# N985FD: 1990 Boeing 757-230ER

- Status: Valid registration
- Airframe: [Boeing 757-230ER](https://openairdocs.org/model/boeing-757-230er) (registry code 138495A, 221 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: 24737
- Year built: 1990
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 20, 2013
- Certificate issued: September 4, 2012
- Expires: September 30, 2028
- Mode S code: ADBE38
- 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=985FD
- Page: https://openairdocs.org/aircraft/N985FD

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 757-230ER)

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 N985FD.

## FAA accident and incident reports

None matched to N985FD.

## Service difficulty reports (83, 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 FDEA202603110335](https://openairdocs.org/sdr/FDEA202603110335), Mar 11, 2026: LAMP. INOPERATIVE. R1 DOOR EXTERIOR SLIDE LIGHT INOP DURING LIGHT TEST RELAMPED IAW ABOVE REF, OPS CHECK GOOD.
- [SDR FDEA202508121410](https://openairdocs.org/sdr/FDEA202508121410), Aug 12, 2025: ELEC CONNECTOR. SHORTED. ON DEPARTURE, PASSING FL190, SPARKS CAME OUT OF OVERHEAD CIRCUIT BREAKER PANEL. THERE WAS NO SMOKE OR FUMES. LOST LT PFD & MFD, LT FMC, LT GPS. DECLARED AN EMER
- [SDR FDEA202506040837](https://openairdocs.org/sdr/FDEA202506040837), Jun 4, 2025: LAMP. INOPERATIVE. R1 DOOR EXTERIOR SLIDE LIGHT DOES NOT ILLUMINATE DURING TEST AMM: 33-51-06-2-1 RELAMPED R1 DOOR SLIDE LIGHT (MPN 767) IAW ABOVE REF, OPS CHECK GOOD.
- [SDR FDEA202505080738](https://openairdocs.org/sdr/FDEA202505080738), May 8, 2025: BEARING. FAILED. L1 DOOR WOULD NOT CLOSE. REMOVED AND REPLACED L1 DOOR INSIDE HANDLE CAM ASSEMBLY, LATCH ROLLER CRANK BEARING AND COCKING ROLLER CRANK BEARING IN REF. AMM 52-11-
- [SDR FDEA202505050717](https://openairdocs.org/sdr/FDEA202505050717), May 5, 2025: GIRT BAR. LACK OF LUBE. R1 DOOR "SLIDE" ARMED LIGHT WILL NOT ILLIMUNATE. RELAMPED NO HELP. ARM LEVER DOES NOT APPEAR TO MOVE FULL TRAVEL WHEN ARMING AND PRESUME DOOR IS NOT ARMED. COMP
- [SDR FDEA202504150593](https://openairdocs.org/sdr/FDEA202504150593), Apr 15, 2025: SKIN. UNKNOWN. DURING AGING INSP. FOUND EXISTING REPAIR ON O/B LOWER FLAP 102" TO THE O/B EDGE, LH O/B AFT FLAP. COMPLIED WITH - EA # F - 5750-T0383010 P1 TITLE: WINGS - FLIGH
- [SDR FDEA202504150592](https://openairdocs.org/sdr/FDEA202504150592), Apr 15, 2025: SKIN. UNKNOWN. DURING AGING INSP. FOUND EXISTING REPAIR ON O/B LOWER FLAP 14.5" TO THE I/B EDGE, LH O/B AFT FLAP. COMPLIED WITH EA # F-5750-T0383010 P1. THIS IS MAJOR REPAIR.
- [SDR FDEA202309221638](https://openairdocs.org/sdr/FDEA202309221638), Sep 22, 2023: BATTERY PACK. FAILED. ON PDC FOUND L1 DOOR INTERIOR EMERGENCY LIGHT INOP. RELEASED FOR SERVICE PER MEL : 33-51-01-01. REPLACED BATTERY PACK. NO DEFECTS NOTED. CHECKS SATIFACTORY.
- [SDR FDEA202110192572](https://openairdocs.org/sdr/FDEA202110192572), Oct 19, 2021: FRAME. CRACKED. FUSELAGE FRAME 1EA FASTENER HOLE CRACKED AT STA1640 S14R REPAIRED THE CRACKED FASTENER HOLE AT FUSELAGE FRAME STA1640 S14R PER EA: F- 5310-T0364454 P1 & SRM 51-
- [SDR FDEA202102110326](https://openairdocs.org/sdr/FDEA202102110326), Feb 11, 2021: VALVE. FAILED. AFTER T/O AT ABOUT 6000' L/H ENGINE EPR STARTED TO FLUCTUATE ABOUT .05 UP AND DOWN. OIL PRESSURE ALSO FLUCTUATED /- 25 PSI. WE TURNED OFF TAI AND THE ENGINE SEE
- [SDR FDEA202004270807](https://openairdocs.org/sdr/FDEA202004270807), Apr 27, 2020: RUDDER. FAILED. SMIS 985 55-40 5529 23APR20 MEM OPEN U MOD TYPE T MOD NO. F-5540-T0353729 REV NO. PS P1 STABILIZERS - RUDDER - MAINTENANCE PROGRAM INSPECTION COMPLY WITH E..A. 
- [SDR FDEA2019112653092](https://openairdocs.org/sdr/FDEA2019112653092), Nov 25, 2019: SKIN. DENTED. LARGE DENT SHOWING AT NR 8 SLAT WEDGE UPPER SKIN. ACCOMPLISHED REPAIR ON NR 8 SLAT T/E WEDGE UPPER SKIN IAW SRM 57-43-02-2R AND IAW SRM 51-70-10-2R REP 4 AND IA
- [SDR FDEA201911223045](https://openairdocs.org/sdr/FDEA201911223045), Nov 22, 2019: SHEAR WEB. CORRODED. MAIN CABIN BETWEEN STA 1681-1720, BL0-LBL50 WEB CORRODED. REMOVED CORR ON SHEAR WEB STA 1681-1720 BL0 - LBL50 IAW SRM 51-10-02 ALL AREAS IN LIMITS EXCEPT STA 17
- [SDR FDEA201911223044](https://openairdocs.org/sdr/FDEA201911223044), Nov 22, 2019: DOUBLER. CRACKED. MAIN CARGO COMPT. L-4 DOOR INTERNAL STRUCTURE, FWD. AND NEAR TO LOWER CORNER GUSSET HAS 1EA. DEEP GOUGE. REMOVED GUSSET (DOUBLER) L-4 DOOR INTERNAL STRUCTURE LW
- [SDR FDEA2019112213026](https://openairdocs.org/sdr/FDEA2019112213026), Nov 21, 2019: WEB. CORRODED. MAIN CABIN BETWEEN STA 1700-1720, BL0-RBL50 WEB CORRORED. REMOVED CORR ON SHEAR WEB 1700-1720 BL0 -RBL50 IAW B757 SRM 51-10-02. ALL AREA'S IN LIMIITS EXCEPT STA
- [SDR FDEA201905111025](https://openairdocs.org/sdr/FDEA201905111025), May 11, 2019: ARMING LEVER. UNSECURE. DURING SERVICE CHECK FOUND L1 DOOR ESCAPE SLIDE ARMED HANDLE ON FLOOR. REATTACHED THE L-1 DOOR ESCAPE SLIDE ARMING HANDLE REF MM 52-11-02-4-0. A/C OK FOR SERVIC
- [SDR FDEA201901170161](https://openairdocs.org/sdr/FDEA201901170161), Jan 17, 2019: UNKNOWN. MALFUNCTIONED. R FWD ENT DOOR SLIDE LIGHT FAILED TO ILLUMINATE CYCLED R1 DOOR ARM LEVER SEVERAL TIMES WITH NO FAULTS NOTED SLIDE LIGHT CHECKS GOOD, GIRT BAR ENGAGES FREELY AND
- [SDR FDEA201712193414](https://openairdocs.org/sdr/FDEA201712193414), Dec 19, 2017: SKIN. CORRODED. FUEL LEAK AT THE RT WING OVERWING FUELING CAP. EVALUTED THE AREA OF THE RT WING UPPER SURFACE AT FUELING PORT CUTOUT. FOUND CORROSION DAMAGE TO BE OUT OF LIMITS
- [SDR FDEA201712083348](https://openairdocs.org/sdr/FDEA201712083348), Dec 8, 2017: STRINGER. CORRODED. E & E COMPT. CORROSION ON STRINGER S21R BETWEEN STA. 460 TO 480. COMPLIED WITH EA F-5310-T0337218 P1.
- [SDR FDEA201712083347](https://openairdocs.org/sdr/FDEA201712083347), Dec 8, 2017: STRINGER. CORRODED. E & E COMPT. CORROSION ON STRINGERS S20R BETWEEN STA. 460 AND 480. COMPLIED WITH EA F-5310-T0337221 P1.
- [SDR FDEA201709252733](https://openairdocs.org/sdr/FDEA201709252733), Sep 25, 2017: COWLING. DELAMINATED. NR 2 ENGINE RIGHT FAN COWL INNER LOWER FWD SURFACE IS DAMAGED. DAMAGE IS FROM CONTINUED OIL CONTAMINATION FROM EITHER SERVICING OR OIL LEAK AT IDG SERVICE DOOR 
- [SDR FDEA201511193716](https://openairdocs.org/sdr/FDEA201511193716), Nov 19, 2015: SHEAR PLATE. CORRODED. MAIN CABIN SHEAR PLATE HAS CORROSION, BETWEEN LBL 58 & 63, BS 377 - 440. ACCOMPLISHED IAW EA F-5310-T0321725 P1.
- [SDR FDEA201511143607](https://openairdocs.org/sdr/FDEA201511143607), Nov 14, 2015: DOOR FRAME. GOUGED. FORWARD E & E BAY DOOR CUT OUT STATION 231.25 IS DENTED & GOUGED. REPAIRED FWD E & E BAY DOOR CUT OUT, STATION 231.25 IAW EA F-5310-T0321509 P 1. FUSELAGE MAIN 
- [SDR FDEA201501040018](https://openairdocs.org/sdr/FDEA201501040018), Jan 4, 2015: PROXIMITY SENSOR. DIRTY. ON PREFLIGHT FOUND THAT R1 SLIDE ARMED ANNUNCIATOR LIGHT IS INOPERATIVE. INSPECTED IAW AMM 25-66-11-2-0. CLEANED & REMOVED EXCESS GREASE & DEBRIS FROM BOTH GIRT
- [SDR FDEA201412310001](https://openairdocs.org/sdr/FDEA201412310001), Dec 31, 2014: ROLLER. DEFECTIVE. RIGHT FWD ENT DOOR EICAS APPEARED ON LANDING ROLLOUT. FOUND R1 DOOR PARTIALLY OPEN, UNABLE TO CLOSE THE DOOR WITHOUT PUSHING ON THE UPPER AFT CORNER. THE UPPER 
- [SDR FDEA201405151029](https://openairdocs.org/sdr/FDEA201405151029), May 15, 2014: GIRT BAR. LACK OF LUBE. R1 DOOR ARM LIGHT INOPERATIVE. CLEARED AT BLOCKING 1 HOUR ON GROUND LIGHT FAILED AGAIN. CHECKED GIRT BAR FLOOR FITTING ADJUSTMENT, CLEANED AND LUBED SLIDERS IAW
- [SDR FDEA201404110716](https://openairdocs.org/sdr/FDEA201404110716), Apr 11, 2014: LANYARD. OUT OF POSITION. RIGHT ENTRY DOOR VERY DIFFICULT TO ARM, IT FEELS LIKE THE MECHANISM IS LOOSE. FOUND RT ENTRY DOOR ESCAPE SLIDE LANYARD INTERFERING WITH GIRT BAR MECHANISM. STOW
- [SDR FDEA201311042681](https://openairdocs.org/sdr/FDEA201311042681), Nov 4, 2013: ELBOW. LOOSE. LEFT PYLON HIGH PRESSURE LINE ELBOW LOOSE. COMPLIED WITH EA F-2910-T0301760. MAJOR REPAIR.
- [SDR FDEA201311042680](https://openairdocs.org/sdr/FDEA201311042680), Nov 4, 2013: SPACER. WRONG PART. NR 2 ENGINE STRUT FWD HYD LINE AT FEED THROUGH UNION HAS WRONG SPACER INSTALLED AT PYLON SKIN OTBD SIDE. COMPLIED WITH EA F-2910-T0301761. MAJOR REPAIR.
- [SDR FDEA201309122198](https://openairdocs.org/sdr/FDEA201309122198), Sep 12, 2013: STRINGER. CRACKED. STRINGER 2R, BS 440 IS DAMAGED, STRINGER REPAIRED IAW 49799180001 AND EA757-5311-16-F4303, REV.
- [SDR FDEA201309052134](https://openairdocs.org/sdr/FDEA201309052134), Sep 5, 2013: FRAME. CORRODED. AFTER REMOVING THE FLOORBEAM AT BS 1681, CORROSION WAS FOUND ON FRAME AT RBL 02, WL 208.10, BS 1681, RT SIDE
- [SDR FDEA201308201976](https://openairdocs.org/sdr/FDEA201308201976), Aug 20, 2013: SEAT TRACK. CORRODED. UPPER LOBE SEAT TRACK HAS CORROSION BS 440, RBL 45. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. R & R SEAT TRACK IA
- [SDR FDEA201308171921](https://openairdocs.org/sdr/FDEA201308171921), Aug 17, 2013: SKIN. DENTED. EXTERNAL FUSELAGE AT BS 1520 BETWEEN S23-24R DENTED. FOUND DENT TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED SKIN IAW SRM 53-00-01, FIG 2
- [SDR FDEA201308151903](https://openairdocs.org/sdr/FDEA201308151903), Aug 15, 2013: CREASE BEAM. CORRODED. L2 DOOR INBD CREASE BEAM CHORD CORRODED. REMOVED CORROSION IAW-SRM-51-10-02, ORIG. MAT .080 100 PERCENT MAT LOSS, OUT OF LIMITS IAW-SRM-53-30-15 DETAIL VI FIG 1
- [SDR FDEA201308141886](https://openairdocs.org/sdr/FDEA201308141886), Aug 14, 2013: SKIN. MISREPAIRED. FUSELAGE SKIN BETWEEN BS 440-460, STR 16R MISREPAIRED. REPAIRED IAW-SRM-53-00-01 FIG 201, REPAIR 16, CAT "B" MAJOR.
- [SDR FDEA201308141885](https://openairdocs.org/sdr/FDEA201308141885), Aug 14, 2013: SKIN. MISREPAIRED. FUSELAGE SKIN BETWEEN BS 440 - 460, S18-19R MISREPAIRED. REPAIRED IAW-53-00-01, FIG 201 REPAIR 16. CAT "B" MAJOR REPAIR.
- [SDR FDEA201308121834](https://openairdocs.org/sdr/FDEA201308121834), Aug 12, 2013: CREASE BEAM. CORRODED. BS 756 TO 780 LT INBD CREASE BEAM IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53 -30-13, FIG 101, DETAIL VIII. R & R CREASE BEAM BS 760
- [SDR FDEA201308061798](https://openairdocs.org/sdr/FDEA201308061798), Aug 6, 2013: FLOORBEAM. DAMAGED. FLOORBEAM UPPER TE AT BS 310.5 HAS AREAS WITH GOUGES, NICKS AND SCRATCHES. REMOVED NICKS, GOUGES, AND SCRATCHES IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW 
- [SDR FDEA201308021749](https://openairdocs.org/sdr/FDEA201308021749), Aug 2, 2013: SEAT TRACK. GOUGED. MAIN DECK SEAT TRACK BS 440 TO 645 RBL 24.75 GOUGED AND SCRATCHED. REMOVED GOUGES AND SCATCHES IAW-SRM-53-00-52 AT STA 440-645, RBL 24.75 SEAT TRACK, ORIG MAT .
- [SDR FDEA201308021753](https://openairdocs.org/sdr/FDEA201308021753), Aug 2, 2013: SEAT TRACK. DAMAGED. AFTER REMOVING SEAT TRACK AT STA 1080-1180, LBL 45. A DAMAGED ELONGATED HOLE. FOUND OUT OF LIMITS IAW DWG 144N5024 AND SRM 51-40-02. R & R SEAT TRACK IAW-SRM-51
- [SDR FDEA201308011743](https://openairdocs.org/sdr/FDEA201308011743), Aug 1, 2013: SEAT TRACK. GOUGED. MAIN CABIN SEAT TRACK FROM FS 1540 TO 1600 RBL 24.75 IS GOUGED AND SCRATCHED. BLENDED AREA IAW SRM-53-00-52 FIG 101, FOUND TO BE OUT OF LIMITS IAW SRM-53-00-52,
- [SDR FDEA201308011742](https://openairdocs.org/sdr/FDEA201308011742), Aug 1, 2013: SEAT TRACK. GOUGED. MAIN CABIN SEAT TRACK FROM FS 1540 TO 1600 RBL 45.50 RBL 45.50 IS GOUGED AND SCRATCHED. BLENDED AREA IAW SRM-53-00-52, FIG 101, DETAIL I, FOUND TO BE OUT OF LIM
- [SDR FDEA201307301702](https://openairdocs.org/sdr/FDEA201307301702), Jul 30, 2013: FRAME. CORRODED. FOUND DURING REMOVAL OF WATER SERVICE PAN ASSY. FRAME AT BS 1661 S27-28L CORRODED ON FWD WEB. REMOVED CORROSION IAW-SRM-51-10-02, FOUND TO BE OUT OF LIMITS IAW 
- [SDR FDEA201307291694](https://openairdocs.org/sdr/FDEA201307291694), Jul 29, 2013: FRAME. DENTED. BS 820 FWD CARGO BAY FRAME DENTED BETWEEN S24-25R. FOUND FRAME OUT OF LIMITS, IAW SRM-53-00-07 FIG 101 SHEET 1 , NO DENTS ALLOWED ON FLANGES. R & R FRAME IAW SR
- [SDR FDEA201307251664](https://openairdocs.org/sdr/FDEA201307251664), Jul 25, 2013: STRINGER. CORRODED. CORROSION ON STRINGER 28R, BS 1520, FOUND EXFOLIATED OUT OF LIMITS IAW-SRM-53-00-03 FIG 101 DETAIL PG 102. REMOVED DAMAGED SECTION OF STRINGER IAW-SRM-53-00-03 
- [SDR FDEA201307241656](https://openairdocs.org/sdr/FDEA201307241656), Jul 24, 2013: CREASE BEAM. CORRODED. R2 DOOR AREA, INBD CREASE BEAM CORRODED. REMOVED CORROSION IAW SRM-51-10-02, CHECKED LIMITS IAW-SRM-53-30-15, DET VI FIG 101 FOUND TO BE OUT OF LIMITS. R & R IN
- [SDR FDEA201307221636](https://openairdocs.org/sdr/FDEA201307221636), Jul 22, 2013: FLOORBEAM. CORRODED. FWD CARGO BAY BS 740 RBL 72 TO LBL72, FLOORBEAM IS CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL VI. R & R FLOORBEAM IAW SRM 51-40-02 AND DWG 
- [SDR FDEA201307161576](https://openairdocs.org/sdr/FDEA201307161576), Jul 16, 2013: CREASE BEAM. MISREPAIRED. CREASE BEAM BS 1620 MISREPAIRED. R & R CREASE BEAM BS 1370-1630 WITH A NEW ONE IAW-SRM-51-40-02 AND DWG 146N5590, CAT "A" MAJOR REPAIR.
- [SDR FDEA201307131554](https://openairdocs.org/sdr/FDEA201307131554), Jul 13, 2013: BULKHEAD. GOUGED. LT PYLON, NAC STA 101 BULKHEAD, LT WEB GOUGED.
- [SDR FDEA201307131553](https://openairdocs.org/sdr/FDEA201307131553), Jul 13, 2013: FIREWALL. CHAFED. NR 2 ENGINE STRUT, INBD FIREWALL AFT SIDE CHAFED.

All 83: https://openairdocs.org/aircraft/N985FD/reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Boeing 757-230ER aircraft: https://openairdocs.org/model/boeing-757-230er/aircraft.md
- The Pratt & Whitney PW2037 engine: https://openairdocs.org/engine/pratt-whitney-pw2037.md

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