# Service difficulty reports: N780FD A list on [N780FD](https://openairdocs.org/aircraft/N780FD.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 108 reports - [SDR FDEA202111272942](https://openairdocs.org/sdr/FDEA202111272942.md): Slide · unknown · Nov 27, 2021 · N780FD · Boeing 757200 · Emergency Equipment > R1 SLIDE DEPLOYED FOR EMERGENCY EVACUATION. REMOVED AND REPLACED R1 DOOR SLIDE PER AMM 25-66-01- 4. A/C OK FOR SERVICE - [SDR FDEA202111272939](https://openairdocs.org/sdr/FDEA202111272939.md): Filter · dirty · Nov 27, 2021 · N780FD · Boeing 757222 · Air Distribution System > "MAIN CARGO FIRE" MESSAGE ON EICAS ON LANDING ROLL OUT. EMER EVAC OFF THE END OF THE RUNWAY. EMERGENCY DECLAERED. SHGN 27NOV21 04:44 ROC U WHEN ARRIVING AT A/C A WALK AROUND WAS PERFORMED. FOUND SAND AND DEBRIS ON BELLY OF A/C FORWARD OF ACM INLETS, IN - [SDR FDEA202111232925](https://openairdocs.org/sdr/FDEA202111232925.md): None · none · Nov 23, 2021 · N780FD · Boeing 757200 · Hydraulic Power System > PDIS 780 29-02 5877 23NOV21 IND OPEN U L HYD QTY SHGN 23NOV21 08:05 IND U ACFT BLOCKED IN W LEFT HYD SYSTEM QTY READING.55. RAN LEFT SYSTEM ELECTRIC PUMPS AND OPENED MAIN CARGO DOOR AS REQ. W/ NO PUMP CAVITATION. SHGN 23NOV21 08:30 IND - [SDR FDEA202106081470](https://openairdocs.org/sdr/FDEA202106081470.md): Pump · leaking · Jun 8, 2021 · N780FD · Boeing 757222 · Hydraulic Pump (Electric/Engine), Main > PDIS 780 29-02 5505 08JUN21 IND OPEN U ON DESCENT HYDRAULIC SYSTEM PRESSURE ILLUMINATED. (L) RAN QRH, LEADING US TO USE ALTN GEAR EXTEND, LE, TE. SHGN 08JUN21 05:48 IND APON SHU - [SDR FDEA202012113123](https://openairdocs.org/sdr/FDEA202012113123.md): Floor Panel · delaminated · Dec 11, 2020 · N780FD · Boeing 757222 · Fuselage Floor Panel > MAIN CABIN FLOOR BOAD IN BAY 5L HAS A PUNCTURE IN UPPER SKIN. REPAIRED PUNCTURE ON MAIN CABIN FLOOR BOARD AND APPLIED ANTI-SKID TAPE TO AREA, IAW B757 SRM 53-00-50 FIG 201. - [SDR FDEA202012093096](https://openairdocs.org/sdr/FDEA202012093096.md): Frame · cracked · Dec 9, 2020 · N780FD · Boeing 757222 · Fuselage Main, Frame > LT 1640 FRAMA INBOARD FASTENER HOLE AT S14L CRACK INDICATION. - [SDR FDEA202012063046](https://openairdocs.org/sdr/FDEA202012063046.md): Frame Angle · cracked · Dec 6, 2020 · N780FD · Boeing 757222 · Nacelle/Pylon, Main Frame > NR 2 PYLON UPPER RT PANEL SUPPORT IS CRACKED APPROXIMATELY STA 156. REPAIRED PER B757 SRM 54-51-71-2R AND 51-70-11-0G FIG 1. - [SDR FDEA202012033024](https://openairdocs.org/sdr/FDEA202012033024.md): Panel · corroded · Dec 3, 2020 · N780FD · Boeing 757222 · Wing, Plate/Skin > LT WING UPPER TRAILING EDGE PANEL OUTBOARD OF AILERON IS CORRODED. REPAIRED PER B757 SRM 57-51-01-2R. - [SDR FDEA202012013011](https://openairdocs.org/sdr/FDEA202012013011.md): Skin · delaminated · Dec 1, 2020 · N780FD · Boeing 757222 · Trailing Edge Flaps > DURING AGING AIRCRAFT INSPECTION FOUND LT OUTBOARD AFT FLAP LOWER INBOARD SKIN TO BE DELAMINATED. REMOVED FINISH, EVALUATED, REMOVED DAMAGE, AND REPAIRED LT OUTBOARD AFT FLAP, IAW B757 SRM 57-53-01-2R TABLE 2, 51-70-04-0G PARA 4A-I. MAJOR REPAIR. - [SDR FDEA202012013010](https://openairdocs.org/sdr/FDEA202012013010.md): Seal Depressor · damaged · Dec 1, 2020 · N780FD · Boeing 757222 · Fuselage Main, Structure > MAIN CARGO DOOR CUTOUT LOWER SEAL DEPRESSOR DAMAGED. COMPLIED WITH FEDEX EA F-5310-T0358270-P1 FUSELAGE-MAINFRAME-SEAL DEPRESSOR-STA 480 AND STA 620-S16L-DENTED. - [SDR FDEA202012013009](https://openairdocs.org/sdr/FDEA202012013009.md): Seal Depressor · damaged · Dec 1, 2020 · N780FD · Boeing 757222 · Fuselage Main, Structure > MAIN CARGO DOOR CUTOUT FWD LOWER SEAL DEPRESSOR DAMAGED. COMPLIED WITH FEDEX EA F-5310-T0358270-P1 MAINFRAME-SEAL DEPRESSOR-STA 480 AND STA 620-S-16L-DENTED. - [SDR FDEA202012013008](https://openairdocs.org/sdr/FDEA202012013008.md): Skin · dented · Dec 1, 2020 · N780FD · Boeing 757222 · Elevator, Plate/Skin > RIGHT ELEVATOR LOWER SURFACE IS DENTED 50 INCHES FROM OUTBOARD EDGE AND 6 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR LOWER SURFACE DENT 50" FROM OUTBOARD EDGE AND 6" FROM TRAILING EDGE, IAW FEDEX EA F-5520-T0358329 AND B757 SRM 51-70-17 PARA 4L AND SR - [SDR FDEA202011292998](https://openairdocs.org/sdr/FDEA202011292998.md): Floor Support · corroded · Nov 29, 2020 · N780FD · Boeing 757222 · Fuselage Miscellaneous Structure > MAIN CABIN FLOOR PANEL SUPPORT UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1663-RBL 54. REMOVED CORROSION, IAW B757 SRM 51-10-02, ORIG MAT.071", REMOVED MAT.003", REMAINING MAT.068". FOUND TO BE WITHIN LIMITS, IAW BOEING DWG 657N4303 REV B AND B757 SRM - [SDR FDEA202011292997](https://openairdocs.org/sdr/FDEA202011292997.md): Floor Support · corroded · Nov 29, 2020 · N780FD · Boeing 757222 · Fuselage Miscellaneous Structure > FLOOR PANEL SUPPORT UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1653-BS 1658, LBL 54. REMOVED CORROSION AS REQUIRED, IAW B757 SRM 51-10-02. ORIGINAL MATERIAL THICKNESS.071 MATERIAL LOSS OF.002 REMAINING MATERIAL THICKNESS.069. FOUND TO BE WITHIN LIMIT - [SDR FDEA202011292996](https://openairdocs.org/sdr/FDEA202011292996.md): Floor Support · corroded · Nov 29, 2020 · N780FD · Boeing 757222 · Fuselage Miscellaneous Structure > FLOOR PANEL SUPPORT STRUCTURE UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1668, LBL 55. REMOVED CORROSION AS REQUIRED, IAW B757 SRM 51-10-02 ORIGINAL THICKNESS.071. MATERIAL LOSS OF.002, REMAINING MATERIAL THICKNESS.069 FOUND TO BE WITHIN LIMITS, IAW B - [SDR FDEA202011293001](https://openairdocs.org/sdr/FDEA202011293001.md): Web · damaged · Nov 29, 2020 · N780FD · Boeing 757222 · Fuselage Miscellaneous Structure > MCD AFT WEB AND CLOSEOUT PANEL DAMAGED. REMOVED, FABRICATED, LOCATED, DRILLED, AND INSTALLED, IAW B757 SRM 51-40-02 B757 SRM 51-40-05, BOEING DWG 69-49309 REV D. TREATED BARE METAL, IAW B757 SRM 51-20-01. - [SDR FDEA202011293000](https://openairdocs.org/sdr/FDEA202011293000.md): Closeout Panel · damaged · Nov 29, 2020 · N780FD · Boeing 757222 · Fuselage Miscellaneous Structure > MCD FWD WEB AND CLOSEOUT PANEL DAMAGED. REMOVED, FABRICATED, LOCATED, DRILLED, AND INSTALLED, IAW B757 SRM 51-40-02, B757 SRM 51-40-05, BOEING DWG 69-49309 REV D, TREATED BARE METAL, IAW B757 SRM 51-20-01. - [SDR FDEA202011292999](https://openairdocs.org/sdr/FDEA202011292999.md): Floor Support · corroded · Nov 29, 2020 · N780FD · Boeing 757222 · Fuselage Miscellaneous Structure > FLOOR PANEL SUPPORT UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1642-BS 1658, RBL 54. REMOVED CORROSION, IAW B757 SRM 51-10-02, ORIG MAT.071", REMOVED MAT.003", REMAINING MAT.068". FOUND TO BE WITHIN LIMITS, IAW BOEING DWG 657N4303 REV B, B757 SRM 53-60 - [SDR FDEA202011282989](https://openairdocs.org/sdr/FDEA202011282989.md): Cover · cracked · Nov 28, 2020 · N780FD · Boeing 757200 · Nose/Tail Landing Gear > **SDR ENTERED IN ERROR** **SDR ENTERED IN ERROR** - [SDR FDEA202011282988](https://openairdocs.org/sdr/FDEA202011282988.md): Cover · cracked · Nov 28, 2020 · N780FD · Boeing 757200 · Nose/Tail Landing Gear > NLG STEERING CABLE PULLY ACCESS COVER IS CRACKED ON THE BOTTOM SURFACE **SDR ENTERED IN ERROR** - [SDR FDEA202011282993](https://openairdocs.org/sdr/FDEA202011282993.md): Duct · cracked · Nov 28, 2020 · N780FD · Boeing 757222 · Air Distribution System > FWD CARGO COMPARTMENT RT SIDE AT STA 670 AIR DISTRIBUTION DUCT CRACKED. REPAIRED FWD CARGO COMPARTMENT RT SIDE AT STA 670 AIR DISTRIBUTION DUCT BY REMOVING DAMAGE AND APPLYING FIBERGLASS FABRIC, IAW B757 AMM 21-23-01-8 REP NR 3 FIG 801. - [SDR FDEA202011282992](https://openairdocs.org/sdr/FDEA202011282992.md): Duct · cracked · Nov 28, 2020 · N780FD · Boeing 757222 · Air Distribution System > FWD CARGO COMPARTMENT RT SIDE AT STA710 AIR DISTRIBUTION DUCT CRACKED. REPAIRED FWD CARGO COMPARTMENT RT SIDE AT STA 710 AIR DISTRIBUTION DUCT BY REMOVING DAMAGE AND APPLYING FIBERGLASS FABRIC, IAW B757 AMM 21-23-01-8 REP NR 3 FIG 801. - [SDR FDEA202011282991](https://openairdocs.org/sdr/FDEA202011282991.md): Duct · cracked · Nov 28, 2020 · N780FD · Boeing 757222 · Air Distribution System > FWD CARGO COMPARTMENT RT SIDE AT STA 690 AIR DISTRIBUTION DUCT CRACKED. REPAIRED FWD CARGO COMPARTMENT RT SIDE AT STA 690 AIR DISTRIBUTION DUCT BY REMOVING DAMAGE AND APPLYING FIBERGLASS FABRIC, IAW B757 AMM 21-23-01-8 REP NR 3 FIG 801. - [SDR FDEA202011282990](https://openairdocs.org/sdr/FDEA202011282990.md): Duct · cracked · Nov 28, 2020 · N780FD · Boeing 757222 · Air Distribution System > FWD CARFO COMPARTMENT RT SIDE AT STA690 AIR DISTRIBUTION DUCT CRACKED. REPAIRED FWD CARGO COMPARTMENT RT SIDE AT STA690 AIR DISTRIBUTION DUCT BY REMOVING DAMAGE AND APPLYING FIBERGLASS FABRIC, IAW B757 AMM 21-23-01-8 REP NR 3 FIG 801. - [SDR FDEA202011252971](https://openairdocs.org/sdr/FDEA202011252971.md): Floorbeam · corroded · Nov 25, 2020 · N780FD · Boeing 757222 · Fuselage Main, Floor Beam > MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681, LBL 24. REPLACED NUT PLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02. - [SDR FDEA202011252970](https://openairdocs.org/sdr/FDEA202011252970.md): Floorbeam · corroded · Nov 25, 2020 · N780FD · Boeing 757222 · Fuselage Main, Floor Beam > MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681, LBL 39.5. REPLACED NUT PLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02. - [SDR FDEA202011252969](https://openairdocs.org/sdr/FDEA202011252969.md): Floorbeam · corroded · Nov 25, 2020 · N780FD · Boeing 757222 · Fuselage Main, Floor Beam > MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681, LBL 32. REPLACED NUT PLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02. - [SDR FDEA202011252968](https://openairdocs.org/sdr/FDEA202011252968.md): Floorbeam · corroded · Nov 25, 2020 · N780FD · Boeing 757222 · Fuselage Main, Floor Beam > MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681-RBL 18. REPLACED NUTPLATE AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV"F", AND B757 SRM 51-40-02. - [SDR FDEA202011252967](https://openairdocs.org/sdr/FDEA202011252967.md): Floorbeam · corroded · Nov 25, 2020 · N780FD · Boeing 757222 · Fuselage Main, Floor Beam > MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUTPLATE BS 1681-RBL 12. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02. - [SDR FDEA202011252966](https://openairdocs.org/sdr/FDEA202011252966.md): Floorbeam · corroded · Nov 25, 2020 · N780FD · Boeing 757222 · Fuselage Main, Floor Beam > MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE AT PRESSURE DECK THRU AFT PIT BULKHEAD PANEL BS 1681-RBL 36. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 "F", AND B757 SRM 51-40-02. - [SDR FDEA202011242962](https://openairdocs.org/sdr/FDEA202011242962.md): Floorbeam · corroded · Nov 24, 2020 · N780FD · Boeing 757222 · Fuselage Main, Floor Beam > MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUTPLATE BS 1681-RBL 24. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F" AND B757SRM 51-40-02. - [SDR FDEA202011242961](https://openairdocs.org/sdr/FDEA202011242961.md): Floorbeam · corroded · Nov 24, 2020 · N780FD · Boeing 757222 · Fuselage Main, Floor Beam > MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUTPLATE BS 1681-RBL 4. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N 5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02. - [SDR FDEA202011242960](https://openairdocs.org/sdr/FDEA202011242960.md): Floorbeam · corroded · Nov 24, 2020 · N780FD · Boeing 757222 · Fuselage Main, Floor Beam > MAIN CABIN FLOOR BEAM UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1681, LBL 24-BL 47. REMOVED SURFACE CORROSION AS REQUIRED, IAW B757 SRM 53-60-51-1A. ORIGINAL MATERIAL THICKNESS.071. MATERIAL LOSS.006. REMAINING MATERIAL THICKNESS.065 FOUND TO BE WI - [SDR FDEA202011242959](https://openairdocs.org/sdr/FDEA202011242959.md): Floorbeam · corroded · Nov 24, 2020 · N780FD · Boeing 757222 · Fuselage Main, Floor Beam > MAIN CABIN FLOOR BEAM UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1681, BL 4-RBL 54. REMOVED SURFACE CORROSION AS REQUIRED, IAW B757 SRM 53-60-51-1A. ORIGINAL MATERIAL THICKNESS.071, MATERIAL LOSS.004 REMAINING MATERIAL THICKNESS.067 FOUND TO BE WITHIN - [SDR FDEA202011242957](https://openairdocs.org/sdr/FDEA202011242957.md): Structure · damaged · Nov 24, 2020 · N780FD · Boeing 757222 · Galley Doors > G1A GALLEY LOWER INBOARD DOOR TRIM DAMAGED AT LOWER INBOARD CORNER. ACCOMPLISHED FEDEX EA F-2530-T0358223-P1 EQUIP AND FURNISH-GALLEY-ICE CHEST DOOR TRIM-DAMAGED. - [SDR FDEA2020050430887](https://openairdocs.org/sdr/FDEA2020050430887.md): Hydraulic Line · ruptured · May 3, 2020 · N780FD · Boeing 757222 · Hydraulic System, Main > LOSS OF ALL LEFT HYD FLUID. FOUND L MLG DOWN LOCK ACTUATOR LINE RUPTURED. R&R'D LINE IN REF TO AMM 32-32-02-4. RAN ENGINE AND ENGAGED EDP TO VERIFY PUMP INTEGRITY PER JRH. OPS CHECK GOOD, LEAK CHECK GOOD. OK FOR SERVICE - [SDR FDEA2020022860409](https://openairdocs.org/sdr/FDEA2020022860409.md): Sensor · inoperative · Feb 26, 2020 · N780FD · Boeing 757222 · Landing Gear Position and Warning > PDIS 780 32-30 4516 26FEB20 MEM OPEN U LOGPAGES:2877688 AFTER TAKEOFF, GEAR DISAGREE EICAS WITH AMBER GEAR LIGHT. GEAR EXTENDED NORMAL. NO EMERGENCY DECLARED. SHGN 26FEB20 22:32 MEM U DEBRIEFED FLIGHT CREW. DURING GEAR RETRACT RECEIVED G - [SDR FDEA2020022100362](https://openairdocs.org/sdr/FDEA2020022100362.md): Cylinder · inoperative · Feb 20, 2020 · N780FD · Boeing 757222 · Emergency Equipment > L1 DOOR EMERGENCY POWER RESERVOIR AT 0 PSI. REMOVED AND REPLACED LEFT #1 DOOR EMERGENCY POWER ASSIST RESERVOIR PER MM 52-11-30-4. PART REPLACED WAS A HR TEXTRON, ENTRANCE DOOR EMERGENCY POWER - [SDR FDEA20200221361](https://openairdocs.org/sdr/FDEA20200221361.md): Slide · damaged · Feb 20, 2020 · N780FD · Boeing 757222 · Passenger/Crew Doors > AFTER BLOCK IN FO DISARMED THE SLIDES AND CRACKED THE DOOR OPEN. WHEN GROUND CREW OPENED THE DOOR, THE SLIDE PARTIALLY DETAINED BUT DID NOT DEPLOY. INSTALLED L1 DOOR ESCAPE SLIDE ASSEMBLY IAW - [SDR FDEA201907111531](https://openairdocs.org/sdr/FDEA201907111531.md): Static Line · out of position · Jul 11, 2019 · N780FD · Boeing 757222 · Passenger/Crew Doors > UPON ARMING R1 WE DID NOT GET AN ARMED SLIDE LIGHT. F/O TRIED TO DISARM DOOR TO TRY AGAIN. DOOR WOULD NOT DISARM. IT APPEARS THE SLIDE WILL ARM BUT NO SLIDE ARMED LIGHT ILLUMINATES. FOUND SLIDE STATIC LINE WRAPPED AROUND GIRT BAR. REPOSITIONED STATIC LIN - [SDR FDEA2019061731300](https://openairdocs.org/sdr/FDEA2019061731300.md): Collar · worn · Jun 13, 2019 · N780FD · Boeing 757222 · Passenger/Crew Doors > L1 DOOR HOLD OPEN LOCK COLLAR BROKEN REMOVED AND REPLACED HOLD OPEN LOCK COLLAR ON L1 DOOR REF AMM 52-11-08-8. ALL DOOR CHECKS GOOD. PANEL REINSTALLED AND SEALED. - [SDR FDEA2019042290859](https://openairdocs.org/sdr/FDEA2019042290859.md): Light · malfunctioned · Apr 19, 2019 · N780FD · Boeing 757222 · Emergency Equipment > L1 DOOR SLIDE ARMED LIGHT NOT COMING ON AFTER ARMING DOOR PERFORMED OPERATIONAL CHECK ON SLIDE ARMED LIGHT IAW B757 AMM 25-66-11-2. OPS CHECK GOOD. - [SDR FDEA201811073128](https://openairdocs.org/sdr/FDEA201811073128.md): Skin · delaminated · Nov 7, 2018 · N780FD · Boeing 757222 · Trailing Edge Flaps > LT OTBD FLAP UPPER SKIN INBD END SHOWS EVIDENCE OF POSSIBLE DELAMINATION. REPAIRED LT OTBD FLAP UPPER SKIN INBD END DELAMINATION IAW SRM 51-70-17-OG PARA 3G AND EA T F-5750-T0343415 P1 FLAP SKIN REPAIR. - [SDR FDEA201703040775](https://openairdocs.org/sdr/FDEA201703040775.md): Proximity Sensor · failed · Mar 4, 2017 · N780FD · Boeing 757222 · Emergency Equipment > SLIDE LIGHT FOR LT ENTRY DOOR DOES NOT ILLUMINATE. REMOVED AND REPLACED THE L1 DOOR GIRT BAR PROXIMITY SENSOR IAW MM 25-66-11-2 AND WDM 25-66-11, OPS CHECKED NORMAL. - [SDR FDEA201610273713](https://openairdocs.org/sdr/FDEA201610273713.md): Seat Track · corroded · Oct 27, 2016 · N780FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings > MAIN CABIN SEAT TRACK BS 345 TO 377.70 LBL 6 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. EVALUATED DAMAGE LOSS.055 FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DET I. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED SEAT TRACK IAW SRM 53-00-52-1A. - [SDR FDEA201610273712](https://openairdocs.org/sdr/FDEA201610273712.md): Seat Track · corroded · Oct 27, 2016 · N780FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings > MAIN CABIN STA 345 TO 377.70 RBL 12 HAS CORROSION ON SEAT TRACK. REMOVED CORROSION IAW SRM 51-10-02. EVALUATED DAMAGE LOSS.060 FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DET I. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED SEAT TRACK IAW SRM 53-00-52- - [SDR FDEA201610193659](https://openairdocs.org/sdr/FDEA201610193659.md): Frame · gouged · Oct 19, 2016 · N780FD · Boeing 757222 · Fuselage Main, Frame > BS 231 FRAME BUTLINE 0 IS GOUGED. REPAIRED IAW EA F-5310-T0329105 P1. - [SDR FDEA201609033109](https://openairdocs.org/sdr/FDEA201609033109.md): Collar · cracked · Sep 3, 2016 · N780FD · Boeing 757222 · Passenger/Crew Doors > L1 GUST LOCK FAILS TO LOCK THE DOOR IN OPEN POSITION. REPLACED THE DAMAGED HOLD/OPEN LOCK TRIGGER CATCH AND THE UPPER COLLAR. - [SDR FDEA201603261074](https://openairdocs.org/sdr/FDEA201603261074.md): Skin · damaged · Mar 26, 2016 · N780FD · Boeing 757222 · Trailing Edge Flaps > RIGHT INBD MAIN & AFT FLAP HAS MULTIPLE HAIL DAMAGE DENTS. COMPLIED WITH EA F-5750-T0324304. RT WING INBD MAIN FLAP HAIL DAMAGE REPAIR. - [SDR FDEA201603261073](https://openairdocs.org/sdr/FDEA201603261073.md): Skin · damaged · Mar 26, 2016 · N780FD · Boeing 757222 · Trailing Edge Flaps > REF WRI 05-50 1554 LT INBD MAIN & AFT FLAP HAS MULTIPLE HAIL DAMAGE DENTS. COMPLIED WITH EA F-5750-T0324301. LT WING INBD MAIN FLAP HAIL DAMAGE REPAIR. Next page: https://openairdocs.org/aircraft/N780FD/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 n_number = 'N780FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N780FD/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.