Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Jun 2023)17 ADs may apply190 service difficulty reports
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A fatigue fracture of the upper lock link that initiated along scratch features on the lower surface at the parting line of the forged aluminum component. Contributing to the accident was the overhaul facilities noncompliance with Service Bulletin 717-32-002.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA23FA339)
A failure of the left power control distribution unit (PCDU).
From NTSB records; matched by serial number.Read NTSB report (search CAROL for NYC03FA067)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2025-21-05 | Landing Gear | Jan 2, 2026 | Airframe (717-200)Serial numbers per Boeing Alert Requirements Bulletin 717-32A0043 RB, dated February 12, 2025 |
| 2025-02-07 | Navigation | Mar 17, 2025 | Airframe (717-200)Only with: Collins GLU-2100 MMR P/N 822-2532-100 with software version earlier than COL4C-0087-0003 installed; MD-11/MD-11F modified by STC ST01895WI, 717-200 by STC ST04416AT, 747-400/-400F by STC ST01892WI, 757 by STC ST04436AT, 767 by STC ST04436AT or ST01883WI. |
| 2024-21-01 | Wings | Nov 7, 2024 | Airframe (717-200) |
| 2024-20-02 | Fuselage | Oct 21, 2024 | Airframe (717-200) |
| 2023-12-15 | Navigation | Jun 21, 2023 | Airframe (717-200) |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2021-12-12 | Wings | Jul 29, 2021 | Airframe (717-200) |
| 2021-02-16 | Ice and rain protection | Mar 30, 2021 | Airframe (717-200) |
| 2018-10-08 | Stabilizers | May 31, 2018 | Airframe (717-200)Serial numbers per Boeing Alert Service Bulletin 717-55A0012, Revision 1, dated April 11, 2018 |
| 2017-01-03 | Standard practices/structures | Mar 14, 2017 | Airframe (717-200) |
| 2015-02-05 | Navigation | Mar 5, 2015 | Airframe (717-200) |
| 2014-05-22 | Fuselage | Apr 15, 2014 | Airframe (717-200) |
| 2013-19-22 | Fuselage | Nov 6, 2013 | Airframe (717-200) |
| 2012-12-09 | Horizontal Stabilizer Structure | Jul 23, 2012 | Airframe (717-200) |
| 2006-10-14 | McDonnell Douglas Model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 Series… | Jun 21, 2006 | Airframe (717-200)Serial numbers per Boeing Service Bulletin 717-52-0007, Revision 1 (for Model 717-200 airplanes). Only with: All DC-9, MD-80, MD-88 and MD-90-30 airplanes; Model 717-200 airplanes only as identified in Boeing Service Bulletin 717-52-0007, Revision 1. |
| 2004-08-02 | McDonnell Douglas Model 717-200 Airplanes | May 19, 2004 | Airframe (717-200)Serial numbers per Boeing Service Bulletin 717-55-0003, dated June 18, 2002 |
| 2004-03-21 | McDonnell Douglas Model 717-200 Airplanes | Mar 17, 2004 | Airframe (717-200)Serial numbers per Boeing Service Bulletin 717-55-0005, dated June 27, 2002 |
| 2001-18-11 | McDonnell Douglas Model 717 Series Airplanes | Oct 1, 2001 | Airframe (717-200)Serial numbers per Boeing Alert Service Bulletin 717-27A0016, including Appendix, dated April 9, 2001 |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
FOUND METAL STRIP DISCONNECTED ON RIGHT WING LEADING EDGE, COMPLIED WITH ER/A 485300- 14. (9085798) (AIRCRAFT GROUNDED).
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACK WAS FOUND ON INNER/OUTER PAN BEAM 2 AND INNER PAN BEAM 1 FWD EDGE AT AFT CARGO DOOR. SUMMARY OF NRC 00578: INNER/OUTER PAN BEAM 2 AND INNER PAN BEAM 1 FWD EDGE AT AFT CARGO DOOR WAS REPAIRED PER PRI 624376-14 REV 2 AND ERA 624376-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A…
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACK WAS FOUND ON INNER PAN AT AFT CARGO DOOR AT STOP FITTING ON BEAM 5 AFT EDGE. SUMMARY OF NRC 00577: INNER PAN ON BEAM 5 AFT EDGE OF AFT CARGO DOOR WAS REPAIRED PER ER/A 566665-14 REV A SECTION II: PERMANENT REPAIR AND PRI 566665-14 REV 4. ASSOCIATED ER/A 14-566665 ADDED FOR AC 9514. (LP…
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACK ON OUTER PAN BTW BEAM 1 AND 2 (AFT EDGE) OF FWD CARGO DOOR WAS FOUND. SUMMARY OF NRC 00552: OUTER PAN AND INNER PAN BTW BEAM #1 AND BEAM #2 (AFT EDGE) AT FWD CARGO DOOR WERE REPAIRED PER ER/A 624433-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 624433-14 REV 2. ASSOCIATED ER/A…
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACK ON PAN NEXT TO AFT HINGE DOOR (UPPER AREA) AT FWD CARGO DOOR. SUMMARY OF NRC 00193: PAN NEXT TO AFT HINGE DOOR (UPPER AREA) OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0866764)
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACKS (2 EA) WERE FOUND ON INNER PAN AT AFT CARGO DOOR STOP FITTING ON BEAM 1 STA Y=990. SUMMARY OF NRC 00589: INNER PAN ON AFT SIDE BETWEEN STOP #1 AND STOP #2 AT AFT CARGO DOOR WAS REPAIRED PER ER/A 624383-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 624383-14 REV 3. (LP #0860120)
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACKS (2 EA) ON OUTER PAN IN BEAM 5 AT AFT CARGO DOOR FWD AND AFT EDGES. SUMMARY OF NRC 00111: DAMAGED AREA OF OUTER PAN IN BEAM 5 AT AFT CARGO DOOR FWD AND AFT EDGES WERE REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 6 REPAIR 6. (LP #0857625)
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACK WAS FOUND ON BEAM 5 AND INNER PAN (FWD EDGE) AT AFT CARGO DOOR. SUMMARY OF NRC 00574: BEAM 5 AND INNER PAN (FWD EDGE) AT AFT CARGO DOOR. WERE REPAIRED PER PRI 624316-14 REV 3 AND ERA 624316-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-624316 ADDED FOR AC 9514. (LP #0851459)
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION ON INNER SKIN PANEL FROM STA Y=657 TO Y=636 BTW L29L AND L29R, STA Y=588 L30 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00183: CORROSION LEVEL 2. INNER SKIN PANEL FROM STA Y=657 TO Y=636 BTW L29L AND L29R, STA Y=588 L30 AT FWD CARGO COMPARTMENT WAS REPAIRED PER PRI 624284-14 REV 2 AND ER/A…
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION ON FRAME BTW STA Y=1022 L28L TO L28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00177: CORROSION LEVEL 2. FRAME BTW STA Y=1022 L28L TO L28R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3, REPAIR 3. PERFORM A DETAIL VISUAL INSPECTION 25,000 CYCLES AFTER…
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 190 reports.