# Service difficulty reports: GE CF6-80C2A5F

A list on [GE CF6-80C2A5F](https://openairdocs.org/engine/ge-cf6-80c2a5f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 262 reports

- [SDR FDEA202607030831](https://openairdocs.org/sdr/FDEA202607030831.md): Engine · damaged · Jul 3, 2026 · N168FE · Boeing 767300 · Engine Oil System (Airframe Furnished)
  > BURNED SMELL ON TAKEOFF. SUSPECT OIL LEAK IN HPC. EMERGENCY DECLARED. O2 USED. ENGINE R & R, COMPLETED RT ENG OPS CHECKS IN REF TO FEDEX WORKCARD 7100000-02-04. OK FOR SERVICE.
- [SDR FDEA201708312443](https://openairdocs.org/sdr/FDEA201708312443.md): Line · chafed · Aug 31, 2017 · N681FE · Airbus A300F4605R · Turbine Engine Oil System
  > DURING PREFLIGHT, FOUND FLUID LEAKING OUT OF REAR OF THE NR 1 ENGINE. FOUND AN OIL SUPPLY LINE MOUNTING CLAMP BROKEN AND OIL LINE CHAFED THROUGH. REMOVED AND REPLACED THE AFFECTED ENGINE OIL LINE AND CLAMPS IAW AMM 70-00-00-02-0-F. RAN THE NR 1 ENGINE. AL
- [SDR FDEA201708082147](https://openairdocs.org/sdr/FDEA201708082147.md): Duct · separated · Aug 8, 2017 · N673FE · Airbus A300F4605R · Pneumatic Distribution System
  > APU BLEED PREASURE WAS 4 PSI ON ENGINE START. ACFT RETURNED TO GATE. COULD HEAR BLEED AIR LEAK ON THE NR 2 ENGINE COWL. GAINED ACCESS FOUND MAIN SUPPLY DUCT CLAMP TOP OF ENGINE BLOWN OFF, PIPE CONNECTION SEPORATED WITH SEVERAL WIRE BUNDLES NEAR IT MELTED.
- [SDR FDEA201704111130](https://openairdocs.org/sdr/FDEA201704111130.md): Engine · failed · Apr 11, 2017 · N651FE · Airbus A300F4605R · Engine (Turbine/Turboprop)
  > FLYING FROM SJC TO IND AT LEVEL OFF THE OIL BUGS WERE SET AT 16QTS ON EACH GAGE TO MATCH THE CORRECT OIL QUANTITY READING. APPROXIMATELY 15-20 MINS LATER, NR 1 ENG OIL QUANTITY DECREASED TO 13 QTS, THEN 5-10MIN LATER WENT TO 12.5 QTS. FO WENT TO THE CABIN ARE
- [SDR FDEA201703150881](https://openairdocs.org/sdr/FDEA201703150881.md): Eec · malfunctioned · Mar 15, 2017 · N660FE · Airbus A300F4605R · Fuel Control/Turbine Engines
  > AT FL 200, THE NR 2 ENGINE ROLLED BACK SUDDENLY. WARNING LIGHTS BUT NO HORNS. STARTED A DESCENT, TURNED OFF AUTO THROTTLES AND SELECTED CONTINOUS RELIGHT AFTER CHECKING N1 AND N2. THE ENGINE RESPONDED, ELECTED TO LEAVE IT AT IDLE UNTIL THE THRUST REVERS
- [SDR FDEA201606041828](https://openairdocs.org/sdr/FDEA201606041828.md): Floor Panel · worn · Jun 4, 2016 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242FJ DAMAGED. FABRICATED AFT CARGO FLOOR PANEL 242FJ ON T16 1211786 IAW SRZ 25-005. CLASSIFIED AS A CAT A MAJOR REPAIR.
- [SDR FDEA201512254078](https://openairdocs.org/sdr/FDEA201512254078.md): Hmu · malfunctioned · Dec 25, 2015 · N652FE · Airbus A300F4605R · Fuel Control/Turbine Engines
  > AT TOP OF DESCENT, NR 1 ENG STARTED A SERIES OF 6 - 7 STALLS. FOLLOWED THE QRH & OPERATED AT IDLE. N1 STARTED TO DECREASE & EGT CLIMBED TO 622 AT SHUTDOWN. PARAMETERS AT SHUTDOWN N1 29.5, EGT 622, N2 66.6 WIND MILLING TIME WAS 10 MIN PERFORMED BORESCOPE IN
- [SDR FDEA201506292123](https://openairdocs.org/sdr/FDEA201506292123.md): Thrust Reverser · damaged · Jun 29, 2015 · N651FE · Airbus A300F4605R · Engine Thrust Reverser
  > NUMBER 1 OTBD THRUST REVERSER AFT HINGE LUG DAMAGED EXHAUST SYS. THRUST REVERSER BLEND REPAIR OF HINGE BEAM REPAIRED IAW EA 6-7830-T0318435. THIS REPAIR IS CLASSIFIED AS A CATEGORY B MAJOR REPAIR.
- [SDR FDEA201408072105](https://openairdocs.org/sdr/FDEA201408072105.md): Connector · unknown · Aug 7, 2014 · N674FE · Airbus A300F4605R · Engine Exhaust System Wiring
  > ON TAKEOFF NR 2 THRUST REVERSER PRESSURIZED. FOUND LT DPV SOLENOID CONNECTOR NOT PROPERLY REMOVED IAW MEL 78-30-01-A. REMOVED CONNECTOR & CONTINUED ON WITH MX PROCEDURES TO END. OK TO CONTINUE ON MEL.
- [SDR FDEA201403210541](https://openairdocs.org/sdr/FDEA201403210541.md): Ecu · failed · Mar 21, 2014 · N677FE · Airbus A300F4605R · Fuel Controlling System
  > NR 1 ENGINE ROLLED BACK PASSING FL 315, N1 & N2 DECREASED IGNITION TURNED ON. ONE MINUTE LATER ENGINE REGAINED POWER. RETURNED & LANDED. NR 1 ENGINE FADEC FAULT LIGHT ILLUMINATED ON LANDING & APU AUTO SHUTDOWN. NO ECAM ALERTS ACCOMPANIED NR 1 ENGINE ROLLB
- [SDR FDEA201401160118](https://openairdocs.org/sdr/FDEA201401160118.md): Engine · leaking · Jan 16, 2014 · N667FE · Airbus A300F4605R · Engine (Turbine/Turboprop)
  > PRIOR TO DECENT, COURIERS NOTIFIED COCKPIT OF SMOKE IN CABIN. NO SMOKE DETECTORS OR ECAM WARNINGS IN COCKPIT OR ODOR OF SMOKE. RAN AIR CONDITIONING SMOKE CHECK LIST. DECLARED EMERGENCY LANDED. ON GROUND HAD ODOR IN COCKPIT. NR 1 ENGINE HAS DEBRIS IN SCR
- [SDR FDEA201311272884](https://openairdocs.org/sdr/FDEA201311272884.md): Engine · failed · Nov 27, 2013 · N664FE · Airbus A300F4605R · Engine (Turbine/Turboprop)
  > PDIS 664 79-310005832 27NOV13 IND OPEN U LOG PAGES 02343904. ENG ADVISORY FOR NR 2 ENG OIL QTY ZERO & FLUCTUATING OIL PRESS ON ECAM & ENG INSTRUMENTS. ADVISORY OCCURRED AT FL 370 EGT REMAINED NORMAL. OIL QTY & PRESS RETURNED TO NORMAL ON FINAL APPROACH. W
- [SDR FDEA201303210639](https://openairdocs.org/sdr/FDEA201303210639.md): Engine · inoperative · Mar 21, 2013 · N672FE · Airbus A300F4605R · Engine (Turbine/Turboprop)
  > PER FLIGHT CREW DEBRIEF, THE NR 1 ENGINE ON TAXI OUT HAD ECAM ENGINE FAILURE AND ASSOCIATED PARAMETERS WINDING DOWN. IAW CAPTAIN, AFTER BEING NOTIFIED BY MEM TOWER OF SMOKE FROM NR 1 ENG THEY PULLED FIRE HANDLE BUT DIDN'T DISCHARGE BOTTLE AND THEN DEPARTED AC
- [SDR FDEA201209223396](https://openairdocs.org/sdr/FDEA201209223396.md): Floor Panel · damaged · Sep 22, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 242QJ CRUSHED AT CLEVIS ADAPTOR CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201209153331](https://openairdocs.org/sdr/FDEA201209153331.md): Link Assy · cracked · Sep 15, 2012 · N686FE · Airbus A300F4605R · Fuselage Main, Structure
  > MAIN DECK CARGO FRAME 48L BELOW SEAT TRACK 4L SUPPORT STRUCTURE ATTACHMENT LUG CRACKED ONE INCH LONG, STR 27-28. R & R DAMAGED LINK ASSY IAW SRM 51-40-21, PG 7, PARA 5.
- [SDR FDEA201209113283](https://openairdocs.org/sdr/FDEA201209113283.md): Web · cracked · Sep 11, 2012 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO FLOOR WEB AT FR 79 RT OTBD OF FLOOR RAIL HAS.25" CRACK EXTENDING FROM LIGHTENING HOLE. R & R WEB IAW SRM 51-72-10, P1.
- [SDR FDEA201209113287](https://openairdocs.org/sdr/FDEA201209113287.md): Floorboard · cracked · Sep 11, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO FLOORBOARD 242UJ CRACKED. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201209103275](https://openairdocs.org/sdr/FDEA201209103275.md): Floorboard · damaged · Sep 10, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOORBOARD 131NG CRACKED ON LOWER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201209073251](https://openairdocs.org/sdr/FDEA201209073251.md): Floorboard · damaged · Sep 7, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOORBOARD 151TF HAS TWO AREAS DAMAGED UPPER AND LOWER SKIN PLYS WITH CRUSHED CORE. THE LARGEST AREA IS 8" BY 3". FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201209073253](https://openairdocs.org/sdr/FDEA201209073253.md): Floorboard · gouged · Sep 7, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOORBOARD 252UH UPPER SURFACE GOUGED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201209073254](https://openairdocs.org/sdr/FDEA201209073254.md): Floorboard · cracked · Sep 7, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO FLOORBOARD 251DF CRACKED, FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201209073256](https://openairdocs.org/sdr/FDEA201209073256.md): Floorbeam · damaged · Sep 7, 2012 · N663FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > FORWARD SIDE OF FLOORBEAM AT FR 17 Y1456 WEB IS DRILLED THROUGH AND HAS A RIVET IN THE HOLE THAT HAS NOT BEEN BUCKED. FABRICATED AND INSTALLED PICKUP FITTING IAW DWG A53611735 AND FSRM 51-40-21, PARA 7.
- [SDR FDEA201209073255](https://openairdocs.org/sdr/FDEA201209073255.md): Skin · chafed · Sep 7, 2012 · N686FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT WING OUTER FLAP INBD SIDE L/E CHAFED MARK APPROX LENGTH IS 1 INCH AND WIDTH IS 0.50 REF AMM 27-00-00-06, ZONE 580. REPAIRED WING OUTER FLAP IAW A300-600 FSRM 57-50-00 PARA 4.H. PG 231 THRU 233 AND FIG 208 AND EA 6-5750-160186 PT. 1.
- [SDR FDEA201209063248](https://openairdocs.org/sdr/FDEA201209063248.md): Skin · damaged · Sep 6, 2012 · N663FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT INBD FLAP LOWER SURFACE HAS 22 DENTS AND 12 GOUGES LOCATED FROM STGR 2.10 TO T/E AND RIB 3A TO RIB19A, COMPLIED WITH EA 6-5730160178.
- [SDR FDEA201209063245](https://openairdocs.org/sdr/FDEA201209063245.md): Spring · broken · Sep 6, 2012 · N688FE · Airbus A300F4605R · Door Warning System
  > AVIONICS DOOR CAME OPEN IN FLIGHT (121BL). DOOR DID NOT OPEN BUT CREW GOT LIGHT IN COCKPIT. FOUND SPRING BROKEN. R & R THE DOOR HANDLE TENSION SPRINGS IAW MM 52-41-14-04. OPS TESTED GOOD. DOOR CLOSES SECURLY AND INDICATES ON ECAM.
- [SDR FDEA201209063247](https://openairdocs.org/sdr/FDEA201209063247.md): Floorbeam · cracked · Sep 6, 2012 · N686FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN CARGO DECK FLOORBEAM AT FR 61 BETWEEN SEAT TRACK 4R AND 5R CRACKED ABOUT 0.125" ON THE AFT FACE EXTRUSION REF AMM 53-10-15-06-02, ZONE 250. BLENDED FLOORBEAM IAW SRM 53- 10-15- PG 14. CUT OUT CRACKED AREA OF FLOORBEAM IAW SRM 53-10-15 FIG 211 PG 386.
- [SDR FDEA201209043220](https://openairdocs.org/sdr/FDEA201209043220.md): Skin · damaged · Sep 4, 2012 · N663FE · Airbus A300F4605R · Elevator, Plate/Skin
  > LT ELEVATOR TIP LOWER SURFACE HAS A LIGHTNING STRIKE. REPAIRED IAW EA 6-5520-157869, AND RAS 70566303/003/2012, ISSUE A.
- [SDR FDEA201209043221](https://openairdocs.org/sdr/FDEA201209043221.md): Skin · damaged · Sep 4, 2012 · N663FE · Airbus A300F4605R · Elevator, Plate/Skin
  > LT ELEVATOR TIP PANEL UPPER SURFACE HAS 2 EA LIGHTNING STRIKES. REPAIRED IAW EA 6-5520-157869 PART 1 AND RAS, ISSUE A.
- [SDR FDEA201209043218](https://openairdocs.org/sdr/FDEA201209043218.md): Floor Support · corroded · Sep 4, 2012 · N718FD · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AFT HOLD FLOOR SUPPORT BETWEEN FR63 AND FR64 SECOND FROM LT SIDE FOUND CORRODED AT ANCHOR NUT LOCATIONS. AFT HOLD SUPPORT BEAM AT FR63 AND FR64 SECOND FROM LT SIDE, REPLACED IAW SRM 51-40-21.
- [SDR FDEA201209043217](https://openairdocs.org/sdr/FDEA201209043217.md): Seat Track · corroded · Sep 4, 2012 · N661FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > CENTER MAIN DECK, FOUND RT 5TH SEAT TRACK CORROSION AREA FROM FR45 TO 54 AT -Y1959 POSITION. FABRICATE AND R & R THE SEAT TRACK IAW DWG NR A53813618 AND AB6F SRM 51-40-21. REINSTALLED THE CROSSBEAMS OF FR45-FR54 -Y1959 WITH CHECK OK FOR SERVICE IAW AMM 20-21
- [SDR FDEA201209043215](https://openairdocs.org/sdr/FDEA201209043215.md): Floorbeam · cracked · Sep 4, 2012 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT CEILING AREA OF M/D FLOORBEAM RT SIDE EDGE AREA GOT CRACK AT FR29 POSITION. REPAIRED IAW EA 6-5310-149065 WITH AB6F SRM 53-10-15. THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
- [SDR FDEA201208273183](https://openairdocs.org/sdr/FDEA201208273183.md): Floor Support · corroded · Aug 27, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO FRAME 11A THRU 13A, Y1456 HAS SURFACE CORROSION ON TOP AND BOTTOM AROUND THE MOUNTING SCREWS ON TEE PROFILE. AFTER REMOVAL OF LEVEL 1 CORROSION FOUND CORROSION BEYOND ECONOMICAL REPAIR, R & R IAW SRM 51-72 10, PG 1-3 AND DWG A536-12519.
- [SDR FDEA2012082631710](https://openairdocs.org/sdr/FDEA2012082631710.md): Floor Panel · damaged · Aug 26, 2012 · N661FE · Airbus A300F4605R · Fuselage Floor Panel
  > CENTER MAIN DECK FLOOR PANEL 242EJ HAS INSERT DAMAGE.
- [SDR FDEA201208263177](https://openairdocs.org/sdr/FDEA201208263177.md): Cargo Track · corroded · Aug 26, 2012 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO TRACK L4 BETWEEN FR 46 & 47 HAS 2EA AREAS OF CORROSION APPROXIMATELY 8" LONG. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 205.
- [SDR FDEA201208263172](https://openairdocs.org/sdr/FDEA201208263172.md): Floor Panel · damaged · Aug 26, 2012 · N661FE · Airbus A300F4605R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131QG EDGE AREA HAS IMPACT DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA201208263168](https://openairdocs.org/sdr/FDEA201208263168.md): Cover · cracked · Aug 26, 2012 · N661FE · Airbus A300F4605R · Wing Miscellaneous Structure
  > LT WING T/E FOUND 1EA COVER CRACKED POSITION NEAR LT MAIN LT MLG AFT TRUNNION INBD SIDE. REMOVED COVER FOR FABRICATION IAW DWG A57240775 THEN REPLACED IAW SRM 51-72-10 & 51-40-21. INSTALLED COVER AND CONDITION CHECKED GOOD. REPAIR CLASSIFIED AS MINOR PER GM
- [SDR FDEA201208253164](https://openairdocs.org/sdr/FDEA201208253164.md): Seat Track · corroded · Aug 25, 2012 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BETWEEN FR 53 AND 54 SEAT TRACK 3R HAS CORROSION APPROX 2" IN THE CENTER OF THE TRACKS IN BET SCALLOPS. AFTER REMOVAL OF LEVEL 1 CORROSION, AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 102. REMOVED SEAT TRACK 3R BET. FR50 AND 54 IAW SR
- [SDR FDEA201208243154](https://openairdocs.org/sdr/FDEA201208243154.md): Skin · gouged · Aug 24, 2012 · N663FE · Airbus A300F4605R · Leading Edge Devices
  > LT WING NR 2 SLAT LWR SURFACE GOUGED 1 SQUARE INCH, LOCATED 3 INCHES FROM INBD EDGE AND 6 INCHES FWD OF T/E SMOOTHED AND BLENDED GOUGE IAW FSRM 51-73-10 MATERIAL LOSS IS.007, BEFORE.047 AFTER.040 FOUND TO OUT OF LIMITS IAW SRM 57-40-00 PARA 4B, PG 104.
- [SDR FDEA201208243155](https://openairdocs.org/sdr/FDEA201208243155.md): Floorboard · damaged · Aug 24, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor Panel
  > FWD CARGO BAY FLOORBOARD 131RG BROKEN AT 2 CORNERS AND CRUSHED BY TOOL ON THE EDGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWGSRZ 25-005 REV J.
- [SDR FDEA201208243157](https://openairdocs.org/sdr/FDEA201208243157.md): Adapter · damaged · Aug 24, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO FLOOR CLEVIS ADAPTER AT FR38.1 BTWN SEAT TRACKS 2R AND 3R HAS BROKEN SCALLOPS,.5 AREA R & R CLEVIS ADAPTER AT FR 38.1 BETWEEN SEAT TRACKS 2R AND 3R IAW SRM 51-72-10.
- [SDR FDEA201208243160](https://openairdocs.org/sdr/FDEA201208243160.md): Adapter · cracked · Aug 24, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO ZONE 250, CLS ADAPTER HAS A 8.5 INCH LONG CRACK IN UPPER RADIUS AT FR61 BTWN SEAT TRACKS 4R(-Y1456) AND 5R (-Y1959). R & R CLEVIS ADAPTER AT FR 61 BETWEEN SEAT TRACKS 4R & 5R IAW FRSM 51-72-10.
- [SDR FDEA201208243161](https://openairdocs.org/sdr/FDEA201208243161.md): Adapter · cracked · Aug 24, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO ZONE 250, CLEVIS ADAPTER HAS A 9.5" LONG CRACK IN UPPER RADIUS AT FR62 BETWEEN SEAT TRACKS 4R(-Y1456) AND 5R (-Y1959). R & R CLEVIS ADAPTER AT FR 62 BETWEEN SEAT TRACKS 4R & 5R IAW FRSM 51-72-10.
- [SDR FDEA201208243158](https://openairdocs.org/sdr/FDEA201208243158.md): Web · damaged · Aug 24, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FR11 TO FR12 WEB DAMAGED. REMOVED DAMAGED WEB IAW SRM 51-40-21 PARA 6. FABRICATED NEW WEB IAW DWG A53612536. INSTALLED NEW WEB AT FR 12A TO FR 14 STA Y953 IAW SRM 51-40-21 PARA 7. REPROTECTED ALL PARTS IAW SRM 51-21-10 AND 51-75-10.
- [SDR FDEA201208243159](https://openairdocs.org/sdr/FDEA201208243159.md): Floor Support · corroded · Aug 24, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO SURFACE CORROSION ON TOP AND BOTTOM AROUND MOUNTING SCREWS ON FLOOR SUPPORT. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-21 PARA 7.
- [SDR FDEA201208233140](https://openairdocs.org/sdr/FDEA201208233140.md): Seat Track · corroded · Aug 23, 2012 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK L4 BETWEEN FR 42 AND 44 HAS 2 AREAS OF CORROSION APPROX 8 INCHES LONG, REF AMM 53-10-16-6 CORROSION AT TRACK 4L FR 42 TO 44 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 102. REMOVED 4L TRACK FR 40 TO 44.5 REDUCTION SPLICE IAW SRM 51-40-21, PARA
- [SDR FDEA201208233145](https://openairdocs.org/sdr/FDEA201208233145.md): Adapter · corroded · Aug 23, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FLOOR CLEVIS ADAPTER UPPER SURFACE CORRODED 10 SQUARE INCHES LOCATED FR 25 BTWN 2R & 3R SEAT TRACKS AFTER REMOVAL OF LEVEL 1 CORROSION IAW FRSM 51-74-10, PARA 5 FOUND NO LIMITS FOR CLEVIS ADAPTER AT FR25. R & R CLEVIS ADAPTER IAW SRM 51-40-21, PARA 6-7. REP
- [SDR FDEA201208223112](https://openairdocs.org/sdr/FDEA201208223112.md): Seat Track · corroded · Aug 22, 2012 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 5R AT FR58 HAS 1 SQUARE INCH OF CORROSION ON INBD FLANGE AROUND NUT PLATE HOLE. AFTER REMOVAL OF LEVEL 1 CORROSION SEAT TRACK 5R WAS FOUND TO BE OUT OF LIMITS IAW SRM 51-74-10 AND 53-10-16 FIG 102. R & R SEAT TRACK 5R AT FR 57.3 TO FR 58 IAW SRM 5
- [SDR FDEA201208223108](https://openairdocs.org/sdr/FDEA201208223108.md): Floor Panel · dented · Aug 22, 2012 · N661FE · Airbus A300F4605R · Fuselage Floor Panel
  > CARGO BAY 162EF FLOOR PANEL UPPER SURFACE HAS SEVERAL SMALL DENTS. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20 & DWG A53279966. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA201208223109](https://openairdocs.org/sdr/FDEA201208223109.md): Floor Panel · debonded · Aug 22, 2012 · N661FE · Airbus A300F4605R · Fuselage Floor Panel
  > CARGO BAY 161AF FLOOR PANEL EDGE AREA DEBONDED. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20 & DWG A53279966. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA201208223110](https://openairdocs.org/sdr/FDEA201208223110.md): Floor Panel · damaged · Aug 22, 2012 · N661FE · Airbus A300F4605R · Fuselage Floor Panel
  > CARGO BAY 162DF FLOOR PANEL EDGE AREA HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Next page: https://openairdocs.org/engine/ge-cf6-80c2a5f/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 = 'CF680C2A5F'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf6-80c2a5f/reports

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