N1619A
Service difficulty reports · 296
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 = 'N1619A' 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 = 'N1619A' 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 UIEA2026100800969Pseu · faultedENTRY DOOR AND EMER DOOR DISCRETE LIGHTS ON OVERHEAD PANEL INOPERATIVE. REMOVED AND REPLACED PSEU IAW AMM 32-09-04-704-013. OPS CHKD GOOD.SDR UIEA2026100500945Proximity Sensor · false activation40 MINS INTO FLIGHT @ FL340, RT LANDING GEAR DISCREET LIGHTS, AMBER REV LIGHT, AND ENTRY DOORS/EMER DOORS DISCREET LIGHTS ILLUMINATED. LANDING GEAR DISCREET LIGHTS EXTINGUISHED 10 MINS AFTER. LDG GEAR MONITOR STATUS MSG. REPLACED S-242 AND S-564 PROXIMITY SENSSDR UIEA2026100500950Battery · inoperativeFLASHLIGHT NEXT TO LAV DEAD BATTERY, NOTICED POST FLIGHT. MX IN WORK WHILE IN AOGM FOR ATB, MULTIPLE ERRONEOUS LANDING GEAR, T/R AND DOOR INDICATIONS. AOGM ETR 07OCT26. REMOVED AND REPLACED FLASHLIGHT & BATTERY NEXT TO LAV. OPS CHECK GOOD IAW AMM 20-11-00, 2SDR UIEA2026100400943Pseu · inoperativeAPPROX 1 HR AFTER T/O DURING CRUISE @ FL360, LEFT LANDING GEAR DISCRETE LIGHT ILLUMINATED. INTERMITTENT - RT LANDING GEAR DISCRETE LIGHT ILLUMINATED. IN FLIGHT DURING CRUISE, INTERMITTENT RT AMBER REV; NO ASSOCIATED EICAS MESSAGE.(<P>ANC MX PERFORMED FIM 32-09SDR UIEA2026052700365Switch · faultedAFTER TAKEOFF AROUND 3000FT AGL, GOT E/E ACCESS DOOR EICAS MESSAGE. R & R E/E ACCESS DOOR SWITCH PER AMM 52-71-00. OPS CHECK GOOD. DMI 253051 CLOSED</P>)SDR UIEA2026052400347Line · disconnectedSHORTLY AFTER TAKEOFF (AROUND 2000 AGL) GOT R ENG EEC MODE EICAS MSG. NO INDICATION OF EPR ON RIGHT ENGINE. FOUND THE PT2 LINE DISCONNECTED AT THE RIGHT ENGINE EEC. RECONNECTED PT2 PER AMM 77-11-00/001. PERFORMED ENGINE RUN IAW AMM 71-00-00. ALL OPS CHECKED GSDR UIEA2026032700108Switch · shortedDURING PREPARATION FOR ENG #2 COOLING BAROMETRIC SWITCH, OPS CHK FOUND DAMAGE TO A SCREW AT NACELLE ZONE VENT SOV. AFTER INVESTIGATING, WE FOUND THAT THIS SCREW WAS TOUCHING THE FEEDER CABLES. TWO CABLES GOT DAMAGED AND PRODUCED ARCING TO THE VALVE HOUSING SCRSDR UIEA2026050500297Sign · brokenDURING GVI OF MAIN DECK CARGO COMPARTMENT, FOUND SELF LUMINOUS EXIT SIGN, ATTACHED OVER THE ENTRY HATCH FOR THE MAIN CARGO, BROKEN. SELF ILLUMINATED EXIT SIGN REPLACED IAW AMM 33-51-02 REV.147 NO FURTHER DEFECTS NOTED.SDR UIEA2026050600298Skin · damagedDURING LIGHTNING STRIKE INSPECTION, FOUND 5EA BURN MARKS ON FUSELAGE SKIN AT STA.522-544. STRG 39L-39R. PERMANENT REPAIR HAS BEEN ACCOMPLISHED AS PER SRM 53-00-01-2R-1, REPAIR 1. REV. 131.SDR UIEA2026050600300Skin · damagedDURING LIGHTNING STRIKE INSPECTION, FOUND 1EA BURN MARK ON FUSELAGE SKIN AT STA.654+44-654+66, BTWN. STRG 39L-39R. PERMANENT REPAIR HAS BEEN ACCOMPLISHED AS PER SRM 53-00-01-2R-1, REPAIR 1. REV. 131.SDR UIEA2026050600301Skin · damagedDURING LIGHTNING STRIKE INSPECTION, FOUND 1EA BURN MARK ON FUSELAGE SKIN AT STA. 654+88-654+110. STRG 39L-39R. PERMANENT REPAIR HAS BEEN ACCOMPLISHED AS PER SRM 53-00-01-2R-1, REPAIR 1. REV. 131.SDR UIEA2026050600302Skin · dentedFOUND ONE DENT ON THE FUSELAGE SKIN RH SIDE BEHIND MLG WW ABOVE THE RAT HOUSING. GOUGE ON FUSELAGE SKIN STA 1153-1175 AT STR 29R IS OUT OF LIMITS IAW SRM 53-00-01-1A-1. ALLOWABLE DAMAGE 1 REV 131. PERFORMED SKIN REPAIR IAW SRM 53-00-01-2R-1 REPAIR 1 REV 131.SDR UIEA2026050700305Skin · damagedDURING LIGHTNING STRIKE INSPECTION, FOUND 5EA BURN MARKS ON FUSELAGE SKIN AT STA. 522-544, BTWN STRG 39L-39R. REPAIR PARTS HAVE BEEN INSTALLED AS PER SRM 53-00-01-2R-1, REPAIR 1. REV. 131.SDR 2026FA0000208Feeder Cable · wrong partDURING PREPARATION FOR NR 2 ENG COOLING BAROMETRIC SWITCH OPC FOUND DAMAGED SCREW AT NACELLE ZONE VENT SHUTOFF VALVE. AFTER INVESTIGATION FOUND THAT THIS SCREW WAS TOUCHING THE FEEDER CABLES. TWO CABLE GOT DAMAGED AND PRODUCED ARCING TO THE VALVE HOUSING SCREWSDR UIEA2026012000015Elt · inoperativeELT LOCATED RT AFT OF OBSERVERS SEAT INOP. REQ REPLACEMENT(<P>R/R ELT FROM RH AFT OF OBSERVERS SEAT IAW B767 AMM 25-26-03. NO DEFECTS NOTED</P>)SDR UIEA2025122701359Elt · looseELT NEAR RH CB PANEL TAPE IS LOOSE & 1 LATCH WILL NOT CLOSE. INSTALLED TAMPER TAPE ON FWD ELT IAW AMM 25-61-05-200-801. NO DEFECTS NOTED.SDR UIEA2025102001275Engine · no discrepancyON TAKE OFF ROLL, RECEIVED LT & RT ENG BLEED EICAS MSG & MASTER CAUTION LIGHT. RTO, PERFORMED BITE TEST IAW FIM 36-20 FT 804. FOUND 0 MSG ON THIS FLT LEG. EICAS MSG CLEARED. ALSO, PERFORMED WEU TEST IAW AMM 31-51-00, OPS CHK GOOD. FOUND MSG TO BE NORMAL.SDR UIEA2025101001264Shutoff Valve · faultedC HYD SYS PRESS EICAS MESSAGE DISPLAYED IN FLIGHT, HMG INOP. HYD PRESS INDICATION OPERATES NORMAL PER AMM 29-31-00-001. PERFORMED ADP SYS TEST PER B767 AMM 29-11-00. NO DEFECTS NOTED. TRANSFER TO DMI 239843 PER MEL 24-25-01-01D CAT A. R & R SOV PER AMM 24-2SDR UIEA2025101001266Regulator · leakingPAX OXYGEN TANK (BOTTLE 2) REGULATOR LEAK(<P>REMOVED AND REPLACED PAX OXYGEN TANK REGULATOR IAW B767 AMM 35-11-03. LEAK & PRESSURE CHK OK</P>)SDR UIEA2025080401084Flashlight · no discrepancyL1 DOOR ENTRY WAY EMERGENCY FLASHLIGHT INOPERATIVE. OPS CHK ENTRY WAY FLASHLIGHT IAW AMM 25-05-03, OPS CHECK GOOD.SDR UIEA2025073001069Lens · scratchedOBSERVER SMOKE GOGGLES LENS SCRATCHED. REPLACED OBS SMOKE GOGGLE PER IPC 25-64-54-01B ITEM 30. NO FURTHER DEFECTS NOTED.SDR UIEA2025071100925Structure · no discrepancyAT APPROXIMATELY 310 KIAS, APPROXIMATELY 10 KNOTS OVERSPEED WITH OVSPD WARNING WHILE IN DESCENT 0 FLAPS ADVISE FLT LEVEL 200. WORK WITH MCC AND PER AMM 05-51-08. COMPLETED PHASE 1 INSPECTION, NO DAMAGE WAS FOUND. LOG ITEM CLOSED.SDR UIEA2025070400832Fmc · odorCAPT REPORTS ELECTRICAL ODOR IN COCKPIT AFTER BLOCK, DETERMINED CAPT FMS CDU BLANKED AND CIRCUIT BREAKER OPEN.(<P>COLLARED CIRCUIT BREAKER, PART ORDERED FOR NGO. REPLACED CA FMC CDU IAW AMM 34-61-02. CLEARED MDDR 233639. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025012600108Elt · abnormalELT AT ENTRANCE HAS MASKING TAPE OVER THE WATER SOLUABLE TAPE(<P>R/R L1 DOOR L1 & BRACKET STRAP OPS CHK GOOD IAW AMM 25-63-03-400-802 & AIPC 25-63-52-97. DMI 224932 CLOSED</P>)SDR UIEA2024111501092Lamp · burned outEMERGENCY LIGHTS "UNARMED" DISCRETE LIGHT HAS BURNED OUT LIGHT BULB(<P>RELAMPED EMERGENCY UNARMED LIGHT PER AMM 33-10-00. OPS CHECK NORMAL</P>)SDR UIEA2024101801052Screen · cloggedATB - FWD EQUIP OVHT EICAS MSG. WENT TO STBY IAW QRH, DID NOT CLEAR. WENT TO OVRD IAW QRH, EICAS MSG CLEARED. DID NOT ENTER ETOPS(<P>FOUND EQPT COOL SUPPLY AIR INLET GRILL DIRTY AND PARTIALLY BLOCKED. CLEANED PER AMM 21-58-10. FOUND SUPPLY FAN SCREEN EQUIPMENTSDR UIEA2024092400931Pdu · leakingRIGHT WING, SLAT PDU INBOARD, WITH EVIDENCE OF HYD LEAK(<P>RIGHT WING, SLAT PDU INBOARD WERE REPLACED IAW AMM 27-81-10-424-023 AND AMM 27-81-10-024-001, LEAK CHECK WERE PERFORMED, NO LEAK WAS FOUND.</P>)SDR UIEA2024092400932Skin · detachedRH WING, SLAT #7, SURFACE INNER SIDE, UPPER AND LOWER AREA WITH SEVERAL POINTS OF DETACHED.(<P>RH WING, SLAT #7, WAS REPLACED IAW AMM 27-81-01-024-001 AND AMM 27- 81-01-424-143. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092400933Skin · corrodedRH WING, SLAT #7, SURFACE INNER SIDE, AREA UPPER MIDDLE, WITH TWO POINTS OF CORROSION EVIDENCE.(<P>RH WING, SLAT #7, WAS REPLACED IAW AMM 27-81-01-024-001 AND AMM 27-81- 01-424-143. OPS CHECK GOOD</P>)SDR UIEA2024092400934Pca · leakingLEFT WING, OUTER AILERON, INNER PCA, WITH EVIDENCE OF HYD LEAKAGE(<P>LEFT WING, OUTER AILERON, INNER PCA, WAS REPLACED, ADJUSTED AND LEAK TEST WAS PERFORMED IAW AMM 27-11- 49-422-028 AND AMM 27-11-49-022-014. NO LEAKS WERE FOUND.</P>)SDR UIEA2024092400935Skin · detachedLEFT WING, LEFT INBOARD AILERON, LEADING EDGE MIDDLE AREA DETACHED.(<P>LEFT WING, INBOARD AILERON, LEADING EDGE MIDDLE AREA WAS REPAIRED IAW SRM 57-60-01-2R-1 FIG 201 SHEET 9 PAG 1-10 AND SRM 51-70-17-0G-0 PAR 4G FIG 15</P>)SDR UIEA2024092400936Fuel Cell · leakingRH WING, FUEL LEAK ON LOWER SKIN AND SPLICE BTW WBL 97.95. TO WS 226.3 AND BTW STGR L7 TO L15(<P>FUEL LEAK WAS REPAIRED AND LEAK TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013</P>)SDR UIEA2024092400937Fire Bottle · expiredENG 2 BOTTLE EXTINGUISHER #2 DATE OFF(<P>ENG 2 BOTTLE EXTINGUISHER #2 WAS REPLACED AND TEST WAS SATISFACTORY IAW AMM 26-21-03-424-095</P>)SDR UIEA2024092400938Skin · crackedDOUBLER INSTALLED ON EMERGENCY LIGHT OF THE MCD SURROUND SKIN CIRCUMFERENTIAL SPLICE STA 654+22 AT AFT FASTENER ROW IN THE SECOND LOWER FASTENER HOLE WITH CRACK INDICATION.(<P>THE SECOND LOWER FASTENER HOLE WAS ENLARGE UP TO SECOND OVERSIZE AND WAS REPAIRED IASDR UIEA2024092400939Skin · crackedAT FWD ENTRY DOOR CUTOUT AFT LOWER CORNER ONE HOLE WITH CRACK INDICATION ON BOTH STRUCTURES FUSELAGE SKIN AND BEAR STRAP APPROX TO THE 10 O´CLOCK.(<P>HOLE INDICATION ON BOTH STRUCTURES FUSELAGE SKIN AND BEAR STRAP APPROX TO THE 10 O´CLOCK. CRACK WAS REPAIREDSDR UIEA2024092400940Skin · crackedAT FWD SERVICE DOOR CUTOUT AFT LOWER CORNER TWO HOLES WITH CRACK INDICATION ON FUSELAGE SKIN APPROX 10 O´CLOCK.(<P>AT FWD SERVICE DOOR CUTOUT AFT LOWER CORNER ON FUSELAGE SKIN APPROX 10 O´CLOCK DAMAGES WERE REPAIRED IAW FVCI #24153-2 A FAA FORM 8110-3 (09/20SDR UIEA2024092400941Skin · wornLH WING, AT WBL 97.5 , BTW STA 785.9 AND STA 830 WING LOWER SKIN WITH WEAR.(<P>LH WING, AT WBL 97.5 , BTW STA 785.9 AND STA 830 WING LOWER SKIN DAMAGE WAS REPAIRED IAW FVCI #24153-3 AN APPROVAL FORM FAA 8110-3 WAS ISSUED. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092400942Seal · wornLEFT WING, OUTBD WING TIP, ANTI-COLLISION LIGHT WITH WORN SEAL(<P>THE WORN SEAL ON LEFT WING, OUTBD WING TIP, ANTI-COLLISION LIGHT WAS REPLACED IAW AMM 33-44-01-002-017. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092400943Frame · corrodedFWD CARGO COMPARTMENT, EVIDENCE OF CORROSION ON WEB FRAME AT BS 764 BTW S37L AND S38L.(<P>WEB FRAME AT BS 764 BTW S37L AND S38L. PAINT WAS REMOVED, REWORKED, INSPECTED AND ALLOWABLE LIMITS FOUND. ALLODINE, PRIMER AND PAINT WAS RESTORED IAW SRM 53-00-07-1A-1. NSDR UIEA2024092400944Jumper · brokenRH WING, FUEL TANK, INSIDE ACCESS PANEL 632DB, BROKEN BONDING JUMPER (2E/A'S) BTW RIB 6/7.(<P>THE BROKEN BONDING JUMPER (2E/A'S) ON RH WING, FUEL TANK, INSIDE ACCESS PANEL 632DB, BTW RIB 6/7 WERE REPLACED IAW SWPM 20-20-10 REV</P>)SDR UIEA2024092400945Sealant · missingRH WING, INSIDE FUEL TANK REAR SPAR, MISSING FILLET SEALANT ON SHUT OFF VALVE (2 E/A'S) BTW RIB 1/6.(<P>RH WING, INSIDE FUEL TANK REAR SPAR, FILLET SEALANT ON SHUT OFF VALVE WAS APPLIED IAW AMM TASK 28-21-02-404-021. NO FURTHER DEFECT NOTED</P>)SDR UIEA2024092400946Actuator · leakingLH WING, LATERAL CENTRAL CONTROL ACTUATORS UPPER AND LOWER (M274 AND M276) LCCA WITH HYDRAULIC LEAK.(<P>LH WING, LATERAL CENTRAL CONTROL ACTUATORS UPPER AND LOWER (M274 AND M276) LCCA LEAK CHECK WAS PERFORMED, NO LEAKS WERE FOUND</P>)SDR UIEA2024092500948Access Panel · puncturedSYS LH HYD BAY, (ACCESS PANEL 437BL), SURFACE INERSIDE AREA LOWER RIGH TSIDE, ANGLE WITH PUNCTURE.(<P>SURFACE INERSIDE AREA LOWER RIGHTSIDE, ANGLE WAS REPAIRED IAW TRE 6754195 ISSUED DATE 13/SEP/24 & CMA-TLS-24-0190, RDR WAS ISSUED. NO FURTHER DEFECTS NOTED</PSDR UIEA2024092500949Access Panel · wornSYST LH HYD BAY, (ACCESS PANEL: 437BL) INNER RIGHTSIDE, LOWER REAR CORNER AREA, PLATE-STRICKER WITH WORN.(<P>LOWER REAR CORNER AREA, PLATE ASSY WAS REPLACED SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092500950Fire Seal · detachedENGINE ONE NACELLE STRUT FIRE SEAL DETACHED ON FWD CORNER LH AND RH SIDE(<P>ENGINE ONE NACELLE STRUT FWD CORNER LH AND RH SIDE; SEAL WAS REPAIRED IAW AMM 54-54-03-308-014. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092500951Fill Port · corrodedRH WING, UPPER SURFACE, BASE OF OVERWING FILL PORT ADAPTER WITH EVIDENCE OF CORROSION(<P>OVERWING FILL PORT ADAPTER. CORROSION LEVE 1 WAS REWORKED, INSPECTED AND ALLOWABLE LIMITS FOUND IAW SRM 57-20-01-1A-1</P>)SDR UIEA2024092500952Bracket · corrodedBULK CARGO COMPARTMENT, AFT BULKHEAD, AFT STA 1540, BTW S-38R, AND S-39R, BRACKET WITH EVIDENCE OF CORROSION.(<P>BRACKET WAS REPLACED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092500953Bulkhead · corrodedBULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38R WITH EVIDENCE OF CORROSION.(<P>BULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38R WAS REPAIRED IAW SRM 53-00-03-2R-2. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092500954Bulkhead · corrodedBULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38L WITH EVIDENCE OF CORROSION.(<P>BULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38L WAS REPAIRED IAW SRM 53-00-03-2R-2</P>)SDR UIEA2024092500955Fire Seal · brokenENG 2, RIGHT T/R DOOR, UPPER AFTER SECTION, FIRE SEAL BROKEN(<P>FIRE SEAL WAS REPAIRED IAW AMM 78-00-00-038-001-N00. NO FURTHER DEFECTS NOTED</P>)
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