAS REPLACED IAW SRM 57-10
- [SDR DALA2016061304546](https://openairdocs.org/sdr/DALA2016061304546.md): Frame · corroded · Jun 12, 2016 · N915AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME ANGLE BS 908 BETWEEN LONGERON 29 AND 30L IN AFT CARGO COMPARTMENT. FRAME ANGLE WAS REPAIRED IAW SRM 53-00-06, FIG 201.
- [SDR DALA2016061104537](https://openairdocs.org/sdr/DALA2016061104537.md): Access Panel · corroded · Jun 10, 2016 · N915AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620DB AT RT WING. CORROSION ON COUNTERSINKS AND SETTLEMENT AREA WAS REMOVED IAW SRM 57-10-01 AND 51-10-04 AND FUEL ACCESS PLATE WERE MEASSURED, 4 HOLES FOUND OUT LIMITS.535,.534,.549,.554 I
- [SDR DALA2016061104536](https://openairdocs.org/sdr/DALA2016061104536.md): Access Panel · corroded · Jun 10, 2016 · N915AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620CB AT RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT AREA WAS REMOVED IAW SRM 57-10-01. FUEL ACCESS PLATE NR 620CB WAS MEASURED, 6 EAS, HOLES FOUND OUT LIMITS.554,.534,.546,.541,.565
- [SDR DALA2016061104533](https://openairdocs.org/sdr/DALA2016061104533.md): Floor Panel · cracked · Jun 10, 2016 · N915AT · Boeing 717200 · Fuselage Floor Panel
  > CRACKED STIFFENERS ON PASSENGER CABIN FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM 53-20-50.
- [SDR DALA2016061104532](https://openairdocs.org/sdr/DALA2016061104532.md): Floor Panel · cracked · Jun 10, 2016 · N915AT · Boeing 717200 · Fuselage Floor Panel
  > CRACKED FLOOR PANEL 211ACF. FLOOR PANEL FABRICATED IAW ER/A 546544-14, REV.
- [SDR DALA2016061004502](https://openairdocs.org/sdr/DALA2016061004502.md): Floor Panel · damaged · Jun 9, 2016 · N915AT · Boeing 717200 · Fuselage Floor Panel
  > CRACK ON PASSENGER CABIN FLOOR PANEL NR 222ZF. SM, CARD 52, ZONE 000. FLOOR PANEL 222ZF WAS REPAIRED IAW SRM 53-00-00, REPAIR 2, FIG 201. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. TREATED, PAINTED, AND APPLIED CIC I
- [SDR DALA2016061004501](https://openairdocs.org/sdr/DALA2016061004501.md): Floor Panel · damaged · Jun 9, 2016 · N915AT · Boeing 717200 · Fuselage Floor Panel
  > DAMAGE AND MISSING FERRULES ON FLOOR PANELS, NR 222ABF, 222AAF, 222AEF, AND 222AKF AT PAX CABIN. SM, CARD 79, ZONE 000. DAMAGE FERRULES WERE REPLACED ON FLOOR PANELS NR 22ABF, 222AAF, 222AEF, AND 222AKF IAW ER/A 546544-14, REV. ORIGINAL ASSOCIATED ER/A 00-54
- [SDR DALA2016061004500](https://openairdocs.org/sdr/DALA2016061004500.md): Floor Panel · damaged · Jun 9, 2016 · N915AT · Boeing 717200 · Fuselage Floor Panel
  > DAMAGE AND MISSING FERRULES ON FLOOR PANELS 221FF, 221CF, 22BF, 22LF, 222JF, 222RF, AND 222UF. SM, CARD 77, ZONE 000. DAMAGE FERRULES ON FLOOR PANEL NR 222BF, 222RF, 222LF, 222JF, AND 221EF WERE REPLACED IAW DWG NR 9936546 AND ER/A 546544-14, REV. ORIGINAL F

Next page: https://openairdocs.org/aircraft/N915AT/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 = 'N915AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N915AT/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.