N993FD

Service difficulty reports · 134

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N993FD' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA202608281248Strut · crackedNR 2 NACELLE STRUT, RIGHT SIDE SKIN, THROUGH ACCESS 443AR, SHOWS A CRACK WITH NO VISIBLE STOP HOLE. THIS ITEM HAS BEEN ACCOMPLISHED ON EA F-5430-T0388382 P1.Aug 28, 2026 · N993FD · Boeing 7572Q8 · Nacelle/Pylon, Main FrameSDR FDEA202608281247Skin · debondedLEFT WING INBD T/E MAIN FLAP, AFT PANEL, REAR EDGE HAD DEBONDING. APPLIED PERMANENT REPAIR ON THE LT WING FLAP AFT PANEL IAW SRM 57-53-01-2R, REP 1, DETAIL I, FIG 201, SHEET 2, IAW IAW SRM 51-70-10-2R, REP 4.Aug 28, 2026 · N993FD · Boeing 7572Q8 · Trailing Edge FlapsSDR FDEA202608261233Strap · crackedON THE LEFT SIDE BS 1640 BTW S-13L AND LOWER HINGE INTERCOSTAL STRAP, A CRACK WAS FOUND IN THE INNER CHORD STRAP; THE CRACK WAS LOCATED AT THE EDGE OF THE SECOND FASTENER HOLE FROM S-13L TO LOWER HINGE INTERCOSTAL WITH A LENGTH OF 0.190 INCHES AT THE 5 OAug 26, 2026 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA202608241221Skin · dentedFUSELAGE BTWN BS 1963.8 - 1992.8 DENTED. APPLIED PERMANENT REPAIR AT BS 1963.8 - 1992.8 IAW SRM 53-80- 01-2R, REP 1, DETAIL I, FIG 201, SHEET 1, & SRM 51-70-10-2R, REP 4.Aug 24, 2026 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA202608241222Crease Beam · corrodedMAIN CARGO BAY BETWEEN BS 860 AND 880, RT CREASE BEAM INBD CHORD CORRODED. R & R INBD CREASE BEAM BTWN BS 760 & 900 RT SIDE IAW SRM 51-40-02-0G, & DWG 143N5520, REV C.Aug 24, 2026 · N993FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA202608201195Beam · crackedVERTICAL STABILIZER REAR SPAR FIN STA:95.00 SUPPORT PANEL 324AL BEAM CRACKED REMOVED AND REPLACED BEAM AT VERTICAL STABILIZER REAR SPAR SUPPORT PANEL 324AL IAW B757 SRM 51-40-02-0G AND DRAWING 173N1300Aug 20, 2026 · N993FD · Boeing 7572Q8 · Vertical Stabilizer Miscellaneous StructureSDR FDEA202301090056Frame · crackedMAINFRAME STA 1640 FUSELAGE FRAME WEB S-14L REQUIRE FRAME REPLACEMENT PER EA F- 5310-T0359452. REPAIRED FRAME IAW EA F-5310-T0359452 PT2. TEMPORARY FREEZE PLUG REPAIR. MAJOR REPAIRJan 9, 2023 · N993FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA202301070048Drag Fitting · gougedDURING ROTO TEST OF HOLE #2 REJECTABLE INDICATIONS OF GOUGING NOTED AT THE 2:00 AND 7:00 POSTION FACING FWD. WINGS - PLATES AND SKINS - RH WING, UPER SKIN AT DRAG FITTING, HOLE 2, CRACK REPAIR THIS EA DEVIATES FROM EO F-5730-E0340076. ACCOMPLISHED STEPS 1Jan 7, 2023 · N993FD · Boeing 7572Q8 · Wing Main, Frame StructureSDR FDEA202212232999Floorboard · damagedZONE 220 FLOORBOARD 221MBF IS DAMAGED. FABRICATED NEW BOARD 11861182-16, 221MBF FROM TRAVELER T22/1651611 IAW DWG SRZ-25- 005 REV R. MAJOR REPAIRDec 23, 2022 · N993FD · Boeing 7572Q8 · Fuselage Floor PanelSDR FDEA202104281056Girt Bar · obstructedL1 DOOR GIRT BAR ENGAGEMENT "SLIDE" LIGHT INOP. GIRT BAR OPERATION NORMAL. REMOVED DEBRIS FROM L1 GRIT BAR AREA AND TESTED THE ARM AND DISARM SLIDE LIGHT INDICATIONS I/A/W AMM 25-66-11-2 PAR. 5, SUB PAR. 11. GND TESTED MULTIPLE TIMES. NO DISCREPANCIES NOTED.Apr 28, 2021 · N993FD · Boeing 7572Q8 · Emergency EquipmentSDR FDEA202103190707Control Unit · malfunctionedBRAKE SOURCE LIGHT ILLUMINATED WHILE ARRIVING IN MEMPHIS ... PASSING 10,000 FT. RAN QRH , DECLARED EMERGENCY , LANDED ... DID NOT TAXI . THE BRAKE SOURCE LIGHT REMAINED ON AFTER SELECTING RESERVE BRAKES. NOTE: PILOT DEBRIEF - ALL HYD. PRESSURES WERE NOMar 19, 2021 · N993FD · Boeing 7572Q8 · Landing Gear Brake SystemSDR FDEA202102120346Line · crackedDEPARTING FROM BFM LANDING GEAR DISAGREE AND GEAR DOOR ON EICAS. ALSO DOORS LIGHT AND NOSE GEAR LIGHT STAYED ON WITH MAIN LEFT AND RIGH GEAR LIGHTS OUT. AFTER ABOUT TWO MINUTES NOSE GEAR LIGHT AND DOORS LIGHT WENT OUT AND LANDING GEAR DISAGREE MESSAGE WEFeb 12, 2021 · N993FD · Boeing 7572Q8 · Hydraulic System, MainSDR FDEA202102120345Line · brokenWHEN EXTENDING FLAPS TO 1 LEADING EDGE SLAT DISAGREE DISPLAYED ON THE EICAS AND FLAP POSITION WAS STUCK BETWEEN UP AND 1. FOLLOWED QRH PROCEDURE AND USED ALTERNATE FLAP EXTENSION TO EXTEND FLAPS TO 20 FOR LANDING. FOUND HYDRAULIC LINE P/N 271N6445-1255 Feb 12, 2021 · N993FD · Boeing 7572Q8 · Hydraulic System, MainSDR FDEA202102090319Frame · crackedBODY STATION 1640 FUSELAGE FRAME WEB AT STRINGER S-14 AT LH. CRACK INDICATION NOTED FOR BOTTOM INBOARD HOLE COMPLIED WITH EA# F-5310-T0359452 P1. FUSELAGE-MAINFRAME-CRACK INDICATION AT STA 1640 FUSELAGE FRAME WEB, S-14L AT LOWER INBOARD HOLE LOCTION- TEMPOFeb 9, 2021 · N993FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA202101060013Switch · damagedAT CRUISE WE RECEIVED AN EICAS MESSAGE LEADING EDGE SLAT ASYM EMERGENCY DECLARED. PER FIM/27-81 F/T 804 FOUND AND WDM 27-81-31. RANG OUT SLAT LOSS SENSING SWITCHES FROM FSEU TEST RECEPTICLE D1251 AND FOUND ALL SWITCHES READING OPEN. FSEU 1 FAULTED SLAT LOSSJan 6, 2021 · N993FD · Boeing 7572Q8 · Leading Edge Slat Control SystemSDR FDEA201907091510Battery Pack · dischargedON PREFLIGHT FOUND LT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED LT BATTERY PACK PER AMM 33-51-07-2. OP'S CHECK GOOD.Jul 9, 2019 · N993FD · Boeing 7572Q8 · Emergency LightingSDR FDEA201902070267Warning System · false activationON FINAL GOT A SLAT DISAGREE LIGHT. RAN QRH, LANDED UNEVENTFULLY USING ALTERNATE FLAP SYSTEM. SLAT DISAGREE LIGHT EXTINGUISHED DURING QRH PROCEDURES. INSPECTED FLAPS AND SLAT AREAS, NO IMMEDIATE DEFECTS NOTICED AT THIS TIME. RESET ALTERNATE FLAP SWITCHES TO NOFeb 7, 2019 · N993FD · Boeing 7572Q8 · Leading Edge Slat Position Indicating SystemSDR FDEA201901200184Intercostal · corrodedCORROSION FOUND @ AFT CARGO COMPT INTERCOSTAL STA 1400-1420 STR 29R-30 FOUND CORR ON INTERCOSTAL IN AFT CARGO STA 1400-1420 STR 29R-30 TO BE OUT OF LIMITS IAW SRM 53-00-04-1A. REMOVED INTERCOSTAL IAW SRM 51-40-02. FABRICATED AND INTALLED NEW INTERCOSTAL IAW DWJan 20, 2019 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201901200185Mount Fitting · corrodedAFT. CARGO COMPT. UPON REMOVAL OF TRANSITION PANEL SECTION FOR REPAIR. FOUND AT BS. 1440, AND STR.27R. CARGO TIEDOWN, MOUNT STRUCTURE FOR TIEDOWN WITH EXFOLIATED CORROSION. FOUND AFT CARGO TIEDOWN MOUNT STRUCTURE CORR. TO BE 100% MAT LOSS OUT OF LIMITS IAW SRMJan 20, 2019 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201901160157Fitting · corrodedUPON REMOVAL OF AFT CARGO COMPT CLIP P/N 146N5422-4 STA 1440 STR 27R FOUND OUT OF LIMITS. FABRICATED LOCATED, DRILLED AND TRIMMED TO FINAL SIZE AFT CARGO COMPT. CLIP STA 1440 STR 27R AS PER DWG 146N5422 REV B & D AND SRM 51-40-05-0G.Jan 16, 2019 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201901160153Intercostal · corrodedAFT CARGO COMPT. BETWEEN BS.1320 AND BS.1340,AND STR 28L.INTERCOSTAL WEB HAS CORROSION. EVALUATED CORROSION AT AFT CARGO COMPT. BETWEEN BS 1320-1340 AND STR 28L INTERCOSTAL. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A FIG 101 REMOVED, FABRICATED AND INSTALLEJan 16, 2019 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201901150135Intercostal · corrodedAFT CARGO COMPT. INTERCOSTAL HAS CORROSION, BETWEEN BS. 1440 AND BS. 1460 AND BETWEEN STR 27R AND STR 26R. REMOVED CORR ON INTERCOSTAL & ANGLE STA 1440 & 1460 STR 26R - 27R IAW SRM 51-10-02. FOUND 100% MAT LOSS OUT OF LIMITS IAW SRM 53-00-04-1A. REMOVED INTERCJan 15, 2019 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201901150134Web · corrodedAFT CARGO COMPARTMENT WEB LOCATED BETWEEN BS 1360 AND 1380 STRINGER 27R HAS CORROSION. AFT CARGO COMPARTMENT WEB STA 1360-1380 - STR 27R HAS COROSION. FOUND CORROSION 100% OUT OF LIMITS IAW SRM 53-60-04-1A AND 53-00-04-1A FIG 1 DETAIL II, FABRICATED, LOCATED AJan 15, 2019 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201901150133Support Angle · corrodedAFT CARGO COMPARTMENT SUPPORT ANGLE AT STA 1380 STR 27R ELONGATED HOLES. FORMED NEW SUPPORT ANGLE (CHANNEL), TRIMMED, LOCATED AND DRILLED IAW DRWG 146N8522 REV E, TREATED AND PRIMED, TOP COAT IAW SRM 51-20-01-0G AND AMM 51-21-10-07.Jan 15, 2019 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201901100071Shear Tie · corrodedAFT CARGO COMPT. AT BS.1380,AND STR .28R. SHEARTIE HAS EXFOLIATED CORROSION. DOT 24/042 ACCOMPLISHED WITH E.A F-5310-T0344528 P1 TITLE: FUSELAGE-MAINFRAME-STA 1380 FRAME OUTER CHORD PARTIAL REPLACEMENT AND SPLICE REPAIR BETWEEN S-26R AND S29R.Jan 10, 2019 · N993FD · Boeing 7572Q8 · Fuselage Internal Mounting StructureSDR FDEA201901070043Skin · gougedLT. WING T/E AFT FLAP 36" FROM O/B END LOWER SURF. IS GOUGED REPAIRED LT. WING GOUGE AT T/E AFT FLAP 36" FROM O/B END LOWER SURFACE IAW SRM 51-70-04-0G (PARA 5.B) & 51-70-17-0G (PARA 3.G) AND EA T F-5750-T0344477 P1 WING- FLIGHT SURFACES- LT OUTBOARD AFT FLAP Jan 7, 2019 · N993FD · Boeing 7572Q8 · Trailing Edge FlapsSDR FDEA201901040016Seat Track · corrodedSUPERNUMERARY SEAT TRACK SHOWS EVIDENCE OF CORROSION FWD OF THE 9G BULKHEAD IN THE VESTUBULE LBL 05. REMOVED CORROSION ON SEAT TRACK AT STA 345 TO 377, LBL 5 IAW SRM 51-10-02-0G. EVALUATED DAMAGED AREA, ORIG. MAT=.070", REM MAT=.046", MAT LOSS=.024" FOUND TO BJan 4, 2019 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201901040015Seat Track · corrodedSUPERNUMERARY SEAT TRACK SHOWS EVIDENCE OF CORROSION FWD OF THE 9G BULKHEAD IN THE VESTUBLUE RBL 12 REMOVED CORROSION ON SEAT TRACK AT STA 345 TO 377, RBL 12 IAW SRM 51-10-02-0G. EVALUATED DAMAGED AREA,ORIG. MAT=.070",REM MAT=.055",MAT LOSS=.015" FOUND TO BE OJan 4, 2019 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201901030013Crease Beam · corrodedCABIN BS 1620 LBL 55 SIDE ANGLE HAS A LARGE SPOT OF CORROSION. REMOVED CORROSION ON MAIN CABIN, ANGLE (CREASE BEAM) BS 1620 LBL 65 IAW SRM 51-10-02-0G. EVALUATED DAMAGED AREA FOUND TO BE OUT OF LIMITS, IAW SRM 53-60-13-1A FIG 101 DETAL VIII. REMOVED DAMAGED CRJan 3, 2019 · N993FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA201709202658Fseu · malfunctioned25 MINUTES AFTER TAKE OFF AT FL 370, CAUTION EICAS FOR LE SLAT ASYM, NO VIBRATION, NO CHANGE ON FLAP GAUGE, FOLLOWED QRH . NO ROLL OR VIBRATION DURING CONFIGURATION. DECLARED AN EMERGENCY. REMOVED AND REPLACED THE NR 2 FSEU IAW AMM 27-51-01-2, OK FOR SSep 20, 2017 · N993FD · Boeing 7572Q8 · Leading Edge Slat Control SystemSDR FDEA201612174486Strut · damagedLEFT PYLON ABOVE FWD ENGINE MOUNT INSIDE FWD ACCESS PANEL HAS SEVERAL OPEN HOLES ON BOTH SIDES. COMPLIED WITH EA # F-5430-TO330415 P1, DRILLED & INSTALLED FASTENERS. MAJOR REPAIR.Dec 17, 2016 · N993FD · Boeing 7572Q8 · Nacelle/Pylon, Main FrameSDR FDEA201612084362Door Frame · crackedR-2 DOOR UPPER HINGE CUTOUT INNER CHORD OF THE DOOR FRAME CRACKED. REPAIRED IAW SRM 52-10-02-2R DETAIL III FIG.201.Dec 8, 2016 · N993FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201604071177Lanyard · out of positionRIGHT CREW DOOR SLIDE WILL NOT ARM. RE-STOWED R1 DOOR SLIDE CORDS IAW AMM 52-11-00-5-0. SYS OPERATIONS CHECKED GOOD.Apr 7, 2016 · N993FD · Boeing 7572Q8 · Emergency EquipmentSDR FDEA201507042152Oxygen Box · leakingCAPTAIN`S OXYGEN PRESS TO TEST DOOR BROKEN. COURIER OXYGEN MASK INOPERATIVE. SWAPPED NR 3 COURIER POSITION OXYGEN STOWAGE BOX TO CAPTAIN`S POSITION TO MAKE CAPTAINS POSITION SERVICEABLE IAW AMM 35-11-51-4-99. REMOVED AND REPLACED THE COURIER NR 3 OXYGEN MASJul 4, 2015 · N993FD · Boeing 7572Q8 · Crew Oxygen SystemSDR FDEA201503050688Latch · damagedCAPTAIN ESCAPE ROPE DOOR WILL NOT STAY SHUT. LATCH APPEARS TO BE BROKEN. LATCH BASE IS BROKEN ON INSIDE OF SIDEWALL PANEL. THE UPPER EAR FOR THE MOUNTING OF THE BUTTON LATCH IS MISSING & BROKEN OFF. REMOVED TWO RIVETS AND OLD LATCH "STRIKER" BASE. INSTALLMar 5, 2015 · N993FD · Boeing 7572Q8 · Emergency EquipmentSDR FDEA201412124116Closeout Panel · dentedMAIN CARGO DOOR, FWD PRESSURE RELIEF DOOR CLOSEOUT PANEL IS GOUGED. REMOVED DAMAGED CLOSEOUT PANEL, FABRICATED NEW CLOSEOUT PANEL, AND INSTALLED IAW SRM 51-40-02, SRM 52-30-02 FIG 101, DRAWING 65-49309 REV A, SRM 51-40-05, SRM 51-20-01, AND SRM 51-40-02 .Dec 12, 2014 · N993FD · Boeing 7572Q8 · Cargo/Baggage DoorsSDR FDEA201412114103Skin · dentedFUSELAGE DENTED AT BS 761 JUST BELOW STRINGER 17L. REPAIRED IAW SRM 53-00-01 REPAIR 16. MAJOR REPAIR.Dec 11, 2014 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201406111410Wedge · damagedNUMBER 10 SLAT TE WEDGE UPPER SURFACE HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 10 SLAT ASSEMBLY IAW AMM 27-81-02. ADJUSTMENT TEST GOOD IAW AMM 27-81-02-4.Jun 11, 2014 · N993FD · Boeing 7572Q8 · Leading Edge DevicesSDR FDEA201406101392Skin · damagedRIGHT WING INBD FLAP UPPER SURFACE HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R RT INBD MAIN FLAP IAW AMM 27-51-02 401. ADJUSTED RT INBD TE FLAP IAW AMM 27-51-12-5. PERFORMED POST INSTALLATION TEST IAW AMM 27-51-02-5, CHECKED GOOD.Jun 10, 2014 · N993FD · Boeing 7572Q8 · Trailing Edge FlapsSDR FDEA201406101391Skin · damagedLEFT WING INBD FLAP UPPER SURFACE HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R LT INBD MAIN FLAP IAW AMM 27-51-02 401. ADJUSTED LT INBD TE FLAP IAW AMM 27-51-02-5. PERFORMED POST INSTALLATION TEST IAW AMM 27-51-020-5 CHECKED GOOD.Jun 10, 2014 · N993FD · Boeing 7572Q8 · Trailing Edge FlapsSDR FDEA201406071351Wedge · damagedNUMBER 7 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 7 SLAT IAW AMM 27-81-02 ADJUSTMENT TEST GOOD IAW AMM 27-81-02-4.Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge DevicesSDR FDEA201406071350Wedge · damagedNUMBER 9 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 9 SLAT IAW AMM 27-81-02 ADJUSTMENT TEST GOOD IAW AMM 27-81-02-4.Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge DevicesSDR FDEA201406071349Wedge · damagedNUMBER 8 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 8 SLAT ASSEMBLY IAW AMM 27-81-02 ADJUSTMENT TEST GOOD IAW AMM 27-81-02-4.Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge DevicesSDR FDEA201406071348Skin · damagedLEFT HORIZONTAL STAB FWD UPPER SKIN HAS NUMEROUS HAIL DAMAGE ADJACENT TO PNLS 332BL, 332CL & 332DL. REPAIRED DENTS BY FILLING & FAIRING IAW EA F5510-T0308665.Jun 7, 2014 · N993FD · Boeing 7572Q8 · Horizontal Stabilizer, Plate/SkinSDR FDEA201406071347Wedge · damagedNUMBER 6 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 6 SLAT ASSEMBLY IAW AMM-27-81-02, ADJUSTMENT TEST GOOD IAW AMM-27-81-02-4, CAT A MAJOR REPAIR.Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge DevicesSDR FDEA201406071346Wedge · damagedNUMBER 6 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 6 SLAT ASSEMBLY IAW AMM-27-81-02, ADJUSTMENT TEST GOOD, IAW AMM-27-81-02-4, CAT A MAJOR REPAIR.Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge DevicesSDR FDEA201406071345Wedge · damagedNUMBER 5 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 5 SLAT ASSEMBLY IAW AMM-27-81-02, ADJUSTMENT & TEST GOOD, IAW AMM-27-81-02-4, CAT A MAJOR REPAIR.Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge DevicesSDR FDEA201406071344Skin · damagedRIGHT HORIZONTAL STAB FWD UPPER SKIN HAS NUMEROUS HAIL DAMAGE ADJACENT TO PNLS 342BR, 342CR & 342DR. SANDED, CLEANED & APPLIED CONVERSION COATING IAW EA F5510-T0308665 & SRM 51-70-01.Jun 7, 2014 · N993FD · Boeing 7572Q8 · Horizontal Stabilizer, Plate/SkinSDR FDEA201406071343Wedge · damagedNUMBER 4 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 4 SLAT ASSEMBLY IAW-AMM-27-81-02, ADJUSTMENT TEST GOOD IAW AMM-27-81-02-4, CAT A MAJOR REPAIR.Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge DevicesSDR FDEA201406071342Wedge · damagedNUMBER 3 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 3 SLAT ASSEMBLY IAW AMM-27-81-02, ADJUSTMENT TEST GOOD IAW AMM-27-81-02-4, CAT A MAJOR REPAIR.Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge Devices
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