# Service difficulty reports: N987FD

A list on [N987FD](https://openairdocs.org/aircraft/N987FD.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 2 · 68 reports

- [SDR FDEA202601090017](https://openairdocs.org/sdr/FDEA202601090017.md): Skin · dented · Jan 9, 2026 · N987FD · Boeing 757231 · Fuselage Main, Plate/Skin
  > RIGHT LOWER FUSELAGE BS 500 STRINGERS S21 TO S22 DENTED. COMPLIED WITH EA F-5330-T0386068 P1. FUSELAGE SKIN NICKS AND PREVIOUS BLENDOUT MARK BETWEEN STA 500 & STA 520, S-21R & S-22R.
- [SDR FDEA202505050716](https://openairdocs.org/sdr/FDEA202505050716.md): Lamp · failed · May 5, 2025 · N987FD · Boeing 757231 · Emergency Lighting
  > R1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. RELAMPED IAW ABOVE REF OPS CHK SERVICEABLE. OK TO CONTINUE.
- [SDR FDEA202402190188](https://openairdocs.org/sdr/FDEA202402190188.md): Web · cracked · Feb 19, 2024 · N987FD · Boeing 757231 · Fuselage Miscellaneous Structure
  > TAIL COMPARTMENT STA 1862 RB8 UNDER AUTOPILOT SERVOS WEB IS CRACKED. FUSELAGE-MAINFRAME-STA 1862 BULKHEAD UPPER WEB CRACKED DUE TO CORROSION-WEB SPLICE AND CHORD STRAP REPAIR ACCOMPLISHED STEPS 1-8 PER EA-5310-T0377991 P1 WITH NO DEVIATION. MAJOR REPAIR
- [SDR FDEA202402130155](https://openairdocs.org/sdr/FDEA202402130155.md): Floorboard · dented · Feb 13, 2024 · N987FD · Boeing 757231 · Fuselage Floor Panel
  > MAIN DECK FOOR PANEL 251MWF HAS BROKEN AND CORRODED INSERTS FABRICATE ZONE 250 FLOORBOARD PANEL 251MWF ON VTMAE TRAVELER # T24/1733499 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR
- [SDR FDEA202305160880](https://openairdocs.org/sdr/FDEA202305160880.md): Holder · failed · May 16, 2023 · N987FD · Boeing 757231 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOVE R1 DOOR WONT TEST REMOVED AND REPLACED R/H EMERGENCY LIGHTS BATTERY PACK REF AMM 33-51-07-2
- [SDR FDEA202206241543](https://openairdocs.org/sdr/FDEA202206241543.md): Relay · faulted · Jun 24, 2022 · N987FD · Boeing 757200 · Aircraft Fuel Filter/Strainer
  > 2HRS INTO FLIGHT AT FL410, FWD AND AFT LEFT FUEL PUMPS BEGAN FLICKERING LOW PRESSURE VIA PRESS LIGHTS. OPENED THE CROSS FEED VALVES, LIGHTS EXTINGUISHED. A FUEL IMBALANCE QUICKLY BEGAN TO DEVELOP, MAX 1,300LBS. DESCENDED TO FL250 TO SUCTION FEED
- [SDR FDEA202203260696](https://openairdocs.org/sdr/FDEA202203260696.md): Skin · corroded · Mar 26, 2022 · N987FD · Boeing 757200 · Fuselage Structure (General)
  > WHILE REMOVING APU INLET DUCT TO F.O.M. THE AFT SIDE OF CUT STRAP WAS FOUND EXFOLIATED. ACCOMPLISHED REPAIR IAW SRM 53-80-15-2R DETAIL I SHEET 2 ON AFT CUT OUT OF APU INLET AT STA. 1825 BETWEEN STRINGERS 5 & 6 FOR CORROSION DAMAGE ON STRAP PART # 148N3141-
- [SDR FDEA202203250692](https://openairdocs.org/sdr/FDEA202203250692.md): Support · corroded · Mar 25, 2022 · N987FD · Boeing 757200 · Standard Practices/Structures
  > CORROSION FOUND BETWEEN STA 345.0 TO 365.0 AT BUTTLINE 0.0. REMOVED CORROSION BETWEEN STA 345.0 TO 365.00 BUTTLINE 0.0 IAW SRM 51-10-02. CHECKED LIMITS AFTER REWORK. DEPTH = 0.048" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A. REMOVED AND REPLACED FLOOR
- [SDR FDEA202203250691](https://openairdocs.org/sdr/FDEA202203250691.md): Angle · corroded · Mar 25, 2022 · N987FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > APU AIR INLET DOOR MANIFOLD ASSY RH SUPPORT ANGLE CORRODED. REMOVED AND REPLACED CORRODED ANGLE WITH A NEW ONE PART # 148N3152-1 BATCH # 0003918563 IAW SRM 51-40-02. MAJOR REPAIR.
- [SDR FDEA202203230660](https://openairdocs.org/sdr/FDEA202203230660.md): Strap · corroded · Mar 23, 2022 · N987FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > WHILE REMOVING THE APU INLET DUCT TO F.O.M. CORROSION WAS FOUND ON THE FWD SIDE OF THE DUCT CUTOUT. REMOVED & REPLACED CORRODED STRAP ON APU INLET DUCT CUTOUT FWD STRAP WITH ONE FABRICATED ON TRAVELER T22/1605340 PART # FX148N3138-20 IAW SRM 51-40-02 & DRA
- [SDR FDEA202203100469](https://openairdocs.org/sdr/FDEA202203100469.md): Floorboard · delaminated · Mar 10, 2022 · N987FD · Boeing 757200 · Passenger Compartment Equipment
  > COURIER AREA FLOOR BOARD 222MBF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 222MBF FROM TRAVELER T22/1602811 IAW DWG SRZ- 25-005 REV. R."MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.
- [SDR FDEA202203100468](https://openairdocs.org/sdr/FDEA202203100468.md): Floorboard · delaminated · Mar 10, 2022 · N987FD · Boeing 757200 · Passenger Compartment Equipment
  > COURIER AREA FLOOR BOARD 222MCF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 222MCF FROM TRAVELER T22/1602800 IAW DWG SRZ- 25-005. "MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.
- [SDR FDEA202203100467](https://openairdocs.org/sdr/FDEA202203100467.md): Floorboard · delaminated · Mar 10, 2022 · N987FD · Boeing 757200 · Passenger Compartment Equipment
  > COURIER AREA FLOOR BOARD 222MDF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 222MDF FROM TRAVELER T22/1602799 IAW DWG SRZ- 25-005 REV. R. "MAJOR REPAIR". PART MARKED IAW GMM 07-0-1001.
- [SDR FDEA202203100466](https://openairdocs.org/sdr/FDEA202203100466.md): Floorboard · delaminated · Mar 10, 2022 · N987FD · Boeing 757200 · Passenger Compartment Equipment
  > COURIER AREA FLOOR BOARD 222MEF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 222MEF FROM TRAVELER T22/1602798 IAW DWG SRZ- 25-005. "MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.
- [SDR FDEA202203100465](https://openairdocs.org/sdr/FDEA202203100465.md): Floorboard · delaminated · Mar 10, 2022 · N987FD · Boeing 757200 · Passenger Compartment Equipment
  > COURIER AREA FLOOR BOARD 222BF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 222BF FROM TRAVELER T22/1602796 IAW DWG SRZ- 25-005. "MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.
- [SDR FDEA202203100464](https://openairdocs.org/sdr/FDEA202203100464.md): Floorboard · delaminated · Mar 10, 2022 · N987FD · Boeing 757* · Passenger Compartment Equipment
  > COURIER AREA FLOOR BOARD 222MAF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 222MAF FROM TRAVELER T22/1602793 IAW DWG SRZ- 25-005 REV. R. "MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.
- [SDR FDEA202203100463](https://openairdocs.org/sdr/FDEA202203100463.md): Floorboard · delaminated · Mar 10, 2022 · N987FD · Boeing 757* · Passenger Compartment Equipment
  > COURIER AREA FLOOF BOARD 222AF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 222AF FROM TRAVELER T22/1602792 IAW DWG SRZ- 25-005 REV. R. "MAJOR REPAIR" AND PART MARKED IAW GMM 07-0-1001.
- [SDR FDEA202203100462](https://openairdocs.org/sdr/FDEA202203100462.md): Floorboard · delaminated · Mar 10, 2022 · N987FD · Boeing 757* · Passenger Compartment Equipment
  > COURIER AREA FLOOR BOARD 221MAF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 221MAF FROM TRAVELER T22/1602730 IAW DWG SRZ-25-005. "MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.
- [SDR FDEA202203100461](https://openairdocs.org/sdr/FDEA202203100461.md): Floorboard · delaminated · Mar 10, 2022 · N987FD · Boeing 757* · Passenger Compartment Equipment
  > COURIER AREA FLOOR BOARD 221AF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 221AF FROM TRAVELER T22/1602729 IAW DWG SRZ- 25-005. "MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.
- [SDR FDEA202203100460](https://openairdocs.org/sdr/FDEA202203100460.md): Floorboard · delaminated · Mar 10, 2022 · N987FD · Boeing 757* · Passenger Compartment Equipment
  > COURIER AREA FLOOR BOARD 221BF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 221BF FROM TRAVELER T22/1602728 IAW DWG SRZ- 25-005. "MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.
- [SDR FDEA202203100459](https://openairdocs.org/sdr/FDEA202203100459.md): Floorboard · delaminated · Mar 10, 2022 · N987FD · Boeing 757* · Passenger Compartment Equipment
  > COURIER AREA FLOOR BOARD 221MBF DELAMINATED. FABRICATED PANEL 221MBF COURIER AREA FLOOR BOARD FROM TRAVELER T22/1602791 IAW DWG SRZ-25-005 REV. R. "MAJOR REPAIR". PART MARKED IAW GMM 07-0-1001.
- [SDR FDEA2020060531121](https://openairdocs.org/sdr/FDEA2020060531121.md): Fitting · lack of lube · Jun 3, 2020 · N987FD · Boeing 757231 · Emergency Equipment
  > L1 DOOR WILL NOT ARM SLIDE. LUBED L1 DOOR GIRT BAR FITTINGS. L1 DOOR ARMS AND DISARMS NORMAL REF MM 25-66-10-2.
- [SDR FDEA202004170756](https://openairdocs.org/sdr/FDEA202004170756.md): Valve · faulty · Apr 17, 2020 · N987FD · Boeing 757231 · Pneumatic Distribution System
  > RT ENG BLEED CAUTION ON TAKEOFF ROLL. REMOVED & REPLACED RIGHT ENGINE RFCC PER AMM 36-11-18-4. REMOVED & REPLACED RIGHT ENGINE HIGH STAGE PILOT VALVE PER AMM 36-11-08-4-2. PERFORMED OPS CHECK OF RIGHT ENGINE RFCC AND HIGH STAGE PILOT VALVE REF AMM 36-11-18-
- [SDR FDEA2020041090727](https://openairdocs.org/sdr/FDEA2020041090727.md): Skin · gouged · Apr 9, 2020 · N987FD · Boeing 757231 · Trailing Edge Flaps
  > RW INBOARD FLAP UPPER SURFACE HAS GOUGES REPAIRED RW INBOARD FLAP UPPER SURFACE GOUGES IAW B757 SRM: 51-40-02, 57-53-01-2A, 51-70-10, 51-20-05, AMM: 51-21-10/701, NDTM PT. 6 51-00-16, 51-00-19, NDTM PT. 4 51-00-05 & EA #F-5750-T0353383; F-5750-T0353383-P1
- [SDR FDEA2020041090726](https://openairdocs.org/sdr/FDEA2020041090726.md): Skin · cracked · Apr 9, 2020 · N987FD · Boeing 757231 · Wing, Plate/Skin
  > LEFT WING I/B FIXED L/E SKIN BEHIND #5 SLAT CRACKED REMOVED DAMAGED LOWER SKIN AND CORE AND REPAIRED IAW B757 SRM 57-41-01 AND B757 SRM 51-70-08-0G. APPLIED FOIL TAPE TO INNER SKIN IAW B757 SRM 57-41-01-0I AND B757 AMM 51-21-04-7. RESTORED INNER SKIN FINIS
- [SDR FDEA2020040870709](https://openairdocs.org/sdr/FDEA2020040870709.md): Stiffener · corroded · Apr 7, 2020 · N987FD · Boeing 757231 · Fluid Service Doors
  > LAVATORY SERVICE DOOR STIFFENER IS CORRODED (119AL) REMOVED AND REPLACED LAVATORY SERVICE DOOR STIFFENER PER BAC DWG #141N8631 REV F AND B757 SRM 51- 40- 02 TOPCOATED AREA PER B757 SRM 51-20-01
- [SDR FDEA202004060703](https://openairdocs.org/sdr/FDEA202004060703.md): Skin · dented · Apr 6, 2020 · N987FD · Boeing 757231 · Horizontal Stabilizer, Plate/Skin
  > LEFT H.STAB UPPER SURFACE HAS NUMEROUS DENTS AUXILIARY SPAR TO FRONT SPAR. REPAIRED LEFT HAND STAB UPPER SURFACE DENTS IAW B757 SRM 55-10-01-1A NOTE I, 51-70- 10-0G, 51-70-10-2R, ALODINED PRIMED AND SEALED REPAIR IAW B757 MM 51-21-04, 51-21-10 AND B757 SR
- [SDR FDEA2020040320658](https://openairdocs.org/sdr/FDEA2020040320658.md): Strap · cracked · Apr 2, 2020 · N987FD · Boeing 757231 · Fuselage Miscellaneous Structure
  > AREA AFT OF THE AFT CARGO COMPARTMENT ST 1661 APPROX RBL 24 MISC MAIN CABIN FLOOR SUPPORT STRUCTURAL STRAP IS CRACKED REPAIRED STRAP IAW B757 SRM 53-00-51-2R PO:958485.5, PO:920167.4, PO:834933.1
- [SDR FDEA201906281425](https://openairdocs.org/sdr/FDEA201906281425.md): Light · inoperative · Jun 28, 2019 · N987FD · Boeing 757231 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT AFT OF L1 DOOR IS INOP. R&R LAMP REF MM 33_51_06_2_1. OPS CK GOOD.
- [SDR FDEA201803140688](https://openairdocs.org/sdr/FDEA201803140688.md): Shear Tie · corroded · Mar 14, 2018 · N987FD · Boeing 757231 · Fuselage Internal Mounting Structure
  > UPON REMOVAL OF DAMAGE OF RT SIDE TRANSITION PANEL, UNDERNEATH OF PANEL. FOUND CORROSION ON SHEAR TIE AT BS 1380 AND STR 26R. EVALUATED SHEAR TIE FOUND TO BE OUT LIMITS IAW SRM 53-00-53-1A, DETAIL V, FIG 101. REMOVED SHEAR TIE AT STA 1380 AND STR 26R IAW SRM 5
- [SDR FDEA201803060607](https://openairdocs.org/sdr/FDEA201803060607.md): Floorbeam · cracked · Mar 6, 2018 · N987FD · Boeing 757231 · Fuselage Main, Floor Beam
  > FWD CARGO BAY MAIN FLOORBEAM AT BS 580, LBL 45.5 IS CRACKED. REPAIRED IAW EA F-5310-T0338759.
- [SDR FDEA201710203014](https://openairdocs.org/sdr/FDEA201710203014.md): Sequence Valve · failed · Oct 20, 2017 · N987FD · Boeing 757231 · Landing Gear Retraction/Extension System
  > ON APPROACH, EXTENDED LANDING GEAR AND RECEIVED A GEAR DISAGREE EICAS. THE NOSE GEAR LIGHT WAS NOT ILLUMINATED. COMPLIED WITH QRH PROCEDURES AND USED THE ALTERNATE GEAR EXTEND SWITCH. UNEVENTFUL LANDING WITH GEAR DOORS LIGHT ILLUMINATED. REMOVED AND REP
- [SDR FDEA201704251260](https://openairdocs.org/sdr/FDEA201704251260.md): Cover · delaminated · Apr 25, 2017 · N987FD · Boeing 757231 · Emergency Equipment
  > CAPTAIN'S ESCAPE ROPE COVER LATCH BROKEN & WILL NOT STAY IN PLACE. THE LATCH NOT BROKEN, BUT FOUND DELAMINATED. LAMINATED AND SECURED THE PANEL IAW AMM 25-51-00-4.
- [SDR FDEA201703301027](https://openairdocs.org/sdr/FDEA201703301027.md): Lock · out of adjust · Mar 30, 2017 · N987FD · Boeing 757231 · Door Warning System
  > MAIN CARGO DOOR LIGHT ILLUMINATED AT 5000 FT, 215 KB, DURING CLIMB OUT. QRH COMPLIED WITH. ADJUSTED FWD LOCK SWITCH IAW AMM 52-72-01-4. ACFT OK FOR SERVICE.
- [SDR FDEA201607202557](https://openairdocs.org/sdr/FDEA201607202557.md): Power Supply · inoperative · Jul 20, 2016 · N987FD · Boeing 757231 · Emergency Lighting
  > LEFT EMERGENCY LIGHT ABOVE L1 DOOR INOPERATIVE. R & R EMERGENCY POWER SUPPLY ASSY IN REF WITH AMM 33-51-0702 AND 33-51-00/501. OPS CK'S GOOD AT THIS TIME.
- [SDR FDEA201607202556](https://openairdocs.org/sdr/FDEA201607202556.md): Power Supply · inoperative · Jul 20, 2016 · N987FD · Boeing 757231 · Emergency Lighting
  > LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE BY L1 DOOR. EMERGENCY POWER SUPPLY ASSY R & R UNDER WRI 33-50/2274. OPS CHECK IN REF WITH AMM 33-51-00/501.
- [SDR FDEA201603010751](https://openairdocs.org/sdr/FDEA201603010751.md): Repair · debonded · Mar 1, 2016 · N987FD · Boeing 757231 · Trailing Edge Flaps
  > DISBOND TOP TE FIX FLAP, STATION 338, RT WING ON EXISTING REPAIR. REMOVED DISBONDED EXISTING REPAIR AND FABRICATED,PREPPED AREA AND HOT BONDED NEW REPAIR TO TOP TE FIX FLAP STA 338 RT WING IAW B757 SRM 51-70-10-2R REPAIR 4. TAP TEST PERFORMED, NO DELAM NOTED
- [SDR FDEA201502070467](https://openairdocs.org/sdr/FDEA201502070467.md): Pseu · failed · Feb 7, 2015 · N987FD · Boeing 757231 · Door Warning System
  > RIGHT EMER DOOR EICAS ALERT CAME ON WITH, EMER DOORS OVERHEAD, DISCRETE LIGHT ON. R & R PSEU IAW AMM 32-09-04-4. ALL CHECKED GOOD. RT EMER DOOR IS NO LONGER DISPLAYED.
- [SDR FDEA201408222289](https://openairdocs.org/sdr/FDEA201408222289.md): Battery Pack · unsecure · Aug 22, 2014 · N987FD · Boeing 757231 · Emergency Lighting
  > ON POST FLIGHT INSPECTION FOUND THAT L1 SLIDE EMER LIGHT & L1 DOOR OVERHEAD EMER EXIT LIGHTS ARE INOPERATIVE AMM. TROUBLE SHOT SYS, FOUND THAT BATTERY PACK WAS NOT SECURED TO THE M731 POWER SUPPLY CAUSING CONNECTION TO BE LOST. REATTACHED & POSITIVELY SECURE
- [SDR FDEA201403130498](https://openairdocs.org/sdr/FDEA201403130498.md): Skin · dented · Mar 13, 2014 · N987FD · Boeing 757231 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN AT BS 524, STRINGER 28R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED DENT IAW SRM 53-00-01, FIG. 201, REPAIR 15. MAJOR REPAIR.
- [SDR FDEA201402170346](https://openairdocs.org/sdr/FDEA201402170346.md): Slat · damaged · Feb 17, 2014 · N987FD · Boeing 757231 · Leading Edge Devices
  > WING, NOTED DURING REPLACEMENT OF NR 7 SLAT INBD SEAL ON SNRM SEQ NR N01672, TWO EACH WRONG FASTENER RIVETS ARE INSTALLED & HOLES ARE FOUND ELONGATED. ACCOMPLISHED EA F-5750-T0304854, WINGS FLIGHT SURFACES NR 7 LE SLAT ELONGATED HOLES REPAIR.
- [SDR FDEA201402130314](https://openairdocs.org/sdr/FDEA201402130314.md): Skin · scratched · Feb 13, 2014 · N987FD · Boeing 757231 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS SCRATCHES BS 1684 - 1694 BETWEEN STRINGER 13A - STRINGER 14A, LT. A SKIN REPAIR WAS ACCOMPLISHED AT STATION 1679 - 1700, STRINGERS 1 - 13A TO 15L, ON STAM WC 6000100458 & EA 757-5361-16-F4480.
- [SDR FDEA201402030252](https://openairdocs.org/sdr/FDEA201402030252.md): Skin · damaged · Feb 3, 2014 · N987FD · Boeing 757231 · Fuselage Main, Plate/Skin
  > INCOMING FUSELAGE SKIN IMPACT STATION 1440 TO 1480, STRINGER 18R. A SKIN REPAIR STATION 1440 - 1480, STRINGER 17R - STRINGER 22R, WAS ACCOMPLISHED ON STAM WC 6000100363 & EA 757-5361-16-F4368, REV WITH FORM 8110-3 ATTACHED, IAW EA F-5330-T0304947. FUSELAGE P
- [SDR FDEA201402030251](https://openairdocs.org/sdr/FDEA201402030251.md): Skin · damaged · Feb 3, 2014 · N987FD · Boeing 757231 · Fuselage Main, Plate/Skin
  > SCRIBE LINE FOUND AT STRINGER 20R LAP SEAM FROM BS 1439.625 TO BS 1459. SCRIBE LINE REPAIR AT LAP SEAM STRINGER 20R BETWEEN BS 1439.625 TO BS 1459 WAS ACCOMPLISHED ON STAM WC 6000100363 & EA 757-5361-F4368 REV. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY.
- [SDR FDEA201401220176](https://openairdocs.org/sdr/FDEA201401220176.md): Skin · dented · Jan 22, 2014 · N987FD · Boeing 757231 · Fuselage Main, Plate/Skin
  > LEFT UPPER LOBE EXTERNAL FUSELAGE SKIN CROWN AREA AT STATION 790, BETWEEN STRINGERS 2L & 2R HAS MULTIPLE DENTS. ACCOMPLISHED EA F-5330-T0304259 PT1, FUSELAGE PLATES & SKINS, SKIN SECTION 43. FUSELAGE SKIN DENT REPAIR NEAR STATION 780 & BETWEEN STRINGER 2L
- [SDR FDEA201401210152](https://openairdocs.org/sdr/FDEA201401210152.md): Attach Angle · damaged · Jan 21, 2014 · N987FD · Boeing 757231 · Vertical Stabilizer, Attach Fittings
  > NOTED VERTICAL TIP PANEL ATTACH ANGLES, BOTH LT & RT SIDES HAS NUMEROUS ELONGATED HOLES AT VERTICAL STAB TIP STRUCTURE. FOUND TO BE OUT OF LIMITS IAW DWG 172N3014 SHT 1 REV D. REMOVED ANGLES IAW SRM 51-40-02. FABRICATED NEW ANGLES IAW DWG 172N3014 & SRM 51
- [SDR FDEA201401150105](https://openairdocs.org/sdr/FDEA201401150105.md): Tee Fitting · corroded · Jan 15, 2014 · N987FD · Boeing 757231 · Fuselage Miscellaneous Structure
  > DURING REMOVAL CORROSION FOR NR N01645 FOUND T CHORD PN 148N3615 3 AT STATION 1885, STRINGER 27L TO STRINGER 27R CORRODED. REMOVED CORROSION ON T CHORD IAW SRM 51-10-02. ORIGINAL THICKNESS.125 INCHES, MATERIAL LOSS.016 INCHES, MATERIAL REMAINING.109 INCHES
- [SDR FDEA201401030018](https://openairdocs.org/sdr/FDEA201401030018.md): Frame · dented · Jan 3, 2014 · N987FD · Boeing 757231 · Fuselage Main, Frame
  > AFTER SKIN REPAIR, IT WAS NOTED A DENT ON FRAME FLANGE BS 223.5, 5 INCHES BELOW STRINGER 20R. REPAIRED IAW EA F-5330-T0304738. MAJOR REPAIR.
- [SDR FDEA201401030019](https://openairdocs.org/sdr/FDEA201401030019.md): Skin · dented · Jan 3, 2014 · N987FD · Boeing 757231 · Fuselage Main, Plate/Skin
  > DURING INSPECTION, A DENT WAS FOUND ON SKIN BS 377 BETWEEN STRINGER 23 - 24R. REPAIRED SKIN AREA IAW SRM 53-00-01 REP 16.
- [SDR FDEA201312183010](https://openairdocs.org/sdr/FDEA201312183010.md): Skin · corroded · Dec 18, 2013 · N987FD · Boeing 757231 · Fuselage Main, Plate/Skin
  > BULK CARGO BAY BILGE AREA AIRFONE SUPPORT DOUBLER & PLATE HAS LIGHT CORROSION INCLUDING DOME NUTS BS 1500 - 1520, STRINGERS 28 - 29L. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET II. REPAIRED SKIN IAW SRM 53-00-01,

Next page: https://openairdocs.org/aircraft/N987FD/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 = 'N987FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N987FD/reports

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