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

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

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 246 reports

- [SDR 2026FA0000429](https://openairdocs.org/sdr/2026FA0000429.md): Turbine · defective · May 26, 2026 · Turbine Section
  > THE ENGINE ABY ESN 577716 WAS SLOTTED IN SAESM THE 17 APRIL 2026. DURING THE MM03 LEVEL INSPECTION OF THE LPT CASE, A DEFECT WAS IDENTIFIED ON 28TH MAY 2026. FOLLOWING THIS FINDING, A CSC CASE WAS RAISED TO CFM (TCH) REQUESTING AN APPROPRIATE REPAIR DISPOSITIO
- [SDR WX0A2024080532144](https://openairdocs.org/sdr/WX0A2024080532144.md): Engine · overtemp · Aug 3, 2024 · N329NV · Airbus A319111 · Engine (Turbine/Turboprop)
  > (AIRCRAFT NOT GROUNDED) ON CLIMB OUT ENG 2 HIGH OIL TEMP ADV. RAN QRH ECAM ADV LED TO ECAM ENG 2 OIL TEMP HIGH ENG 2 SHUTDOWN / REMOVED AND REPLACED #2 ENG IDG IAW AMM 24-21-51-000-040-B/24-21-51-400-040-E. LEAKS AND OPS CHECK GOOD AT THIS TIME."
- [SDR WX0A2021071473765](https://openairdocs.org/sdr/WX0A2021071473765.md): Engine · power loss · Jul 12, 2021 · N313NV · Airbus A319111 · Engine (Turbine/Turboprop)
  > (EMERGENCY DECLARED) #2 ENGINE ROLLED BACK DURING DECENT. ENGINE #2 WINDMILLED FOR ABOUT:17 MIN / AIRCRAFT IS CURRENTLY AOS AT TOL. TROUBLESHOOTING IN PROGRESS."
- [SDR QEMY29012021](https://openairdocs.org/sdr/QEMY29012021.md): Frame · damaged · Jan 22, 2021 · N466L · Turbine Section
  > ON INCOMING INSPECTION AT GE AVIATION WALES EASYJET ESN 699785, THE LPT FRAME WAS FOUND DAMAGED. THE LPT FRAME HAS BEEN REMOVED FROM SERVICE. DAMAGE CONSISTENT WITH ENGINE REMOVAL DAMAGE. OPERATOR INFORMED AND TO COMPLETE INVESTIGATION.
- [SDR WX0A2019062173399](https://openairdocs.org/sdr/WX0A2019062173399.md): Gasket · failed · Jun 21, 2019 · N333NV · Airbus A319111 · Fuel Injector Nozzle
  > EMERGENCY DECLARED, NR 1 ENGINE FAILED. R & R FUEL NOZZLE FILTER GASKET.
- [SDR A8ZR20170414001](https://openairdocs.org/sdr/A8ZR20170414001.md): Bearing · migrated · Apr 4, 2017 · N330NV · Airbus A319111 · Rudder Control System
  > DURING PRE-FLIGHT CHECK, THE RUDDER TRAVEL DID NOT TOUCH FULL CONTROL BOX ON LOWER ECAM PAGE AND THE LAST 1/10 OF PEDAL TRAVEL WAS HARD. TROUBLESHOOTING AND INSPECTION FOUND THE LOWER RUDDER BELLCRANK BEARING MIGRATED FROM THE LEFT HAND LUG.
- [SDR AALA201701229008](https://openairdocs.org/sdr/AALA201701229008.md): Engine · stalled · Jan 21, 2017 · N770UW · Airbus A319112 · Engine (Turbine/Turboprop)
  > AIRCRAFT WAS GROUNDED. NEAR TOP OF DESCENT, MOMENTARY ONE TIME NR 1 ENGINE STALL, CORRECTED BEFORE ENGINE INDICATIONS CHANGED, ECAM CAME ON VERY BRIEFLY. MAINTENANCE REPLACED ENGINE PER TASK CARD 26L40071001.
- [SDR WX0A2016042973145](https://openairdocs.org/sdr/WX0A2016042973145.md): Engine · failed · Apr 28, 2016 · N311NV · Airbus A319111 · Engine (Turbine/Turboprop)
  > NUMBER 2 ENG FAILED DURING GO AROUND. DISCHARGED NR 1 FIRE BOTTLE. R&R NR 2 ENGINE PER T/C 71-400-001. ALL OPS AND LEAK CHECKS GOOD.
- [SDR F3LA2014081201050](https://openairdocs.org/sdr/F3LA2014081201050.md): Valve · closed · Aug 8, 2014 · N928FR · Airbus A319111 · Pneumatic Distribution System
  > IN CRUISE AT 31000 FT UNABLE TO MAINTAIN CABIN PRESS. CABIN ALTITUDE ROSE TO 10,200. R & R NR 2 ENG PRV IAW AMM 36-11-52-PB 401. OPERATIONS & LEAK CHECKED VLV & NO LEAKS NOTED. PREFORMED OPERATIONAL TEST OF THE BLEED AIR SYS IAW AMM 36-11-00-710-003-A. O
- [SDR CA111103009](https://openairdocs.org/sdr/CA111103009.md): Brake · failed · Oct 29, 2011 · Airbus A319114 · Leading Edge Slat Position Indicating System
  > (CAN) ON APPROACH, FLIGHT CREW REPORTED A FLIGHT CONTROL PROBLEM WHICH REQUIRED A GO-AROUND. AS A PRECAUTION, THE CREW DECLARED AN EMERGENCY WITH ATC (PAN-PAN) AND LANDED SAFELY. ON FLAP EXTENSION TO FLAPS 1 DURING APPROACH S-LOCKED. UNABLE TO CLEAR BY REC
- [SDR F3LA200800505](https://openairdocs.org/sdr/F3LA200800505.md): Sign · broken · Jul 20, 2008 · N918FR · Airbus A319111 · Emergency Lighting
  > DURING C-CHECK, INSP NOTED R1 DOOR FWD LOWER EXIT LIGHT IS BROKEN. MAINT REMOVED AND REPLACED R1 DOOR FWD LOWER EXIT LIGHT IAW AMM 33-51-13-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800501](https://openairdocs.org/sdr/F3LA200800501.md): Sill · damaged · Jul 19, 2008 · N918FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, INSP NOTED THE R2 DOOR SILL PLATE REQUIRED REPLACEMENT DUE TO MISDRILLED HOLE. MAINT REMOVED AND REPLACED R2 DOOR SILL PLATE IAW A319 SRM 51-42-11 AND 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800500](https://openairdocs.org/sdr/F3LA200800500.md): Shear Plate · corroded · Jul 19, 2008 · N918FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, INSP NOTED THE RT LATERAL SHEAR PLATE AT Y-1162, FROM FRAME 69 TO FRAME 70, HAD CORROSION AND FOUR SHEARED FASTENERS AT THE FWD EDGE. MAINT REMOVED AND REPLACED THE LATERAL SHEAR PLATE AT Y-1162 AT FRAME 69 TO FRAME 70 IAW SRM 51-42-11. UPON
- [SDR F3LA200800499](https://openairdocs.org/sdr/F3LA200800499.md): Floor Panel · broken · Jul 18, 2008 · N918FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C4 S1 C CHECK, INSPECTION NOTED THE AFT CARGO FLOORBOARD, 151CE, HAD TWO BROKEN CORNERS. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 151CE. INSTALLATION WAS COMPLETED ON EMPIRE AERO CENTER NON ROUTINE NR 9642. UPON COMPLETION OF THE REPAIR IT WAS IN
- [SDR F3LA200800490](https://openairdocs.org/sdr/F3LA200800490.md): Skin · dented · Jul 16, 2008 · N918FR · Airbus A319111 · Nacelle/Pylon, Plate/Skin
  > DURING C-CHECK INSP NOTED THAT THE DAMAGE ON NR 1 ENGINE INLET COWL REQUIRES PERMANENT REPAIR OF DENT AT THE 2 O`CLOCK POSITION. MAINT REPAIRED DAMAGED AREA IAW CMM 54-10-00, REPAIR PROCEDURE NR 23. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCE
- [SDR F3LA200800489](https://openairdocs.org/sdr/F3LA200800489.md): Fitting · corroded · Jul 16, 2008 · N918FR · Airbus A319111 · Emergency Equipment
  > DURING C-CHECK INSP NOTED THE R1 DOOR GIRT BAR FITTING IB MOUNT HOLES ON SILL PLATE HAD CORROSION. MAINT BLENDED CORROSION IAW SRM 51-74-00. MAINT REPAIRED AREAS THAT WERE DEEPER THAT.016" WITH A FILLER AND FILLED AREAS THAT WERE LESS THAN.016" WITH ADHESIVE
- [SDR F3LA200800486](https://openairdocs.org/sdr/F3LA200800486.md): Profile · corroded · Jul 16, 2008 · N918FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT RT SIDE PROFILE HAD CORROSION AT FRAME 59 ON RT SIDE IAW A319 SRM 51-72-11 AND 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800491](https://openairdocs.org/sdr/F3LA200800491.md): Fitting · cracked · Jul 15, 2008 · N918FR · Airbus A319111 · Engine Mount Section
  > DURING C-CHECK INSP NOTED THE NR 1 ENGINE PYLON PANEL NR 413CL MOUNTS STRUCTURE WAS CRACKED AT AFT UPPER SCREW HOLE. MAINT REPAIRED NR 1 ENGINE PYLON PANEL NR 413CL MOUNT STRUCTURE AT AFT UPPER HOLE IAW SRM 54-52-12 AND 51-42-11. UPON COMPLETION OF THE REPAIR
- [SDR F3LA200800488](https://openairdocs.org/sdr/F3LA200800488.md): Door Frame · corroded · Jul 15, 2008 · N918FR · Airbus A319111 · Fuselage Main, Structure
  > DURING C-CHECK INSP NOTED CORROSION ON TOP LEG OF FRAME C55A AT FWD EDGE OF C2 DOOR. MAINT REPAIRED DAMAGE ON TOP LEG OF FRAME C55A IAW EA NR A9-53R-30442. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800483](https://openairdocs.org/sdr/F3LA200800483.md): Profile · gouged · Jul 15, 2008 · N918FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT PROFILE AT FRAME C63 IS GOUGED AND HAS A RIVET PULLING THROUGH. MAINT REMOVED AND REPLACED PROFILE AT FRAME C63 IAW SRM 51-72-11, 51-21-11 AND 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUN
- [SDR F3LA200800484](https://openairdocs.org/sdr/F3LA200800484.md): Profile · corroded · Jul 15, 2008 · N918FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT PROFILE AT FRAME C59 HAD CORROSION AT BOTH ENDS OF THE PROFILE. MAINT REMOVED AND REPLACED THE PROFILE IAW SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800485](https://openairdocs.org/sdr/F3LA200800485.md): Profile · corroded · Jul 15, 2008 · N918FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT SMALL PROFILE RT SIDE JUST INSIDE DOOR FWD OF FRAME C56 HAS CORROSION. MAINT REMOVED SMALL PROFILE, FABRICATED NEW PROFILE, TREATED, PRIMED AND TOP COATED NEW PROFILE AND INSTALLED IAW SRM 51-21-11, 51-53-11,
- [SDR F3LA200800482](https://openairdocs.org/sdr/F3LA200800482.md): Battery Box · worn · Jul 15, 2008 · N918FR · Airbus A319111 · Battery Box Structure
  > DURING C-CHECK INSP, NOTED AFT BATTERY TRAY OB FWD AND AFT MOUNTS HAVE WEAR. MAINT REMOVED AND REPLACED AFT BATTERY TRAY, OB FWD AND AFT MOUNTS IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800469](https://openairdocs.org/sdr/F3LA200800469.md): Floorbeam · corroded · Jul 14, 2008 · N918FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT CENTER FLOORBEAM HAS CORROSION BETWEEN FRAME C57 AND FRAME C58. MAINT REMOVED AND REPLACED CORRODED FLOORBEAM AT FRAME C57 AND FRAME C58 IAW SRM 51-41-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND
- [SDR F3LA200800470](https://openairdocs.org/sdr/F3LA200800470.md): Profile · corroded · Jul 14, 2008 · N918FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED CORROSION SEVERAL PLACES ON AFT MOST PROFILE AT FWD CARGO COMPARTMENT AFT OF FRAME C30. MAINT REMOVED AND REPLACED PROFILE IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800465](https://openairdocs.org/sdr/F3LA200800465.md): Frame · corroded · Jul 14, 2008 · N918FR · Airbus A319111 · Fuselage Main, Frame
  > DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT INSIDE OF C2 DOOR SHORT ANGLE PIECE AT FRAME C59 HAS CORROSION. MAINT REMOVED SHORT ANGLE PIECE APPLIED PROTECTION TREATMENT FABRICATED NEW SHORT ANGLE TREATED, PRIMED AND PAINTED AND INSTALLED IAW SRM 51-72-11,
- [SDR F3LA200800449](https://openairdocs.org/sdr/F3LA200800449.md): Deu · inoperative · Jul 13, 2008 · N919FR · Airbus A319111 · Passenger Compartment Lighting
  > DURING FLIGHT MANY CABIN LIGHTS WERE COMING ON AND OFF ON AC RT. THE F/A NOTICED A BURNING SMELL OVER ROWS 16,17 AND 18 ON AC RT. MAINT FOUND DEU-A 200RH12 INOPERATIVE AND HAD A SMELL TO IT. MAINT REMOVED AND REPLACED DEU-A 200RH12 IAW AMM 23-73-46 AND OPS CHE
- [SDR F3LA200800480](https://openairdocs.org/sdr/F3LA200800480.md): Seat Track · corroded · Jul 11, 2008 · N918FR · Airbus A319111 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK INSP NOTED THE RT LONGERON BEAM Y-765 AT FRAME 66 HAD CORROSION AROUND THE HOLE. MAINT REMOVED AND REPLACED CORRODED LONGERON BEAM AT Y-765 FRAME 64 TO FRAME 66 IAW SRM 51-42-11 AND 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FO
- [SDR F3LA200800478](https://openairdocs.org/sdr/F3LA200800478.md): Profile · corroded · Jul 11, 2008 · N918FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP, NOTED CORROSION ON AFT CARGO COMPARTMENT LT PROFILE, FWD AREA OF AFT CARGO, AT FRAME C47 TO FRAME C51. MAINT REMOVED AND REPLACED PROFILE AT FRAME C47 TO FRAME C51 IAW SRM 51-72-11, 51-21-11 AND 51-42-11. UPON COMPLETION FO THE REPAIR IT W
- [SDR F3LA200800477](https://openairdocs.org/sdr/F3LA200800477.md): Fitting · corroded · Jul 11, 2008 · N918FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED CORROSION ON PLATE BELOW TIE-DOWN PLATE AT FRAME C29 FWD CARGO COMPARTMENT. MAINT REMOVED AND REPLACED FITTING, REINSTALLED PLATE AND TIE-DOWN AT FWD CARGO COMPARTMENT FRAME C29 IAW SRM 51-42-11 AND 51-72-11. UPON COMPLETION OF THE RE
- [SDR F3LA200800476](https://openairdocs.org/sdr/F3LA200800476.md): Profile · corroded · Jul 11, 2008 · N918FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED CORROSION ON PROFILE PARALLEL WITH FRAME C28 FWD CARGO COMPARTMENT. MAINT REMOVED AND REPLACED CORRODED PROFILE ON FRAME C28 IN FWD CARGO COMPARTMENT IAW FO A319 SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND A
- [SDR F3LA200800475](https://openairdocs.org/sdr/F3LA200800475.md): Girt Bar · sticking · Jul 11, 2008 · N918FR · Airbus A319111 · Emergency Equipment
  > DURING C-CHECK INSP NOTED R1 GIRT BAR FITTING FOR DOOR SLIDE STOP LEVER STICKS, DOES NOT SNAP BACK WHEN PRESSED DOWN AND RELEASED. MAINT REMOVED AND REPLACED WITH NEW GIRT BAR FITTING IAW AMM 52-11-31-000-003 AND 52-11-31-400-003. UPON COMPLETION OF THE REPAIR
- [SDR F3LA200800474](https://openairdocs.org/sdr/F3LA200800474.md): Cargo Track · corroded · Jul 11, 2008 · N918FR · Airbus A319111 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK INSP NOTED CORROSION ON PLATE BELOW TIE-DOWN PLATE UNDER FRAME C25 FWD CARGO PIT. MAINT REMOVED PLATE AND BLENDED CORROSION, MORE THAN 50 PERCENT MATERIAL LOSS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-14 OUT TO LIMITS OR ACTIONS NOT STATED.
- [SDR F3LA200800473](https://openairdocs.org/sdr/F3LA200800473.md): Longeron · corroded · Jul 11, 2008 · N918FR · Airbus A319111 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK INSP NOTED RT LONGERON BEAM AT Y-1162 FROM FRAME 68 TO FRAME 69 HAD AREAS OF CORROSION. MAINT REMOVED AND REPLACED FLOORBEAM LONGERON Y-1162 FROM FRAME 68 TO FRAME 69 IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACC
- [SDR F3LA200800472](https://openairdocs.org/sdr/F3LA200800472.md): Floor Support · corroded · Jul 11, 2008 · N918FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED RT LONGERON BEAM AT Y-1292 FROM FRAME 66 TO FRAME 68 HAD AREAS OF CORROSION. MAINT REMOVED AND REPLACED FLOOR SUPPORT LONGERON Y-1292 FROM FRAME 66 TO FRAME 69 IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND
- [SDR F3LA200800471](https://openairdocs.org/sdr/F3LA200800471.md): Profile · corroded · Jul 11, 2008 · N918FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED CORROSION SEVERAL PLACES ON PROFILE LT SIDE AFT OF FRAME C28 FWD CARGO COMPARTMENT. MAINT REMOVED OLD PROFILE AT FRAME C28 ON LT SIDE, LOCATED AND DRILLED HOLES ON NEW PROFILE AND INSTALLED NEW PROFILE IAW SRM 51-72-11 AND SRM 51-42-1
- [SDR F3LA200800487](https://openairdocs.org/sdr/F3LA200800487.md): Skin · chafed · Jul 11, 2008 · N918FR · Airbus A319111 · Ailerons
  > DURING C-CHECK INSP NOTED THE RT AILERON APPEARS TO BE CHAFING AT IB LOWER EDGE. MAINT CLEANED AREA OF DAMAGE AND REPAIRED IAW SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800481](https://openairdocs.org/sdr/F3LA200800481.md): Floor Panel · damaged · Jul 11, 2008 · N918FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP, NOTED FLOOR PANEL 261PF HAD COMPOSITE DAMAGE. MAINT REMOVED AND REPLACED FLOOR PANEL 261PF WITH NEW PANEL, REFERENCED ON EAC NON ROUTINE ITEM 9651. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800464](https://openairdocs.org/sdr/F3LA200800464.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED FWD PIT PANEL 131EG DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800451](https://openairdocs.org/sdr/F3LA200800451.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP, NOTED AFT PIT PANEL 161CF DAMAGED. MAINT REMOVED DAMAGE AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800452](https://openairdocs.org/sdr/F3LA200800452.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP, NOTED AFT PIT PANEL 162EF DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800453](https://openairdocs.org/sdr/F3LA200800453.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP AFT PIT PANEL 161BF DAMAGED. MIANT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800454](https://openairdocs.org/sdr/F3LA200800454.md): Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP, NOTED AFT PIT PANEL 161NF DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800455](https://openairdocs.org/sdr/F3LA200800455.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED AFT PIT PANEL 151PE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800456](https://openairdocs.org/sdr/F3LA200800456.md): Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED AFT PIT PANEL 151DE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800457](https://openairdocs.org/sdr/F3LA200800457.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED AFT PIT PANEL 151FE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800458](https://openairdocs.org/sdr/F3LA200800458.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED AFT PIT PANEL 152WG DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800459](https://openairdocs.org/sdr/F3LA200800459.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED AFT PIT PANEL 152UG DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800460](https://openairdocs.org/sdr/F3LA200800460.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED AFT PIT FLOOR PANEL 151CE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800461](https://openairdocs.org/sdr/F3LA200800461.md): Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151GE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Next page: https://openairdocs.org/engine/cfm-international-cfm56-5b5-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 = 'CFM565B5'
ORDER BY difficulty_date DESC
```

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

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