# N995FD: 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: 25131
- Year built: 1992
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 19, 2011
- Certificate issued: January 6, 2011
- Expires: January 31, 2030
- Mode S code: ADE5B7
- 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=995FD
- Page: https://openairdocs.org/aircraft/N995FD

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 N995FD.

## FAA accident and incident reports

None matched to N995FD.

## Service difficulty reports (111, 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 FDEA202610091507](https://openairdocs.org/sdr/FDEA202610091507), Oct 9, 2026: SHUTOFF VALVE. FAULTED. AT FL350, GOT MASTER WARNING CABIN ALTITUDE, WENT TO 12,000FT. (EMERGENCY DECLARED) R & R LT PACK FLOW CONTROL AND SHUTOFF VALVE. OPS CHECK, LEAK CHECK GOOD.
- [SDR FDEA202608281244](https://openairdocs.org/sdr/FDEA202608281244), Aug 28, 2026: EXTINGUISHER. DISCHARGED. WHEN ACFT WAS TOWED INTO GATE AND MX INSP. FOUND NR 1 CARGO FIRE BOTTLE DISCHARGED. AMM: 26-23-02-4 R & R NR 1 CARGO FIRE BOTTLE AND TEST IAW MM 26-23-02-4 WITH
- [SDR FDEA202608271238](https://openairdocs.org/sdr/FDEA202608271238), Aug 27, 2026: SMOKE DETECTOR. INOPERATIVE. ON CLIMBOUT FROM LFT-MEM WE HAD A MAIN CARGO MIDDLE SMOKE DETECTOR LIGHTS 2,3,4 ILLUMINATE . NO OTHER INDICATIORS OF SMOKE OR FIRE, DECLARED EMERGENCY, RETURNED
- [SDR FDEA202409101278](https://openairdocs.org/sdr/FDEA202409101278), Sep 10, 2024: BOTTLE. EMPTY. DURING B-CHECK FOUND AFT O2 BOTTLE AT ZERO PRESSURE. REPLACED BOTTLE PER AMM ON NON ROUTINE 8, PERFORMED MVP ON WRI 0000813271. REMOVED AND REPLACED AFT OXYGEN 
- [SDR FDEA202407060961](https://openairdocs.org/sdr/FDEA202407060961), Jul 6, 2024: GROUND STUD. UNSECURE. EMERGENCY LIGHTS WON'T TEST FROM NOSE GEAR SWITCH S10035. CK OK FROM TEST SWITCH ABOVE L1 DOOR. CHECKED FOR POWER AND GROUND AT SWITCH S10035. POWER GOOD AT TER
- [SDR FDEA202407020912](https://openairdocs.org/sdr/FDEA202407020912), Jul 2, 2024: BATTERY PACK. NO TEST. EMERGENCY LIGHTS WON'T TEST USING ANY/ALL SWITCHES. REMOVED AND REPLACED BATTERY PACK FOR POWER SUPPLY M 730 AND M731 OPS CHECK GOOD REF AMM 33-51-07- 2. PART R
- [SDR FDEA202110082491](https://openairdocs.org/sdr/FDEA202110082491), Oct 8, 2021: SKIN. UNKNOWN. DURING THE ACCOMPLISHMENT OF THE PREVENTATIVE DOUBLER INSTALLATION PER EO F- 5330-E0341230-P12, IT WAS NOTED THAT HAECO MX COULD NOT COMPLY WITH WORK INSTRUCTIO
- [SDR FDEA202110032456](https://openairdocs.org/sdr/FDEA202110032456), Oct 3, 2021: FLAP. DELAMINATED. INBOARD FLAP LOWER INBOARD PANEL IS DELAMINATED. REPAIRED I/B FLAP LOWER I/B PANEL WITH PERMANENT REPAIR IAW B757 SRM 57-53-01-2R FIG 201 SHEET 2 AND 51-70-10-2
- [SDR FDEA202110022446](https://openairdocs.org/sdr/FDEA202110022446), Oct 2, 2021: WEB. DAMAGED. L1 DOOR CUTOUT, INNER WEB AT SNUBBER LOCATION IS DAMAGED DAMAGE BLENDED ON L1 DOOR CUTOUT WEB IAW B757-200 SRM 51-10-02 . ORIGINAL THICKNESS OF WEB IS .050 , RE
- [SDR FDEA202109292431](https://openairdocs.org/sdr/FDEA202109292431), Sep 29, 2021: NONE. NONE. LEFT ELEVATOR LOWER INBOARD SURFACE HAS TWO DENTS REPAIRED LEFT ELEVATOR LOWER INBOARD SURFACE IAW B757 SRM 55-20-01-2R AND 51-70- 05-0G PARA. 5.B.
- [SDR FDEA202109272423](https://openairdocs.org/sdr/FDEA202109272423), Sep 27, 2021: NONE. DELAMINATED. LEFT WING, OUTBOARD FLAP, AFT FLAP, 6 - INCHES FROM INBOARD EDGE POSSIBLLY DELAMINATED. REMOVED DELAMINATED PREVIOUS REPAIR AND REPAIRED LEFT WING OUTBOARD FLAP
- [SDR FDEA202109222356](https://openairdocs.org/sdr/FDEA202109222356), Sep 22, 2021: SKIN. DENTED. FUSELAGE LOWER EXTERIOR SURFACE AT STA 1730 HAS 3 EA PROTRUDING DENTS MEASURED DENTS ON FUSELAGE LOWER EXTERIOR SURFACE SKIN AT STA 1730 , DENT1 : A=.300 AND Y=
- [SDR FDEA202109202351](https://openairdocs.org/sdr/FDEA202109202351), Sep 20, 2021: SEAT TRACK. DAMAGED. MAIN DECK SEAT TRACK SECTION IS DAMAGED @ STA 580, LBL 45 REPAIRED SEAT TRACK SECTION FROM STA 530 - STA 610, LBL 45 IAW FEDEX EA # F-5310-T0364284-P1, RELEASED
- [SDR FDEA202109202349](https://openairdocs.org/sdr/FDEA202109202349), Sep 20, 2021: SKIN. CHAFED. RIGHT WING, OUTBD MAIN FLAP, CENTER LEADING EDGE SKIN HAS 2EA WEAR SPOTS. REPAIRED RH WING OB MAIN FLAP IAW EA F-5750-T0364593-P1,
- [SDR FDEA202004230776](https://openairdocs.org/sdr/FDEA202004230776), Apr 23, 2020: CONTROL PANEL. MALFUNCTIONED. WHILE FINISHING PRE-FLIGHT WITH 'BEFORE START CHECKLIST' COMPLETED 'TO-THE-LINE' THE AFT PEDESTAL FIRE/OVERHEAT FAIL LIGHT WAAS ILLUMINATING INTERMITTENTLY. THE
- [SDR FDEA202004230777](https://openairdocs.org/sdr/FDEA202004230777), Apr 23, 2020: TEST PANEL. CONTAMINATED. AFT PEDESTAL FIRE/OVERHEAT FAIL LIGHT ILLUMINATED INTRMITNLY. SMELLED SMOKE VISUALLY VERIFIED FIRE INSIDE THE AFT PEDESTAL. SHUT DOWN PWR TO AC. AIRCRAFT MX AND
- [SDR FDEA202004080718](https://openairdocs.org/sdr/FDEA202004080718), Apr 8, 2020: BOTTLE. FAILED. L1 DOOR ASSIST BOTTLE HAS BEEN DEPLETED REMOVED REPLACED L-1 DOOR EMERGENCY POWER RESERVOIR PER BOEING AMM 52-11-30-4. A/C OK FOR SERVICE AT THIS TIME.
- [SDR FDEA2020012430213](https://openairdocs.org/sdr/FDEA2020012430213), Jan 23, 2020: PROBE. FAILED. RT AUX PITOT EICAS AND LIGHT 15 MINS INTO FLIGHT. ON DECENT WENT INTO ICING CONDITIONS AFTER CONSULTATION WITH MOCC THAT THIS WOULD BE ACCEPTABLE. GOT EICAS IAS
- [SDR FDEA2019122313276](https://openairdocs.org/sdr/FDEA2019122313276), Dec 21, 2019: SKIN. CHAFED. REWORK REQUIRED OF EA F-5750-T0351491 PT1 STEP 3. REPAIR ACCOMPLISHED IAW SRM 57-53-01-2R REPAIR 2 AND EA F-5750-T0351491 A P1 WING - FLIGHT SURFACES. RT INBOAR
- [SDR FDEA2019121303220](https://openairdocs.org/sdr/FDEA2019121303220), Dec 10, 2019: DOUBLER. WORN. RIGHT WING INBOARD FLAP HAS WORN MARKED IN MULTIPLES AREAS OF LEADING EDGE SURFACE. REMOVED DAMAGE ON RT WING I/B FLAP L/E O/B SIDE AND FOUND DAMAGE AT SKIN PLA
- [SDR FDEA2019120973207](https://openairdocs.org/sdr/FDEA2019120973207), Dec 7, 2019: SKIN. CHAFED. CHAFED MARK SHOWING AT RIGHT WING OUTBOARD FLAP LEADING EDGE. COMPLIED WITH EA F-5750-T0351338 P1 TITLE: WING - FLIGHT SURFACE - RT OUTBOARD MAIN FLAP LEADING E
- [SDR FDEA2019120653191](https://openairdocs.org/sdr/FDEA2019120653191), Dec 5, 2019: SEAT TRACK. CORRODED. MAIN DECK BETWEEN STA 1180 - 1200 BL0 SEAT TRACK FLANGE CORRODED. COMPLIED WITH EA F-5310-T0351165 P1. TITLE FUSELAGE - MAINFRAME - BL 0 SEAT TRACK SPLICE REPAI
- [SDR FDEA2019120653190](https://openairdocs.org/sdr/FDEA2019120653190), Dec 5, 2019: SKIN. WORN. RIGHT WING LEADING EDGE WORN MARKED AT INBOARD SIDE, OUTBD FLAP INBD L/E. BLENDED AREA AT RIGHT WING LEADING EDGE OF O/B FLAP IB SIDE, INBD L/E FOUND AREA OUT O
- [SDR FDEA201912043173](https://openairdocs.org/sdr/FDEA201912043173), Dec 4, 2019: FLOORBEAM. CRACKED. CRACK FLOORBEAM T CAP STA 580 LBL 45.5. COMPLIED WITH EA F-5310-T0351069 P1. TITLE : FUSELAGE - MAINFRAME - STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CR
- [SDR FDEA201912043172](https://openairdocs.org/sdr/FDEA201912043172), Dec 4, 2019: WEB. CORRODED. MAIN DECK BETWEEN STA 1640 - 1681 RBL 50 WEB CORRODED ON TOP AND UNDER NUT PLATE. REMOVED CORROSION IN AREA AT MAIN DECK BETWEEN STA 1640 - 1681 RBL 50 WEB, ORI
- [SDR FDEA201906271419](https://openairdocs.org/sdr/FDEA201906271419), Jun 27, 2019: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ABOVE R1 DOOR AND COCKPIT DOOR INOP. REMOVED AND REPLACED NR 1 RADIANT POWER CORP BATTERY PACK IAW AMM 33-51-07-2. OPS CHECKED GOOD.
- [SDR FDEA201810162935](https://openairdocs.org/sdr/FDEA201810162935), Oct 16, 2018: LIGHT. INOPERATIVE. L1 DOOR EXTERIOR EMER EXIT LIGHT IS INOP. RELAMPED L1 EMER EXIT SLIDE LIGHT REF AMM 33-51-06-2-1, OP'S NORMAL. HISTORY SHOWS POWER SUPPLY R&R AND LOOSE GROUND W
- [SDR FDEA2018091412302](https://openairdocs.org/sdr/FDEA2018091412302), Aug 31, 2018: GROUND WIRE. LOOSE. L1 DOOR EXTERIOR EMERGENCY LIGHT IS INOP. REMOVED LIGHT ASSY FROM A/C FOUND GROUND WIRE LOOSE TIGHTEN WIRE PER GMP AND OPS CHECKED SYSTEM. ALL LITES OK.
- [SDR FDEA201804261129](https://openairdocs.org/sdr/FDEA201804261129), Apr 26, 2018: COMPUTER. MALFUNCTIONED. TCAS WAS NOT SHOWING MULTIPLE KNOWN OTHER TRAFFIC AND ON FINAL COURSE TRAFFIC DIRECTLY IN FRONT OF AIRCRAFT WAS DISPLAYED 20 TO 30 DEGREES RIGHT OF NOSE. REMOVE
- [SDR FDEA201712013329](https://openairdocs.org/sdr/FDEA201712013329), Dec 1, 2017: SKIN. MECHANIC ERROR. REPAIR DOUBLER AT STA. 1380-1400 S23L-26L DOES NOT COMPLY WITH THE SRM. ALL WORK WAS ACCOMPLISHED IAW FEDEX EA F-5330-T0336912 P1 FUSELAGE - PLATES & SKINS - FU
- [SDR FDEA201712013328](https://openairdocs.org/sdr/FDEA201712013328), Dec 1, 2017: SKIN. MECHANIC ERROR. REPAIR DOUBLER AT STA. 1380-1400 S20L-22L DOES NOT COMPLY WITH THE SRM. ALL WORK WAS ACCOMPLISHED IAW FEDEX EA F-5330-T0336913 P1 FUSELAGE- PLATES & SKINS - FUS
- [SDR FDEA201712013327](https://openairdocs.org/sdr/FDEA201712013327), Dec 1, 2017: SKIN. MECHANIC ERROR. REPAIR DOUBLER AT STA. 1560-1580 S17R TO 20R DOES NOT COMPLY WITH THE SRM. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5330-T0336798 P1 FUSELAGE PLATES & SKINS - FUSEL
- [SDR FDEA201711283318](https://openairdocs.org/sdr/FDEA201711283318), Nov 28, 2017: FLOORBEAM. CORRODED. FORWARD WET AREA CORROSION STA 345 FLOORBEAM UPPER CHORD UPPER SURFACE, APPROX BBL 0- LBL 25. REMOVED CORR. ON FLOOR BEAM UPPER CHORD IAW B757 SRM 51-10-02 @ ST
- [SDR FDEA201711283317](https://openairdocs.org/sdr/FDEA201711283317), Nov 28, 2017: SEAT TRACK. CORRODED. FORWARD WET AREA CORROSION LBL8 SEAT TACK FORWARD FLANGE, UPPER SURFACE AT NUT PLATE RIVETS APPROX STA 370. REMOVED CORR LBL8 APPROX STA. 370 SEAT TRACK IAW B75
- [SDR FDEA201711283316](https://openairdocs.org/sdr/FDEA201711283316), Nov 28, 2017: FLOORBEAM. CORRODED. FORWARD WET AREA CORROSION UPPER CHORD, UPPER SURFACE OF STA 365 FLOORBEAM, APPROX RBL 50. REMOVED PREVIOUS REPAIR ON FLOOR BEAM @ STA 365 DUE TO NO ALLOWABLE D
- [SDR FDEA201710172967](https://openairdocs.org/sdr/FDEA201710172967), Oct 17, 2017: POWER SUPPLY. INOPERATIVE. L1 DOOR EMERGENCY SIGN AND L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-07-2, ALL INTERIOR AND EXTERIOR EME
- [SDR FDEA201701100110](https://openairdocs.org/sdr/FDEA201701100110), Jan 10, 2017: LIGHT. INOPERATIVE. RT EXTERIOR SLIDE LIGHT IS INOP. RELEASED FOR SERVICE PER MEL 33-51-02-02.
- [SDR FDEA201511273800](https://openairdocs.org/sdr/FDEA201511273800), Nov 27, 2015: PANEL. CORRODED. MAIN CABIN AFT 9G SHEAR WEB AT STATION 422.5, RBL 15.5, AREA CORROSION. COMPLIED WITH EA F-5310-T0321795 PT1 FUSELAGE-MAINFRAME-MAIN CABIN SHEAR PANEL CORROSION
- [SDR FDEA201508052470](https://openairdocs.org/sdr/FDEA201508052470), Aug 5, 2015: DOOR SILL. DIRTY. L1 CABIN DOOR HANDLE EXTREMELY HARD TO ROTATE & LOCKED CLOSED. CLEANED DEBRIS FROM L1 DOOR SILL & GIRT BAR FLOOR FITTINGS. L1 DOOR OPERATIONS CHECKED NORMAL. OK
- [SDR FDEA201506292115](https://openairdocs.org/sdr/FDEA201506292115), Jun 29, 2015: LIGHT. INOPERATIVE. ONE EXT EMER LIGHT INOPERATIVE. RELAMPED IAW SMP, OPERATIONS NORMAL IAW AMM 33-51-00-5.
- [SDR FDEA201404050667](https://openairdocs.org/sdr/FDEA201404050667), Apr 5, 2014: CAM. WORN. L1 DOOR IS JAMMED. R & R L1 DOOR CONTROL CAM & FWD CRANK BEARING, OPERATIONS CHECKED GOOD IAW AMM 52-11-13-2 & IPC 52-11-13-01C.
- [SDR FDEA201311142784](https://openairdocs.org/sdr/FDEA201311142784), Nov 14, 2013: SKIN. PUNCTURED. ACFT SKIN PUNCTURED BS 1622 BETWEEN S25-26R. REMOVED DAMAGE IAW SRM 51-10-02. FABRICATED REPAIR DOUBLER, STRINGER FILLER AND FILLER IAW SRM 51-40-05, 51-40-08, 
- [SDR FDEA201301260195](https://openairdocs.org/sdr/FDEA201301260195), Jan 26, 2013: LAMP. INOPERATIVE. L1 SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW MM 33-51-06-2-1.
- [SDR FDEA201212254374](https://openairdocs.org/sdr/FDEA201212254374), Dec 25, 2012: COVER. DISLODGED. WHILE OPENING L1 CREW ENTRY DOOR UPPER DOOR HINGE COVER FELL OFF. REPLACED L1 DOOR UPPER HINGE PLATE IN REF TO SRM 51-40-02.
- [SDR FDEA201212064252](https://openairdocs.org/sdr/FDEA201212064252), Dec 6, 2012: WINDSHIELD. FAILED. F/O'S WINDSCREEN SHATTERED ON CLIMBOUT AFTER DE-ICING. RETURNED TO DEPARTURE IAW QRH. R & R IAW AMM 56-11-01-4. F/O'S WINDOW CHECKED SERVICEABLE.
- [SDR FDEA201208042855](https://openairdocs.org/sdr/FDEA201208042855), Aug 4, 2012: CAM. OUT OF RIG. DURING B CHECK, L1 DOOR UPPER FWD CAM PLATE NEEDS TO BE RIGGED. ACCOMPLISHED RIGGING OF L1 DOOR UPPER FWD CAM PLATE IAW AMM. NO FAULTS NOTED.
- [SDR FDEA201208042854](https://openairdocs.org/sdr/FDEA201208042854), Aug 4, 2012: ROLLER. OUT OF ADJUST. DURING B-CHECK, FOUND L1 DOOR UPPER FWD CRANK ARM ROLLER CONTACTS THE CAM PLATE WHEN CLOSING THE DOOR. ACCOMPLISHED RIGGING OF L1 DOOR UPPER FWD CRANK ROLLER CA
- [SDR FDEA201207312768](https://openairdocs.org/sdr/FDEA201207312768), Jul 31, 2012: CIRCUIT BREAKER. MALFUNCTIONED. RT SIDE EMERGENCY EXIT LIGHT STAYS ILLUMINATED WITH DOOR ARMED AND DISARMED. RESET CIRCUIT BREAKERS AND PERFORMED OPS CHECK IAW MM 33-51-00-5. OPS CHECKED GOOD.
- [SDR FDEA201207262701](https://openairdocs.org/sdr/FDEA201207262701), Jul 26, 2012: WINDOW. OUT OF ADJUST. CAPTAIN`S SLIDING WINDOW DOES NOT STAY CLOSED WITH LATCH LOCKED CLOSED. WINDOW WILL CRANK OPEN WITH WINDOW LOCKED CLOSED. PERFORMED ADJUSTMENT TEST IAW MM 56-11
- [SDR FDEA201207262700](https://openairdocs.org/sdr/FDEA201207262700), Jul 26, 2012: WINDOW. OUT OF ADJUST. F/O SLIDING WINDOW DOES NOT STAY CLOSED WITH LOCK IN LOCKED CLOSED. WINDOW WILL CRANK OPEN WITH WINDOW IN LOCKED CLOSED. PERFORMED ADJUSTMENT TEST OF F/O'S SLID

All 111: https://openairdocs.org/aircraft/N995FD/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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