# N993FD: 1992 Boeing 757-2Q8 - Status: Valid registration - Airframe: [Boeing 757-2Q8](https://openairdocs.org/model/boeing-757-2q8) (registry code 1384972, 178 seats) - Engine: [Pratt & Whitney PW2037](https://openairdocs.org/engine/pratt-whitney-pw2037) (registry code 52117) - Data sheets: [TCDS E17NE](https://openairdocs.org/tcds/E17NE) (Pratt & Whitney) (OpenAirDocs) - Serial number: 24965 - Year built: 1992 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 19, 2011 - Certificate issued: November 19, 2009 - Expires: November 30, 2028 - Mode S code: ADDE49 - Registered owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP) - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Corporation - Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=993FD - Page: https://openairdocs.org/aircraft/N993FD From the FAA registry file of October 22, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 15 in force ### Matched by airframe (Boeing 757-2Q8) None in force. ### Matched by engine (Pratt & Whitney PW2037) - [AD 2026-07-06](https://openairdocs.org/ad/2026-07-06): Turbine Section · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 3 more. Effective May 29, 2026 - [AD 2024-12-04](https://openairdocs.org/ad/2024-12-04): Turbine Section · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Aug 13, 2024 - [AD 2021-14-13](https://openairdocs.org/ad/2021-14-13): Turbine Section · Pratt & Whitney F117-PW-100, PW2037, PW2037M and 1 more. Effective Sep 1, 2021 - [AD 2019-05-01](https://openairdocs.org/ad/2019-05-01): Turbine/Turboprop Engine · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 6 more. Effective Apr 16, 2019 - [AD 2018-22-06](https://openairdocs.org/ad/2018-22-06): Fuel Control/Turbine Engines · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Dec 3, 2018 - [AD 2018-14-10](https://openairdocs.org/ad/2018-14-10): Fuel Control Turbine Engines · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Sep 28, 2018 - [AD 2012-02-01](https://openairdocs.org/ad/2012-02-01): Fan blades · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Apr 24, 2012 - [AD 2009-14-05](https://openairdocs.org/ad/2009-14-05): High-pressure compressor (HPC) · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Jul 23, 2009 - [AD 2009-10-08](https://openairdocs.org/ad/2009-10-08): High-pressure turbine 2nd stage hubs that have previously been exposed to Pratt & Whitney cleaning procedure SPOP 10 or SPOP 9 or equivalent procedure. · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Jun 17, 2009 - [AD 2007-02-06](https://openairdocs.org/ad/2007-02-06): High pressure compressor (HPC) drum rotor disk assemblies · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Feb 28, 2007 - [AD 2005-18-03](https://openairdocs.org/ad/2005-18-03): Engine manufacturer's time limits section (TLS) · Pratt & Whitney Division PW2037, PW2037D, PW2037M and 5 more. Effective Feb 28, 2006 - [AD 99-20-03](https://openairdocs.org/ad/99-20-03): High Pressure Turbine Disks · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 2 more. Effective Nov 23, 1999 - [AD 96-18-08 R1](https://openairdocs.org/ad/96-18-08-R1): (HPT) High Pressure or (LPT) Low Pressure Turbine · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 2 more. Effective Nov 10, 1998 - [AD 97-11-51 R1](https://openairdocs.org/ad/97-11-51-R1): First Stage High Pressure Turbine (HPT) Disk Assembly · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective Aug 7, 1997 - [AD 88-03-52](https://openairdocs.org/ad/88-03-52): Fuel Quantity Indication System · Pratt & Whitney Division PW2037 and PW2040. Effective Jul 13, 1988 ### Historical (superseded or no longer in force) - [AD 2017-12-03](https://openairdocs.org/ad/2017-12-03) (historical): Fuel Control Turbine Engines · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Jul 20, 2017 - [AD 2017-11-06](https://openairdocs.org/ad/2017-11-06) (historical): Turbine/ Turboprop Engine · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 6 more. Effective Jul 18, 2017 - [AD 2014-05-32](https://openairdocs.org/ad/2014-05-32) (historical): Diffuser-to-high-pressure turbine (HPT) case flange · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 8 more. Effective May 5, 2014 - [AD 2002-12-06](https://openairdocs.org/ad/2002-12-06) (historical): Time Limits Section (TLS) · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective Jul 17, 2002 - [AD 2000-21-09](https://openairdocs.org/ad/2000-21-09) (historical): Critical Life-limited Parts · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective Jan 22, 2001 - [AD 99-08-14](https://openairdocs.org/ad/99-08-14) (historical): Maintenance Program, Mandatory Inspections · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective May 13, 1999 ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N993FD. ## FAA accident and incident reports None matched to N993FD. ## Service difficulty reports (134, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FDEA202608281248](https://openairdocs.org/sdr/FDEA202608281248), Aug 28, 2026: STRUT. CRACKED. 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), Aug 28, 2026: SKIN. DEBONDED. 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, F - [SDR FDEA202608261233](https://openairdocs.org/sdr/FDEA202608261233), Aug 26, 2026: STRAP. CRACKED. 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 SECON - [SDR FDEA202608241221](https://openairdocs.org/sdr/FDEA202608241221), Aug 24, 2026: SKIN. DENTED. 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- - [SDR FDEA202608241222](https://openairdocs.org/sdr/FDEA202608241222), Aug 24, 2026: CREASE BEAM. CORRODED. 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, - [SDR FDEA202608201195](https://openairdocs.org/sdr/FDEA202608201195), Aug 20, 2026: BEAM. CRACKED. 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 - [SDR FDEA202301090056](https://openairdocs.org/sdr/FDEA202301090056), Jan 9, 2023: FRAME. CRACKED. 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 - [SDR FDEA202301070048](https://openairdocs.org/sdr/FDEA202301070048), Jan 7, 2023: DRAG FITTING. GOUGED. 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 DR - [SDR FDEA202212232999](https://openairdocs.org/sdr/FDEA202212232999), Dec 23, 2022: FLOORBOARD. DAMAGED. 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), Apr 28, 2021: GIRT BAR. OBSTRUCTED. 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 INDICA - [SDR FDEA202103190707](https://openairdocs.org/sdr/FDEA202103190707), Mar 19, 2021: CONTROL UNIT. MALFUNCTIONED. BRAKE SOURCE LIGHT ILLUMINATED WHILE ARRIVING IN MEMPHIS ... PASSING 10,000 FT. RAN QRH , DECLARED EMERGENCY , LANDED ... DID NOT TAXI . THE BRAKE SOURCE LIGHT - [SDR FDEA202102120346](https://openairdocs.org/sdr/FDEA202102120346), Feb 12, 2021: LINE. CRACKED. 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 A - [SDR FDEA202102120345](https://openairdocs.org/sdr/FDEA202102120345), Feb 12, 2021: LINE. BROKEN. 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 ALTERN - [SDR FDEA202102090319](https://openairdocs.org/sdr/FDEA202102090319), Feb 9, 2021: FRAME. CRACKED. 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-MAINF - [SDR FDEA202101060013](https://openairdocs.org/sdr/FDEA202101060013), Jan 6, 2021: SWITCH. DAMAGED. 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 SWITC - [SDR FDEA201907091510](https://openairdocs.org/sdr/FDEA201907091510), Jul 9, 2019: BATTERY PACK. DISCHARGED. 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), Feb 7, 2019: WARNING SYSTEM. FALSE ACTIVATION. ON FINAL GOT A SLAT DISAGREE LIGHT. RAN QRH, LANDED UNEVENTFULLY USING ALTERNATE FLAP SYSTEM. SLAT DISAGREE LIGHT EXTINGUISHED DURING QRH PROCEDURES. INSPECTED - [SDR FDEA201901200184](https://openairdocs.org/sdr/FDEA201901200184), Jan 20, 2019: INTERCOSTAL. CORRODED. 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 S - [SDR FDEA201901200185](https://openairdocs.org/sdr/FDEA201901200185), Jan 20, 2019: MOUNT FITTING. CORRODED. 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 EXFOLIATE - [SDR FDEA201901160157](https://openairdocs.org/sdr/FDEA201901160157), Jan 16, 2019: FITTING. CORRODED. 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. - [SDR FDEA201901160153](https://openairdocs.org/sdr/FDEA201901160153), Jan 16, 2019: INTERCOSTAL. CORRODED. 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 - [SDR FDEA201901150135](https://openairdocs.org/sdr/FDEA201901150135), Jan 15, 2019: INTERCOSTAL. CORRODED. 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 S - [SDR FDEA201901150134](https://openairdocs.org/sdr/FDEA201901150134), Jan 15, 2019: WEB. CORRODED. 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 COR - [SDR FDEA201901150133](https://openairdocs.org/sdr/FDEA201901150133), Jan 15, 2019: SUPPORT ANGLE. CORRODED. 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 - [SDR FDEA201901100071](https://openairdocs.org/sdr/FDEA201901100071), Jan 10, 2019: SHEAR TIE. CORRODED. 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 1 - [SDR FDEA201901070043](https://openairdocs.org/sdr/FDEA201901070043), Jan 7, 2019: SKIN. GOUGED. 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. - [SDR FDEA201901040016](https://openairdocs.org/sdr/FDEA201901040016), Jan 4, 2019: SEAT TRACK. CORRODED. 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 IA - [SDR FDEA201901040015](https://openairdocs.org/sdr/FDEA201901040015), Jan 4, 2019: SEAT TRACK. CORRODED. 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 IA - [SDR FDEA201901030013](https://openairdocs.org/sdr/FDEA201901030013), Jan 3, 2019: CREASE BEAM. CORRODED. 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. EVALUATE - [SDR FDEA201709202658](https://openairdocs.org/sdr/FDEA201709202658), Sep 20, 2017: FSEU. MALFUNCTIONED. 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 CONFIGURA - [SDR FDEA201612174486](https://openairdocs.org/sdr/FDEA201612174486), Dec 17, 2016: STRUT. DAMAGED. 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 FASTE - [SDR FDEA201612084362](https://openairdocs.org/sdr/FDEA201612084362), Dec 8, 2016: DOOR FRAME. CRACKED. 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), Apr 7, 2016: LANYARD. OUT OF POSITION. 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), Jul 4, 2015: OXYGEN BOX. LEAKING. 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 CAPT - [SDR FDEA201503050688](https://openairdocs.org/sdr/FDEA201503050688), Mar 5, 2015: LATCH. DAMAGED. 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 - [SDR FDEA201412124116](https://openairdocs.org/sdr/FDEA201412124116), Dec 12, 2014: CLOSEOUT PANEL. DENTED. MAIN CARGO DOOR, FWD PRESSURE RELIEF DOOR CLOSEOUT PANEL IS GOUGED. REMOVED DAMAGED CLOSEOUT PANEL, FABRICATED NEW CLOSEOUT PANEL, AND INSTALLED IAW SRM 51-40-0 - [SDR FDEA201412114103](https://openairdocs.org/sdr/FDEA201412114103), Dec 11, 2014: SKIN. DENTED. 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), Jun 11, 2014: WEDGE. DAMAGED. 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- - [SDR FDEA201406101392](https://openairdocs.org/sdr/FDEA201406101392), Jun 10, 2014: SKIN. DAMAGED. 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 - [SDR FDEA201406101391](https://openairdocs.org/sdr/FDEA201406101391), Jun 10, 2014: SKIN. DAMAGED. 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 2 - [SDR FDEA201406071351](https://openairdocs.org/sdr/FDEA201406071351), Jun 7, 2014: WEDGE. DAMAGED. 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), Jun 7, 2014: WEDGE. DAMAGED. 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), Jun 7, 2014: WEDGE. DAMAGED. 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 - [SDR FDEA201406071348](https://openairdocs.org/sdr/FDEA201406071348), Jun 7, 2014: SKIN. DAMAGED. 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), Jun 7, 2014: WEDGE. DAMAGED. 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-27-8 - [SDR FDEA201406071346](https://openairdocs.org/sdr/FDEA201406071346), Jun 7, 2014: WEDGE. DAMAGED. 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- - [SDR FDEA201406071345](https://openairdocs.org/sdr/FDEA201406071345), Jun 7, 2014: WEDGE. DAMAGED. 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-2 - [SDR FDEA201406071344](https://openairdocs.org/sdr/FDEA201406071344), Jun 7, 2014: SKIN. DAMAGED. RIGHT HORIZONTAL STAB FWD UPPER SKIN HAS NUMEROUS HAIL DAMAGE ADJACENT TO PNLS 342BR, 342CR & 342DR. SANDED, CLEANED & APPLIED CONVERSION COATING IAW EA F5510-T - [SDR FDEA201406071343](https://openairdocs.org/sdr/FDEA201406071343), Jun 7, 2014: WEDGE. DAMAGED. 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-27-8 - [SDR FDEA201406071342](https://openairdocs.org/sdr/FDEA201406071342), Jun 7, 2014: WEDGE. DAMAGED. 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-27-8 All 134: https://openairdocs.org/aircraft/N993FD/reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Boeing 757-2Q8 aircraft: https://openairdocs.org/model/boeing-757-2q8/aircraft.md - The Pratt & Whitney PW2037 engine: https://openairdocs.org/engine/pratt-whitney-pw2037.md --- 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.