Airbus A320-211

Service difficulty reports · 5,271

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'A320211'
  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 CA110722004Windshield · crackedIN THE CLIMB THROUGH F250, THE CAPTAIN`S WINDSCREEN CRACKED. A PAN-PAN WAS CALLED AND THE FLIGHT RETURNED WHERE AN OVERWEIGHT LANDING OF APPROX 46.0 WAS CARRIED OUT. NO ADVERSE PASSENGER REACTION WAS OBSERVED.Jul 21, 2011 · Airbus A320211 · Flight Compartment WindowsSDR CA110721002Flap System · failedCREW ADVISED FLIGHT DISPATCH VIA THE VHF THAT THEY HAD A FLAP/SLAT FAIL AFTER TAKEOFF. FLIGHT CONTINUED ON TO DESTINATION. OPERATION TESTED ON FLAP SLAT SYS AND ALSO PERFORMED SYS TEST ON MCDU, NO EICAS MSG, NO PREVIOUS HISTORY, CONSIDERED SERVICEABLE.Jul 20, 2011 · Airbus A320211 · Trailing Edge Flap Control SystemSDR DALA1144073227Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHTS INOPERATIVE AT DIFFERENT LOCATION SEAT (13 - 16, 18 - 20 AND24 - 26). MAINTENANCE REPLACED AFT LEFT EMERGENCY POWER SUPPLY AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Jul 20, 2011 · N327NW · Airbus A320211 · Emergency LightingSDR CA110708017Control Unit · malfunctionedAFTER DEPARTURE, THE FLIGHT CREW RECEIVED AN EICAS MESSAGE "AVIONICS SMOKE." THE FLIGHT CREW ELECTED TO RETURN. THE LANDING WAS APPROX 6000 KGS OVER THE MAXIMUM STRUCTURAL LANDING WEIGHT. CFR WAS ON STANDBY AS A PRECAUTION. MX DID PERFORM A BRIEF INSP PRIORJul 8, 2011 · Airbus A320211 · Smoke DetectionSDR CA110621003Fuel Feed · malfunctionedWHILE TAXIING TO DEPART FROM STATION THE CREW REPORTED AN AUTO FUEL FEED FAULT AND RETURNED TO THE GATE. AS THE ACFT WAS RETURNING TO THE GATE GROUND PERSONNEL REPORTED FUEL LEAKING FROM THE RT WING TANK. NO EMERGENCY WAS DECLARED. AFTER ENGINE START AND TAJun 17, 2011 · Airbus A320211 · Aircraft Fuel Distribution SystemSDR CA110621002Acm · failedFLIGHT RETURNED TO STATION DUE SMOKE IN THE CABIN. NO EMERGENCY WAS DECLARED AND THE LANDING WEIGHT WAS BELOW MAXIMUM. FOUND NR2 PACK INOP. NR2 PACK INOP SUSPECT NR 2 ACM WEAK INLET & EXAUST AIRFLOW WEAK. REPLACED ACM IAW AMM 21-52-21, OPS TEST CARRIED OUTJun 17, 2011 · Airbus A320211 · Cabin Cooling SystemSDR CA110620006Actuator · failedSLAT FAIL ON APPROACH - FLIGHT DECLARED AN EMERGENCY WITH ATC AS A PRECAUTION - LANDING WAS NORMAL - NO PASSENGER IMPACT TSM 27-81-00-810-0810 CARRIED OUT. FOUND LT NR 6 (FIN 6029CM) SLAT TORQUE LIMITER TRIPPED. SLAT ROTORY ACUATOR 6029CM REPLACED IAW AMM 27Jun 16, 2011 · Airbus A320211 · Leading Edge Slat ActuatorSDR CA110606014Window · crackedTHE CREW ADVISED FLIGHT DISPATCH THAT THE F/O`S OUTER WINDSHIELD HAD CRACKED AT FL360 ENROUTE. CREW DESCENDED DOWN TO FL230, AND SENT A DIVERSION DUE TO LACK OF FUEL TO CARRY ON AT THE LOWER FLIGHT LEVEL. NO EMERGENCY DECLARED WITH ATC. F/O WINDSCREEN REPLACJun 5, 2011 · Airbus A320211 · Flight Compartment WindowsSDR DALA1138623209Light · missingFLIGHT CREW REPORTED EMERGENCY PATH FLOOR LIGHT SEAT 5C MISSING AND WIRES ARE EXPOSED. INSTALLED COVER AND LIGHT HARNESS AND TESTS OK.Jun 5, 2011 · N309US · Airbus A320211 · Emergency LightingSDR CA110606013Proximity Sensor · out of rigECAM MESSAGE MLG NOT DOWNLOCKED, MANUAL GEAR EXTENSION, COMPLETED OVERSHOT & RECYCLED MLG. ON 2ND RECYCLE & WHILE IN TURN, MLG EXTENDED & LOCKED. TSM 32-31-00-810-857 CARRIED OUT & FOUND PROXIMITY SENSORS 33GA & 35GA OUT OF LIMITS. ADJUSTED IAW TSM 32-31-73-Jun 4, 2011 · Airbus A320211 · Landing Gear Position and WarningSDR CA110606012Sensor · failedFLIGHT ADVISED FLIGHT DISPATCH THAT THEY HAD A BRAKE TEMPERATURE INDICATION PROBLEM, AND THE WERE RETURNING BACK TO STATION. JUST AFTER LIFTOFF HAD A ECAM BRAKE HOT. NR 1 BRAKE TEMP INCREASED TO 1,000 DEGREES C. GEAR SELECTED DOWN WITH NO EFFECT. EVENTUAJun 4, 2011 · Airbus A320211 · Landing Gear Brake SystemSDR DALA1137563277Floor Panel · dentedFWD CARGO COMPARTMENT, FLOOR PANEL 131EF HAS SEVERAL PUNCTURES AND DENTS. REMOVED FLOOR PANEL 131EF AT FWD CARGO IAW A320 AMM 53-22-14-000-001. RECEIVED NEW PANEL 131EF AT FWD CARGO P/N 5367200500000 TRAVELER T11/884323 BATCH 2014175 TYPE OF MATL 422476009ICJun 1, 2011 · N377NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1137473233Water Heater · odorON DESCENT APPROXIMATELY 20000 FEET, FLIGHT ATTENDANT CALLED WITH A SLIGHT SMOKEY SMELL IN AFT GALLEY AREA. PILOT IN JUMP SEAT CONFIRMED SLIGHT SMELL, GALLEY POWER WAS TURNED OFF FOR REMAINDER OF FLIGHT AND LANDING WAS UNEVENTFUL. REPLACED RIGHT AFT LAVATORYJun 1, 2011 · N333NW · Airbus A320211 · Potable Water SystemSDR DALA1137443216Damper · failedDURING L CHECK FORWARD LEFT DOOR DAMPER FAILED OPERATIONAL CHECK. REPLACED DAMPER PER AMM 52-13-14. OPERATIONAL CHECK GOOD PER AMM 52-13-14.Jun 1, 2011 · N316US · Airbus A320211 · Passenger/Crew DoorsSDR DALA1137433216Damper · failedDURING L CHECK AFT LEFT DOOR DAMPER FAILED OPERATIONAL CHECK. REMOVED AND REPLACED DOOR DAMPER PER AMM 52-13-14. OPERATIONAL CHECK GOOD PER AMM 52-13-14.Jun 1, 2011 · N316US · Airbus A320211 · Passenger/Crew DoorsSDR DALA1137333277Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL 131AF HAS SEVERAL PUNCTURES AND DISBOND. REMOVED FLOOR PANEL NR 131AF IAW A320 AMM 53-22-14 000-001. FABRICATED FLOOR PANEL NR 131AF IAW STAM TRAVELER NR T11/884322 AND SRM 53-02-00 FIG 209 P/N D5367200300000. BATCH NR 2014May 31, 2011 · N377NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1137153277Floor Panel · dentedAFT CARGO COMPARTMENT FLOOR PANEL 151DF HAS DENTS AND PUNCTURES. REMOVED FLOOR PANEL IAW AMM 53-42-14-000-001. RECEIVED NEW FLOOR PANEL FABRICATED IAW STAM TRAVELER NR T11/884324 MAT 422349 600-9JC, BATCH NR 20014175 AND DWG NR SRM 53-02-00 FIG 209. LOCATEDMay 29, 2011 · N377NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1137253219Wire · damagedDURING EMERGENCY LIGHT TEST FOUND ROW 4 PATH LIGHT INOP, REPAIRED WIRE AND TESTS OK.May 28, 2011 · N319US · Airbus A320211 · Light System WiringSDR DALA1137133277Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL 132GF HAS DENTS, PUNCTURED AND CRACKS. REMOVED FLOOR PANEL IAW AMM 53-22-14 PB401. RECEIVED NEW FLOOR PANEL NR 132GF PER SRM 53-02-00 FIG 209, TRAVELER NR T11/884325 BATCH NR 2014175. INSTALLED NEW FLOOR PANEL IAW AMM 53-22May 28, 2011 · N377NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1137123277Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL 131BF HAS CRACKS AND PUNCTURED. REMOVED FLOOR PANEL NR 131BF IAW AMM 53-22-14 000-001. RECEIVED NEW FLOOR PANEL NR 131BF P/N DA-5367301200000 TRAVELER NR T11/884326. DWG NR SRM 53-02-00 FIG 209. BATCH NR 2014175, MATERIAL-May 28, 2011 · N377NW · Airbus A320211 · Fuselage Floor PanelSDR CA110530001Actuator · failedWHEN SELECTING FLAPS, SLATS DID NOT EXTEND,NO EMERGENCY DECLARED APPROACH SPEED INCREASED, LANDED WITH OUT INCIDENT. REPLACED ROTARY SLAT ACTUATORS 6029CM AND 6077CM IAW AMM 27-84-49. OPS TEST CARRIED OUT SERV. SLAT ROTARY ACTUATOR MPNS: 830C0000-01 AND 820May 27, 2011 · Airbus A320211 · Leading Edge Slat ActuatorSDR DALA1137243218Wire · damagedDURING EMERGENCY LIGHT TEST FOUND WIRE DAMAGED AT SEAT 5C, REPLACED PATH LIGHT ASSEMBLY AND TESTS OK.May 27, 2011 · N318US · Airbus A320211 · Light System WiringSDR DALA1137423216Damper · failedDURING L CHECK FORWARD RIGHT DOOR DAMPER FAILED. OPERATIONAL CHECK. REPLACED DAMPER PER A320 AMM 52-13-14. ACCOMPLISHED OPERATIONAL CHECK OF DAMPER WITH SLIDE AND PANELS INSTALLED PER AMM 52-13-14, CHECKS GOOD.May 26, 2011 · N316US · Airbus A320211 · Service DoorsSDR CA110525007Unknown · multiple failCREW REJECTED T/O AT 105KTS ON RWY 12. UNABLE TO OBTAIN TOGA THRUST, NO TOGA AUTOTHRUST INDICATION ON THE FMA (BLANK). N1 TOGA THRUST 96 PERCENT AND N1,S INDICATED TOGA POSITION. REJECTED T/O SPEED 105 KTS. NO FAULTS ON PFR, NO FAULTS ECAM, ENG RUNS CARRIEMay 22, 2011 · Airbus A320211 · Indicating/Recording SystemSDR CA110525003Pump · failedAPPROX HALFWAY THROUGH THE FLIGHT THE CREW REPORTED A BLUE HYD SYS LOW PRESSURE. ECAM HYD B SYS LOW PR ECAM ACTION , B SYS HYD TURNED OFF B HYD PUMP REPLACED IAW AMM 29-12-51.May 21, 2011 · Airbus A320211 · Hydraulic Pump (Electric/Engine), MainSDR CA110518005Manifold · leakingWHILE ENROUTE PRIOR TO THE APPROACH THE CREW REPORTED THEY HAD LOST THE GREEN HYD SYS AND WOULD REQUIRE A TOW TO THE GATE ON ARRIVAL. LEAVING CRUISE ALTITUDE FOR DESCENT HAD FOLLOWING ECAM "HYD LO RESVR LVL" ECAM ACTION ACCOMPLISHED. EMERGENCY GEAR EXTENSIONMay 17, 2011 · Airbus A320211 · Hydraulic System, MainSDR DALA1135053218Tee Fitting · damagedRT WING FWD EMERGENCY AND REPLACED TWO TEE FITTINGS (AFT AND FWD) AT RT WING FWD EMERGENCY DOOR IAW SRM 51-42-11.May 17, 2011 · N318US · Airbus A320211 · Emergency ExitsSDR DALA1135213233Relay · malfunctionedDURING CRUISE, THE CREW NOTED THAT THE RT TANK WAS DROPPING AA MUCH HIGHER RATE THAN NORMAL, SO THEY INITIATED THE RETURN WITH THE THOUGHTS OF A FUEL LEAK. ABOUT 50 MILES NW OF THE FIELD DID QRH PROCEDURE AND THE RT ENGINE WAS SHUTDOWN, THE LANDING WAS UNEVENMay 16, 2011 · N333NW · Airbus A320211 · Fuel Transfer ValveSDR DALA1134973218Skin · damagedLT SIDE OF AFT FUSELAGE, BELOW L-2 DOOR, JUST FWD OF FR66 AT S27L. REMOVED DOUBLER IAW SRM 51-42-11 CUTOUT DAMAGED AREA IAW SRM 53-41-11. FABRICATED NEW DOUBLER, & FILLER. INST DOUBLER AND FILLER AFT LT SIDE OF AFT FUSELAGE BELOW L-2 DOOR IAW SRM 53-41-11May 16, 2011 · N318US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA1134813218Skin · corrodedAFT FUSELAGE SKIN AROUND VACUUM VENT HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. REMAINING MATERIAL OUT OF LIMITS PER SRM 53-41-11. REMOVED EXISTING FASTENERS PER SRM 51-42-11. CUT OUT DAMAGED SKIN AREA IAW SRM 53-41-11. FABRICATED DOUBLER AND FILLMay 16, 2011 · N318US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA1134803218Floor Panel · delaminatedAFT PIT FLOOR PANEL 151LF IS DELAMINATED 4" BY 4" AREA. REMOVED FLOOR PANEL 151LF IAW AMM 53-42-14. FABRICATED NEW FLOOR PANEL 151LF IAW DWG 3D25-37705 ON STAM TRAVELER T11/882044. INSTALLED NEW FLOOR PANEL 151LF IAW AMM 53-42-14-400-001.May 16, 2011 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA1134793218Floor Panel · delaminatedAFT PIT FLOOR PANEL 151PF IS DELAMINATED 4" BY 4" AREA. REMOVED FLT PNL 151PF AT AFT PIT IAW SRM 51-42-11. FABRICATED NEW FLOOR PANEL 151PF ON STAM TRAVELER T11/882046 IAW DWG 3D25-37705. INSTALLED NEW FLOOR PANEL 151PF IAW AMM 53-42-14-400-001.May 16, 2011 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA1134783218Hook · corrodedRT WING AFT EMERGENCY HATCH HAS CORROSION AT LWR T HOOK FITTINGS FWD AND AFT AREA. REMOVED AND REPLACED 2 T FITTING IAW2 SRM 51-42-11 P/N D522790 5420400 LOCATED AND DRILLED NEW 2 PARTS IAW SRM 51-44-11. TREATED AND PRIMED AND PAINTED IAW SRM 51-21-11 AND 51May 16, 2011 · N318US · Airbus A320211 · Emergency ExitsSDR DALA1134123218Escape Hatch · crackedRT WING AFT EMERGENCY HATCH RT LOAD TRANSMITTING PROFILE HAS A CRACK (2 PLACES). REMOVED LOAD TRANSMITTING PROFILE PER SRM 51-42-11;LOCATED AND DRILLED NEW LOAD TRANSMITTING PROFILE P/N D5227902620300 PER SRM 51-44-11; INSTALLED NEW LOAD TRANSMITTING PROFILE May 15, 2011 · N318US · Airbus A320211 · Emergency ExitsSDR DALA1134083218Structure · crackedLT WING FWD EMERGENCY HATCH RT LOAD HAS CRACKS. REMOVED AND INSTALLED NEW LOAD TRANSMITTING PROFILE IAW SRM 51-42-11. PROFILE INST P/N D5227902020511 BATCH#0002046848. CRACK DIM; 0.100".May 15, 2011 · N318US · Airbus A320211 · Emergency ExitsSDR DALA1134353218Floor Panel · delaminatedAFT PIT FLOOR PANEL 151GF IS DELAMINATED. 8" BY 8" AREA REMOVED FLOOR PANEL 151GF OF AFT PIT IAW SRM 51-42-11. FABRICATED NEW FLOOR PANEL 151GF ON STAM TRAVELER T11/882043 IAW DWG#3D25-37705. INSTALLED NEW FLOOR PANEL 151GF IAW AMM 53-42-14PB401.May 14, 2011 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA1134333218Floor Panel · delaminatedAFT PIT FLOOR PANEL 151DF IS DELAMINATED ON SEVERAL AREAS DIA. 6" BY 6" AREA. REMOVED FLOOR PNL 151DF IN AFT PIT IAW SRM 51-42-11. FABRICATED NEW FLOOR PNL 151DF ON STAM TRAVELER T11/882012 IAW INSTALLED NEW FLOOR PNL 151DF IAW AMM 53-42-14PB401.May 14, 2011 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA1134303218Floor Panel · delaminatedAFT PIT FLOOR PANEL 161AF IS DELAMINATED. 5" BY 5" REMOVED AFT PIT FLOOR PANEL 161AF IAW AMM 53-42-14. FABRICATED FLOOR PANEL . INSTALLED AFT PIT FLOOR PANEL 161AF IAW AMM 53-42-14-400-001.May 14, 2011 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA1134223218Floor Panel · damagedFWD CARGO COMPARTMENT, FLOOR PANEL 131EF IS DAMAGE. REMOVED FLOOR PANEL 131EF OF FWD CARGO COMP IAW SRM 51-42-11. FABRICATED NEW FLOOR PANEL 131EF ON STAM TRAVELER T11/88204IAW DWG 3D25-37705. INSTALLED NEW FLOOR PANEL 131EF IAW AMM 53-22-14-400-001.May 14, 2011 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA1134183218Floor Panel · puncturedFWD CARGO COMPARTMENT, FLOOR PANEL 131AF HAS DENT AND PUNCTURES. REMOVED FLOOR PANEL 131AF AT FWD COMPT IAW SRM 51-42-11. FABRICATED NEW FLOOR PANEL 131AF ON STAM TRAVELER T11/882040 IAW DWG NR 3D25-37705. INSTALLED FLOOR PANEL 131AF IAW AMM 53-22-14-400-00May 14, 2011 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA1134153218Escape Hatch · corrodedLT WING AFT EMERGENCY HATCH HAS CORROSION AT LOWER FWD T HOOK FITTING. REMOVED AND REPLACED T FITTING LT WING AFT EMERGENCY HATCH IAW SRM 51-42-11 T FITTING P/N D5227905420400.May 13, 2011 · N318US · Airbus A320211 · Emergency ExitsSDR DALA1133653232Skin · corrodedLWR AFT FUSELAGE SKIN APPROX 3 INCH BY 1.5 INCH AREA OF CORROSION 12 INCH AFT OF FR 69, 3 INCH ABOVE STR 34R LAV VENT EXHAUST. REMOVED CORROSION IAW SRM 53-41-11 OUT OF LIMITS IAW SRM 53-41-11. CUT OUT DAMAGE AREA IAW SRM 53-41-11. FABRICATED DOUBLER AND FIMay 12, 2011 · N332NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA1133643232Profile · corrodedLT FWD EMERGENCY EXIT DOOR RT LOAD TRANSMITTING PROFILE HAVE CRACKS ON FASTENER HOLES EDGE. REMOVED CRACKED ANGLE AND CENTER SUPPORT ANGLE FOR ACCESS TO REPAIR IAW SRM 51-42-11. LOCATED AND DRILLED ANGLE IAW SRM 51-44-11. INSTALLED ANGLE AND CENTER SUPPORT May 12, 2011 · N332NW · Airbus A320211 · Emergency ExitsSDR DALA1133633232Fitting · corrodedLT AFT EMERGENCY EXIT DOOR LWR FWD AND AFT HOOK "T" FITTING HAS CORROSION. REMOVED LOWER SEAL EMERGENCY DOOR LT AFT IAW AMM 52-21-18-401. REMOVED 2 LATCH IAW SRM 51-42-11. REMOVED T FITTING LOWER SECTION IAW SRM 51-42-11 FWD FITTING. REMOVED FITTING LOWEMay 12, 2011 · N332NW · Airbus A320211 · Emergency ExitsSDR DALA1133613232Profile · crackedRT FWD EMERGENCY EXIT DOOR RT LOAD TRANSMITTING PROFILE HAS CRACKS ON FASTENER HOLES EDGE. REMOVED AND REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-42-11.May 12, 2011 · N332NW · Airbus A320211 · Emergency ExitsSDR DALA1133453232Floor Panel · puncturedFORWARD CARGO COMPT FLOORBOARD PNL 131AF UPPER SURFACE HAS PUNCTURED AND DENTED SEVERAL PLACES APPROXIMATELY 2 TO 3 INCHES, AS MARKED. REMOVED FLOOR PANEL IAW AMM 53-22-14 PB401 FABRICATED FLOOR PANEL ON STAM TRAVELER NR T11/881687 IAW DWG3D25-37705 MAT. A40 May 11, 2011 · N332NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1133443232Floorboard · damagedFORWARD CARGO COMPT FLOORBOARD PNL 131EF HAS BROKEN WASHERS SEVERAL PLACES, AS MARKED. REMOVED FLOOR PANEL IAW AMM 53-22-14 PB401. FABRICATED FLOOR PANEL ON STAM TRAVELER NR T11/881688 IAW DWG 3D25-37705 MAT. A40 2AB-60X144. INSTALLED FLOOR PNL 131EF IAW AMMay 11, 2011 · N332NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1133433232Floor Panel · brokenFORWARD CARGO COMPT FLOORBOARD PNL 131HF HAS BROKEN WASHERS SEVERAL PLACES, AS MARKED. REMOVED FLOOR PANEL 131HF IAW AMM53-22-14 PB401 FABRICATED FLOOR PANEL ON STAM TRAVELER NR T11/881682 IAW DWG 3D25-37705 MAT A402AB-60X144, BATCH NR 1886727. INSTALLED FLOMay 11, 2011 · N332NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1133073232Floorboard · damagedAFT CARGO COMPARTMENT FLOORBOARD PNL 151GF HAS BROKEN WASHERS AT SEVERAL PLACES. REMOVED FLOORBOARD PNL 151GF IAW AMM 53-42-14-000-001. FABRICATED FLOORBOARD PNL 151GF ON STAM TRAVELER T11/881684 IAW DWG NR 3D25-37705 MATERIAL TYPE: A402AB-60X144 BATCH 18867May 10, 2011 · N332NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1133063232Floorboard · damagedAFT CARGO COMPARTMENT FLOOR BOARD PNL NR 151DF HAS SEVERAL BROKEN WASHERS AS MARKED. REMOVED FLOOR PANEL 151DF IAW AMM 53-42-14-000-001. FABRICATED FLOOR PANEL 151DF ON STAM TRAVELER T11/881685 IAW DWG NR 3D25-3770 5. MATERIAL TYPE: A402AB-60X144 BATCH 1886May 10, 2011 · N332NW · Airbus A320211 · Fuselage Floor Panel
Back to Airbus A320-211