Boeing 777-FS2

Service difficulty reports · 693

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '777FS2'
  ORDER BY difficulty_date DESC"

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SDR FDEA202602090152Skin · crackedDURING 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 2Feb 9, 2026 · N856FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202602090151Skin · crackedDURING 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, Feb 9, 2026 · N856FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202602090150Skin · crackedDURING 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 51-40-02Feb 9, 2026 · N856FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202602090149Skin · crackedDURING WORK CARD: EG-5710-E0376285F P11 STEP3.B.(1) & 5.A.(2) THE FOUND TWO CRACKS ON LT UPPER WING SKIN FASTENER NR 5. THE LEFT WING UPPER SKIN NR 5 FASTENER HOLE CRACKED AREA REPAIRED IAW SRM 51- 20-07-0G, FIGURE 2, SRM 51-50-02-0G, FIGURE 1, SRM 51-40-02-0Feb 9, 2026 · N856FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202602080223Safety Wire · wrong partREMOVE RH DOOR SLIDE FOR FEA INSPECTION OF PROPER CAD PLATED COPPER SAFETY WIRE MS20995CY16. REMOVED R1 DOOR SLIDE IN REF TO 777 AMM. SLIDE WAS REMOVED DUE TO THE WRONG WIRE INSTALLED ALSO THE TOP LEVER LATCH CLIP DAMAGED. 10 MAN LIFE RAFT INSTALLED. AMMFeb 8, 2026 · N869FD · Boeing 777FS2 · Escape SlideSDR FDEA202602010111Light · no testDURING PREFLT, EMERGENCY LIGHT TEST IN GALLEY, SMALL SQUARE LIGHT ABOVE L1 DID NOT ILLUMINATE IAW TEST REQUIREMENTS. REPLACED SMALL SQUARE LIGHT (AREA LIGHT) ASSY ABOVE L1 DOOR PER REFERENCE ABOVE. EMERGENCY LIGHT TEST OK. VERIFIED SMALL SQUARE LIGHT ILLUFeb 1, 2026 · N886FD · Boeing 777FS2 · Emergency LightingSDR FDEA202601220080Skin · dentedFOUND RT WWING T/E OTBD FLAP LOWER SURFACE DENT 1EA AT THE CROSS OTEF 335 AND T/E 2 INCHS. REPAIRED RHW T/E O/B FLAP LOWER SURFACE DENT 1EA AT THE CROSS OTEF 335 AND T/E 2 INCHES AS PER B777 SRM 57-53-01-2R-2 FIGURE 203 AND SRM 51-70-04-2R-1 REV 51.0 AND Jan 22, 2026 · N857FD · Boeing 777FS2 · Trailing Edge FlapsSDR FDEA202601220078Fitting · crackedFOUND RH WING NR 11 SLAT L/E UPPER SKIN 1 EA BULGE AT THE O/B MAIN TRACK FITTING AREA. RH WING NO.11 SLAT L/E UPPER SKIN BULGE AREA REPAIRED AS PER B777 SRM 57-43-01-2R REPAIR 9 FIG 202 REV:51.0 AND EA G-5750-T0386209 P1. TITLE:WING-FLIGHT SURFACES-RH WING Jan 22, 2026 · N857FD · Boeing 777FS2 · Leading Edge DevicesSDR FDEA202601210077Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285E P12 STEP 3.B.& STEP5 A.(2) THEN FOUND TWO CRACKS ON RT UPPER WING SKIN FASTENER NR 5. RT WING UPPER SKIN FASTENER HOLE REPAIRED IAW SRM 51-50-02-0G, FIGURE 1, SRM 51-40-02-0G, FIGURE 12, SRM 51-20-07-0G, FIGURE 1, SRJan 21, 2026 · N857FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202601210076Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285F P12 STEP4. B. (2). (B). THEN FOUND TWO CRACKS ON RT UPPER WING SKIN FASTENER NR 6. RT WING UPPER SKIN NR 6 CRACKED FASTENER HOLE REPAIRED IAW SRM 51-50-02-0G, FIGURE 1, SRM 51-40-02-0G, FIGURE 12, SRM 51-20-07-0GJan 21, 2026 · N857FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202601200074Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL 241SF (P/N 152W8601-7) DAMAGED AT STA 1450 LBL 2. MAIN DECK FLOOR PANEL 241SF (P/N 152W8601-7) CRACKED AT STA 1450 LBL 2 DAMAGE SIZE: L= 0.8" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 FIGURE Jan 20, 2026 · N857FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202601200073Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL 241LF DAMAGED AT BS 1300, LBL 45. FLOOR PANEL 241LF DAMAGED: L= 1", DAMAGE OUT OF ALLOWABLE LIMIT IAW SRM 53-00-50-1A, ALLOWABLE DAMAGE 1, FIGURE 101-106, REV 51. REPAIRED IAW SRM 53-00-50-2R, REPAIR 1, FIGURE 201-202, REV 51.Jan 20, 2026 · N857FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202601200072Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL 241QF (P/N 152W8402-21) DAMAGED AT STA 1400 LBL 45. MAIN DECK FLOOR PANEL 241QF (P/N 152W8402-21) CRACKED AT STA 1400 LBL 45 DAMAGE SIZE: L= 1.2" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 FIGUJan 20, 2026 · N857FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202601200071Skin · damagedNUMBER 7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS184 SCREW HOLE FOUND ELONGATE. NR 7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS 184 ELONGATE SCREW HOLE REPAIRED IAW SRM 57-43-01-2R REPAIR 6, FIG 203, REV: 51.0 AND EA G-5750-T0386196 P1, MAJOR REPAIR IJan 20, 2026 · N857FD · Boeing 777FS2 · Leading Edge DevicesSDR FDEA202601200070Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285F P11 STEP3. B. (1). & STEP5 A. (2), THEN FOUND 02EA CRACKS ON LH UPPER WING SKIN FASTENER #5 AS MARKED. THE LEFT WING UPPER SKIN #5 FASTENER CRACKED HOLE REPAIRED IAW SRM 51-50- 02-0G, FIGURE 1, SRM 51-40-02-0G, FIGUJan 20, 2026 · N857FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202512052223Lamp · no testPRE-FLT MX INSP, L1 DOOR OVRHD EMERGENCY LIGHT INOP. REPLACED THE LAMP, IAW AMM 33-50-00-2. EMERGENCY LIGHTS TEST SATIS, ITEM OK FOR SVC.Dec 5, 2025 · N892FD · Boeing 777FS2 · Emergency LightingSDR FDEA202512042219Lamp · inoperativeEMERGENCY LIGHT OVERHEAD DOOR 1L INOPERATIVE. REPLACED THE LAMP OF EMERGENCY AREA LIGHT OVERHEAD DOOR 1L REF AMM 33-51-03-2 , TEST NORMAL. A/C OK TO CONTINUE.Dec 4, 2025 · N851FD · Boeing 777FS2 · Emergency LightingSDR FDEA202511232199Modulating Valve · failedDURING DESCENT, FLIGHT DECK TEMP EXCESSIVELY COLD. RAN ECL CABIN TEMP COLD CHECKLIST WITHOUT IMPROVEMENT. DESCENDED FOR MANUAL VENTILATION. FLIGHT DECK TEMP REACH 15C AND TRIM AIR/COCKPIT AIR STILL FULL COLD. AMM: 21-61-02-4 FIM: 21-22-00-2/803 NOTE THNov 23, 2025 · N895FD · Boeing 777FS2 · Heating SystemSDR FDEA202511202194Switch · malfunctionedWHEN EMERGENCY LIGHTS SWITCH COVER IS CLOSED, THE EMERGENCY LIGHTS ARE NOT AUTOMATICALLY ARMED BY THE SWITCH COVER AND STAY IN THE OFF POSITION. MUST MANUALLY ARM SWITCH AND THEN CAREFULLY CLOSE COVER TO ENSURE LIGHTS ARE ARMED. CHECKED SWITCH FUNCTION NORMNov 20, 2025 · N869FD · Boeing 777FS2 · Emergency LightingSDR FDEA202511052126Skin · damagedFOUND A LIGHTNING STRIKE DAMAGE AT RUDDER LH SURFACE AT RUD STA 487 & 4" FWD OF RUDDER TRAILING EDGE. REPAIRED A LIGHTNING STRIKE DAMAGE AT RUDDER LH SURFACE AT RUD STA 487 AS PER B777 SRM 55-40-01-2R-1 FIGURE 202, SRM 51-70-04-2R-1 FIGURE 201, SRM 51-6Nov 5, 2025 · N886FD · Boeing 777FS2 · Rudder, Plate/SkinSDR FDEA202510101945Skin · wornNUMBER 7 SLAT OUTER SKIN FASTENER HOLE FOUND WORN OUT AT ISS 184. NR 7 SLAT OUTER SKIN FASTENER HOLE AT ISS 184 REPAIRED IAW SRM 57-43-01-2R, REPAIR 6, FIGURE 203, REV 51, & EA G-5750-T0385264 P1, MAJOR REPAIR IAW GMM 6-2-100.Oct 10, 2025 · N887FD · Boeing 777FS2 · Leading Edge DevicesSDR FDEA202510081920Skin · crackedDURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF LT WING UPPER SKIN COMMON TO FASTENERS 0-5, FOUND ONE CRACK AT 6 O'CLOCK ON HOLE NR 5. NR 5 HOLE AT LT WING UPPER SKIN RIB BAY 10 TRAILING EDGE WAS REPAIRED IAW SRM 51-40-05-0G, 51-40-02-0G, 51-40-04-0G, REV 5Oct 8, 2025 · N887FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202510081918Skin · crackedDURING PERFORMANCE OF UT &OPEN HOLE HFEC INSPECTION OF RT WING UPPER SKIN COMMON TO FASTENERS 0-5 & FOUND TWO CRACKS AT 6 O'CLOCK & 12 O'CLOCK ON HOLE NR 5. NR 5 HOLE AT RT WING UPPER SKIN RIB BAY 10 TRAILING EDGE REPAIRED IAW SRM 51-40-05-0G, 51-40-02-0G, 5Oct 8, 2025 · N887FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202509231776Spring · damagedWHILE CLOSING DOOR 1L, AN INTERIOR SPRING BROKEN. REMOVED AND REPLACED 2 EACH SPRINGS ON VENT DOOR ASSY IAW AMM 52-11-04-4-0.Sep 23, 2025 · N884FD · Boeing 777FS2 · Passenger/Crew DoorsSDR FDEA202508261542Lamp · no testON ARRIVAL FOUND DOOR 1L INTERIOR FWD EMERGENCY LIGHT NO FULLY ILLUMINATED DURING GROUND TEST. AMM 33-51-01-2 RELAMPED DOOR 1L INTERIOR FWD EMERGENCY EXIT SIGN PER ABOVE REFERENCE. 2X LAMPS MPN 925007-1 REPLACED.Aug 26, 2025 · N863FD · Boeing 777FS2 · Emergency LightingSDR FDEA202508201514Skin · crackedUT&OPEN HOLE HFEC INSPECTION ON THE RIGHT WING UPPER WING SKIN COMMON TO FASTENERS 0-6 AND FOUND 02EA CRACK ON THE HOLE #5. RIGHT WING UPPER WING SKIN #5 HOLE CRACK REPAIRED AS PER B777 SRM51-50-02- 0G,SRM51-40-02-0G,SRM51-20-05-0G,SRM51-10-01-0G,SRM51-20-0Aug 20, 2025 · N853FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202508181496Power Supply · no test2 EMERGENCY LIGHTS IN COURIER AREA ABOVE R1 ARE INOP. ONE INOPERATIVE LIGHT LOCATED ABOVE GALLEY AREA, SECOND INOPERATIVE LIGHT LOCATED NEAR R1 DOOR. AMM: 33-51-06-2, AMM: 33-51-00-5. REPLACED RIGHT POWER SUPPLY PER AMM 33-51-06-2, ACCOMPLISHED EMERGENCY Aug 18, 2025 · N855FD · Boeing 777FS2 · Emergency LightingSDR FDEA202508171484Skin · dentedLEFT OTBD FLAP LWR SURFACE FROM IB TO OB 40 INCHES CORSS TE TO LE 12 INCHES FOUND ONE DENT. REPAIRED LH OB FLAP LWR SURFACE DENT AT OTEF STA 73 AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1 REV 47.6 AND EA: G-5750-T0384564 PI, TITLE: WIAug 17, 2025 · N853FD · Boeing 777FS2 · Trailing Edge FlapsSDR FDEA202508171483Skin · dentedLEFT OTBD FLAP LWR SURFACE FROM OB TO IB 93 INCHES CORSS TE TO LE 4 INCHES FOUND ONE DENT. REPAIRED LH OB FLAP LWR SURFACE DENT AT OTEF STA 434 AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1 REV 47.6 AND EA: G-5750-T0384564 PI, TITLE: WIAug 17, 2025 · N853FD · Boeing 777FS2 · Trailing Edge FlapsSDR FDEA202508171482Skin · dentedFOUND RHW T/E O/B FLAP LOWER SURFACE 01 EA DENT AT THE CROSS OTEF 428 AND T/E 4 INCHES. REPAIRED RHW T/E O/B FLAP LOWER SURFACE 01 EA DENT AT OTEF STA 428 AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1 REV 47.6 AND EA:G-5750-T0384565 P1Aug 17, 2025 · N853FD · Boeing 777FS2 · Trailing Edge FlapsSDR FDEA202508171481Skin · dentedFOUND RHW T/E O/B FLAP LOWER SURFACE 01EA DENT AT THE CROSS OTEF 127 AND T/E 01 INCHES. REPAIRED RHW T/E O/B FLAP LOWER SURFACE 01EA DENT AT OTEF STA 127 AS PER B777 SRM 57- 53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1 REV 47.6 AND EA: G-5750-T0384565 P1 , Aug 17, 2025 · N853FD · Boeing 777FS2 · Trailing Edge FlapsSDR FDEA202508171480Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N: 152W8302-33 FOUND CRACKED AT STA 1010 LBL 85 - LBL 113. MAIN DECK CARGO FLOOR PANEL P/N:152W8302-33 CRACKED AT STA 1010 LBL 85 -LBL 113. DAMAGE SIZE:(1) L=3.4"; (2) L=2.8"; (3) L=2.2" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B7Aug 17, 2025 · N853FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202508171479Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N: 152W8302-34 FOUND CRACKED AT STA 1010 RBL 85. MAIN DECK CARGO FLOOR PANEL P/N:152W8302-34 CRACKED AT STA 1010 RBL 85. DAMAGE SIZE: L=2.8", DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 FIGURE Aug 17, 2025 · N853FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202507121185Floor Panel · crackedREWORK: MAIN DECK CARGO FLOOR PANEL P/N:152W8302-33 FOUND CRACKED AT STA1010 LBL85. MAIN DECK CARGO FLOOR PANEL P/N:152W8302-33 CRACKED AT STA1010 LBL85 DAMAGE SIZE: L=3.5" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLWABLE DAMAGE 1 FIGJul 12, 2025 · N851FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202507111177Floor Support · corrodedMAIN DECK CARGO FLOOR FITTING FOUND CORROSION AT STA1434 RBL40. MAIN DECK CARGO FLOOR FITTING CORROSION AT STA1434 RBL40 REMOVED AND EVALUATED: THE REWORKED AREA AT ZONE "B", THE MAX ALLOWABLE BLEND OUT IS 0.030", THE MAX CLEAN UP DEPTH IS X=0.092", FOUND Jul 11, 2025 · N851FD · Boeing 777FS2 · Fuselage Miscellaneous StructureSDR FDEA202507101167Fitting · corrodedMAIN DECK CARGO FLOOR FITTING FOUND CORROSION AT STA 1393 LBL6.5 MAIN DECK CARGO FLOOR FITTING CORROSION AT STA 1393 LBL6.5 REMOVED AND EVALUATED : THE REWORKED AREA AT ZONE "C", THE MAX ALLOWABLE BLEND OUT IS 0.002". THE MAX CLEAN UP DEPTH IS X = 0.033", Jul 10, 2025 · N851FD · Boeing 777FS2 · Fuselage Miscellaneous StructureSDR FDEA202507101166Fitting · corrodedMAIN DECK CARGO FLOOR FITING FOUND CORROSION AT STA1393 RBL6.5. MAIN DECK CARGO FLOOR FITTING CORROSION AT STA 1393 RBL6.5 REMOVED AND EVALUATED : THE REWORKED AREA AT ZONE "C", THE MAX ALLOWABLE BLEND OUT IS 0.002". THE MAX CLEAN UP DEPTH IS X = 0.022", FJul 10, 2025 · N851FD · Boeing 777FS2 · Fuselage Main, Attach FittingsSDR FDEA202507061125Skin · delaminatedLH WING OB FLAP LWR SURFACE FROM IB TO OB 20 INCH CROSS TE TO LE 5 INCH FOUND DELAMINATION.Jul 6, 2025 · N851FD · Boeing 777FS2 · Trailing Edge FlapsSDR FDEA202507041114Skin · crackedMFEC INSPECTION OF THE OUTBOARD SLAT NO.10 OUTER SKIN DETECTED 1EA FASTENER WITH TWO CRACKS, APPROXIMATELY 4MM AND 6MM IN LENGTH RESPECTIVELY. RH WING NO.10 SLAT OUTER SKIN CRACK AREA REPAIRED AS PER B777 SRM 57-43-01-2R REPAIR 9 FIG 202 REV47.6 AND EA GJul 4, 2025 · N851FD · Boeing 777FS2 · Leading Edge DevicesSDR FDEA202507041113Skin · bulgedRH WING NO.11 SLAT OUTER SKIN FOUND BULGE AT 28-33 INCH TO OB EDGE. RH WING NO.11 SLAT OUTER SKIN BULGE AREA REPAIRED AS PER B777 SRM 57-43-01-2R REPAIR 9 FIG 202 REV 47.6 AND EA G-5750-T0384008 P1. TITLE : WING - FLIGHT SURFACES - RH WING #11 SLAT OUTER SJul 4, 2025 · N851FD · Boeing 777FS2 · Leading Edge DevicesSDR FDEA202507031101Skin · crackedDURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF THE LEFT UPPER WING SKIN COMMON TO FASTENERS 0-5 AND FOUND 02EA CRCAK AT HOLE #5. LEFT WING UPPER SKIN #5 HOLE 02EA CRACKS REPAIRED AS PER B777 SRM 51-40-05-0G, SRM 51-40-04-0G, SRM 51-40-02-0G REV47.6 AND EJul 3, 2025 · N851FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202507031100Skin · crackedDURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF THE RIGHT UPPER WING SKIN COMMON TO FASTENERS 0-5 AND FOUND 02EA CRCAK AT HOLE #5. RIGHT WING UPPER SKIN #5 HOLE 02EA CRACKS REPAIRED AS PER B777 SRM 51-40-02-0G, SRM 51-40-04-0G, SRM 51-40-05-0G REV47.6 ANDJul 3, 2025 · N851FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202507021098Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8302-33 CRACKED AT STA1010 LBL85 DAMAGE SIZE:L=3.5" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 FIGURE 101-106 REV 47.6 AND REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1 FIGURE 201-20Jul 2, 2025 · N851FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202507011144Warning Light · false activationAFTER BLOCK OUT, EMER LIGHTS ICAS ALERT ILLUMINATED. WORKED WITH MANT. TURNED EMER LIGHT ARMING SWITCH TO OFF. CYCLE FLIGHT ATTENDANT EMER LIGHT SWITCH AND REARMED THE EMER SWITCH IN COCKPIT. ICAS CLEARED GMM 6-3-100 AT 37,127:43 HOUR(S), 6,163 CYCLEJul 1, 2025 · N869FD · Boeing 777FS2 · Emergency LightingSDR FDEA202506120926Fan · faultedABOUT 1:30 INTO FLIGHT RECEIVED EQUIP COOLING FAN R STATUS MESSAGE. ABOUT 10 MINUTES AFTERWARD FUMES WERE PRESENT IN THE COCKPIT. DONNED O2 AND RAN THE SMOKE, FIRE, OR FUMES CHECKLIST. FUMES SLOWLY DISSIPATED DURING THE CHECKLIST. EMERGENCY DECLARED AND Jun 12, 2025 · N860FD · Boeing 777FS2 · Air Distribution FanSDR FDEA202506100881Skin · nickedFOUND A NICK AT RH LOWER FWD FUSELAGE SKIN AT STA 518.5 S-47R. A NICK AT RH LOWER FWD FUSELAGE SKIN AT STA 518.5 S-47R REPAIRED AS PER B777 SRM 53-00- 01-2R REPAIR 3 FIGURE 202 REV 47.5. THIS IS A CATEGORY B REPAIR PER B777 SRM 53-00-01-2R REPAIR 3 REV 47.5Jun 10, 2025 · N852FD · Boeing 777FS2 · Fuselage Main, Plate/SkinSDR FDEA202506060845Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8302-31 FOUND CARCKED AT STA1010 LBL85. DAMAGE SIZE:L=4.5" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 REV 47.5 AND REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1 REV 47.5.THIS IS A MAJOR RJun 6, 2025 · N852FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202506060844Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8302-34 FOUND CRACKED AT STA 1010 RBL85. MAIN DECK CARGO FLOOR PANEL P/N:152W8302-34 CRACKED AT STA 1010 RBL 85.DAMAGE SIZE:L=4.9" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 REV 47.5 ANDJun 6, 2025 · N852FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202506060843Skin · dentedLEFT WING OTBD FLAP LOWER SKIN FOUND DENT AT 300 MM FROM T/E AND 1700 MM FROM INBOARD SIDE OF FLAP. REPAIRED LH WING OTBD FLAP LOWER SKIN DENT AT 300MM FROM T/E AND 1700MM FROM INBOARD SIDE OF FLAP AS PER B777 SRM 57-53-01-2R-2 & SRM 51-70-04-2R-1 REV 47.5 AJun 6, 2025 · N852FD · Boeing 777FS2 · Trailing Edge FlapsSDR FDEA202506060842Skin · dentedRIGHT WING OB FLAP LWR SURFACE FOUND MATERIAL MISSING AT 305 IN TO IB AND 3 IN TO AFT EDGE. REPAIRED RH WING OB FLAP LWR SURFAE MATERIAL MISSING AT 305 IN TO IB AND 3 IN TO AFT EDGE AS PER B777 SRM 57-53-01-2R-2 & SRM 51-70-04-2R-1 REV 47.5 AND EA:G-5750-TJun 6, 2025 · N852FD · Boeing 777FS2 · Trailing Edge Flaps
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