# N996FD: 1993 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: 26270
- Year built: 1993
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 9, 2011
- Certificate issued: January 6, 2011
- Expires: January 31, 2030
- Mode S code: ADE96E
- 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=996FD
- Page: https://openairdocs.org/aircraft/N996FD

From the FAA registry file of October 24, 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 N996FD.

## FAA accident and incident reports

None matched to N996FD.

## Service difficulty reports (117, 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 FDEA202609131331](https://openairdocs.org/sdr/FDEA202609131331), Sep 13, 2026: BALLSCREW. FAILED. FOUND LT WING FLAP INBD TRANSMISSION WITH INDICATOR TRIPPED & JACKSCREW DAMAGED. AMM: 27-51-11-4 AMM: 27-51-06-4 REMOVED INBD T/E FLAP XMISSION & INBD TE BALLSC
- [SDR FDEA202609111324](https://openairdocs.org/sdr/FDEA202609111324), Sep 11, 2026: TRANSMISSION. FAULTED. WHEN FLAPS 20 SELECTED ON ARRIVAL TE FLAPS DISAGREE EICAS ALERT. TE FLAPS STOPPED AT APPROXIMATELY 18 DEGREES. DECLARED EMERGENCY, ACCOMPLISHED QRH PROCEDURE, L
- [SDR FDEA202606230791](https://openairdocs.org/sdr/FDEA202606230791), Jun 23, 2026: GIRT BAR. OUT OF ADJUST. RT ENTRY DOOR SLIDE WILL NOT ARM. RELEASED FOR SERVICE PER MEL : 52-11-01-A. R1 DOOR OR SLIDE INOP. ADJUSTED R1 DOOR GIRT BAR REF AMM 25-66-10-2. OPS CHECKED GO
- [SDR FDEA202606100695](https://openairdocs.org/sdr/FDEA202606100695), Jun 10, 2026: DOOR. FOD. CREW REPORTED R1 DOOR WILL NOT ARM AMM 52-11-25-5 REMOVED DEBRIS FROM AREA AND PERFORMED SATISFACTORY ARM AMD DISARM OF R1 DOOR. AMM 52-11-25-5 REMOVED DEBRIS F
- [SDR FDEA202505200770](https://openairdocs.org/sdr/FDEA202505200770), May 20, 2025: BATTERY PACK. FAILED. R/H EMGERGENCY EXIT SIGN AND EXTERIOR LT INOP. REPLACED R/H EMGERGENCY EXIT SIGN AND EXTERIOR LT BATTERY PACK ASSY (RADIANT POWER CORP). OK FOR SERVICE.
- [SDR FDEA202503050331](https://openairdocs.org/sdr/FDEA202503050331), Mar 5, 2025: SLIDE. PARTIAL DEPLOY. L 1 DOOR SLIDE PARTIAL DEPLOYMENT DUE POSIBLE FOD IN GIRT BAR. ( GRAY MATS). REMOVED AND REPLACED L1 DOOR SLIDE. AMM: 25-66-01-4.
- [SDR FDEA202407181030](https://openairdocs.org/sdr/FDEA202407181030), Jul 18, 2024: IRU. FAILED. REJECTED TAKEOFF. SIMULTANEOUS L & C IRS FAULT EICAS AND ASSOCIATED ATT & HDG FAILURES. REFERENCE WRI 05-50-0566: ACCOMPLISHED WATER ACCUMULATION INSPECTION AND
- [SDR FDEA202404030441](https://openairdocs.org/sdr/FDEA202404030441), Apr 3, 2024: WINDOW. ARCED. AT CRUISE FL360, R FWD WINDOW BEGAN ARCING FOR 20-30 SECONDS FOLLOWED BY THE OUTER PAIN SHATTERING. THE INNER PAIN APPEARS INTACT WITH NO LEAK OR LOSS OF PRESSU
- [SDR FDEA202307251290](https://openairdocs.org/sdr/FDEA202307251290), Jul 25, 2023: FLOORBOARD. DELAMINATED. ZONE 220 FLOORBOARD 221 MBF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221 MBF ON VT MAE TRAVELER # T23/1691348 IAW DWG SRZ -25-005 REVISION R MAJOR REPAIR.
- [SDR FDEA202307251289](https://openairdocs.org/sdr/FDEA202307251289), Jul 25, 2023: FLOORBOARD. DAMAGED. ZONE 220 FLOORBOARD 221BF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221 BF ON VT MAE TRAVELET # T23/1691347 IAW DWG SRZ -25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202307211266](https://openairdocs.org/sdr/FDEA202307211266), Jul 21, 2023: FLAP. DAMAGED. L/H WING O/B AFT FLAP LOWER SKIN APPROX. MID POINT HAS A REPAIR THAT IS NOT ON THE AGING MAJOR REPAIR LIST. VISUALLY INSPECTED REPAIR IAW ATTACHMENT "B" OF EO F
- [SDR FDEA202307211265](https://openairdocs.org/sdr/FDEA202307211265), Jul 21, 2023: WEB. DAMAGED. WEB REPAIR ON MAIN DECK AT STA1720 BL 0 TO LBL 47.5 IS NOT ON AGING MAJOR REPAIR LIST. VISUALLY INSPECTED REPAIR IAW ATTACHMENT "B" OF EO F-5100-7-5001. REPAIR 
- [SDR FDEA202307191242](https://openairdocs.org/sdr/FDEA202307191242), Jul 19, 2023: SEAT TRACK. CORRODED. MAIN CABIN BETWEEN STA 1160 & 1200, RBL 45, SEAT TRACK FLANGE HAS CORROSION. REMOVED AND REPLACED SEAT TRACK FROM STA 1180-1230 RBL 45 PER SRM 53-00-52-2R REPAI
- [SDR FDEA202307131214](https://openairdocs.org/sdr/FDEA202307131214), Jul 13, 2023: SEAT TRACK. CORRODED. CORRODED SEAT TRACK AT STA. 345.0 RBL 24. CORROSION ON SEAT TRACK WAS EVALUATED AND FOUND OUT LIMITS IAW B 757 SRM 53-00-52- 1A. FABRICATED NEW SECTION SEAT TRA
- [SDR FDEA202212092895](https://openairdocs.org/sdr/FDEA202212092895), Dec 9, 2022: SLIDE. DISLODGED. AFTER L CREW ENTRANCE DOOR WAS OPENED, WITH NO SLIDE DEPLOYMENT, GROUND CREW OPENED THE ALREADY CRACKED, DISARMED DOOR AND DURING THE OPENING PROCESS THE SLIDE 
- [SDR FDEA202207151732](https://openairdocs.org/sdr/FDEA202207151732), Jul 15, 2022: COLLAR. CRACKED. FOUND L1 DOOR HOLD-OPEN LOCK BROKEN. REMOVED AND REPLACED L1 DOOR HOLD OPEN LOCK REF AMM 52-11-08-4. OK FOR SERVICE.
- [SDR FDEA202203110494](https://openairdocs.org/sdr/FDEA202203110494), Mar 11, 2022: NONE. NONE. TE FLAP DISAGREE WHEN FLAPS 1 SELECTED. DID NOT CLEAR WITH QRH. PROCEEDED TO TE FLAP ASYM QRH AND LANDED WITH FLAPS SHOWING BETWEEN 0 AND 1. T/S AND FOUND THE L
- [SDR FDEA202111272941](https://openairdocs.org/sdr/FDEA202111272941), Nov 27, 2021: FLAP SYSTEM. FAULTED. TE FLAP DISSAGREE EICAS MSG WHEN FLAP HANDLE SELECTED AT 1. RAN CHECKLIST AND LANDED FLAPS 20 WITH NO FURTHER ISSUES. PERFORMED FSEU BITE PROCEDURE. NO FSEU HAD
- [SDR FDEA202108292155](https://openairdocs.org/sdr/FDEA202108292155), Aug 29, 2021: SKIN. DEBONDED. #3 SLAT DISBOND INDICATION FOUND: T/E WEDGE LOWER SKIN 1.5" IN DIAMETER, 30" FROM O/B, 2" FROM TOP T/E REPLACED #3 SLAT PER B757 AMM 27-81-02-4
- [SDR FDEA202108272119](https://openairdocs.org/sdr/FDEA202108272119), Aug 27, 2021: ATTACH BRACKET. CRACKED. EXTERIOR FUSELAGE NOSE RADOME HOLD OPEN ROD STOWAGE PIN ATTACH BRACKET IS DEFORMED ON THE LEFT FWD BULKHEADS WALL (ZONE 111) REMOVED DAMAGED BRACKET , INSTALLED
- [SDR FDEA202108262106](https://openairdocs.org/sdr/FDEA202108262106), Aug 26, 2021: FLOORBEAM. CRACKED. MAIN FLOOR BEAM AT STA 580 LBL 45.5 IS CRACKED. REPAIRED FLOOR BEAM AT STA 580 LBL 45.5 IAW FEDEX E.A. F-5310-T0363608 AND FEDEX STANDARD REWORK DRAWING SR57-53
- [SDR FDEA202108252096](https://openairdocs.org/sdr/FDEA202108252096), Aug 25, 2021: BRACKET. CRACKED. WIRE CONDUIT BRACKET CRACKED BETWEEN FASTENER HOLES UNDER ACCESS PANEL 435AL REMOVED AND REPLACED BRACKET PER DWG 313N3053 REV E
- [SDR FDEA202103040559](https://openairdocs.org/sdr/FDEA202103040559), Mar 4, 2021: PUMP. LEAKING. L HYD SYS PRESSURE LOSS OF LEFT HYD. QUANTITY "0". QRH REFERENCED. PTU FUNCTIONED PROPERLY. DECLARED EMERGENCY. REQUESTED TOW FROM MAINTENANCE. IND REMOVED AND 
- [SDR FDEA202009092156](https://openairdocs.org/sdr/FDEA202009092156), Sep 9, 2020: HOLDER. DAMAGED. MDIS 996, 33-50, 7681, 09SEP20, MEM, FACT, U. ON PREFLIGHT, DISCOVERED EMERGENCY LIGHTS FOR L1 DOOR, BOTH INTERIOR AND EXTERIOR, INOPERABLE. R/I 09SEP20 06:37 M
- [SDR FDEA202004230775](https://openairdocs.org/sdr/FDEA202004230775), Apr 23, 2020: HYDRAULIC LINE. NOT REPORTED. L HYD ELEC PUMP AND L HYD QTY EIAS AT CRUISE. FOLLOWED BY L HYD SYS PRESS. QRH COMPLETED EMERGENCY DECLARED. PTU OPERATED NORMALLY TO MAINTAIN L SYS PRESSURE ON
- [SDR FDEA2019123183322](https://openairdocs.org/sdr/FDEA2019123183322), Dec 28, 2019: LIGHT. FALSE ACTIVATION. R1 ENTRY DOOR SLIDE LIGHT REMAINS ILLUMINATED WHEN SLIDE ARMING LEVER MOVED TO DISARM. CHECKED SWITCH SENSOR GAP IAW AMM 25-66-11-2 FIG 201 CHECKED GOOD. OPERAT
- [SDR FDEA2019120103157](https://openairdocs.org/sdr/FDEA2019120103157), Nov 30, 2019: TRANSMITTER. FAILED. RIGHT ENG WOULD NOT RELIGHT AFTER INTENTIONAL SHUTDOWN FOR TEST FLIGHT PROFILE. ENGINE VALVE DISCREET LIGHT REMAINED ILLUMINATED WHEN RIGHT FIRE HANDLE WAS PULL
- [SDR FDEA2019112213022](https://openairdocs.org/sdr/FDEA2019112213022), Nov 21, 2019: FLOORBEAM. CORRODED. MAIN CABIN STA 1681 LBL 39/40 FLOOR BEAM UPPER T-CAP IS CORRODED REMOVE DAMAGE AND REPAIRED IAW FEDEX EA# F-5310-T0350636
- [SDR FDEA201911192995](https://openairdocs.org/sdr/FDEA201911192995), Nov 19, 2019: WEB. CORRODED. CABIN FLOOR WEB CORRODED BS 1681, BL 11L -BL47L REMOVED DAMAGE AND REPAIRED IAW B757-200 SRM 53-60-51-2R AND EA# F5310-T0350636
- [SDR FDEA201911162967](https://openairdocs.org/sdr/FDEA201911162967), Nov 16, 2019: SEAL DEPRESSOR. GOUGED. MCD CUT OUT FWD SEAL RETAINER IS GOUGED - DOT & STREAMER ATTACHED REMOVED, FABRICATED AND REPLACED SEAL DEPRESSOR IAW B757 DWG 69-34527 AND DWG DWG 143N8730 REV
- [SDR FDEA2019111542962](https://openairdocs.org/sdr/FDEA2019111542962), Nov 14, 2019: FRAME. DENTED. AFT PIT FRAME BENT B.S.1420 BETWEEN STR 23L AND 24L. BS1420, STR 23L STR 24L REPAIRED FRAME AT STA 1420 STR23L-STR24L IAW FDX E.A.#F-5310-T0350569
- [SDR FDEA2019111542961](https://openairdocs.org/sdr/FDEA2019111542961), Nov 14, 2019: PLATE. CRACKED. #1 ENG O/B CORE COWL L/E PLATE CRACKED AT LWR END REMOVED AND REPLACED FILLER PER FEDEX EA # F7110-T0350560P1
- [SDR FDEA201911122926](https://openairdocs.org/sdr/FDEA201911122926), Nov 12, 2019: SKIN. DAMAGED. EXTERNAL SKIN DOUBLER REPAIR IS GOUGED IN 2 PLACES AND DENTED AT FASTENER HOLE BS 418-BS 419,STR 17 LEFT SIDE AFT OF L1 DOOR REMOVED AND REPLACED DOUBLER PER B7
- [SDR FDEA2019111522926](https://openairdocs.org/sdr/FDEA2019111522926), Nov 12, 2019: SKIN. GOUGED. EXTERNAL SKIN DOUBLER REPAIR IS GOUGED IN 2 PLACES AND DENTED AT FASTENER HOLE BS 418-BS 419,STR 17 LEFT SIDE AFT OF L1 DOOR REMOVED AND REPLACED DOUBLER PER B7
- [SDR FDEA2019111102916](https://openairdocs.org/sdr/FDEA2019111102916), Nov 10, 2019: RUB STRIP. CRACKED. #1 ENG O/B REV T/E LWR CHAFE STRIP CRACKED REMOVED AND REPLACED CHAFE STRIP PER EA # F-7830-T0350620-P1
- [SDR FDEA2019110762897](https://openairdocs.org/sdr/FDEA2019110762897), Nov 6, 2019: BRACKET. BROKEN. #1 ENG O/B REV T/E BRACKET BROKEN STREAMER ATTACH REMOVED AND REPLACED BRACKET AT #1 ENG O/B REV T/E PER BAC DWG # 315N3105 REV CATCHR AND B757 SRM 51-40-02
- [SDR FDEA2019110752872](https://openairdocs.org/sdr/FDEA2019110752872), Nov 5, 2019: FLOORBEAM. CRACKED. MAIN CABIN STA 1640 AT APPROX RBL 45 FLOOR BEAM SUB-STRUCTURE IS CRACKED VIEWED FROM BELOW (STREAMER ATTACHED) REPAIRED STA 1640 @ RBL 45 FLOOR BEAM SUB STRUCTU
- [SDR FDEA2019110752871](https://openairdocs.org/sdr/FDEA2019110752871), Nov 5, 2019: WEB. CORRODED. CABIN FLOOR WEB CORRODED BS 1640 - BS 1653, BL 54R - BL-58R REPAIRED FLOOR WEB AT STA BS1640-1653, BL 54R-58R IAW B757 SRM 53-60-15-1A AND B757 SRM 51-20-01-0G
- [SDR FDEA2019110752870](https://openairdocs.org/sdr/FDEA2019110752870), Nov 5, 2019: WEB. CORRODED. CABIN FLOOR WEB CORRODED BS 1642 - BS 1649, BL 57L REPAIRED FLOOR WEB AT BS 1642-1649 BL 57L IAW B757 SRM 53-60-15-1A AND B757 51-20-1-0G
- [SDR FDEA2019110752868](https://openairdocs.org/sdr/FDEA2019110752868), Nov 5, 2019: WEB. CORRODED. CABIN FLOOR WEB CORRODED BS 1712, BL 0 REPAIRED FLOOR WEB AT B1712,BL0 IAW B757 SRM 53-60-51-1A AND B757 51-20-01-06
- [SDR FDEA201911032851](https://openairdocs.org/sdr/FDEA201911032851), Nov 3, 2019: ACCESS PANEL. CRACKED. R/W #9 SLAT AFT FACE I/B OF ACCESS PNL 624CB FASTENER HOLE POSSIBLE CRACK FABRICATED NEW PANEL PER DWG # 114N4076
- [SDR FDEA201911022830](https://openairdocs.org/sdr/FDEA201911022830), Nov 2, 2019: BRACKET. BENT. MAIN CARGO OVER WING AREA AT BS 1088 LBL55 BRAVKET BENT FABRICATED NEW BRACKET PER BAC DWG# 287N4407 REV T AND INSTALLED NEW BRACKET PER BAC DWG# 287N4407 REV F
- [SDR FDEA201910302788](https://openairdocs.org/sdr/FDEA201910302788), Oct 30, 2019: NUT PLATE. CORRODED. MAIN CABIN 1681 APPROX LBL 12 NUTPLATE STRIP UNDER THE FLOOR BEAM UPPER CAP IS CORRODED REMOVED CORRODED NUTPLATE STRAP, REMOVED CORROSIONUNDER STRAP, TREATED B
- [SDR FDEA201910302787](https://openairdocs.org/sdr/FDEA201910302787), Oct 30, 2019: NUT PLATE. CORRODED. MAIN CABIN STA 1681 APPROX RBL 11.5 NUTPLATE STRIP UNDER THE FLOOR BEAM UPPER CAP IS CORRODED REMOVED CORRODED NUTPLATE STRAP, REMOVED CORROSION UNDER STRAP, TR
- [SDR FDEA201910302786](https://openairdocs.org/sdr/FDEA201910302786), Oct 30, 2019: NUT PLATE. CORRODED. MAIN CABIN STA 1681 APPROX RBL 24 NUTPLATE STRIP UNDER THE FLOOR BEAM UPPER CAP IS CORRODED REMOVED CORRODED NUTPLATE STRAP , REMOVED CORROSION UNDER STRAP,TREA
- [SDR FDEA2019102872762](https://openairdocs.org/sdr/FDEA2019102872762), Oct 27, 2019: FLOOR SUPPORT. CORRODED. CABIN FLOOR INTERCOSTAL CORRODED BS1675,BL 0 REMOVED AND REPLACED INTERCOSTAL PER B757 SRM 51-40-02 AND DWG # 146N5576
- [SDR FDEA201811283389](https://openairdocs.org/sdr/FDEA201811283389), Nov 28, 2018: PLACARD. LOOSE. POST FLIGHT L1 DOOR SLIDE ARM/DISARM CONDITION INDICATOR RED/GREEN PLACARD LOOSE. RESECURED L1 DOOR ARM/DISARM CONDITION INDICATOR PLACARD, DOOR ARM/DISARM OPS 
- [SDR FDEA201608232959](https://openairdocs.org/sdr/FDEA201608232959), Aug 23, 2016: LIGHT. INOPERATIVE. EMERGENCY SLIDE LIGHT FO R1 PASSENGER DOOR INOPERATIVE. REPLACED BULB.
- [SDR FDEA201512013836](https://openairdocs.org/sdr/FDEA201512013836), Dec 1, 2015: FIRE WARNING. FALSE ACTIVATION. MAIN CARGO FIRE WARNING ILLUMINATED AT APPROX 100 KNOTS ON TAKEOFF ROLL. REJECTED TAKEOFF ACCOMPLISHED & QRH CONSULTED. CRASH & FIRE RESCUE RESPONDED, NEGATIVE 
- [SDR FDEA201509262964](https://openairdocs.org/sdr/FDEA201509262964), Sep 26, 2015: DOUBLER. MISSING. BONDED DOUBLER REPAIR MISSING, RT HORIZONTAL STABILIZER UPPER SKIN NEAR LE, APPROX 24" FROM INBD END OF STABILIZER. REPAIRED IAW IAW SRM 55-10-01-1A FIG 101 & S

All 117: https://openairdocs.org/aircraft/N996FD/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

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