# Service difficulty reports: N987DN, cancelled Mar 1, 2025

A list on [N987DN, cancelled Mar 1, 2025](https://openairdocs.org/deregistered/N987DN-2025-03-01.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 · 61 reports

- [SDR DALA2020030601668](https://openairdocs.org/sdr/DALA2020030601668.md): Skin · cracked · Mar 6, 2020 · N987DN · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STABILIZER RAM AIR INLET LEADING EDGE IS CRACKED ON THE LEFT SIDE. REPAIRED PER B717 SRM 55-30-01-2R PROCEDURE 1. REQUIRES REPETITIVE VISUAL INSPECTION EVERY 4500 HOURS. (LP #1518223)
- [SDR DALA2019050102763](https://openairdocs.org/sdr/DALA2019050102763.md): Battery Pack · inoperative · Apr 29, 2019 · N987DN · Boeing 717200 · Emergency Lighting
  > MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS OUT IN THE CABIN DURING THE TURN AROUND CHECK. TROUBLE SHOOTING PER MD88 SSM 33-51 FOUND THE BATTERIES B5-123, B5-259, B5-118, B5-121, AND B5-119 TO BE BAD AND REPLACED THEM PER B717 AMM 33-52. ALL OPERATIONS ARE NOW
- [SDR DALA2018041602479](https://openairdocs.org/sdr/DALA2018041602479.md): Wire · loose · Apr 16, 2018 · N987DN · Boeing 717200 · Emergency Lighting
  > THE AFT EMERGENCY EXIT LIGHT CAME ON AND WOULD NOT EXTINGUISH. MAINTENANCE FOUND A LOOSE WIRING AND SECURED IT. THE EMERGENCY EXIT LIGHT WORKS PROPERLY.
- [SDR DALA2018040602228](https://openairdocs.org/sdr/DALA2018040602228.md): Door Frame · corroded · Apr 5, 2018 · N987DN · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON THE SPLICE OF THE DOOR FRAME AT THE AFT CARGO BAY, BS 954 AND 994. THE SPLICES WERE REPLACED IAW SRM 53-20-15-2R FIG 201.
- [SDR DALA201801240085](https://openairdocs.org/sdr/DALA201801240085.md): Tab · delaminated · Jan 24, 2018 · N987DN · Boeing 717200 · Aileron Tabs
  > DURING NON ROUTINE UNSCHEDULED CHECK, FOUND THE AILERON TAB TO BE DELAMINATED.
- [SDR DALA201812210058](https://openairdocs.org/sdr/DALA201812210058.md): Tab · delaminated · Dec 21, 2017 · N987DN · Boeing 717200 · Elevator, Tab Structure
  > CUSTOMER FOUND DURING INSPECTION CHECK DELAMINATION ON LOWER AND UPPER SURFACE- FULL SKIN REPLACEMENT REQUIRED
- [SDR DALA2016040602655](https://openairdocs.org/sdr/DALA2016040602655.md): Power Supply · inoperative · Apr 5, 2016 · N987DN · Boeing 717200 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY FLOOD LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA2016033102566](https://openairdocs.org/sdr/DALA2016033102566.md): Skin · dented · Mar 30, 2016 · N987DN · Boeing 717200 · Rudder, Tab Structure
  > DENT ON RUDDER TAB L/H SIDE, 33" FROM LOWER EDGE AND 5" FROM AFT EDGE. CUT OUT DAMAGED AREA IN RUDDER TAB LT SIDE AND ACCOMPLISHED A HOT BOND DOUBLER REPAIR IAW SRM 55-41-01.
- [SDR DALA2016033102565](https://openairdocs.org/sdr/DALA2016033102565.md): Skin · dented · Mar 30, 2016 · N987DN · Boeing 717200 · Rudder, Tab Structure
  > DENT ON RUDDER TAB RT SIDE, 35" FROM LOWER EDGE AND 6.5" FROM AFT EDGE. CUTOUT DAMAGED AREA ON RUDDER TAB RT SIDE 35" FROM LOWER EDGE AND ACCOMPLISHED A HOT BOND DOUBLER REPAIR IAW SRM 55-41-01, REPAIR 1 AND TC 2000-8149-04.
- [SDR DALA2016032202625](https://openairdocs.org/sdr/DALA2016032202625.md): Floorboard · delaminated · Mar 22, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 222YF IS DELAMINATED WITH 2 EA DAMAGED STIFFENERS AND 1 EACH COVER DAMAGED. MAIN CABIN FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOORBOARD IAW SRM 51-41-08, 51-4
- [SDR DALA2016032202624](https://openairdocs.org/sdr/DALA2016032202624.md): Floorboard · delaminated · Mar 22, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 222ATF IS DELAMINATED. MAIN CABIN FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936584, REV AH.
- [SDR DALA2016032202623](https://openairdocs.org/sdr/DALA2016032202623.md): Keelbeam · cracked · Mar 21, 2016 · N987DN · Boeing 717200 · Fuselage Main, Keel
  > RT KEELBEAM BARREL FORMER CRACKED AT BS 696 OTBD END. RELACED RT KEELBEAM FORMER AT BS 696 OTBD END. CRACK DIM. 4.0" IAW SRM 51-41-02, 51-41-05, DWG 9923418, REV AB, AND 9923453, REV A.
- [SDR DALA2016031802622](https://openairdocs.org/sdr/DALA2016031802622.md): Floorboard · delaminated · Mar 18, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 222ADF IS DELAMINATED WITH DAMAGE TO LT COVER AND RT STIFFENER. MAIN CABIN FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL WITH 1 EA NEW STIFFENER AND 1 EAC
- [SDR DALA2016031702621](https://openairdocs.org/sdr/DALA2016031702621.md): Keelbeam · corroded · Mar 16, 2016 · N987DN · Boeing 717200 · Fuselage Main, Keel
  > UNDER WING BARREL KEELBEAM AT BS 679 OTBD END OF FORMER CRACKED RT SIDE. REMOVED FORMER AND SHEAR CLIP FROM RT OF UNDER WING BARREL KEELBEAM AT BS 679, AND LOCATED, DRILLED, AND DEBURR NEW FORMER AND SHEAR CLIP IAW SRM 51-40-08, AND FABRICATED REPAIR ANGLE TO
- [SDR DALA2016031702620](https://openairdocs.org/sdr/DALA2016031702620.md): Keelbeam · corroded · Mar 16, 2016 · N987DN · Boeing 717200 · Fuselage Main, Keel
  > UNDER WING BARREL KEELBEAM BS 695, LONG 29R CORRODED. UNDER WING BARREL KEELBEAM LONGERON 29RT, FITTING FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-00. REPLACED LONGERON FITTING IAW SRM 51-41-05, DWG 5971090, REV AB, AND REV AF.
- [SDR DALA2016031702619](https://openairdocs.org/sdr/DALA2016031702619.md): Keelbeam · corroded · Mar 16, 2016 · N987DN · Boeing 717200 · Fuselage Main, Keel
  > UNDER WING BARREL KEELBEAM BS 662 LONG 29LT CORRODED. CORROSION DAMAGE ON UNDER WING KEELBEAM LONGERON 29LT, FITTING, FOUND OUT OF LIMITS. REPAIRED IAW SRM 51-41-05, DWG 5971090, REV AB AND REV AF.
- [SDR DALA2016031702617](https://openairdocs.org/sdr/DALA2016031702617.md): Skin · corroded · Mar 16, 2016 · N987DN · Boeing 717200 · Fuselage Main, Plate/Skin
  > AFT CARGO COMPARTMENT DOOR CUTOUT INTERIOR FWD LOWER CORNER BS 946-954 SKIN HAS CORROSION LOWER SURFACE HAS CORROSION AT 4 EA SEAT TRACK N/P'S. CORROSION DAMAGE ON CLOSEOUT WEB AT AFT CARGO COMPARTMENT DOOR CUTOUT INTERIOR SIDE AT 4 EA SEAT TRACK NUTPLATES, OR
- [SDR DALA2016031702618](https://openairdocs.org/sdr/DALA2016031702618.md): Stop Fitting · cracked · Mar 15, 2016 · N987DN · Boeing 717200 · Cargo/Baggage Doors
  > FWD CARGO COMPARTMENT DOOR UPPER FWD INT DOOR STOP FITTING IS CRACKED. REPLACED STOP FITTING FROM FWD CARGO DOOR UPPER FWD INT. ARA IAW SRM 51-41-01, IAW DWG 9957664 REV N AND ALODINED, PRIMED, AND TOP COATED FITTING IAW SRM 51-10-04, AMM 51-10-00.
- [SDR DALA2016031602616](https://openairdocs.org/sdr/DALA2016031602616.md): Keelbeam · cracked · Mar 15, 2016 · N987DN · Boeing 717200 · Fuselage Main, Keel
  > UNDERWING BARREL KEELBEAM-BS 679 OTBD END OF FORMER CRACKED LT. INSTALLED FOR FORMER AT BS 679 IAW SRM 51-41-02, 51-41-05, AND DWG 9923453, REV A. PLEASE DISREGARD SCEPTRE LOG PAGE 2398032 CLOSED IN ERROR. ASSOCIATED ER/A 14-544128 ADDED FOR AC 9587. REMOVE
- [SDR DALA2016031602615](https://openairdocs.org/sdr/DALA2016031602615.md): Keelbeam · cracked · Mar 15, 2016 · N987DN · Boeing 717200 · Fuselage Main, Keel
  > UNDERWING BARREL KEELBEAM BS 679 OTBD END OF FORMER CRACKED LT. INSTALLED FOR FORMER AT BS 679 IAW SRM 51-41-02, 51-41-05, AND DWG 9923453, REV A. ASSOCIATED ER/A 14-544128 ADDED FOR AC 9587.
- [SDR DALA2016031602614](https://openairdocs.org/sdr/DALA2016031602614.md): Floor Panel · damaged · Mar 15, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > FLIGHT COMPARTMENT FLOOR PANEL 211AJF IS DAMAGED. CUTOUT DAMAGED AREA ON FLOOR PANEL NR 211AJF DIM. 2.1250" X 3" IAW SRM 53-10-50 REPAIR 1. FABRICATED REPAIR DOUBLER DIM. 4.3750" X 3.5" X.032", AND FILLER DIM. 2.1250" X 3" X.025", AND INSTALLED REPAIR PARTS
- [SDR DALA2016031602607](https://openairdocs.org/sdr/DALA2016031602607.md): Floorboard · delaminated · Mar 15, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD NR 222LF IS DELAMINATED. FLOORBOARD FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FABRICATED AND INSTALLED A NEW FLOORBOARD IAW 53-20-50, REPAIR 3, DWG 9936585, REV G, AND AMM 53-21-0
- [SDR DALA2016031602606](https://openairdocs.org/sdr/DALA2016031602606.md): Floorboard · delaminated · Mar 15, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD NR 222DF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FABRICATED AND INSTALLED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3, DWG NR 9936688 REV H, AND AMM
- [SDR DALA2016031602605](https://openairdocs.org/sdr/DALA2016031602605.md): Floorboard · delaminated · Mar 15, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD NR 222GF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FABRICATED AND INSTALLED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3, DWG NR 9936688, REV H, AND AMM
- [SDR DALA2016031602608](https://openairdocs.org/sdr/DALA2016031602608.md): Stop Fitting · cracked · Mar 14, 2016 · N987DN · Boeing 717200 · Cargo/Baggage Doors
  > FWD CARGO DOOR MID FWD STOP BRACKET IS CRACKED. REMOVED, LOCATED, DRILLED, AND INSTALLED A NEW BRACKET ALL IAW SRM 51-41-05, 51-40-08 AND DWG 5910141, REV FE, DIM OF CRACK 1.5".
- [SDR DALA2016031502604](https://openairdocs.org/sdr/DALA2016031502604.md): Seat Track · damaged · Mar 14, 2016 · N987DN · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > SCRATCHES AND GOUGES THROUGHOUT SEAT TRACK CROWN AND INNER FLAT SURFACES AT AFT CABIN FLOOR, FROM BS 798 - 898 AND RBL 56.0. REMOVED SCRATCHES AND GOUGES THROUGH OUT SEAT TRACK INNER FLAT SURFACE AND EVALUATED ORIGINAL MATERIAL.100, AND MAT LOSS.045" AND R
- [SDR DALA2016031502603](https://openairdocs.org/sdr/DALA2016031502603.md): Floorboard · delaminated · Mar 14, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 222JF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FABRICATED AND INSTALLED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3, DWG NR 9936585, REV G, AND AMM 53-
- [SDR DALA2016031502602](https://openairdocs.org/sdr/DALA2016031502602.md): Floorboard · delaminated · Mar 14, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 222BF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FABRICATED A NEW FLOORBOARD AND INSTALLED IAW SRM 53-20-50 REPAIR 3, DWG NR 9936585, REV G, AND AMM 53-2
- [SDR DALA2016031502601](https://openairdocs.org/sdr/DALA2016031502601.md): Floorboard · delaminated · Mar 14, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 222AVF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED AND FABRICATED A NEW FLOORBOARD. INSTALLED THE FLOORBOARD IAW SRM 53-20-50, REPAIR 3, DWG 9936584, RE
- [SDR DALA2016031502600](https://openairdocs.org/sdr/DALA2016031502600.md): Floorboard · delaminated · Mar 14, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD NR 221LF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936553, REV C.
- [SDR DALA2016031502599](https://openairdocs.org/sdr/DALA2016031502599.md): Floorboard · delaminated · Mar 14, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 211ALF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50 REPAIR 3 AND DWG 9936537, REV AG.
- [SDR DALA2016031502598](https://openairdocs.org/sdr/DALA2016031502598.md): Floorboard · delaminated · Mar 14, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 221AF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50. REPAIR 3 AND DWG 9936544, REV G.
- [SDR DALA2016031502597](https://openairdocs.org/sdr/DALA2016031502597.md): Floorboard · delaminated · Mar 14, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD NR 221KF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936552, REV K.
- [SDR DALA2016031502596](https://openairdocs.org/sdr/DALA2016031502596.md): Floorboard · delaminated · Mar 14, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 221DF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936547, REV W.
- [SDR DALA2016031502595](https://openairdocs.org/sdr/DALA2016031502595.md): Floorboard · delaminated · Mar 14, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 221HF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9965855, REV G.
- [SDR DALA2016031502594](https://openairdocs.org/sdr/DALA2016031502594.md): Floorboard · delaminated · Mar 14, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 221CF IS DELAMINATED. FLOORBOARD FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936546, REV C.
- [SDR DALA2016031502593](https://openairdocs.org/sdr/DALA2016031502593.md): Floorboard · delaminated · Mar 14, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 221EF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936549 REV K.
- [SDR DALA2016031502592](https://openairdocs.org/sdr/DALA2016031502592.md): Floorboard · delaminated · Mar 14, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 221FF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936547, REV W.
- [SDR DALA2016031502591](https://openairdocs.org/sdr/DALA2016031502591.md): Floorboard · delaminated · Mar 14, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 221JF IS DELAMINATED. FLOORBOARD FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG NR 9936551, REV AN.
- [SDR DALA2016031302590](https://openairdocs.org/sdr/DALA2016031302590.md): Floorboard · delaminated · Mar 12, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 222APF IS DELAMINATED. FLOORBOARD FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50 REPAIR 3 AND DWG 9936585, REV G.
- [SDR DALA2016031302589](https://openairdocs.org/sdr/DALA2016031302589.md): Floorboard · delaminated · Mar 12, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 222AMF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW IAW SRM 53-20-50. REPAIR 3 AND DWG 9936585, REV G.
- [SDR DALA2016031302588](https://openairdocs.org/sdr/DALA2016031302588.md): Floorboard · delaminated · Mar 12, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 222AHF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936585, REV G.
- [SDR DALA2016031302587](https://openairdocs.org/sdr/DALA2016031302587.md): Floorboard · delaminated · Mar 12, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 222AGF IS DELAMINATED. FLOORBOARD FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936585, REV G.
- [SDR DALA2016031302586](https://openairdocs.org/sdr/DALA2016031302586.md): Floorboard · delaminated · Mar 12, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 222AAF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINTED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936640, REV D.
- [SDR DALA2016031302585](https://openairdocs.org/sdr/DALA2016031302585.md): Floorboard · delaminated · Mar 12, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 222ABF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCNET DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936640, REV D.
- [SDR DALA2016031302584](https://openairdocs.org/sdr/DALA2016031302584.md): Floorboard · delaminated · Mar 12, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 221BF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936545, REV M.
- [SDR DALA2016031302583](https://openairdocs.org/sdr/DALA2016031302583.md): Floorboard · delaminated · Mar 12, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 221UF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936585, REV G.
- [SDR DALA2016031302582](https://openairdocs.org/sdr/DALA2016031302582.md): Floorboard · delaminated · Mar 12, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 211ANF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936539, REV AB.
- [SDR DALA2016031302581](https://openairdocs.org/sdr/DALA2016031302581.md): Floorboard · delaminated · Mar 12, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 222PF IS DELAMINATED. MAIN CABIN FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936585, REV G.
- [SDR DALA2016031302580](https://openairdocs.org/sdr/DALA2016031302580.md): Floorboard · delaminated · Mar 12, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 223DF IS DELAMINATED. MAIN CABIN FLOORBOARD FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOORBOARD IAW SRM 53-20-50 REPAIR 3 AND DWG 9936688, REV H.

Next page: https://openairdocs.org/deregistered/N987DN-2025-03-01/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 = 'N987DN' AND deregistration_id = 'N987DN-2025-03-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N987DN-2025-03-01/reports

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