# N1997A: 1994 Boeing 767-33A - Status: Valid registration - Airframe: [Boeing 767-33A](https://openairdocs.org/model/boeing-767-33a) (registry code 1385209, 330 seats) - Engine: [GE CF6-80C2B6F](https://openairdocs.org/engine/ge-cf6-80c2b6f) (registry code 30109) - Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs) - Serial number: 27310 - Year built: 1994 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 22, 2016 - Certificate issued: March 30, 2023 - Expires: March 31, 2030 - Mode S code: A18CE8 - Registered owner: [Andromeda Leasing II LLC](https://openairdocs.org/faa-owner/ANDROMEDA%20LEASING%20II%20LLC) - Location: [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase) - Owner type: LLC - 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=1997A - Page: https://openairdocs.org/aircraft/N1997A 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): 34 in force ### Matched by airframe (Boeing 767-33A) None in force. ### Matched by engine (GE CF6-80C2B6F) - [AD 2023-20-08](https://openairdocs.org/ad/2023-20-08): Engine (Turbine/Turboprop) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 4 more. Effective Oct 19, 2023 - [AD 2021-26-22](https://openairdocs.org/ad/2021-26-22): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 14, 2022 - [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 25 more. Effective Aug 27, 2021 - [AD 2021-03-02](https://openairdocs.org/ad/2021-03-02): Fuel Control/Turbine Engines · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Mar 31, 2021 - [AD 2020-22-02](https://openairdocs.org/ad/2020-22-02): Engine Fuel and Control · General Electric CF6-80C2A5F, CF6-80C2B1F, CF6-80C2B2F and 13 more. Effective Dec 3, 2020 - [AD 2016-08-10](https://openairdocs.org/ad/2016-08-10): Accessory heat shield · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Jun 1, 2016 - [AD 2014-21-01](https://openairdocs.org/ad/2014-21-01): Fuel manifold · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Nov 28, 2014 - [AD 2013-08-20](https://openairdocs.org/ad/2013-08-20): Fuel tube · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 14 more. Effective May 31, 2013 - [AD 2012-03-12](https://openairdocs.org/ad/2012-03-12): No. 3 bearing packing · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Apr 5, 2012 - [AD 2012-04-05](https://openairdocs.org/ad/2012-04-05): Electronic control unit (ECU) · General Electric CF6-80C2B1F, CF6-80C2B1F1, CF6-80C2B1F2 and 8 more. Effective Mar 30, 2012 - [AD 2009-21-07](https://openairdocs.org/ad/2009-21-07): Thrust and thrust control · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Dec 1, 2009 - [AD 2009-07-03](https://openairdocs.org/ad/2009-07-03): Eddy current inspection (ECI) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Apr 30, 2009 - [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10): Critical life-limited parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 30 more. Effective Mar 30, 2009 - [AD 2008-21-11](https://openairdocs.org/ad/2008-21-11): Low-pressure turbine (LPT) cases · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Nov 28, 2008 - [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007 - [AD 2007-05-14](https://openairdocs.org/ad/2007-05-14): Cast titanium weld- repaired forward engine mount platforms · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 9, 2007 - [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06): Certain stage 1 high- pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Sep 5, 2006 - [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005 - [AD 2004-22-07](https://openairdocs.org/ad/2004-22-07): Stage 2 nozzle guide vanes (HPT S2 NGVs) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 1, 2004 - [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003 - [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003 - [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002 - [AD 2000-03-04](https://openairdocs.org/ad/2000-03-04): General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Apr 10, 2000 - [AD 99-01-01](https://openairdocs.org/ad/99-01-01): Accessory Gearbox (AGB) idler adapters · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jan 21, 1999 - [AD 98-22-06](https://openairdocs.org/ad/98-22-06): Fan Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 41 more. Effective Nov 23, 1998 - [AD 97-22-14](https://openairdocs.org/ad/97-22-14): (HPCR) 3-9 Spool · General Electric CF6-50A, CF6-50C, CF6-50C1 and 29 more. Effective Nov 17, 1997 - [AD 96-16-07](https://openairdocs.org/ad/96-16-07): Rear Right Hand Mount Link · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective Aug 28, 1996 - [AD 95-10-11](https://openairdocs.org/ad/95-10-11): Fan Reversers · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective May 31, 1995 - [AD 94-20-06](https://openairdocs.org/ad/94-20-06): Oil System · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 27, 1994 - [AD 94-06-03](https://openairdocs.org/ad/94-06-03): High Pressure Turbine Disk · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 29, 1994 - [AD 93-14-18](https://openairdocs.org/ad/93-14-18): High pressure turbine (HPT) thermal shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Oct 4, 1993 - [AD 91-15-25](https://openairdocs.org/ad/91-15-25): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Sep 6, 1991 - [AD 91-11-05](https://openairdocs.org/ad/91-11-05): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Jul 5, 1991 - [AD 91-05-21](https://openairdocs.org/ad/91-05-21): High Pressure Turbine · General Electric CF6-80C2A5, CF6-80C2B6, CF6-80C2B6F and 1 more. Effective Mar 27, 1991 ### Historical (superseded or no longer in force) - [AD 2020-20-13](https://openairdocs.org/ad/2020-20-13) (historical): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Nov 12, 2020 - [AD 2018-15-04](https://openairdocs.org/ad/2018-15-04) (historical): Turbine/Turboprop Engine--Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Oct 2, 2018 - [AD 2009-05-02](https://openairdocs.org/ad/2009-05-02) (historical): Drainless fuel manifold assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Mar 31, 2009 - [AD 2007-12-07](https://openairdocs.org/ad/2007-12-07) (historical): Electronic control units (ECUs) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 5 more. Effective Jul 11, 2007 - [AD 2004-04-07](https://openairdocs.org/ad/2004-04-07) (historical): Stage 1 HPT rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 12, 2004 - [AD 2002-07-12](https://openairdocs.org/ad/2002-07-12) (historical): Life Limits Section of Continued Airworthiness (ICA) - Selected Critical Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 27 more. Effective May 15, 2002 - [AD 2001-10-07](https://openairdocs.org/ad/2001-10-07) (historical): High Pressure Turbine Rotor Disks · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jun 18, 2001 - [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12) (historical): High Pressure Compressor Rotor Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Sep 5, 2000 - [AD 2000-04-14](https://openairdocs.org/ad/2000-04-14) (historical): Fuel tube flange seating · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective May 1, 2000 - [AD 99-24-15](https://openairdocs.org/ad/99-24-15) (historical): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Jan 28, 2000 - [AD 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999 - [AD 91-20-02](https://openairdocs.org/ad/91-20-02) (historical): Fuel Manifolds · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective Nov 25, 1991 - [AD 90-26-01](https://openairdocs.org/ad/90-26-01) (historical): Fuel Manifold Systems · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 11 more. Effective Dec 20, 1990 ## Information bulletins (advisory) (4 in force) - [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023 - [SAIB NE-10-37](https://openairdocs.org/saib/NE-10-37): Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback Faults. Issued Jul 12, 2010 - [SAIB NE-08-44](https://openairdocs.org/saib/NE-08-44): Engine Thrust Reverser Transcowl Clevis Pin. Issued Sep 3, 2008 - [SAIB NE-07-01](https://openairdocs.org/saib/NE-07-01): Dual engine flameouts on twin engine airplanes. Issued Oct 12, 2006 ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DCA26MA352](https://openairdocs.org/ntsb/DCA26MA352), Sep 6, 2026: Boeing 767 (N1997A), Miami, FL, substantial damage, 5 fatal, investigation ongoing ## FAA accident and incident reports None matched to N1997A. ## Service difficulty reports (374, 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 ABXR2026060400010](https://openairdocs.org/sdr/ABXR2026060400010), Jun 4, 2026: ANGLE. CRACKED. RIGHT WING L/E #9 SLAT AREA INTERNAL ANGLE CRACKED AT LOWER FWD WEB LOWER ANGLE. LES668. FABRICATED NEW ANGLE IAW B767 SRM 57-41-13 REPAIR 1 - [SDR ABXR2026060400009](https://openairdocs.org/sdr/ABXR2026060400009), Jun 4, 2026: FRAME. CORRODED. CORROSION AT STA. 1219 RBL22 "J" FRAME FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-511. - [SDR 21GA202509030017](https://openairdocs.org/sdr/21GA202509030017), Aug 29, 2025: CONTROLLER. FAULTED. ON APPROACH, RECEIVED WHEEL WELL FIRE EICAS MESSAGE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND NO EVIDENCE OF FIRE. REPLACED DETECTION - [SDR 21GA20250610011](https://openairdocs.org/sdr/21GA20250610011), Jun 10, 2025: BATTERY. INOPERATIVE. DURING SERVICE CHECK, L1 DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. REPLACED BATTERY ASSEMBLY. - [SDR UIEA2024112901131](https://openairdocs.org/sdr/UIEA2024112901131), Nov 29, 2024: PSEU. MALFUNCTIONED. AS FLAPS MOVED FROM 1 TO UP ON CLIMB OUT; FLAP (RED). EICAS STATUS MSG: NOSE A/G DISAGREE ALSO F/O HAD SPEED LIM ON HIS SPEED TAPE(

TROUBLESHOT & FOUND PS - [SDR UIEA2024112701117](https://openairdocs.org/sdr/UIEA2024112701117), Nov 27, 2024: WEDGE. DAMAGED. 8028 - EA-1957A155 PART(3) REV(0) WINGS - LEADING EDGE DEVICES - RH WING #8 LEADING EDGE SLAT (PN 114T4105-58 /SN 000598) TRAILING EDGE WEDGE EXISTING REPAIR DE - [SDR UIEA2024112601116](https://openairdocs.org/sdr/UIEA2024112601116), Nov 27, 2024: BEAR STRAP. CRACKED. LH FWD DOOR, AFT LOWER CORNER WITH CRACK INDICATION AT SECOND LOWER HOLE ON BEAR STRAP APPROX. 10 O'CLOCK.(

CRACK WAS REPAIRED IAW EA 6753A937. NO FURTHER DEF - [SDR UIEA2024112601115](https://openairdocs.org/sdr/UIEA2024112601115), Nov 27, 2024: SHEAR TIE. CORRODED. BULK CARGO COMPARTMENT, STA 1480 BTW STGR 28R-29R FRAME WITH CORROSION(

SHEAR TIE WAS REPLACED IAW DWG 146T1519. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024112501114](https://openairdocs.org/sdr/UIEA2024112501114), Nov 27, 2024: SKIN. SCRATCHED. TRAFFIC ALERT & COLLISION AVOIDANCE SYS HEALTH CHECK, ON TCAS UPPER ANTENNA WITH SCRATCHES ON FUSELAGE SKIN(

THE TCAS UPPER ANTENNA DOUBLER WAS BLEND OUT - [SDR UIEA2024112501113](https://openairdocs.org/sdr/UIEA2024112501113), Nov 27, 2024: WEB. CORRODED. AFT CARGO, BTW STA 1263 AND DOOR FRAME, BTW STRG 32R AND 32R, CORROSION ON WEB.(

CLIP P/N 146T8081-13 SMALL AUTHORIZATION IAW CONSECUTIVE NUMBER M675498 & - [SDR UIEA2024112401111](https://openairdocs.org/sdr/UIEA2024112401111), Nov 27, 2024: FRAME. CORRODED. FRAME AT STA 1480 BETWEEN STGR 27R / 29R WITH CORROSION (BULK CARGO COMPARTMENT AREA)(

FRAME N/P 146T1519-3 WAS MANUFACTURED IN ACCORDANCE SMAL AUTHORIZATION - [SDR UIEA2024112201104](https://openairdocs.org/sdr/UIEA2024112201104), Nov 27, 2024: SHEAR TIE. CORRODED. BULK CARGO, FLOOR LEVEL AT FRAME 1540, SHEAR TIE WITH CORROSION BTW STRG 39R AND 38R.(

THE SHEAR TIE WITH CORROSION WAS REMOVED. THE AREA WAS CLEANED. THE NEW - [SDR UIEA2024112201103](https://openairdocs.org/sdr/UIEA2024112201103), Nov 27, 2024: SKIN. CRACKED. RH FWD DOOR, AFT LOWER CORNER WITH CRACK INDICATION AT THIRD HOLE ON SKIN APPROX 1 O'CLOCK, AND VISUAL CRACK (CONFIRMED WITH HFEC) AT FOURTH HOLE ON SKIN AND BE - [SDR UIEA2024112201102](https://openairdocs.org/sdr/UIEA2024112201102), Nov 27, 2024: SUPPORT BEAM. CORRODED. BULK CARGO DOOR, INTERNAL STRUCTURE, CORROSION BTW BEAMS 2 AND 4.(

THE AREA WAS CLEANED, NEW SUPPORT WAS DRILLED, SUPPORT BEAM WAS INSTALLED. THE BEAM SUPPORT - [SDR UIEA2024112201101](https://openairdocs.org/sdr/UIEA2024112201101), Nov 27, 2024: BEARING. COKED. ENGINE 1, BEARING #5, LH/RH SUMP PIPES WITH LEAK EVIDENCE.(

DURING VISUAL EXAMINATION, OIL COKE BUILD-UP WAS FOUND, COKING WAS REMOVED AND NO OIL LEAK WAS FOU - [SDR UIEA2024112201100](https://openairdocs.org/sdr/UIEA2024112201100), Nov 27, 2024: SPLICE. CORRODED. BULK CARGO COMPARTMENT AT STA 1502 BTW STGR 31R-32R SPLICE WITH CORROSION.(

A NEW SPLICE WEB WAS MANUFACTURED AND INSTALLED IAW SRM 51-10-02-0G-0. NO FURTHER - [SDR UIEA2024112201099](https://openairdocs.org/sdr/UIEA2024112201099), Nov 27, 2024: SKATE ANGLE. CRACKED. CRACK ON LH SKATE ANGLE ON STRUT #2 (FOUND DURING SEALANT REMOVAL)(

A SEGMENT OF THE SKATE WITH CRACK WAS REMOVED, AND THE NEW SEGMENT WAS MANUFACTURED AND IN - [SDR UIEA2024112201098](https://openairdocs.org/sdr/UIEA2024112201098), Nov 27, 2024: FRAME. CORRODED. BULK CARGO COMPARTMENT AT STA 1480 BTW STGR 31R-32R FRAME WITH CORROSION(

FRAME WAS MANUFACTURED AND REPLACED WITH THE NEW ONE. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024111901096](https://openairdocs.org/sdr/UIEA2024111901096), Nov 27, 2024: SKIN. DEBONDED. RH WING, INBOARD AILERON, LEADING EDGE DISBONDED BTW RIB 1 AND 2.(

RH WING, INBOARD AILERON, L/E BETWEEN RIB 1 AND 2 WAS REPAIRED AS PER B767-300 SRM 57-60-01 - [SDR UIEA2024051900395](https://openairdocs.org/sdr/UIEA2024051900395), May 19, 2024: LIGHT. BROKEN. EMERGENCY EXIT LIGHT BY L1 BOOR BROKEN(

RESECURED EMERGRNCY EXIT SIGN LENSE IAW 33-51-01. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2023071300756](https://openairdocs.org/sdr/UIEA2023071300756), Jul 13, 2023: HOSE. UNKNOWN. O2 DISCHARGED COMPLETELY THROUGH FO'S REGULATOR IN MASSIVE AND SUDDEN LEAK(

FOUND FO'S OXYGEN MASK BOX CONNECTION HOSE BLOWN OFF AND MASSIVELY LEAKING. REMOVE - [SDR UIEA2023040300310](https://openairdocs.org/sdr/UIEA2023040300310), Apr 3, 2023: PIMU. UNKNOWN. RH PIMU FAULT MESSAGE.(

R/R RH PIMU & OPS CHECK OK PER AMM 77-35-02.

) - [SDR UIEA2023040300309](https://openairdocs.org/sdr/UIEA2023040300309), Apr 3, 2023: LEAD. UNKNOWN. ENG #1 LOWER HIGH TENSION LEAD DAMAGED.(

REMOVED & REPLACED ENG #1 LOWER HIGH TENSION LEAD IAW 767-300 AMM 74-21-02. PERFORMED AUDIBLE TEST FOR ENG #1, AU - [SDR UIEA2023040300308](https://openairdocs.org/sdr/UIEA2023040300308), Apr 3, 2023: UNKNOWN. UNKNOWN. FWD E/E CREW OXYGEN NEED SERVICE TO FULL.(

SERVICED FWD E&E CREW OXYGEN AS PER B767 AMM CH 12-15-08, AC 43.18-1B PAR 9-46 THRU 9-51 PGS 9-448 THRU&NB - [SDR UIEA2023040300307](https://openairdocs.org/sdr/UIEA2023040300307), Apr 3, 2023: CONTROLLER. UNKNOWN. CABIN COMPT TEMP CONTROL SYS INOP.(

R/R CABIN COMPT TEMP CONTROLLER M195 & ZONE TEMP CONTR. 1 SYS. OPS TEST GOOD PER AMM 21-61-03. MDDR 182947 CLEARED UP< - [SDR UIEA2023040300306](https://openairdocs.org/sdr/UIEA2023040300306), Apr 3, 2023: UNKNOWN. UNKNOWN. ECM 2023P-168 N1997A ENG #1 ESN #702928 IS EXPERIENCING HIGH FAN VIBRATION. A TRIM BALANCE IS REQUIRED TSLV 10,240 CSLV 3,348.(

PERFORMED LH ENG RUN UP PER AM - [SDR UIEA2022122701217](https://openairdocs.org/sdr/UIEA2022122701217), Dec 23, 2022: LAMP. INOPERATIVE. EMERGENCY LIGHT AT L1 DOOR INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED NORMAL IAW AMM 33-51-00. - [SDR UIEA2022053100562](https://openairdocs.org/sdr/UIEA2022053100562), May 26, 2022: PCA. LEAKING. WITH LEFT AND CENTER HYD SYS DEPRESSURIZED LEFT INBOARD AILERON FLOATS UP DURING LEVEL FLIGHT RESULTING IN HARD LEFT ROLL. FOUND LEFT INBOARD AILERON INBOARD & - [SDR UIEA2022053100561](https://openairdocs.org/sdr/UIEA2022053100561), May 25, 2022: PCA. ERRATIC. AIRPLANE WAS HAVING PROBLEMS MAINTAINING VNAV PTH ON THE ARRIVAL ROUTE. AFTER DISCONNECTING AUTOPILOT I FELT HEAVY RESISTANCE WITH AILERON FLIGHT CONTROLS. BOTH - [SDR UIEA2022042000350](https://openairdocs.org/sdr/UIEA2022042000350), Apr 19, 2022: TRANSDUCER. NONE. SUPERNUMERARY O2 INDICATION IS ERRATIC(

TRANSFERRED TO MMDR 164289 IAW MEL 35-11-03-02A, CAT C.

/

LOGPAGE 1504123 - ITEM #4: REMOVED AND REPLACED PAX O - [SDR UIEA2022032800249](https://openairdocs.org/sdr/UIEA2022032800249), Apr 16, 2022: NONE. NONE. CORROSION IN THE AFT CARGO COMPARTMENT HORIZONTAL ATTACH FITTING BETWEEN STR,23R AND STR.24R JUST AFT OF THE BS.1065 BULKHEAD. DOT 129-097(

REMOVED AND - [SDR UIEA2022040800268](https://openairdocs.org/sdr/UIEA2022040800268), Apr 16, 2022: NONE. NONE. CORROSION AROUND FASTENER HOLE AND UNDER ROLLER TRAY IN THE AFT CARGO COMPARTMENT FLOOR BEAM UPPER CHORD LOWER SURFACE BS.1241 LBL.43.(

REMOVED, FABRICATED NE - [SDR UIEA2022040800270](https://openairdocs.org/sdr/UIEA2022040800270), Apr 16, 2022: FITTING. NONE. CORROSION IN THE AFT CARGO COMPARTMENT HORIZONTAL ATTACH FITTING BETWEEN STR,23L AND STR.24L JUST AFT OF THE BS.1065 BULKHEAD(

REMOVED AND REPLACED THE LH HOR - [SDR UIEA2022041000279](https://openairdocs.org/sdr/UIEA2022041000279), Apr 16, 2022: FITTING. NONE. RH PYLON OB SIDE AFT STA 280 APPROX LWR FITTING CRACKED AT LWR END.(

REMOVED AND REPLACED&NBSP;RH PYLON OB SIDE AFT LWR FITTING&NBSP;STA 28 - [SDR UIEA2022041400306](https://openairdocs.org/sdr/UIEA2022041400306), Apr 16, 2022: NONE. NONE. RH WING UPPER SIDE BODY SPLICE CENTER WING WBL.95 BTWN. 1, 2 STRINGERS U 10, U7 SKIN FOUND CORRODED AREA DOT 11/ 0013(

REMOVED CORROSION FROM RH WING UPPER SI - [SDR UIEA2022041800312](https://openairdocs.org/sdr/UIEA2022041800312), Apr 16, 2022: BOTTLE. LOW PRESSURE. CREW O2 LOW AT DEPARTURE CREW O2 READ 1600 ON ARRIVAL 1220(

REMOVED AND REPLACED CREW O2 BOTTLE IAW AMM 12-15-08 & LEAKED CHECKED OKAY PER GMM 3.25.3. NO - [SDR UIEA2022012300073](https://openairdocs.org/sdr/UIEA2022012300073), Jan 23, 2022: NONE. NONE. GEAR DISAGREE EICAS AFTER SELECTING GEAR DOWN. RAN QRH PROCEDURES(

ON WALK AROUND FOUND TAIL SKID RETRACTED. PERFORMED FIM 32-30 FT 305. ON PSEU BITE TEST FOU - [SDR UIEA2022010500006](https://openairdocs.org/sdr/UIEA2022010500006), Jan 5, 2022: SWITCH. NONE. EMERGENCY LIGHT KORRY SWITCH INOP(

REMOVED AND REPLACED EMERGENCY LIGHT KORRY SWITCH IAW AMM 33-13-00. OPS TEST GOOD.

) - [SDR UIEA2021120502445](https://openairdocs.org/sdr/UIEA2021120502445), Dec 6, 2021: ELEVATOR SYSTEM. FAILED. ELEVATOR NOT RETURNING TO CENTER POSITION WHEN DOING FLIGHT CONTROL CHECK.(

PERFORMED ELEVATOR POSITION INDICATING SYSTEM OPS TEST IAW AMM 27-38-00. OPS CHECK - [SDR UIEA2021110802362](https://openairdocs.org/sdr/UIEA2021110802362), Nov 6, 2021: NONE. NONE. FWD EQPT VAL EICAS MSG MOMENTARILY APPEARED DURING ROTATION. REPEAT WRITE UP.(

REF ITEM M9 LP 1431441 FOR CORRECTIVE ACTION. EQ COOLING GROUND VALVE POSITION - [SDR UIEA2021110802365](https://openairdocs.org/sdr/UIEA2021110802365), Nov 6, 2021: NONE. NONE. L ENG SPEED CARD EICAS MSG.(

FOUND CANNON PLUG D4978P WITH BROKEN WIRE PIN 38 TO N2 SPEED CARD. RETERMINATED IAW SWPM 70-60-02 AND WDM77-12-12. PERFORMED IDLE - [SDR UIEA2021110502349](https://openairdocs.org/sdr/UIEA2021110502349), Nov 5, 2021: NONE. NONE. DURING TAXI OUT CAPTS PFD & UPPER EICAS SCREENS WENT BLANK.(

CAPT'S ADI AND UPPER EICAS CAME BACK AFTER SHUTDOWN. SUPPLIED AIR FOR HOT/HUMID WEATHER CONDI - [SDR UIEA2021110802370](https://openairdocs.org/sdr/UIEA2021110802370), Nov 5, 2021: NONE. NONE. L ENG SPEED CARD STATUS MSG REPEAT WRITE UP.(

R/R N2 SPEED CARD ON L/H ENG. FAULT CLEARED. FOUND CONNECTOR ON D10064 TO HAVE DAMAGED THREADED INSERTS CAUSING - [SDR UIEA2021110502351](https://openairdocs.org/sdr/UIEA2021110502351), Nov 5, 2021: NONE. NONE. REPEAT WRITE UP LEFT ENG SPEED CARD STATUS MESSAGE AFTER ENG START(

PERFORMED ENG N2 SPEED CARD TEST AS PER B767 AMM TASK 73-21-54-705-005-H00 TEST OK.

) - [SDR UIEA2021110402347](https://openairdocs.org/sdr/UIEA2021110402347), Nov 4, 2021: NONE. NONE. L ENG SPEED CARD STATUS MESSAGE AFTER START ...REPEAT WRITE UP(

PERFORMED FIM 73-21 TASK TT#871 BLOCK #21 FOUND L END SPEED CARD DISPLAYED. REMOVED/REPLACED M - [SDR UIEA2021110402344](https://openairdocs.org/sdr/UIEA2021110402344), Nov 4, 2021: NONE. NONE. L. ENG SPEED CARD STATUS MESSAGE AFTER START(

T/S PER B767 AMM 73-21-54-705-005-HOO AND B767 FIM 73-21 FAULT TREE 871. TEST PASSED NORMAL. MESSAGE CLEAR - [SDR UIEA2021110302331](https://openairdocs.org/sdr/UIEA2021110302331), Nov 2, 2021: NONE. NONE. LEFT / #1 ENGINE "VIB" INDICATION BETWEEN 1 AND 4 ON STATUS PAGE DURING DEPARTURE. FLUCTUATIONS WERE ALSO SLIGHTLY FELT.(

RAN #1 ENGINE HIGH POWER RUN VIBRATI - [SDR UIEA2021100202163](https://openairdocs.org/sdr/UIEA2021100202163), Sep 30, 2021: RADOME. DAMAGED. BIRD STRIKE ON RADOME. INSPECTED NOSE RADOME FOUND DAMAGE ON THE EXTERNAL SIDE SURFACE WAS OUT OF LIMITS IAW AMM 05-51-18 & SRM 53-10-72.LP 1401419, ITEM M6: RE - [SDR UIEA2021082501877](https://openairdocs.org/sdr/UIEA2021082501877), Aug 24, 2021: VALVE. FAULTED. APU PNEUMATICS INOP ( AUXILIARY POWER UNIT, PNEUMATIC FUNCTION )(

TRANSCRIBED TO MEL LIST MDDR 152437 DMI # 49-11-01-01 DUE 03SEP21, CAT C. MAINT ACTIONS C/W - [SDR UIEA2021082401862](https://openairdocs.org/sdr/UIEA2021082401862), Aug 23, 2021: CONTROL VALVE. FAULTED. AFT CABIN COMPARTMENT SHOWS 7D EVENT THOUGH AFT CABIN TEMPERATURE CONTROLLER IS SET TO WARM DURING CRUISE FLIGHT(

PERFORMED BITE CHECK ON DECK SYSTEM IAW FIM. All 374: https://openairdocs.org/aircraft/N1997A/reports.md ## STCs that may be installed (OpenAirDocs) (5) 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 (GE CF6-80C2B6F) - [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 SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic - [STC SE01471AT](https://openairdocs.org/stc/SE01471AT): Replace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine. Unison Industries. Lists CF6-80C2 Series - [STC SE00463LA](https://openairdocs.org/stc/SE00463LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220. Hi Temp Insulation Inc - [STC SA2227SO](https://openairdocs.org/stc/SA2227SO): Installation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES. Rolls Royce, Inc. Lists CF6-80 Series ## Earlier aircraft with N1997A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N1997A before. - [Cancelled 1994-08-26](https://openairdocs.org/deregistered/N1997A-1994-08-26): Cameron Balloons US N-90, S/N 5327. Triennial form not returned. Owner: [Sky High Adventures Inc](https://openairdocs.org/faa-owner/SKY%20HIGH%20ADVENTURES%20INC), [Batavia, IL](https://openairdocs.org/faa-place/IL/Batavia) - [Cancelled 1967-11-14](https://openairdocs.org/deregistered/N1997A-1967-11-14): Piper PA-18-135, S/N 18-1821. Owner: [Fosdick Bryce](https://openairdocs.org/faa-owner/FOSDICK%20BRYCE), [Dowagiac, MI](https://openairdocs.org/faa-place/MI/Dowagiac) ## Related - Other Boeing 767-33A aircraft: https://openairdocs.org/model/boeing-767-33a/aircraft.md - The GE CF6-80C2B6F engine: https://openairdocs.org/engine/ge-cf6-80c2b6f.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.