# Service difficulty reports: N910AT

A list on [N910AT](https://openairdocs.org/aircraft/N910AT.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 DALA2020033002058](https://openairdocs.org/sdr/DALA2020033002058.md): Power Supply · inoperative · Mar 29, 2020 · N910AT · Boeing 717200 · Emergency Lighting
  > MAINTENANCE FOUND THE CENTER OVERWING INTERIOR EXIT LIGHT TO BE INOPERATIVE ON THE SERVICE CHECK. THE POWER SUPPLY AND BATTERY AT B5-120 WERE REPLACED. THE EXIT SIGN NOW WORKS PER B717 AMM 35-51. OK FOR SERVICE. (LP #6512675)
- [SDR DALA2019012200396](https://openairdocs.org/sdr/DALA2019012200396.md): Lens · missing · Jan 21, 2019 · N910AT · Boeing 717200 · Emergency Lighting
  > EXIT SIGN FROM OVERWING/AISLE LOCATION MISSING. MAINTENANCE REPLACED THE EXIT SIGN LENS. (LP #5520022)
- [SDR DALA201808064869](https://openairdocs.org/sdr/DALA201808064869.md): Battery Pack · inoperative · Aug 2, 2018 · N910AT · Boeing 717200 · Emergency Lighting
  > THE LEFT AND RIGHT AFT OVER WING EXIT SIGNS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND BATTERY B5-119 IAW AMM 33-51. OPS CHECKED NORMAL.
- [SDR DALA2018020700755](https://openairdocs.org/sdr/DALA2018020700755.md): Sign · broken · Feb 7, 2018 · N910AT · Boeing 717200 · Emergency Lighting
  > EXIT SIGN IN FIRST CLASS IS BROKEN. RE-SECURED EXIT SIGN PER AMM 33-22.
- [SDR DALA2017112108242](https://openairdocs.org/sdr/DALA2017112108242.md): Longeron · damaged · Nov 21, 2017 · N910AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > LONGERON 17L FOUND DAMAGED BEHIND FUSELAGE SKIN. REMOVED SECTION OF THE LONGERON, FABRICATED A 35 INCH SECTION OF REPLACEMENT LONGERON IAW SRM 53-00-05-2R-2, FIG 201, SHEET 1, AND INSTALLED IAW SRM 53-00-05-2R-2, FIG 201. COMPLIED WITH THE PERMANENT REPAIR IA
- [SDR DALA2017100807377](https://openairdocs.org/sdr/DALA2017100807377.md): Lens · loose · Oct 7, 2017 · N910AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT SIGN LENS FOUND LOOSE SECURED THE LENS. OK FOR SERVICE.
- [SDR DALA2017051603896](https://openairdocs.org/sdr/DALA2017051603896.md): Lens · loose · May 15, 2017 · N910AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT COVER DIFFUSER LENS LOOSE AT LOCATION 602. SECURED THE LOOSE LENS. CHECKED OK.
- [SDR DALA2017051103764](https://openairdocs.org/sdr/DALA2017051103764.md): Lens · unsecure · May 10, 2017 · N910AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT DIFFUSER LENS FOUND UNSECURE. SECURED THE LENS.
- [SDR DALA2017042703441](https://openairdocs.org/sdr/DALA2017042703441.md): Power Supply · inoperative · Apr 27, 2017 · N910AT · Boeing 717200 · Emergency Lighting
  > ON SERVICE CHECK, FOUND THE EXIT LIGHTS OVER SEAT 20 OUT. REPLACED THE EMERGENCY LIGHTS BATTERY POWER SUPPLY IAW AMM 33-51. LIGHTS CHECKED GOOD AT THIS TIME.
- [SDR DALA2017040802850](https://openairdocs.org/sdr/DALA2017040802850.md): Scuff Plate · damaged · Apr 7, 2017 · N910AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR SCUFF PLATE DAMAGED. REMOVED AND REPLACED THE SCUFF PLATE IAW ER/A 557273-14, REV 2.
- [SDR DALA2017040802849](https://openairdocs.org/sdr/DALA2017040802849.md): Door Frame · torn · Apr 7, 2017 · N910AT · Boeing 717200 · Fuselage Main, Structure
  > FWD CARGO DOOR FRAME AND SKIN TORN. REPAIRED IAW PRI 557273-14, REV 2, AND ER/A 667273-14, REV ORIGINAL, SECTION 1.
- [SDR DALA2017040802848](https://openairdocs.org/sdr/DALA2017040802848.md): Skin · damaged · Apr 7, 2017 · N910AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FWD CARGO DOOR LOWER FRAME, SKIN DENTED AND CRACKED. REPAIRED IAW PRI 557277-14, REV 1, AND ER/A 557277-14, REV ORIGINAL.
- [SDR DALA2017032002195](https://openairdocs.org/sdr/DALA2017032002195.md): Unknown · odor · Mar 18, 2017 · N910AT · Boeing 717200 · Air Distribution System
  > THE CREW RETURNED THE AIRCRAFT TO THE GATE DUE TO STRONG SULFUR TYPE SMELL AFTER SECOND ENGINE START. AFTER ENGINE SHUTDOWN, SMELL REMAINED AND ACTUALLY GOT STRONGER. CREW REPORTED ODOR OCCURRED AFTER DE-ICING PROCEDURE. FOLLOWED ODI PREVENTION FOR ATA2172. RE
- [SDR DALA2016F00190](https://openairdocs.org/sdr/DALA2016F00190.md): Spoiler · delaminated · Sep 20, 2016 · N910AT · Boeing 717200 · Spoilers
  > DURING UNSCHEDULED MAINTENANCE CHECK LT INBD SPOILER WAS FOUND DELAMINATED.
- [SDR DALA2016110108051](https://openairdocs.org/sdr/DALA2016110108051.md): Skin · corroded · Aug 2, 2016 · N910AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN STA 1002 L-24R - L-25R. CORROSION REPAIRED BY ER/A 547501-14. ACCOMPLISH SECTION II INSPECTIONS EVERY 8000 CYCLES AFTER SECTION I REPAIR.
- [SDR DALA2016080405754](https://openairdocs.org/sdr/DALA2016080405754.md): Skin · corroded · Aug 2, 2016 · N910AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE INTERIOR SKIN AND FINGER DOUBLERS FROM STA 1002 TO STA 1012 BETWEEN LONGERONS 22R AND 26R. BLENDED CORROSION ON INTERNAL SKIN. NOMINAL THICKNESS.063. REMAINING.041. FOUND TO BE OUT OF LIMITS IAW SRM 53-01-01, FIG 103, STA 1005 L25R.
- [SDR DALA2016080205719](https://openairdocs.org/sdr/DALA2016080205719.md): Fitting · corroded · Aug 1, 2016 · N910AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 25R END CAP AND POSSIBLY ON LONGERON 25R FROM STA 1002 TO STA 1022. REPLACED LONGERON 25R END FITTING AT FS 1002 IAW SRM 51-4-05. NO CORROSION NOTED ON LONGERON 25R FS 1002 TO 1022.
- [SDR DALA2016080205718](https://openairdocs.org/sdr/DALA2016080205718.md): Door Frame · corroded · Aug 1, 2016 · N910AT · Boeing 717200 · Fuselage Main, Structure
  > FUSELAGE AFT CARGO LOWER DOOR JAMB HAS NUMEROUS AREAS OF CORROSION FROM THE AFT LOWER STOP FITTING DOWN TO AND AROUND THE FORWARD LOWER STOP FITTING. REPLACED LOWER DOOR JAMB IAW SRM 53-20-15, REPAIR 7.
- [SDR DALA2016073105671](https://openairdocs.org/sdr/DALA2016073105671.md): Former · cracked · Jul 28, 2016 · N910AT · Boeing 717200 · Fuselage Main, Frame
  > LEFT CANTED KEEL FORMERS CRACKED AT STA 674 AND STA 714 ON OTBD END. REPAIR IAW ER/A 545683-14MA, REF ORNRC 69946-0100-0127. REPAIRED LT CANTED KEEL FORMERS AT STA 674, 696, & 714 ON OTBD END IAW ER/A 545683-14MA, TAG 6782.
- [SDR DALA2016073105670](https://openairdocs.org/sdr/DALA2016073105670.md): Longeron · corroded · Jul 27, 2016 · N910AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 23R FROM STA 1002 TO STA 1037. MARKED CHECK LIMITS, REPLACE AS REQUIRED, REF ORNRC 69946-0100-0060. REPLACED LONGERON 23R AT FS 1002 TO FS1043 IAW SRM 51-41-02, PARA D, NOTE 3, 51-41-05, PG 17, NR 8.
- [SDR DALA2016072805620](https://openairdocs.org/sdr/DALA2016072805620.md): Angle · corroded · Jul 27, 2016 · N910AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON CUSP WEB ANGLE IN BOTH FWD AND AFT LOWER CORNERS OF GALLEY SERVICE DOOR. REPAIRED THE ANGLE IAW SRM 53-00-55 REPAIR 3.
- [SDR DALA2016072705587](https://openairdocs.org/sdr/DALA2016072705587.md): Pan · corroded · Jul 26, 2016 · N910AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR JAMB LOWER PAN IS CORRODED AT STOPS, MARKED. REPLACED FWD LOWER CARGO DOOR JAMB PAN SECTION WITH PAN SECTION IAW SRM 51-20-15, REPAIR 6, FIG 201. APPLIED LOG DECAL IAW DPS 900-5-1, NR 04.
- [SDR DALA2016072805621](https://openairdocs.org/sdr/DALA2016072805621.md): Seat Track · corroded · Jul 25, 2016 · N910AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SEAT TRACK RBL 56 BS 200 AND END FITTING CORRODED. FABRICATED NEW SECTION OF SEAT TRACK IAW SRM 51-40-08 AND DWG 5971185.
- [SDR DALA2016072605547](https://openairdocs.org/sdr/DALA2016072605547.md): Cusp Web · corroded · Jul 25, 2016 · N910AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > WEB AT BS 160-200 RBL 56 CORRODED BEYOND LIMITS. REPLACED THE WEB IAW ER/A 547495-14. A NEW CUSP WEB AND SPLICE DOUBLER WERE FABRICATED IAW ER/A 547495-14. THE TRIMMED SECTION WAS CHECKED FOR CRACKS USING HFEC IAW NDTSPM 06-10-01.001 NO DEFECTS FOUND. ALL
- [SDR DALA2016080105674](https://openairdocs.org/sdr/DALA2016080105674.md): Former · cracked · Jul 24, 2016 · N910AT · Boeing 717200 · Fuselage Main, Frame
  > RIGHT CANTED KEEL FORMERS AT STA 674, 696, AND 714 CRACKED ON OTBD END. REPAIR IAW ER/A 545683-14MA, REF ORNRC 69946-0100-0130. REMOVED FORMERS ON RT CANTED KEEL AT STA 674, 696, AND 714. FABRICATED AND INSTALLED DOUBLERS AND FILLERS TO FORMERS IAW ER/A 545
- [SDR DALA2016072505501](https://openairdocs.org/sdr/DALA2016072505501.md): Floor Support · corroded · Jul 24, 2016 · N910AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FLOOR PANEL SUPPORT STRUCTURE STA 215, RBL11 CORRODED. BLENDED CORROSION AND CHECKED LIMITS ON FLOOR PANEL SUPPORT STRUCTURE. NOMINAL THICKNESS IS.080". REMOVED.035", REMAINING IS.045". FOUND OUT OF LIMITS IAW SRM 53-00-00, FIG 103. FABRICATED NEW FLOO
- [SDR DALA2016072305500](https://openairdocs.org/sdr/DALA2016072305500.md): Cusp Web · corroded · Jul 21, 2016 · N910AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB MEMBRANE, STA 200-218 RBL 56-44. CORRODED BEYOND LIMTS. REPLACED RT CUSP MEMBRANE AT STA 210-218, RBL 56-44 IAW SRM 51-41-02, PAR 2. FABRICATED IAW DWG 9936535. THE NEW PART WAS ALODINED IAW PSM 900-2-4-1, 02. THE WEB WAS THEN PRIMED IAW P
- [SDR DALA2016072205470](https://openairdocs.org/sdr/DALA2016072205470.md): Cargo Track · corroded · Jul 21, 2016 · N910AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT AFT CARGO SEAT TRACK, AFT OF CARGO DOOR, HAS CORROSION AND CHAFING, MARKED. RIGHT AFT SEAT TRACK CORRODED BEYOND LIMITS. REPLACED SEAT TRACK AND MATCHED DRILL TO SAMPLE IAW SRM 51-40-08.
- [SDR DALA2016072105449](https://openairdocs.org/sdr/DALA2016072105449.md): Seat Track · corroded · Jul 20, 2016 · N910AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT INBD SEAT TRACK X 22 BS 256-465 HAS THREE NOTED AREAS OF CORROSION. FOUND OUT OF LIMITS IAW SRM 53-20-52 FIG 101. REPAIRED IAW SRM 53-20-52 REPAIR 1 FIG 201.
- [SDR DALA2016071805347](https://openairdocs.org/sdr/DALA2016071805347.md): Longeron · corroded · Jul 17, 2016 · N910AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 24R AND LONGERON 24R END CAP FROM STA 1002 AND STA 1022. REPLACED LONGERON 24R F/S 1002-1022 + FWD END CAP IAW SRM 51-40-05, PG 17, NR 8, SRM 51-41-02, PARA D. NOTE 3, FASTENERS FROM F/S 1002-1022 + SHEAR TIE AT F/S 1002-1022 LT OPEN TO
- [SDR DALA2016071605336](https://openairdocs.org/sdr/DALA2016071605336.md): Cusp Web · cracked · Jul 15, 2016 · N910AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > RT CUSP WEB CRACKED STA 823 BETWEEN 2 RIVETS, RBL 44.5. VIEWED IN LIGHTING HOLE WITH MIRROR. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER IAW SRM 53-00-55, REPAIR NR 4. INSTALLED IAW SRM 51-41-02 AND SRM 53-00-55, REPAIR 4.
- [SDR DALA2016071205258](https://openairdocs.org/sdr/DALA2016071205258.md): Cusp Web · cracked · Jul 11, 2016 · N910AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > ON INSTALLING OTBD RT SEAT TRACK FOUND CUSP WEB CRACKED FROM EOP TRAVELING INBD TO LIGHTNING HOLE AT BS 245. CUT OUT THE DAMAGE & REPAIRED THE CUSP WEB IAW SRM 53-00-55, REPAIR 4.
- [SDR DALA2015100605975](https://openairdocs.org/sdr/DALA2015100605975.md): Battery Pack · inoperative · Oct 6, 2015 · N910AT · Boeing 717200 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY FLOOD LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.
- [SDR DALA2015060303582](https://openairdocs.org/sdr/DALA2015060303582.md): Battery Pack · inoperative · Jun 2, 2015 · N910AT · Boeing 717200 · Emergency Lighting
  > DURING SERVICE CHECK BOTH EXTERNAL EMERGENCY ILLUMINATION LIGHTS WERE INOPERATIVE. APPLIED MEL 33-51-02A AND LATER REPLACED EMERGENCY BATTERY. OPERATION THEN CHECKED NORMALLY. LP 7066591.
- [SDR DALA2015041402757](https://openairdocs.org/sdr/DALA2015041402757.md): Frame · cracked · Apr 13, 2015 · N910AT · Boeing 717200 · Fuselage Main, Frame
  > RT FUSELAGE MAIN FRAME CRACKED AT FS 674. REPLACED FRAME AT 674 IAW AMDS 5310-01436-03B. LP 1902809.
- [SDR DALA2015041402758](https://openairdocs.org/sdr/DALA2015041402758.md): Frame · cracked · Apr 7, 2015 · N910AT · Boeing 717200 · Fuselage Main, Frame
  > RT FUSELAGE MAIN FRAME CRACKED AT STA 715. REPLACED FRAME AT STA 715 IAW AMDS CARD 5310-01436-03B. LP 1902812.
- [SDR DALA1612189581](https://openairdocs.org/sdr/DALA1612189581.md): Fastener · damaged · Jul 15, 2014 · N910AT · Boeing 717200 · Fuselage Main, Structure
  > FUSELAGE, DAMAGED FASTENER AT BS 1152, LONGERON-2L AND 3L /527412-14.
- [SDR SWAA2014071429977](https://openairdocs.org/sdr/SWAA2014071429977.md): Charger · inoperative · Jul 8, 2014 · N910AT · Boeing 717200 · Emergency Lighting
  > LEFT AFT LOWER TAIL CONE EMER LIGHT INOPERATIVE. R & R CHARGER IAW AMM.
- [SDR SWAA2014070729697](https://openairdocs.org/sdr/SWAA2014070729697.md): Light · inoperative · Jul 4, 2014 · N910AT · Boeing 717200 · Emergency Lighting
  > TAIL COMPARTMENT AFT HAND RAIL EMER LIGHT BULB INOPERATIVE. LAMPED LIGHT IAW AMM.
- [SDR SWAA2014070729696](https://openairdocs.org/sdr/SWAA2014070729696.md): Light · inoperative · Jul 3, 2014 · N910AT · Boeing 717200 · Emergency Lighting
  > AFT LOWER EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.
- [SDR SWAA2014070229573](https://openairdocs.org/sdr/SWAA2014070229573.md): Sign · cracked · Jun 27, 2014 · N910AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY LIGHT SIGN ASSEMBLY AT AFT BULKHEAD DOOR CRACKED. R & R LIGHT ASSEMBLY IAW MM.
- [SDR SWAA2014070129539](https://openairdocs.org/sdr/SWAA2014070129539.md): Sign · cracked · Jun 27, 2014 · N910AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY LIGHT SIGN ASSEMBLY AT R1 DOOR CRACKED. R & R SIGN IAW MM.
- [SDR SWAA2014070229572](https://openairdocs.org/sdr/SWAA2014070229572.md): Sign · cracked · Jun 26, 2014 · N910AT · Boeing 717200 · Emergency Lighting
  > ROW 1 ABC, EMER EXIT SIGN CRACKED. R & R SIGN IAW MM.
- [SDR SWAA2014062729453](https://openairdocs.org/sdr/SWAA2014062729453.md): Lens · cracked · Jun 24, 2014 · N910AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT LIGHT LENS ABOVE L2 DOOR CRACKED. R & R LENS IAW MM.
- [SDR SWAA2014062729452](https://openairdocs.org/sdr/SWAA2014062729452.md): Lens · cracked · Jun 24, 2014 · N910AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT LIGHT LENS ABOVE R2 DOOR CRACKED. R & R LENS IAW MM.
- [SDR SWAA2014062729451](https://openairdocs.org/sdr/SWAA2014062729451.md): Lens · cracked · Jun 24, 2014 · N910AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT LIGHT LENS ABOVE R1 DOOR CRACKED. R & R LENS IAW MM.
- [SDR SWAA2014062729450](https://openairdocs.org/sdr/SWAA2014062729450.md): Lens · cracked · Jun 24, 2014 · N910AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT LIGHT LENS ABOVE L1 DOOR CRACKED. R & R LENS IAW MM.
- [SDR SWAA2014062329288](https://openairdocs.org/sdr/SWAA2014062329288.md): Floorboard · damaged · Jun 11, 2014 · N910AT · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD PANEL 211ALF DAMAGED. R & R PANEL IAW SRM.
- [SDR SWAA2014062329287](https://openairdocs.org/sdr/SWAA2014062329287.md): Floor Panel · damaged · Jun 11, 2014 · N910AT · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 221JF DAMAGED. R & R PANEL IAW SRM.
- [SDR SWAA2014061329013](https://openairdocs.org/sdr/SWAA2014061329013.md): Support Bracket · cracked · Jun 9, 2014 · N910AT · Boeing 717200 · Ailerons
  > RIGHT WING AILERON OTBD SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.

Next page: https://openairdocs.org/aircraft/N910AT/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 = 'N910AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N910AT/reports

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