# Service difficulty reports: N958AT, cancelled Apr 30, 2025

A list on [N958AT, cancelled Apr 30, 2025](https://openairdocs.org/deregistered/N958AT-2025-04-30.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 · 208 reports

- [SDR DALA2019120307004](https://openairdocs.org/sdr/DALA2019120307004.md): Battery Pack · inoperative · Dec 3, 2019 · N958AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS ARE OUT IN THE FIRST CLASS & COMFORT PLUS SECTIONS OF THE CABIN. MAINTENANCE REPLACED THE BATTERY PACK, B5-227, IAW AMM 33-51-03. OPS CHECKED NORMAL. (LP #6626493)
- [SDR DALA2019090905218](https://openairdocs.org/sdr/DALA2019090905218.md): Power Supply · inoperative · Sep 8, 2019 · N958AT · Boeing 717200 · Emergency Lighting
  > ALL EMERGENCY LIGHT IN CEILING AFT OF ROW 23 DO NOT TEST. MAINTENANCE REPLACED THE CABIN EMERGENCY LIGHT POWER SUPPLY POS B5-231 AND REPLACED THE COMPLETE EMERGENCY POWER SUPPLY ASSEMBLY POS B5-260 PER AMM 33- 51. ALSO, RELAMPED BURNT BULBS AS REQUIRED. OPERAT
- [SDR DALA2019061703592](https://openairdocs.org/sdr/DALA2019061703592.md): Tire · failed · Jun 15, 2019 · N958AT · Boeing 717200 · Tire
  > THE CREW RETURNED TO THE DEPARTURE AIRPORT FOLLOWING THE #2 TIRE FAILURE ON TAKEOFF ROTATION. CORRECTIVE ACTION: MAINTENANCE REPLACED BOTH THE #1 AND #2 TIRES. THERE WAS SOME DAMAGE FOUND ON LMLG WHEEL WELL DOWN LOCK CONDUIT, LMLG DOWN/UP LOCK SENSORS, AND LML
- [SDR DALA2019032901985](https://openairdocs.org/sdr/DALA2019032901985.md): Battery Pack · discharged · Mar 29, 2019 · N958AT · Boeing 717200 · Emergency Lighting
  > THE FORWARD DOORS AND FIRST ROW OF OVERWING EMERGENCY EXIT SIGNS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE EMERGENCY LIGHTS IAW AMM 33-51. THE LIGHTS NOW OPERATE NORMALLY. (LP #5786770)
- [SDR DALA2019030601503](https://openairdocs.org/sdr/DALA2019030601503.md): Skin · damaged · Jan 13, 2019 · N958AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > ABRASION TO THE FUSELAGE SKIN; STATION 427-434, FORWARD CARGO DOOR CUT-OUT (LOWER CORNER, AFT). REMOVED ALL PAINT, PRIMER, AND SEALANT IN AREA. REMOVED NEGLIGIBLE MATERIAL. TOTAL AREA AFFECTED IS H=17.0" W=15.250". U/T CHECKED PER NDT SPM 04-10-00 FOUND ORIGIN
- [SDR DALA2019030601502](https://openairdocs.org/sdr/DALA2019030601502.md): Door Frame · damaged · Jan 13, 2019 · N958AT · Boeing 717200 · Fuselage Main, Structure
  > DAMAGE TO FWD CARGO DOOR CUT-OUT LOWER EDGE AT STATION 408. INSTALLED DOUBLER AND TRIPLER REPAIR PER ER/A 574411-14 REV ORG. SECTION II. INSTALLED NEW SCUFF PLATE AND FILLERS. (LP #0901653)
- [SDR DALA2018112306745](https://openairdocs.org/sdr/DALA2018112306745.md): Bottle · low pressure · Nov 22, 2018 · N958AT · Boeing 717200 · Escape Slide
  > TAIL CONE SLIDE BOTTLE IN THE RED. REMOVED SLIDE S/N 1277 & INSTALLED SLIDE S/N 1399 PER AMDS WORK CARD 2561-9006. (LP5175880)
- [SDR DALA2017081406170](https://openairdocs.org/sdr/DALA2017081406170.md): Lens · damaged · Aug 11, 2017 · N958AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED. REPAIRED THE LENS. OK FOR SERVICE.
- [SDR DALA2016092606848](https://openairdocs.org/sdr/DALA2016092606848.md): Longeron · damaged · Sep 24, 2016 · N958AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > LEFT FUSELAGE LONGERON L26 DAMAGED BETWEEN Y351 AND Y370. REMOVED DAMAGED SECTION, FABRICATED NEW STR FROM FACTORY SPLICE POINT Y380-Y408 TO NEW POINT Y351-Y370. OK TO TREAT AND PAINT. TREATED AND PAINTED IAW P/S 900-2-4, NR 2. OK TO INSTALL LONGERON L26 B
- [SDR DALA2016071805437](https://openairdocs.org/sdr/DALA2016071805437.md): Support · cracked · Jul 18, 2016 · N958AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CRACKED BULKHEAD DIVISOR SUPPORT, STA Y=655, X=22Z=-10 AT FORWARD CARGO COMPARTMENT. BULKHEAD DIVISOR SUPPORT STA Y=655, X=22 Z=-10 WAS REPAIRED WITH ER/A 547883-14, REV ORIGINAL AND ETI-17-16-093. CRACK 0.187" WEIGHT REPAIR, PARTS 0.32LB. ASSOCIATED ER/A 0
- [SDR DALA2016071805349](https://openairdocs.org/sdr/DALA2016071805349.md): Pan · cracked · Jul 17, 2016 · N958AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON OUTER PAN STA Y=954, BEAM 1 FORWARD EDGE AT AFT CARGO COMPARTMENT DOOR, C2, CARD 11, ZONE 810. PAN WAS REPAIRED IAW ETI-17-16-081 AND ER/A 547860-14, REV ORIGINAL. LONGERON CRACK 0.128".
- [SDR DALA2016071805348](https://openairdocs.org/sdr/DALA2016071805348.md): Beam · cracked · Jul 17, 2016 · N958AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKED BEAM 1 ON FORWARD EDGE OF AFT CARGO COMPARTMENT STA Y=954, REF CARD 11, ZONE 810, CARD 45 ZONE 810. BEAM 1 WAS REPAIRED IAW ETI-17-16-081 REV 2 AND ER/A 547860-14, REV ORIGINAL. LONG CRACK 0.156".
- [SDR DALA2016071805346](https://openairdocs.org/sdr/DALA2016071805346.md): Beam · cracked · Jul 17, 2016 · N958AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKED DOOR JAMB BEAM STA Y=47, RT SIDE AT NLG WW. DOOR JAMB BEAM WAS REPAIRED. ER/A 547858-14, REV ORIGINAL.
- [SDR DALA2016071705345](https://openairdocs.org/sdr/DALA2016071705345.md): Fitting · cracked · Jul 17, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED CLIP AT STA Y=1152 BETWEEN LONGERONS 3R/2R. CLIP WAS REPLACED IAW ER/A 547861-14 REV ORIGINAL.
- [SDR DALA2016071705344](https://openairdocs.org/sdr/DALA2016071705344.md): Skin · worn · Jul 17, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > WORN RT WING LOWER SKIN BETWEEN STA SXR 69 AND XRS 111.500. REPAIR OF WORN AREA AT RT WING LOWER SKIN WAS PERFORMED WITH ER/A 547869-14, REV ORIGINAL.
- [SDR DALA2016071705343](https://openairdocs.org/sdr/DALA2016071705343.md): Door Frame · corroded · Jul 16, 2016 · N958AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON LOWER DOOR JAMB FROM STA Y=954 TO Y=994 AT AFT CARGO COMPARTMENT, SM, C2, CARD 27, ZONE 810. DUE TO EXCESIVE CORROSION WAS REPLACED IAW SRM 53-20-15, FIG 201, 51-41-05, AND 51-41-02. RII COMPLETED.
- [SDR DALA2016071705342](https://openairdocs.org/sdr/DALA2016071705342.md): Skin · cracked · Jul 16, 2016 · N958AT · Boeing 717200 · Cargo/Baggage Doors
  > WEAR AND CRACK ON OUTER SKIN STA Y=972 BETWEEN BEAM 1 AND 2 JUST ABOVE OF HANDLE RELEASE AT AFT CARGO COMPARTMENT DOOR. SKIN STA Y=972 BETWEEN BEAM 1 AND 2 JUST ABOVE OF HANDLE RELEASE WAS REPAIRED IAW SRM 52-30-01, FIG 201, LENGTH CRACK 0.300".
- [SDR DALA2016071705341](https://openairdocs.org/sdr/DALA2016071705341.md): Longeron · corroded · Jul 16, 2016 · N958AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > EXCESSIVE CORROSION ON LONGERON 630 BETWEEN STA 960-1010, IN REF CARD 10, ZONE 180. SECTION OF LONGERON WAS REPLACED IAW SRM 53-20-05, REPAIR 1, 51-41-05, 51-40-08, AND 51-10-04, PAR 15, 21, 26, AND 37. RII COMPLETED.
- [SDR DALA2016071605340](https://openairdocs.org/sdr/DALA2016071605340.md): Channel · cracked · Jul 15, 2016 · N958AT · Boeing 717200 · Landing Gear Doors
  > CRACKED FORWARD CHANNEL STA Y=757 AT RT MLG DOOR LOWER SECTION SM, MLG, CARD 1, ZONE 720. CHANNEL WAS REPAIRED IAW ETI-17-16-077 REV 1 AND ER/A 547857-14, REV ORIGINAL.
- [SDR DALA2016071605339](https://openairdocs.org/sdr/DALA2016071605339.md): Pan · cracked · Jul 15, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED PAN BETWEEN BEAM 7/8, STA 161.3 AT FWD ENTRY DOOR, CARD 18, ZONE 820. PAN WAS REPAIRED IAW 717, ETI-17-16-073, REV 1 AND ER/A 547853-14, REV ORIGINAL.
- [SDR DALA2016071605335](https://openairdocs.org/sdr/DALA2016071605335.md): Stop Fitting · cracked · Jul 15, 2016 · N958AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON DOOR STOP FITTING STA, Y=994, BEAM 3 AT AFT CARGO COMPARTMENT DOOR. DOOR STOP FITTING STA Y=994, BEAM 3 AT AFT CARGO COMPARTMENT DOOR WAS REPLACED IAW SRM 51-41-01 AND 51-41-05, IPC 52-33-01-01, FIG 01.
- [SDR DALA2016071605334](https://openairdocs.org/sdr/DALA2016071605334.md): Angle · cracked · Jul 15, 2016 · N958AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON ANGLE STA Y=994, INNER SIDE BEAM 3 AT AFT CARGO COMPARTMENT DOOR. CRACKED ANGLE STA Y994 WAS REMOVED AND NEW ANGLE WAS INSTALLED IAW SRM 51-41-05. PARA 8, LONG CRACK 0.35".
- [SDR DALA2016071605333](https://openairdocs.org/sdr/DALA2016071605333.md): Skin · worn · Jul 15, 2016 · N958AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > WEAR ON FUSELAGE SKIN IN LONGERON 20RT BETWEEN STA Y=520-526, SM, CARD 27, ZONE 110. DAMAGE WAS REPAIRED IAW ETI-17-16-084, REV 1 AND ER/A 547867-14, REV ORIGINAL. RII COMPLETED.
- [SDR DALA2016071605332](https://openairdocs.org/sdr/DALA2016071605332.md): Skin · worn · Jul 15, 2016 · N958AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > WEAR ON FUSELAGE SKIN IN LONGERON 21RT BETWEEN STA Y=503-508,SM, CARD 28, ZONE 110. WEAR ON FUSELAGE SKIN IN LONGERON 21RT BETWEEN STA Y=503-508 OUT OF LIMITS. ORIGINAL THICKNESS 0.050" REMAINING THICKNESS 0.035", DAMAGE WAS REPAIRED IAW ETI-17-16-084, REV 1
- [SDR DALA2016071505398](https://openairdocs.org/sdr/DALA2016071505398.md): Pan · cracked · Jul 14, 2016 · N958AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON INNER PAN STA Y=427 BEAM 1 AT FWD CARGO COMPARTMENT DOOR, SM, C1, CARD 33, ZONE 810. INNER PAN WAS REPAIRED IAW SRM 52-30-02, REPAIR 1, FIG 1, FIG 201, LONG CRACK 1.312". RII COMPLETED.
- [SDR DALA2016071505296](https://openairdocs.org/sdr/DALA2016071505296.md): Access Panel · damaged · Jul 14, 2016 · N958AT · Boeing 717200 · Nacelle/Pylon, Plate/Skin
  > ELONGATED HOLE AND TOOL MARKS ON LOWER ACCESS 440 INBD AT RT PYLON SM, E/P, CARD 40, ZONE 000. TOOL MARKS AND ELONGATED HOLE WERE REPAIRED IAW SRM 54-00-00, FIG 201, SRM 51-10-04, PAR 15, 21.
- [SDR DALA2016071505294](https://openairdocs.org/sdr/DALA2016071505294.md): Access Panel · corroded · Jul 14, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON FUEL ACCESS PLATE 520JB COUNTERSINK. 2EA IN REF ORNRC 64, ACFT ZONE 000, CARD 110, ZONE 000, CORROSION WAS REMOVED IAW SRM 54-10-01, COUNTERSINK WERE MEASURED WITH 0.610", 0.607", AND 0.610". ADJACENT HOLES THEREFORE IS OUT OF LIMITS IAW SRM 57-
- [SDR DALA2016071505293](https://openairdocs.org/sdr/DALA2016071505293.md): Intercostal · cracked · Jul 14, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BETWEEN Y=617 TO Y=636 X=0 AT CEILING AREA OF FWD CARGO COMPARTMENT. C1, SM, CARD 26, ZONE 120 CRACK ON INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00, FIG 201, CRACK LENGTH 1.093".
- [SDR DALA2016071505292](https://openairdocs.org/sdr/DALA2016071505292.md): Longeron · corroded · Jul 14, 2016 · N958AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > EXCESSIVE CORROSION ON LONGERON 30 BETWEEN STA 218 TO 237 AT FWD CARGO COMPARTMENT IN REF CARD 15, ZONE 120, CARD 45, ZONE 120. DUE TO EXCESSIVE DAMAGED SECTION OF LONGERON 30 BETWEEN STA 150 TO 227 WAS REPLACED IAW SRM 53-10-05, 51-41-02, AND 51-41-05.
- [SDR DALA2017010500099](https://openairdocs.org/sdr/DALA2017010500099.md): Access Panel · corroded · Jul 13, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON FUEL ACCESS PLATE 620PB COUNTERSINK. (2EA) CORROSION ON FUEL ACCESS PLATE 620PB COUNTERSINK WAS REMOVED AND MEASURE AND FOUND TWO HOLES OUT OF LIMITS.608" AND.613". THEREFORE WERE REPAIRED WITH BUSHINGS PER SRM 57-10-01.
- [SDR DALA2017010500098](https://openairdocs.org/sdr/DALA2017010500098.md): Access Panel · corroded · Jul 13, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON FUEL ACCESS PLATE 520GB COUNTERSINK. (2EA) CORROSION ON FUEL ACCESS PLATE 520GB COUNTERSINK WAS REMOVED AND MEASURE AND FOUND TWO HOLES OUT OF LIMITS.603" AND.606". THEREFORE WAS REPAIRED WITH BUSHINGS PER SRM 57-10-01.
- [SDR DALA2017010500097](https://openairdocs.org/sdr/DALA2017010500097.md): Access Panel · corroded · Jul 13, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON FUEL ACCESS PLATE 620QB COUNTERSINK. (1EA) CORROSION ON FUEL ACCESS PLATE 620QB COUNTERSINK WAS REMOVE AND MEASURED AND FOUND ONE HOLE OUT OF LIMITS.609". THEREFORE WAS REPAIRED WITH BUSHING PER SRM 57-10-01.
- [SDR DALA2017010500096](https://openairdocs.org/sdr/DALA2017010500096.md): Access Panel · corroded · Jul 13, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON FUEL ACCESS PLATE 620LB COUNTERSINK. (2EA) CORROSION ON FUEL ACCESS PLATE 620LB COUNTERSINK WAS REMOVED AND MEASURED AND FOUND TWO HOLES OUT OF LIMITS.608" AND.613". THEREFORE WAS REPAIRED WITH BUSHINGS PER SRM 57-10-01.
- [SDR DALA2016110108049](https://openairdocs.org/sdr/DALA2016110108049.md): Access Panel · corroded · Jul 13, 2016 · N958AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > CORROSION ON DORSAL FIN JUST ON SETTLEMENT AREA OF ACCESS PANEL 370 AL. FABRICATED NEW AND REPLACED IAW SRM 51-41-02, 51-20-09, 51-10-04 PAR 15 AND 21, AND DWG 5911432 REV "CF".
- [SDR DALA2017010500095](https://openairdocs.org/sdr/DALA2017010500095.md): Access Panel · corroded · Jul 12, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON SETTLEMENT AND COUNTERSINK LT FUEL TANK ACCESS PLATE 520FT. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 520FT WAS REMOVED AND MEASURED AND 4 COUNTERSINK WERE FOUND OUT OF LIMITS.664".667".665".670" THEREFORE WERE REPAIRED
- [SDR DALA2016110108048](https://openairdocs.org/sdr/DALA2016110108048.md): Access Panel · corroded · Jul 12, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 520HB. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 520HB WERE REMOVED AND MEASURED AND FOUND OUT OF LIMIT WITH 3 ADJACENT HOLES 0.563", 0.558", 0.555" THEREFORE WAS REPLACED PER S
- [SDR DALA2016110108047](https://openairdocs.org/sdr/DALA2016110108047.md): Access Panel · corroded · Jul 12, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 520LB. CORROSION ON FUEL ACCESS PLATE 520LB WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 HOLES ADJACENT 0.553", 0.553", 0.553" THEREFORE WAS REPLACED PER SRM 51-10-04 AN
- [SDR DALA2016110108046](https://openairdocs.org/sdr/DALA2016110108046.md): Access Panel · corroded · Jul 12, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK FUEL ACCESS PLATE 620GB. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE NR 620GB WERE REMOVED AND MEASURED AND FOUND OUT OF LIMIT WITH 3 HOLES ADJACENT 0.540", 0.560", 0.560" THEREFORE WAS REPLACED PER SRM 51-10-04
- [SDR DALA2016110108045](https://openairdocs.org/sdr/DALA2016110108045.md): Access Panel · corroded · Jul 12, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 620HB. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 620HB WERE REMOVED AND MEASURED AND FOUND OUT OF LIMITS WITH 3 HOLES ADJACENT "0.556" "0.556" "0.556" THEREFORE WAS REPLACED PER
- [SDR DALA2016071305263](https://openairdocs.org/sdr/DALA2016071305263.md): Beam · cracked · Jul 12, 2016 · N958AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKED FWD EDGE BEAM NR 7 AT L1 DOOR. BEAM WAS REPAIRED IAW SRM 52-10-02 REPAIR 13 FIGURE 202.
- [SDR DALA2016071205262](https://openairdocs.org/sdr/DALA2016071205262.md): Frame · cracked · Jul 12, 2016 · N958AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED FRAME BS 693 BETWEE1 LONGERONS 26 & 27R. THE FRAME WAS REPLACED.
- [SDR DALA2016110108042](https://openairdocs.org/sdr/DALA2016110108042.md): Access Panel · corroded · Jul 11, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620JB. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620JB WERE REMOVED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES.555".545".545" THEREFORE WAS REPLACED PER SRM 51-10-
- [SDR DALA2016110108041](https://openairdocs.org/sdr/DALA2016110108041.md): Access Panel · corroded · Jul 11, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620MB. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 620MB WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED MAX DIAMETER ALLOWED IS 0.532" AND MAX DIAMETER MEASURE IS 0.58" IN 3 HOLES ADJACENT THE
- [SDR DALA2016110108040](https://openairdocs.org/sdr/DALA2016110108040.md): Access Panel · corroded · Jul 11, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 520EB. CORROSION ON COUNTERSINK WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.535" 0.554" AND.540" IAW SRM 57-10-01 MAGNETIC DRIPLESS FUEL MEASURING STI
- [SDR DALA2016110108039](https://openairdocs.org/sdr/DALA2016110108039.md): Access Panel · corroded · Jul 11, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 520MB. CORROSION ON FUEL ACCESS PLATE WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED ON COUNTERSINK AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.554" 0.551" AND 0.549" IAW SRM 57-10-01. MAGNETIC DRI
- [SDR DALA2016110108038](https://openairdocs.org/sdr/DALA2016110108038.md): Access Panel · corroded · Jul 11, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620EB. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 620 EB WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED MAX DIAMETER ALLOWED IS 0.532 AND MAX DIAMETER MEASURED IS 0.565 IN 3 HOLES ADJACENT TH
- [SDR DALA2016071205261](https://openairdocs.org/sdr/DALA2016071205261.md): Skin · cracked · Jul 11, 2016 · N958AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL FUSELAGE SKIN BS 1022 BETWEE1 LONGERONS 3 - 14L. THE SKIN WAS REPAIRED IAW ER/A 547827-14.
- [SDR DALA2016071205260](https://openairdocs.org/sdr/DALA2016071205260.md): Skin · cracked · Jul 11, 2016 · N958AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL FUSELAGE SKIN BS 1037 BETWEEN LONGERONS 13 & 14L. THE SKIN WAS REPAIRED IAW ER/A 547828-14.
- [SDR DALA2016103107968](https://openairdocs.org/sdr/DALA2016103107968.md): Access Panel · corroded · Jul 10, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON FUEL ACCESS PANEL COUNTERSINK & SETTLEMENT AREA. THE ACCESS PANEL CANNOT BE REPAIRED UNDER CONDITIONS I AND II THEREFORE WAS REPLACED IAW SRM 57-10-01 STEP 5, C(1).
- [SDR DALA2016103107967](https://openairdocs.org/sdr/DALA2016103107967.md): Access Panel · corroded · Jul 10, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON FUEL ACCESS PANEL COUNTERSINK & SETTLEMENT AREA. THE ACCESS PANEL CANNOT BE REPAIRED UNDER CONDITIONS I AND II THEREFORE WAS REPLACED IAW SRM 57-10-01 STEP 5, C(1).

Next page: https://openairdocs.org/deregistered/N958AT-2025-04-30/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 = 'N958AT' AND deregistration_id = 'N958AT-2025-04-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N958AT-2025-04-30/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.