# Service difficulty reports: N988DN, cancelled Mar 1, 2025

A list on [N988DN, cancelled Mar 1, 2025](https://openairdocs.org/deregistered/N988DN-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 · 63 reports

- [SDR DALA2019112806952](https://openairdocs.org/sdr/DALA2019112806952.md): Door Frame · cracked · Nov 27, 2019 · N988DN · Boeing 717200 · Fuselage Main, Structure
  > RH OVERWING EXIT FRAME HAS A CONDITION 3 CRACK AT STA 674 FRAME TAB UPPER RADIUS REF 5310-01436-01D STEP 7. NRC 138-0004:5310-01436-01D/001 00087: REPLACED FRAME REF AMDS 5310-01436-03B. (LP #1377797)
- [SDR DALA2018030501385](https://openairdocs.org/sdr/DALA2018030501385.md): Light · broken · Mar 2, 2018 · N988DN · Boeing 717200 · Emergency Lighting
  > EMERGENCY LIGHT STRIP BROKEN AT SEAT 21B. REINSTALLED THE LIGHT STRIP. CHECKED OK.
- [SDR DALA20180301295](https://openairdocs.org/sdr/DALA20180301295.md): Unknown · malfunctioned · Feb 27, 2018 · N988DN · Boeing 717200 · Trailing Edge Flap Control System
  > THE FLIGHT CREW DECLARED AN EMERGENCY ON APPROACH INTO CAE AFTER THE FLAPS STOPPED EXTENDING BEYOND 18 DEGREES. MAINTENANCE FUNCTIONALLY CHECKED THE FLAP CONTROL SYSTEM, THE FLAP POSITION TRANSMITTERS, THE FLAP RATE TEST, AND THE ADJUSTMENT OF THE FLAP BUS CAB
- [SDR DALA2018022601169](https://openairdocs.org/sdr/DALA2018022601169.md): Power Supply · inoperative · Feb 25, 2018 · N988DN · Boeing 717200 · Emergency Lighting
  > THE OVERWING EMERGENCY LIGHT DOES NOT TURN ON. TROUBLE SHOT PER 33-50-00 810-801. DURING CHECK POWER SUPPLY B5-119 REPLACEMENT BECAME REQUIRED. POWER SUPPLY WAS REPLACED PER AMM 33-51-03 AND TEST WAS PERFORMED PER AMM 33-51-00. OPERATIONAL TEST IS OK.
- [SDR DALA2018022201830](https://openairdocs.org/sdr/DALA2018022201830.md): Skin · cracked · Feb 22, 2018 · N988DN · Boeing 717200 · Service Doors
  > CRACK WAS FOUND OF 0.250" ON R1 FWD SERVICE DOOR, BOTTOM AREA, OUTER SKIN. PERMANENT REPAIR. CRACK ON R1 FWD SERVICE DOOR BOTTOM AREA WAS REPAIRED PER SRM 51-70-01-2R. HFEC INSPECTION WAS ACCOMPLISHED ON R1 FWD SERVICE DOOR BOTTOM AREA, OUTER SKIN AFTER TRIM O
- [SDR DALA2018022301091](https://openairdocs.org/sdr/DALA2018022301091.md): Access Panel · damaged · Feb 22, 2018 · N988DN · Boeing 717200 · Wing, Plate/Skin
  > ELONGATED HOLES ON FUEL ACCESS PANEL 520DT ON THE LT WING. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01-2R-2, PAR 5, CONDITION II.
- [SDR DALA2017123009014](https://openairdocs.org/sdr/DALA2017123009014.md): Lens · damaged · Dec 29, 2017 · N988DN · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED. MAINTENANCE REPLACED LIGHT ASSY IAW DRAWING BR9051. OPS CHECKED GOOD.
- [SDR DALA2017032002193](https://openairdocs.org/sdr/DALA2017032002193.md): Battery · discharged · Mar 20, 2017 · N988DN · Boeing 717200 · Emergency Lighting
  > FWD EMERGENCY LIGHT FOUND INOP DURING SERVICE CHECK. REPLACED EMERGENCY LIGHT BATTERY IAW AMM 33-51. OPS CHECK GOOD AT THIS TIME. A/C OK FOR SVC.
- [SDR DALA2016012900837](https://openairdocs.org/sdr/DALA2016012900837.md): Skin · dented · Jan 28, 2016 · N988DN · Boeing 717200 · Fuselage Main, Plate/Skin
  > AA WORK CARD 2330-01340-01A. DURING STEP 3 OF TASK CARD, 7 EA DENT DOTS FOUND AT ANTENNA INSTALLATION AREA. CUT OUT AREAS ON FUSELAGE SKIN BETWEEN BS 332 AND BS 351, BETWEEN LONGERONS 29LT AND 29RT. CUTOUT DIMENSIONS: 8.25" X 4.875" AND 1.875" X 1.125". FABR
- [SDR DALA2016012400588](https://openairdocs.org/sdr/DALA2016012400588.md): Seat Track · corroded · Jan 23, 2016 · N988DN · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 218-589, RBL 54. CORROSION DAMAGE ON MAIN CABIN SEAT TRACK, RBL 54, STA 218-589. FOUND OUT OF LIMITS, ORIGINAL THICKNESS.100", MATERIAL LOSS.042", MATERIAL REMAINING.058" IAW SRM 53-20-52. REPLACED SEAT TRACK IAW
- [SDR DALA2016012300583](https://openairdocs.org/sdr/DALA2016012300583.md): Seat Track · corroded · Jan 22, 2016 · N988DN · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK CORRODED UNDER TIEDOWN BS 237, RBL 44. CORROSION DAMAGE ON MAIN CABIN SEAT TRACK BS 237, RBL 44 FOUND OUT OF LIMITS, ORIGINAL THICKNESS.100", MAT. LOSS 100 PERCENT, DIM. 8" IAW 53-20-52 ALLOWABLE DAMAGE 1 AND DWG S00484, REV B. REPLACE
- [SDR DALA2016012300582](https://openairdocs.org/sdr/DALA2016012300582.md): Floorbeam · corroded · Jan 22, 2016 · N988DN · Boeing 717200 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR SUPPORT, BS 195, LBL 22-LBL 44 CORRODED. CORROSION DAMAGE ON MAIN CABIN FLOOR SUPPORT BS 195, LBL 22-LBL 44 FOUND TO BE OUT OF LIMITS, ORIGINAL THICKNESS.070", MATERIAL LOSS.029", MATERIAL REMAINING.041" DIM 3" X 1" IAW SRM 53-00-00, 53-10
- [SDR DALA2016012100480](https://openairdocs.org/sdr/DALA2016012100480.md): Floor Panel · delaminated · Jan 20, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR 222ADF IS DELAMINATED AND 1 EA COVER DAMAGED. MAIN CABIN FLOOR PANEL NR 222ADF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL AND INSTALLED NEW COVER ON NEW PANEL
- [SDR DALA2016012100479](https://openairdocs.org/sdr/DALA2016012100479.md): Floor Panel · damaged · Jan 20, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL, NR 222YF HAS 2 EA DAMAGED COVERS AND 2 EA DAMAGED STIFFENERS, LT AND RT SIDES. REPLACED MAIN CABIN FLOOR PANEL 222YF STIFFENERS, 2 EA AND COVERS 2 EA IAW SRM 51-41-08 AND DWG 9936639, REV P.
- [SDR DALA2016011600425](https://openairdocs.org/sdr/DALA2016011600425.md): Angle · damaged · Jan 15, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous Structure
  > UPPER ANGLE FOUND TO BE DAMAGED INSIDE OF CENTER TANK, FWD OF ACCESS PANEL 141AL CUTOUT BS 676, LBL 22. REPLACED UPPER ANGLE IAW SRM 51-41-05 AND DWG 9919346, REV. W.
- [SDR DALA2016011600424](https://openairdocs.org/sdr/DALA2016011600424.md): Cusp Web · corroded · Jan 15, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous Structure
  > MAIN CABIN CORRODED ON CUSP WEB CORRODED BETWEEN BS 908 TO 946 RT SIDE. CORROSION DAMAGE FOUND TO BE OUT OF LIMITS IN TWO LOCATIONS, BS 908-927 AND BS 927-946. CUT OUT DAMAGED AREAS AND INSTALLED REPAIR TO ENCOMPASS BOTH AREAS IAW SRM 53-00-55, REPAIR 4.
- [SDR DALA2016011500333](https://openairdocs.org/sdr/DALA2016011500333.md): Floor Support · broken · Jan 14, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous Structure
  > FLIGHT COMPARTMENT FLOOR SUPPORT ANGLE IS BROKEN AT APPROXIMATELY BS 150, RBL 52. REPLACED FLIGHT COMPARTMENT FLOOR SUPPORT ANGLE APPROXIMATELY RBL 52, STA 150 IAW SRM 51-41-02 AND DWG 9936533, REV CM.
- [SDR DALA2016011500326](https://openairdocs.org/sdr/DALA2016011500326.md): Floor Support · cracked · Jan 14, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL 222AFF LOWER HAT CHANNEL CRACKED. REPLACED FLOOR PANEL 222AFF LOWER HAT CHANNEL IN MAIN CABIN IAW SRM 51-20-05, DWG 9952521, REV BB, AND PROCESS STANDARD 1.07-100, REV NEW.
- [SDR DALA2016011500325](https://openairdocs.org/sdr/DALA2016011500325.md): Seat Track · corroded · Jan 14, 2016 · N988DN · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BETWEEN BS 200-265, RBL 24 CORRODED. FOUND TO BE OUT OF LIMITS DUE TO 100 PERCENT MATERIAL LOSS IAW SRM 53-20-52, ALLOWABLE DAMAGE 1 AND DWG S00483, REV A. REPLACED SEAT TRACK SECTION IAW SRM 51-41-01.
- [SDR DALA2016011900471](https://openairdocs.org/sdr/DALA2016011900471.md): Floor Panel · punctured · Jan 13, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR 222ZF HAS A PUNCTURE APPROXIMATELY BS 730, RBL 46. CUTOUT DAMAGED AREA ON MAIN CABIN FLOOR PANEL NR 222ZF, DIM 1.8" X 1.2", FABRICATED REPAIR PARTS, AND INSTALLED REPAIR PARTS, DOUBLER DIM. 4" X 5" IAW SRM 53-20-50, REPAIR 2.
- [SDR DALA2016011400272](https://openairdocs.org/sdr/DALA2016011400272.md): Former · cracked · Jan 13, 2016 · N988DN · Boeing 717200 · Fuselage Main, Frame
  > LEFT KEELBEAM BARREL BS 696-OTBD END OF FORMER CRACKED. DISPLACED BARREL WEB LT KEELBEAM AT BS 696 IAW SRM 51-41-02 AND SRM 51-41-05 TO FOM. REMOVED FORMER IAW SRM 51-41-02 AND SRM 51-41-05. LOCATED, DRILLED, DEBURRED NEW FORMER IAW SRM 51-40-08 AND DWG 9923
- [SDR DALA2016011400271](https://openairdocs.org/sdr/DALA2016011400271.md): Web · cracked · Jan 13, 2016 · N988DN · Boeing 717200 · Fuselage Main, Structure
  > RT SIDE KEELBEAM BARREL BS 696 OTBD END OF FORMER CRACKED. DISPLACED BARREL WEB FOR FOM, R & R RT SIDE KEELBEAM BARREL FORMER, BS 696 IAW SRM 51-41-02, 51-40-05 AND DWG 9923453, REV A, AB, C REINSTALLED IAW SRM 51-41-02 AND 51-41-05.
- [SDR DALA2016011200196](https://openairdocs.org/sdr/DALA2016011200196.md): Support Angle · corroded · Jan 11, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous Structure
  > WING TO BS 813, LONGERON 30 CLIP SUPPORT CORRODED. CORROSION DAMAGE ON WING TO BODY CLIP BS 813, BL 0 FOUND TO BE OUT OF LIMITS, ORIG THICKNESS.156", MATERIAL LOSS.056", MAT REMAINING.100", DIM. 1" X 2" IAW SRM 53-00-00 AND DWG S2914624, REV A. REPLACED C
- [SDR DALA2016011200195](https://openairdocs.org/sdr/DALA2016011200195.md): Former · cracked · Jan 11, 2016 · N988DN · Boeing 717200 · Fuselage Main, Frame
  > RIGHT SIDE KEEL BEAM BARREL BS 679, OTBD END OF FORMER CRACKED. REPLACED RT KEEL BEAM BARREL BS 679 FORMER IAW SRM 51-41-02 AND DWG 9923453, REV A AND REV C. ACCOMPLISHED A REPAIR TO FORMER TO ACCOMMODATE FLANGE SHORTNESS ISSUE IAW ER/A'S 536322-14, REV 0 AND
- [SDR DALA2016011200194](https://openairdocs.org/sdr/DALA2016011200194.md): Former · cracked · Jan 11, 2016 · N988DN · Boeing 717200 · Fuselage Main, Frame
  > LEFT KEEL BEAM BARREL BS 679 OTBD END OF FORMER CRACKED. REPLACED FORMER AS LT KEEL BEAM BARREL BS 679 IAW SRM 51-41-02 AND DWG 9923453, REV C AND REV A. ACCOMPLISHED A REPAIR TO FORMER TO ACCOMMODATE FLANGE SHORTNESS ISSUE IAW ER/A 536323-14, REV 0 AND REV
- [SDR DALA2016011200193](https://openairdocs.org/sdr/DALA2016011200193.md): Support Frame · corroded · Jan 11, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous Structure
  > RT WING TO BODY FAIRING SUPPORT FRAME BS 851 HAS CORROSION UNDER NUT CLIPS. CORROSION DAMAGE ON RT WING TO BODY FAIRING SUPPORT FRAME BS 851 FOUND OUT OF LIMITS, ORIG THICKNESS.050", MATERIAL LOSS.036", MATERIAL REMAINING.014" DIM 12" X 1" IAW SRM 53-00-00
- [SDR DALA2016011100192](https://openairdocs.org/sdr/DALA2016011100192.md): Floor Panel · cracked · Jan 10, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > COCKPIT FLOOR PANEL 211AKF CRACKED. CUT OUT DAMAGED AREA OF COCKPIT FLOOR PANEL 211AKF DIM 2.5" X 1.5" AND INSTALLED A REPAIR IAW SRM 53-10-50 AND 53-10-50, REPAIR 1. DOUBLER DIM. 3.6" X 2.0" CRACK DIM. 1.0".
- [SDR DALA2016011100191](https://openairdocs.org/sdr/DALA2016011100191.md): Cap · cracked · Jan 10, 2016 · N988DN · Boeing 717200 · Elevator Structure
  > LEFT ELEVATOR OTBD END, T/E END CAP CRACKED. REPLACED LT ELEVATOR OTBD END T/E END CAP IAW SRM 51-41-02 AND DWG 5910412, REV DS CRACK DIM.750".
- [SDR DALA2016011100190](https://openairdocs.org/sdr/DALA2016011100190.md): Skin · delaminated · Jan 10, 2016 · N988DN · Boeing 717200 · Rudder, Plate/Skin
  > RUDDER UPPER AFT END DELAMINATED. REPAIRED RUDDER UPPER AFT END DIM 4" X 4" IAW SRM 55-00-01, REPAIR 2.
- [SDR DALA2016011100177](https://openairdocs.org/sdr/DALA2016011100177.md): Seat Track · damaged · Jan 10, 2016 · N988DN · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK HAS SCRATCHES AND GOUGES BETWEEN BS 899- BS 1022, RBL 24. SEAT TRACK SECTION BS 899-1022, RBL 24 FOUND TO BE OUT OF LIMITS DUE TO SCALLOP DAMAGE, ORIGINAL THICKNESS.460", MATERAL LOSS.060", MATERIAL REMAINING.400" IAW SRM 53-20-53 AND
- [SDR DALA2016010900189](https://openairdocs.org/sdr/DALA2016010900189.md): Floor Panel · delaminated · Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 222AEF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222AEF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 21" X 41" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936640, REV. D.
- [SDR DALA2016010900188](https://openairdocs.org/sdr/DALA2016010900188.md): Floor Panel · delaminated · Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 222DF IS DELAMINATED. MAIN CABIN FLOOR PANEL FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 21" X 19" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936688, REV H.
- [SDR DALA2016010900187](https://openairdocs.org/sdr/DALA2016010900187.md): Floor Panel · delaminated · Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 211ANF IS DELAMINATED. MAIN CABIN FLOOR PANEL FOUND TO BE 60 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 22" X 28" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936651, REV U.
- [SDR DALA2016010900186](https://openairdocs.org/sdr/DALA2016010900186.md): Floor Panel · delaminated · Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 222ACF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222ACF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 21" X 41" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936640, REV D.
- [SDR DALA2016010900185](https://openairdocs.org/sdr/DALA2016010900185.md): Floor Panel · delaminated · Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR 222ABF IS DELAMINATED. MAIN CABIN FLOOR PANEL FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 21" X 22" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936640, REV D.
- [SDR DALA2016010900184](https://openairdocs.org/sdr/DALA2016010900184.md): Floor Panel · delaminated · Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 221AF IS DELAMINATED. MAIN CABIN FLOOR PANEL 221AF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 36" X 11" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936544, REV G.
- [SDR DALA2016010900183](https://openairdocs.org/sdr/DALA2016010900183.md): Floor Panel · delaminated · Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 221EF IS DELAMINATED. MAIN CABIN FLOOR PANEL FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 40" X 9" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936549, REV K.
- [SDR DALA2016010900182](https://openairdocs.org/sdr/DALA2016010900182.md): Floor Panel · delaminated · Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 211AQF IS DELAMINATED. MAIN CABIN FLOOR PANEL 211AQF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 11" X 9" IAW SRM 53-20-50. REPAIR 3 AND DWG 9936537, REV AG.
- [SDR DALA2016010900181](https://openairdocs.org/sdr/DALA2016010900181.md): Floor Panel · delaminated · Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR 222FF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222FF FOUND TO BE 60 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 21" X 38" IAW SRM 53-20-50, REPAIR 3 AND DWG NR 9936583 REV E.
- [SDR DALA2016010900180](https://openairdocs.org/sdr/DALA2016010900180.md): Floor Panel · delaminated · Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 222AAF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222AAF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 21" X 22" IAW SRM 53-20-50, REPAIR 3 AND DWG NR 9936640, REV
- [SDR DALA2016010900179](https://openairdocs.org/sdr/DALA2016010900179.md): Floor Panel · delaminated · Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 22GF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222GF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 21" X 19" IAW SRM 53-20-50 REPAIR 3 AND DWG 9936688, REV H.
- [SDR DALA2016010900178](https://openairdocs.org/sdr/DALA2016010900178.md): Floor Panel · delaminated · Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR 211ARF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 211ARF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 15" X 9" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936537, R
- [SDR DALA2016010800098](https://openairdocs.org/sdr/DALA2016010800098.md): Floor Support · corroded · Jan 7, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous Structure
  > MAIN CABIN BETWEEN BS 149-200, LBL 8 FLOOR SUPPORT CORRODED. REMOVED CORROSION FROM MAIN CABIN FLOOR SUPPORT BS 149-200, LBL 8, WITH 100 PERCENT MATERIAL LOSS ORIGINAL MATERIAL.125". R & R WITH NEW FLOOR SUPPORT IAW SRM 51-41-05, 51-41-02, AND DWG 9936534,
- [SDR DALA2016010700092](https://openairdocs.org/sdr/DALA2016010700092.md): Floor Support · corroded · Jan 6, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT CORRODED, BS 145, RBL 44. CORROSION DAMAGE ON FLOOR SUPPORT IN THE MAIN CABIN BS 145, RBL 44 FOUND TO BE OUT OF LIMITS DUE TO 100 PERCENT MATERIAL LOSS, ORIGINAL THICKNESS.070". DIM.1" X 3" IAW SRM 53-00-00 AND DWG S2929169, REV. B.
- [SDR DALA2016010600091](https://openairdocs.org/sdr/DALA2016010600091.md): Seat Track · corroded · Jan 5, 2016 · N988DN · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 589-899, RBL 54. THE SEAT TRACK WAS FOUND OUT LIMITS DUE TO SCALLOP DAMAGE. REPLACED THE SEAT TRACK IAW SRM 51-41-01 AND AMM 53-22-01.
- [SDR DALA2016010500090](https://openairdocs.org/sdr/DALA2016010500090.md): Floor Panel · delaminated · Jan 4, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR 221BF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 221BF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 40" X 36" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936545, REV
- [SDR DALA2016010500089](https://openairdocs.org/sdr/DALA2016010500089.md): Floor Panel · delaminated · Jan 4, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR 221JF IS DELAMINATED. MAIN CABIN FLOOR PANEL 221JF FOUND TO BE 30PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL IAW SRM 53-20-50, REPAIR 3 AND DWG 9936551, REV AN.
- [SDR DALA2016010500088](https://openairdocs.org/sdr/DALA2016010500088.md): Floor Panel · delaminated · Jan 4, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR 221DF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 221DF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 36" X 20" IAW SRM 53-20-50, REPAIR 3 AND DWG NR 9936547, R
- [SDR DALA2016010500087](https://openairdocs.org/sdr/DALA2016010500087.md): Floor Panel · delaminated · Jan 4, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR 211 ASF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 211ASF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 15" X 11" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936539, R
- [SDR DALA2016010500086](https://openairdocs.org/sdr/DALA2016010500086.md): Floor Panel · delaminated · Jan 4, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 211 ATF IS DELAMINATED. MAIN CABIN FLOOR PANEL 211ATF FOUND TO BE 50 PERCENT DELAMINATED AND TO BE OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 15" X 11" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936539, R

Next page: https://openairdocs.org/deregistered/N988DN-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 = 'N988DN' AND deregistration_id = 'N988DN-2025-03-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N988DN-2025-03-01/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.