# Service difficulty reports: N993FD

A list on [N993FD](https://openairdocs.org/aircraft/N993FD.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 · 134 reports

- [SDR FDEA202608281248](https://openairdocs.org/sdr/FDEA202608281248.md): Strut · cracked · Aug 28, 2026 · N993FD · Boeing 7572Q8 · Nacelle/Pylon, Main Frame
  > NR 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.
- [SDR FDEA202608281247](https://openairdocs.org/sdr/FDEA202608281247.md): Skin · debonded · Aug 28, 2026 · N993FD · Boeing 7572Q8 · Trailing Edge Flaps
  > LEFT 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.
- [SDR FDEA202608261233](https://openairdocs.org/sdr/FDEA202608261233.md): Strap · cracked · Aug 26, 2026 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous Structure
  > ON 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 O
- [SDR FDEA202608241221](https://openairdocs.org/sdr/FDEA202608241221.md): Skin · dented · Aug 24, 2026 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/Skin
  > FUSELAGE 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.
- [SDR FDEA202608241222](https://openairdocs.org/sdr/FDEA202608241222.md): Crease Beam · corroded · Aug 24, 2026 · N993FD · Boeing 7572Q8 · Fuselage Main, Structure
  > MAIN 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.
- [SDR FDEA202608201195](https://openairdocs.org/sdr/FDEA202608201195.md): Beam · cracked · Aug 20, 2026 · N993FD · Boeing 7572Q8 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL 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 173N1300
- [SDR FDEA202301090056](https://openairdocs.org/sdr/FDEA202301090056.md): Frame · cracked · Jan 9, 2023 · N993FD · Boeing 7572Q8 · Fuselage Main, Frame
  > MAINFRAME 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 REPAIR
- [SDR FDEA202301070048](https://openairdocs.org/sdr/FDEA202301070048.md): Drag Fitting · gouged · Jan 7, 2023 · N993FD · Boeing 7572Q8 · Wing Main, Frame Structure
  > DURING 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 1
- [SDR FDEA202212232999](https://openairdocs.org/sdr/FDEA202212232999.md): Floorboard · damaged · Dec 23, 2022 · N993FD · Boeing 7572Q8 · Fuselage Floor Panel
  > ZONE 220 FLOORBOARD 221MBF IS DAMAGED. FABRICATED NEW BOARD 11861182-16, 221MBF FROM TRAVELER T22/1651611 IAW DWG SRZ-25- 005 REV R. MAJOR REPAIR
- [SDR FDEA202104281056](https://openairdocs.org/sdr/FDEA202104281056.md): Girt Bar · obstructed · Apr 28, 2021 · N993FD · Boeing 7572Q8 · Emergency Equipment
  > L1 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.
- [SDR FDEA202103190707](https://openairdocs.org/sdr/FDEA202103190707.md): Control Unit · malfunctioned · Mar 19, 2021 · N993FD · Boeing 7572Q8 · Landing Gear Brake System
  > BRAKE 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 NO
- [SDR FDEA202102120346](https://openairdocs.org/sdr/FDEA202102120346.md): Line · cracked · Feb 12, 2021 · N993FD · Boeing 7572Q8 · Hydraulic System, Main
  > DEPARTING 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 WE
- [SDR FDEA202102120345](https://openairdocs.org/sdr/FDEA202102120345.md): Line · broken · Feb 12, 2021 · N993FD · Boeing 7572Q8 · Hydraulic System, Main
  > WHEN 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
- [SDR FDEA202102090319](https://openairdocs.org/sdr/FDEA202102090319.md): Frame · cracked · Feb 9, 2021 · N993FD · Boeing 7572Q8 · Fuselage Main, Frame
  > BODY 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- TEMPO
- [SDR FDEA202101060013](https://openairdocs.org/sdr/FDEA202101060013.md): Switch · damaged · Jan 6, 2021 · N993FD · Boeing 7572Q8 · Leading Edge Slat Control System
  > AT 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 LOSS
- [SDR FDEA201907091510](https://openairdocs.org/sdr/FDEA201907091510.md): Battery Pack · discharged · Jul 9, 2019 · N993FD · Boeing 7572Q8 · Emergency Lighting
  > ON PREFLIGHT FOUND LT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED LT BATTERY PACK PER AMM 33-51-07-2. OP'S CHECK GOOD.
- [SDR FDEA201902070267](https://openairdocs.org/sdr/FDEA201902070267.md): Warning System · false activation · Feb 7, 2019 · N993FD · Boeing 7572Q8 · Leading Edge Slat Position Indicating System
  > ON 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 NO
- [SDR FDEA201901200184](https://openairdocs.org/sdr/FDEA201901200184.md): Intercostal · corroded · Jan 20, 2019 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous Structure
  > CORROSION 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 DW
- [SDR FDEA201901200185](https://openairdocs.org/sdr/FDEA201901200185.md): Mount Fitting · corroded · Jan 20, 2019 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous Structure
  > AFT. 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 SRM
- [SDR FDEA201901160157](https://openairdocs.org/sdr/FDEA201901160157.md): Fitting · corroded · Jan 16, 2019 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous Structure
  > UPON 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.
- [SDR FDEA201901160153](https://openairdocs.org/sdr/FDEA201901160153.md): Intercostal · corroded · Jan 16, 2019 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous Structure
  > AFT 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 INSTALLE
- [SDR FDEA201901150135](https://openairdocs.org/sdr/FDEA201901150135.md): Intercostal · corroded · Jan 15, 2019 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous Structure
  > AFT 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 INTERC
- [SDR FDEA201901150134](https://openairdocs.org/sdr/FDEA201901150134.md): Web · corroded · Jan 15, 2019 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous Structure
  > AFT 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 A
- [SDR FDEA201901150133](https://openairdocs.org/sdr/FDEA201901150133.md): Support Angle · corroded · Jan 15, 2019 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR FDEA201901100071](https://openairdocs.org/sdr/FDEA201901100071.md): Shear Tie · corroded · Jan 10, 2019 · N993FD · Boeing 7572Q8 · Fuselage Internal Mounting Structure
  > AFT 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.
- [SDR FDEA201901070043](https://openairdocs.org/sdr/FDEA201901070043.md): Skin · gouged · Jan 7, 2019 · N993FD · Boeing 7572Q8 · Trailing Edge Flaps
  > LT. 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
- [SDR FDEA201901040016](https://openairdocs.org/sdr/FDEA201901040016.md): Seat Track · corroded · Jan 4, 2019 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach Fittings
  > SUPERNUMERARY 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 B
- [SDR FDEA201901040015](https://openairdocs.org/sdr/FDEA201901040015.md): Seat Track · corroded · Jan 4, 2019 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach Fittings
  > SUPERNUMERARY 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 O
- [SDR FDEA201901030013](https://openairdocs.org/sdr/FDEA201901030013.md): Crease Beam · corroded · Jan 3, 2019 · N993FD · Boeing 7572Q8 · Fuselage Main, Structure
  > CABIN 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 CR
- [SDR FDEA201709202658](https://openairdocs.org/sdr/FDEA201709202658.md): Fseu · malfunctioned · Sep 20, 2017 · N993FD · Boeing 7572Q8 · Leading Edge Slat Control System
  > 25 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 S
- [SDR FDEA201612174486](https://openairdocs.org/sdr/FDEA201612174486.md): Strut · damaged · Dec 17, 2016 · N993FD · Boeing 7572Q8 · Nacelle/Pylon, Main Frame
  > LEFT 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.
- [SDR FDEA201612084362](https://openairdocs.org/sdr/FDEA201612084362.md): Door Frame · cracked · Dec 8, 2016 · N993FD · Boeing 7572Q8 · Passenger/Crew Doors
  > R-2 DOOR UPPER HINGE CUTOUT INNER CHORD OF THE DOOR FRAME CRACKED. REPAIRED IAW SRM 52-10-02-2R DETAIL III FIG.201.
- [SDR FDEA201604071177](https://openairdocs.org/sdr/FDEA201604071177.md): Lanyard · out of position · Apr 7, 2016 · N993FD · Boeing 7572Q8 · Emergency Equipment
  > RIGHT CREW DOOR SLIDE WILL NOT ARM. RE-STOWED R1 DOOR SLIDE CORDS IAW AMM 52-11-00-5-0. SYS OPERATIONS CHECKED GOOD.
- [SDR FDEA201507042152](https://openairdocs.org/sdr/FDEA201507042152.md): Oxygen Box · leaking · Jul 4, 2015 · N993FD · Boeing 7572Q8 · Crew Oxygen System
  > CAPTAIN`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 MAS
- [SDR FDEA201503050688](https://openairdocs.org/sdr/FDEA201503050688.md): Latch · damaged · Mar 5, 2015 · N993FD · Boeing 7572Q8 · Emergency Equipment
  > CAPTAIN 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. INSTALL
- [SDR FDEA201412124116](https://openairdocs.org/sdr/FDEA201412124116.md): Closeout Panel · dented · Dec 12, 2014 · N993FD · Boeing 7572Q8 · Cargo/Baggage Doors
  > MAIN 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.
- [SDR FDEA201412114103](https://openairdocs.org/sdr/FDEA201412114103.md): Skin · dented · Dec 11, 2014 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/Skin
  > FUSELAGE DENTED AT BS 761 JUST BELOW STRINGER 17L. REPAIRED IAW SRM 53-00-01 REPAIR 16. MAJOR REPAIR.
- [SDR FDEA201406111410](https://openairdocs.org/sdr/FDEA201406111410.md): Wedge · damaged · Jun 11, 2014 · N993FD · Boeing 7572Q8 · Leading Edge Devices
  > NUMBER 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.
- [SDR FDEA201406101392](https://openairdocs.org/sdr/FDEA201406101392.md): Skin · damaged · Jun 10, 2014 · N993FD · Boeing 7572Q8 · Trailing Edge Flaps
  > RIGHT 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.
- [SDR FDEA201406101391](https://openairdocs.org/sdr/FDEA201406101391.md): Skin · damaged · Jun 10, 2014 · N993FD · Boeing 7572Q8 · Trailing Edge Flaps
  > LEFT 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.
- [SDR FDEA201406071351](https://openairdocs.org/sdr/FDEA201406071351.md): Wedge · damaged · Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge Devices
  > NUMBER 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.
- [SDR FDEA201406071350](https://openairdocs.org/sdr/FDEA201406071350.md): Wedge · damaged · Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge Devices
  > NUMBER 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.
- [SDR FDEA201406071349](https://openairdocs.org/sdr/FDEA201406071349.md): Wedge · damaged · Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge Devices
  > NUMBER 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.
- [SDR FDEA201406071348](https://openairdocs.org/sdr/FDEA201406071348.md): Skin · damaged · Jun 7, 2014 · N993FD · Boeing 7572Q8 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STAB FWD UPPER SKIN HAS NUMEROUS HAIL DAMAGE ADJACENT TO PNLS 332BL, 332CL & 332DL. REPAIRED DENTS BY FILLING & FAIRING IAW EA F5510-T0308665.
- [SDR FDEA201406071347](https://openairdocs.org/sdr/FDEA201406071347.md): Wedge · damaged · Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge Devices
  > NUMBER 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.
- [SDR FDEA201406071346](https://openairdocs.org/sdr/FDEA201406071346.md): Wedge · damaged · Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge Devices
  > NUMBER 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.
- [SDR FDEA201406071345](https://openairdocs.org/sdr/FDEA201406071345.md): Wedge · damaged · Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge Devices
  > NUMBER 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.
- [SDR FDEA201406071344](https://openairdocs.org/sdr/FDEA201406071344.md): Skin · damaged · Jun 7, 2014 · N993FD · Boeing 7572Q8 · Horizontal Stabilizer, Plate/Skin
  > RIGHT 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.
- [SDR FDEA201406071343](https://openairdocs.org/sdr/FDEA201406071343.md): Wedge · damaged · Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge Devices
  > NUMBER 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.
- [SDR FDEA201406071342](https://openairdocs.org/sdr/FDEA201406071342.md): Wedge · damaged · Jun 7, 2014 · N993FD · Boeing 7572Q8 · Leading Edge Devices
  > NUMBER 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.

Next page: https://openairdocs.org/aircraft/N993FD/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 = 'N993FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N993FD/reports

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