ANC MX PERFORMED FIM 32-09 - [SDR UIEA2026052700365](https://openairdocs.org/sdr/UIEA2026052700365.md): Switch · faulted · May 24, 2026 · N1619A · Boeing 7673Y0 · Door Warning System > AFTER 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
) - [SDR UIEA2026052400347](https://openairdocs.org/sdr/UIEA2026052400347.md): Line · disconnected · May 24, 2026 · N1619A · Boeing 7673Y0 · Fuel Controlling System > SHORTLY 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 G - [SDR UIEA2026032700108](https://openairdocs.org/sdr/UIEA2026032700108.md): Switch · shorted · May 12, 2026 · N1619A · Boeing 7673Y0 · Engine Cooling System > DURING 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 SCR - [SDR UIEA2026050500297](https://openairdocs.org/sdr/UIEA2026050500297.md): Sign · broken · May 12, 2026 · N1619A · Boeing 7673Y0 · Emergency Lighting > DURING 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 UIEA2026050600298](https://openairdocs.org/sdr/UIEA2026050600298.md): Skin · damaged · May 12, 2026 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/Skin > DURING 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 UIEA2026050600300](https://openairdocs.org/sdr/UIEA2026050600300.md): Skin · damaged · May 12, 2026 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/Skin > DURING 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 UIEA2026050600301](https://openairdocs.org/sdr/UIEA2026050600301.md): Skin · damaged · May 12, 2026 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/Skin > DURING 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 UIEA2026050600302](https://openairdocs.org/sdr/UIEA2026050600302.md): Skin · dented · May 12, 2026 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/Skin > FOUND 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 UIEA2026050700305](https://openairdocs.org/sdr/UIEA2026050700305.md): Skin · damaged · May 12, 2026 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/Skin > DURING 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 2026FA0000208](https://openairdocs.org/sdr/2026FA0000208.md): Feeder Cable · wrong part · Mar 24, 2026 · N1619A · Boeing 7673Y0 · Electrical Power System Wiring > DURING 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 SCREW - [SDR UIEA2026012000015](https://openairdocs.org/sdr/UIEA2026012000015.md): Elt · inoperative · Jan 15, 2026 · N1619A · Boeing 7673Y0 · Emergency Locator Beacon > ELT LOCATED RT AFT OF OBSERVERS SEAT INOP. REQ REPLACEMENT(R/R ELT FROM RH AFT OF OBSERVERS SEAT IAW B767 AMM 25-26-03. NO DEFECTS NOTED
) - [SDR UIEA2025122701359](https://openairdocs.org/sdr/UIEA2025122701359.md): Elt · loose · Dec 27, 2025 · N1619A · Boeing 7673Y0 · Emergency Locator Beacon > ELT 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 UIEA2025102001275](https://openairdocs.org/sdr/UIEA2025102001275.md): Engine · no discrepancy · Oct 20, 2025 · N1619A · Boeing 7673Y0 · Central Warning > ON 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 UIEA2025101001264](https://openairdocs.org/sdr/UIEA2025101001264.md): Shutoff Valve · faulted · Oct 10, 2025 · N1619A · Boeing 7673Y0 · Hydraulic Indicating System > C 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 24-2 - [SDR UIEA2025101001266](https://openairdocs.org/sdr/UIEA2025101001266.md): Regulator · leaking · Oct 9, 2025 · N1619A · Boeing 7673Y0 · Crew Oxygen System > PAX OXYGEN TANK (BOTTLE 2) REGULATOR LEAK(REMOVED AND REPLACED PAX OXYGEN TANK REGULATOR IAW B767 AMM 35-11-03. LEAK & PRESSURE CHK OK
) - [SDR UIEA2025080401084](https://openairdocs.org/sdr/UIEA2025080401084.md): Flashlight · no discrepancy · Aug 4, 2025 · N1619A · Boeing 7673Y0 · Emergency Equipment > L1 DOOR ENTRY WAY EMERGENCY FLASHLIGHT INOPERATIVE. OPS CHK ENTRY WAY FLASHLIGHT IAW AMM 25-05-03, OPS CHECK GOOD. - [SDR UIEA2025073001069](https://openairdocs.org/sdr/UIEA2025073001069.md): Lens · scratched · Jul 30, 2025 · N1619A · Boeing 7673Y0 · Emergency Equipment > OBSERVER SMOKE GOGGLES LENS SCRATCHED. REPLACED OBS SMOKE GOGGLE PER IPC 25-64-54-01B ITEM 30. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025071100925](https://openairdocs.org/sdr/UIEA2025071100925.md): Structure · no discrepancy · Jul 11, 2025 · N1619A · Boeing 7673Y0 · Standard Practices/Structures > AT 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 UIEA2025070400832](https://openairdocs.org/sdr/UIEA2025070400832.md): Fmc · odor · Jul 4, 2025 · N1619A · Boeing 7673Y0 · Flight Management Computing Hardware System > CAPT REPORTS ELECTRICAL ODOR IN COCKPIT AFTER BLOCK, DETERMINED CAPT FMS CDU BLANKED AND CIRCUIT BREAKER OPEN.(COLLARED CIRCUIT BREAKER, PART ORDERED FOR NGO. REPLACED CA FMC CDU IAW AMM 34-61-02. CLEARED MDDR 233639. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025012600108](https://openairdocs.org/sdr/UIEA2025012600108.md): Elt · abnormal · Jan 27, 2025 · N1619A · Boeing 7673Y0 · Emergency Locator Beacon > ELT AT ENTRANCE HAS MASKING TAPE OVER THE WATER SOLUABLE TAPE(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
) - [SDR UIEA2024111501092](https://openairdocs.org/sdr/UIEA2024111501092.md): Lamp · burned out · Nov 15, 2024 · N1619A · Boeing 7673Y0 · Emergency Lighting > EMERGENCY LIGHTS "UNARMED" DISCRETE LIGHT HAS BURNED OUT LIGHT BULB(RELAMPED EMERGENCY UNARMED LIGHT PER AMM 33-10-00. OPS CHECK NORMAL
) - [SDR UIEA2024101801052](https://openairdocs.org/sdr/UIEA2024101801052.md): Screen · clogged · Oct 18, 2024 · N1619A · Boeing 7673Y0 · Air Distribution System > ATB - 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(FOUND EQPT COOL SUPPLY AIR INLET GRILL DIRTY AND PARTIALLY BLOCKED. CLEANED PER AMM 21-58-10. FOUND SUPPLY FAN SCREEN EQUIPMENT - [SDR UIEA2024092400931](https://openairdocs.org/sdr/UIEA2024092400931.md): Pdu · leaking · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Hydraulic System, Main > RIGHT WING, SLAT PDU INBOARD, WITH EVIDENCE OF HYD LEAK(
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.
) - [SDR UIEA2024092400932](https://openairdocs.org/sdr/UIEA2024092400932.md): Skin · detached · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Ailerons > RH WING, SLAT #7, SURFACE INNER SIDE, UPPER AND LOWER AREA WITH SEVERAL POINTS OF DETACHED.(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
) - [SDR UIEA2024092400933](https://openairdocs.org/sdr/UIEA2024092400933.md): Skin · corroded · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Leading Edge Devices > RH WING, SLAT #7, SURFACE INNER SIDE, AREA UPPER MIDDLE, WITH TWO POINTS OF CORROSION EVIDENCE.(RH WING, SLAT #7, WAS REPLACED IAW AMM 27-81-01-024-001 AND AMM 27-81- 01-424-143. OPS CHECK GOOD
) - [SDR UIEA2024092400934](https://openairdocs.org/sdr/UIEA2024092400934.md): Pca · leaking · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Hydraulic System, Main > LEFT WING, OUTER AILERON, INNER PCA, WITH EVIDENCE OF HYD LEAKAGE(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.
) - [SDR UIEA2024092400935](https://openairdocs.org/sdr/UIEA2024092400935.md): Skin · detached · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Ailerons > LEFT WING, LEFT INBOARD AILERON, LEADING EDGE MIDDLE AREA DETACHED.(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
) - [SDR UIEA2024092400936](https://openairdocs.org/sdr/UIEA2024092400936.md): Fuel Cell · leaking · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuel Storage > RH WING, FUEL LEAK ON LOWER SKIN AND SPLICE BTW WBL 97.95. TO WS 226.3 AND BTW STGR L7 TO L15(FUEL LEAK WAS REPAIRED AND LEAK TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013
) - [SDR UIEA2024092400937](https://openairdocs.org/sdr/UIEA2024092400937.md): Fire Bottle · expired · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fire Bottle, Fixed > ENG 2 BOTTLE EXTINGUISHER #2 DATE OFF(ENG 2 BOTTLE EXTINGUISHER #2 WAS REPLACED AND TEST WAS SATISFACTORY IAW AMM 26-21-03-424-095
) - [SDR UIEA2024092400938](https://openairdocs.org/sdr/UIEA2024092400938.md): Skin · cracked · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/Skin > DOUBLER 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.(THE SECOND LOWER FASTENER HOLE WAS ENLARGE UP TO SECOND OVERSIZE AND WAS REPAIRED IA - [SDR UIEA2024092400939](https://openairdocs.org/sdr/UIEA2024092400939.md): Skin · cracked · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/Skin > AT 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.(
HOLE INDICATION ON BOTH STRUCTURES FUSELAGE SKIN AND BEAR STRAP APPROX TO THE 10 O´CLOCK. CRACK WAS REPAIRED - [SDR UIEA2024092400940](https://openairdocs.org/sdr/UIEA2024092400940.md): Skin · cracked · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/Skin > AT FWD SERVICE DOOR CUTOUT AFT LOWER CORNER TWO HOLES WITH CRACK INDICATION ON FUSELAGE SKIN APPROX 10 O´CLOCK.(
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 (09/20 - [SDR UIEA2024092400941](https://openairdocs.org/sdr/UIEA2024092400941.md): Skin · worn · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Wing, Plate/Skin > LH WING, AT WBL 97.5, BTW STA 785.9 AND STA 830 WING LOWER SKIN WITH WEAR.(
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
) - [SDR UIEA2024092400942](https://openairdocs.org/sdr/UIEA2024092400942.md): Seal · worn · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Exterior Lighting > LEFT WING, OUTBD WING TIP, ANTI-COLLISION LIGHT WITH WORN SEAL(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
) - [SDR UIEA2024092400943](https://openairdocs.org/sdr/UIEA2024092400943.md): Frame · corroded · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Main, Frame > FWD CARGO COMPARTMENT, EVIDENCE OF CORROSION ON WEB FRAME AT BS 764 BTW S37L AND S38L.(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. N - [SDR UIEA2024092400944](https://openairdocs.org/sdr/UIEA2024092400944.md): Jumper · broken · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Wing System Wiring > RH WING, FUEL TANK, INSIDE ACCESS PANEL 632DB, BROKEN BONDING JUMPER (2E/A'S) BTW RIB 6/7.(
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
) - [SDR UIEA2024092400945](https://openairdocs.org/sdr/UIEA2024092400945.md): Sealant · missing · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Wing Main, Frame Structure > RH WING, INSIDE FUEL TANK REAR SPAR, MISSING FILLET SEALANT ON SHUT OFF VALVE (2 E/A'S) BTW RIB 1/6.(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
) - [SDR UIEA2024092400946](https://openairdocs.org/sdr/UIEA2024092400946.md): Actuator · leaking · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Hydraulic System, Main > LH WING, LATERAL CENTRAL CONTROL ACTUATORS UPPER AND LOWER (M274 AND M276) LCCA WITH HYDRAULIC LEAK.(LH WING, LATERAL CENTRAL CONTROL ACTUATORS UPPER AND LOWER (M274 AND M276) LCCA LEAK CHECK WAS PERFORMED, NO LEAKS WERE FOUND
) - [SDR UIEA2024092500948](https://openairdocs.org/sdr/UIEA2024092500948.md): Access Panel · punctured · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Nacelle/Pylon, Plate/Skin > SYS LH HYD BAY, (ACCESS PANEL 437BL), SURFACE INERSIDE AREA LOWER RIGH TSIDE, ANGLE WITH PUNCTURE.(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
SYST LH HYD BAY, (ACCESS PANEL: 437BL) INNER RIGHTSIDE, LOWER REAR CORNER AREA, PLATE-STRICKER WITH WORN.(LOWER REAR CORNER AREA, PLATE ASSY WAS REPLACED SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2024092500950](https://openairdocs.org/sdr/UIEA2024092500950.md): Fire Seal · detached · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Nacelle/Pylon, Main Frame > ENGINE ONE NACELLE STRUT FIRE SEAL DETACHED ON FWD CORNER LH AND RH SIDE(ENGINE ONE NACELLE STRUT FWD CORNER LH AND RH SIDE; SEAL WAS REPAIRED IAW AMM 54-54-03-308-014. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2024092500951](https://openairdocs.org/sdr/UIEA2024092500951.md): Fill Port · corroded · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Wing Main, Frame Structure > RH WING, UPPER SURFACE, BASE OF OVERWING FILL PORT ADAPTER WITH EVIDENCE OF CORROSION(OVERWING FILL PORT ADAPTER. CORROSION LEVE 1 WAS REWORKED, INSPECTED AND ALLOWABLE LIMITS FOUND IAW SRM 57-20-01-1A-1
) - [SDR UIEA2024092500952](https://openairdocs.org/sdr/UIEA2024092500952.md): Bracket · corroded · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Miscellaneous Structure > BULK CARGO COMPARTMENT, AFT BULKHEAD, AFT STA 1540, BTW S-38R, AND S-39R, BRACKET WITH EVIDENCE OF CORROSION.(BRACKET WAS REPLACED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2024092500953](https://openairdocs.org/sdr/UIEA2024092500953.md): Bulkhead · corroded · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Main, Bulkhead > BULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38R WITH EVIDENCE OF CORROSION.(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
) - [SDR UIEA2024092500954](https://openairdocs.org/sdr/UIEA2024092500954.md): Bulkhead · corroded · Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Main, Bulkhead > BULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38L WITH EVIDENCE OF CORROSION.(BULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38L WAS REPAIRED IAW SRM 53-00-03-2R-2
) Next page: https://openairdocs.org/aircraft/N1619A/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 = 'N1619A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N1619A/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.