# Rolls-Royce RB211-535E437

- Type: Engine model (FAA registry)
- Registry code: 54053
- Manufacturer (registry): ROLLS-ROYC
- Model: RB211-535E437
- Engine type: Turbo-fan
- Power: 39,610 lb thrust
- Data sheet: [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (OpenAirDocs)
- Holder: Rolls-Royce Deutschland Ltd & Co KG
- Installed in: 6 registered aircraft
- Page: https://openairdocs.org/engine/rolls-royce-rb211-535e437

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [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 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 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)

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

## Registered aircraft (6)

- [N757HW](https://openairdocs.org/aircraft/N757HW): [Honeywell Aerospace US LLC](https://openairdocs.org/faa-owner/HONEYWELL%20AEROSPACE%20US%20LLC), [Phoenix, AZ](https://openairdocs.org/faa-place/AZ/Phoenix), built 1982, S/N 22194
- [N783SP](https://openairdocs.org/aircraft/N783SP): [Kalitta Charters II LLC](https://openairdocs.org/faa-owner/KALITTA%20CHARTERS%20II%20LLC), [Ypsilanti, MI](https://openairdocs.org/faa-place/MI/Ypsilanti), built 1985, S/N 22611
- [N901FD](https://openairdocs.org/aircraft/N901FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1993, S/N 27122
- [N921FD](https://openairdocs.org/aircraft/N921FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1991, S/N 24924
- [N940FD](https://openairdocs.org/aircraft/N940FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1990, S/N 24772
- [N957FD](https://openairdocs.org/aircraft/N957FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1990, S/N 24774

## NTSB investigations (2)

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 DCA24FA002](https://openairdocs.org/ntsb/DCA24FA002), Oct 5, 2023: Boeing 757-236 (N977FD), Chattanooga, TN, substantial damage. Probable cause: The failure of the alternate gear extension system, which prevented the landing gear from being lowered. The cause of the system failure was a broken wire, due to tensile overload, between the…
- [NTSB BFO93IA175](https://openairdocs.org/ntsb/BFO93IA175), Sep 13, 1993: Boeing 757-200ER (N757NA), Jamaica, NY, incident, no damage. Probable cause: THE FAILURE OF THE LEFT HYDRAULIC PRESSURE SWITCH, WHICH CAUSED THE LEFT YAW DAMPER MODULE TO BECOME INOPERATIVE RESULTING IN UNCOMMANDED RUDDER MOVEMENTS DURING FLIGHT.

## FAA accident and incident reports (7)

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 20240522005149I](https://openairdocs.org/incident/20240522005149I), May 22, 2024: Boeing 757-225 (N757HW), Phoenix, AZ, No damage. On 05/22/2024 at approximately 1049 MST an experimental 757 aircraft was making its approach to Phoenix sky Harbor airport in Phoenix Arizona when it lost…
- [Incident 20150824023889I](https://openairdocs.org/incident/20150824023889I), Aug 24, 2015: Boeing 757-204 (N903NV), Austin, TX, No damage. High speed abort @110-120 due to rt engine EGT caution 79? Right N3 caution 9? Noted by mx ref fim fault tree 71-05 (819) no further inspection required. No…
- [Incident 20140118002459I](https://openairdocs.org/incident/20140118002459I), Jan 18, 2014: Boeing 757-23N (N203UW), Charlotte, NC, No damage. On takeoff water spilled out of the forward galley ice bin. Flight attendant slipped and injured her head and foot. Flight returned to Charlotte where medical…
- [Incident 20000107002559I](https://openairdocs.org/incident/20000107002559I), Jan 7, 2000: Boeing 75723A (N757NA), Las Vegas, NV, Minor damage. Flight 351 enroute from dfw to las on decent to Las Vegas could not deploy leading edge slats. Pliot and first officer followed in their qrh declaredan…
- [Incident 19990826024829I](https://openairdocs.org/incident/19990826024829I), Aug 26, 1999: Boeing 75723A (N757NA), Las Vegas, NV, Minor damage. During rotation a fire bell sounded and fire warning light illuminated on right engine. Smoke and fire was reported to the crew by ATC. Two f/a's aboard…
- [Incident 19940403009589I](https://openairdocs.org/incident/19940403009589I), Apr 3, 1994: Boeing 75723A (N757NA), Des Moines, IA. Lost oil presure. Secured NR1 engine. Found P3 sealing air tube had failed.
- [Incident 19930913038109I](https://openairdocs.org/incident/19930913038109I), Sep 13, 1993: Boeing 75723A (N757NA), New York, NY. Rudder ratio eicas message came on at alitude. Returned. Landed safely. Replaced righ rudder contro module.

## Service difficulty reports (236, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR 7C7A202409100005](https://openairdocs.org/sdr/7C7A202409100005), Sep 8, 2024: BATTERY PACK. WEAK. SEVERAL EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE WHEN SWITCHED ON
- [SDR 2024FA0000362](https://openairdocs.org/sdr/2024FA0000362), May 4, 2024: FIRE WARNING. FALSE INDICATION. NUMBER 1 ENGINE FIRE WARNING. IN FLIGHT ENGINE SHOUTDOWN, DISCHARGE NUMBER ONE AND NUMBER TWO FIRE EXTINGUISHER BOTTLES. FIRE WARNING REMAINED ON. DIVERTED TO A
- [SDR FDEA202104010807](https://openairdocs.org/sdr/FDEA202104010807), Apr 1, 2021: VALVE. FAILED. PDIS 901 73-21 4020 31MAR21 VIE FACT U R ENG FUEL VALVE LIGHT AFTER SHUTDOWN. OFF MPN: 8062-551 POS: 2 SRL: 2488744 TAG NBR: 8022F9 ON MPN: 8062-551 CPN: 731094
- [SDR FDEA202103310803](https://openairdocs.org/sdr/FDEA202103310803), Mar 31, 2021: STIFFENER. CRACKED. #2 ENGINE ,INBOARD THRUST REVERSER, LEADING EDGE, STIFFENER IS CRACKED REMOVED AND REPLACED CRACKED STIFFENER IAW B757 SRM 51-40-02 PAGE 11 AND 12 PARAGRAPH 5 A
- [SDR FDEA2020070631437](https://openairdocs.org/sdr/FDEA2020070631437), Jul 3, 2020: FRAME. DAMAGED. ENG NR 1 O/B UPPER AND LOWER "A" FRAMES FAIRING DAMAGED. PERFORMED TEMPORARY REPAIR OF DELAMINATED SKIN PLIES ON ENG NR 1 O/B UPPER AND LOWER "A" FRAME FAIRINGS
- [SDR AALA201906179022](https://openairdocs.org/sdr/AALA201906179022), Jun 14, 2019: CONNECTOR. DISCONNECTED. AIRCRAFT WAS GROUNDED: PILOT DIVERTED ON ACCOUNT OF MULTIPLE FLIGHT INSTRUMENT FAULTS/ELECTRONIC DISPLAY ISSUES. EMERGENCY WAS DECLARED. DURING INSPECTION, FOUN
- [SDR U2RA201811210001](https://openairdocs.org/sdr/U2RA201811210001), Nov 15, 2018: LAMP. BURNED OUT. DURING MAINTENANCE INSPECTION FOUND EMERGENCY AISLE LIGHT AT BULLNOSE OF OVERHEAD BIN 6A INOPERATIVE. REMOVED AND REPLACED AISLE LIGHT LAMP AT BIN 6A OVERHEAD B
- [SDR FDEA201805251317](https://openairdocs.org/sdr/FDEA201805251317), May 25, 2018: ENGINE. FAILED. DURING A TEST FLIGHT, 2 HOURS 39 MINUTES INTO FLIGHT, THE RIGHT ENGINE OIL QUANTITY WENT TO ZERO & OIL PRESSURE DECREASED TO 4 PSI IN THE RED BAND. SHUT THE RT 
- [SDR U2RA20180514001](https://openairdocs.org/sdr/U2RA20180514001), Mar 22, 2018: SKIN. GOUGED. DURING INSPECTION, FOUND THE LEFT OUTBOARD FLAP UPPER SURFACE WITH FIVE GOUGES IN THE SKIN, 32, & 38 INCHES FROM INBOARD END, AND 25 INCHES FROM TRAILING EDGE. 
- [SDR U2RA201704240001](https://openairdocs.org/sdr/U2RA201704240001), Apr 24, 2017: CONNECTOR. NOT SEATED. MAIN CABIN AT ROW 3 EMERGENCY AISLE LIGHT INOPERATIVE. RESEATED ENRGENCY LIGHT CONNECTOR AT SEAT ROW 3 IAW SWP 20-61-00. LIGHT OPS CHECKED GOOD IAW AMM 33-51-00
- [SDR U2RA201704240002](https://openairdocs.org/sdr/U2RA201704240002), Apr 24, 2017: CONNECTOR. NOT SEATED. MAIN CABIN AT ROW 10 EMERGENCY AISLE LIGHT INOPERATIVE. RESEATED THE ENRGENCY LIGHT CONNECTOR AT SEAT ROW 3 IAW SWP 20-61-00. LIGHT OPS CHECKED GOOD IAW AMM 51-
- [SDR U2RA201704240003](https://openairdocs.org/sdr/U2RA201704240003), Apr 24, 2017: CONNECTOR. NOT SEATED. MAIN CABIN AT ROW 30 EMERGENCY AISLE LIGHT INOPERATIVE. RESEATED ENRGENCY LIGHT CONNECTOR AT SEAT ROW 3 IAW SWPM 20-61-00. THE LIGHT OPS CHECKED GOOD IAW AMM 33
- [SDR U2RA201704240004](https://openairdocs.org/sdr/U2RA201704240004), Apr 24, 2017: CONNECTOR. NOT SEATED. MAIN PASSENGER CABIN AT ROW 7 EMERGENCY AISLE LIGHT INOPERATIVE. RESEATED ENRGENCY LIGHT CONNECTOR AT SEAT ROW 3 IAW SWPM 20-61-00. LIGHT OPS CHECKED GOOD AMM 3
- [SDR U2RA201703250001](https://openairdocs.org/sdr/U2RA201703250001), Mar 25, 2017: LIGHT. INOPERATIVE. EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 34 DOES NOT ILLUMINATE. RELAMPED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 34 IN ACCORDANCE WITH AMM 33-51-11 LIGHT TESTS 
- [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 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 U2RA201609220001](https://openairdocs.org/sdr/U2RA201609220001), Sep 22, 2016: SWITCH. DIRTY. L1 DOOR EXIT LIGHT INOPERATIVE. TROUBLESHOT SYSTEM IAW WIRING DIAGRAIM MANUAL 33-51-12. CLEANED AND SECURED EMERGENCY LIGHT SWITCH, ON P-5 PANEL. SYSTEM OPS CHE
- [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 AALA201609149028](https://openairdocs.org/sdr/AALA201609149028), Sep 12, 2016: ENGINE. ODOR. AIRCRAFT WAS GROUNDED: ON INITIAL DESCENT AS POWER REDUCED TO IDLE DEPARTING FL360, STRONG ODOR NOTICED ON FLIGHT DECK AND REPORTED BY F/A`S IN CABIN. AT INTERM
- [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 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 U2RA201609090003](https://openairdocs.org/sdr/U2RA201609090003), Sep 9, 2016: LAMP. INOPERATIVE. DURING DOD, AFTER FLIGHT WALK AROUND INSPECTION, R2 DOOR EXTERIOR EMERGENCY LIGHT FOUND INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR U2RA201609050001](https://openairdocs.org/sdr/U2RA201609050001), Sep 5, 2016: CONTROL MODULE. INOPERATIVE. SEVERAL AREAS OF EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACKS AND CONTROL MODULES IAW MM 33-51-07.
- [SDR U2RA201608160001](https://openairdocs.org/sdr/U2RA201608160001), Aug 16, 2016: TEE FITTING. CRACKED. RIGHT SHEAR PANEL AFT CORNER CRACKED AND CORRODED AT BS 1720 AFT BULKHEAD IN MAIN CABIN. REMOVED AND REPLACED THE TEE FITTING ANGLE IAW SRM 51-40-04. DRAWING 14
- [SDR U2RA201608160002](https://openairdocs.org/sdr/U2RA201608160002), Aug 16, 2016: CHANNEL. CORRODED. BS 355, STRINGER 17R, HAT CHANNEL HAS UPPER SURFACE CORROSION. REMOVED AND REPLACED THE HAT CHANNEL IAW SRM 51-40-02. DRAWING 141N8422.
- [SDR AALA201608159005](https://openairdocs.org/sdr/AALA201608159005), Aug 12, 2016: CIRCUIT CARD. MALFUNCTIONED. FLIGHT CREW REPORTED THAT DURING CLIMB OUT EICAS CAUTION RIGHT CENTER FUEL PUMP OCCURRED. AT 045 DEGREES WITH RT ENGINE N3 BEGAN TO FLUCTUATE ERRATICALLY BETWEE
- [SDR U2RA201608090001](https://openairdocs.org/sdr/U2RA201608090001), Aug 9, 2016: SUPPORT BRACKET. CORRODED. LEFT MAIN LANDING GEAR WHEEL WELL AFT INBOARD CORNER SUPPORT FROM AFT BULKHEAD TO CORNER BULKHEAD CORRODED. REMOVED AND REPLACED CORNER SUPPORT BARCKET IAW SRM 
- [SDR U2RA201608090002](https://openairdocs.org/sdr/U2RA201608090002), Aug 9, 2016: STRUCTURE. CORRODED. LEFT MAIN LANDING GEAR WHEEL WELL FORWARD DOOR CUTOUT, OUTBOARD SIDE HAS CORROSION. REPAIRED WING TO BODY FAIRING OUTER CHORD AT BS 1094 IAW ENGINEERING ORDER F
- [SDR U2RA201608080001](https://openairdocs.org/sdr/U2RA201608080001), Aug 8, 2016: SUPPORT CHANNEL. CRACKED. RIGHT MAIN LANDING GEAR FORWARD OUTBOARD LOWER DOOR CUTOUT STRUCTURE (WING TO BODY FAIRING) CRACKED UNDER PROXIMITY SENSOR. REMOVED AND REPLACED SUPPORT CHANNEL
- [SDR WX0A2016080873181](https://openairdocs.org/sdr/WX0A2016080873181), Aug 7, 2016: MONITOR. FAILED. EMERGENCY DECLARED, LT ENGINE VIB 2.6 WITH CLB, Z-POWER, ALTITUDE 17,000, EST, PERFORMED QRH ENGINE VIBRATION, 72.18, RETARDING THRUST. RETURNED VIBRATION TO NO
- [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 WX0A2016033173115](https://openairdocs.org/sdr/WX0A2016033173115), Mar 30, 2016: GEARBOX. FAULTY. DURING ARRIVAL THE CREW NOTED THAT THE RT OIL QTY HAD DECREASED TO 0, FOLLOWED QUICKLY BY THE RT OIL PRESS. EXECUTED QRH ENG FAILURE & SHUTDOWN CHECKLIST & SECU
- [SDR CA160222005](https://openairdocs.org/sdr/CA160222005), Feb 19, 2016: COMPUTER. MALFUNCTIONED. (CAN) ON DESCENT A "BURNED INSULATION" ODOR WAS NOTED, THE ODOR PERSISTED, BUT NO SMOKE WAS EVIDENT. ON THE GROUND, TROUBLESHOOTING REVEALED THE RT FLIGHT CONTR
- [SDR AALA201511259009](https://openairdocs.org/sdr/AALA201511259009), Nov 22, 2015: ENGINE. FAILED. INFLIGHT ENG SHUTDOWN. FLIGHT DIVERTED DUE TO A LT ENG FAILURE. AN EMER WAS DECLARED & THE ACFT LANDED SAFELY WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT EN
- [SDR CA151124002](https://openairdocs.org/sdr/CA151124002), Nov 20, 2015: TEE FITTING. CRACKED. (CAN) DURING PRE DEPARTURE MAINTENANCE FOUND HYDRAULIC LEAK IN LT WHEEL WELL. REPLACED TEE FITTING ON RETURN LINE OF CENTER AUTO PILOT AILERON SERVO. LEAK CHECK
- [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 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 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 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 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 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 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 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 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 AALA20150901005](https://openairdocs.org/sdr/AALA20150901005), Aug 31, 2015: SENSOR. INTERMITTENT. DURING CRUISE, THE LT ENG THRUST REVERSER DEPLOY LIGHT ILLUMINATED INTERMITTENTLY. EMERGENCY DECLARED, DIVERTED, AND LANDING UNEVENTFUL. R & R LT ENGINE SENSOR 
- [SDR U2RA201504290001](https://openairdocs.org/sdr/U2RA201504290001), Apr 29, 2015: POWER SUPPLY. INTERMITTENT. WITH EMERGENCY LIGHT SWITCH ARMED, VARIOUS EMERGENCY LIGHTS IN THE CABIN GO ON AND OFF AT RANDOM TIMES, WITH SWITCH IN ON POSITION, ALL OVERHEAD EMERGENCY LIGHT
- [SDR WX0A2015050172562](https://openairdocs.org/sdr/WX0A2015050172562), Apr 27, 2015: ATTENUATOR. MALFUNCTIONED. ON CLIMB OUT AROUND 2200"" AGT, VNAV SELECTION, LT ENG COMPRESSOR STALL, LT ENG EGT WENT TO 874 DEG. FLIGHT ATTENDANTS REPORTED FLAMES OUT OF LT ENG, FAULT CODE
- [SDR U2RA201504260001](https://openairdocs.org/sdr/U2RA201504260001), Apr 26, 2015: WINDOW. FAILED. F/O R-1 WINDOW SHATTERED IN FLIGHT. SHOWS SIGNS OF ARCING AND IS DEFORMED. R & R R-1 WINDOW IAW AMM 56-10-01. ALSO REPLACED WINDOW HEAT CONTROLLER IAW AMM 30-41

All 236: https://openairdocs.org/engine/rolls-royce-rb211-535e437/reports.md

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

Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

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

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