N178US

Service difficulty reports · 347

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

Query with SQL
duckdb -csv -c "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 = 'N178US' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR AALA201905299015Floor Panel · delaminatedAIRCRAFT IN BASE VISIT: DELAMINATED FLOOR PANEL 221EF AT FWD GALLEY AREA (1 EA). REPLACED FLOOR PANEL 221EF AT FWD GALLEY AREA WITH NEW REPLACEMENT MATERIAL AS PER SRM 53-12-00-300-006 PARA 2. FIG. 20106, IRM9701 REV.I.May 24, 2019 · N178US · Airbus A321211 · Fuselage Floor PanelSDR AALA201905299016Floor Panel · delaminatedAIRCRAFT IN BASE VISIT: DELAMINATED FLOOR PANEL 221DF AT FWD GALLEY AREA (1 EA). REPLACED FLOOR PANEL 211DF AT FWD GALLEY AREA WITH NEW REPLACEMENT MATERIAL AS PER SRM 53-12-00-300-006 PARA 2 FIG. 20106 IRM 9701 REV.I.May 24, 2019 · N178US · Airbus A321211 · Fuselage Floor PanelSDR AALA201905299017Floor Panel · delaminatedAIRCRAFT IN BASE VISIT: DELAMINATED FLOOR PANEL 231CF AT FWD GALLEY AREA (1 EA). REPLACED FLOOR PANEL 231CF AT FWD GALLEY AREA WITH NEW REPLACEMENTMATERIAL ASPER SRM 53-12-00-300-006 PARA 2 FIG. 20106 IRM 9701 REV.I.May 24, 2019 · N178US · Airbus A321211 · Fuselage Floor PanelSDR AALA201905239019Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD WET AREA FLOORBEAM BETWEEN FR 12 AND FR 24 AT -Y1292. REPLACED FLOORBEAM PER SRM 51-72-11.May 22, 2019 · N178US · Airbus A321211 · Fuselage Main, Floor BeamSDR AALA201905239018Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY AREA FLOOR PANEL 232EF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.May 22, 2019 · N178US · Airbus A321211 · Fuselage Floor PanelSDR AALA201905239017Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: AFT GALLEY AREA FLOOR PANEL 261BG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.May 22, 2019 · N178US · Airbus A321211 · Fuselage Floor PanelSDR AALA201905239016Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: AFT GALLEY AREA FLOOR PANEL 261AG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.May 22, 2019 · N178US · Airbus A321211 · Fuselage Floor PanelSDR AALA201905159013Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: AFT GALLEY AREA FLOOR PANEL 261PF DELAMINATED. REPAIRED FLOOR PANEL PER SRM 53-02-00-300-013.May 14, 2019 · N178US · Airbus A321211 · Fuselage Floor PanelSDR AALA201906269008Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER41R BETWEEN FRAMES 58 AND 61. REPAIRED THE STRINGER IAW EA 294528.May 12, 2019 · N178US · Airbus A321211 · Fuselage Main, Longeron/StringerSDR AALA201905239026Intercostal · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND FORWARD PASSENGER / CREW DOOR CUTOUT INTERCOSTAL CRACKED AT FR 20 LEFT AND DOOR STOP #7. REPLACED INTERCOSTAL PER SRM 51-72-11.May 8, 2019 · N178US · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201905229023Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR CUTOUT INTERCOSTAL FITTING CRACKED, FR 16 LEFT HAND SIDE AT DOOR STOP #7. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.May 8, 2019 · N178US · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201905229022Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR CUTOUT INTERCOSTAL FITTING CRACKED BETWEEN FR 15 AND FR 16 RIGHT HAND SIDE AT DOOR STOP #7. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.May 8, 2019 · N178US · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201905229019Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT PASSENGER / CREW ENTRY DOOR CUTOUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.May 8, 2019 · N178US · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201906269007Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT WET AREA SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.May 7, 2019 · N178US · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201906069015Structure · gougedAIRCRAFT IN BASE VISIT: RIGHT OUTBOARD TRAILING EDGE FLAP IS DENTED AND GOUGED ON THE UNDERSIDE, (L=6.75" W=6.60" CUT OUT AREA). REPAIRED OUTBOARD TRAILING EDGE FLAP TAB LOWER SURFACE ON RH WING IAW A321 SRM 57-53-00-300-015 AND EA #265175B.May 7, 2019 · N178US · Airbus A321211 · Trailing Edge FlapsSDR AALA201905289014Floorbeam · corrodedAIRCRAFT IN BASE VISIT: CORROSION FLOORBEAM -Y1292 BTW FR12/FR24 AT FWD GALLEY AREA (1EA) L=1.507"X W=1.1875"X D=0.0490" CORRODED AREA. REPLACED FLOORBEAM -Y1292 BTW FR12/FR24 AT FWD GALLEY AREA (1EA) AND FASTENERS IAW SRM 51-72-11, 51-42-11 AND DRAWING D53115May 7, 2019 · N178US · Airbus A321211 · Fuselage Main, Floor BeamSDR AALA201905239025Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOORBEAM BETWEEN FR 64 AND FR 65 AT +Y1292. REPLACED FLOORBEAM PER SRM 51-72-11.May 7, 2019 · N178US · Airbus A321211 · Fuselage Main, Floor BeamSDR AALA201905239024Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN SEAT TRACK BETWEEN FR 12 AND FR 24 AT +Y765 AND S23L. REPLACED SEAT TRACK PER SRM 51-72-11.May 7, 2019 · N178US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201905229021Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN SEAT TRACK BETWEEN FR 12 AND FR 24 AT -Y765 AND S23R. REPLACED SEAT TRACK PER SRM 51-72-11.May 7, 2019 · N178US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201905229020Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD WET AREA FLOORBEAM BETWEEN FR 12 AND FR 24 AT +Y1292. REPLACED FLOORBEAM PER SRM 51-72-11.May 7, 2019 · N178US · Airbus A321211 · Fuselage Main, Floor BeamSDR AALA201906269009Skin · corrodedAIRCRAFT IN BASE MAINTENANCE, CORROSION ON RIGHT WING UPPER SKIN LOWER SURFACE TRAILING EDGE OVERHANG BETWEEN RIB 6 AND RIB 7 AT THE FALSE SPAR BOX ON THE REAR SPAR. REPAIRED SKIN PER EA 294667.May 6, 2019 · N178US · Airbus A321211 · Wing, Plate/SkinSDR AALA201906269006Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE NR 7 HAS EXCESSIVE PLAY AT RIB 11 ON THE VERTICAL STABILIZER. REPLACED HINGE FITING PER AMM 55-36-41-400-001-A.May 6, 2019 · N178US · Airbus A321211 · Rudder StructureSDR AALA2019061439027Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK FLOOR PANEL 211JF DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-12-11-400-001-A.May 6, 2019 · N178US · Airbus A321211 · Fuselage Floor PanelSDR AALA2019061439026Skin · contaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER BETWEEN RIB 6 AND RIB 7 AT 3 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR UPPER SURFACE SKIN PER SRM 55-21-11-300-005.May 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA2019061439024Skin · contaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR LOWER SURFACE SKIN HAS INDICATION OF TRAPPED WATER BETWEEN RIB 8 AND RIB 9 AT 3.5 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR LOWER SURFACE SKIN PER SRM 55-21-11-300-005.May 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA2019061439023Skin · contaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR LOWER SURFACE SKIN HAS INDICATION OF TRAPPED WATER BETWEEN RIB 8 AND RIB 9 AT 4 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR LOWER SURFACE SKIN PER SRM 55-21-11-300-005.May 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA2019061439022Skin · contaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR LOWER SURFACE SKIN HAS INDICATION OF TRAPPED WATER BETWEEN RIB 5 AND RIB 6 AT 3 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR LOWER SURFACE SKIN PER SRM 55-21-11-300-005.May 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906139021Skin · contaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR LOWER SURFACE SKIN HAS INDICATION OF TRAPPED WATER BETWEEN RIB 9 AND RIB 10 AT 3 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR LOWER SURFACE SKIN PER SRM 55-21-11-300-005.May 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA2019061439020Skin · contaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER BETWEEN RIB 8 AND RIB 9 AT 3 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR UPPER SURFACE SKIN PER SRM 55-21-11-300-005.May 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA2019061439019Skin · contaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR LOWER SURFACE SKIN HAS INDICATION OF TRAPPED WATER BETWEEN RIB 6 AND RIB 7 AT 4 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR LOWER SURFACE SKIN PER SRM 55-21-11-300-005.May 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906079015Skin · contaminatedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 62 IN. INBOARD FROM RIB 10 AND 4 FROM TRAILING EDGE ON LH HORIZONTAL STABILIZER (1 EA) (L = 3 IN. W = 1.7 IN. APPROX.), TRAPPED WATER L=3.16" W=2.12"May 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906069018Skin · contaminatedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 7.5 IN. INBOARD FROM RIB 4 AND 5.3 IN. FROM TRAILING EDGE ON LH HORIZONTAL STABILIZER (1 EA) (L = 2.7 IN. W = 1.6 IN. APPROX.). REPAIRED UPPER SKIN LMay 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906069017Skin · contaminatedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 53.5 IN. INBOARD FROM RIB 5 AND 3.5 IN. FROM TRAILING EDGE ON LH HORIZONTAL STABILIZER (1 EA) (L = 3.4 IN. W = 2.2 IN. APPROX.). REPAIRED UPPER SKIN May 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906069016Skin · contaminatedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 13 IN. INBOARD FROM RIB 10 AND 3.5 IN. FROM TRAILING EDGE ON LH HORIZONTAL STABILIZER (1 EA) (L = 2.5 IN. W = 1.7 IN. APPROX). REPAIRED UPPER SKIN ONMay 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906059022Skin · contaminatedTRAPPED WATER INDICATION ON ELEVATOR LOWER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 69 IN. INBOARD OF RIB 10 AND 3.5 IN FROM TRAILING EDGE ON LH HORIZONTAL STABILIZER (1 EA) (L=1.9 IN W=1.3 IN APPROX). REPAIRED LOWER SKIN ON LH ELEVATOR HORIZONTAL STABILIZEMay 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906059023Skin · contaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 7.5 IN. INBOARD FROM RIB 10 AND 4 IN. FROM TRAILING EDGE ON LH HORIZONTAL STABILIZER (1 EA) (L = 2.5 IN. W = 1.7 IN. APPROX.). REPAIRED UPPER SKIN ON LH ELEVATOR HORIZONTAL May 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906059024Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 19.5 INBOARD FROM RIB 10 AND 3.5 IN. FROM TRAILING EDGE ON LH HORIZONTAL STABILIZER (1 EA) (L = 2 IN. W= 1.6 IN. APPROX.). REPAIRED UPPER SKIN ON LH ELEVATOR HORIZONTAL STABMay 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906059025Skin · contaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 33 IN. INBOARD FROM RIB 10 AND 3.5 IN. FROM TRAILING EDGE ON LH HORIZONTAL STABILIZER (1 EA) (L = 2.9 IN W = 1.8 IN. APPROX.) REPAIRED UPPER SKIN ON LH ELEVATOR HORIZONTAL SMay 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906059026Skin · contaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 25 IN. INBOARD FROM RIB 10 AND 4 IN. FROM TRAILING EDGE ON LH HORIZONTAL STABILIZER (1 EA) (L = 2.7 IN. W = 2 IN. APPROX.) TRAPPED WATER L=3.20" W=2.23". REPAIRED UPPER SKINMay 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906059020Floor Panel · delaminatedDELAMINATED FLOOR PANEL 212NF IN COCKPIT (1 EA). REPLACED FLOOR PANEL 212NF IN COCKPIT (1EA) I.A.W AMM 53-12-11-400-001-A THE INSTALLATION OF FLOOR PANEL IS DOCUMENTED IN JOB CARD 26C21053004.May 6, 2019 · N178US · Airbus A321211 · Fuselage Floor PanelSDR AALA201906059019Skin · contaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 18.5 IN. OUTBOARD FROM RIB 5 AND 3.2 IN. FROM TRAILING EDGE ON LH HORIZONTAL STABILIZER (1 EA) (L = 3.8IN. W = 2.6 IN. APPROX). REPAIRED UPPER SKIN ON LH ELEVATOR HORIZONTALMay 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906059017Skin · contaminatedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 4 IN. OUTBOARD FROM RIB 5 AND 3.5 IN. FROM TRAILING EDGE ON LH HORIZONTAL STABILIZER (1 EA) ( L = 4 IN. W = 2.4 IN. APPROX.). REPAIRED UPPER SKIN ON May 6, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906059021Skin · contaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 32 IN. OUTBOARD FROM RIB 5 AND 3.5 IN. FROM TRAILING EDGE ON RH HORIZONTAL STABILIZER (1 EA) (L = 5 IN. W = 2 IN. APPROX). REPAIRED UPPER SKIN ON RH ELEVATOR HORIZONTAL STABMay 5, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906059018Skin · contaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 6.5 IN. INBOARD FROM RIB 4 AND 4 IN. FROM TRAILING EDGE ON RH HORIZONTAL STABILIZER (1 EA) L= (L = 4 IN. W = 1.6 IN. APPROX.). REPAIRED UPPER SKIN ON RH ELEVATOR HORIZONTAL May 5, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906059016Skin · contaminatedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 26.5 IN. OUTBOARD FROM RIB 5 AND 3.5 IN. FROM TRAILING EDGE ON RH HORIZONTAL STABILIZER (1 EA) (L = 2.5IN. W = 2 APPROX.). REPAIRED UPPER SKIN ON RH May 5, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906049034Skin · contaminatedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 69 IN. INBOARD FROM RIB 10 AND 3.2 IN. FROM TRAILING EDGE ON RH HORIZONTAL STABILIZER (1EA) (L= 3.5IN W=3 IN. APPROX). REPAIRED UPPER SKIN ON RH ELEVMay 5, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906049035Skin · contaminatedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 61 IN. OUTBOARD FROM RIB 5 AND 3.5 IN. FROM TRAILING EDGE ON RH HORIZONTAL STABILIZER (1 EA) (L = 4.7 IN W = 2.6 IN. APPROX). REPAIRED UPPER SKIN ON May 5, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906049036Skin · contaminatedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 0.5 IN. OUTBOARD FROM RIB 4 AND 18.5 IN. FROM TRAILING EDGE ON RH HORIZONTAL STABILIZER (1 EA) (L = 3.8IN. W = 1.6 IN APPROX.). REPAIRED UPPER SKIN OMay 5, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906049037Skin · contaminatedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 58.5 INBOARD FROM RIB 10 AND 6.3 IN. FROM TRAILING EDGE ON RH HORIZONTAL STABILIZER (1 EA) (L = 4 IN. W = 1.3 IN). REPAIRED UPPER SKIN ON RH ELEVATORMay 5, 2019 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201906049038Skin · contaminatedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 52.5 IN. OUTBOARD FROM RIB 5 AND 3.2 IN. FROM TRAILING EDGE ON RH HORIZONTAL STABILIZER (1 EA) (L = 5 IN. W = 3 IN. APPROX.).May 5, 2019 · N178US · Airbus A321211 · Elevator, Plate/Skin
Back to N178US