# N1619A: 1994 Boeing 767-3Y0 - Status: Valid registration - Airframe: [Boeing 767-3Y0](https://openairdocs.org/model/boeing-767-3y0) (registry code 1385240, 190 seats) - Engine: [Pratt & Whitney PW4060](https://openairdocs.org/engine/pratt-whitney-pw4060) (registry code 52140) - Data sheets: [TCDS E24NE](https://openairdocs.org/tcds/E24NE) (Pratt & Whitney Division) (OpenAirDocs) - Serial number: 26208 - Year built: 1994 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 21, 2018 - Certificate issued: December 28, 2017 - Expires: December 31, 2027 - Mode S code: A0F8F9 - Registered owner: [Atlas Air Inc](https://openairdocs.org/faa-owner/ATLAS%20AIR%20INC) - Location: [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase) - Owner type: Corporation - Owner's area on the map: 41.0382° N, 73.7107° W: Placed by OpenAirDocs at the center of ZIP code 10577, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1619A - Page: https://openairdocs.org/aircraft/N1619A From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 24 in force ### Matched by airframe (Boeing 767-3Y0) None in force. ### Matched by engine (Pratt & Whitney PW4060) - [AD 2026-21-06](https://openairdocs.org/ad/2026-21-06): Engine Fuel and Control · Pratt & Whitney Division PW4052, PW4056, PW4060 and 10 more. Effective Nov 23, 2026 - [AD 2018-13-02](https://openairdocs.org/ad/2018-13-02): Turbine Engine Combustion Section · Pratt & Whitney Division PW4052, PW4056, PW4060 and 7 more. Effective Jul 20, 2018 - [AD 2016-08-09](https://openairdocs.org/ad/2016-08-09): HPC 10th stage disk · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Jun 1, 2016 - [AD 2015-22-03](https://openairdocs.org/ad/2015-22-03): LPT 4th stage IAS · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Dec 1, 2015 - [AD 2012-22-16](https://openairdocs.org/ad/2012-22-16): 3rd stage LPT duct segments · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Dec 19, 2012 - [AD 2012-14-09](https://openairdocs.org/ad/2012-14-09): 3rd and 4th stage vane fractures · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Nov 7, 2012 - [AD 2012-18-17](https://openairdocs.org/ad/2012-18-17): HPC drum rotor disk assembly · Pratt & Whitney Division PW4052, PW4056, PW4060 and 16 more. Effective Oct 22, 2012 - [AD 2012-18-03](https://openairdocs.org/ad/2012-18-03): 1st stage HPT air seal rings · Pratt & Whitney Division PW4050, PW4052, PW4056 and 18 more. Effective Oct 11, 2012 - [AD 2012-16-01](https://openairdocs.org/ad/2012-16-01): High-pressure turbine (HPT) stage 1 front hubs · Pratt & Whitney Division PW4052, PW4056, PW4060 and 14 more. Effective Sep 28, 2012 - [AD 2012-06-18](https://openairdocs.org/ad/2012-06-18): Engine · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Apr 27, 2012 - [AD 2012-04-04](https://openairdocs.org/ad/2012-04-04): fuel metering units (FMUs) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Apr 5, 2012 - [AD 2011-25-09](https://openairdocs.org/ad/2011-25-09): PW4000 turbofan engines · Pratt & Whitney Division PW4050, PW4052, PW4056 and 18 more. Effective Jan 10, 2012 - [AD 2010-24-14](https://openairdocs.org/ad/2010-24-14): HPC 10th stage disk · Pratt & Whitney Division PW4050, PW4052, PW4056 and 17 more. Effective Jan 21, 2011 - [AD 2010-24-09](https://openairdocs.org/ad/2010-24-09): No. 3 bearing oil pressure tubes · Pratt & Whitney Division PW4050, PW4052, PW4056 and 34 more. Effective Dec 28, 2010 - [AD 2008-24-13](https://openairdocs.org/ad/2008-24-13): Electronic engine controls (EECs) · Pratt & Whitney Division PW4052, PW4056, PW4060 and 6 more. Effective Jan 8, 2009 - [AD 2005-25-09](https://openairdocs.org/ad/2005-25-09): Engine manufacturer's time limits section (TLS) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 26 more. Effective Jun 12, 2006 - [AD 2003-19-15](https://openairdocs.org/ad/2003-19-15): High-Pressure-Compressor (HPC) Surges · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Oct 30, 2003 - [AD 2002-12-15](https://openairdocs.org/ad/2002-12-15): Front Drum Rotors · Pratt & Whitney Division PW4052, PW4056, PW4060 and 6 more. Effective Jul 31, 2002 - [AD 2001-05-07](https://openairdocs.org/ad/2001-05-07): Low Pressure Turbine (LPT) 4th Stage Air Seal · Pratt & Whitney Division PW4052, PW4056, PW4060 and 11 more. Effective Mar 30, 2001 - [AD 98-23-08](https://openairdocs.org/ad/98-23-08): High Pressure Compressor Blade Tips · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Jan 12, 1999 - [AD 98-19-03](https://openairdocs.org/ad/98-19-03): High Pressure Turbine Rotating Airseals · Pratt & Whitney Division PW4052, PW4056, PW4060 and 9 more. Effective Nov 9, 1998 - [AD 96-13-08](https://openairdocs.org/ad/96-13-08): AFT Cascade Support Frame Assembly · Pratt & Whitney assembly Part Number 221D5015, Revision A (STC SE744NE). Effective Aug 1, 1996 - [AD 93-08-16](https://openairdocs.org/ad/93-08-16): Fuel Pump · Pratt & Whitney Division PW4050, PW4052, PW4056 and 2 more. Effective Jul 12, 1993 - [AD 90-22-02](https://openairdocs.org/ad/90-22-02): Low Pressure Turbine Shaft · Pratt & Whitney Division PW4050, PW4052, PW4056 and 6 more. Effective Oct 18, 1990 ### Historical (superseded or no longer in force) - [AD 2010-18-13](https://openairdocs.org/ad/2010-18-13) (historical): Blade · Pratt & Whitney Division PW4052, PW4056, PW4060 and 16 more. Effective Oct 18, 2010 - [AD 2003-11-18](https://openairdocs.org/ad/2003-11-18) (historical): High-Pressure-Compressor (HPC) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Jul 7, 2003 - [AD 2002-21-10](https://openairdocs.org/ad/2002-21-10) (historical): High pressure compressor (HPC) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Nov 12, 2002 - [AD 2002-03-08](https://openairdocs.org/ad/2002-03-08) (historical): Time Limits Section of Engine Manuals (EM's) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 25 more. Effective Apr 16, 2002 - [AD 2001-25-11](https://openairdocs.org/ad/2001-25-11) (historical): Compressor Surges · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Jan 17, 2002 - [AD 2001-20-13](https://openairdocs.org/ad/2001-20-13) (historical): High Pressure Compressor Front Drum Rotors · Pratt & Whitney Division PW4052, PW4056, PW4060 and 6 more. Effective Nov 16, 2001 - [AD 2001-15-12](https://openairdocs.org/ad/2001-15-12) (historical): High Pressure Compressors (HPC) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Aug 10, 2001 - [AD 2001-09-07](https://openairdocs.org/ad/2001-09-07) (historical): High Pressure Compressor (HPC) Surge · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective May 14, 2001 - [AD 2001-08-52](https://openairdocs.org/ad/2001-08-52) (historical): Multiple-engine power loss due to HPC surges · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more - [AD 2000-25-06](https://openairdocs.org/ad/2000-25-06) (historical): Low Pressure Turbine (LPT) 4th Stage Air Seal · Pratt & Whitney Division PW4052, PW4056, PW4060 and 11 more. Effective Dec 29, 2000 - [AD 2000-22-01](https://openairdocs.org/ad/2000-22-01) (historical): High Pressure Compressor Cutback Stator · Pratt & Whitney Division PW4050, PW4052, PW4056 and 6 more. Effective Nov 9, 2000 - [AD 2000-12-02](https://openairdocs.org/ad/2000-12-02) (historical): Critical Life-Limited Part · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Sep 13, 2000 - [AD 99-17-16](https://openairdocs.org/ad/99-17-16) (historical): Pratt & Whitney Division PW4050, PW4052, PW4056 and 11 more. Effective Sep 24, 1999 - [AD 99-08-15](https://openairdocs.org/ad/99-08-15) (historical): Pratt & Whitney Division PW4050, PW4052, PW4056 and 20 more. Effective May 13, 1999 ## Information bulletins (advisory) (5 in force) - [SAIB 2025-06](https://openairdocs.org/saib/2025-06): High Pressure Turbines. Issued Jul 22, 2025 - [SAIB NE-19-02](https://openairdocs.org/saib/NE-19-02): Turbine Engine Compressor Section -- Low-pressure turbine uncontainment. Issued Feb 19, 2019 - [SAIB NE-16-01R1](https://openairdocs.org/saib/NE-16-01R1): Turbine Section. Issued Jan 14, 2016 - [SAIB NE-15-19](https://openairdocs.org/saib/NE-15-19): Turbine Section. Issued Jul 14, 2015 - [SAIB NE-13-31](https://openairdocs.org/saib/NE-13-31): Turbine Engine Oil System Scavenge Oil Tube Coking and Proper Cleaning at Overhaul. Issued May 9, 2013 - [SAIB NE-16-01](https://openairdocs.org/saib/NE-16-01) (historical): Turbine Section. Issued Oct 5, 2015 ## NTSB investigations None matched to N1619A. ## FAA accident and incident reports None matched to N1619A. ## Service difficulty reports (296, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UIEA2026100800969](https://openairdocs.org/sdr/UIEA2026100800969), Oct 7, 2026: PSEU. FAULTED. ENTRY 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 UIEA2026100500945](https://openairdocs.org/sdr/UIEA2026100500945), Oct 5, 2026: PROXIMITY SENSOR. FALSE ACTIVATION. 40 MINS INTO FLIGHT @ FL340, RT LANDING GEAR DISCREET LIGHTS, AMBER REV LIGHT, AND ENTRY DOORS/EMER DOORS DISCREET LIGHTS ILLUMINATED. LANDING GEAR DISCREET LIG - [SDR UIEA2026100500950](https://openairdocs.org/sdr/UIEA2026100500950), Oct 4, 2026: BATTERY. INOPERATIVE. FLASHLIGHT 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 - [SDR UIEA2026100400943](https://openairdocs.org/sdr/UIEA2026100400943), Oct 4, 2026: PSEU. INOPERATIVE. APPROX 1 HR AFTER T/O DURING CRUISE @ FL360, LEFT LANDING GEAR DISCRETE LIGHT ILLUMINATED. INTERMITTENT - RT LANDING GEAR DISCRETE LIGHT ILLUMINATED. IN FLIGHT - [SDR UIEA2026052700365](https://openairdocs.org/sdr/UIEA2026052700365), May 24, 2026: SWITCH. FAULTED. 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), May 24, 2026: LINE. DISCONNECTED. 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 - [SDR UIEA2026032700108](https://openairdocs.org/sdr/UIEA2026032700108), May 12, 2026: SWITCH. SHORTED. 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 - [SDR UIEA2026050500297](https://openairdocs.org/sdr/UIEA2026050500297), May 12, 2026: SIGN. BROKEN. 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 R - [SDR UIEA2026050600298](https://openairdocs.org/sdr/UIEA2026050600298), May 12, 2026: SKIN. DAMAGED. 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- - [SDR UIEA2026050600300](https://openairdocs.org/sdr/UIEA2026050600300), May 12, 2026: SKIN. DAMAGED. 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 - [SDR UIEA2026050600301](https://openairdocs.org/sdr/UIEA2026050600301), May 12, 2026: SKIN. DAMAGED. 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 - [SDR UIEA2026050600302](https://openairdocs.org/sdr/UIEA2026050600302), May 12, 2026: SKIN. DENTED. 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- - [SDR UIEA2026050700305](https://openairdocs.org/sdr/UIEA2026050700305), May 12, 2026: SKIN. DAMAGED. 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- - [SDR 2026FA0000208](https://openairdocs.org/sdr/2026FA0000208), Mar 24, 2026: FEEDER CABLE. WRONG PART. 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 - [SDR UIEA2026012000015](https://openairdocs.org/sdr/UIEA2026012000015), Jan 15, 2026: ELT. INOPERATIVE. 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), Dec 27, 2025: ELT. LOOSE. 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), Oct 20, 2025: ENGINE. NO DISCREPANCY. 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 - [SDR UIEA2025101001264](https://openairdocs.org/sdr/UIEA2025101001264), Oct 10, 2025: SHUTOFF VALVE. FAULTED. 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 29-1 - [SDR UIEA2025101001266](https://openairdocs.org/sdr/UIEA2025101001266), Oct 9, 2025: REGULATOR. LEAKING. 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), Aug 4, 2025: FLASHLIGHT. NO DISCREPANCY. 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), Jul 30, 2025: LENS. SCRATCHED. 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), Jul 11, 2025: STRUCTURE. NO DISCREPANCY. 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 - [SDR UIEA2025070400832](https://openairdocs.org/sdr/UIEA2025070400832), Jul 4, 2025: FMC. ODOR. CAPT REPORTS ELECTRICAL ODOR IN COCKPIT AFTER BLOCK, DETERMINED CAPT FMS CDU BLANKED AND CIRCUIT BREAKER OPEN.(

COLLARED CIRCUIT BREAKER, PART ORDERED FOR NGO - [SDR UIEA2025012600108](https://openairdocs.org/sdr/UIEA2025012600108), Jan 27, 2025: ELT. ABNORMAL. 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 - [SDR UIEA2024111501092](https://openairdocs.org/sdr/UIEA2024111501092), Nov 15, 2024: LAMP. BURNED OUT. 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), Oct 18, 2024: SCREEN. CLOGGED. 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 - [SDR UIEA2024092400931](https://openairdocs.org/sdr/UIEA2024092400931), Sep 29, 2024: PDU. LEAKING. 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 CH - [SDR UIEA2024092400932](https://openairdocs.org/sdr/UIEA2024092400932), Sep 29, 2024: SKIN. DETACHED. 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 2 - [SDR UIEA2024092400933](https://openairdocs.org/sdr/UIEA2024092400933), Sep 29, 2024: SKIN. CORRODED. 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 A - [SDR UIEA2024092400934](https://openairdocs.org/sdr/UIEA2024092400934), Sep 29, 2024: PCA. LEAKING. 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 - [SDR UIEA2024092400935](https://openairdocs.org/sdr/UIEA2024092400935), Sep 29, 2024: SKIN. DETACHED. 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 F - [SDR UIEA2024092400936](https://openairdocs.org/sdr/UIEA2024092400936), Sep 29, 2024: FUEL CELL. LEAKING. 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 2 - [SDR UIEA2024092400937](https://openairdocs.org/sdr/UIEA2024092400937), Sep 29, 2024: FIRE BOTTLE. EXPIRED. 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), Sep 29, 2024: SKIN. CRACKED. 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 - [SDR UIEA2024092400939](https://openairdocs.org/sdr/UIEA2024092400939), Sep 29, 2024: SKIN. CRACKED. 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 INDI - [SDR UIEA2024092400940](https://openairdocs.org/sdr/UIEA2024092400940), Sep 29, 2024: SKIN. CRACKED. 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 - [SDR UIEA2024092400941](https://openairdocs.org/sdr/UIEA2024092400941), Sep 29, 2024: SKIN. WORN. 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 REPAI - [SDR UIEA2024092400942](https://openairdocs.org/sdr/UIEA2024092400942), Sep 29, 2024: SEAL. WORN. 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 - [SDR UIEA2024092400943](https://openairdocs.org/sdr/UIEA2024092400943), Sep 29, 2024: FRAME. CORRODED. 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, IN - [SDR UIEA2024092400944](https://openairdocs.org/sdr/UIEA2024092400944), Sep 29, 2024: JUMPER. BROKEN. 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 A - [SDR UIEA2024092400945](https://openairdocs.org/sdr/UIEA2024092400945), Sep 29, 2024: SEALANT. MISSING. 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 S - [SDR UIEA2024092400946](https://openairdocs.org/sdr/UIEA2024092400946), Sep 29, 2024: ACTUATOR. LEAKING. LH WING, LATERAL CENTRAL CONTROL ACTUATORS UPPER AND LOWER (M274 AND M276) LCCA WITH HYDRAULIC LEAK.(

LH WING, LATERAL CENTRAL CONTROL ACTUATORS UPPER AND LOW - [SDR UIEA2024092500948](https://openairdocs.org/sdr/UIEA2024092500948), Sep 29, 2024: ACCESS PANEL. PUNCTURED. SYS LH HYD BAY, (ACCESS PANEL 437BL), SURFACE INERSIDE AREA LOWER RIGH TSIDE, ANGLE WITH PUNCTURE.(

SURFACE INERSIDE AREA LOWER RIGHTSIDE, ANGLE WAS REPAIRED - [SDR UIEA2024092500949](https://openairdocs.org/sdr/UIEA2024092500949), Sep 29, 2024: ACCESS PANEL. WORN. 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 - [SDR UIEA2024092500950](https://openairdocs.org/sdr/UIEA2024092500950), Sep 29, 2024: FIRE SEAL. DETACHED. 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- - [SDR UIEA2024092500951](https://openairdocs.org/sdr/UIEA2024092500951), Sep 29, 2024: FILL PORT. CORRODED. RH WING, UPPER SURFACE, BASE OF OVERWING FILL PORT ADAPTER WITH EVIDENCE OF CORROSION(

OVERWING FILL PORT ADAPTER. CORROSION LEVE 1 WAS REWORKED, INSPECTED AN - [SDR UIEA2024092500952](https://openairdocs.org/sdr/UIEA2024092500952), Sep 29, 2024: BRACKET. CORRODED. 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 - [SDR UIEA2024092500953](https://openairdocs.org/sdr/UIEA2024092500953), Sep 29, 2024: BULKHEAD. CORRODED. 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 - [SDR UIEA2024092500954](https://openairdocs.org/sdr/UIEA2024092500954), Sep 29, 2024: BULKHEAD. CORRODED. 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 - [SDR UIEA2024092500955](https://openairdocs.org/sdr/UIEA2024092500955), Sep 29, 2024: FIRE SEAL. BROKEN. ENG 2, RIGHT T/R DOOR, UPPER AFTER SECTION, FIRE SEAL BROKEN(

FIRE SEAL WAS REPAIRED IAW AMM 78-00-00-038-001-N00. NO FURTHER DEFECTS NOTED

) All 296: https://openairdocs.org/aircraft/N1619A/reports.md ## STCs that may be installed (OpenAirDocs) (3) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the engine (Pratt & Whitney PW4060) - [STC SE01543CH](https://openairdocs.org/stc/SE01543CH): Replace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve. Cook Airtomic - [STC SE00053AT-D](https://openairdocs.org/stc/SE00053AT-D): Modification of fan exit guide vane, to line replaceable unit configuration. Chromalloy Gas Turbine Corp - [STC SE00131LA](https://openairdocs.org/stc/SE00131LA): Modification of the subject engines to incorporate an oil tank reservoir insulation blanket in accordance with Hi Temp Insulation Inc. Drawing List 46M1024-301, Revision N/C, dated December 5, 1995, or later FAA approved revision as an acceptable alternate to Pratt & Whitney part number 50R280-01 or 51R059-01 insulation blankets. Hi Temp Insulation Inc ## Earlier aircraft with N1619A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N1619A before. - [Cancelled 1980-07-02](https://openairdocs.org/deregistered/N1619A-1980-07-02): Piper PA-18, S/N 18-1260, built 1951. Owner: [Reeder Charles T](https://openairdocs.org/faa-owner/REEDER%20CHARLES%20T), [Twin Falls, ID](https://openairdocs.org/faa-place/ID/Twin%20Falls) ## Related - Other Boeing 767-3Y0 aircraft: https://openairdocs.org/model/boeing-767-3y0/aircraft.md - The Pratt & Whitney PW4060 engine: https://openairdocs.org/engine/pratt-whitney-pw4060.md --- 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.