# N684UA: 2002 Boeing 767-3CB

- Status: Valid registration
- Airframe: [Boeing 767-3CB](https://openairdocs.org/model/boeing-767-3cb) (registry code 1385187, 300 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: 33466
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 23, 2002
- Certificate issued: July 18, 2018
- Expires: July 31, 2028
- Mode S code: A913D6
- Registered owner: [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC)
- Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago)
- Owner type: Corporation
- Owner's area on the map: 41.8813° N, 87.6375° W: Placed by OpenAirDocs at the center of ZIP code 60606, 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=684UA
- Page: https://openairdocs.org/aircraft/N684UA

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 767-3CB)

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 N684UA.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20250624006419I](https://openairdocs.org/incident/20250624006419I), Jun 24, 2025: Boeing 767-3CB (N684UA), Zurich, No damage. Due to an airspeed disagree the crew rejected takeoff at approximately 120KTS. The aircraft is on the runway, with six blown tires after the rejected takeoff.…

## Service difficulty reports (43)

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 CALA2026082518904](https://openairdocs.org/sdr/CALA2026082518904), Aug 24, 2026: OVEN. ODOR. OVEN 109 IN FWD GALLEY HAD LIGHT SMOKEY ODOR WHEN PLATES CAME OU T GALLEY OVEN 109 HEAVILY CONTAMINATED, CLEANED IAW AMM 25-05-03-100-801-C1. OVEN OPERATED FOR 
- [SDR CALA2026050816083](https://openairdocs.org/sdr/CALA2026050816083), May 6, 2026: IRU. FAULTED. RIGHT IRS FAULT EICAS PER FLT CREW DEBRIEF, HAD ATTITUDE DISAGREE EICAS, PITCH/ROLL DISPLAYED ON BOTH PFDS. F/OS SIDE PFD INDICATED A DESCENT WHILE THE A/C WAS 
- [SDR CALA2026042715739](https://openairdocs.org/sdr/CALA2026042715739), Apr 27, 2026: UNKNOWN. ODOR. ON LEFT ENGINE STARTUP- FLT ATT REPORTED VERY STRONG GAS FUMES I N CABIN. COCKPIT SMELL TOOREFER TO LP# 8627807 EGC PERFORMED FUEL DISTRIBUTION INSPECTION UP TO
- [SDR CALA2026042415693](https://openairdocs.org/sdr/CALA2026042415693), Apr 20, 2026: IGNITER. FAULTED. ON FIRST ENGINE START ATTEMPT ON LEFT ENGINE WITH ENGINE START IGNITER IN NO. 2 POSITION. NO ENGINE VALVE LIGHT WITH NO RISE IN EGT. ABORTED START WITH CHECKLIS
- [SDR CALA2026031314545](https://openairdocs.org/sdr/CALA2026031314545), Mar 10, 2026: HOUSING. DETACHED. 40D AISLE EMERGENCY PATH LIGHT FOUND DETATCHED 40D AISLE EMERGENCY PATH LIGHT HOUSING REPLACED IAW CMM 25-23-52. PARTS USED: 58-2523-3-0048, QTY :1 40D AISLE EM
- [SDR CALA2026031314544](https://openairdocs.org/sdr/CALA2026031314544), Mar 10, 2026: LIGHT. DAMAGED. EMERGENCY LIGHT OPPOSITE LAV 1A-1L DAMAGED. THE EMERGENCY EXIT LIGHT ASSY REPLACED IAW SWPM 20-30-12
- [SDR CALA2026031114493](https://openairdocs.org/sdr/CALA2026031114493), Mar 10, 2026: FEEDER CABLE. DAMAGED. DURING INSPECTION ON NR 2 ENGINE, FOUND IDG FEEDER CABLE HAS BARE WIRE EXPOSED. FEEDER CABLE RE-SLEEVED AND INSTALLED IAW AMM24-11-01-404-001-006 AND SWPM 20-30
- [SDR CALA2026030914408](https://openairdocs.org/sdr/CALA2026030914408), Mar 4, 2026: FMU. UNSERVICEABLE. EGT REACHED 597C DURING ENGINE START NR 2 PILOT DEBRIEFED UPON RTB EVENT, THEY CONFIRMED THAT START PROCEDURE WAS NORMAL UP UNTIL THE LATER STAGE WHEN THEY NOTI
- [SDR CALA2026012913431](https://openairdocs.org/sdr/CALA2026012913431), Jan 27, 2026: WARNING MESSAGE. FALSE ACTIVATION. HYD GEN VAL STATUS MESSAGE FOUND C/B RT AC BUS SENSE P11-6 AND CB L AC BUSS SENSE P11-3 PULLED AND COLLARED. RESET CBS RAN HMG TEST REF AMM24-25-01-424-005. TES
- [SDR CALA2025103010751](https://openairdocs.org/sdr/CALA2025103010751), Oct 29, 2025: LIGHT. BROKEN. 36D EMERGENCY PATH LIGHT ON SEAT BROKEN AND FOUND HANGING FROM SEAT. LIGHT HOUSING HAS BROKEN TABS SO UNABLE TO SECURE TO SEAT. TAPE FOUND ON SIDE WHICH FAILED 
- [SDR CALA2025082508082](https://openairdocs.org/sdr/CALA2025082508082), Aug 22, 2025: DISPLAY. FAULTED. EICAS UPPER DISPLAY BLANK AFTER TAKEOFF. NO AUTO. INTERMITTENT ON/OFF UPON ARIVAL FOUND UPPER EICAS DISPLAY FULLY OPS. PERFORMED EICAS OPS TEST REF 31-41-00-715
- [SDR CALA2025070706242](https://openairdocs.org/sdr/CALA2025070706242), Jul 1, 2025: UNKNOWN. NOISE. FA REPORTED HISSING SOUND AT L OVERWING EXIT 4000 FT ON DESCENT PERFORMED A LEAK TEST PER MM TASK 05-51-24-782-001. NO HISSING OR LEAK OBSERVED.
- [SDR CALA2025062706007](https://openairdocs.org/sdr/CALA2025062706007), Jun 24, 2025: INDICATOR. FAULTED. REJECT TO DUE TO A/S DISAGRE. CAP+STB 120KT/ FO 100 KT AND FLAG BRK TEMP 9 FOUND RIGHT HAND MAC AIRSPEED INDICATOR FLICKERING. REMOVED AND INSTALLED NEW MAC AIR
- [SDR CALA2025062705988](https://openairdocs.org/sdr/CALA2025062705988), Jun 24, 2025: UNKNOWN. ODOR. AFT FA NOTICED SLIGHT SMOKE SMELL ON T/O PRIOR TO REJECT REF AMM TASK 05-51-56-940-801-C1, SMOKE/ODOR EVENT QUESTIONNAIRE FORM WAS NOT COMPLETED BY CREW. SMOKE/
- [SDR CALA2025042404205](https://openairdocs.org/sdr/CALA2025042404205), Apr 20, 2025: CONTROLLER. FAULTY. EXCESSIVE CABIN TEMP. UP TO 83F ALL ALTS. CLIM B AND CRUISE. RAN QRH NO HELP.PER CREW DEBRIEF A/C TEMPS WERE HIGHER THEN NORMAL ON GROUND, SUSPECTED TEMPS WOULD
- [SDR CALA2025042104100](https://openairdocs.org/sdr/CALA2025042104100), Apr 20, 2025: COVER. DETACHED. DOOR 1L..SLIDE COVER FALLING OFF INSPECTED DOOR SLIDE BUSTLE AT L1 AN FOUND COVER COMPLETELY SECURE. INSPECTED R1 DOOR AS PRECAUTIONARY AND FOUND SAME RESULTS. 
- [SDR CALA2025021000331](https://openairdocs.org/sdr/CALA2025021000331), Feb 9, 2025: STRINGER. CORRODED. FWD CARGO COMPT BELOW FLOOR S39R FND CORROSION AT STA 478 - STA 500 REFER HX NR WO4336886. FWD CGO COMPT STR 39R BETWEEN STA 478 AND STA 500 REPAIRED AS PER ECR
- [SDR CALA2025021000330](https://openairdocs.org/sdr/CALA2025021000330), Feb 9, 2025: STRINGER. CORRODED. BELOW FLOOR S39L FOUND CORROSION AT STA478-STA500 REF HX NR WO.4336897, ORGI BY V896820 FWD CARGO COMPT STR 39L BETWEEN STA478 AND STA500 REPAIRED AS PER ECRA 5
- [SDR CALA2025012900237](https://openairdocs.org/sdr/CALA2025012900237), Jan 28, 2025: STICKER. CRACKED. EA 5310-07143 REV E OP 002, 1EA CRACK FOUND ON SUBSURFACE OF RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BETWEEN WL 118 TO 159 APPROX. 1.125" IN LENGTH AS 
- [SDR CALA2025010201740](https://openairdocs.org/sdr/CALA2025010201740), Dec 30, 2024: LENS. MISSING. 2X EMERGENCY LIGHT LENS COVER MISSING AT DOOR 1L 2X EMERGENCY LIGHT LENS COVERED INSTALLED IAW AMM TASK 33-51-10-962-172. OPS TEST GOOD. SDR RAISED AS PER GMM.
- [SDR CALA2025010201739](https://openairdocs.org/sdr/CALA2025010201739), Dec 30, 2024: BULB. INOPERATIVE. R/H SIDE EXTERIOR EMERGENCY LIGHT NOT WORKING EXTERIOR EMERGENCY LIGHT BLUB REPLACED IAW AMM 33-51-00. OPS TEST CARRIED OUT. ALL SATIS. SDR RAISED AS PER GMM.
- [SDR CALA2024080100340](https://openairdocs.org/sdr/CALA2024080100340), Jul 31, 2024: STATOR. BROKEN. ON LANDING SMOKE AND FLAMES OBSERVED ON RIGHT MAIN GEAR REPORT BY ANOTH A/C #7 BRAKE FOUND DAMAGED REF PICS, NO DAMAGE FOUND TO WHEEL AXEL OR NEIGHBOURING COMPO
- [SDR CALA2024031100683](https://openairdocs.org/sdr/CALA2024031100683), Mar 7, 2024: HOSE. MISINSTALLED. MAIN (LEFT, RIGHT, AND CENTER) HYDRAULIC SYSTEMS HYD QTY (01=L, 02=R) DECREASED TO _. QTY STABLE WITH EDP DEPRESSURIZED AND ACMP OFF 01 45 MINS AFTER TAKEOFF L 
- [SDR CALA2024022800588](https://openairdocs.org/sdr/CALA2024022800588), Feb 27, 2024: TRANSMITTER. INOPERATIVE. 15 MIN AFTER TO OIL QTY 7 20 MIN AFTER TO OIL QTY 0. DEFERED DUE INDICATION FOUND AT FAULT. NO OIL LOSS RECORDED OR V ISUALLY FOUND. CREW REPORTED NO LOSS OF OI
- [SDR CALA2024020500311](https://openairdocs.org/sdr/CALA2024020500311), Feb 1, 2024: CABLE. INTERMITTENT. EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - EMERGENCY AISLE LIGHTS AT SEAT 32 DEF WORKS INTERMITENTLY, SEAT BACK MOVED FORWARD AND BACK, LIGHT FLICKER
- [SDR CALA2024011900157](https://openairdocs.org/sdr/CALA2024011900157), Jan 12, 2024: FUEL CAP. MISSING. LH FUEL RECEPTACLE CAP MISSING NIL STOCK LHR REQUEST MEL 2821J ADD FAULT: 2821 MEL COMPLIED WITH APPROVED REPLACED LH FUEL RECEPTACLE CAP IN REF WITH IPC 28-21-
- [SDR CALA2024010800056](https://openairdocs.org/sdr/CALA2024010800056), Jan 5, 2024: TANK UNIT. INTERMITTENT. LEFT FUEL QUANTITY DROPPED FROM 36.5 TO 29.7 IN APPOX 30 SECS THEN RETURNED TO 35.6 ACCOMPLISHED IDT INSPECTION OF FUEL PROBE #8 INSTALLATION, VERIFIED CDCCL''S
- [SDR CALA2023053101725](https://openairdocs.org/sdr/CALA2023053101725), May 30, 2023: SKIN. CORRODED. CORROSION LOWER SURFACE RIGHT WING CENTER BS 785.9 BTW KEEL BEAM AND BL 62 AT LOWER FUSELAGE (4 EA). REFER TO AEROMAN NON ROUTINE 2023-239484 MEASURES ON REWORK
- [SDR CALA2023041001070](https://openairdocs.org/sdr/CALA2023041001070), Apr 7, 2023: SKIN. UNKNOWN. EA5100-02345 REV E FOUND REINFORCINGT DOUBLER REPAIR ON AFT CARGO DOOR EXTERNAL SKIN AT 6OCLOCK FROM UPPER EDGE 13IN FROM AFT EDGE SIZE 13/12X9 REPAIR HAS A DEE
- [SDR CALA2023010900058](https://openairdocs.org/sdr/CALA2023010900058), Jan 7, 2023: TIRE. FLAT. DURING INCOMMING FOUND TIRE NR 2 FLAT ZERO PRESSURE.
- [SDR CALA2022092302446](https://openairdocs.org/sdr/CALA2022092302446), Sep 23, 2022: LINE. LEAKING. CENTER HYDRAULIC SYSTEM LOST ALL FLUID. EMERGENCY LANDING DECLARED. ADP PRESSURE/CASE DRAIN FILTER MODULE CASE DRAIN PIPE IS SHEARED CASE DRAIN PIPE (GREEN) AND
- [SDR AALA2022080900001](https://openairdocs.org/sdr/AALA2022080900001), Aug 9, 2022: STRINGER. CORRODED. TEST, TEST, TEST - B767-53-3-7058 BULK CARGO STA 1540-STA 1562 S37L STRINGER FOUND CORRODED BULK CARGO COMPT STA 1540-1562 S37L STRINGER REPAIRED AS PER SRM53-0
- [SDR CALA2022040800936](https://openairdocs.org/sdr/CALA2022040800936), Apr 8, 2022: ACCESS PANEL. MISSING. INSPECTION ACCESS PANEL MISSING RT WING LEADING EDGE SLAT MECHANISM LUBRICATION ACCESS DOOR 621XB ITEM PLACED ON CDL MISSING PLACED ON CW CDL OK TO CONTINUE DIS
- [SDR CALA2022032300758](https://openairdocs.org/sdr/CALA2022032300758), Mar 23, 2022: SWITCH. NONE. SMOKE IN FLIGHT DECK CREW DEBRIEF: THE FLIGHT CREW STATED AT THE APPROXIMATE SAME SPOKE WITH TOMC AND WE WILL START THE AMM TASK 05-51-56-940-8 ACCOMPLISHED INI
- [SDR CALA2022030300562](https://openairdocs.org/sdr/CALA2022030300562), Mar 3, 2022: LENS. NONE. EXTERIOR EMERGENCY LIGHTING SYSTEM HAS BEEN DEFERRED IN COMPLIANCE WITH CDL CARD 335110 AND REF LOGPAGE 8107342 REPAIR TO BE CARRIED OUT WITHIN 1 FLT CYCLE. EXT
- [SDR CALA2021071201071](https://openairdocs.org/sdr/CALA2021071201071), Jul 11, 2021: SENSOR. FAULTED. LE SLAT ASSYM EICAS ALERTED TWICE FLAP INDICATOR INDICATED BETWE EN 0 AND 1 ACCOMPLISHED FSEU BITE CHECK FAULT IMAGE UPDATED COULD NOT DUPLICATE FLAP ASYMMETRY 
- [SDR CALA2021060400791](https://openairdocs.org/sdr/CALA2021060400791), Jun 4, 2021: FLOAT VALVE. MISINSTALLED. SUPPORT TASK - L/H WING AUX TANK NGS FLOAT VALVE INCORRECT INSTALLED REFER NR LP 9131168. LHW AUX TANK NGS FLOAT VALVE AND COVER PLATE RELOCATED TO BTN STR U-13
- [SDR CALA2020032000617](https://openairdocs.org/sdr/CALA2020032000617), Mar 10, 2020: WARNING SYSTEM. FALSE ACTIVATION. AUTO-THROTTLE EICAS MSG ON TAKEOFF LOW SPEED ABORT PERFORMED GROUND VISUAL FOR REJECTED TAKEOFF. PERFORMED MCDP GROUND TEST 2 AND TEST 30. TEST PASSED AS PER AM
- [SDR CALA2019052700843](https://openairdocs.org/sdr/CALA2019052700843), May 25, 2019: SHEAR TIE. CORRODED. SUPPORT TASK - QC PICKUP SHEET AFT COMPARTMENT BS 1562 FRAME AFT SHEAR TIE CORRODED BETWEEN STR 39L-39R REFER NR LP 9132543 AFT COMPARTMENT STA 1562 BETWEEN S39
- [SDR CALA2019052400005](https://openairdocs.org/sdr/CALA2019052400005), May 23, 2019: FITTING. CORRODED. REF NR LP 9132453 - SUPPORT TASK - EA 5340-01478 REV E OP 007 AD 2012-09-04 LT SIDE STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP "T" FITTING FOUND SURFACE CORROSIO
- [SDR CALA2019052400004](https://openairdocs.org/sdr/CALA2019052400004), May 19, 2019: STRINGER. CORRODED. B767-53-3-7058 BULK CARGO STA 1540-STA 1562 S37L STRINGER FOUND CORRODED BULK CARGO COMPT STA 1540-1562 S37L STRINGER REPAIRED AS PER SRM53-00-03 REPAIR 2 AND R
- [SDR CALA2019052400003](https://openairdocs.org/sdr/CALA2019052400003), May 19, 2019: STRINGER CLIP. CORRODED. REF NR LP 9131853 - B767-53-3-7058 BULK CARGO COMPT STA 1540 AND STA 1562 S37L ATTACH STRINGER CLIPS FOUND CORROSION BULK CARGO COMPT STA1540 AND STA1562 S37L S
- [SDR CALA2019051300001](https://openairdocs.org/sdr/CALA2019051300001), May 4, 2019: SKIN. CORRODED. BULK CARGO STA 1540 STR 37L AREA INTERIOR SKIN FOUND CORROSION. REPAIRED IAW ECRA 5331-02373PART 1 ITERIM REPAIR AT NRC TJE518820 INSP 156019. REPAIR IS CONSIDE

## 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

## Related

- Other Boeing 767-3CB aircraft: https://openairdocs.org/model/boeing-767-3cb/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.