# Service difficulty reports: N935DL, cancelled Nov 9, 2020

A list on [N935DL, cancelled Nov 9, 2020](https://openairdocs.org/deregistered/N935DL-2020-11-09.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 · 139 reports

- [SDR DALA2018082305212](https://openairdocs.org/sdr/DALA2018082305212.md): Cam · missing · Aug 22, 2018 · N935DL · Doug MD88 · Auxiliary Power Unit (APU) Doors
  > DURING A WALK AROUND INSPECTION, FOUND ONE CAM LOCK MISSING ON RIGHT APU COMPARTMENT DOOR. INSTALLED THE CAM LOCK IAW AMM 52-45. ACFT OK FOR SERVICE.
- [SDR DALA201808205134](https://openairdocs.org/sdr/DALA201808205134.md): Extinguisher · leaking · Aug 19, 2018 · N935DL · Doug MD88 · Fire Bottle, Portable
  > DURING A SERVICE CHECK, FOUND FWD WATER EXTINGUISHER WAS LEAKING. REPLACED FWD PORTABLE WATER FIRE EXTINGUISHER IAW AMM 26-20. OK FOR SERVICE.
- [SDR DALA2018080804930](https://openairdocs.org/sdr/DALA2018080804930.md): Wire Harness · broken · Aug 8, 2018 · N935DL · Doug MD88 · Light System Wiring
  > SEAT 20 DE EMERGENCY LIGHT INOP. FOUND A WIRE HARNESS BROKEN. R & R THE WIRE HARNESS IAW AMM 33-52, OPS NORMAL.
- [SDR DALA2018061604035](https://openairdocs.org/sdr/DALA2018061604035.md): Doubler · cracked · Jun 15, 2018 · N935DL · Doug MD88 · Fuselage Main, Plate/Skin
  > INITIAL INSPECTION, CRACKED PRODUCTION DOUBLER ON FWD LAVATORY SERVICE PANEL. PRODUCTION DOUBLER ON FWD LAVATORY SERVICE PANEL WAS REPAIRED PER ER/A 569279-14 REV ORIGINAL SEC I AND ETI-88-18-060 REV 4.
- [SDR DALA2018061504023](https://openairdocs.org/sdr/DALA2018061504023.md): Doubler · corroded · Jun 15, 2018 · N935DL · Doug MD88 · Fuselage Main, Plate/Skin
  > AWR, INITIAL INSPECTION: CORROSION ON PREVIOUS REPAIR DOUBLERS AND FILLER AT AFT LAVATORY SERVICE PANEL SUMMARY OF NRC 00108, CORROSION LEVEL II, TEMPORARY REPAIR ON AFT LAVATORY SERVICE PANEL WAS ACCOMPLISHED PER ER/A 508310-14 REV A SEC III AND ETI-88-18-061
- [SDR DALA2018061203949](https://openairdocs.org/sdr/DALA2018061203949.md): Skin · cracked · Jun 11, 2018 · N935DL · Doug MD88 · Fuselage Main, Plate/Skin
  > INITIAL INSPECTION, CRACK ON FUSELAGE SKIN STA Y 69 REF LONG 21L. CRACK ON FUSELAGE SKIN STA Y 69 REF LONG 21L WAS REPAIRED PER SRM 53-04-3 FIG 8.
- [SDR DALA2017112108254](https://openairdocs.org/sdr/DALA2017112108254.md): Battery Pack · inoperative · Nov 21, 2017 · N935DL · Doug MD88 · Emergency Lighting
  > EMERGENCY CEILING LIGHTS AT SEATS 16-19 INOPERATIVE. REPLACED THE BATTERIES AT B5-102. CHECKED GOOD.
- [SDR DALA2017070505218](https://openairdocs.org/sdr/DALA2017070505218.md): Battery Pack · inoperative · Jul 5, 2017 · N935DL · Doug MD88 · Emergency Lighting
  > FWD GALLEY OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACKS IAW AMM 33-50. OPS CHECKED GOOD.
- [SDR DALA2017031602119](https://openairdocs.org/sdr/DALA2017031602119.md): Angle · cracked · Mar 15, 2017 · N935DL · Doug MD88 · Fuselage Miscellaneous Structure
  > FOUND LOWER ANGLE CRACKED AT BS 942.225 ON LOUVER FWD FRAME. REPLACED THE ANGLE.
- [SDR DALA2017031602118](https://openairdocs.org/sdr/DALA2017031602118.md): Bracket · broken · Mar 15, 2017 · N935DL · Doug MD88 · Fuselage Main, Attach Fittings
  > FOUND BROKEN BRACKET ON RT CANTED FRAME, AFT SIDE. LOCATED AT THE OTBD END OF STIFFENER LONGERON 7R, BS 942.225. REPLACED THE BRACKET.
- [SDR DALA2017031602110](https://openairdocs.org/sdr/DALA2017031602110.md): Frame · cracked · Mar 15, 2017 · N935DL · Doug MD88 · Fuselage Main, Frame
  > FOUND A CRACK ON THE FRAME WEB, FWD SIDE. LOCATED 4 FASTENERS BELOW LONGERON 7L, BS 942.225. REPAIRED IAW SRM 53-03D FIG. 38D.
- [SDR DALA2017012600673](https://openairdocs.org/sdr/DALA2017012600673.md): Pin · pulled · Jan 25, 2017 · N935DL · Doug MD88 · Escape Slide
  > L1 DOOR SLIDE PINS PULLED. REPLACED L1 DOOR SLIDE IAW JIC 2561-4964, OK FOR SERVICE.
- [SDR DALA2016051203900](https://openairdocs.org/sdr/DALA2016051203900.md): Block · damaged · May 12, 2016 · N935DL · Doug MD88 · Aerodynamic Fairings
  > TAIL INTERIOR, TAIL CONE RELEASE LOCK CABLE BLOCK IS NOT.5" AWAY FROM TUBING, CONDUIT, AS REQUIRED IAW STEP 7. OPS CHECKED GOOD IAW AMDS 5350-01077-0101.
- [SDR DALA2016051003857](https://openairdocs.org/sdr/DALA2016051003857.md): Scuff Plate · corroded · May 9, 2016 · N935DL · Doug MD88 · Fuselage Miscellaneous Structure
  > MID CARGO BAY DOOR LOWER JAMB UNDER ENTERY SCUFF PLATE CORRODED. REPAIRED IAW ER/A 499523-14MA, REV O.
- [SDR DALA2016051003837](https://openairdocs.org/sdr/DALA2016051003837.md): Threshold · corroded · May 9, 2016 · N935DL · Doug MD88 · Fuselage Miscellaneous Structure
  > FOUND ON "OK TO TREAT", L1 DOOR, THRESHOLD, INBD THRESHOLD/FLOORBOARD SUPPORT, 4" FROM DOOR OPENING, CORRODED, IN MULTIPLE AREAS ALONG ENTIRE LENGTH OF SUPPORT. TREATED PRIMED AND PAINTED AND INSTALLED IAW DWG 9936534.
- [SDR DALA2016050903831](https://openairdocs.org/sdr/DALA2016050903831.md): Shear Tie · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Internal Mounting Structure
  > AFT CARGO BILGE, LAV SPILL, SHEAR TIE AT BS 1287 AFT SIDE HAS CORROSION, L29L TO L26L. REPAIRED IAW SRM 53-01, FIG 1.
- [SDR DALA2016050903830](https://openairdocs.org/sdr/DALA2016050903830.md): Longeron Splice · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BILGE, LAV SPILL, L22L SPLICE AT BS 1300 HAS CORROSION. REPAIRED IAW SRM 53-01 FIG 1.
- [SDR DALA2016050903829](https://openairdocs.org/sdr/DALA2016050903829.md): Longeron · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > LONGERON 23L AT BS 1289 CORRODED. REPLACED SPLICE AND LONGERON IAW SRM 53-02, FIG 18, CORROSION FOUND TO BE LEVEL 2 CAUSED BY A LAV SPILL.
- [SDR DALA2016050903828](https://openairdocs.org/sdr/DALA2016050903828.md): Longeron · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BILGE, LAV SPILL, L29R HAS CORROSION, BS 1287-1309. REPAIRED IAW SRM 53-01, FIG 1.
- [SDR DALA2016050903827](https://openairdocs.org/sdr/DALA2016050903827.md): Longeron · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BILGE, LAV SPILL, L24L HAS CORROSION BLOW OUT AT BS 1290. REPAIRED IAW SRM 53-01, FIG 1.
- [SDR DALA2016050903826](https://openairdocs.org/sdr/DALA2016050903826.md): Finger Doubler · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Plate/Skin
  > AFT CARGO BILGE, LAV SPILL, LAP SEAM FINGER DOUBLER HAS CORROSION, NEAR L26L, BS 1287-1300. REPAIRED IAW SRM 53-01, FIG 1.
- [SDR DALA2016050903825](https://openairdocs.org/sdr/DALA2016050903825.md): Frame · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Frame
  > AFT CARGO BILGE, LAV SPILL, B-FRAME AT BS 1287 AFT FACE HAS CORROSION, OTBD OF L25L. REPAIRED IAW SRM 53-01, FIG 1.
- [SDR DALA2016050903824](https://openairdocs.org/sdr/DALA2016050903824.md): Frame · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Frame
  > AFT CARGO BILGE, LAV SPILL, FRAME AT BS 1309 AFT SIDE HAS CORROSION ABV L27-26L. REPAIRED IAW SRM 53-01, FIG 1 FOUND CORROSION TO BE LEVEL 1.
- [SDR DALA2016050903823](https://openairdocs.org/sdr/DALA2016050903823.md): Longeron · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BILGE, LAV SPILL, L29L HAS CORROSION, BS 1290-1300. REPAIRED IAW SRM 53-01, FIG 1.
- [SDR DALA2016050903822](https://openairdocs.org/sdr/DALA2016050903822.md): Shear Tie · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPARTMENT, LAV SPILL: SHEAR TIE CORRODED BS 1193 BETWEEN L29L TO L30. MAX MATERIAL REMOVED WAS.005" FROM ORIGINAL THICKNESS OF.071" IAW DWG 9936073. PART IS WITHIN LIMITS IAW SRM 53-01, FIG 1.
- [SDR DALA2016050903821](https://openairdocs.org/sdr/DALA2016050903821.md): Longeron · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > L22 AT ST 1290 CORRODED. REPAIRED IAW SRM 53-01, FIG 1.
- [SDR DALA2016050903820](https://openairdocs.org/sdr/DALA2016050903820.md): Frame · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Frame
  > FRAME AT ST 1322 AT LT L23 CORRODED. REPAIRED IAW SRM 53-01, FIG 1.
- [SDR DALA2016050903819](https://openairdocs.org/sdr/DALA2016050903819.md): Longeron · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > LONGERON 23 LT HAS CORROSION, BS 1322, INSTALLED. LONGERON AND SPLICE REPAIR IAW 53-02, FIG 18, CORROSION FOUND TO BE LEVEL 2 CAUSED BY A LAV SPILL.
- [SDR DALA2016050903818](https://openairdocs.org/sdr/DALA2016050903818.md): Longeron · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BILGE, LAV SPILL, LONGERON 25L, SPLICE HAS CORROSION AT BS 1295. COMPLETED LONGERON AND SPLICE REPAIR IAW 53-02, FIG 18 CORROSION FOUND TO BE LEVEL 2 CAUSED BY A LAV SPILL.
- [SDR DALA2016050903817](https://openairdocs.org/sdr/DALA2016050903817.md): Longeron · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BILGE, LAV SPILL, L27L HAS MANY SPOTS OF CORROSION, BS 1287-1322. REPAIRED IAW SRM 53-01, FIG 1.
- [SDR DALA2016050903816](https://openairdocs.org/sdr/DALA2016050903816.md): Longeron · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BILGE, LAV SPILL, LONGERON 26L SPLICE CORRODED BLOW OUT, BS 1295. INSTALLED LONGERON AND SPLICE REPAIR IAW 53-02, FIG 18 CORROSION FOUND TO BE LEVEL 2 CAUSED BY A LAV SPILL.
- [SDR DALA2016050903815](https://openairdocs.org/sdr/DALA2016050903815.md): Longeron · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BILGE, LAV SPILL-L25L HAS CORROSION, BS 1287-1309. INSTALLED LONGERON AND SPLICE REPAIR IAW 53-02, FIG 18 CORROSION FOUND TO BE LEVEL 2 CAUSED BY A LAV SPILL.
- [SDR DALA2016050903814](https://openairdocs.org/sdr/DALA2016050903814.md): Door Sill · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT AFT DOOR SILL SUPPORT GUSSET HAS CORROSION, BS 1212. REPLACED SUPPORT.
- [SDR DALA2016050903813](https://openairdocs.org/sdr/DALA2016050903813.md): Butt Joint · corroded · May 8, 2016 · N935DL · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT, LAV SPILL, BUTT SPLICE CORRODED AND STAINED BETWEEN BS 1174 AND 1193, L26L TO L28R. REPAIRED IAW SRM 53-01, FIG 1.
- [SDR DALA2016050803812](https://openairdocs.org/sdr/DALA2016050803812.md): Spacer · corroded · May 7, 2016 · N935DL · Doug MD88 · Fuselage Main, Structure
  > MID CARGO COMPARTMRNT, SHIM, SPACER UNDER FWD LOWER JAMB DOOR STOP CORRODED, EXFOLIATED, FASTENERS HEADS GOING THROUGH LOWER SKIN THROUGH DOOR STOP ARE POPPED. REPAIRED IAW 53-05, FIG 123A.
- [SDR DALA2016050803811](https://openairdocs.org/sdr/DALA2016050803811.md): Spacer · corroded · May 7, 2016 · N935DL · Doug MD88 · Fuselage Main, Structure
  > MID CARGO COMPARTMENT SHIM SPACER UNDER FWD LOWER JAMB DOOR STOP CORRODED, EXFOLIATED, FASTENERS HEADS GOING THROUGH LOWER SKIN THROUGH DOOR STOP ARE POPPED. REPAIRED IAW 53-05, FIG 123A.
- [SDR DALA2016050803810](https://openairdocs.org/sdr/DALA2016050803810.md): Floor Support · corroded · May 7, 2016 · N935DL · Doug MD88 · Fuselage Miscellaneous Structure
  > MID CARGO COMPARTMENT HAS CORROSION UNDER FLOOR SUPPORT NUTPLATES BS 786. REPLACED FLOOR SUPPORT SRM 51-30-02.
- [SDR DALA2016010300012](https://openairdocs.org/sdr/DALA2016010300012.md): Skin · cracked · Jan 2, 2016 · N935DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FOUND APPROXIMATELY 1.75 CRACK IN SKIN APPROXIMATELY 6 IN AFT FROM ELEVATOR ACCUMULATOR ACCESS DOOR. ELEVATOR ACCUMULATOR ACCESS DOOR CUTOUT SKIN CRACKED FROM UPPER AFT CORNER RADIUS TO CLOSEST FASTENER AFT. C/W PRI 542690-14, REV 0,1,2,3,4 AND FINAL, C/W ER
- [SDR DALA2016010100010](https://openairdocs.org/sdr/DALA2016010100010.md): Skin · damaged · Dec 31, 2015 · N935DL · Doug MD88 · Fuselage Main, Plate/Skin
  > THREE LIGHTINING STRIKE DAMAGE LOWER FORWARD FUSELAGE JUST AFT OF ELECTRONIC EQUIPMENT COMPARTMENT ACCESS. 1, 7" AFT OF ELECTRONIC EQUIPMENT CUTOUT AT S29R, 2, 9.5 " AFT OF E/E CUTOUT 3" RT OF S30 AT FASTENER. 3, 11" AFT OF ELECTRONIC EQUIPMENT CUTOUT 3" RT
- [SDR DALA2015091705692](https://openairdocs.org/sdr/DALA2015091705692.md): Housing · worn · Sep 16, 2015 · N935DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENACE FOUND AFT ENTRANCE DOOR TAILCONE RELEASE PULL CABLE HOUSING WORN. THE TAIL CONE RELEASE CABLE WAS REPLACED.
- [SDR DALA2015081304955](https://openairdocs.org/sdr/DALA2015081304955.md): Battery Pack · inoperative · Aug 12, 2015 · N935DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 11-15 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.
- [SDR DALA2015081004872](https://openairdocs.org/sdr/DALA2015081004872.md): Battery Pack · inoperative · Aug 6, 2015 · N935DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTS IN ROWS 11-14 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.
- [SDR DALA2015072804734](https://openairdocs.org/sdr/DALA2015072804734.md): Actuator · malfunctioned · Jul 27, 2015 · N935DL · Doug MD88 · Landing Gear Actuator
  > DURING CLIMBOUT AT ABOUT FL200, RT MAIN GEAR RED LIGHT ILLUMINATED. SEVERAL MINUTES LATER AMBER GEAR DOOR OPEN LIGHT ILLUMINATED INTERMITTENTLY. AT FL250 LEVELED OFF AND LIGHT CONTINUED. RAN QRH 14.19, THRU STEP 3. AUTO SPEEDBRAKE RESET ON ITS OWN. ALL L
- [SDR DALA2015050803183](https://openairdocs.org/sdr/DALA2015050803183.md): Connector · disconnected · May 7, 2015 · N935DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE AT SEAT 14D. MAINTENANCE CONNECTED A DISCONNECTED CONNECTOR AND THE OPS CHECKED GOOD.
- [SDR DALA14020430935](https://openairdocs.org/sdr/DALA14020430935.md): Striker · out of position · Apr 3, 2014 · N935DL · Doug MD88 · Aerodynamic Fairings
  > PERFORMED TAILCONE RELEASE SYSTEM OPS CHECK, SYS FAILED, AND MAINTENANCE FOUND THE TAILCONE EXTERIOR RELEASE CABLE PULL FORCE WAS OUT OF ALLOWABLE LIMITS. FOUND WAS THE DOOR JAMB UPPER FITTING WAS OUT OF CONFIGURATION AND WAS CORRECTED BY REMOVING THE STRIKER
- [SDR DALA14020330935](https://openairdocs.org/sdr/DALA14020330935.md): Pulley · worn · Apr 1, 2014 · N935DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE INBD RELEASE LATCH CABLE PULLEY FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE CABLE PULLEY WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.
- [SDR DALA14020230935](https://openairdocs.org/sdr/DALA14020230935.md): Bracket · worn · Mar 29, 2014 · N935DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE KEVLAR CABLE CAM BASE BRACKET FOR THE TAILCONE WAS WORN, OUT OF ALLOWABLE LIMITS. THE KEVLAR CABLE CAM BASE BRACKET WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.
- [SDR DALA13067060935](https://openairdocs.org/sdr/DALA13067060935.md): Wire Harness · damaged · Dec 6, 2013 · N935DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 12DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.
- [SDR DALA13012060935](https://openairdocs.org/sdr/DALA13012060935.md): Airstair · lack of lube · Mar 1, 2013 · N935DL · Doug MD88 · Entrance Stairs
  > CATWALK IN TAIL SECTION DOWN, WILL NOT COME UP WITH AIRSTAIRS DOWN. FOUND NO DAMAGE TO LIFT CABLES OR RIGGING. SPRINGS DO NOT APPEAR TO BE BROKEN BUT MAY BE WORN OUT. VERIFIED DOWNLOCK PIN OPERATES NORMALLY. LUBED CATWALK OPS CHECKS GOOD IAW AMM 52-62.
- [SDR DALA12015540935](https://openairdocs.org/sdr/DALA12015540935.md): Frame · cracked · Dec 7, 2012 · N935DL · Doug MD88 · Fuselage Main, Frame
  > FUSELAGE FRAME CRACKED AT LONGERON 1. REPAIRED IAW ER/A 489679-14 REV C. CHECKED GOOD.

Next page: https://openairdocs.org/deregistered/N935DL-2020-11-09/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 = 'N935DL' AND deregistration_id = 'N935DL-2020-11-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N935DL-2020-11-09/reports

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