# Service difficulty reports: N958DL, cancelled Apr 25, 2022

A list on [N958DL, cancelled Apr 25, 2022](https://openairdocs.org/deregistered/N958DL-2022-04-25.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 4 · 191 reports

- [SDR DALA2019102206061](https://openairdocs.org/sdr/DALA2019102206061.md): Battery Pack · inoperative · Oct 22, 2019 · N958DL · Doug MD88 · Emergency Lighting
  > F/C EMERGENCY LIGHT INOP. FOUND BATTERY PACK FOR F/C AREA LOW/ REMOVED AND RPLACED BATTERY PACK IAW MD88AMM 33-51 OPS CHECK GOOD. (LP6193565)
- [SDR DALA2019092505495](https://openairdocs.org/sdr/DALA2019092505495.md): Smoke Detector · malfunctioned · Sep 24, 2019 · N958DL · Doug MD88 · Smoke Detection
  > AFT RT LAV SMOKE DETECTOR CHIRPING. R/R AFT RT LAV SMOKE DETECTOR - REF AMM 2617. (LP6040676)
- [SDR DALA2019041502422](https://openairdocs.org/sdr/DALA2019041502422.md): Smoke Detector · false activation · Apr 14, 2019 · N958DL · Doug MD88 · Smoke Detection
  > AFT LEFT LAV SMOKE DET GOING OFF. INSP HEAT DET NO IND OF OVER TEMP R/R SMOKE DET IAW MD88 AMM 26-13 CHKS GOOD. (LP5672344)
- [SDR DALA2018101806183](https://openairdocs.org/sdr/DALA2018101806183.md): Fuse · blown · Oct 18, 2018 · N958DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS AT ROWS 24-30 ARE INOPERATIVE. MAINTENANCE FOUND A FUSE ON BATTERY PACK B5-212 TO BE BAD. THE BAD FUSE WAS REPLACED AND THE LIGHTS NOW OPERATE NORMALLY REF AMM 33-50.
- [SDR DALA2018091805642](https://openairdocs.org/sdr/DALA2018091805642.md): Unknown · odor · Sep 17, 2018 · N958DL · Doug MD88 · Air Distribution System
  > WHILE DES FROM FL360 NOTICED ACRID SMOKE SMELL IN THE COCKPIT. FLIGHT ATTENDANT THEN HAD SMOKE IN THE CABIN THAT STARTED NEAR ROW 26 AND STARTED AFTER SET OFF BOTH SMOKE ALARMS IN THE TWO AFT LAVS NORMAL CABIN PX + ENG INDICATIONS. SMOKE DISSIPATED AFTER 10 MI
- [SDR DALA2018080604866](https://openairdocs.org/sdr/DALA2018080604866.md): Fan · odor · Aug 4, 2018 · N958DL · Doug MD88 · Air Distribution Fan
  > AFTER TAKEOFF, FROM WHEELS UP TILL 2 MINUTES, FA REPORTED AN ODOR, SHE DESCRIBED AS ELECTRICAL. 2 MINUTES LATER THE ODOR WENT AWAY AND NEVER REOCCURRED. DURING TROUBLESHOOTING IAW AMDS CARD 2120-2367, FOUND THE RECIRCULATION FAN INOPERATIVE. REPLACED
- [SDR DALA2018072604696](https://openairdocs.org/sdr/DALA2018072604696.md): Panel · damaged · Jul 25, 2018 · N958DL · Doug MD88 · Spoilers
  > RT INBOARD FLIGHT SPOILER DAMAGED. REMOVED AND REPLACED RT INBOARD SPOILER PANEL REF WORKCARD 2700-4727.
- [SDR DALA2018072404638](https://openairdocs.org/sdr/DALA2018072404638.md): Skin · corroded · Jul 23, 2018 · N958DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 1322 L-20L - L-22L CORROSION. CORROSION WAS REMOVED AND REPAIRED PER ER/A 524660-14.
- [SDR DALA2018072304606](https://openairdocs.org/sdr/DALA2018072304606.md): Skin · corroded · Jul 21, 2018 · N958DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN AND PAN AT AFT LAV SERVICE PANEL LOWER QUADRANT. COMPLIED WITH ERA 569995-14 REV O.
- [SDR DALA2018072404641](https://openairdocs.org/sdr/DALA2018072404641.md): Skin · corroded · Jul 16, 2018 · N958DL · Doug MD88 · Fuselage Main, Plate/Skin
  > REPAIR OF CORROSION LOCATED AT THE AFT LAV SERVICE PANEL CUTOUT. FS 1307 TO FS 1322, L-21L AND L-22L.
- [SDR DALA2018071104448](https://openairdocs.org/sdr/DALA2018071104448.md): Vane · gouged · Jul 10, 2018 · N958DL · Doug MD88 · Trailing Edge Flaps
  > LT WING LE OF FLAP VANE GOUGED AFT OF CENTER HINGE POINT OB FLAP- REF NRC 189. FLAP VANE REPLACED ON NRC 189.
- [SDR DALA2018062504173](https://openairdocs.org/sdr/DALA2018062504173.md): Battery · discharged · Jun 25, 2018 · N958DL · Doug MD88 · Emergency Lighting
  > TAIL CAT WALK CEILING LIGHTS INOP. REMOVED AND REPLACED 'D' CELL BATTERIES TWO IN AFT LAV RIGHT. OPERATIONAL CHECK OK IAW AMM 33-50.
- [SDR DALA2018020800787](https://openairdocs.org/sdr/DALA2018020800787.md): Slide · low pressure · Feb 8, 2018 · N958DL · Doug MD88 · Escape Slide
  > L2 DOOR SLIDE PRESSURE LOW. REPL L2 DOOR SLIDE PER WORK CARD 2561-4002.
- [SDR DALA2017112008215](https://openairdocs.org/sdr/DALA2017112008215.md): Frame · cracked · Nov 16, 2017 · N958DL · Doug MD88 · Fuselage Main, Frame
  > LT AND RT WHEEL WELL FWD FRAMES CRACKED. STOP DRILLED RT AND LT WHEEL WELL FWD FRAMES IAW ERA 536531-14, REV ORIG. OK FOR SERVICE.
- [SDR DALA2017063005083](https://openairdocs.org/sdr/DALA2017063005083.md): Fitting · broken · Jun 29, 2017 · N958DL · Doug MD88 · Fuselage, Landing Gear Attach Fittings
  > CREW REPORTED A RED LT MLG UNSAFE INDICATION WITH ASSOCIATED AMBER GEAR DOOR OPEN LIGHT AND AUTO-SPOILER FAIL EOAP MESSAGE AFTER GEAR RETRACTION. GEAR WAS EXTENDED AND CREW RECEIVED 3 GREEN DOWN AND LOCKED INDICATIONS WITH GEAR DOOR LIGHT EXTINGUISHED AND RETU
- [SDR DALA2017052604234](https://openairdocs.org/sdr/DALA2017052604234.md): Unknown · odor · May 25, 2017 · N958DL · Doug MD88 · Air Distribution System
  > FLIGHT ATTENDANT IN REAR OF AIRCRAFT REPORT THAT DURING TAXI INTO THE GATE THEY OBSERVED A VERY INTENSE ODOR DESCRIBED AS POPCORN BURNED IN A MICROWAVE OVEN. INBOUND PILOTS REPORTED THAT THEY SHUTDOWN THE RIGHT ENGINE. DURING TAXI IN AND STARTED THE APU BEFORE
- [SDR DALA2017050703630](https://openairdocs.org/sdr/DALA2017050703630.md): Line · leaking · May 6, 2017 · N958DL · Doug MD88 · Hydraulic System, Main
  > ON APPROACH, LT HYD PRESSURE LOW CAUTION LIGHT, HYD PRESSURE & QTY BOTH INDICATED 0. LEAK COMING FROM CHAFED LEFT WING NR 4 FLAP ACTUATOR UP LINE. REPLACED THE HYD LINE AND SERVICED SYSTEM. CHECKED GOOD.
- [SDR DALA2017041002872](https://openairdocs.org/sdr/DALA2017041002872.md): Battery Pack · inoperative · Apr 9, 2017 · N958DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS IN CEILING FIRST CLASS SECTION INOPERATIVE. REPLACED THE BATTERY PACKS IAW AMM 33-53. OPS CHECKED GOOD.
- [SDR DALA2016062404904](https://openairdocs.org/sdr/DALA2016062404904.md): Pan · cracked · Jun 23, 2016 · N958DL · Doug MD88 · Emergency Exits
  > RIGHT AFT OVERWING EXIT DOOR, PAN CRACKED AT FWD AFT SUPPORT BRACKET. REPAIRED IAW PRI 548238-14, REV 0 AND ER/A 548238-14, REV ORIGINAL.
- [SDR DALA2016062404902](https://openairdocs.org/sdr/DALA2016062404902.md): Splice · cut · Jun 23, 2016 · N958DL · Doug MD88 · Fuselage Main, Bulkhead
  > SPLICE IN APB, STA 1338, TEE CHORD BETWEEN L26L AND L27L WITH NO FASTENERS IN FORMER TAB, SPLICE CUT IS BETWEEN FORMER TAB AND L26L END FITTING. REPAIRED IAW PRI 548159-14, REV "0" AND "1" AND FINAL ER/A 548159-14, REV "A".
- [SDR DALA2015060403597](https://openairdocs.org/sdr/DALA2015060403597.md): Wire · damaged · Jun 3, 2015 · N958DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 14D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND WIRES DAMAGED IN THE UNDERSEAT HARNESS. THE WIRE HARNESS WAS REPAIRED AND THE SYS RETURNED TO NORMAL OPERATION. LP 6717398.
- [SDR DALA2020031901940](https://openairdocs.org/sdr/DALA2020031901940.md): Skin · cracked · Apr 28, 2015 · N958DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV4 AT QRO, WHILE A SID INSPECTION WAS BEING PERFORMED, A 0.125 LONG CRACK ON THE FUSELAGE SKIN 5911432-81, AND TWO (0.152 AND 1.906 LONG) CRACKS ON THE FUSELAGE SKIN 5911432-83 WERE FOUND, ALL OF THEM LOCATED NEAR STA Y=1418, BETWEEN L3LH AND L3RH,
- [SDR DALA2014110305897](https://openairdocs.org/sdr/DALA2014110305897.md): Display · inoperative · Oct 29, 2014 · N958DL · Doug MD88 · Central Display
  > THE F/O PRIMARY FLIGHT DISPLAY FAILED AFTER TAKEOFF WITH CREATED SMOKE AND FUMES IN THE COCKPIT. CREW RETURNED THE ACFT AND LANDED UNEVENTFULLY. F/O PRIMARY FLIGHT DISPLAY WAS FOUND TO BE INOPERATIVE. INSPECTED WIRING AND PROPER VOLTAGE AT THE CONNECTOR WITH
- [SDR DALA14028140958](https://openairdocs.org/sdr/DALA14028140958.md): Longeron · damaged · May 4, 2014 · N958DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > ELONGATED HOLES WERE FOUND ON LONGERON 2R BS 1407-1422. DAMAGE LONGERON REMOVED, NEW LONGERON WAS DRILLED, ADJUSTED, TREATED, AND PAINTED. NEW LONGERON INSTALLED IAW SRM 53-02, PAR 12, FIG 18.
- [SDR DALA14028130958](https://openairdocs.org/sdr/DALA14028130958.md): Vane · corroded · May 3, 2014 · N958DL · Doug MD88 · Trailing Edge Flaps
  > RUSTED HARDWARE ON LT OTBD FLAP INBD VANE CLEVIS (AYP). RUSTED HARDWARE ON LT OTBD FLAP INBD VANE CLEVIS WERE REPLACED IAW AMM 20-30-01. CORROSION LEVEL 2. PRIMARY STRUCTURE.
- [SDR DALA2016110808572](https://openairdocs.org/sdr/DALA2016110808572.md): Longeron · corroded · May 2, 2014 · N958DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 22L, BS 1297-1309. THE DAMAGE WAS REMOVED, AND A NEW SECTION OF THE LONGERON WAS DRILLED, ADJUSTED, TREATED, PAINTED AND INSTALLED.
- [SDR DALA14028040958](https://openairdocs.org/sdr/DALA14028040958.md): Access Panel · corroded · May 2, 2014 · N958DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON RT FUEL TANK ACCESS PLATE NR 1460C AT COUNTERSINK AREA, MRB 57-083-02, REF 20000005843, CORROSION ON COUNTERSINK WAS REMOVED AND MAXIMUM DIAMETER ALLOWABLE IS 0.532" AND WERE FOUND 4 COUNTERSINK ADJACENT OUT OF LIMITS MEASURED 0.545", 0.570", 0
- [SDR DALA14027650958](https://openairdocs.org/sdr/DALA14027650958.md): Cargo Track · corroded · Apr 30, 2014 · N958DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON CARGO TRACK BS 1007-1222. NEW CARGO TRACK DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-3, PAR 14,21 AND 38 AND 51-30-1.
- [SDR DALA14027640958](https://openairdocs.org/sdr/DALA14027640958.md): Cargo Track · corroded · Apr 29, 2014 · N958DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON CARGO TRACK FROM BS 1212-1240. CARGO TRACK REMOVED AND TRACK DRILLED AND INSTALLED IAW SRM 51-10-3 PAR. 14 AND 21 SRM 51-30-1.
- [SDR DALA14026480958](https://openairdocs.org/sdr/DALA14026480958.md): Longeron · corroded · Apr 27, 2014 · N958DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 24L BETWEEN BS 1338-1380. LONGERON REPLACED IAW SRM 51-30-2, 51-30-5, 53-14-4, AND 51-10-3 PAR 21,14,38.
- [SDR DALA14026470958](https://openairdocs.org/sdr/DALA14026470958.md): Longeron · cracked · Apr 27, 2014 · N958DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 5R BS 1437. DAMAGE LONGERON WAS REMOVED NEW LONGERON AND SPLICE WERE DRILLED, ADJUSTED, TREATED, PAINTED AND WERE INSTALLED IAW SRM 53-02, FIG 18, 51-10-3, 51-30-2, 51-30-5.
- [SDR DALA14026350958](https://openairdocs.org/sdr/DALA14026350958.md): Pan · cracked · Apr 26, 2014 · N958DL · Doug MD88 · Fuselage Main, Structure
  > CRACKED FWD DOOR PAN ON BEAM NR 3 AT MID CARGO DOOR, C2, REF NRC 20000006058 CARD 67 A/C ZONE 100. CRACK IN DOOR PAN STOP DRILLED 52.05, FIG 50, NEW DOUBLER WAS FABRICATED IAW SRM 52.05, FIG 50. NEW DOUBLER WAS PAINTED IAW SRM 51.10.3 PAR 14. REPAIR DOUBLER
- [SDR DALA2016111008668](https://openairdocs.org/sdr/DALA2016111008668.md): Access Panel · corroded · Apr 25, 2014 · N958DL · Doug MD88 · Wing, Plate/Skin
  > RT WING FUEL TANK ACCESS PANEL 1460 CORRDED. REPLACED THE ACCESS PANEL.
- [SDR DALA14026320958](https://openairdocs.org/sdr/DALA14026320958.md): Angle · cracked · Apr 25, 2014 · N958DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE BS 1418 BETWEEN LONGERON 1-2R.
- [SDR DALA2016111008667](https://openairdocs.org/sdr/DALA2016111008667.md): Cusp Web · corroded · Apr 23, 2014 · N958DL · Doug MD88 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB CORRODED, BS 1180-1190, 1193-1195, 1212, 1216, 1235-1244, 1272. X -54 TO -60. DAMAGE REMOVED AND A REPAIR FABRICATED AND INSTALLED.
- [SDR DALA14025400958](https://openairdocs.org/sdr/DALA14025400958.md): Access Panel · corroded · Apr 23, 2014 · N958DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON FUEL TANK ACCESS PANEL 1466. CORROSION REMOVED AND FOUND OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A CONDITION.
- [SDR DALA2016111008665](https://openairdocs.org/sdr/DALA2016111008665.md): Cusp Web · corroded · Apr 22, 2014 · N958DL · Doug MD88 · Fuselage Miscellaneous Structure
  > PREVIOUS REPAIR OF RH CUSP WEB CORRODED, BS 1060 - 1079, X -54 TO -60. A NEW REPAIR WAS FABRICATED AND INSTALLED.
- [SDR DALA2016111008664](https://openairdocs.org/sdr/DALA2016111008664.md): Cusp Web · corroded · Apr 22, 2014 · N958DL · Doug MD88 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB CORRODED BS 996 - 1005, X -54 TO X -60. DAMAGE REMOVED, REPAIR INSTALLED.
- [SDR DALA14025330958](https://openairdocs.org/sdr/DALA14025330958.md): Skin · damaged · Apr 22, 2014 · N958DL · Doug MD88 · Rudder, Plate/Skin
  > DAMAGED METAL ON RT AND LT RUDDER SURFACE. REPAIRED IAW SRM 51-70-1.
- [SDR DALA14025320958](https://openairdocs.org/sdr/DALA14025320958.md): Tab · damaged · Apr 22, 2014 · N958DL · Doug MD88 · Rudder, Tab Structure
  > DAMAGED METALLIZED ON RUDDER CONTROL TAB. METALLIZED ON RUDDER CONTROL TAB WAS REPAIRED IAW AC 0958 CARD 2000-8149-07, CREW 02 "7412731" SRM 51-70-1, AD PAR 23A. RII COMPLETED BY INSPECTION STAMP INSPECTOR C.D.T.L 200500612 TECHOPS DELTA ID550902.
- [SDR DALA2016111008662](https://openairdocs.org/sdr/DALA2016111008662.md): Cusp Web · corroded · Apr 21, 2014 · N958DL · Doug MD88 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB CORRODED BS 844 - 855, X -54 TO X -60. THE DAMAGE WAS REMOVED AND A REPAIR FABRICATED AND INSTALLED.
- [SDR DALA2016111008661](https://openairdocs.org/sdr/DALA2016111008661.md): Cusp Web · corroded · Apr 21, 2014 · N958DL · Doug MD88 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB CORRODED, BS 719 - 721, X -54 TO X -60. THE DAMAGE WAS REMOVED, REPAIR FABRICATED AND INSTALLED.
- [SDR DALA2016110908660](https://openairdocs.org/sdr/DALA2016110908660.md): Cusp Web · corroded · Apr 21, 2014 · N958DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORRODED CUSP WEB BS 984-988 X -54 TO -60. DOUBLER, TRIPLER FABRICATED AND INSTALLED.
- [SDR DALA2016110908659](https://openairdocs.org/sdr/DALA2016110908659.md): Cusp Web · corroded · Apr 21, 2014 · N958DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CUSP WEB CORRODED BS 650-653, 622-644 X 54 - 60. DOUBLERS FABRICATED AND INSTALLED.
- [SDR DALA2016110908658](https://openairdocs.org/sdr/DALA2016110908658.md): Cusp Web · corroded · Apr 21, 2014 · N958DL · Doug MD88 · Fuselage Miscellaneous Structure
  > PREVIOUS CUSP WEB REPAIR CORRODED, REPLACED STA 465-484, X -54 TO -60.
- [SDR DALA2016110908657](https://openairdocs.org/sdr/DALA2016110908657.md): Longeron · corroded · Apr 21, 2014 · N958DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > LONGERON 23L END FITTING CORRODED, BS 1338 IN AFT CARGO. REPLACED.
- [SDR DALA14025390958](https://openairdocs.org/sdr/DALA14025390958.md): Access Panel · corroded · Apr 21, 2014 · N958DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON RT FUEL TANK ACCESS PANEL 1470C. CORROSION REMOVED AND FOUND OUT OF LIMITS. ACCESS PANEL REMOVED IAW SRM 51-22-2A CONDITION II. BUSHING FABRICATED" AND COUNTERSUNK IAW SRM 51-22-2A PAR NR 6. NEW BUSHING AND AREA WERE TREATED IAW SRM 51-10-
- [SDR DALA2016110908656](https://openairdocs.org/sdr/DALA2016110908656.md): Cusp Web · corroded · Apr 19, 2014 · N958DL · Doug MD88 · Fuselage Miscellaneous Structure
  > PREVIOUS CUSP WEB REPAIR CORRODED. BS 712-731 BETWEEN X 44 - 60. REPAIR FABRICATED AND INSTALLED.
- [SDR DALA14024490958](https://openairdocs.org/sdr/DALA14024490958.md): Access Panel · corroded · Apr 18, 2014 · N958DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON RT FUEL TANK ACCESS PANEL 1335C AT COUNTERSINK AREA AND DAMAGED DOME NUTS, CORROSION REMOVED, AND FOUND TO BE OUT OF LIMITS. REWORKED IAW SRM 51-22-2A, CONDITION II, REPAIR BUSHINGS INSTALLED IAW SRM 51-22-2A, NUTS DAMAGED WERE REMOVED AND NEW
- [SDR DALA14024480958](https://openairdocs.org/sdr/DALA14024480958.md): Longeron · cracked · Apr 18, 2014 · N958DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > LONGERON 4L BS 1437 CRACKED. SPLICE AND LONGERON SECTION REMOVED IAW SRM 53-02, FIG 18. NEW LONGERON SECTION AND SPLICE FABRICATED IAW SRM 53-02, FIG 18. NEW LONGERON SECTION AND SPLICE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21. NEW LONGERON SECTION

Next page: https://openairdocs.org/deregistered/N958DL-2022-04-25/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 = 'N958DL' AND deregistration_id = 'N958DL-2022-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N958DL-2022-04-25/reports

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