# Service difficulty reports: N676AN, cancelled Oct 3, 2018

A list on [N676AN, cancelled Oct 3, 2018](https://openairdocs.org/deregistered/N676AN-2018-10-03.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 104 reports

- [SDR FOTR20180928033](https://openairdocs.org/sdr/FOTR20180928033.md): Skin · none · Sep 28, 2018 · N676AN · Boeing 757223 · Fuselage Main, Plate/Skin
  > PER NR 254 AND GA-EO-18-001 AFTER REMOVAL OF ANTENNA DOUBLER FOR AIRCELL SYSTEM AT STA 510 BTWN STR27-28R, REPAIR FUSELAGE AS REQ.
- [SDR FOTR20180928032](https://openairdocs.org/sdr/FOTR20180928032.md): Elevator · none · Sep 28, 2018 · N676AN · Boeing 757223 · Elevator Structure
  > PREVIOUS REPAIR FOUND ON LH ELEVATOR LOWER SURFACE, APPROX. 84" FROM OB END. INSPECT AND REPLACE IF FOUND TO BE A TEMPORARY REPAIR. ANNOTATE STATION LOCATIONS AND FINAL DIMENSIONS OF NEW REPAIR.
- [SDR FOTR20180928031](https://openairdocs.org/sdr/FOTR20180928031.md): Skin · none · Sep 28, 2018 · N676AN · Boeing 757223 · Fuselage Main, Plate/Skin
  > PER NR254 AND GA-EO-18-001, AFTER REMOVAL OF ANTENNA DOUBLER FOR AIRCELL SYSTEM AT STA 1350 BTWN STR29R-30, REPAIR FUSELAGE AS REQ.
- [SDR FOTR20180928030](https://openairdocs.org/sdr/FOTR20180928030.md): Skin · dented · Sep 28, 2018 · N676AN · Boeing 757223 · Leading Edge Devices
  > MULTIPLE DENTS FOUND ON #2 SLAT UPPER SURFACE OF AFT WEDGE.
- [SDR FOTR20180928029](https://openairdocs.org/sdr/FOTR20180928029.md): Wedge · dented · Sep 28, 2018 · N676AN · Boeing 757223 · Leading Edge Devices
  > #4 SLAT UPPER SURFACE T/E WEDGE HAS AN OUT OF LIMIT DENT AT 19" FROM I/B END.
- [SDR FOTR20180829027](https://openairdocs.org/sdr/FOTR20180829027.md): Skin · dented · Aug 29, 2018 · N676AN · Boeing 757223 · Horizontal Stabilizer, Plate/Skin
  > DENT AND GOUGE FOUND ON THE LOWER SURFACE OF THE RT HORIZONTAL STABILIZER APPROXIMATELY 14 INCHES AFT OF AUX SPAR, 112 INCHES FROM INBD END.
- [SDR FOTR20180829026](https://openairdocs.org/sdr/FOTR20180829026.md): Skin · damaged · Aug 29, 2018 · N676AN · Boeing 757223 · Fuselage Main, Plate/Skin
  > AFTER REMOVAL OF ANTENNA DOUBLER AT BS 1430 BETWEEN STRINGERS 1L AND 2L, REPAIR THE SKIN.
- [SDR FOTR20180829025](https://openairdocs.org/sdr/FOTR20180829025.md): Skin · dented · Aug 29, 2018 · N676AN · Boeing 757223 · Fuselage Main, Plate/Skin
  > MULTIPLE DENTS FOUND ON THE SKIN PANEL BETWEEN STRINGERS 3L & 5L, BS 1787-1862.
- [SDR FOTR20180829023](https://openairdocs.org/sdr/FOTR20180829023.md): Skin · corroded · Aug 29, 2018 · N676AN · Boeing 757223 · Trailing Edge Flaps
  > LEFT OTBD FLAP UPPER AREA INSIDE FLAP WAS CORRODED.
- [SDR FOTR20180829022](https://openairdocs.org/sdr/FOTR20180829022.md): Skin · gouged · Aug 29, 2018 · N676AN · Boeing 757223 · Fuselage Structure (General)
  > GOUGE ON INTERNAL DOUBLER AT B.S. 298, UNDER STR.20R
- [SDR FOTR20180829021](https://openairdocs.org/sdr/FOTR20180829021.md): Skin · dented · Aug 29, 2018 · N676AN · Boeing 757223 · Fuselage Main, Plate/Skin
  > A DENT WAS FOUND ON AIRCRAFT SKIN, BS 1389, STRINGERS 25L & 26L.
- [SDR FOTR20180807020](https://openairdocs.org/sdr/FOTR20180807020.md): Skin · dented · Aug 7, 2018 · N676AN · Boeing 757223 · Leading Edge Devices
  > NR 1 SLAT UPPER SURFACE WEDGE HAS AN OUT OF LIMITS DENT, LOCATED 14.5 INCHES FROM THE OTBD END AND 2 INCHES FROM T/E.
- [SDR FOTR20180807019](https://openairdocs.org/sdr/FOTR20180807019.md): Skin · dented · Aug 7, 2018 · N676AN · Boeing 757223 · Leading Edge Devices
  > NR 1 SLAT LOWER INTERIOR WEDGE AREA HAS AN OUT OF LIMIT DENT LOCATED 43 INCHES FROM THE OTBD END AND 4.5 INCHES FROM THE T/E.
- [SDR FOTR20180806018](https://openairdocs.org/sdr/FOTR20180806018.md): Skin · dented · Aug 6, 2018 · N676AN · Boeing 757223 · Leading Edge Devices
  > NR 1 SLAT INTERIOR WEDGE HAS A DENT THAT WAS OUT OF LIMITS. 53 INCHES FROM THE OTBD END AND 5.3 INCHES FROM THE T/E.
- [SDR FOTR20180806016](https://openairdocs.org/sdr/FOTR20180806016.md): Skin · dented · Aug 6, 2018 · N676AN · Boeing 757223 · Leading Edge Devices
  > NR 5 SLAT UPPER SURFACE, AFT WEDGE HAD A DENT THAT WAS OUT OF LIMITS. 8 INCHES FROM OTBD END, AND 2.75 INCHES FROM AFT EDGE.
- [SDR FOTR20180806015](https://openairdocs.org/sdr/FOTR20180806015.md): Skin · dented · Aug 6, 2018 · N676AN · Boeing 757223 · Leading Edge Devices
  > NR 9 SLAT UPPER SURFACE AFT WEDGE HAD A DENT THAT WAS OUT OF LIMITS, 5.75 INCHES FROM INDB END, AND.075 INCH FROM AFT EDGE.
- [SDR FOTR20180806014](https://openairdocs.org/sdr/FOTR20180806014.md): Skin · debonded · Aug 6, 2018 · N676AN · Boeing 757223 · Leading Edge Devices
  > NR 5 SLAT UPPER SURFACE HAD A DISBONDED DENT THAT WAS OUT OF LIMITS, 47.5 INCHES FROM THE INBD END, AND 5 INCHES FROM THE T/E.
- [SDR FOTR20180806013](https://openairdocs.org/sdr/FOTR20180806013.md): Skin · dented · Aug 6, 2018 · N676AN · Boeing 757223 · Leading Edge Devices
  > LT WING NR 1 SLAT INTERIOR WEDGE WAS DENTED ON THE LOWER SURFACE, 22 INCHES FROM THE OTBD END, AND 4 INCHES FROM T/E.
- [SDR FOTR20180806012](https://openairdocs.org/sdr/FOTR20180806012.md): Skin · dented · Aug 6, 2018 · N676AN · Boeing 757223 · Leading Edge Devices
  > NR 2 SLAT UPPER SURFACE T/E WEDGE HAD TWO DENTS OVERLAPPING AT 73 INCHES FROM INBD END AND 6 INCHES FROM T/E, FOUND TO BE OUT OF LIMITS.
- [SDR FOTR20180806007](https://openairdocs.org/sdr/FOTR20180806007.md): Panel · punctured · Aug 6, 2018 · N676AN · Boeing 757223 · APU Cowling/Containment
  > APU COMPARTMENT, RIGHT ELEVATOR INDEX PLATE HARDWARE PUNCTURING THROUGH INTERIOR COMPOSITE PANEL.
- [SDR FOTR20180806006](https://openairdocs.org/sdr/FOTR20180806006.md): Frame · gouged · Aug 6, 2018 · N676AN · Boeing 757223 · Fuselage Main, Frame
  > MAIN CABIN, RT SIDE BS 1640 FRAME WAS GOUGED AT STRINGER 6R.
- [SDR FOTR20180806005](https://openairdocs.org/sdr/FOTR20180806005.md): Skin · dented · Aug 6, 2018 · N676AN · Boeing 757200 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STABILZER RT SIDE SKIN WAS DENTED APPROXIMATELY 5 INCHES FROM L/E OF AUX SPAR AND VSS 230.
- [SDR FOTR20180806004](https://openairdocs.org/sdr/FOTR20180806004.md): Fill Port · corroded · Aug 6, 2018 · N676AN · Boeing 757223 · Fuel Storage
  > LEFT WING FUEL FILL PORT LANDING CORRODED.
- [SDR FOTR 20180806003](https://openairdocs.org/sdr/FOTR%2020180806003.md): Skin · dented · Aug 6, 2018 · N676AN · Boeing 757223 · Fuselage Main, Plate/Skin
  > DENT FOUND ON FUSELAGE SKIN AT BS 1677, STRINGERS 25L TO 26L.
- [SDR FOTR20180802002](https://openairdocs.org/sdr/FOTR20180802002.md): Skin Panel · dented · Aug 2, 2018 · N676AN · Boeing 757223 · Vertical Stabilizer, Plate/Skin
  > DENT FOUND ON VERTICAL STABILIZER RIGHT SURFACE 12"AFT OF AUX SPAR FSS 231.0.
- [SDR AALA201708079004](https://openairdocs.org/sdr/AALA201708079004.md): Warning Light · inoperative · Aug 3, 2017 · N676AN · Boeing 757223 · Door Warning System
  > AIRCRAFT WAS NOT GROUNDED. SLIDE LIGHT AT 1L, INOPERATIVE. REPLACED L1 DOOR LIGHT PER FIM 25-66-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
- [SDR AALA201708039007](https://openairdocs.org/sdr/AALA201708039007.md): Light · inoperative · Jul 31, 2017 · N676AN · Boeing 757223 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. REPLACED 15D SEAT MOUNTED LIGHT PER AMM 33-51-11. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
- [SDR AALA20170613002](https://openairdocs.org/sdr/AALA20170613002.md): Web · corroded · Jun 13, 2017 · N676AN · Boeing 757223 · Cargo/Baggage Doors
  > CORROSION ON INSIDE OF FORWARD CARGO DOOR AT LOWER WEB ON FORWARD AND AFT ENDS. REMOVED AND REPLACED WEB.
- [SDR AALA20170104013](https://openairdocs.org/sdr/AALA20170104013.md): Girt Bar · dirty · Dec 31, 2016 · N676AN · Boeing 757223 · Emergency Equipment
  > AIRCRAFT NOT GROUNDED. L4 DOOR EVACUATION SLIDE GIRT BAR ARM LEVER IS DIFFICULT TO MOVE. REMOVED DEBRIS AND LUBRICATED GIRT BAR DOOR SILL IAW AMM 52-10-00. OPERATIONAL CHECK GOOD.
- [SDR AALA20161109009](https://openairdocs.org/sdr/AALA20161109009.md): Cover · loose · Nov 7, 2016 · N676AN · Boeing 757223 · Escape Slide
  > L3 DOOR SLIDE COVER IS LOOSE. SECURED THE COVER CENTER LATCH STRAP IAW 25-66-01. OPERATIONAL CHECK GOOD.
- [SDR AALA20151103012](https://openairdocs.org/sdr/AALA20151103012.md): Filter · dirty · Oct 29, 2015 · N676AN · Boeing 757223 · Air Distribution System
  > AFTER TAKEOFF & FOR 10 - 15 MINUTES, ODOR WAS NOTED BY FLIGHT ATTENDANT & PILOTS. SMELLED LIKE MOLD OR MUSTY. DISSIPATED AFTER HIGHER HEAT LEVELS WERE SELECTED IN ALL 3 ZONES, 78 - 79 DEGREES INDICATED IN COMPARTMENT ZONES. REPLACED LT RECYCLE FAN AIR FILTE
- [SDR AALA20150825006](https://openairdocs.org/sdr/AALA20150825006.md): Plate · corroded · Aug 25, 2015 · N676AN · Boeing 757223 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT LOWER SPLICE PLATE OF HORIZONTAL STABILIZER IS CORRODED BEYOND LIMITS. REPAIRED SPLICE PLATE IAW EA 253610.
- [SDR AALA20150818022](https://openairdocs.org/sdr/AALA20150818022.md): Deck Plate · corroded · Aug 18, 2015 · N676AN · Boeing 757223 · Fuselage Miscellaneous Structure
  > MAIN FLOOR DECK PLATE HAS MULTIPLE AREAS OF CORROSION FROM STATION 1681 TO 1720. R & R ENTIRE AFT DECK SHEAR PLATE IAW SRM 51-40-02, AARD 51-00-05-1 & DWG 148N2301.
- [SDR AALA20150814005](https://openairdocs.org/sdr/AALA20150814005.md): Bulkhead · cracked · Aug 14, 2015 · N676AN · Boeing 757223 · Nacelle/Pylon, Bulkhead/Firewall
  > RIGHT PYLON AFT BULKHEAD HOLE NR 4 ON AFT FACE HAS A CRACK INDICATION IN THE ALUMINUM LAYER AT APPROX THE 2:00 O CLOCK POSITION. ENLARGED FASTENER HOLE IN THE ALUMINUM BULKHEAD ONLY TO 0.650 & INSTALLED ALUMINUM FREEZE PLUG & REAMED TO 0.4995. INSTALLED NEW
- [SDR AALA20150817005](https://openairdocs.org/sdr/AALA20150817005.md): Cusp Web · corroded · Jul 27, 2015 · N676AN · Boeing 757223 · Fuselage Miscellaneous Structure
  > CORROSION ON TOP SURFACE OF CUSP AT STATION 1719 & LBL 56. R & R CUSP SECTION IAW DWG 146N8722 & 146N3700.
- [SDR AALA20150312002](https://openairdocs.org/sdr/AALA20150312002.md): Light · inoperative · Mar 11, 2015 · N676AN · Boeing 757223 · Emergency Lighting
  > FORWARD EMER LIGHT ON SEAT 5E INOPERATIVE. REPLACED FWD EMER LIGHT ASSEMBLY AT SEAT 5E IAW AMM 33-51-01. SYS CHECKED NORMAL.
- [SDR AALA20141117015](https://openairdocs.org/sdr/AALA20141117015.md): Module · defective · Nov 17, 2014 · N676AN · Boeing 757223 · Stabilizer Position Indicating
  > TAKEOFF ABORTED. MASTER WARNING LIGHT ILLUMINATED & WARNING HORN SOUNDED DURING TAKEOFF AT 110 KNOTS. RED STABILIZER MSG APPEARED MOMENTARILY. ACCOMPLISHED FIM 27-09-00-815-811, FIM 27-09-00-815-803 & CARD 05-96-28 WITH NO FAULTS FOUND. FLIGHT DATA RECORDE
- [SDR AALA20140629002](https://openairdocs.org/sdr/AALA20140629002.md): Light · inoperative · Jun 29, 2014 · N676AN · Boeing 757223 · Emergency Lighting
  > LEFT NR 4 DOOR EMER SLIDE LIGHT FAILED TO TEST. REPLACED LAMP FOR LT NR 4 DOOR EMER SLIDE LIGHT. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140629001](https://openairdocs.org/sdr/AALA20140629001.md): Light · inoperative · Jun 28, 2014 · N676AN · Boeing 757223 · Emergency Lighting
  > LEFT NR 4 DOOR EXTERIOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR EXTERIOR EMER LIGHT. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140316017](https://openairdocs.org/sdr/AALA20140316017.md): Light · inoperative · Mar 15, 2014 · N676AN · Boeing 757223 · Emergency Lighting
  > OVERHEAD HATCH LIGHT AT ROW 17DEF INOPERATIVE. REPLACED LAMP FOR OVERHEAD HATCH LIGHT AT ROW 17DEF. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140316016](https://openairdocs.org/sdr/AALA20140316016.md): Light · inoperative · Mar 15, 2014 · N676AN · Boeing 757223 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT AT SEAT 5E INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT AT SEAT 5E. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140316015](https://openairdocs.org/sdr/AALA20140316015.md): Light · inoperative · Mar 15, 2014 · N676AN · Boeing 757223 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT AT SEAT 2E INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT AT SEAT 2E. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140316014](https://openairdocs.org/sdr/AALA20140316014.md): Light · inoperative · Mar 15, 2014 · N676AN · Boeing 757223 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT AT SEAT 16C INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT AT SEAT 16C. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140316013](https://openairdocs.org/sdr/AALA20140316013.md): Placard · worn · Mar 15, 2014 · N676AN · Boeing 757223 · Placards and Markings
  > ARROW AT RT NR 1 DOOR WORN. REPLACED DECAL AT RT NR 1 DOOR. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140316012](https://openairdocs.org/sdr/AALA20140316012.md): Placard · worn · Mar 15, 2014 · N676AN · Boeing 757223 · Placards and Markings
  > ARROW AT ROW 18DEF FOR EMERGENCY EXIT WORN. REPLACED DECAL FOR EMERGENCY EXIT AT 18DEF. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140316011](https://openairdocs.org/sdr/AALA20140316011.md): Light · inoperative · Mar 15, 2014 · N676AN · Boeing 757223 · Emergency Lighting
  > LEFT NR 4 DOOR SLIDE LIGHT INOPERATIVE. REPLACED LAMP FOR SLIDE LIGHT AT LT NR 4 DOOR. OPERATIONS CHECKED NORMAL.
- [SDR AALA20131020001](https://openairdocs.org/sdr/AALA20131020001.md): Bottle · no test · Oct 19, 2013 · N676AN · Boeing 757223 · Escape Slide
  > EMERGENCY ESCAPE SLIDE TEST DOES NOT TEST IN POSITION 2. REPLACED OFF WING ESCAPE SLIDE SYSTEM PRESSURE BOTTLE. OPERATIONS CHECKED NORMAL.
- [SDR AALA20130919011](https://openairdocs.org/sdr/AALA20130919011.md): Fan · malfunctioned · Sep 19, 2013 · N676AN · Boeing 757223 · Air Distribution Fan
  > ADZ INFLIGHT SJO-MIA CREW REPORTED SMOKE ODOR IN THE CABIN & COCKPIT. EMERGENCY DECLARED FLIGHT DIVERTED ADZ LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PLACARDED RT CABIN RECIRCULATION FAN IAW MEL 21-1A. REPLACED FAN AT LAX ON 09/20/2013. SYS
- [SDR AALA20130312011](https://openairdocs.org/sdr/AALA20130312011.md): Access Door · gouged · Mar 12, 2013 · N676AN · Boeing 757223 · Fuselage Miscellaneous Structure
  > ACCESS DOOR 113AL HAS GOUGES IN BOTH LEFT DOOR STOP CASTINGS. ACCOMPLISHED REPAIR PER EA B757-53-028722.
- [SDR AALA20130312010](https://openairdocs.org/sdr/AALA20130312010.md): Floor Support · corroded · Mar 12, 2013 · N676AN · Boeing 757223 · Fuselage Miscellaneous Structure
  > MAIN CABIN RIGHT NUMBER 4 DOOR SILL AREA FLOOR SUPPORT STRUCTURE CORRODED AROUND FASTENER HOLES FROM BODY STATIONS 1660 TO 1680. REMOVED AND REPLACED SUPPORT STRUCTURE AT STATIONS 1660 TO 1680 PER SRM 51-40-02-0G.

Next page: https://openairdocs.org/deregistered/N676AN-2018-10-03/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N676AN' AND deregistration_id = 'N676AN-2018-10-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N676AN-2018-10-03/reports

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