Safety record in brief:1 NTSB incident (Jan 2003)17 ADs may apply223 service difficulty reports
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the flight crew's failure to follow the checklist and detect an out of trim condition prior to takeoff.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX03IA098)
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 DAMAGE AFT OF AFT CARGO DOOR OPENING, COMPLIED WITH ER/A 637189-14. (9197562) (AIRCRAFT GROUNDED).
From FAA Service Difficulty Reports; matched by N-number and serial number.TAIL CONE HAS MULTIPLE LIGHTNING STRIKES BEYOND ALLOWABLE LIMITS. REPLACED TAIL CONE IAW AMDS W/C 5352-4013. (9204003) (AIRCRAFT GROUNDED)
From FAA Service Difficulty Reports; matched by N-number and serial number.UFC/DE- TRAILING EDGE FLAPS LOCKED OUT ON APPROACH. LEADING EDGE SLATS EXTENDED NORMALLY. FOUND FLAP CONTROL VALVE CONTROL ROD BOLT BROKEN/MISSING. REPLACED SAME. OPS CHECK GOOD. (8360108) (AIRCRAFT GROUNDED)
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING ACCOMPLISHMENT OF ERA 633150-14AD PRI REV 0 STEP 15 FOUND 7 EA UNINSPECTABLE HOLES IN UPPER MLG SUPPORT DOUBLER AND TE PANEL LE. HOLES ARE NUMBERED UNK 1-7. COMPLIED WITH ERA 633274-14 (1536155) (AIRCRAFT GROUNDED)
From FAA Service Difficulty Reports; matched by N-number and serial number.WHILE PERFORMING AMDS 5720-01103-01B. INSPECTION FOUND A CRACK AT APPROX STA XRS= 170REAR SPAR. COMPLIED WITH ER/A- 628659-14AD REV. ORIGINAL (1215975)
From FAA Service Difficulty Reports; matched by N-number and serial number.SHIP 9594 ER/A 628659-14AD REV ORIGINAL REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. CORRECTIVE ACTION: COMPLIED WITH ERA 628659-14AD REV ORIGINAL REP INSPECTION II. (1215579)
From FAA Service Difficulty Reports; matched by N-number and serial number.NUMBER 2 LT SLAT ATTACH POINT INSPECTION, SLAT DRIVE TRACK NR 5 CHAFED WING STRUCTURE ON INBD AT EDGE. REPAIRED ERA 628327-14 REV. (1143308)
From FAA Service Difficulty Reports; matched by N-number and serial number.EXISTING REPAIR FOUND THAT IMPACTS INSPECTION ACCOMPLISHMENT. REPAIR INVESTIGATION REQUIRED PRIOR TO FURTHER FLIGHT. FOUND AT RT WING REAR SPAR INSPECTION AREA DURING ACCOMPLISHMENT OF AA EM 5720-01103. REPAIR PER ER/A 624368-14AD (1143045)
From FAA Service Difficulty Reports; matched by N-number and serial number.-AD- CORROSION FOUND DURING INSPECTION OF RH WING AFT LOWER SKIN. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT PER INSPECTION FC5720-01103. SUMMARY SEE NRC 004-0001:5720-01103- 01B/001 00001: COMPLIED WITH PRI 624368-14AD REV 0, PRI 624368-14AD REV 1, PRI 624368-14AD…
From FAA Service Difficulty Reports; matched by N-number and serial number.EXFOLIATING CORROSION FOUND ON RIGHT WING REAR SPAR LOWER CAP AT APPROXIMATELY STATION XRS=164. (6925752)
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 223 reports.