# Service difficulty reports: N938DL, cancelled Oct 8, 2020

A list on [N938DL, cancelled Oct 8, 2020](https://openairdocs.org/deregistered/N938DL-2020-10-08.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 3 · 129 reports

- [SDR DALA2018080304835](https://openairdocs.org/sdr/DALA2018080304835.md): Charger · odor · Aug 2, 2018 · N938DL · Doug MD88 · Battery/Charger System
  > DURING WALKAROUND NOTICED ELECTRICAL FUME/SMELL FROM E&E COMPARTMENT AND FWD GALLEY. FOUND BATTERY CHARGER RELAY A2 TERMINAL BURNT. REMOVED A/C BATTERIES PER AMM24-30. REMOVED BATTERY CHARGER RELAY PER AMM 24-00 GENERAL. REPLACED R2-56, R2-63 AND BATTERY CHARG
- [SDR DALA2018061804043](https://openairdocs.org/sdr/DALA2018061804043.md): Spar · cracked · Jun 18, 2018 · N938DL · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > RT HOR STAB AFT SPAR UPR CHORD- INBD FASTENER HAS A 3/16 INCH CRACK AT 12:00 EXTENDING PAST HEAD. MK'D VERIFIED WITH HFEC PER NDT SPM 06-10-01.001. RT HORIZONTAL STAB SPAR CAP SPLICE REPAIR COMPLETED ON 5510-01074-16 STEP 7, ACCESS GAINED FOR REPAIR RESTORED.
- [SDR DALA2018061804041](https://openairdocs.org/sdr/DALA2018061804041.md): Slide · defective · Jun 16, 2018 · N938DL · Doug MD88 · Escape Slide
  > AFT SLIDE P/N D29985-103 S/N 0980 DEFECTIVE UPPER RELEASE PIN / TIE OFF. REMOVED AND REPLACE SLIDE PER 2561-4002.
- [SDR DALA2018061504022](https://openairdocs.org/sdr/DALA2018061504022.md): Skin · gouged · Jun 14, 2018 · N938DL · Doug MD88 · Trailing Edge Flaps
  > LT WING OB TE FLAP HAS GOUGE IN UPPER SURFACE APPROX 43 IN FROM IB EDGE. REPAIRED PER PRI 569265-14 REV 0 AND 1. COMPLIED WITH ER/A 569265-14 REV ORIGINAL.
- [SDR DALA2018061504020](https://openairdocs.org/sdr/DALA2018061504020.md): Floorbeam · corroded · Jun 13, 2018 · N938DL · Doug MD88 · Fuselage Main, Floor Beam
  > DURING FORWARD GALLEY NTF REPLACEMENT, FOUND CORROSION ON FLOOR BEAM BETWEEN FLOOR PANEL 160B & 160C. REPLACED FLOOR SUPPORT REF SRM 51-01, PAGE 1 AND DWG 9936534. THIS IS CONSIDERED LEVEL 2 CORROSION.
- [SDR DALA2018060403776](https://openairdocs.org/sdr/DALA2018060403776.md): Mechanism · out of adjust · Jun 2, 2018 · N938DL · Doug MD88 · Aerodynamic Fairings
  > TAILCONE RELEASE MECHANISM CAM FAILED TORQUE CHECK. ADJUSTED CAM MECHANISM W/REF TO AMM 53-53-02.
- [SDR DALA2018041102334](https://openairdocs.org/sdr/DALA2018041102334.md): Battery Pack · inoperative · Apr 10, 2018 · N938DL · Doug MD88 · Emergency Lighting
  > NUMEROUS CEILING EMERGENCY LIGHTS OUT. REPLACED THE BATTERY PACK B5-100, B5-102, B5-106, AND B5-107 IAW AMM 33-53-00.
- [SDR DALA2017122208816](https://openairdocs.org/sdr/DALA2017122208816.md): Battery · inoperative · Dec 20, 2017 · N938DL · Doug MD88 · Smoke Detection
  > LAVATORY SMOKE DETECTOR WILL NOT TURN OFF. REPLACED THE SMOKE DETECTOR BATTERY AND TESTED GOOD IAW AMM 26-21.
- [SDR DALA2017121808719](https://openairdocs.org/sdr/DALA2017121808719.md): Connector · disconnected · Dec 17, 2017 · N938DL · Doug MD88 · Light System Wiring
  > EMERGENCY LIGHT AT 23 DE INOPERATIVE. FOUND THE CONNECTOR DISCONNECTED. RECONNECTED.
- [SDR DALA2017121808650](https://openairdocs.org/sdr/DALA2017121808650.md): Battery · discharged · Dec 15, 2017 · N938DL · Doug MD88 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 11 AND 15 INOP. REPLACED BATTERIES AT BATTERY PACK ROW 12 RIGHT. OPS CKS GOOD PER AMM 33-50.
- [SDR DALA2017101007389](https://openairdocs.org/sdr/DALA2017101007389.md): Door · excess play · Oct 9, 2017 · N938DL · Doug MD88 · Landing Gear Doors
  > CREW REPORTED DURING TAKE OFF, THE CREW REPORTED A NOSE WHEEL VIBRATION AND RUBBER ODOR AT V1. FLT CONTINUED. AFTER LANDING, THE TIRE TREAD WAS INTACT WITH NO VISIBLE DAMAGE. FOUND THE LT NOSE GEAR DOOR WITH EXCESSIVE PLAY. ADJUSTED DOOR AND LUBRICATED DOORS
- [SDR DALA2017072805729](https://openairdocs.org/sdr/DALA2017072805729.md): Fuse · inoperative · Jul 27, 2017 · N938DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS IN AFT SECTION OF CABIN ARE INOPERATIVE. REPLACED THE FUSES IN THE AFT BATTERY PACK. CHECKED GOOD IAW AMM 33-53.
- [SDR DALA2017070805271](https://openairdocs.org/sdr/DALA2017070805271.md): Lamp · inoperative · Jul 7, 2017 · N938DL · Doug MD88 · Emergency Lighting
  > RT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS, CHECKED GOOD.
- [SDR DALA2015040602627](https://openairdocs.org/sdr/DALA2015040602627.md): Connector · failed · Apr 5, 2015 · N938DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROW 4C, 24E, 28E, AND 33E IN THE CABIN WERE INOPERATIVE. MAINTENANCE FOUND A FAILED CONNECTOR IN THE WIRE HARNESS AND REPLACED IT. THE FUNCTIONAL CHECK OF THE SYSTEM WAS GOOD. LP 1892209
- [SDR DALA14023540938](https://openairdocs.org/sdr/DALA14023540938.md): Light · inoperative · Apr 15, 2014 · N938DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE RED EMERGENCY LIGHT FOR EXIT ROW 24DE WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.
- [SDR DALA14017150938](https://openairdocs.org/sdr/DALA14017150938.md): Skin · cracked · Mar 16, 2014 · N938DL · Doug MD88 · Fuselage Main, Plate/Skin
  > ACFT SKIN HAS A.3750" CRACK AT FASTENER HOLE, BS 1380, 1 INCH ABOVE LONGERON 13 LT. CONFIRMED WITH HFEC, SUMMARY OF EMPOWER NRC 68; REPAIRED IAW PRI ER/A 524139-14, REV 0-REV 1 BY DAMAGE CUTOUT AND DOUBLER INSTALLATION. DOUBLER WAS MADE LARGER FOR AREA TO I
- [SDR DALA14017140938](https://openairdocs.org/sdr/DALA14017140938.md): Skin · cracked · Mar 15, 2014 · N938DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR, CRACK EMINATING FROM FASTENER AT BS 1437 JUST BELOW RT SKATE ANGLE. HFEC VERIFIED, REF NR 102, COMPLETED REPAIR IAW PRI 524140-14, REV ORIG WAITING FOR FINAL ER/A.
- [SDR DALA12012300938](https://openairdocs.org/sdr/DALA12012300938.md): Lanyard · misinstalled · Nov 5, 2012 · N938DL · Doug MD88 · Escape Slide
  > INSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE HAD AN IMPROPERLY INSTALLED LANYARD. THE TAILCONE SLIDE AND LANYARD WERE INSTALLED CORRECTLY.
- [SDR DALA12012280938](https://openairdocs.org/sdr/DALA12012280938.md): Release Cable · frayed · Nov 4, 2012 · N938DL · Doug MD88 · Aerodynamic Fairings
  > MX DISCOVERED THAT THE TAILCONE RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.
- [SDR DALA12012070938](https://openairdocs.org/sdr/DALA12012070938.md): Tee Fitting · cracked · Nov 1, 2012 · N938DL · Doug MD88 · Fuselage Main, Structure
  > DETAILED INSPECTION PERFORMED. CRACKED TEE OF LT MLG JAMB WAS FOUND. REMOVED AND NEW TEE WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-02, 51-10-4, 51-10-3 AND DWG 5936395, REV BF.
- [SDR DALA12012060938](https://openairdocs.org/sdr/DALA12012060938.md): Beam · corroded · Nov 1, 2012 · N938DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON BEAM BS 1221 BETWEEN LONGERONS 30 AND 28 RIGHT AT AFT CARGO COMPARTMENT (C3). FASTENERS AND CORROSION WERE REMOVED AND REWORKED AREA WAS TREATED AND PAINTED. FASTENERS WERE INSTALLED IAW SRM 51-30-05 AND 51-10-03 PARA 14, 21 AND 26.
- [SDR DALA12012050938](https://openairdocs.org/sdr/DALA12012050938.md): Door Frame · corroded · Nov 1, 2012 · N938DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON LOWER DOOR FRAME BEAM AT MID CARGO COMPARTMENT BETWEEN BS 652 TO 677. REPAIRED IAW ER/A 506669-14 REV O.
- [SDR DALA12012150938](https://openairdocs.org/sdr/DALA12012150938.md): Window Frame · nicked · Oct 31, 2012 · N938DL · Doug MD88 · Fuselage Main, Structure
  > NICK ON LT WINDOW BELT FRAME BTW BS 1193-1212 AFT LOWER CORNER. AREA WAS BLEND OUT, MEASURE, AND TREATED IAW ER/A 506655-14 REV ORIG.
- [SDR DALA12012140938](https://openairdocs.org/sdr/DALA12012140938.md): Window Frame · damaged · Oct 31, 2012 · N938DL · Doug MD88 · Fuselage Main, Structure
  > SCRATCH ON LT WINDOW BELT FRAME BETWEEN BS 636-655 AFT LOWER CORNER. AREA WAS BLEND OUT, MEASURE, AND TREATED IAW ER/A 506655-14, REV ORIG.
- [SDR DALA12012130938](https://openairdocs.org/sdr/DALA12012130938.md): Window Frame · damaged · Oct 31, 2012 · N938DL · Doug MD88 · Fuselage Main, Structure
  > LIGHTNING STRIKE ON RT WINDOW BELT FRAME BETWEEN BS 370-389 AFT LOWER CORNER. AREA WAS BLEND OUT, MEASURE, AND TREATED IAW ER/A 506655-14, REV ORIG.
- [SDR DALA12012120938](https://openairdocs.org/sdr/DALA12012120938.md): Window Frame · damaged · Oct 31, 2012 · N938DL · Doug MD88 · Fuselage Main, Structure
  > LIGHTNING STRIKE ON RT WINDOW BELT FRAME BTW BS 465-484 FWD EDGE AND AFT UPPER CORNER. AREA WAS BLEND OUT MEASURE TREATED IAW ER/A 506655-14, REV ORIG.
- [SDR DALA12012110938](https://openairdocs.org/sdr/DALA12012110938.md): Pan · cracked · Oct 31, 2012 · N938DL · Doug MD88 · Cargo/Baggage Doors
  > CRACKED OUTER PAN ON AFT EDGE BELOW TO STOP FITTING NR 3 OF FWD CARGO COMPARTMENT DOOR AFT EDGE REF NRC (T0 262757) PAN WAS REPAIRED IAW SRM 52-05D FIG 50 RII COMPLETED.
- [SDR DALA12012100938](https://openairdocs.org/sdr/DALA12012100938.md): Bearing · worn · Oct 31, 2012 · N938DL · Doug MD88 · Aerodynamic Fairings
  > DURING INSPECTION OF THE TAILCONE RELEASE SYSTEM, MX FOUND THE RELEASE CAM BEARING WORN BEYOND LIMITS, ALLOWING EXCESSIVE FREE PLAY. THE CAM BEARING WAS REPLACED. FOLLOW UP FUNCTIONAL CHECKED GOOD.
- [SDR DALA12011890938](https://openairdocs.org/sdr/DALA12011890938.md): Duct · cracked · Oct 30, 2012 · N938DL · Doug MD88 · Air Distribution System
  > CRACKED RADIO RACK COOLING EXHAUST DUCT ON FWD CORNERS. REPAIRED IAW ERA 464964-14 MA REV ORIG.
- [SDR DALA12011870938](https://openairdocs.org/sdr/DALA12011870938.md): Skin · corroded · Oct 30, 2012 · N938DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING FROM BS 1114 TO 1119 L24 TO 30 LT. REPAIRED IAW SRM 53-04 P57.
- [SDR DALA12011760938](https://openairdocs.org/sdr/DALA12011760938.md): Stringer · corroded · Oct 30, 2012 · N938DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON PREVIOUS REPAIR DOUBLER BS 465 TO 535 BTW STA X=-50 TO -60. REPLACED IAW SRM 53-05, FIG 827D AND 53-05, FIG 131 & DWG 9930538, REV CF.
- [SDR DALA12011710938](https://openairdocs.org/sdr/DALA12011710938.md): Longeron · corroded · Oct 30, 2012 · N938DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 24L BS 1290. REPLACED LONGERON IAW SRM 53-02, FIG 18.
- [SDR DALA12011540938](https://openairdocs.org/sdr/DALA12011540938.md): Longeron · cracked · Oct 29, 2012 · N938DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 8R BS 1309. REPAIRED IAW SRM 53-02, FIG 18 AND DWG 5936436.
- [SDR DALA12011530938](https://openairdocs.org/sdr/DALA12011530938.md): Cusp Web · corroded · Oct 29, 2012 · N938DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON LT CUSP WEB BTW X=54-60 FROM STA Y=579-983. REPAIRED IAW SRM 53-05, FIG 131A-10.
- [SDR DALA12011520938](https://openairdocs.org/sdr/DALA12011520938.md): Cusp Web · corroded · Oct 29, 2012 · N938DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON PREVIOUS REPAIR DOUBLER AT RT CUSP WEB BTW X=-54 TO X=-60 FROM BS 938-1020. CUSP WEB REPAIRED IAW 53-05 D FIG 827D AND ERA 398191-14MA REV B ASSOCIATED ER/A 39-819114 ADDED FOR AC 0938.
- [SDR DALA12011510938](https://openairdocs.org/sdr/DALA12011510938.md): Cusp Web · corroded · Oct 29, 2012 · N938DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS ON LT CUSP WEB FROM STA 787- 804 BETWEEN X=54 TO X=60 AT PAX CABIN WITH REF OM828H CARD 33, ZONE 58 AND NRC (T0 262756). REF NRC (T0 263839) CUSP WEB WAS REPAIRED IAW SRM 53-01, FIG 4.
- [SDR DALA12011770938](https://openairdocs.org/sdr/DALA12011770938.md): Longeron · cracked · Oct 28, 2012 · N938DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 13 LT BS 1380. REPLACED IAW SRM 51-30-2, 51-30-5 AND 53-02 FIG 18, DDWG 5911433 REV.
- [SDR DALA12011750938](https://openairdocs.org/sdr/DALA12011750938.md): Support · cracked · Oct 28, 2012 · N938DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED LT SLANT SUPPORTS STA Y=560 AND RT STA Y=560, 598 AT MID CARGO COMPARTMENT (C2) REF NRC: (T0 263134). SLANT SUPPORT WERE REPLACED IAW ERA 413029-14MA REV:B ASSOCIATED ER/A 41-302914 ADDED FOR AC 0938.
- [SDR DALA12011700938](https://openairdocs.org/sdr/DALA12011700938.md): Intercostal · corroded · Oct 28, 2012 · N938DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL FROM STA BS 1309 TO 1322. REMOVED AND INSTALLED NEW INTERCOSTALS IAW SLM 51-30-2.
- [SDR DALA12011690938](https://openairdocs.org/sdr/DALA12011690938.md): Cusp Web · corroded · Oct 28, 2012 · N938DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BETWEEN BS 769 TO 755 X= -54 AND X= -60. REPAIRED IAW DRD 53-05D, FIG 827D.
- [SDR DALA12011500938](https://openairdocs.org/sdr/DALA12011500938.md): Skin · cracked · Oct 28, 2012 · N938DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN FWD STAIRWAY DOOR JAMB AFT LWR CORNER. CRACK ON FUSELAFE SKIN ON FWD STAIRWAY DOOR JAMB AFT LOWER CORNER WAS REPAIRED IAW ERA/A 506635-14AD REV ORIG.
- [SDR DALA12011860938](https://openairdocs.org/sdr/DALA12011860938.md): Pan · cracked · Oct 27, 2012 · N938DL · Doug MD88 · Cargo/Baggage Doors
  > CRACKED INNER PAN ON AFT CARGO COMPARTMENT DOOR INNER STRUCTURE OF AFT EDGE BTW UPPER EDGE AND BEAM NR 5. PAN WAS REPAIRED IAW ER/A 455904-14MA REV A ASSOCIATED ER/A 45-590414 ADDED FOR AC 0938.
- [SDR DALA12011850938](https://openairdocs.org/sdr/DALA12011850938.md): Cusp Web · corroded · Oct 27, 2012 · N938DL · Doug MD88 · Wing Miscellaneous Structure
  > CORROSION ON LT CUSP WEB UPPER LOWER SURFACE BETWEEN BS 987 TO 1054 X=54 TO X=60. REPAIRED IAW SRM 53-05.
- [SDR DALA12011740938](https://openairdocs.org/sdr/DALA12011740938.md): Seat Track · corroded · Oct 27, 2012 · N938DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK X=44 FROM BS 1136 TO 1160. SEAT TRACK REPLACED IAW SRM 53-05, FIG YF.
- [SDR DALA12011730938](https://openairdocs.org/sdr/DALA12011730938.md): Support · broken · Oct 27, 2012 · N938DL · Doug MD88 · Fuselage Miscellaneous Structure
  > BROKEN SLANT PANEL SUPPORTS BS 237 AND 256. PANEL SUPPORTS REPLACED IAW E/A 413029-14 MA REV.
- [SDR DALA12011720938](https://openairdocs.org/sdr/DALA12011720938.md): Longeron · corroded · Oct 27, 2012 · N938DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 23L BS 1297 TO 1323. REPAIRED IAW SRM 53-02-F16.
- [SDR DALA12014620938](https://openairdocs.org/sdr/DALA12014620938.md): Skin · damaged · Oct 26, 2012 · N938DL · Doug MD88 · Fuselage Main, Plate/Skin
  > A LIGHTNING STRIKE WAS REPORTED ON THE RT WINDOW BELT PANEL BETWEEN BS 579 AND 598. A REPAIR DOUBLER WAS INSTALLED.
- [SDR DALA12011680938](https://openairdocs.org/sdr/DALA12011680938.md): Support · corroded · Oct 26, 2012 · N938DL · Doug MD88 · Fuselage Main, Bulkhead
  > CORROSION ON LOWER SUPPORT OF AFT BULKHEAD BETWEEN 24RH TO 24LH AT MID CARGO COMPARTMENT. REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIG 2, (SHEET 3).
- [SDR DALA12011230938](https://openairdocs.org/sdr/DALA12011230938.md): Longeron · cracked · Oct 26, 2012 · N938DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERONS 3 LT AT INTERSECTION WITH FRAME Y=1437 AFT ACCESSORY COMP. LONGERON REPAIRED IAW SRM 53-02, FIG 18.
- [SDR DALA12011210938](https://openairdocs.org/sdr/DALA12011210938.md): Longeron · cracked · Oct 25, 2012 · N938DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON NR 4 RT AT STA Y=1212 CABIN STRUCTURE. LONGERON WAS REPAIR IAW SRM 53-02, FIG 18, RII COMPLETED.

Next page: https://openairdocs.org/deregistered/N938DL-2020-10-08/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 = 'N938DL' AND deregistration_id = 'N938DL-2020-10-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N938DL-2020-10-08/reports

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