# Service difficulty reports: N928DL, cancelled Mar 19, 2019

A list on [N928DL, cancelled Mar 19, 2019](https://openairdocs.org/deregistered/N928DL-2019-03-19.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 · 99 reports

- [SDR DALA2017062304901](https://openairdocs.org/sdr/DALA2017062304901.md): Handset · shorted · Jun 23, 2017 · N928DL · Doug MD88 · Communications System Wiring
  > DURING CLIMBOUT AT APPROX 7500 FT, FLIGHT ATTENDANTS NOTIFIED COCKPIT OF AN ELECTRICAL ODOR WHICH DID DISAPATE. EXACT ORIGIN UNKNOWN BUT CONCENTRATED IN REAR OF AIRCRAFT. FOUND AFT F/A HANDSET HAD BEEN PINCHED AND WORN BY JUMPSEAT CAUSING BARE WIRES TO SHORT
- [SDR DALA2017061304699](https://openairdocs.org/sdr/DALA2017061304699.md): Battery · failed · Jun 13, 2017 · N928DL · Doug MD88 · Smoke Detection
  > FORWARD LAVATORY SMOKE DETECTOR WENT OFF FOR 10 SECONDS WITH NO EVIDENCE OF COMBUSTION. REPLACED THE BATTERY IAW AMM 26-13. OK FOR SERVICE.
- [SDR DALA2017050503590](https://openairdocs.org/sdr/DALA2017050503590.md): Lamp · inoperative · May 5, 2017 · N928DL · Doug MD88 · Emergency Lighting
  > TAIL COMPARTMENT EMERGENCY LIGHT, OVER HEAD IS INOPERATIVE. REPLACED THE LAMPS AND OPS NORMAL.
- [SDR DALA2017033102596](https://openairdocs.org/sdr/DALA2017033102596.md): Panel · delaminated · Mar 30, 2017 · N928DL · Doug MD88 · Wing, Plate/Skin
  > MECHANIC FOUND A CRACK ON THE UNDERNEATH PANLE FWD OF THE SPOILER. FOUND PANEL COMPLETELY DELAMINATED. REMOVED THE DAMAGED PANEL. DRILLED AND TRIMMED A NEW PANEL AND INSTALLED IAW DRAWING 9936823.
- [SDR DALA2017021701305](https://openairdocs.org/sdr/DALA2017021701305.md): Skin · dented · Feb 16, 2017 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > SKIN DENT AT BS 95. REPAIRED IAW SRM 53-03, FIG 36B AND 56B. (LP2893840)
- [SDR DALA2017021301191](https://openairdocs.org/sdr/DALA2017021301191.md): Bulb · inoperative · Feb 12, 2017 · N928DL · Doug MD88 · Emergency Lighting
  > DURING A CHECK, FOUND ROW 15 EF EMERGENCY LIGHT ON SEAT INOPERATIVE. REPLACED THE BULBS IAW 33-23. OPS CHECKED OK.
- [SDR DALA2016120709676](https://openairdocs.org/sdr/DALA2016120709676.md): Battery Pack · discharged · Dec 6, 2016 · N928DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE AT FORWARD GALLEY AND OVERHEAD AT ENTRY DOOR. INSTALLED A NEW BULB IN THE FWD GALLEY RED LIGHT AND CHARGED THE BATTERIES.
- [SDR DALA2016120609641](https://openairdocs.org/sdr/DALA2016120609641.md): Bracket · broken · Dec 5, 2016 · N928DL · Doug MD88 · Aerodynamic Fairings
  > TAIL CONE CAM LOCK RECEPTACLE BRACKET BROKEN FOR ACCESS DOOR. FABRICATED A NEW BRACKET AND INSTALLED IAW DWG 5940163.
- [SDR DALA2016120509537](https://openairdocs.org/sdr/DALA2016120509537.md): Spar Cap · cracked · Dec 5, 2016 · N928DL · Doug MD88 · Wing Spar
  > RIGHT WING WS 164 INTERNAL SPAR LOWER CAP HAS 1/8 INCH LONG CRACK RUNNING FROM UNDER RIB END FITTING TO RADIUS. REPAIRED IAW DRAWING J060271-510 AND ER/A 552142-14AD, REV. ORIG.
- [SDR DALA2016120509536](https://openairdocs.org/sdr/DALA2016120509536.md): Hinge Fitting · cracked · Dec 5, 2016 · N928DL · Doug MD88 · Wing, Control Surface Attach Fittings
  > RIGHT WING REAR SPAR LOWER CAP INBD HINGE FITTING AT XRS 164 SHOWS A CRACK INDICATION. REPAIRED IAW DRAWING J060271-510 AND ER/A 552142-14AD, REV. ORIG.
- [SDR DALA2016100507080](https://openairdocs.org/sdr/DALA2016100507080.md): Fuse · failed · Oct 4, 2016 · N928DL · Doug MD88 · Emergency Lighting
  > 13ED TO 30ED EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOT IAW WDM 33-51-14. REPLACED FUSE IAW CMM 33-21. CHECKED GOOD.
- [SDR DALA2016092106772](https://openairdocs.org/sdr/DALA2016092106772.md): Battery Pack · discharged · Sep 21, 2016 · N928DL · Doug MD88 · Emergency Lighting
  > OVERWING EMERGENCY LIGHT INOPERATIVE. R & R B5-49 BATTERY PACK REF AMM 33-53. OPS CK GOOD.
- [SDR DALA2016091606690](https://openairdocs.org/sdr/DALA2016091606690.md): Wire · damaged · Sep 16, 2016 · N928DL · Doug MD88 · Light System Wiring
  > EMERGENCY LIGHT 19CD. TERMINATED SPLICE AT 19CD IAW SWPM 20 AND EWIS. OPS CHECKED GOOD.
- [SDR DALA2016081906089](https://openairdocs.org/sdr/DALA2016081906089.md): Actuator · failed · Aug 19, 2016 · N928DL · Doug MD88 · Landing Gear Actuator
  > RETURNED TO DEPARTURE, DUE TO RIGHT MAIN LANDING GEAR UNSAFE INDICATION AFTER GEAR RETRACTION. RIGHT MAIN LANDING GEAR RETRACT ACTUATOR FOUND TO BE BYPASSING. REPLACED ACTUATOR PER AMM 32-32-02. COMPLIED WITH NO-GO ODI PREVENTION. CYCLED GEAR 15 TIMES. ALL OP
- [SDR DALA2015073004746](https://openairdocs.org/sdr/DALA2015073004746.md): Cable · broken · Jul 29, 2015 · N928DL · Doug MD88 · Steering Unit
  > BREAK TENSION NOSE WHEEL STEERING CONTROL SYSTEM CABLES ARE BROKEN. REPAIRED IAW AMM 32-51-00.
- [SDR DALA2014102705759](https://openairdocs.org/sdr/DALA2014102705759.md): Inlet · dirty · Oct 24, 2014 · N928DL · Doug MD88 · APU Core Engine
  > CREW REPORTED LIGHT HAZE AND BURNING ODOR IN FORWARD CABIN WITH FIRST CLASS LAVATORY SMOKE DETECTOR SOUNDING DURING CLIMBOUT. CREW REDUCED POWER AND HAZE/ODOR DISSIPATED. PROBLEM RETURNED WITH POWER RE-APPLIED. THE ACFT WAS RETURNED TO DEPARTURE. MAINTENANC
- [SDR DALA14021970928](https://openairdocs.org/sdr/DALA14021970928.md): Skin · cracked · Apr 8, 2014 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > TAIL EXTERIOR, SKIN CRACKED AT STA 1380, JUST ABOVE LONGERON 13L. INSTALLED DOUBLER IAW ER/A 524784-14, REV O, WORK ACCOMPLISHED ON PRI 524784-14 AND N/R 103.
- [SDR DALA14022040928](https://openairdocs.org/sdr/DALA14022040928.md): Frame · cracked · Apr 3, 2014 · N928DL · Doug MD88 · Fuselage Main, Frame
  > LT VERTICAL BS 1429 FRAME WEB CRACKED FWD SIDE, BETWEEN L6 AND L7. REMOVED TAIL ANTI ICE DUCT IAW AMM 30-10-17. REPAIRED LT VERTICAL WEB FRAME STA 1437 WEB CRACK BETWEEN L-8 AND L-9 IAW ER/A 519146-14MA. INSTALLED TAIL ANTI ICE DUCT IAW AMM 30-10-17. NR 125
- [SDR DALA13049040928](https://openairdocs.org/sdr/DALA13049040928.md): Skin · damaged · Oct 2, 2013 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CARGO DOOR SURROUND DOUBLER DAMAGED. REMOVED DOOR DOUBLER. REPAIR INSTALLED ON NR 18 IAW ER/A 518711-14.
- [SDR DALA13049030928](https://openairdocs.org/sdr/DALA13049030928.md): Skin · damaged · Oct 2, 2013 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGE FS 712 - 740 BETWEEN L23-26R. DAMAGE REMOVED IAW SRM 53-04, FIG12C 660169. PERFORMED HFEC ON CUT-OUT AREAS IAW NDT MAN PT 6 CH 6-10-01.001. NO CRACKS NOTED. REPAIR INSTALLED IAW SRM 53-04, FIG 12C.
- [SDR DALA13049020928](https://openairdocs.org/sdr/DALA13049020928.md): Skin · damaged · Oct 2, 2013 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGED AFT OF NR 2 CARGO DOOR, DAMAGE REMOVED AND REPAIRED IAW SRM 53-04, FIG 12C.
- [SDR DALA13048100928](https://openairdocs.org/sdr/DALA13048100928.md): Doubler · dented · Sep 29, 2013 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > INTERNAL DOUBLER DENTED FS 728 BETWEEN L28R AND L27R. DAMAGE R & R IAW PRI 518871-14, REV 1 ON N/R 12.
- [SDR DALA13048090928](https://openairdocs.org/sdr/DALA13048090928.md): Doubler · dented · Sep 29, 2013 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > INTERNAL DOUBLER DENTED AT FS 730 BETWEEN L29R AND L28R. DAMAGE R & R IAW PRI 518871-14 REV 1 ON N/R 12.
- [SDR DALA13048080928](https://openairdocs.org/sdr/DALA13048080928.md): Doubler · cracked · Sep 29, 2013 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > INTERNAL DOUBLER CRACKED AND DENTED FS 725 AT L29R. HFEC VERIFIED CRACK AND MARKED ENDS. DAMAGE REMOVED AND REPAIRED IAW PRI 518871-14, REV 1 ON N/R 12.
- [SDR DALA13048060928](https://openairdocs.org/sdr/DALA13048060928.md): Frame · damaged · Sep 29, 2013 · N928DL · Doug MD88 · Fuselage Main, Frame
  > FORMER AT FS 712 BETWEEN LONGERONS 21R-25R DAMAGED. REMOVED DAMAGES FRAME SECTION. INSTALLED NEW FRAME SECTIONS IAW SRM 53-04, FIG 12C. C/W PRI 518883-14, REV O.
- [SDR DALA13005760928](https://openairdocs.org/sdr/DALA13005760928.md): Power Supply · inoperative · Jan 31, 2013 · N928DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT BOTH OF THE OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MX REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA13000090928](https://openairdocs.org/sdr/DALA13000090928.md): Power Supply · inoperative · Dec 31, 2012 · N928DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT BOTH OF THE AFT OVERWING OVERHEAD EMERGENCY EXIT SIGNS WERE INOPERATIVE. MX REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA12017160928](https://openairdocs.org/sdr/DALA12017160928.md): Power Supply · inoperative · Dec 22, 2012 · N928DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT THE EMERGENCY EXIT SIGN LIGHTS OVER THE LT AND RT SIDES OF ROW 25 IN THE CABIN WERE INOPERATIVE. MX REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA1210390928](https://openairdocs.org/sdr/DALA1210390928.md): Slide · detached · Feb 23, 2012 · N928DL · Doug MD88 · Escape Slide
  > FLIGHT CREW FOUND DOOR 1R SLIDE NOT ATTACHED PROPERLY. MAINTENANCE SECURED SLIDE. AIRCRAFT OKAY FOR SERVICE.
- [SDR DALA1206700928](https://openairdocs.org/sdr/DALA1206700928.md): Battery · discharged · Feb 6, 2012 · N928DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE TWO OVERHEAD EMERGENCY ESCAPE LIGHTING IN THE MOST AFT SECTION OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE OPERATIONAL CHECK WAS GOOD.
- [SDR DALA1163760928](https://openairdocs.org/sdr/DALA1163760928.md): Doubler · damaged · Nov 17, 2011 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > HIDDEN DAMAGE; ELONGATED HOLES ON INNER PRODUCTION DOUBLER OF FUSELAGE SKIN AT STA Y=237 BTW LONGERONS 18LT AND 19LT. REPAIR ACCOMPLISHED ON N/R (TO 226870).
- [SDR DALA1163750928](https://openairdocs.org/sdr/DALA1163750928.md): Skin · damaged · Nov 17, 2011 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > HIDDEN DAMGE; ELONGATED HOLES ON EXTERNAL FUSELAGE SKIN FROM STA Y=229 TO Y=250 BTW LONGERONS 18LT AND 19LT. REPAIR WAS ACCOMPLISHED ON N/R (TO 226865).
- [SDR DALA1163740928](https://openairdocs.org/sdr/DALA1163740928.md): Skin · dented · Nov 17, 2011 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > HIDDEN DAMAGE; DENT ON EXTERNAL FUSELAGE SKIN STA Y=231 AND LONGERON 19L. REPAIR ACCOMPLISHED ON N/R (T0 226875).
- [SDR DALA1163710928](https://openairdocs.org/sdr/DALA1163710928.md): Doubler · damaged · Nov 17, 2011 · N928DL · Doug MD88 · Fuselage Miscellaneous Structure
  > ELONGATED HOLES ON PREVIOUS REPAIR DOUBLER FROM STA Y=229 TO Y=250 AND LONGERON 18LT. DOUBLER REPAIR WAS ACCOMPLISHED IAW IAW ERA 334241-14 REV B.
- [SDR DALA1163700928](https://openairdocs.org/sdr/DALA1163700928.md): Door Frame · corroded · Nov 17, 2011 · N928DL · Doug MD88 · Fuselage Main, Structure
  > SUPPLEMENT TO N/R T0226803. NEW BEAM, INTERCOSTALS STRAPS AND FLOOR SUPPORTS WERE INSTALLED IAW DC9/MD80 SRM 51-30-2 AND51-30-5 AND DOUGLAS DWG 5976038 REV A.
- [SDR DALA1163580928](https://openairdocs.org/sdr/DALA1163580928.md): Cusp Web · corroded · Nov 15, 2011 · N928DL · Doug MD88 · Fuselage Miscellaneous Structure
  > SUPPLEMENT N/R T0225448. NEW SECTION OFF CUSP ANGLE WAS INSTALLED IAW DC9/MD80 SRM 53-05 FIG 25. (TO 225448) (NO ORIG MRR ENTRY FOR "SUPP INFO" TO ATTACH TO)
- [SDR DALA1163530928](https://openairdocs.org/sdr/DALA1163530928.md): Beam · damaged · Nov 15, 2011 · N928DL · Doug MD88 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE ON AFT DOORJAMB BEAM STA Y=427 BTW LONG 24RT-25RT AT C1. REPAIRED PER ERA 497374-14 REV B.
- [SDR DALA1163470928](https://openairdocs.org/sdr/DALA1163470928.md): Skin · damaged · Nov 15, 2011 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV ELONGATED HOLES WAS FOUND ON FUSELAGE SKIN FROM STA Y=1418 TO 1422 BTW LONGERON 1 AND 2RT. CUT OUT DAMAGE AREA OF FUSELAGE SKIN AND INSTALLED FILLER, DOUBLER IAW ERA 497385-14 REV ORIG.
- [SDR DALA1163460928](https://openairdocs.org/sdr/DALA1163460928.md): Skin · cracked · Nov 15, 2011 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV A CRACK WAS FOUND ON FUSELAGE SKIN AT STA Y=1418 BTW LONGERON 1 AND 2RT WITH 0.562" LENGTH. CRACK AREA ON FUSELAGE WAS CUT OUT AND FILLER, DOUBLER INSTALLED IAW ERA 497385-14 REV ORIG.
- [SDR DALA1163350928](https://openairdocs.org/sdr/DALA1163350928.md): Fairing · worn · Nov 15, 2011 · N928DL · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > DURING HMV WEAR WAS FOUND ON OUTER OF VERTICAL STABILIZER TIP FAIRING BETWEEN STA YV=200 AND 220 AT RT AND LT SIDE. BLEND OUT DAMAGE RT SIDE WITHIN LIMITS REF MD88 SRM 55-01 FIG 1 THE LT SIDE WAS REPAIRED IAW ERA 451447-14 REV A.
- [SDR DALA1163310928](https://openairdocs.org/sdr/DALA1163310928.md): Filler · corroded · Nov 14, 2011 · N928DL · Doug MD88 · Fuselage Miscellaneous Structure
  > DURING HMV CORROSION WAS FOUND ON PREVIOUS REPAIR FILLER STA Y=1190=1194 BTW LONGERON 30 TO 29LT C3. FILLER WAS REPLACED IAW MD88 SRM 53-04D FIG 12B.
- [SDR DALA1163150928](https://openairdocs.org/sdr/DALA1163150928.md): Pan · cracked · Nov 13, 2011 · N928DL · Doug MD88 · Cargo/Baggage Doors
  > DURING HMV A CRACK WAS FOUND ON C3 DOOR PAN AT FWD EDGE AND NR 4 BEAM INTERSECTION (UNDER DOOR STOP FITTING POSITION). DOOR PAN WAS STOP DRILLED AND DOUBLER WAS INSTALLED IAW MD88 SRM 52-05 FIG 50.
- [SDR DALA1163140928](https://openairdocs.org/sdr/DALA1163140928.md): Frame · cracked · Nov 13, 2011 · N928DL · Doug MD88 · Fuselage Main, Frame
  > DURING HMV A CRACK WAS FOUND ON FRAME AT STAY=1451 AND LONGERON 1. CRACK ON FRAME WAS BLENDED OUT AND INSTALL FILLER, DOUBLER IAW MD88 SRM 53-03D FIG 4.
- [SDR DALA1163130928](https://openairdocs.org/sdr/DALA1163130928.md): Finger Doubler · damaged · Nov 13, 2011 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV NEED TO RE-EVALUATE OF REPAIR PARTS AT PREVIOUS FUSELAGE SKIN REPAIR ON STA Y=1316-1322 BTW LONGERON 18RT-21RT. REPLACED FINGER DOUBLER IAW MD88 SRM 53-04D FIG 12B.
- [SDR DALA1162880928](https://openairdocs.org/sdr/DALA1162880928.md): Skin · cracked · Nov 11, 2011 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV CRACKS WERE FOUND ON FUSELAGE SKIN AT STA Y=373.750 OF 0.046" LENGTH,Y=374.750 OF 0.046" LENGTH, Y=375.250 OF 0.031" LENGTH AND Y=376.0 OF 0.093" LENGTH OF THE FWD CARGO DOOR JAMB UPPER CORNER. DAMAGED SKIN WAS CUT OUT AND DOUBLERS INSTALLED IAW MD
- [SDR DALA1160570928](https://openairdocs.org/sdr/DALA1160570928.md): Skin · damaged · Oct 30, 2011 · N928DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HNV, LIGHTNING STRIKE WAS FOUND ON LEFT WINDOW BELT FRAME LOWER EDGE STA 275-712 LOWER AFT EDGE. REPAIRED IAW ERA.
- [SDR DALA1160600928](https://openairdocs.org/sdr/DALA1160600928.md): Angle · corroded · Oct 30, 2011 · N928DL · Doug MD88 · Fuselage Miscellaneous Structure
  > DURING HMV, CORROSION WAS FOUND ON CUSP WEB ANGLE FROM BS 148-160 X=-52--60. CUSP WEB WAS REPAIRED IAW ERA 497030-15 REV ORIG.
- [SDR DALA1160610928](https://openairdocs.org/sdr/DALA1160610928.md): Angle · corroded · Oct 30, 2011 · N928DL · Doug MD88 · Fuselage Miscellaneous Structure
  > DURING HMV CORROSION WAS FOUND ON CUSP WEB ANGLE STA Y=197 BTW X=-54--60. ANGLE WAS REPAIRED IAW ERA 497030-14 REV ORIGINAL AND DWG 9910078 REV JC.
- [SDR DALA1160630928](https://openairdocs.org/sdr/DALA1160630928.md): Cusp Web · corroded · Oct 30, 2011 · N928DL · Doug MD88 · Fuselage Miscellaneous Structure
  > DURING HMV, CORROSION WAS FOUND ON RT CUSP WEB. REPAIRED IAW SRM 53-20-02D.
- [SDR DALA1160620928](https://openairdocs.org/sdr/DALA1160620928.md): Cusp Web · corroded · Oct 30, 2011 · N928DL · Doug MD88 · Fuselage Miscellaneous Structure
  > DURING HMV, CORROSION WAS FOUND ON RT CUSP WEB BTW X-54--60 BS 1193-1250. THE CUSP WEB WAS REPLACED IAW SRM 53-20-02D.

Next page: https://openairdocs.org/deregistered/N928DL-2019-03-19/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 = 'N928DL' AND deregistration_id = 'N928DL-2019-03-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N928DL-2019-03-19/reports

---
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