# Service difficulty reports: CFM International CFM56-5B5/P series

A list on [CFM International CFM56-5B5/P series](https://openairdocs.org/engine/cfm-international-cfm56-5b5-p-series.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 166 reports

- [SDR WX0A2024012631951](https://openairdocs.org/sdr/WX0A2024012631951.md): Hmu · faulted · Jan 25, 2024 · N313NV · Airbus A319111 · Fuel Controlling System
  > ENGINE 1 ROLLED BACK AT FL 370 IN CLEAR AIR AUTO IGNITION AND RE-LIGHT OCCURRED / PERFORMED TROUBLESHOOTING OF #1 ENGINE ROLLBACK IAW TSM 72-00-00-810-806-A. HMU FOUND BAD, REMOVED AND REPLACED PER IAW AMM 73-21-10-400-002, OPS AND LEAK CHECKS GOOD.
- [SDR WX0A2020010373451](https://openairdocs.org/sdr/WX0A2020010373451.md): Oil System · low · Jan 2, 2020 · N233NV · Airbus A320214 · Turbine Engine Oil System
  > EMERGENCY DECLARED, NR 1 ENGINE LOW OIL QTY INDICATION. REMOVED & REPLACED THE NR 1 ENGINE.
- [SDR F3LA201910240128](https://openairdocs.org/sdr/F3LA201910240128.md): Unknown · odor · Oct 22, 2019 · N229FR · Airbus A320214 · Air Distribution System
  > ODOR EVENT AT CRUISE ALTITUDE STARTED SLIGHT AND GOT VERY STRONG ODOR. DID QRH PROCEDURE FOR ODOR IN FLIGHT, THIS DID NOT CHANGE INTENSITY OF ODOR. CORRECTIVE ACTION: PLACED ON TDI -T 1156114 FOR 60 A.C. DUE AT AC 9424 BY AUTHORITY EA# A0-21T-34386 (ENG #2 I
- [SDR EE4Y2019040108585](https://openairdocs.org/sdr/EE4Y2019040108585.md): Inlet · cracked · Apr 1, 2019 · N774XF · Airbus A319112 · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE INLET COWL LIP SKIN AT 4 AND 12 O’CLOCK POSITION WITH TOOL MARKS AROUND FASTENERS HEAD.FOR CORRECTIVE ACTION SEE COOPESA NRI 4-86,ACTION TAKEN,PERFORMED PERMANENT REPAIR IAW COO-EO-2019-8117 R01 AND COLLINS AEROSPACE MESSAGE # CV19-01268 REV D.
- [SDR F3LA2018041000321](https://openairdocs.org/sdr/F3LA2018041000321.md): Mechanism · seized · Apr 5, 2018 · N923FR · Airbus A319111 · Compressor Bleed Control
  > DURING DESCENT AND RETARDING OF THROTTLES ENG-2 COMPRESSOR AND VANE ECAM APPEARED FOLLOWED BY COMPRESSOR STALL WHICH WAS FELT AND HEARD BY CREW. REMOVED AND REPLACED BLEED VALVE STOP MECHANISM REFERENCE AMM 75-31-20-400-002A. OPERATIONAL AND LEAK CHECK GOOD.
- [SDR F3LA2018041000322](https://openairdocs.org/sdr/F3LA2018041000322.md): Motor · seized · Apr 5, 2018 · N923FR · Airbus A319111 · Compressor Bleed Valve
  > DURING DESCENT AND RETARDING OF THROTTLES ENG-2 COMPRESSOR AND VANE ECAM APPEARED FOLLOWED BY COMPRESSOR STALL WHICH WAS FELT AND HEARD BY CREW. REMOVED AND REPLACED VARIABLE BLEED VALVE FUEL GEAR MOTOR. REFERENCE AMM 75-31-20-400-002A. OPERATIONAL AND LEAK CH
- [SDR F3LA2016062100051](https://openairdocs.org/sdr/F3LA2016062100051.md): Engine · shutdown · Jun 19, 2016 · N935FR · Airbus A319111 · Engine (Turbine/Turboprop)
  > DURING CRUISE FLIGHT THE CREW NOTED, ECAM ENGINE 2 STALL WHICH WAS SOON FOLLOWED BY ENGINE 2 SHUTDOWN. THE CREW DECLARED EMERGENCY LANDING. MAINTENANCE R & R NR 2 ENGINE. REF WC MP71042-01 AND MP71042-02, REMOVAL AND INSTALLATION CARDS. OPS CHECK GOOD.
- [SDR WX0A2016042973141](https://openairdocs.org/sdr/WX0A2016042973141.md): Acoustic Panel · cracked · Apr 27, 2016 · N327NV · Airbus A319111 · Turbine Engine Air Inlet Section
  > DURING DAILY CHECK WALK AROUND, DISCOVERED CRACKED ACOUSTIC PANEL AT 12 - 2 O'CLOCK POSITION ON NR 2 ENG. R & R ACOUSTIC PANEL AT 12 - 2 O'CLOCK POSITION IAW AMM 72-23-00. ALL IS GOOD.
- [SDR F3LA2016032600014](https://openairdocs.org/sdr/F3LA2016032600014.md): Engine · leaking · Mar 24, 2016 · N922FR · Airbus A319111 · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF THE FLIGHT CREW RECEIVED A CARGO & LAVATORY SMOKE MSG. THE ACFT RETURNED TO THE FIELD & MX DISCOVERED OIL WETTING IN THE NR 2 ENG COMPRESSOR. MX REMOVED ENG SN 575632 & INSTALLED SERVICEABLE ENG 575640 IAW MPD TASK CARDS MP 71042-01, MP 71042-0
- [SDR F3LA2015051101132](https://openairdocs.org/sdr/F3LA2015051101132.md): Fuel Line · leaking · May 11, 2015 · N905FR · Airbus A319111 · Engine Fuel Distribution
  > NUMBER 2 ENG FUEL LEAK FROM MAIN FUEL SUPPLY LINE. R & R MAIN FUEL SUPPLY LINE IAW AMM 73-11-11 PAGE BLOCK 401. LEAK CHECKED GOOD. TORQUE WRENCH F9TAB3949C CALIBRATION DATE 10 15, LOG PAGE 896973.
- [SDR F3LA2015041501130](https://openairdocs.org/sdr/F3LA2015041501130.md): Duct · failed · Apr 12, 2015 · N920FR · Airbus A319111 · Pneumatic Distribution System
  > DISCREPANCY, ENG 2 FIRE, AIR TURN BACK 1839 Z. ENG 2 FIRE INDICATION ON TAKEOFF AFTER THRUST REDUCTION ON ENG 2 IAW ECAM. FIRE INDICATION CHANGED TO AMBER, ENG 2 SHUTDOWN. ENG 2 SHUTDOWN COMPLETED. FOUND HIGH PRESS BLEED DUCT BROKEN CAUSING ENG 2 FIRE INDI
- [SDR F3LA2014112401088](https://openairdocs.org/sdr/F3LA2014112401088.md): Engine · malfunctioned · Nov 22, 2014 · N925FR · Airbus A319111 · Engine (Turbine/Turboprop)
  > AIRCRAFT DEPARTED & ENG 1 LOST OIL PRESS, OIL QTY WAS AT 0. CREW PERFORMED IN FLIGHT SHUTDOWN. EMER WAS DECLARED. ACFT ARRIVED WITHOUT FURTHER INCIDENT. ACFT ARRIVED WITH OIL TANK EMPTY. OIL WAS FOUND IN HOT STREAM OF EXHAUST PIPE, NO EVIDENCE OF OIL IN C
- [SDR F3LA2014070101047](https://openairdocs.org/sdr/F3LA2014070101047.md): Skin · debonded · Jun 20, 2014 · N918FR · Airbus A319111 · Elevator, Plate/Skin
  > LT ELEVATOR THERMO GRAPHIC INSPECTION REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED LT ELEVATOR UPPER SURFACE OF LIQUID INGRESS IAW SRM 55-20-00 PB201, SRM 55-21-11 PB201 & CMM 55-21-15-210-010-601. ACFT SCHEDULED BACK IN
- [SDR F3LA2014052701040](https://openairdocs.org/sdr/F3LA2014052701040.md): Idg · failed · May 22, 2014 · N921FR · Airbus A319111 · AC Generator-Alternator
  > NUMBER 1 ENG GEN FAILED IN FLIGHT, UNABLE TO RESET. NR 2 ENG GEN FAILED IN FLIGHT, UNABLE TO RESET. REPLACED NR 1 ENG IDG IAW AMM 24-21-51 PB 401. OPERATIONS & LEAK CHECKED GOOD. R & R NR 2 ENG IDG IAW AMM 24-21-57 PB 401.
- [SDR F3LA2013012400824](https://openairdocs.org/sdr/F3LA2013012400824.md): Line · failed · Jan 18, 2013 · N945FR · Airbus A319112 · Hydraulic System, Main
  > DURING CRUISE FLIGHT LOST GREEN SYSTEMS HYD; GREEN SYS HYD INOPERATIVE. FOUND BROKEN HYD LINE AT RT MLG DOOR ACTUATOR. R & R AFT HYD LINE ON RT MLG DOOR ACTUATOR. SERVICED GREEN HYD SYSTEM. LEAK AND OPS CHECKS NORMAL. REF 32-31-35 PB 401.
- [SDR F3LA2013010300823](https://openairdocs.org/sdr/F3LA2013010300823.md): Acm · malfunctioned · Dec 28, 2012 · N927FR · Airbus A319111 · Cabin Cooling System
  > AFTER LANDING, CABIN FILLED WITH SMOKE, DUCT TEMPS INCREASED TO OVER 110 DEGREES. MX DETERMINED THE NR 1 PACK TO BE OVERHEATING. RAN NR 1 PACK FOR 45 MINTUES. OPS CHECKED GOOD REF AMM 21-61-00-710-001A.
- [SDR F3LA2012091700790](https://openairdocs.org/sdr/F3LA2012091700790.md): Light · burned out · Sep 17, 2012 · N949FR · Airbus A319112 · Escape Slide
  > C-CHECK: R2 DOOR "SLIDE ARMED" LIGHT DOES NOT ILLUMINATED DURING TEST. REMOVED SLIDE ARMED INDICATOR LIGHT ASSY IAW AMM 52-76-000-002-A. INSTALLED SERVICEABLE SLIDE ARMED LIGHT ASSY IAW AMM 52-73-21-400-002A. OPS CHECK GOOD IAW AMM 52-73-00-710-001-A.
- [SDR F3LA2012091700792](https://openairdocs.org/sdr/F3LA2012091700792.md): Sill · corroded · Sep 17, 2012 · N949FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: R2 DOOR SILL BEAM CORRODED AROUND FASTENER HOLE AT FRAME 66. REPAIRED DOOR SILL BEAM WITH CUTOUT, FILLER AND SPLICE IAW SRM 53-41-14 PB201, PARA 5.A, FIG 201.
- [SDR F3LA2012091700793](https://openairdocs.org/sdr/F3LA2012091700793.md): Lamp · burned out · Sep 17, 2012 · N949FR · Airbus A319112 · Emergency Lighting
  > C-CHECK: MAIN CABIN LT SEATS, ROW 13 HAS BURNED OUT LAMP FOR EMERGENCY EXIT LIGHT. R & R LAMP IAW AMM 33-51-19-420-052D. OPS CHECKED GOOD LAW AMM 33-51-00-71 0-00L-A.
- [SDR F3LA2012083100782](https://openairdocs.org/sdr/F3LA2012083100782.md): Actuator · intermittent · Aug 28, 2012 · N912FR · Airbus A319111 · Landing Gear Actuator
  > ACFT LEFT C-CHECK AFTER COMPLETE SET LANDING GEAR TIME, DEPARTED. NLG DID NOT LOCK UP, GEAR DOORS DID NOT CLOSE. ACFT WAS PREPPED FOR GEAR DOWN FERRY FLIGHT. FERRY FLIGHT DID NOT OCCUR. DISCREPANCY WAS WORKED AT AIRPORT, ADJUSTMENTS MADE, REF NR 43936. OCF U
- [SDR F3LA2012083100780](https://openairdocs.org/sdr/F3LA2012083100780.md): Skin · dented · Aug 27, 2012 · N940FR · Airbus A319111 · Nacelle/Pylon, Plate/Skin
  > NR 1 ENGINE NOSE COWL INNER BARREL AT 9:00 POSITION HAS A DENT, REPAIRED IAW SRM 54-10-00, REPAIR 23, PARAGRAPH 2.A,B,C(1 -3), D, E(1 -2), F( 1-2), G AND H( 1-4).
- [SDR F3LA2012081500777](https://openairdocs.org/sdr/F3LA2012081500777.md): Ballast · failed · Aug 13, 2012 · N921FR · Airbus A319111 · Passenger Compartment Lighting
  > ODOR COMING FROM AFT CABIN. R & R BALLAST ASSY COVE LIGHT AT ROW 24 DEF. OPS CHECK GOOD, NO TROUBLE NOTED REF AMM 33-21-11, PAGE BLOCK 401.
- [SDR F3LA2012003200728](https://openairdocs.org/sdr/F3LA2012003200728.md): Blade · lack of lube · Mar 20, 2012 · N904FR · Airbus A319111 · Turbine Engine Compressor Section
  > NR 1 ENGINE VIBRATION IN CLIMB OVER 4.0. VIBRATION WOULD FOLLOW THRUST. AIR TURN BACK. PERFORMED TSM TASKS 77-00-00-81 0-863-A AND 77-00-00-81 O-B64-A INCLUDING FAN BLADE LUBE REF AMM 72-21-00-210-004 AND COLD TRIM BALANCE REF AMM 71-00-00-750-001. MAXIMUM
- [SDR F3LA2011052300652](https://openairdocs.org/sdr/F3LA2011052300652.md): Pump · leaking · May 19, 2011 · N942FR · Airbus A319111 · Hydraulic Pump (Electric/Engine), Main
  > PILOT REPORT YELLOW HYDRAULIC LOW RESERVOIR LEVEL. REMOVED AND REPLACED ENGINED NR2 HYDRAULIC PUMP DRIVER IAW AMM 29-13-51, PB 401, OPS CHECKS GOOD. FOUND SEVERAL LEAK YELLOW SYSTEM LINE TO PRESSURE SWITCH. REMOVED AND REPLACED LINE IAW AMM 28-23-11 LEAKED CH
- [SDR F3LA2011022100606](https://openairdocs.org/sdr/F3LA2011022100606.md): Stop · seized · Feb 17, 2011 · N904FR · Airbus A319111 · Turbine Engine Compressor Section
  > ACFT LOG PAGE 590497: AIR TURN BACK AT 01302. ECAM WARNING NR 2 ENGINE COMPRESSOR VANE (AIR RETURN. REPLACED NR 2 ENGINE MASTER BALLSCREW ACTUATOR STOP. REF AMM 75-31-50 PB 401, OPS CHECK NORMAL.
- [SDR F3LA2010122900571](https://openairdocs.org/sdr/F3LA2010122900571.md): Smoke Detector · faulty · Dec 28, 2010 · N918FR · Airbus A319111 · Smoke Detection
  > PILOT REPORT: LP 594710; AFT CARGO / LAV SMOKE DETECT FAULT. R & R THE AFT CARGO SMOKE DETECT UNIT (3WH) AND AFT LAV (E) DETECT UNIT. IAW AMM 26-46-15, PB 401. OPS TEST OK.
- [SDR F3LA2010122000563](https://openairdocs.org/sdr/F3LA2010122000563.md): Floor Panel · chafed · Dec 17, 2010 · N945FR · Airbus A319112 · Fuselage Floor Panel
  > C-CHECK: NON ROUTINE N0399; AFT CARGO PANEL 151VG AFT EDGE IS WORN THROUGH TOP PLY. AREA IS 10 SQ INCHES. DAMAGE IS OUT OF LIMITS. FABRICATED REPLACEMENT PANEL 151VG IAW MCG IRM 9701 REV G.
- [SDR F3LA2010122000565](https://openairdocs.org/sdr/F3LA2010122000565.md): Floorbeam · corroded · Dec 17, 2010 · N945FR · Airbus A319112 · Fuselage Main, Floor Beam
  > C-CHECK: NON ROUTINE N0436; LT FLOORBEAM, Y1292 AT FRAME 68L HAS A 2 SQ. INCHES OF CORROSION ON THE UPPER AND LOWER SIDERS. CORROSION IS OUT OF LIMITS. REPLACED FLOORBEAM, Y1292 BETWEEN FRAMES 68LT AND 69LT IAW SRM 51-72-11, PARA 6.
- [SDR F3LA2010122000567](https://openairdocs.org/sdr/F3LA2010122000567.md): Splice · corroded · Dec 17, 2010 · N945FR · Airbus A319112 · Fuselage Main, Floor Beam
  > C-CHECK: NON ROUTINE N0438; LT FLOORBEAM, Y1292 SPLICE COUPLING AT FRAME 66L HAS 2 INCHES OF CORROSION. CORROSION IS OUT OF LIMITS. REPLACED SPLICE COUPLING AT FRAME 66L IAW SRM 53-72-11, PARA 6.
- [SDR F3LA2010122000570](https://openairdocs.org/sdr/F3LA2010122000570.md): Plate · corroded · Dec 17, 2010 · N945FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE N0596; FR69-70 SHEAR WEB PLATE HAS CORROSION AROUND FASTNER HOLES AND IS OLD CONFIGURATION. FOUND TO BE OUT OF LIMITS. REPLACED SHEAR WEB PLATE WITH NEW CONFIGURATION IAW EO AO-53EO-31434.
- [SDR F3LA2010113000553](https://openairdocs.org/sdr/F3LA2010113000553.md): Skin · cracked · Nov 22, 2010 · N922FR · Airbus A319111 · Nacelle/Pylon, Plate/Skin
  > C-CHECK: NON ROUTINE N0178; NR2 ENGINE PYLON UPPER PANEL NR423DL HAS A 1 EACH CRACK ON THE INTERIOR SIDE AT THE CUT OUT ABOUT.25" IN LENGHT. IAW SRM 54-52-11, STOP DRILL CRACK ENDS AND WELDED IAW PMS 01-04-21.
- [SDR F3LA2010113000554](https://openairdocs.org/sdr/F3LA2010113000554.md): Skin · cracked · Nov 22, 2010 · N922FR · Airbus A319111 · Nacelle/Pylon, Plate/Skin
  > C-CHECK: NON ROUTINE N0179; RT PYLON UPPER PANEL NR 423DL HAS A 4.0" CRACK AROUND LOUVERS AND ABOUT 1.0" IN LENGHT. IAW SRM 54-52-11 AND PMS 01-04-21, STOP DRILLED CRACK AND WELDED.
- [SDR F3LA2010113000555](https://openairdocs.org/sdr/F3LA2010113000555.md): Access Panel · cracked · Nov 22, 2010 · N922FR · Airbus A319111 · Nacelle/Pylon, Plate/Skin
  > C-CHECK: NON ROUTINE N0565; LT PYLON ACCESS PANEL NR413DL CRACKED. IAW SRM 54-50-80 AND PMS 01-04-21, STOP DRILLED CRACK ENDS AND WELDED.
- [SDR F3LA2010120200556](https://openairdocs.org/sdr/F3LA2010120200556.md): Transition Panel · delaminated · Nov 22, 2010 · N922FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE N0467; AFT CARGO COMPARTMENT LT TRANSITION PANEL NR 151DE HAS A 1.0" PUNTURE AND 3.0" SQUARE OF DELAMINATION. FABRICATED REPLEACEMENT PANEL IAW MCG IRM 9701, REV G.
- [SDR F3LA2010111400549](https://openairdocs.org/sdr/F3LA2010111400549.md): Actuator · out of rig · Nov 12, 2010 · N927FR · Airbus A319111 · Rudder Tab Control System
  > ACFT FLEW AT 5 TO 10 DEGREE LT WING DOWN ON AP, FL CTL SHOWED LT AILERON UP. FUEL BALANCE OK. ACFT WANTED TO FLY IN LT SLIP. FOUND RUDDER TRIM TO BE OUT RIG. REMOVED RUDDER TRIM ACTUATOR, PERFORM ZEROING PROCEDURE ON ACTUATOR. ADJUST ARTIFICIAL FEEL SPRING
- [SDR F3LA2010103000533](https://openairdocs.org/sdr/F3LA2010103000533.md): Floor Panel · delaminated · Oct 26, 2010 · N921FR · Airbus A319111 · Fuselage Floor Panel
  > C-CHECK: NON ROUTINE N0573: AFT CARGO FLOOR PANEL 162EF HAS TOP SKIN DISBONDED FWD INBD CORNER. FABRICATED AND REPLACEMENT PANEL 162 EF IAW MCG IRM 9701 REV G.
- [SDR 2010FA0001072](https://openairdocs.org/sdr/2010FA0001072.md): Spool · unserviceable · Sep 20, 2010 · Airbus A319111 · Turbine Engine Compressor Section
  > INCOMING FLUORESCENT PENETRANT INSP OF HPC 1-2 SPOOL REVEALED CRACK INDICATIONS IN 2 OF DOVE TAIL POSTS ALONG THE EDGE OF BEDDING MARK. ON 1 OF POST, THE CRACKING EXTENDS ACROSS BOTH THE FWD AND AFT FACES. CRACKING MEASURED AT 1.5 INCHES AND 0.375 INCHES. T
- [SDR F3LA2010090100501](https://openairdocs.org/sdr/F3LA2010090100501.md): Power Supply · inoperative · Sep 17, 2010 · N922FR · Airbus A319111 · Emergency Lighting
  > WHILE TROUBLESHOOTING EPSU REF. SWAPPED LT FWD EPSU INTO MID POSITION RESULTING IN ITS FAILURE. R & R LT FWD EPSU 10WL, OPS CHECKS NORMAL IAW AMM 33-51-38, PB 401.
- [SDR F3LA2010090100497](https://openairdocs.org/sdr/F3LA2010090100497.md): Power Supply · inoperative · Sep 13, 2010 · N922FR · Airbus A319111 · Emergency Lighting
  > LT SIDE AFT FACING EXIT ROW SIDE AND EXIT SIGN INOPERATIVE. R & R LT OVERWING EPSU. IAW AMM 33-51-38, PB 401.
- [SDR F3LA2010090100493](https://openairdocs.org/sdr/F3LA2010090100493.md): Seat Track · corroded · Sep 3, 2010 · N934FR · Airbus A319111 · Fuselage, Seat/Cargo Attach Fittings
  > C-CHECK, NON ROUTINE N0567, AFT MAIN CABIN RT SEAT TRACK YR2 DOOR SILL TRAY AT FRAME 66-Y122 AT FRAME 68 HAS 2 AREAS OF CORROSION ON UPPER SURFACE. REMOVED CORROSION IAW SRN 51-74-00. BLEND OUT MEASURES 2.5 INCH X 1.5 INCH X.012 INCH AND 3 INCH X 1.5 INCH X.
- [SDR F3LA2010090100495](https://openairdocs.org/sdr/F3LA2010090100495.md): Sill · corroded · Sep 3, 2010 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE N0590, R2 DOOR SILL TRAY AT FRAME 66 HAS 1 AREA OF CORROSION AROUND NUT PLATE HOLE. REMOVED CORROSION IAW SRM 51-74-00. OPENED HOLE TO.310, BLEND OUT MEASURES 1 INCH X 1.5 INCH X.020 WITHIN LIMITS IAW 53-00-14 FIG 102. REPROTECTED IAW SR
- [SDR F3LA2010090100496](https://openairdocs.org/sdr/F3LA2010090100496.md): Roll Pin · broken · Sep 3, 2010 · N934FR · Airbus A319111 · Escape Slide
  > C-CHECK: NON ROUTINE N0785. LT EMERGENCY EXIT SLIDE ARMING MECHANISM WILL NOT STAY IN ARMED POSITION. R & R SLIDE RELEASE MECHANISM SPRING PIN IAW AMM 52-21-11-000-003 AND AMM 52-11-420-051. PERFORMED SLIDE MECHANISM OPS CHECK IAW AMM 52-21-00-720-001. NO DEFE
- [SDR F3LA2010080800480](https://openairdocs.org/sdr/F3LA2010080800480.md): Plate · corroded · Aug 8, 2010 · N933FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REF NON-ROUTINECARD N0392, AFT CABIN RT SHEAR PLATE BETWEEN FRAMES 69 AND 70, HAS CORROSION THAT IS OUT OF LIMITS. R & R SHEAR PLATE AT AFT CABIN RT SIDE BETWEEN FRAMES 69 AND 70 IAW SRM 51-42-11 AND EO AO-53E0-31434.
- [SDR F3LA2010080800482](https://openairdocs.org/sdr/F3LA2010080800482.md): Floor Panel · damaged · Aug 8, 2010 · N933FR · Airbus A319111 · Fuselage Floor Panel
  > REF NON=ROUTINE N0691, FWD CARGO FLOOR PANEL 131AF BROKEN COTR APPROX 2.0 IN X 2.5 IN. ACFT IS IN C-CHECK. REPAIR DAMAGE AREA ON PANEL 131AF USING RESIN AND GLASS CLOTH PATCH METHOD IAW SRM 53-02-00, PARA 8B.
- [SDR F3LA2010080800483](https://openairdocs.org/sdr/F3LA2010080800483.md): Sill · corroded · Aug 8, 2010 · N933FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR STRUCTURE LONGERON AT OTBD POSITION FRAME 66 HAS A 1 SQ IN ARE OF CORROSION REF NON-ROUTINE N0451. CUT OUT CORROSION AT NUTPLATE HOLE IAW SRM 53-42-14 PRINCIPLE 6 FABRICATED REPAIR ANGLES IAW SRM 53-42-14 PRINCIPLE 6 TREATED PRIMED AND TOP COO
- [SDR F3LA2010080200477](https://openairdocs.org/sdr/F3LA2010080200477.md): Engine · overserviced · Jul 31, 2010 · N905FR · Airbus A319111 · Turbine Engine Oil System
  > AIR TURN BACK DUE TO OIL TEMP TRENDING TOWARD EXCEEDANCE. REACHED 135 DEGREES CELCIUS MAXIMUM. PRECAUTIONARY RETURN BASED. ALSO ON ENGINE START, OIL PRESSURE REMAINED IN RED ARC UNTIL ABOUT 52.5 PERCENT N1. OIL QUANTITY INDICATED 20.5 QUARTS. FOUND NR 2 ENGINE
- [SDR F3LA2010080200476](https://openairdocs.org/sdr/F3LA2010080200476.md): Valve · failed · Jul 30, 2010 · N905FR · Airbus A319111 · Engine Fuel Distribution
  > ON CLIMBOUT NR 2 ENGINE OIL OVERTEMP. SHUTDOWN ENGINE NR 2 IAW ECAM. MAXIMUM NOTED OIL TEMP 160 DEGREES CELCIUS. MAXIMUM NOTED OIL PRESSURE WAS ABOUT 36 PSI, 10 PSI LOWER THAN ENGINE NR 1. R & R FUEL RETURN VALVE ASSY FOR NR 2 ENGINE. REF AMM 73-11-50 PAGE BLO
- [SDR F3LA2010080300479](https://openairdocs.org/sdr/F3LA2010080300479.md): Floor Support · corroded · Jul 26, 2010 · N933FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REF HEAVY MX NON ROUTINE N0561. RT CABIN FLOOR AT FRAME 69 TO FRAME 70 SUPPORT EXTRUSION BELOW SHEAR PLATE IS CORRODED. R & R SUPPORT IAW SRM 51-72-11.
- [SDR F3LA2010060400435](https://openairdocs.org/sdr/F3LA2010060400435.md): Computer · malfunctioned · Jun 3, 2010 · N928FR · Airbus A319111 · Smoke Detection
  > PILOT REPORT REF LOG PAGE 524666 ITEMS 1 AND 2. SMOKE WARNING ACTUATED UPON LANDING. NO SMOKE NOTICED IN COCKPIT. BOTH BLOWER AND EXTRACT FAULTED AT SAME TIME ON THE VENTILLATION SYS. R & R AEVC COMPUTER.
- [SDR F3LA2010052200422](https://openairdocs.org/sdr/F3LA2010052200422.md): Sign · inoperative · May 19, 2010 · N931FR · Airbus A319111 · Emergency Lighting
  > REF HEAVY MX NON ROUTINE N0773. RT FWD LOWER EMERGENCY EXIT IDENTIFIER DOES NOT ILLUMINATE. R & R IDENTIFIER IAW AMM 33-51-13-000-001.

Next page: https://openairdocs.org/engine/cfm-international-cfm56-5b5-p-series/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 = 'CFM565B5P'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/cfm-international-cfm56-5b5-p-series/reports

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