Safety record in brief:1 NTSB accident (substantial damage, Oct 2012)17 ADs may apply119 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
An obstruction (a sleeve of cups) that lodged under the catering truck brake pedal, which prevented the driver from stopping the truck before it struck the parked airplane.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN13LA004)
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.
SHIP 9554 -ATO- THE FLIGHT CREW ABORTED THE TAKEOFF AT 130 KTS DUE TO THE #1 PRIMARY FLIGHT DISPLAY AND MULTI-FUNCTIONAL DISPLAY BLANKING OUT. CORRECTIVE ACTION: MAINTENANCE FOUND 2 EACH COAX CABLES LOOSE ON VIA #1 SPLITTERS AND REPLACED BOTH DISPLAY UNITS. (LP #6196222)
From FAA Service Difficulty Reports; matched by N-number and serial number.DOOR R1 EXIT SIGN IS MISSING. MAINTENANCE REPLACED AND INSTALLED THE MISSING LENS COVER IAW B717 AMM 33-51. LIGHT OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4579222)
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACKS ON LH CUSP WEB AROUND RING BTW STA 652 AND 655. SUMMARY OF NRC 00668: LH CUSP WEB AROUND RING BTW STA 652 AND 655 WAS REPAIRED PER B717 SRM 53-00-55-2R-4 PAR 5. B. FIGURE 211. (LP #2863892 )
From FAA Service Difficulty Reports; matched by N-number and serial number.-AD- CENTER WING BOX LOWER SKIN XCW=20 TO XCW=42 REAR SPAR TO STRINGER #12 HAS CORROSION AND ELONGATED HOLES. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 14MAR23. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR LONGER THAN 24 MONTHS FROM…
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION WAS FOUND ON FWD PASSENGER DOOR STAIRWELL INTERNAL STRUCTURE IN REF NRC 2060-1001. SUMMARY OF NRC 00572: CORROSION LEVEL 2. FWD PASSENGER DOOR STAIRWELL WAS REPLACED WITH SERVICEABLE STAIRWELL PER B717-200 AMM 52-63-01. TOOL USED CALIBRATED STD DUE DATE 25MAY23. (LP #2663000)
From FAA Service Difficulty Reports; matched by N-number and serial number.SKIN PANELS BTW STA 954 TO STA 974 LONG 30 TO R29 ARE CORRODED OUT OF LIMITS. WITH ORIGINAL THICKNESS OF 0.071 IN. AND THE MAXIMUM REMOVED MATERIAL FOUND IS 0.033 IN. THEREFOR AREA IS OUT OF LIMITS IN REF NRC 00192 AT AFT CARGO (C2). SUMMARY OF NRC 00512: CORROSION LEVEL 2. SKIN DOUBLER BTW STA…
From FAA Service Difficulty Reports; matched by N-number and serial number.SEVERAL DENTS ON AFT MOVABLE FLAP VANE (LOWER SURFACE) AT LH WING (AI). SUMMARY OF NRC 00160: DENTS (26 EAS) ON AFT MOVABLE FLAP VANE (LOWER SURFACE) AT LH WING WERE FOUND AND EVALUATED AS FOLLOWS, WHERE, L=LENGTH, W=WIDTH, Y=DEPTH, AND W/Y MUST BE 10 OR MORE, BEING THE MOST CRITICAL DENT: DENT…
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION ON FLOOR SUPPORT 4 (EA) STA Y=218 AND X=0 TO X=13.5, STA Y=200 X=16 TO X=-6, STA Y=200-210 X=-10.5 (CPAX)(W1). SUMMARY OF NRC 00433: CORROSION LEVEL 2. FLOOR SUPPORT 4 (EA) STA Y=218 AND X=0 TO X=13.5, STA Y=200 X=16 TO X=-6, STA Y=200-210 X=-10.5 WERE REPLACED PER B717-200 SRM…
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACK ON PAN, FWD/UPPER INNER SIDE NEAR TO BEAM 5 OF FWD CARGO COMPARTMENT DOOR. (C1) SUMMARY OF NRC 00541: PAN FWD/UPPER OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1 FIGURE 201. (LP #2640421)
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION ON SEAT TRACKS STA Y=200-237 X=-22, STA Y=200-218 X=-44.5 AND STA Y=200 X=22 (CPAX)( W1). SUMMARY OF NRC 00425: CORROSION LEVEL 2. CORROSION WAS REMOVED ON SEAT TRACKS STA Y=200-237 X=-22, STA Y=200-218 X=-44.5 AND STA Y=200 X=22 PER B717-200 SRM 51-10-04-0G PAR. 26 C(1), UT. THICKNESS…
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 119 reports.