Safety record in brief:1 NTSB accident (Oct 2009)17 ADs may apply218 service difficulty reports
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The captain's excessive maneuver in response to a traffic alert and collision avoidance system (TCAS) alert, which resulted in a serious injury to a flight attendant. Contributing to the accident was the operator's inadequate TCAS training and guidance.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA10LA041)
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.
SEVERAL EMERGENCY LIGHTS DO NOT TURN ON, ALONG CPAX INCLUDING DOORS AND CEILING PANELS ALSO 2 UPPER LIGHTS ON AFT ACCESORIES COMPARTMENT. CONNECTOR P1-1217 AND LINE ( C9318-51-18) OF (L2-787) AND LINE (C9318-64-20) OF (L2-506) WERE FOUND LOOSE AND WAS CONNECTED CORRECTLY. ALL LIGTH OK. (1572526)…
From FAA Service Difficulty Reports; matched by N-number and serial number.ATB, CREW REPORTED CABIN ODOR IN AFT CABIN ON TAKEOFF CLIMB. BORESCOPE BOTH ENGINES, NO DEFECTS NOTED. INSPECTED THE BOTH PACKS COALESCER BAGS AND FOUND THE HOUSING DIRTY. PERFORMED HIGH POWER RUNS WITH SNIFFER, NTF.
From FAA Service Difficulty Reports; matched by N-number and serial number.RETURNED TO STL DUE TO BURNT OIL SMELL AT 300FT AFTER GEAR RETRACTION. UNABLE TO DUPLICATE ODOR AT GATE RUNNING APU OR ENGINES. GATHERING PARTS AND P-TRACK FROM CARGO TO BEGIN FURTHER EVALUATION. FOUND GLYCOL IN RAM AIR INLET. REPLACED COALESCER BAGS AND DUCT BURN OUT. NO SMELL NOTED.(7585196)
From FAA Service Difficulty Reports; matched by N-number and serial number.PASSENGER EXIT SIGN IS MISSING THE WORD "EXIT". MISSING FROM LIGHT NEAREST CLOSET. MAINTENANCE FOUND THAT THE SIGN HAD BEEN INSTALLED BACKWARDS. ADJUSTED FWD CABIN EXIT SIGN PER B717 AMM 33-51. (LP #4601783)
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION ON RH CUSP ANGLE BTW STA Y=160-169 AND STA Y=200 AT PAX CABIN. SUMMARY OF NRC 00489: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=160-169 AND STA Y=200 AT PAX CABIN WAS REPAIRED PER ER/A 616043-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-616043 ADDED FOR AC 9564. (LP…
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION ON FRAME FROM STA 1022 LONGERON 30 CORDENATED X=-4 TO X=4. SUMMARY OF NRC 00708: CORROSION LEVEL 2. FRAME FROM STA 1022 LONGERON 30 CORDENATED X=-4 TO X=4 WAS REPAIRED PER B717 SRM 53-20-07-2R-3, 51-41-02-0G, AND 51-41-05-0G. PERFORM AN INITIAL VISUAL INSPECTION AT 25,000 CYCLES THEN…
From FAA Service Difficulty Reports; matched by N-number and serial number.TWO DISBONDS WERE FOUND OF: 0.500 IN LENGTH .X 0.500 IN. WIDTH. ON DENTS LOWER SKIN AT LH CENTER FLAP VANE 26.500 IN. INBOARD EDGE, 12.500 IN. TRAILING EDGE AND 28.000 IN. INBOARD EDGE, 12.500 IN. TRAILING EDGE. (IN REFERENCE JOB# 020-0001) SUMMARY OF NRC 00653: AFT MOVABLE FLAP VANE LEFT WING WAS…
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACK ON SKIN STA Y=370 BTW L20 AND L22 APROX AT FWD DOOR CARGO COMPARMENT. SUMMARY OF NRC 00227: SKIN STA Y=370 BTW L20 AND L22 APROX AT FWD DOOR CARGO COMPARMENT WAS REPAIRED PER PRI 616337-14 REV 0 AND ERA 616337-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-616337 ADDED FOR AC…
From FAA Service Difficulty Reports; matched by N-number and serial number.WEAR ON RIBS (3 EA) BETWEEN STA XIS 174 TO XIS 186 INSIDE FIXED LEADING-EDGE AT LH WING. SUMMARY OF NRC 00621: RIBS (3 EA) BETWEEN STA XIS 174 TO XIS 186 INSIDE FIXED LEADING-EDGE AT LH WING WERE REPAIRED PER ERA 616112-14 REV ORIG SECTION 1 PERMANENT REPAIR. ASSOCIATED ERA 14-616112 ADDED FOR AC…
From FAA Service Difficulty Reports; matched by N-number and serial number.ELONGATED HOLES ON WEB BTW STA 370 TO 360 AND LONGERONS 24 RH TO 26 RH AT CUT OUT FORWARD CARGO COMPARTMENT DOOR (CCD). SUMMARY OF NRC 00131: WEB BTW STA 370 TO 360 AND LONGERONS 24 RH TO 26 RH AT CUT OUT FORWARD CARGO COMPARTMENT DOOR (CCD) WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2…
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 218 reports.