N854NN
Service difficulty reports · 110
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 = 'N854NN' 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.
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 = 'N854NN' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AALA202210064807None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION AREAS FOUND ON TRANSITION PANEL LOCATED BETWEEN STA 727 AND 767 AND RIGHT BUTT LINE 21. REMOVED AND REPLACED TRANSITION PANEL PER SRM 53-00-53.SDR AALA202210063724None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON TRANSITION PANEL LOCATED AT STA 777 AND LEFT BUTT LINE 21. REMOVED AND REPLACED TRANSITION PANEL PER SRM 53-00-53.SDR AALA202210060719Skin · crackedAIRCRAFT IN BASE MAINTENANCE: 1 IN CRACK IN LOWER SKIN OF LEFT HORIZONTAL STABILIZER. LOCATED AT LEFT STABILIZER STATION 101.9 AND 9 INCHES FROM THE AFT SPAR. REMOVED CRACK BY GRINDING AND INSTALLING DOUBLER WITH FILLER PER SRM 55-10-01-2R-11.SDR AALA202210057132Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 147.90, 8 INCHES FROM FORWARD SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202210052033Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 101.90, 9 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202210055424Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 157.10, 8 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202203046673Lens · missingAIRCRAFT WAS GROUNDED: RIGHT AFT SERVICE DOOR EMERGENCY EXIT SIGN MISSING. REPLACED LENS PER AMM 33-51-01.SDR AALA202112078935Shim · gougedAIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY DOOR LIGHT ON DURING PUSH BACK WITH DOOR CLOSED AND LOCKED. TROUBLESHOOT PER FIM 52-10-00-810-801. FOUND FORWARD ENTRY DOOR TARGET GOUGED, REPLACED TARGET SHIM - DOOR INDICATION OPERATIONS NORMAL PER AMM 52-71-00.SDR AALA202112067435Mechanism · inoperativeAIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPERATE. CLEANED AND LUBED LOCKING MECHANISM PER AMM 52-51-00 OK FOR SERVICE.SDR AALA202111290687Lock · out of positionAIRCRAFT WAS NOT GROUNDED: PLASTIC TRIM ON LEFT SIDE OF GIRT BAR FALLS OFF WHEN FLIGHT ATTENDANT INSTALLS GIRT BAR AT DOOR 4R. RE INSTALLED GIRT BAR BAR LOCK ON 4R GIRT BAR PER AMM 25-66-01.SDR AALA202110066472Handle · looseAIRCRAFT WAS NOT GROUNDED: INSIDE HANDLE OF FORWARD LAVATORY DOOR IS LOOSE. TIGHTENED HANDLE OF FORWARD LAVATORY DOOR.SDR AALA202104069012Lamp · inoperativeAIRCRAFT WAS NOT GROUNDED: SEAT 16F EXIT LAMP INOPERATIVE. REPLACED LAMP PER AMM 33-51-00.SDR AALA202103089020Door · out of positionAIRCRAFT WAS NOT GROUNDED: DURING PRE-FLIGHT THE LOWER PORTION OF EMERGENCY WING DOOR WAS NOT IN CORRECT POSITION. FOUND TRIM CLOSE OUT PANEL MISALIGNED. OPENED EMERGENCY EXIT REPOSITIONED PANEL AND CLOSE EXIT DOOR IAW AMM 52-22-00-580-803.SDR AALA202011019016Window · arcedAIRCRAFT WAS GROUNDED. CRACK IN RT NR 1 WINDOW WITH INDICATIONS OF ARCING. REPLACED WINDOW WITH NEW, IAW WORKCARD 08L21056004.SDR AALA2020090869018Transmitter · inoperativeAIRCRAFT WAS GROUNDED: DURING CONFIGURATION FOR LANDING, FLAP GAUGE INDICATED FLAP ASYMMETRY BETWEEN FLAP 0 AND FLAP 1 SETTINGS; FLIGHT CREW ACCOMPLISHED FLAPS UP LANDING CHECKLIST, FLAP GAUGE NORMALIZED AFTER SELECTION OF A DIFFERENT FLAP SETTING. NO ROLL ENCSDR AALA202008039011Control Unit · inoperativeAIRCRAFT WAS GROUNDED: L-1 FLIGHT DECK WINDSHIELD CRACKED OCCURRED AT 39000 WITH NO OVERHEAT INDICATION. OVERHEAT LIGHT CAME ON APPROXIMATELY 30 SECOND AFTER THE WINDSHIELD CRACKED. REMOVED AND REPLACED WINDOW HEAT CONTROL UNIT (AALA202008039011) FOR L1 WINDOWSDR AALA2020080319003Windshield · crackedAIRCRAFT WAS GROUNDED: L-1 FLIGHT DECK WINDSHIELD CRACKED OCCURRED AT 39000 WITH NO OVERHEAT INDICATION. OVERHEAT LIGHT CAME ON APPROXIMATELY 30 SECOND AFTER THE WINDSHIELD CRACKED. REMOVED AND REPLACED WINDOW HEAT CONTROL UNIT FOR L1 WINDOW AND THE L1 WINDSHISDR AALA2020032319007Lens · missingAIRCRAFT WAS GROUNDED: EXIT SIGN AT AFT LEFT LAVATORY WAS MISSING ITS PLASTIC LENS COVER. MAINTENANCE REPLACED LIGHT ASSEMBLY EXIT SIGN PER MM 33-51-14.SDR AALA201910159020Engine · unknownAIRCRAFT WAS GROUNDED: PILOT REPORTS UPON ENGINE SHUTDOWN THE NO.1 ENG DID NOT SHUT DOWN FOR APPROX. 15 SEC AFTER CUTOFF SELECTED. MAINTENANCE CHECKED HPSOV CONTROL POWER AT DP1203 LEFT HMU IAW FIM 73-06-00.VOLTAGE OK IN IDLE AND CUTOFF POSITIONS. CHECKED RESISDR AALA2019100879032Warning Message · false activationAIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO DFW ON ACCOUNT OF ENGINE OVERHEAT INDICATION. EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED FIM 26-10-00-810-811. NO FAULTS FOUND. RAN ENGINE TO TAKE-OFF POWER. NO FAULTS. ACCOMPLISHED ENG/APU FIRE DETECTION CONTRSDR AALA201910029028Pad · wornAIRCRAFT IN BASE MAINTENANCE: PREVIOUS STRAP REPAIR TO THE GROUND PNEUMATIC DOOR OUTBOARD LATCH PAD WORN AT BS 538 AND RBL 40.875. REPAIRED LATCH PAD PER SRM 57-10-13-2R-3 REPAIR 3.SDR AALA201812179010Bulkhead Web · crackedRIGHT WHEEL WELL BULKHEAD WEB WAS CRACKED, BS 663, RBL 48. REPAIRED THE BULKHEAD WEB IAW RD 57-10-10-9, REPAIR 9.SDR AALA201801229034Cover · unsecureAIRCRAFT WAS NOT GROUNDED: EXIT SIGN COVER FELL OFF AT THE R1 LOCATION. MAINTENANCE REPLACED R1 EMERGENCY LIGHT ASSEMBLY AND PERFORMED SATISFACTORY OPERATIONAL CHECK.SDR AALA201711169024Seat · defectiveTHE AIRCRAFT WAS NOT GROUNDED. F/O SEAT WILL NOT STAY LOCKED IN POSITION, SLID BACK ON TAKE OFF ROTATION. REPLACED FIRST OFFICER SEAT IAW AMM 25-11-01. CKD OK.SDR AALA201704109062Cover · damagedEXIT LIGHT AT DOOR 2R DAMAGED. REPLACED EMERG EXIT LIGHT COVER AT DOOR 2R IAW GPM. THE AIRCRAFT WAS NOT GROUNDED.SDR AALA20161214010Lens · missingRIGHT OVERWING EMERGENCY EXIT LIGHT AT SEAT 15F IS MISSING THE LENS COVER. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.SDR AALA20160923002Beam · wornSUPPORT BEAM IS WORN AT ACCESS DOOR 192DR. REPAIRED THE BEAM IAW EA 263622 AND SRM 51-70-12-2R.SDR AALA20160919004Floorbeam · corrodedCABIN FLOORBEAM AT BS 947 IS CORRODED BETWEEN LBL 49 AND LBL 50. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R, PROCEDURE 5.SDR AALA20160919003Floor Support · corrodedCABIN OUTBOARD FLOOR SUPPORT AT LBL 52 BETW BS 947 AND 967 IS CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.SDR AALA20160917004Rib · crackedLEFT HORIZONTAL STABILIZER RIB AT HSS 92.7 IS CRACKED AT THE 3RD VERTICAL STIFFENER FROM FRONT. REPAIRED THE RIB IAW SRM 55-10-09-2R-4.SDR AALA20160917002Rib · crackedRIGHT HORIZONTAL STABILIZER RIB AT HSS 92.7 IS CRACKED AT THE 2ND AND 3RD VERTICAL STIFFENERS FROM FRONT. REPAIRED RIB IAW SRM 55-10-09-2R-4.SDR AALA20160915004Floor Support · crackedCABIN FLOOR, SUPPORT CRACKED, BS 344 TO 360, BUTTLINE 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW REPAIR DOCUMENT 51-00-05-1 AND DRAWING 141A5400, SHEET 7.SDR AALA20160915003Floor Support · crackedFLOOR SUPPORT CRACKED BS 344 TO 360, LBL 11. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW REPAIR DOCUMENT 51-00-05-1 AND DRAWING 141A5400-6, SHEET 12.SDR AALA20160212012Transmitter · faultyON APPROACH, FLAP INDICATOR STOPPED AT FLAPS 2 WITH FLAP HANDLE AT 10. THE FLIGHT EXECUTED A MISSED APPROACH & DECLARED AN EMER. ON SECOND APPROACH, DID QRH ALTERNATE FLAPS EXTENSION PROCEDURE & LANDED WITHOUT FURTHER INCIDENT. R & R THE LT FLAP POSITION TRSDR AALA20160212007Transmitter · faultyFLAPS STUCK AT JUST LESS THAN 2 WHEN CONFIGURING FOR APPROACH. FLIGHT OVERFLEW THE APPROACH & WAS VECTORED FOR ANOTHER ATTEMPT. THE CREW FOLLOWED QRH PROCEDURES & DECLARED AN EMER. ALTERNATE FLAPS USED FOR FLAPS 15 LANDING. THE FLIGHT LANDED ON SECOND ATTESDR AALA20160208007Flap · malfunctionedON APPROACH, FLAPS FROZE AT 10 DEG WITH LE DEVICES PANEL SHOWING ALL GREEN. ACCOMPLISHED QRH, FLAPS ALTERNATE EXTEND, NORMAL FLAPS 15 LANDING. FLIGHT DECLARED AN EMER & LANDED WITHOUT FURTHER INCIDENT. BITE CHECK OF FSEU SHOWS FAULT 27-52261 & IN AN INTERMISDR AALA20151226001Sensor · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB RT WING BODY OVERHEAT AMBER LIGHTS & MASTER CAUTION ILLUMINATED. QRH PROCEDURES COMPLETED & LIGHTS EXTINGUISHED. NGAR FOR TROUBLESHOOTING. ACCOMPLISHESDR AALA20150208005Shaft · dirtyEMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH CREW RECEIVED AN AFT ENTRY DOOR WARNING. FOUND DOOR SENSOR SWITCH SHAFT STICKING. CLEANED SENSOR SHAFT. ACCOMPLISHED ENTRY & SERVICE DOOR INDICATION SENSOR TEST IAW MM 52-71-11. SSDR AALA20140912006Skin · corrodedCORROSION WAS FOUND UNDER 2 FASTENER HEADS AT STATION 947 BETWEEN STRINGERS 21 & 22 LT. CORROSION REMOVED FROM SKIN IAW SRM 51-10-02 & ACCOMPLISHED REPAIR IAW EA B737-53-026206.SDR AALA20140912005Skin · corrodedCORROSION ON FUSELAGE SKIN AT STATION 937 & STRINGER 23 LT AT AFT EDGE OF CATERING STRIPE. REMOVED CORROSION FROM SKIN IAW SRM 51-10-02 & ACCOMPLISHED REPAIR IAW EA B737-53-026206.SDR AALA20140912004Skin · corrodedCORROSION ON FUSELAGE SKIN AT STATION 927 FROM STRINGERS 21 TO 23 LT. REMOVED CORROSION IAW SRM 51-10-02 & ACCOMPLISHED REPAIR IAW EA B737-026206.SDR AALA20140912007Skin · corrodedCORROSION WAS FOUND ON THE FUSELAGE SKIN AT STATION 1016 FROM STRINGERS 20 TO 23 LT. ACCOMPLISHED REPAIR IAW EA B737-53-026206.SDR AALA20140423003Light · inoperativeLEFT NR 2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 2 DOOR EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.SDR AALA20120928016Skin · corrodedCORROSION ON FUSELAGE SKIN BELOW AND AFT OF THE LAVATORY TANK VENT FROM STATIONS 905 TO 927, STRINGERS 23 TO 24 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026206.SDR AALA20120926005Skin · corrodedCORROSION ON FUSELAGE SKIN BELOW AND AFT OF THE LAVATORY TANK VENT FROM STATIONS 905 TO 927, STRINGERS 24 TO 25 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026206.SDR AALA20120928015Skin · corrodedCORROSION ON FUSELAGE SKIN BELOW AND AFT OF THE LAVATORY TANK VENT FROM STATIONS 967 TO 987, STRINGERS 22 TO 23 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026206.SDR AALA20120928014Skin · corrodedCORROSION ON FUSELAGE SKIN BELOW AND AFT OF THE LAVATORY TANK VENT FROM STATIONS 947 TO 967, STRINGERS 22 TO 23 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026206.SDR AALA20120928013Skin · corrodedCORROSION ON FUSELAGE SKIN BELOW AND AFT OF THE LAVATORY TANK VENT FROM STATIONS 927 TO 947, STRINGERS 22 TO 23 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026206.SDR AALA20120928012Skin · corrodedCORROSION ON FUSELAGE SKIN BELOW AND AFT OF THE LAVATORY TANK VENT FROM STATIONS 905 TO 927, STRINGERS 22 TO 23 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026206.SDR AALA20120928011Skin · corrodedCORROSION ON FUSELAGE SKIN BELOW AND AFT OF THE LAVATORY TANK VENT FROM STATIONS 1006 TO 1016, STRINGERS 21 TO 22 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026206.
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