Accident · substantial damage
Apr 5, 2019 · Atlanta, GAfailure of the tug driver to give way to the taxiing airplane.
- Damage
- Substantial
- Report
- DCA19CA146
From NTSB records; matched by N-number.Read NTSB report (search CAROL for DCA19CA146)
This N-number isn't registered right now. Below is its last known registration, canceled Sep 6, 2019.
Safety record in brief:1 NTSB accident (substantial damage, Apr 2019)No ADs since 1998 matched239 service difficulty reports
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failure of the tug driver to give way to the taxiing airplane.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for DCA19CA146)
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.
No ADs published since 1998 matched this airframe or engine model.
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.
AWR. IN REFERENCE AMDS 5530-01045-05 STEP 2 LOOSE FASTENERS WAS FOUND ON VERTICAL STABILIZER LEADING EDGE STA ZFS: 52.26. FASTENERS ON VERTICAL STABILIZER LEADING EDGE STA ZFS: 52.26 WERE REPLACED PER ETI-88-19-028 REV.2 AND ERA 576759-14AD REV. ORIGINAL. SECTION I PERMANENT REPAIR. REPAIR…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING WAKE UP CHECK LIST AMP INDICATION NO SHOW. ELECTRICAL CABLE P44A24 AND C/B WERE FOUND BURNED, CABLE AND C/B B1-171 WERE REPLACED PER MD88 SWPM 20-10-06 AMD AMM 24-00-00. TEST WAS PERFORMED PER AMM 24-30-02 TEST OK. (LP4883756)
From FAA Service Difficulty Reports; matched by N-number and serial number.STABILIZERS VERTICAL FIXED LE SKIN, ZFS. ELONGATED HOLES. DTA MONITOR INSPECTION LOG REFERENCE ER/A 576759-14AD SECTION II REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS. DISCONTINUE REVENUE SERVICE ON OR BEFORE THE NEXT 24 MONTHS PENDING A DAMAGE TOLERANCE AND FATIGUE REVIEW. (LP1004366)
From FAA Service Difficulty Reports; matched by N-number and serial number.INITIAL INSPECTION: CRACK ON DOUBLER REPAIR OF LEADING EDGE BTW XRS= 190 AND XRS= 210 LT WING. DOUBLER REPAIR OF LEADING EDGE BTW XRS= 190 AND XRS= 210 LT WING WAS REPLACED PER ETI-88-19-026 REV. ORIGINAL AND ER/A 532516-14 REV A SECTION III. (LP1001760)
From FAA Service Difficulty Reports; matched by N-number and serial number.INITIAL INSPECTION: CORROSION AT SPACER OF THE CENTER LOWER CARGO DOOR JAMB BEAM. (CORROSION LEVEL 2): SPACER WAS REPLACED PER SRM 53-05 FIG 123A (SHEET1). (LP1000032)
From FAA Service Difficulty Reports; matched by N-number and serial number.INITIAL INSPECTION : WEAR ON REPAIR DOUBLER AT EXT USELAGE SKIN FWD PASSENGER DOOR ( L1 ) PROJECTION LONG 16/ 15L AT FUSELAGE. REPAIR DOUBLER AT EXT FUSELAGE SKIN FWD PASSENGER DOOR, PROJECTION LONG 16/ 15L WAS REPLACED PER SRM 52-05 PAR. 17 FIG. 20A. (LP0997037)
From FAA Service Difficulty Reports; matched by N-number and serial number.WEAR AT UPPER PREVIOUS REPAIR SKIN ON INTERNAL VANE GUIDE AT OUTBOARD FLAP RT WING. INTERNAL VANE GUIDE AT OUTBOARD FLAP RT WING WAS REPAIRED PER SRM 57-03D. (LP0995827)
From FAA Service Difficulty Reports; matched by N-number and serial number.INITIAL INSPECTION: CORROSION AT SPACER OF THE AFT LOWER CARGO DOOR JAMB BEAM. (CORROSION LEVEL 2): SPACER OF THE AFT LOWER CARGO DOOR JAMB BEAM WAS REPLACED PER SRM 53-05 FIG. 123. (LP0990137)
From FAA Service Difficulty Reports; matched by N-number and serial number.23D SEAT EMERGENCY LIGHT OUT. R/R BULB AT SEAT 23D PER STANDARD PRACTICE. (LP4807909)
From FAA Service Difficulty Reports; matched by N-number and serial number.FOUND CRACK AT STA. 1474 LEFT SIDE FWD OF TAILCONE SLIDE HANDLE. REPAIRED PER SRM 53-01 FIG 2 SHEET 3. (LP5088564)
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 239 reports.