# N176CA: 1990 Boeing 757-28A

- Status: Valid registration
- Airframe: [Boeing 757-28A](https://openairdocs.org/model/boeing-757-28a) (registry code 1384976, 249 seats)
- Engine: [Rolls-Royce RB211-535E4 series](https://openairdocs.org/engine/rolls-royce-rb211-535e4-series) (registry code 54223)
- Data sheets: [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 24543
- Year built: 1990
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 10, 2012
- Certificate issued: January 5, 2021
- Expires: January 31, 2028
- Mode S code: A12FAA
- Registered owner: [Cascade Spares Inc](https://openairdocs.org/faa-owner/CASCADE%20SPARES%20INC)
- Location: [Knoxville, TN](https://openairdocs.org/faa-place/TN/Knoxville)
- Owner type: Corporation
- Owner's area on the map: 35.9763° N, 84.1263° W: Placed by OpenAirDocs at the center of ZIP code 37931, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=176CA
- Page: https://openairdocs.org/aircraft/N176CA

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. The registry lists only the engine series, so ADs for every Rolls-Royce RB211-535E4 model are included.

## ADs that may apply (OpenAirDocs): 20 in force

### Matched by airframe (Boeing 757-28A)

None in force.

### Matched by engine (Rolls-Royce RB211-535E4 series)

- [AD 2024-10-06](https://openairdocs.org/ad/2024-10-06): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jun 27, 2024
- [AD 2020-08-03](https://openairdocs.org/ad/2020-08-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective May 18, 2020
- [AD 2017-24-08](https://openairdocs.org/ad/2017-24-08): Fuel control/Turbine engines · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 16, 2018
- [AD 2016-03-04](https://openairdocs.org/ad/2016-03-04): Life-limited rotating parts · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Mar 15, 2016
- [AD 2013-23-17](https://openairdocs.org/ad/2013-23-17): High-pressure (HP) and intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-C-37 and 3 more. Effective Dec 11, 2013
- [AD 2013-16-23](https://openairdocs.org/ad/2013-16-23): Cracked and distorted FCL metering panel · Rolls-Royce RB211-524B-02, RB211-524B2-19, RB211-524B3-02 and 13 more. Effective Oct 8, 2013
- [AD 2012-25-09](https://openairdocs.org/ad/2012-25-09): Intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 10 more. Effective Feb 6, 2013
- [AD 2012-02-11](https://openairdocs.org/ad/2012-02-11): LP turbine stage 1, 2, and 3 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Mar 6, 2012
- [AD 2009-20-14](https://openairdocs.org/ad/2009-20-14): Eddy current inspection (ECI) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Nov 17, 2009
- [AD 2008-20-04](https://openairdocs.org/ad/2008-20-04): HP turbine discs · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 26 more. Effective Nov 3, 2008
- [AD 2006-11-05 R2](https://openairdocs.org/ad/2006-11-05-R2): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 21, 2008
- [AD 2007-14-07](https://openairdocs.org/ad/2007-14-07): Fluorescent penetrant inspections (FPI) · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 21 more. Effective Aug 16, 2007
- [AD 2006-17-12](https://openairdocs.org/ad/2006-17-12): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Sep 27, 2006
- [AD 2004-19-04](https://openairdocs.org/ad/2004-19-04): Critical Life-Limited Rotating Engine Parts · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Nov 1, 2004
- [AD 2004-01-21](https://openairdocs.org/ad/2004-01-21): Frount engine mount housing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 27, 2004
- [AD 2003-10-03 R1](https://openairdocs.org/ad/2003-10-03-R1): High pressure (HP) turbine discs · Rolls-Royce RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2001-19-05](https://openairdocs.org/ad/2001-19-05): High Speed Gearbox Drive · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Oct 11, 2001
- [AD 2000-09-14](https://openairdocs.org/ad/2000-09-14): Radial Drive Steady Bearings · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Jul 11, 2000
- [AD 97-02-12](https://openairdocs.org/ad/97-02-12): Fuel Flow Governor (FFG) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 4, 1997
- [AD 87-25-04](https://openairdocs.org/ad/87-25-04): Fuel Quantity Indication System · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Dec 8, 1987

### Historical (superseded or no longer in force)

- [AD 2015-17-21](https://openairdocs.org/ad/2015-17-21) (historical): High-pressure turbine (HPT) disks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Dec 2, 2015
- [AD 2014-24-08](https://openairdocs.org/ad/2014-24-08) (historical): Fuel leaks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 6, 2015
- [AD 2013-19-18](https://openairdocs.org/ad/2013-19-18) (historical): LPT stage 2 disc failure · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Nov 7, 2013
- [AD 2013-19-17](https://openairdocs.org/ad/2013-19-17) (historical): Failure of rotating life limited parts · Rolls-Royce RB211-535E4-B-37. Effective Nov 7, 2013
- [AD 2011-11-08](https://openairdocs.org/ad/2011-11-08) (historical): LP Turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Jun 30, 2011
- [AD 2008-22-24](https://openairdocs.org/ad/2008-22-24) (historical): Low pressure compressor (LPC) fan blade · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 9, 2008
- [AD 2006-11-05 R1](https://openairdocs.org/ad/2006-11-05-R1) (historical): Disc assemblies · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective May 1, 2007
- [AD 2006-11-05](https://openairdocs.org/ad/2006-11-05) (historical): High pressure compressor (HPC) stage 3 disc assemblies · Rolls-Royce RB211-22B-02, RB211-524B-02, RB211-524B-B-02 and 24 more. Effective Jun 27, 2006
- [AD 2005-02-05](https://openairdocs.org/ad/2005-02-05) (historical): Low Pressure Compressor (LPC) Fan Blade Roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Feb 11, 2005
- [AD 2004-26-03](https://openairdocs.org/ad/2004-26-03) (historical): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Jan 13, 2005
- [AD 2004-01-20](https://openairdocs.org/ad/2004-01-20) (historical): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 24, 2004
- [AD 2003-17-15](https://openairdocs.org/ad/2003-17-15) (historical): Low pressure (LP) turbine stage 2 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Oct 2, 2003
- [AD 2003-12-15](https://openairdocs.org/ad/2003-12-15) (historical): LPC fan blade roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jul 30, 2003
- [AD 2003-10-03](https://openairdocs.org/ad/2003-10-03) (historical): High Pressure (HP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2002-23-08](https://openairdocs.org/ad/2002-23-08) (historical): Low Pressure (LP) Turbine Stage 2 Discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 30, 2002
- [AD 2001-23-02](https://openairdocs.org/ad/2001-23-02) (historical): High Pressure Turbine Disks · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 2 more. Effective Dec 24, 2001
- [AD 98-07-07](https://openairdocs.org/ad/98-07-07) (historical): Fuel System Tube Assembly · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 29, 1998
- [AD 86-07-01](https://openairdocs.org/ad/86-07-01) (historical): Outer Combustion Case Inspection · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective May 16, 1986

## Information bulletins (advisory) (1 in force)

- [SAIB 2026-11](https://openairdocs.org/saib/2026-11): Theft of Turbofan Engine Parts before Mutilation. Issued Jun 8, 2026

## NTSB investigations

None matched to N176CA.

## FAA accident and incident reports

None matched to N176CA.

## Service difficulty reports (109, 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 U2RA201809190001](https://openairdocs.org/sdr/U2RA201809190001), Sep 19, 2018: OVEN. SMOKE. AFT GALLEY LEFT HAND NR 3 OVEN SMOKING WHEN IN USE. CIRCUIT BREAKER PULLED. OVEN PLACED ON NON-ESSENTIAL FURNISHING DEFERRED MAINTENANCE ITEM, IN ACCORDANCE WIT
- [SDR U2RA201807240001](https://openairdocs.org/sdr/U2RA201807240001), Jul 29, 2018: LIGHT. INOPERATIVE. GIRT BAR ENGAGEMENT LIGHT FLICKERS AND GOES OUT AT R2 DOOR. REPLACED L2 DOOR ARM LIGHT ASSEMBLY IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 25-66-00.
- [SDR U2RA201807120001](https://openairdocs.org/sdr/U2RA201807120001), Jul 12, 2018: SENSOR. OBSTRUCTED. RIGHT NR 2 MAIN ENTRY DOOR GIRT BAR ENGAGEMENT LIGHT INTERMITTENT. CLEANED DEBRIS FROM RIGHT NR 2 MAIN ENTRY DOOR SENSOR. PERFORMED OPERATIONAL CHECK DOOR ARMIN
- [SDR U2RA201806090002](https://openairdocs.org/sdr/U2RA201806090002), Jun 9, 2018: LIGHT. INOPERATIVE. EMERGENCY AISLE LIGHT AT SEAT ROW 9ABC INOP - RELAMPED EMERGENCY LIGHT PER AMM 33-51-05, OPS NORMAL.
- [SDR U2RA20180419001](https://openairdocs.org/sdr/U2RA20180419001), Apr 18, 2018: BULB. INOPERATIVE. WITH THE EMERGENCY LIGHTS ON , THE AFT LEFT EXIT SIGN HAS ONLY 3 LIGHT BULBS WORKING.. REPLACED THE BULBS IAW AMM 33-51-10. OPS TESTED SATISFACTORY.
- [SDR U2RA201803210002](https://openairdocs.org/sdr/U2RA201803210002), Mar 21, 2018: LAMP. INOPERATIVE. R3 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP AND OPS CHECKED NORMAL.
- [SDR U2RA201803210001](https://openairdocs.org/sdr/U2RA201803210001), Mar 21, 2018: LAMP. INOPERATIVE. R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP AND OPS CHECKED NORMAL.
- [SDR U2RA201802110002](https://openairdocs.org/sdr/U2RA201802110002), Feb 10, 2018: BATTERY. DISCHARGED. DOORS 3 LEFT AND 3 RIGHT EXTERNAL EMERGENCY LIGHTS ARE INOPERATIVE. CHARGED EMERGENCY LIGHT BATTERIES PER AIRCRAFT MAINTENANCE MANUAL 33-51-07. LIGHT OPERATES N
- [SDR U2RA201802110001](https://openairdocs.org/sdr/U2RA201802110001), Feb 10, 2018: BATTERY. DISCHARGED. INTERNAL EMERGENCY LIGHT AT NUMBER 3 LEFT DOOR IS INOPERATIVE. - CHARGED EMERGENCY LIGHT BATTERIES PER AIRCRAFT MAINTENANCE MANUAL 33-51-07. LIGHT OPERATES NORM
- [SDR U2RA201802010001](https://openairdocs.org/sdr/U2RA201802010001), Feb 1, 2018: ACTUATOR. CRACKED. FLUID LEAK NOTED ON THE RIGHT WING. FOUND THE NR 11 SPOILER ACTUATOR CASTING CRACKED AT PRESSURE FITTING. REMOVED AND REPLACED SPOILER ACTUATOR IAW AMM 27-61-02
- [SDR U2RA201801100001](https://openairdocs.org/sdr/U2RA201801100001), Jan 10, 2018: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT AT THE L3 DOOR FOUND INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-06.
- [SDR U2RA201711050001](https://openairdocs.org/sdr/U2RA201711050001), Nov 5, 2017: SLEEVE. PERFORATED. NR 1 ENGINE, OUTBOARD THRUST REVERSER INNER SLEEVE PANEL PERFORATED AT THE 7:00 POSITION. REPAIRED IAW EA 17131, REVISION IR.
- [SDR U2RA201705180001](https://openairdocs.org/sdr/U2RA201705180001), May 18, 2017: BULKHEAD WEB. CHAFED. APU COMPARTMENT FORWARD BULKHEAD CHAFED AT BS 1885 AND RBL 6, APPROXIMATELY 8 INCHES FROM LOWER EDGE OF BULKHEAD. REPAIRED THE FIREWALL IAW SRM 53-80-08, REPAIR
- [SDR U2RA201705150001](https://openairdocs.org/sdr/U2RA201705150001), May 15, 2017: STRAP. CRACKED. FLOORBEAM BS 365, BL 0, ABOVE NOSE GEAR BOX HAS A BROKEN STRAP. REMOVED AND REPLACED THE STRAP IAW SRM 53-00-51, SRM 53-00-51, SRM 53-00-51, SRM 51-40-02, AND S
- [SDR U2RA201704180001](https://openairdocs.org/sdr/U2RA201704180001), Apr 18, 2017: LIGHT. INOPERATIVE. EXTERIOR EMERGENCY LIGHT AT R3 DOOR IS INOPERATIVE. REPLACED LAMP AT EXTERNAL EMERGENCY LIGHT AT R3 DOOR PER MM 33-51-06.
- [SDR U2RA201702060001](https://openairdocs.org/sdr/U2RA201702060001), Feb 6, 2017: CHARGER. INOPERATIVE. R3 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY CHARGER IAW AMM 33-51-07. OPS CHECKED GOOD.
- [SDR U2RA201701170001](https://openairdocs.org/sdr/U2RA201701170001), Jan 17, 2017: BATTERY PACK. INOPERATIVE. L1 EMERGENCY LIGHT INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07. SYSTEM OPS CHECKED GOOD.
- [SDR U2RA201611270001](https://openairdocs.org/sdr/U2RA201611270001), Nov 27, 2016: BATTERY PACK. INOPERATIVE. L1 DOOR EMERGENCY LIGHTS INOPERATIVE REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-07.
- [SDR U2RA201611070002](https://openairdocs.org/sdr/U2RA201611070002), Nov 7, 2016: CHARGER. INOPERATIVE. RIGHT AFT CABIN EMERGENCY LIGHT BATTERY CHARGER FAILED DURING TEST. REMOVED AND REPLACED RIGHT AFT CABIN EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY IN ACCORDANCE 
- [SDR U2RA201611070001](https://openairdocs.org/sdr/U2RA201611070001), Nov 7, 2016: CHARGER. INOPERATIVE. LEFT AFT CABIN EMERGENCY LIGHT BATTERY CHARGER FAILED DURING TEST. REMOVED AND REPLACED LEFT AFT CABIN EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY IN ACCORDANCE WI
- [SDR U2RA201609160001](https://openairdocs.org/sdr/U2RA201609160001), Sep 16, 2016: LIGHT. INOPERATIVE. DURING INSPECTION, FOUND RT AFT EMERGENCY EXTERIOR LIGHT LAMP NOT ILLUMINATED. R & R LIGHT BULB AND PERFORMED OPS CHECK IAW AMM 33-51-07.
- [SDR U2RA201609090002](https://openairdocs.org/sdr/U2RA201609090002), Sep 9, 2016: LAMP. INOPERATIVE. DURING FLIGHT WALK AROUND INSPECTION, L1 DOOR EXTERIOR EMERGENCY LIGHT FOUND INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR U2RA201609090001](https://openairdocs.org/sdr/U2RA201609090001), Sep 9, 2016: POWER SUPPLY. INOPERATIVE. DURING FLIGHT WALK AROUND INSPECTION, R1 DOOR EXTERIOR EMERGENCY LIGHT FOUND INOPERATIVE. REMOVED AND REPLACED THE FWD DOOR POWER SUPPLY IAW AMM 33-51-07. OPS C
- [SDR U2RA201607200001](https://openairdocs.org/sdr/U2RA201607200001), Jul 20, 2016: LAMP. DEFECTIVE. SLIDE LIGHT AT DOOR R2 WILL NOT ILLUMINATE. REPLACED THE LAMP IAW AMM 33-16-02, CHECKED OK. OK FOR SERVICE.
- [SDR U2RA201605040001](https://openairdocs.org/sdr/U2RA201605040001), May 4, 2016: BATTERY PACK. DISCHARGED. DURING OPS CHECK OF EMERGENCY EXIT LIGHT, DOOR 2 LT AND 2 RT AND SEAT ROWS 2 THROUGH 6 OVERHEAD EMERGENCY EXIT LIGHTS FOUND INOPERATIVE. R & R EMERGENCY EXIT LI
- [SDR U2RA201511090002](https://openairdocs.org/sdr/U2RA201511090002), Nov 9, 2015: FRAME. CRACKED. LEFT WING AT WS 70. L/E ACCESS PANEL FRAME CRACKED, CRACK LENGTH 1.5". CRACK REPAIRED IAW FAS EA 15777.
- [SDR U2RA201511050001](https://openairdocs.org/sdr/U2RA201511050001), Nov 5, 2015: TEE FITTING. CORRODED. RIGHT AT BS 1220, WING TO BODY FAIRING, T-CHORD HAS CORROSION AT BOTTOM END. REPLACED WING TO BODY FAIRING T-CHORD.
- [SDR U2RA201511020002](https://openairdocs.org/sdr/U2RA201511020002), Nov 2, 2015: SUPPORT FRAME. CORRODED. LOWER FUSELAGE RT SIDE AT WING TO BODY FAIRING PANEL 196DR. CORROSION ON SUPPORT FRAME. SUPPORT FRAME REPLACED WITH NEW SUPPORT FRAME.
- [SDR U2RA201511020001](https://openairdocs.org/sdr/U2RA201511020001), Nov 2, 2015: RESERVOIR. LOW PRESSURE. LEFT NR 4 ENTRY DOOR POWER ASSIST RESERVOIR HAS LOW PRESSURE. SERVICED RESERVOIR IAW AMM 12-15-10.
- [SDR U2RA201511090001](https://openairdocs.org/sdr/U2RA201511090001), Oct 24, 2015: FRAME. CRACKED. RIGHT NR 2 DOOR FORWARD SIDE UPPER HINGE ROD CUTOUT CRACKED. CRACK LENGTH 1.5". REPAIRED RT NR 2 DOOR FORWARD SIDE UPPER HINGE CUTOUT IAW SRM 52-10-02, REPAIR 1
- [SDR U2RA201510220001](https://openairdocs.org/sdr/U2RA201510220001), Oct 22, 2015: SKIN. DENTED. LEFT INBD FLAP OTBD AREA LOWER SIDE HAS 3 EACH DENTS BETWEEN WRS 320-340. REPAIRED LEFT INBD FLAP LOWERSKIN IAW SRM 57-53-01-2R-1, REPAIR 1, AND SRM 51-70-10, R
- [SDR U2RA201510210004](https://openairdocs.org/sdr/U2RA201510210004), Oct 21, 2015: LAMP. BURNED OUT. LEFT NR 2 ENTRY/EXIT DOOR EMERGENCY ESCAPE SLIDE LIGHT IS INOPERATIVE. REPLACED LT NR 2 ENTRY/EXIT DOOR EMERGENCY ESCAPE SLIDE LAMP IAW AMM 33-51-06, OPERATIONA
- [SDR U2RA201510210003](https://openairdocs.org/sdr/U2RA201510210003), Oct 21, 2015: RECEPTACLE. DIRTY. RIGHT NR 4 ENTRY/EXIT DOOR EMERGENCY ESCAPE SLIDE LIGHT IS INOPERATIVE. CLEANED RT NR 4 ENTRY/EXIT DOOR EMERGENCY ESCAPE SLIDE LAMP RECEPTACLE, INSTALLED LAMP. 
- [SDR U2RA201510210002](https://openairdocs.org/sdr/U2RA201510210002), Oct 21, 2015: POWER SUPPLY. INOPERATIVE. RIGHT NR 3 EMERGENCY EXIT DOOR ESCAPE SLIDE LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT POWER SUPPLY ASSEMBLY AND ESCAPE SLIDE LAMP. PERFORMED SATISFACTORY OPS 
- [SDR U2RA201510210001](https://openairdocs.org/sdr/U2RA201510210001), Oct 21, 2015: LAMP. BURNED OUT. LEFT NR 4 ENTRY/EXIT DOOR ESCAPE SLIDE LIGHT INOPERATIVE. RELAMPED LT NR 4 ENTRY/EXIT DOOR EMERGENCY ESCAPE SLIDE LIGHT IAW AMM 33-51-06, OPERATIONALLY TESTS GO
- [SDR U2RA201511180001](https://openairdocs.org/sdr/U2RA201511180001), Oct 21, 2015: CONNECTOR. NOT SEATED. ALL EMERGENCY EXIT SIGNS IN THE AFT GALLEY AT BS 1664 ARE INOPERATIVE. FOUND CONNECTOR D78 NOT PROPERLY SEATED. SECURED CONNECTOR D78. PERFOMED SATISFACTORY OPS
- [SDR U2RA201506260003](https://openairdocs.org/sdr/U2RA201506260003), Jun 26, 2015: BULB. INOPERATIVE. DURING ACCOMPLISHMENT OF TASK CARD 33-001-00-01, FOUND EMERGENCY LIGHT ASSY AT FLOOR LEVEL OF THE LT NR 2 DOOR WITH SOME OF THE BULBS INOPERATIVE.
- [SDR U2RA201506260002](https://openairdocs.org/sdr/U2RA201506260002), Jun 26, 2015: LIGHT. INOPERATIVE. DURING ACCOMPLISHMENT OF TASK CARD 33-001-00-01, FOUND EMERGENCY LIGHT OVERHEAD OF SEAT 16D INOPERATIVE.
- [SDR U2RA201506260001](https://openairdocs.org/sdr/U2RA201506260001), Jun 26, 2015: LIGHT. INOPERATIVE. DURING ACCOMPLISHMENT OF TASK CARD 33-001-00-01, FOUND RT EMERGENCY EXIT DOOR (R-3) EXTERIOR LIGHT INOPERATIVE.
- [SDR U2RA201410220001](https://openairdocs.org/sdr/U2RA201410220001), Oct 22, 2014: BATTERY PACK. DISCHARGED. WHILE ACCOMPLISHING TASK CARD 33-001-00-01 FOUND EMER EXIT LIGHT AT SEAT ROW 25 LT INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-01. TESTED NORMAL.
- [SDR U2RA201410170009](https://openairdocs.org/sdr/U2RA201410170009), Oct 17, 2014: LIGHT. INOPERATIVE. EMERGENCY AISLE LIGHT AT SEAT ROW 21 LT BELOW OVERHEAD BIN IS INOPERATIVE.
- [SDR U2RA201410170008](https://openairdocs.org/sdr/U2RA201410170008), Oct 17, 2014: LIGHT. INOPERATIVE. EMERGENCY AISLE LIGHT AT SEAT ROW 20 RT BELOW OVERHEAD BIN INOPERATIVE.
- [SDR U2RA201410170007](https://openairdocs.org/sdr/U2RA201410170007), Oct 17, 2014: LIGHT. INOPERATIVE. EMERGENCY AISLE LIGHT AT SEAT ROW 18 LT BELOW OVERHEAD BIN INOPERATIVE.
- [SDR U2RA201410170006](https://openairdocs.org/sdr/U2RA201410170006), Oct 17, 2014: LIGHT. INOPERATIVE. LEFT PAX DOOR 2 SIDEWALL EXIT LIGHT HAS TWO EACH BULBS BURNT OUT. LAMPED L2 DOOR SIDEWALL EXIT LIGHT IAW AMM 33-51-01. TESTED GOOD.
- [SDR U2RA201410170005](https://openairdocs.org/sdr/U2RA201410170005), Oct 17, 2014: LIGHT. INOPERATIVE. LEFT PAX DOOR 1 SIDEWALL EXIT LIGHT HAS 1 EACH BULB BURNT OUT. LAMPED L1 DOOR SIDEWALL EXIT LIGHT IAW AMM 33-51-01. TESTED GOOD.
- [SDR U2RA201410170004](https://openairdocs.org/sdr/U2RA201410170004), Oct 17, 2014: LIGHT. INOPERATIVE. WHILE ACCOMPLISHING TASK CARD 33-001-00-01 FOUND RT EMER EXIT DOOR LIGHT INOPERATIVE. R & R BURNT LAMPS IAW AMM 33-51-01. TESTED GOOD.
- [SDR U2RA201410170003](https://openairdocs.org/sdr/U2RA201410170003), Oct 17, 2014: LIGHT. INOPERATIVE. WHILE ACCOMPLISHING TASK CARD 33-001-00-01 FOUND RT PAX DOOR 1 EMER EXIT LIGHT INOPERATIVE. R & R LAMPS IAW AMM 33-51-01. TESTED GOOD.
- [SDR U2RA201410170002](https://openairdocs.org/sdr/U2RA201410170002), Oct 17, 2014: LIGHT. INOPERATIVE. WHILE ACCOMPLISHING TASK CARD 33-001-00-01 FOUND LT PAX DOOR 1 EMER EXIT LIGHT INOPERATIVE. R & R LAMPS IAW AMM 33-51-01. TESTED GOOD.
- [SDR U2RA201408290011](https://openairdocs.org/sdr/U2RA201408290011), Aug 26, 2014: BATTERY PACK. DISCHARGED. WHILE PERFORMING TASK CARD 33-001-00-01 FOUND EMER BATTERY PACK AT L1 DOOR INOPERATIVE. REPLACED BATTERY PACK.
- [SDR U2RA201406110001](https://openairdocs.org/sdr/U2RA201406110001), Jun 11, 2014: WINDOW. CRACKED. CRACK FOUND AT FIRST OFFICER`S WINDOW R 1.

All 109: https://openairdocs.org/aircraft/N176CA/reports.md

## STCs that may be installed (OpenAirDocs) (1)

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 (Rolls-Royce RB211-535E4 series)

- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc. Lists RB211-535E4-37

## Related

- Other Boeing 757-28A aircraft: https://openairdocs.org/model/boeing-757-28a/aircraft.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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