# Service difficulty reports: Rolls-Royce RB211-535E437 A list on [Rolls-Royce RB211-535E437](https://openairdocs.org/engine/rolls-royce-rb211-535e437.md). Newest first. General aviation reporting is voluntary. Page 1 of 5 · 236 reports - [SDR 7C7A202409100005](https://openairdocs.org/sdr/7C7A202409100005.md): Battery Pack · weak · Sep 8, 2024 · N629NP · Boeing 7572B7 · Emergency Lighting > SEVERAL EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE WHEN SWITCHED ON - [SDR 2024FA0000362](https://openairdocs.org/sdr/2024FA0000362.md): Fire Warning · false indication · May 4, 2024 · N629NP · Boeing 7572B7 · Fire Detection > NUMBER 1 ENGINE FIRE WARNING. IN FLIGHT ENGINE SHOUTDOWN, DISCHARGE NUMBER ONE AND NUMBER TWO FIRE EXTINGUISHER BOTTLES. FIRE WARNING REMAINED ON. DIVERTED TO ALTERNET AIRPORT. AFTER LANDING AN INSPECTION OF THE ENGINE NO EVIDENCE OF A FIRE WAS FOUND. - [SDR FDEA202104010807](https://openairdocs.org/sdr/FDEA202104010807.md): Valve · failed · Apr 1, 2021 · N901FD · Boeing 7572B7 · Fuel Controlling System > 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: 7310944 SRL: 2336761 - [SDR FDEA202103310803](https://openairdocs.org/sdr/FDEA202103310803.md): Stiffener · cracked · Mar 31, 2021 · N977FD · Boeing 757236 · Engine Thrust Reverser > #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 AND ROHR OVERHAUL SHOP DETAIL PARTS REFERENCE 78-31-00 - [SDR FDEA2020070631437](https://openairdocs.org/sdr/FDEA2020070631437.md): Frame · damaged · Jul 3, 2020 · N901FD · Boeing 7572B7 · Turbine Engine Compressor Section > 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 IAW AMM SUBTASK 72-34-10-308-038-R04. - [SDR AALA201906179022](https://openairdocs.org/sdr/AALA201906179022.md): Connector · disconnected · Jun 14, 2019 · N204UW · Boeing 75723N · Turbine Engine System Wiring > AIRCRAFT WAS GROUNDED: PILOT DIVERTED ON ACCOUNT OF MULTIPLE FLIGHT INSTRUMENT FAULTS/ELECTRONIC DISPLAY ISSUES. EMERGENCY WAS DECLARED. DURING INSPECTION, FOUND #2 ENGINE FIREWALL DISCONNECT CONNECTOR PLUG AND RECEPTACLE D1216J/9 HAS EVIDENCE OF SEVERE ARCIN - [SDR U2RA201811210001](https://openairdocs.org/sdr/U2RA201811210001.md): Lamp · burned out · Nov 15, 2018 · N567CA · Boeing 757223 · Emergency Lighting > DURING MAINTENANCE INSPECTION FOUND EMERGENCY AISLE LIGHT AT BULLNOSE OF OVERHEAD BIN 6A INOPERATIVE. REMOVED AND REPLACED AISLE LIGHT LAMP AT BIN 6A OVERHEAD BULLNOSE IN ACCORDANCE WITH B757 AMM 33-51-05. OPERATIONAL CHECK OF LIGHT FOUND SATISFACTORY. - [SDR FDEA201805251317](https://openairdocs.org/sdr/FDEA201805251317.md): Engine · failed · May 25, 2018 · N957FD · Boeing 75721B · Engine Oil Indicating System > 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 ENGINE DOWN. RT ENGINE VIBRATION BITE COMPLETED. NR 2 ENGINE REPLACED IAW TC 7180260-02-02. PER - [SDR U2RA20180514001](https://openairdocs.org/sdr/U2RA20180514001.md): Skin · gouged · Mar 22, 2018 · N567CA · Boeing 757223 · Trailing Edge Flaps > 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. ACCOMPLISHED INTERIM POTTED FILLER REPAIR OF LEFT OUTBOARD FLAP UPPER SKIN PANEL IAW EO 57-18111- - [SDR U2RA201704240001](https://openairdocs.org/sdr/U2RA201704240001.md): Connector · not seated · Apr 24, 2017 · N567CA · Boeing 757223 · Light System Wiring > 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.md): Connector · not seated · Apr 24, 2017 · N567CA · Boeing 757223 · Light System Wiring > 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 51-00. - [SDR U2RA201704240003](https://openairdocs.org/sdr/U2RA201704240003.md): Connector · not seated · Apr 24, 2017 · N567CA · Boeing 757223 · Emergency Lighting > 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 33-51-00 - [SDR U2RA201704240004](https://openairdocs.org/sdr/U2RA201704240004.md): Connector · not seated · Apr 24, 2017 · N567CA · Boeing 757223 · Light System Wiring > 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 33-51-00 - [SDR U2RA201703250001](https://openairdocs.org/sdr/U2RA201703250001.md): Light · inoperative · Mar 25, 2017 · N567CA · Boeing 757223 · Emergency Lighting > 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 GOOD. - [SDR U2RA201611070001](https://openairdocs.org/sdr/U2RA201611070001.md): Charger · inoperative · Nov 7, 2016 · N176CA · Boeing 75728A · Emergency Lighting > LEFT AFT CABIN EMERGENCY LIGHT BATTERY CHARGER FAILED DURING TEST. REMOVED AND REPLACED LEFT AFT CABIN EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY IN ACCORDANCE WITH AMM 33-51-07. OPERATIONAL CHECK FOUND SATISFACTORY. - [SDR U2RA201611070002](https://openairdocs.org/sdr/U2RA201611070002.md): Charger · inoperative · Nov 7, 2016 · N176CA · Boeing 75728A · Emergency Lighting > RIGHT AFT CABIN EMERGENCY LIGHT BATTERY CHARGER FAILED DURING TEST. REMOVED AND REPLACED RIGHT AFT CABIN EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY IN ACCORDANCE WITH AMM 33-51-07. OPERATIONAL CHECK FOUND SATISFACTORY. - [SDR U2RA201609220001](https://openairdocs.org/sdr/U2RA201609220001.md): Switch · dirty · Sep 22, 2016 · N567CA · Boeing 757223 · Emergency Lighting > 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 CHECKED SATISFACTORY IAW AMM 33-51-00. - [SDR U2RA201609160001](https://openairdocs.org/sdr/U2RA201609160001.md): Light · inoperative · Sep 16, 2016 · N176CA · Boeing 75728A · Emergency Lighting > 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.md): Engine · odor · Sep 12, 2016 · N203UW · Boeing 75723N · Engine (Turbine/Turboprop) > 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 INTERMEDIATE LEVEL OFF WITH POWER ABOVE IDLE ODOR DISSIPATED SOMEWHAT-EVERY TIME POWER REDUCED ODOR RETUR - [SDR U2RA201609090001](https://openairdocs.org/sdr/U2RA201609090001.md): Power Supply · inoperative · Sep 9, 2016 · N176CA · Boeing 75728A · Emergency Lighting > 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 CHECKED GOOD. - [SDR U2RA201609090002](https://openairdocs.org/sdr/U2RA201609090002.md): Lamp · inoperative · Sep 9, 2016 · N176CA · Boeing 75728A · Emergency Lighting > 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.md): Lamp · inoperative · Sep 9, 2016 · Boeing 75728A · Emergency Lighting > 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.md): Control Module · inoperative · Sep 5, 2016 · N567CA · Boeing 757223 · Emergency Lighting > 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.md): Tee Fitting · cracked · Aug 16, 2016 · N567CA · Boeing 757223 · Fuselage Main, Attach Fittings > 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 146N8722. - [SDR U2RA201608160002](https://openairdocs.org/sdr/U2RA201608160002.md): Channel · corroded · Aug 16, 2016 · N567CA · Boeing 757223 · Fuselage Miscellaneous Structure > 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.md): Circuit Card · malfunctioned · Aug 12, 2016 · N941UW · Boeing 7572B7 · Engine Indicating System > 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 BETWEEN 73-81%. NO VIBRATION OR SURGE NOTED. AIRCRAFT GROUNDED. MAINTENANCE REPLACED THE RT ENGINE SP - [SDR U2RA201608090001](https://openairdocs.org/sdr/U2RA201608090001.md): Support Bracket · corroded · Aug 9, 2016 · N567CA · Boeing 757223 · Fuselage Miscellaneous Structure > 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 51-40-02. DRAWING 144N8161. - [SDR U2RA201608090002](https://openairdocs.org/sdr/U2RA201608090002.md): Structure · corroded · Aug 9, 2016 · N567CA · Boeing 757223 · Fuselage Miscellaneous Structure > 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 FAS EA 16259. - [SDR U2RA201608080001](https://openairdocs.org/sdr/U2RA201608080001.md): Support Channel · cracked · Aug 8, 2016 · N567CA · Boeing 757223 · Fuselage Miscellaneous Structure > RIGHT MAIN LANDING GEAR FORWARD OUTBOARD LOWER DOOR CUTOUT STRUCTURE (WING TO BODY FAIRING) CRACKED UNDER PROXIMITY SENSOR. REMOVED AND REPLACED SUPPORT CHANNEL IN ACCORDANCE WITH B757 SRM 51-40-08 - [SDR WX0A2016080873181](https://openairdocs.org/sdr/WX0A2016080873181.md): Monitor · failed · Aug 7, 2016 · N903NV · Boeing 757204 · Engine Vibration Analyzer > 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 NORMAL LEVEL, HOWEVER VIBRATION APPEARED TO SLOWLY INCREASE AS FLT PROGRESSED WITH CRUISE POWER. - [SDR U2RA201605040001](https://openairdocs.org/sdr/U2RA201605040001.md): Battery Pack · discharged · May 4, 2016 · N176CA · Boeing 75728A · Emergency Lighting > 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 LIGHT BATTERY PACKS IAW AMM CHAPTER 33-51-07, ALL EMERGENCY EXIT LIGHTS OPERATIONALLY CHECK GOOD. - [SDR WX0A2016033173115](https://openairdocs.org/sdr/WX0A2016033173115.md): Gearbox · faulty · Mar 30, 2016 · N906NV · Boeing 757204 · Turbine Engine Accessory Drive > 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 & SECURED THE RT ENG. OCCURRED APPROX 10 MINS PRIOR TO LANDING. ENG WAS WINDMILLED APPROX 10 MIN. NO O - [SDR CA160222005](https://openairdocs.org/sdr/CA160222005.md): Computer · malfunctioned · Feb 19, 2016 · Boeing 7572B7 · Flight Controller > (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 CONTROL COMPUTER HAS INTERNALLY MALFUNCTIONED, CAUSING THE ODOR. THE FCC WAS REPLACED. - [SDR AALA201511259009](https://openairdocs.org/sdr/AALA201511259009.md): Engine · failed · Nov 22, 2015 · N204UW · Boeing 75723N · Engine (Turbine/Turboprop) > 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 ENGINE PER TASK CARD 19L40071001. - [SDR CA151124002](https://openairdocs.org/sdr/CA151124002.md): Tee Fitting · cracked · Nov 20, 2015 · Boeing 75728A · Hydraulic System, Main > (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 CARRIED OUT SERVICEABLE. - [SDR U2RA201511090002](https://openairdocs.org/sdr/U2RA201511090002.md): Frame · cracked · Nov 9, 2015 · N176CA · Boeing 75728A · Wing Main, Frame Structure > 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.md): Tee Fitting · corroded · Nov 5, 2015 · N176CA · Boeing 75728A · Aerodynamic Fairings > 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.md): Reservoir · low pressure · Nov 2, 2015 · N176CA · Boeing 75728A · Passenger/Crew Doors > 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.md): Support Frame · corroded · Nov 2, 2015 · N176CA · Boeing 75728A · Fuselage Miscellaneous Structure > 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.md): Frame · cracked · Oct 24, 2015 · N176CA · Boeing 75728A · Service Doors > 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.md): Skin · dented · Oct 22, 2015 · N176CA · Boeing 75728A · Trailing Edge Flaps > 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, REPAIR 2. - [SDR U2RA201511180001](https://openairdocs.org/sdr/U2RA201511180001.md): Connector · not seated · Oct 21, 2015 · N176CA · Boeing 75728A · Light System Wiring > 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 TEST OF EMERGENCY EXIT SIGNS AT AFT GALLEY IAW AMM 33-51-00. - [SDR U2RA201510210001](https://openairdocs.org/sdr/U2RA201510210001.md): Lamp · burned out · Oct 21, 2015 · N176CA · Boeing 75728A · Emergency Lighting > 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 GOOD. - [SDR U2RA201510210002](https://openairdocs.org/sdr/U2RA201510210002.md): Power Supply · inoperative · Oct 21, 2015 · N176CA · Boeing 75728A · Emergency Lighting > 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 TEST IAW AMM 33-51-07. - [SDR U2RA201510210003](https://openairdocs.org/sdr/U2RA201510210003.md): Receptacle · dirty · Oct 21, 2015 · N176CA · Boeing 75728A · Emergency Lighting > 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. PERFORMED SATISFACTORY TEST IAW AMM 33-51-07. - [SDR U2RA201510210004](https://openairdocs.org/sdr/U2RA201510210004.md): Lamp · burned out · Oct 21, 2015 · N176CA · Boeing 75728A · Emergency Lighting > 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, OPERATIONALLY TESTS GOOD. - [SDR AALA20150901005](https://openairdocs.org/sdr/AALA20150901005.md): Sensor · intermittent · Aug 31, 2015 · N687AA · Boeing 757223 · Engine Thrust Reverser > DURING CRUISE, THE LT ENG THRUST REVERSER DEPLOY LIGHT ILLUMINATED INTERMITTENTLY. EMERGENCY DECLARED, DIVERTED, AND LANDING UNEVENTFUL. R & R LT ENGINE SENSOR S436. OPS CHECKED NORMAL IAW AMM 78-30-00. - [SDR U2RA201504290001](https://openairdocs.org/sdr/U2RA201504290001.md): Power Supply · intermittent · Apr 29, 2015 · N567CA · Boeing 757223 · Emergency Lighting > 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 LIGHTS COME ON, BUT ONLY SOME FLOOR PATH LIGHTS WORK. R & R POWER SUPPLY ASSY IAW AMM 33-51-07. EMERGENC - [SDR WX0A2015050172562](https://openairdocs.org/sdr/WX0A2015050172562.md): Attenuator · malfunctioned · Apr 27, 2015 · N906NV · Boeing 757204 · Compressor Bleed Valve > 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 R7106XE01, REF LOG PAGE 557148. R & R TPU. OPERATIONS CHECKED GOOD. PERFORMED TEST NR 3 IP & HP - [SDR U2RA201504260001](https://openairdocs.org/sdr/U2RA201504260001.md): Window · failed · Apr 26, 2015 · N567CA · Boeing 757223 · Flight Compartment Windows > 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 30-41-01. OPS CHECK GOOD. Next page: https://openairdocs.org/engine/rolls-royce-rb211-535e437/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'RB211535E437' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/engine/rolls-royce-rb211-535e437/reports --- 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.