# Service difficulty reports: N989DN, cancelled Mar 1, 2025

A list on [N989DN, cancelled Mar 1, 2025](https://openairdocs.org/deregistered/N989DN-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 · 79 reports

- [SDR DALA2019120407052](https://openairdocs.org/sdr/DALA2019120407052.md): Release Mech · out of position · Nov 26, 2019 · N989DN · Boeing 717200 · Aerodynamic Fairings
  > TAILCONE RELEASE CAM MECHANISM IS CLOCKED INCORRECTLY. NRC 001-0310:5300-2004/015 00218: RECLOCKED CAM REF AMDS CARD 5352-4002 TAILCONE INSTALL. (LP #1377133)
- [SDR DALA2019112836950](https://openairdocs.org/sdr/DALA2019112836950.md): Skin · corroded · Nov 22, 2019 · N989DN · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION AFT CARGO THRESHOLD DOOR PAN AND LOWER SKIN DOOR CUT OUT. NRC 001-0371:5231-2002/002 00002: COMPLIED WITH ER/A 582992-14 REV O. (LP #1371567)
- [SDR DALA2019111906760](https://openairdocs.org/sdr/DALA2019111906760.md): Pan · corroded · Nov 18, 2019 · N989DN · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND ON THE AFT CARGO DOOR JAMB PAN. MAINTENANCE REPLACED THE LOWER DOOR JAMB PAN SECTION REF B717 SRM 53-20-15-2R PROCEDURE 7. CORROSION LEVEL 1. (LP #1365811)
- [SDR DALA2019101005821](https://openairdocs.org/sdr/DALA2019101005821.md): Lens · missing · Oct 10, 2019 · N989DN · Boeing 717200 · Emergency Lighting
  > THE AFT DOOR EMERGENCY EXIT LIGHT DIFFUSER COVER IS MISSING. MAINTENANCE LOCATED THE LENS AND RESECURED IT. SYSTEM IS NOW OK FOR SERVICE. (LP #6567004)
- [SDR DALA2019100105611](https://openairdocs.org/sdr/DALA2019100105611.md): Battery Pack · inoperative · Oct 1, 2019 · N989DN · Boeing 717200 · Emergency Lighting
  > THE RH OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE RH OVERWING EMERGENCY EXIT LIGHT BATTERY IAW B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. (LP #6172176)
- [SDR DALA2019031901824](https://openairdocs.org/sdr/DALA2019031901824.md): Battery · discharged · Mar 19, 2019 · N989DN · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS AT ROWS 15-19 ARE INOPERATIVE. MAINTENANCE INSTALLED A SERVICEABLE EMERGENCY LIGHT BATTERY POWER SUPPLY AND BATTERY PER AMM 33-51-03. (LP #5291341)
- [SDR DALA2018022001002](https://openairdocs.org/sdr/DALA2018022001002.md): Spar Cap · damaged · Feb 19, 2018 · N989DN · Boeing 717200 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER LEFT FRONT SPAR CAP DAMAGED, BELOW ZFS 52.267. REPAIRED THE SPAR CAP IAW ERA 565658-14AD, REV ORIGINAL.
- [SDR DALA2017060504514](https://openairdocs.org/sdr/DALA2017060504514.md): Frame · cracked · Jun 4, 2017 · N989DN · Boeing 717200 · Fuselage Main, Frame
  > FRAME 1225 CRACKED AT TAIL CONE ALIGNMENT PIN 7 O'CLOCK POSITION. REMOVED DAMAGED AREA REF 497316-14MA. MANUFACTURED DOUBLER AND DRILLED REF 497316-14MA. INSTALLED REPAIR PER RI 559273-14.
- [SDR DALA2017052304108](https://openairdocs.org/sdr/DALA2017052304108.md): Light · contaminated · May 23, 2017 · N989DN · Boeing 717200 · Emergency Lighting
  > OVERWING AISLE OVERHEAD EMERGENCY EXIT SIGN PARTIALLY OBSCURED. REMOVED DEBRIS FROM INSIDE BOTH LENS, OPS CHECKED GOOD.
- [SDR DALA2016073105683](https://openairdocs.org/sdr/DALA2016073105683.md): Connector · failed · Jul 29, 2016 · N989DN · Boeing 717200 · Light System Wiring
  > THE PILOT REPORTED THAT THE EEPL EXIT SIGN AT THE AFT DOOR AND AT THE OVERWING EXITS IN THE CABIN WERE FLASHING ON & OFF AND WOULD NOT RESPOND TO COMMANDS DURING FLIGHT. MAINTENANCE FOUND A FAILED CONNECTOR IN THE WIRE HARNESS FOR THE OVERWING LIGHTS AND REPL
- [SDR DALA2016073105681](https://openairdocs.org/sdr/DALA2016073105681.md): Power Supply · unknown · Jul 29, 2016 · N989DN · Boeing 717200 · Emergency Lighting
  > THE PILOT REPORTED THAT THE EEPL EXIT SIGN AT THE AFT DOOR AND AT THE OVERWING EXITS IN THE CABIN WERE FLASHING ON & OFF AND WOULD NOT RESPOND TO COMMANDS DURING FLIGHT. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY AT P1-119 AND THE FUNCTIONAL CHECK OF T
- [SDR DALA2016072705623](https://openairdocs.org/sdr/DALA2016072705623.md): Switch · intermittent · Jul 27, 2016 · N989DN · Boeing 717200 · Emergency Lighting
  > THE PILOT REPORTED THAT SOME OF THE EMERGENCY LIGHTS IN THE AIRCRAFT HAD ILLUMINATED UNCOMMANDED. MAINTENANCE REPLACED AN INTERMITTENT EMERGENCY LIGHT SWITCH S1-177 IN THE COCKPIT AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA2016072705588](https://openairdocs.org/sdr/DALA2016072705588.md): Light · malfunctioned · Jul 26, 2016 · N989DN · Boeing 717200 · Emergency Lighting
  > THE F/A REPORTED THAT THE EEPL AT THE LOWER SIDEWALL OVERWING AND THE TAIL EXIT LIGHTS HAD ILLUMINATED UNCOMMANDED DURING FLIGHT. MAINTENANCE CYCLED THE EEPL SWITCH IN THE COCKPIT AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA2016041103477](https://openairdocs.org/sdr/DALA2016041103477.md): Light · inoperative · Apr 5, 2016 · N989DN · Boeing 717200 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE LT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.
- [SDR DALA2016030401627](https://openairdocs.org/sdr/DALA2016030401627.md): Frame · cracked · Mar 3, 2016 · N989DN · Boeing 717200 · Fuselage Main, Frame
  > UPPER RADIUS BS 696 OF OVERWING FRAME TAB RT CRACKED. REPLACED FRAME AT RT BS 696 IAW SRM 51-41-02, 51-41-05, DWG SR95530013, REV: A, PN SA95530034-9.
- [SDR DALA2016022201273](https://openairdocs.org/sdr/DALA2016022201273.md): Vane · punctured · Feb 21, 2016 · N989DN · Boeing 717200 · Trailing Edge Flaps
  > RIGHT WING, INBD FLAP VANE, INBD END HAS A PUNCTURE HOLE. REMOVED DAMAGE ON RT WING INBD FLAP VANE INBD END IAW SRM 57-53-01 REPAIR NR 1. MATERIAL REMOVED.75" DIA CIRCLE. FABRICATED.75" FILLER FROM 7075-T6 BARE.016", FABRICATED 11.5" X 4.25" DOUBLER FROM
- [SDR DALA2016102807812](https://openairdocs.org/sdr/DALA2016102807812.md): Cargo Track · corroded · Feb 20, 2016 · N989DN · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO BAY. CARGO TRACK CORRODED AT BS 427 - 655. REMOVED CORROSION IAW SRM 51-10-04. FOUND TO BE BEYOND LIMITS IAW SRM 53-20- 52. REPLACED THE CARGO TRACK IAW SRM 53-20-52 AND DWG 5965411 REV AW.
- [SDR DALA2016021901246](https://openairdocs.org/sdr/DALA2016021901246.md): Longeron · damaged · Feb 18, 2016 · N989DN · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT CENTER LONGERON 30 HAS CHIPPED PAINT, POSSIBLE LIGHT CORROSION FRAME BS 908. REMOVED CORRODED IAW SRM 51-10-04 AT AFT CARGO BS 908, L30. EVALUATED AND FOUND ORIG.093" LOSS.040" REM.053" OUT OF LIMITS IAW SRM 53-00-00 REMOVED, FABRICA
- [SDR DALA2016102707774](https://openairdocs.org/sdr/DALA2016102707774.md): Cargo Track · corroded · Feb 17, 2016 · N989DN · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO BAY, CARGO TRACK CORRODED BS 813 TO 1028 S26L. REMOVED CORROSION IAW SRM 51-10-04. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52 AND 51-30-07 AND DWG 5956331 REV BS. REPLACED FWD CARGO TRACK IAW DWG 5956331 REV BS & BE.
- [SDR DALA2016021802609](https://openairdocs.org/sdr/DALA2016021802609.md): Duct · dented · Feb 17, 2016 · N989DN · Boeing 717200 · Air Distribution System
  > AFT ACCESSORY COMPARTMENT, GROUND AC DUCT LOWER SIDE HAS DENT.
- [SDR DALA2016021801685](https://openairdocs.org/sdr/DALA2016021801685.md): Slat Track · gouged · Feb 17, 2016 · N989DN · Boeing 717200 · Leading Edge Devices
  > RIGHT WING FIXED L/E INBD SIDE OF SLAT TRACK NR 2 HAS GOUGE ON DOUBLER. ASSOCIATED ER/A 14-542808 ADDED FOR AC 9589. REPLACED EXISTING REPAIR AT RT WING FIXED L/E INBD SIDE OF TRACK NR 2 SLAT IAW SRM 51-40-02 AND COMPLIED WITH ER/A 542808-14, REV: ORIGINAL.
- [SDR DALA2016021501050](https://openairdocs.org/sdr/DALA2016021501050.md): Cargo Track · corroded · Feb 1, 2016 · N989DN · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO BAY CARGO TRACK AT BS 813 - 1028, CORRODED, REMOVED CORROSION IAW SRM 51-10-04 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52, FIG 101 & 51-30-07, FIG 18. REPLACED THE CARGO TRACK IAW SRM 51-41-01, 51-41-02, AND DWG 59366 63, REV: W.
- [SDR DALA2016031501960](https://openairdocs.org/sdr/DALA2016031501960.md): Seat Track · damaged · Jan 29, 2016 · N989DN · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK HAS CORROSION, SCRATCHES AND GOUGES BETWEEN BS 237-589, RBL 22. REPLACED MAIN CABIN SEAT TRACK AT RBL 22, FS 237-589 IAW SRM 51-41-01. DAMAGE REMOVED IAW SRM 53-20-52. ORIGINAL MATERIAL 0.100", MATERIAL REMOVED 0.060", MATERIAL REMAINING
- [SDR DALA2016013001039](https://openairdocs.org/sdr/DALA2016013001039.md): Cusp Web · cracked · Jan 29, 2016 · N989DN · Boeing 717200 · Fuselage Miscellaneous Structure
  > MAIN CABIN CUSP WEB CRACKED AT LT BS 674 AND 696 BETWEEN LBL 44 -54. CUT OUT DAMAGE, FABRICATE AND INSTALLED CUSP WEB 7075-T6.020, 2 EA SPLICES 7075-T6.032 IAW SRM 51-41-02 AND 53-00-55, FIG 223.
- [SDR DALA2016013000746](https://openairdocs.org/sdr/DALA2016013000746.md): Angle · cracked · Jan 25, 2016 · N989DN · Boeing 717200 · Fuselage Miscellaneous Structure
  > AFT ACCESSORY COMPARTMENT BS 1152 HAS CRACKED ANGLE L2R. REPLACED ANGLE IAW SRM 51-41-05 AND DWG 9911860, REV L.
- [SDR DALA2016102707768](https://openairdocs.org/sdr/DALA2016102707768.md): Floorbeam · corroded · Jan 24, 2016 · N989DN · Boeing 717200 · Fuselage Main, Floor Beam
  > BS 200 FLOORBEAM IS CORRODED BETWEEN RBL 44 & 52. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53- 00-00. THE FLOORBEAM WAS REPLACED IAW DWG 9936534 REV BW & SRM 51-41-02.
- [SDR DALA2016012400589](https://openairdocs.org/sdr/DALA2016012400589.md): Former · corroded · Jan 23, 2016 · N989DN · Boeing 717200 · Fuselage Main, Structure
  > LEFT KEEL BEAM BARREL, BS 715, OTBD END CORRODED FORMER. REPLACED LT KEELBEAM FORMER BS 715 IAW SRM 51-41-05, DWG 9923454, REV: F. REMOVED CORROSION & EVALUAED DAMAGE ORIGINAL MATERIAL.063 REMAINING.000 AND IS OUT OF LIMITS IAW SRM 53-00-00.
- [SDR DALA2016012500592](https://openairdocs.org/sdr/DALA2016012500592.md): Former · cracked · Jan 22, 2016 · N989DN · Boeing 717200 · Fuselage Main, Structure
  > LEFT KEELBEAM BARREL BS 696, OTBD END OF FORMER CRACKED. REPLACED LT KEELBEAM FORMER BS 696 IAW SRM 51-41-02 AND 51-41-05 AND DWG 9923453, REV C, REV A.
- [SDR DALA2016012400591](https://openairdocs.org/sdr/DALA2016012400591.md): Longeron · cracked · Jan 22, 2016 · N989DN · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > AFT ACCESSORY COMPARTMENT, BS 1133, LONG 2R CRACKED. REMOVED EWIS PROTECTION FROM WORK AREA IAW SWPM 20-10-10. CUTOUT DAMAGED AREA AT AFT ACCESSORY COMPARTMENT BS 1133, LONG 2R, DIM 15" IAW SRM 20-10-10, FABRICATED, LOCATED, AND DRILLED LONGERON SECTION FROM
- [SDR DALA2016012400590](https://openairdocs.org/sdr/DALA2016012400590.md): Former · not reported · Jan 22, 2016 · N989DN · Boeing 717200 · Fuselage Main, Structure
  > REPLACED LT KEELBEAM FORMER BS 696 IAW SRM 51-41-02 AND 51-41-05 AND DWG 9923453, REV C, REV A.
- [SDR DALA2016012400587](https://openairdocs.org/sdr/DALA2016012400587.md): Door Frame · cracked · Jan 22, 2016 · N989DN · Boeing 717200 · Fuselage Main, Structure
  > CRACKED DOOR LANDING AT FWD OTBD CORNER OF GROUND CONDITIONED AIR SUPPLY DOOR CUTOUT. REMOVED DOOR ASSY FOR CONDITIONED AIR GROUND CONNECTION IAW SRM 51-41-01. REMOVED DOOR LANDING IAW SRM 51-41-02. REMOVED AIR GROUND CONNECTION IAW SRM 51-41-02. FABRICATED
- [SDR DALA2016012400586](https://openairdocs.org/sdr/DALA2016012400586.md): Angle · corroded · Jan 21, 2016 · N989DN · Boeing 717200 · Fuselage Miscellaneous Structure
  > FWD GALLEY SERVICE DOOR LOWER JAMB AREA, Z-ANGLE IS CORRODED FWD OF RBL 54 SEAT TRACK AT FS 202. REMOVED CORROSION FWD GALLEY GALLEY SERVICE DOOR LOWER JAMB AREA "Z" ANGLE FWD OF RBL 54, SEAT TRACK AT FS 202 IAW SRM 51-10-04. EVALUATED AREA AND FOUND ORIG MA
- [SDR DALA2016012400585](https://openairdocs.org/sdr/DALA2016012400585.md): Former · cracked · Jan 21, 2016 · N989DN · Boeing 717200 · Fuselage Main, Structure
  > AFT ACCESSORY COMP BS 1116 BELOW LONGERON 15R FORMER CRACKED. REPLACED FORMER BS 1116 BELOW LONGERON 15R IAW SRM 51-41-02.
- [SDR DALA2016102607662](https://openairdocs.org/sdr/DALA2016102607662.md): Doubler · corroded · Jan 19, 2016 · N989DN · Boeing 717200 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE ANTENNA INTERNAL DOUBLER IS CORRODED AT FS 212 BETWEEN L229L & LONGERON 30 IN E&E COMPARTMENT. APPLIED TOP COAT ON AREA IAW AMM 51-10-00 701. REMOVED CORROSION FROM INTERNAL DOUBLER STA 212 BETWEEN 629L & L30L IAW SRM 51-10-04. NO LIMITS IN S
- [SDR DALA2016012100482](https://openairdocs.org/sdr/DALA2016012100482.md): Shear Tie · cracked · Jan 19, 2016 · N989DN · Boeing 717200 · Fuselage Internal Mounting Structure
  > AFT FUSELAGE BS 1022 BULKHEAD FWD FACE SHEAR TIE IS CRACKED BETWEEN LONGERON 6L AND L7L, MARKED. REMOVED SHEAR TIE AT AFT FUSELAGE FS 1022 BETWEEN LONG 6L TO L7L IAW SRM 51-40-02, LOCATED, DRILLED, AND DEBURRED NEW SHEAR TIE IAW SRM 51-40-08. INSTALLED NEW S
- [SDR DALA2016012000473](https://openairdocs.org/sdr/DALA2016012000473.md): Former · cracked · Jan 19, 2016 · N989DN · Boeing 717200 · Fuselage Main, Frame
  > AFT ACCESSORY COMPARTMENT BS 1116 BELOW LONG 15L FORMER CRACKED. REMOVED FORMER BS 1116, BELOW LONGERON 15L IAW SRM 51-41-02 LOCATED, DRILLED, AND DEBARRED NEW FORMER IAW SRM 51-40-08 AND DWG 5913596, REV AN. INSTALLED NEW FORMER BS 1116 BELOW LONGERON 15L I
- [SDR DALA2016012000472](https://openairdocs.org/sdr/DALA2016012000472.md): Support · chafed · Jan 19, 2016 · N989DN · Boeing 717200 · Rudder Structure
  > RUDDER L/E PANEL 370GL CENTER MOUNTING SUPPORT IS CHAFED, MARKED. REMOVED DAMAGED SUPPORT AT RUDDER L/E IAW SRM 51-41-02 LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-08 AND DWG 9971306, REV, INSTALLED NEW SUPPORT ON L/E OF RUDDER IAW SRM 51-41-02.
- [SDR DALA2016012300584](https://openairdocs.org/sdr/DALA2016012300584.md): Former · cracked · Jan 16, 2016 · N989DN · Boeing 717200 · Fuselage Main, Structure
  > LEFT KEEL BEAM FORMER BS 674 CRACKED ON OTBD END. INSTALLED NEW FORMER IAW SRM 51-41-02, 51-41-05 AND DWG 9923453, REV C, REV A. REPLACED KEEL BEAM FORMER BS 674 IAW SRM 51-41-02 AND 51-41-05 COMPLIED WITH ER/A 542797-14, REV O FOR ALL OTHER WORK REQUIRED. A
- [SDR DALA2016102607661](https://openairdocs.org/sdr/DALA2016102607661.md): Panel · corroded · Jan 15, 2016 · N989DN · Boeing 717200 · Fuselage Main, Keel
  > LT KEEL BEAM PANEL BETWEEN STA 715-747 LONG 30 TO OB SIDE OF CONT KEEL EDGE CORRODED. INSTALLED FASTENERS LT KEEL BEAM STA 715-747 IAW SRM 51-41-02. REMOVED CORROSION LT KEEL BEAM STA 715-747 LONG 30 TO OB SIDE OF CANTED KEEL EDGE IAW SRM 51-10-04 C/W NDT UT
- [SDR DALA2016102607660](https://openairdocs.org/sdr/DALA2016102607660.md): Keelbeam · corroded · Jan 14, 2016 · N989DN · Boeing 717200 · Fuselage Main, Keel
  > LT KEEL BEAM BARREL, BETWEEN STA 715-696 LONG 30 TO OB SIDE OF CANT KEEL EDGE CORRODED. TOPCOATED LT KEEL BEAM BARREL IAW SRM 51-10-04. REMOVED CORROSION LT KEEL BEAM STA 696-715 LONG 30 TO OB SIDE OF CANTED KEEL EDGE IAW SRM 51-10-04. C/W NDT UT INSPECTION
- [SDR DALA2016012200580](https://openairdocs.org/sdr/DALA2016012200580.md): Floor Panel · damaged · Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 221 AF IS DAMAGED. MAIN CABIN FLOOR PANEL 221AF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50. ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 221AF DIM 36" X 11" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936544, RE
- [SDR DALA2016011600430](https://openairdocs.org/sdr/DALA2016011600430.md): Floor Support · corroded · Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Miscellaneous Structure
  > AFT CARGO - SIDE PLATE FLOOR SUPPORT CORRODED AT BS 994, S 28L MARKED. REMOVED CORROSION AFT CARGO SIDE PLATE FLOOR SUPPORT BS 994 S28L, EVALUATED AREA FOUND ORIGINAL MATERIAL.063, MATERIAL REMOVED.015, MATERIAL REMAINING.048 AND IS FOUND TO BE BEYOND LIMI
- [SDR DALA2016011600429](https://openairdocs.org/sdr/DALA2016011600429.md): Shear Tie · corroded · Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Internal Mounting Structure
  > UPON REMOVAL OF RT KEEL BEAM BARREL FORMER BS 674 FOUND SEVERAL AREAS OF CORROSION ON THE FORMER SHEAR CLIP. REMOVED SHEAR CLIP FROM RT KEELBEAM FORMER BS 674 IAW SRM 51-41-02 FROM SHEAR CLIP AND EVALUATED AREA FOUND ORIGINAL MATERIAL.062", MATERIAL LOSS.0
- [SDR DALA2016011600427](https://openairdocs.org/sdr/DALA2016011600427.md): Floorboard · delaminated · Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD NR 211ATF IS DELAMINATED. 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 DWG 9936539, REV AB.
- [SDR DALA2016011500360](https://openairdocs.org/sdr/DALA2016011500360.md): Floor Panel · damaged · Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 221BF IS DAMAGED. MAIN CABIN FLOOR PANEL 221BF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 221 BF DIM 40" X 36" IAW SRM 53-20-50 REPAIR 3 AND DWG 9936545, REV M.
- [SDR DALA2016011500359](https://openairdocs.org/sdr/DALA2016011500359.md): Floorboard · delaminated · Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 221LF IS DELAMINATED. MAIN CABIN FLOOR PANEL 221LF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 221LF DIM 21" X 56" IAW SRM 53-20-50, REPAIR 3. DWG 9936553, REV: C.
- [SDR DALA2016011500358](https://openairdocs.org/sdr/DALA2016011500358.md): Floorboard · delaminated · Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 211ANF IS DELAMINATED. MAIN CABIN FLOOR PANEL 211 AND FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 211ANF DIM 22" X 29" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936539 REV
- [SDR DALA2016011500357](https://openairdocs.org/sdr/DALA2016011500357.md): Floorboard · delaminated · Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 222AEF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222 AEF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 222AEF DIM 21" X 41" IAW SRM 53-20-50 REPAIR 3 AND DWG 9936640, RE
- [SDR DALA2016011500356](https://openairdocs.org/sdr/DALA2016011500356.md): Floor Panel · damaged · Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 221EF IS DAMAGED. MAIN CABIN FLOOR PANEL NR 221EF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 221EF DIM 40" X 9" IAW SRM 53-20-50. REPAIR 3 AND DWG 9936549, REV K
- [SDR DALA2016011500355](https://openairdocs.org/sdr/DALA2016011500355.md): Floorboard · delaminated · Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD, 211ALF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 211ALF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 211ALF DIM 40" X 29" IAW SRM 53-20-50, REPAIR 3 AND DWG 993

Next page: https://openairdocs.org/deregistered/N989DN-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 = 'N989DN' AND deregistration_id = 'N989DN-2025-03-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N989DN-2025-03-01/reports

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