# Service difficulty reports: Boeing 777-FS2

A list on [Boeing 777-FS2](https://openairdocs.org/model/boeing-777-fs2.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 14 · 690 reports

- [SDR FDEA202608221219](https://openairdocs.org/sdr/FDEA202608221219.md): Tire Tread · separated · Aug 22, 2026 · N857FD · Boeing 777FS2 · Tire
  > CHECK FOUND NR 11 TIRE TREAD SEPARATION.
- [SDR FDEA202608221218](https://openairdocs.org/sdr/FDEA202608221218.md): Power Supply · inoperative · Aug 22, 2026 · N854FD · Boeing 777FS2 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND EXTERIOR RT EMERGENCY LIGHT NOT WORKING. RT EMERGENCY LIGHT POWER SUPPLY REPLACED IAW AMM 33-51-06-2. TESTED OK.
- [SDR FDEA202607150925](https://openairdocs.org/sdr/FDEA202607150925.md): Skin · bulged · Jul 15, 2026 · N896FD · Boeing 777FS2 · Leading Edge Devices
  > RIGHT WING NR 9 SLAT UPPER SURFACE 32IN FROM OTBD EDGE FOUND BULGE. NR 9 SLAT UPPER SURFACE 32 INCH FROM OB EDGE BULGE AREA REPAIRED IAW SRM 51-40-02-0G, SRM 57-43-01-2R REPAIR 16 FIG 202, SRM 51-40-05-0G, SRM 51-20-01-0G REV 53.0 AND EA G-5750-T0388015 P1.
- [SDR FDEA202607120916](https://openairdocs.org/sdr/FDEA202607120916.md): Light Sys · malfunctioned · Jul 12, 2026 · N850FD · Boeing 777FS2 · Emergency Lighting
  > CHECK FOUND WHEN THE OVERHEAD PANEL EMER LIGHTS SWITCH IN "ON" POSITION, THE EMERGENCY LIGHTS NOT ILLUMINATED. AMM: 33-51-00-5 RESET THE CB'S AND PERFORMED EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE CONTROL SWITCH ON THE OVERHEAD PANEL REF AMM33-51-00
- [SDR FDEA202606090690](https://openairdocs.org/sdr/FDEA202606090690.md): Retainer · damaged · Jun 9, 2026 · N859FD · Boeing 777FS2 · Leading Edge Devices
  > FOUND RH WING SLAT NR 8 IB EDGE SEAL RETAINER UPPER SURFACE AFT SECOND FASTENER HOLE WORN. RH WING NO.8 SLAT IB EDGE OUTER SKIN FASTENER HOLE WORN AREA REPAIRED IAW SRM 57-43-01-2R REPAIR 6 FIGURE 203, SRM 51-40-02-0G, SRM 51-40-05-0G, SRM 51-20-01-0G, REV
- [SDR FDEA202606090689](https://openairdocs.org/sdr/FDEA202606090689.md): Skin · damaged · Jun 9, 2026 · N859FD · Boeing 777FS2 · Leading Edge Devices
  > NO.7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS 184 SCREW HOLE FOUND WORN. NO.7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS 184 SCREW HOLE WORN AREA REPAIRED AS PER B777 SRM 57-43-01-2R REPAIR 6 FIGURE 203, SRM 51-40-02-0G, SRM 51-40-05-0G, SRM 51-20-
- [SDR FDEA202606060678](https://openairdocs.org/sdr/FDEA202606060678.md): Skin · cracked · Jun 6, 2026 · N859FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING PERFORM WORK CARD: E G-5710-E0376285 G P11 STEP 5.A.(2) THEN FOUND 01 EA CRACKED ON LT UPPER WING SKIN FASTENER NR 5. REPAIRED AS PER B777 SRM 51-40-05- 0G FIGURE 4 TABLE C, SRM 51-40-02-0G FIGURE 12, SRM 51-40-04-0G FIGURE 2 TABLE A, REV 53.0 AND
- [SDR FDEA202606060677](https://openairdocs.org/sdr/FDEA202606060677.md): Skin · cracked · Jun 6, 2026 · N859FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING PERFORM WORK CARD:E G-5710-E0376285 G P12 STEP 5.A.(2) THEN FOUND 01 EA CRACK ON RH UPPER WING SKIN FASTENER #5. REPAIRED AS PER B777 SRM 51-40-05- 0G FIGURE 4 TABLE C, SRM 51-40-02-0G FIGURE 12, SRM 51-40-04-0G FIGURE 2 TABLE A, REV 53.0 AND EA G
- [SDR FDEA202606050674](https://openairdocs.org/sdr/FDEA202606050674.md): Skin · cracked · Jun 5, 2026 · N869FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP 5.A.(2) THEN FOUND 02EA CRACKS ON RH UPPER WING SKIN COMMON TO FASTENER #5 AS MARKED.
- [SDR FDEA202606050673](https://openairdocs.org/sdr/FDEA202606050673.md): Skin · damaged · Jun 5, 2026 · N859FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > REQUEST A PERMANENT REPAIR ON AFT FUSELAGE SKIN STA 2319 TO STA 2344.5, S-48R TO S-49R.
- [SDR FDEA202606040671](https://openairdocs.org/sdr/FDEA202606040671.md): Lamp · inoperative · Jun 4, 2026 · N851FD · Boeing 777FS2 · Emergency Lighting
  > POST-FLT INSP, L1 OVERHEAD EMERGENCY LT INOP. AMM: 33-51-04-2 RE-LAMPED, REF B777 AMM: 33-51-04-2. LT TESTS SATIS, ITEM OK FOR SVC.
- [SDR FDEA202606010665](https://openairdocs.org/sdr/FDEA202606010665.md): Fire Bottle · failed · Jun 1, 2026 · N884FD · Boeing 777FS2 · Fire Bottle, Fixed
  > AT 2335Z (APPROX 1:15 INTO THE FLIGHT), FL340, TAT -11,.838MACH, GOT BOTTLE DISCHARGE APU CAUTION WITH LIGHT APU BTL DSCG ON OVERHEAD AND BOTTLE APU ON STATUS PAGE. PERFORMED APU FIRE EXTINGUISHING BOTTLE PRESSURE SWITCH TEST PER ABOVE REF, TEST PASS, AND
- [SDR FDEA202605310656](https://openairdocs.org/sdr/FDEA202605310656.md): Skin · damaged · May 31, 2026 · N852FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > REQUEST A PERMANENT REPAIR ON LT AFT FUSELAGE AT APPROXIMATELY STA 1895 TO 1958 AND S-40L TO S-43L. LT AFT FUSELAGE AT APPROXIMATELY BS 1895 TO 1958 AND S-40L TO S-43L. DAMAGED SKIN & STRINGER PERFORMED PERMANENT REPAIR IAW SRM51-10-02-0G. SRM51-20-01-0G.
- [SDR FDEA202605300655](https://openairdocs.org/sdr/FDEA202605300655.md): Wire · detached · May 30, 2026 · N885FD · Boeing 777FS2 · Light System Wiring
  > ARMING WIRE ON EMERGENCY LIGHTS SWITCH ON OVERHEAD PANEL IS STRETCHED OUT AND NOT ARMING EMERGENCY LIGHTS NORMALLY WHEN THE WIRE FALLS OFF SWITCH. AMM: 33-51-00-710-803 REINSTALLED ARMING WIRE IN NORMAL POSITION, OP TEST WAS SUCCESSFUL,AS PER AMM 33-51-0
- [SDR FDEA202605140595](https://openairdocs.org/sdr/FDEA202605140595.md): Skin · debonded · May 14, 2026 · N855FD · Boeing 777FS2 · Trailing Edge Flaps
  > LEFT OTBD FLAP LWR SURFACE FROM OTBD TO INBD 268 INCHES CROSS TE TO LE 10 INCHES FOUND DEBONDED. REPAIRED LH OB FLAP LWR SURFACE DISBOND AT OTEF STA 260 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 AND SRM 51-70-04-2R-0 PARA 4N FIGURE
- [SDR FDEA202605110586](https://openairdocs.org/sdr/FDEA202605110586.md): Switch · out of adjust · May 11, 2026 · N861FD · Boeing 777FS2 · Emergency Lighting
  > EMERGENCY LIGHTS ADVISORY MESSAGE STILL APPEARS. AMM: 33-51-00-5 ADJUSTED SWITCH GAURD, OPS CHECK GOOD.
- [SDR FDEA202605110585](https://openairdocs.org/sdr/FDEA202605110585.md): Warning Message · false activation · May 11, 2026 · N861FD · Boeing 777FS2 · Central Warning
  > EMERGENCY LIGHTS ADVISORY APPEARED ON PREFLIGHT. AMM: 33-51-00-5 EMERGENCY LIGHTS OPS CHECKS OK PER ABOVE REF, OK FOR SERVICE
- [SDR FDEA202605110581](https://openairdocs.org/sdr/FDEA202605110581.md): Skin · bulged · May 11, 2026 · N855FD · Boeing 777FS2 · Leading Edge Devices
  > FOUND RT WING LE NR 11 SLAT EXTERNAL SURFACE A BULGE AT STA 873. BULGE REPAIRED AS PER B777 SRM57- 43-01-2R REPAIR 9 FIGURE 202 REV:51.0 AND EA G-5750-T0387321 P1. TITLE: WING-FLIGHT SURFACES-RH WING #11 SLAT OUTER SKIN BULGES AT NOSE BEAM AREA BETWEEN OSB
- [SDR FDEA202605110580](https://openairdocs.org/sdr/FDEA202605110580.md): Skin · bulged · May 11, 2026 · N855FD · Boeing 777FS2 · Leading Edge Devices
  > FOUND RT WING LE NR 9 SLAT EXTERNAL SURFACE A BULGE AT STA 564. BULGE REPAIRED AS PER B777 SRM57-43- 01-2R REPAIR 16 FIGURE 202 REV:53.0. AND EA G-5750-T0387322 P1. TITLE: WING - FLIGHT SURFACES-RH WING #9 SLAT OUTER SKIN BULGE AT NOSE RIB AT OSCS 564 - SR
- [SDR FDEA202605100579](https://openairdocs.org/sdr/FDEA202605100579.md): Skin · cracked · May 10, 2026 · N855FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP3.B & STEP5.A.(2) THEN FOUND 01EA CRACK ON THE RH UPPER WING SKIN FASTENER #5. RH UPPER WING SKIN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-40-05- 0G FIGURE 4 TABLE C,51-40-02-0G,51-40-
- [SDR FDEA202605100578](https://openairdocs.org/sdr/FDEA202605100578.md): Skin · cracked · May 10, 2026 · N855FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING PERFORM WORK CARD:EG-5710-E0376285 G P11 STEP3.B & STEP5.A.(2) FOUND TWO CRACKS ON THE LT UPPER WING SKIN FASTENER #5. H WING UPPER SKIN IN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-50- 02-0G FINGURE 1,51-40-02-0G,51-10-01-0G,51-20
- [SDR FDEA202605030534](https://openairdocs.org/sdr/FDEA202605030534.md): Skin · dented · May 3, 2026 · N884FD · Boeing 777FS2 · Trailing Edge Flaps
  > FOUND LEFT WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT THE CROSS OTEF 127 INCHES AND T/E 10 INCHES. REPAIRED LH WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT OTEF STA 127 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4I FIG
- [SDR FDEA202605030533](https://openairdocs.org/sdr/FDEA202605030533.md): Skin · dented · May 3, 2026 · N884FD · Boeing 777FS2 · Trailing Edge Flaps
  > FOUND LEFT WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT THE CROSS OTEF 231 INCHES AND T/E 8 INCHES. REPAIRED LH WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT OTEF STA 231 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4I FIGU
- [SDR FDEA202604300524](https://openairdocs.org/sdr/FDEA202604300524.md): Skin · cracked · Apr 30, 2026 · N884FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK AT RH WING UPPER WING SKIN COMMON TO FASTENER 5. RT WING UPPER SKIN 5 FASTENER HOLE CRACKED AREA REPAIRED IAW SRM 51-50-02-0G, FIG 1, SRM 51-40-02-0G, FIG 12,
- [SDR FDEA202604300523](https://openairdocs.org/sdr/FDEA202604300523.md): Skin · cracked · Apr 30, 2026 · N884FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING PERFORM WORK CARD:EG-5710-E0376285 G P11 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK AT LT WING UPPER WING SKIN COMMON TO FASTENER 5. LT WING UPPER SKIN NR 5 FASTENER HOLE CRACKED AREA REPAIRED IAW SRM 51-50- 02-0G, FIGURE 1, SRM 51-40-02-0G F
- [SDR FDEA202604240496](https://openairdocs.org/sdr/FDEA202604240496.md): Bulb · inoperative · Apr 24, 2026 · N890FD · Boeing 777FS2 · Emergency Lighting
  > R1 DOOR AFT EMERGENCY EXIT SIGN LIGHT INOP (1EA BULB). REPLACED THE BULB EMERGENCY EXIT LIGHT AT R1 DOOR IAW AMM 33-51-01-2.
- [SDR FDEA202603200359](https://openairdocs.org/sdr/FDEA202603200359.md): Skin · dented · Mar 20, 2026 · N854FD · Boeing 777FS2 · Trailing Edge Flaps
  > RIGHT WING OTBD FLAP LOWER SURFACE FROM OB TO IB 272 INCHES CROSS TE TO LE 12 INCHES FOUND ONE DENT. REPAIRED RH WING OB FLAP LOWER SURFACE DENT AT OTEF STA 250 IAW SRM 57-53-01- 2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4G FIGURE 210 REV 51.0 AND E
- [SDR FDEA202603170356](https://openairdocs.org/sdr/FDEA202603170356.md): Skin · cracked · Mar 17, 2026 · N854FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING PERFORM WORK CARD:EG-5710-E0376285G P12 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK ON UPPER WING SKIN FASTENER NR 5. RH WING UPPER SKIN #5 HOLE CRACK REPAIRED AS PER B777 SRM 51-50-02-0G FIGURE 1, SRM 51-40-02-0G FIGURE 12, SRM 51-10-01-0G F
- [SDR FDEA202603160354](https://openairdocs.org/sdr/FDEA202603160354.md): Skin · cracked · Mar 16, 2026 · N854FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING PERFORM WORK CARD:EG-5710-E0376285G P11 STEP 3.B.(1)& STEP 5.A.(2) THEN FOUND 01EA CRACK ON UPPER WING SKIN FASTENER #5. LT WING UPPER SKIN #5 HOLE CRACK REPAIRED AS PER B777 SRM51-40-05-0G FIGURE 4 TABLE C, SRM51-40-02-0G FIGURE 12, SRM51-40-04-0G
- [SDR FDEA202603050315](https://openairdocs.org/sdr/FDEA202603050315.md): Lamp · inoperative · Mar 5, 2026 · N854FD · Boeing 777FS2 · Emergency Lighting
  > DURING POSTFLIGHT, FOUND R1 DOOR SLIDE EMERGENCY LIGHT INOP. REPLACED THE LAMPS, R1 DOOR SLIDE EMERGENCY EXTERIOR LIGHT 777 AMM. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA202603020314](https://openairdocs.org/sdr/FDEA202603020314.md): Slide · faulted · Mar 2, 2026 · N895FD · Boeing 777FS2 · Escape Slide
  > UPON CLOSING THE AIRCRAFT ENTRY DOOR AND ARMING THE EVACUATION SLIDES, F/O NOTICED AN FSS FAULT ON POSITIONS 13L AND 13R. F/O OPENED THE DOOR TO SEE IF THE FAULTS WOULD RESET WITHOUT DISARMING DOOR 1L AND THE EVACUATION SLIDE DEPLOYED BUT DID NOT INFLATE.
- [SDR FDEA202603020304](https://openairdocs.org/sdr/FDEA202603020304.md): Slide · unwanted deploy · Mar 2, 2026 · N895FD · Boeing 777FS2 · Escape Slide
  > UPON CLOSING THE ACFT ENTRY DOOR AND ARMING THE EVACUATION SLIDES, F/O NOTICED AN FSS FAULT ON POSITIONS 13L & 13R. F/O OPENED THE DOOR TO SEE IF THE FAULTS WOULD RESET WITHOUT DISARMING DOOR 1L & THE EVACUATION SLIDE DEPLOYED BUT DID NOT INFLATE. MAINTENANC
- [SDR FDEA202602280291](https://openairdocs.org/sdr/FDEA202602280291.md): Safety Wire · wrong part · Feb 28, 2026 · N868FD · Boeing 777FS2 · Emergency Equipment
  > LEFT SLIDE PACKBOARD RELEASE CABLE MECHANISM REQUIRES CAD COPPER SAFETY WIRE. REF FEA G-2560-F0386282 C P1. SAFETIED LT SLIDE PACKBOARD RELEASE CABLE MECHANISH WITH CAD COPPER BREAKAWAY WIRE.
- [SDR FDEA202602230259](https://openairdocs.org/sdr/FDEA202602230259.md): Safety Wire · wrong part · Feb 23, 2026 · N852FD · Boeing 777FS2 · Passenger/Crew Doors
  > FOUND INCORRECT SAFETY WIRE ON L1 DOOR SLIDE. AMM: 25-66-01-4 REPLACED SAFETY WIRE WITH CAD COPPER.
- [SDR FDEA202602200247](https://openairdocs.org/sdr/FDEA202602200247.md): Skin · dented · Feb 20, 2026 · N889FD · Boeing 777FS2 · Trailing Edge Flaps
  > LH WING OB FLAP LOWER SURFACE FROM OB TO IB 97 INCHES CROSS TE TO LE 8 INCHES FOUND ONE DENT. REPAIRED LT WING OB FLAP LOWER SURFACE DENT AT OTEF STA 431 AS PER B777 SRM 57-53-01- 2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4 FIGURE 210 REV 51.0 AND EA
- [SDR FDEA202602180233](https://openairdocs.org/sdr/FDEA202602180233.md): Slide · damaged · Feb 18, 2026 · N859FD · Boeing 777FS2 · Escape Slide
  > R1 DOOR SLIDE REQUIRES CORRECT BREAKAWAY WIRE TO BE INSTALLED ON PACKBOARD RELEASE CABLE. REF F.E.A. G2560-F0386294 C P1. INSTALLED CAD-PLATED COPPER BREAKAWAY WIRE MS20995CY16 ON R1 DOOR SLIDE SERIAL # M10771 PACKBOARD RELEASE CABLE PER F.E.A. WORK CARD IN
- [SDR FDEA202602160217](https://openairdocs.org/sdr/FDEA202602160217.md): Safety Wire · wrong part · Feb 16, 2026 · N858FD · Boeing 777FS2 · Escape Slide
  > LEFT SLIDE ASSY. SN 3359, FOUND BREAK AWAY WIRE SECURES THE RELEASE MECHANISM NOT TO BE CLAD-PLATED COPPER WIRE. RELEASED FOR SERVICE PER MEL: 52-11-01-02 CATEGORY: C EXPIRATION: 22FEB26 "MEL 52-11-01-02: DOOR _L1__ DOOR - INOP. IF SLID E/RAFT TO BE
- [SDR FDEA202602160216](https://openairdocs.org/sdr/FDEA202602160216.md): Safety Wire · wrong part · Feb 16, 2026 · N886FD · Boeing 777FS2 · Escape Slide
  > FOUND L1 DOOR SLIDE SAFETY WIRE NON-COMPATIBLE, NEEDS REPLACING. REPLACED SAFETY WIRE WITH PART NO. MS20995CY16 CAD PLATED COPPER. REF. AMM 25-66-01-4. AC OK FOR SERVICE.
- [SDR FDEA202602160215](https://openairdocs.org/sdr/FDEA202602160215.md): Safety Wire · wrong part · Feb 16, 2026 · N887FD · Boeing 777FS2 · Escape Slide
  > RH SLIDE - REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER SMIS 25-60/5696 (F.E.A.# G-2560-F0386294 C PART 1) RH SLIDE - REPLACE THE BREAKAWAY WIRE SE
- [SDR FDEA202602160214](https://openairdocs.org/sdr/FDEA202602160214.md): Safety Wire · wrong part · Feb 16, 2026 · N887FD · Boeing 777FS2 · Escape Slide
  > LH SLIDE - REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOAR RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER SMIS 25-60/3937 (FEA G-2560-F0386282 C P1). REMOVED AND REPLACED BREAKAWAY WIRE SECURING RELE
- [SDR FDEA202602150211](https://openairdocs.org/sdr/FDEA202602150211.md): Safety Wire · wrong part · Feb 15, 2026 · N890FD · Boeing 777FS2 · Escape Slide
  > WRI TO REPLACE THE R1 DOOR SLIDE WIRE WITH MS20995CY16 WIRE. AMM: 25-66-01-4 REPLACED R1 DOOR SLIDE SHEAR WIRE WITH MS20995CY16 WIRE PER REF ABOVE
- [SDR FDEA202602150204](https://openairdocs.org/sdr/FDEA202602150204.md): Release Cable · wrong part · Feb 15, 2026 · N863FD · Boeing 777FS2 · Escape Slide
  > RIGHT SLIDE PACKBOARD RELAEASE CABLE MECHANISM REQUIRES CAD PLATED COPPER BREAKAWAY WIRE. REF WRI 25-60/4116 FEA 2560-F0386282 C P1. SAFETIED RT SLIDE PACKBOARD RELEASE CABLE MECHANISM WITH CAD PLATED COPPER WIRE.
- [SDR FDEA202602150203](https://openairdocs.org/sdr/FDEA202602150203.md): Slide · fom · Feb 15, 2026 · N863FD · Boeing 777FS2 · Standard Practices/Structures
  > L1 DOOR SLIDE REMOVED FOR F.O.M. OF F.E.A. MOD TYPE F MOD NR G-2560-F0386282 REV NR C PS P1. INSTALLED L1 DOOR SLIDE OPS CHECKS GOOD IAW AMM 25-66-01-4, & AMM 25-66-01-4.
- [SDR FDEA202602140194](https://openairdocs.org/sdr/FDEA202602140194.md): Safety Wire · wrong part · Feb 14, 2026 · N864FD · Boeing 777FS2 · Escape Slide
  > SAFETY WIRE FOUND ON SLIDE WAS NOT THE CORRECT TYPE ACCORDING TO F.E.A.#:G-2560-F0386282 C PART: 1 (P1) REPLACED BREAKAWAY WIRE WITH CORRECT WIRE SPEC (MS20995CY16) THAT SECURES THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD. MP
- [SDR FDEA202602140193](https://openairdocs.org/sdr/FDEA202602140193.md): Safety Wire · wrong part · Feb 14, 2026 · N857FD · Boeing 777FS2 · Escape Slide
  > RIGHT SLIDE, REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER SMIS 25-60/5696 (F.E.A. G-2560-F0386294 C PART 1) CMM: 25-61-31 EA: 9-2560-T0386431 FEA:
- [SDR FDEA202602130192](https://openairdocs.org/sdr/FDEA202602130192.md): Slide · miswired · Feb 13, 2026 · N864FD · Boeing 777FS2 · Escape Slide
  > R1 DOOR SLIDE HAS INCORRECT SAFETY WIRE ON PACKBOARD RELEASE CABLE. INSTALLED PROPER SAFETY WIRE ON R1 SLIDE PACKBOARD RELEASE CABLE IAW B777MM 25-66-01-4. A/C OK FOR SERVICE.
- [SDR FDEA202602120183](https://openairdocs.org/sdr/FDEA202602120183.md): Wire · wrong part · Feb 12, 2026 · N858FD · Boeing 777FS2 · Emergency Equipment
  > FOUND BREAKAWAY WIRE THAT SECURES THE RELEASE MECHANISM NOT TO BE CLAD-PLATED COPPER WIRE. REMOVED LT DOOR SLIDE IAW MM 25-66-01-4. REMOVED STAINLESS SAFETY WIRE AND INSTALLED CORRECT WIRE IAW FEA G-2560-F0386282C. REINSTALLED DOOR SLIDE IAW 25-66-01-4. DO
- [SDR FDEA202602090152](https://openairdocs.org/sdr/FDEA202602090152.md): Skin · cracked · Feb 9, 2026 · N856FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING WORK CARD: EG-5710-E0376285F P12 STEP3.B(1) & 5.A.(2), FOUND TWO CRACKS ON RT UPPER WING SKIN FASTENER NR 5. RIGHT WING UPPER SKIN NR 5 FASTENER HOLE REPAIRED IAW SRM 51-40-05-0G, FIGURE 4, TABLE C, SRM 51-40-02-0G, FIGURE 12, SRM 51-40-04-0G, FIGURE 2
- [SDR FDEA202602090151](https://openairdocs.org/sdr/FDEA202602090151.md): Skin · cracked · Feb 9, 2026 · N856FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING WORK CARD: EG-5710-E0376285F P12 STEP4.B(2).(B), THEN FOUND ONE CRACK ON RT UPPER WING SKIN FASTENER #6 AS MARKED. RIGHT WING UPPER SKIN NR 6 FASTENER HOLE REPAIRED IAW SRM 51-40-05-0G, FIGURE 4, TABLE C, SRM 51-40-02-0G, FIGURE 12, SRM 51-40-04-0G,
- [SDR FDEA202602090150](https://openairdocs.org/sdr/FDEA202602090150.md): Skin · cracked · Feb 9, 2026 · N856FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING WORK CARD: EG-5710-E0376285F P11 STEP4.B(2).(B), THEN FOUND ONE CRACK ON LT UPPER WING SKIN FASTENER NR 6. THE LEFT WING UPPER SKIN #6 FASTENER HOLE CRACKED AREA REPAIRED AS PER B777 SRM 51- 20-07-0G FIGURE 2, SRM 51-50-02-0G FOGURE 1, SRM 51-40-02

Next page: https://openairdocs.org/model/boeing-777-fs2/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 aircraft_model_key = '777FS2'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-777-fs2/reports

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