# Service difficulty reports: N926DL, cancelled Apr 8, 2019

A list on [N926DL, cancelled Apr 8, 2019](https://openairdocs.org/deregistered/N926DL-2019-04-08.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 4 · 198 reports

- [SDR DALA2018022301105](https://openairdocs.org/sdr/DALA2018022301105.md): Battery Pack · inoperative · Feb 22, 2018 · N926DL · Doug MD88 · Emergency Lighting
  > FWD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERIES.
- [SDR DALA2017080906071](https://openairdocs.org/sdr/DALA2017080906071.md): Threshold · damaged · Aug 8, 2017 · N926DL · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR THRESHOLD FWD AND AFT OF DOOR STOP FITTINGS. NUMEROUS FASTENER AND RIVNUT HOLES ARE OUT OF ROUND AND CORRODED BS 1155 - 1212. BEAM INSTALLATION COMPLETED IAW DWG 5930483.
- [SDR DALA2017080906068](https://openairdocs.org/sdr/DALA2017080906068.md): Skin · corroded · Aug 8, 2017 · N926DL · Doug MD88 · Fuselage Main, Plate/Skin
  > AFT CARGO HAD MULTIPLE AREAS OF CORROSION ON INNER SKIN UNDER CARGO DOOR BEAM BETWEEN BS 1155 AND 1212. COMPLIED WITH PRI ER/A 560725-14, REV 0, AND ER/A 560725-14, REV ORIGINAL. RECEIVED FINAL ER/A 560725-14, REV ORIGINAL.
- [SDR DALA2017080705987](https://openairdocs.org/sdr/DALA2017080705987.md): Tee Fitting · corroded · Aug 6, 2017 · N926DL · Doug MD88 · Fuselage Main, Attach Fittings
  > AFT CARGO BAY LONGERONS 28 AND 29R, BS 1231 FOUND CORROSION ON TEE BRACKET. REPLACED THE TEE BRACKET IAW DWG 5930483.
- [SDR DALA2017080705986](https://openairdocs.org/sdr/DALA2017080705986.md): Tee Fitting · corroded · Aug 6, 2017 · N926DL · Doug MD88 · Fuselage Main, Attach Fittings
  > AFT CARGO BAY LONGERON 28 AND 29R, BS 1212 LIGHT CORROSION ON TEE BRACKET. REPLACED THE TEE BRACKET IAW DWG 5930483.
- [SDR DALA2017080405960](https://openairdocs.org/sdr/DALA2017080405960.md): Strap · corroded · Aug 3, 2017 · N926DL · Doug MD88 · Fuselage Main, Structure
  > AFT CARGO DOOR FRAME STRAP CORRODED. THE STRAP WAS REPLACED.
- [SDR DALA2017080205863](https://openairdocs.org/sdr/DALA2017080205863.md): Shear Tie · corroded · Aug 1, 2017 · N926DL · Doug MD88 · Fuselage Internal Mounting Structure
  > AFT CARGO, CORROSION ON SHEAR TIE BS 1212 BETWEEN LONGERONS 29-30R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-10-03, AND 51-30-05.
- [SDR DALA2017041703110](https://openairdocs.org/sdr/DALA2017041703110.md): Slide · low pressure · Apr 14, 2017 · N926DL · Doug MD88 · Escape Slide
  > L1 DOOR SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED THE SLIDE IAW AMDS 2561-4964.
- [SDR DALA2017010800208](https://openairdocs.org/sdr/DALA2017010800208.md): Fitting · cracked · Jan 7, 2017 · N926DL · Doug MD88 · Spoilers
  > RIGHT WING GROUND SPOILER ATTACH FITTING CRACKED AT ACTUATOR FWD POINT. REPLACED THE FITTING ASSY.
- [SDR DALA2017010500138](https://openairdocs.org/sdr/DALA2017010500138.md): Battery Pack · discharged · Jan 4, 2017 · N926DL · Doug MD88 · Emergency Lighting
  > CEILING EMERGENCY LIGHTING INOP-ROWS 16 THROUGH 20. REMOVED AND REPLACED B5-102 BATTERY PACK PER AMM 33-53.
- [SDR DALA2017010400076](https://openairdocs.org/sdr/DALA2017010400076.md): Wire · broken · Jan 3, 2017 · N926DL · Doug MD88 · Light System Wiring
  > SEAT EMERGENCY LIGHT INOP ROW 31-36. FOUND BROKEN WIRE AT SEAT 31. REPAIRED WIRE PER SWPM 20-10-03.
- [SDR DALA2017010200029](https://openairdocs.org/sdr/DALA2017010200029.md): Skin · damaged · Jan 1, 2017 · N926DL · Doug MD88 · Fuselage Main, Plate/Skin
  > SKIN BS 1128, STRINGER 29L DAMAGED. REPAIRED IAW PRI 554017 REV. 0 AND REV. 1 AND ER/A 554017-14 REV. ORIGINAL.
- [SDR DALA2016121909970](https://openairdocs.org/sdr/DALA2016121909970.md): Light · inoperative · Dec 17, 2016 · N926DL · Doug MD88 · Emergency Lighting
  > FWD RED EMER LIGHT INOP. RELAMPED PER AMM 33-53.
- [SDR DALA2016051203902](https://openairdocs.org/sdr/DALA2016051203902.md): Connector · damaged · May 12, 2016 · N926DL · Doug MD88 · Light System Wiring
  > SEAT ROW 34ED EMERGENCY LIGHT INOPERATIVE. REPLACED PIGTAIL LIGHT ASSEMBLY, OPS NOW OK IAW AMM 33-51.
- [SDR DALA2016040802711](https://openairdocs.org/sdr/DALA2016040802711.md): Cam · loose · Apr 6, 2016 · N926DL · Doug MD88 · Aerodynamic Fairings
  > TAILCONE JETTISON CAM ASSY LOOSE. RIGGED JETTISON CAM IAW AMM 53-50.
- [SDR DALA2016040802709](https://openairdocs.org/sdr/DALA2016040802709.md): Skin · not reported · Mar 27, 2016 · N926DL · Doug MD88 · Rudder, Plate/Skin
  > RUDDER FLAME SPRAY BAD. REPLACED RUDDER IAW WC 2720-4187.
- [SDR DALA2016032302284](https://openairdocs.org/sdr/DALA2016032302284.md): Wire Harness · inoperative · Mar 22, 2016 · N926DL · Doug MD88 · Light System Wiring
  > EMERGENCY LIGHT ON SEAT 26RT IS INOPERATIVE. REPLACED WIRING HARNESS ON SEAT 26 RT.
- [SDR DALA2016022801523](https://openairdocs.org/sdr/DALA2016022801523.md): Skin · cracked · Feb 27, 2016 · N926DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACKED FUSELAGE SKIN IN BS 535 BETWEEN LONG 18R AND 19R. REPAIRED IAW ETI-88-16-080 REV 3 AND ER/A 543170-14, REV ORIGINAL.
- [SDR DALA2016022701502](https://openairdocs.org/sdr/DALA2016022701502.md): Shear Angle · damaged · Feb 26, 2016 · N926DL · Doug MD88 · Fuselage Miscellaneous Structure
  > MINIMUM FASTENER REQUIRMENT ON SHEAR ANGLE FWD TAB, EITHER SIDE OF THE LOWER TEE CHORD CUT LINE DOES NOT COMPLY BS 1338 BETWEEN LONGERONS 26-27L, & 26-27R. REPAIR WAS PERFORMED IAW ER/A 543163-14, REV ORIGINAL
- [SDR DALA2016022601458](https://openairdocs.org/sdr/DALA2016022601458.md): Skin · corroded · Feb 25, 2016 · N926DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON PREVIOUS REPAIR DOUBLER AT FUSELAGE SKIN INNER STRUCTURE BETWEEN BS 1250- 1271 AND LONGERON 29RT AND LONGERON 28RT AT AFT CARGO COMPARTMENT INNER STRUCTURE. DOUBLER WAS REPLACED IAW ETI-88-16-078, REV 1 AND ER/A 543166-14, REV ORIGINAL.
- [SDR DALA2016022601448](https://openairdocs.org/sdr/DALA2016022601448.md): Intercostal · cracked · Feb 25, 2016 · N926DL · Doug MD88 · Passenger/Crew Doors
  > CRACKED INTERCOSTAL BETWEEN BEAM NR 4 AND 5 AT L1 PASSENGER DOOR. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2, 51-10-4, 51-10-3 PAR 14/21 AND DWG: 9955763, REV: M.
- [SDR DALA2016022601446](https://openairdocs.org/sdr/DALA2016022601446.md): Pan · cracked · Feb 25, 2016 · N926DL · Doug MD88 · Passenger/Crew Doors
  > CRACKED PAN INNER STRUCTURE AFT EDGE OF FWD MAIN ENTRANCE DOOR, L1 ON AFT UPPER CORNER POSITION. DUE TO EXCESSIVE DAMAGE THE L1 DOOR WAS REPLACED AND WILL BE INSTALLED UNDER CARD 48, ZONE 201.
- [SDR DALA2016022301339](https://openairdocs.org/sdr/DALA2016022301339.md): Door Frame · corroded · Feb 22, 2016 · N926DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON AFT CARGO COMPARTMENT DOOR JAMB UPPER BEAM FROM BS 1155 TO 1190. BEAM WAS REPLACED IAW SRM 51-30-5, 51-10-4, 51-10-3, PAR 14 AND 21.
- [SDR DALA2016022301335](https://openairdocs.org/sdr/DALA2016022301335.md): Intercostal · corroded · Feb 22, 2016 · N926DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BETWEEN BS 1212 TO 1231 LONGERON 29LT AT AT AFT CARGO COMPARTMENT STRUCTURE. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR DALA2016022301334](https://openairdocs.org/sdr/DALA2016022301334.md): Beam · cracked · Feb 22, 2016 · N926DL · Doug MD88 · Passenger/Crew Doors
  > CRACKED BEAM NR 1 AFT EDGE AT FWD MAIN ENTRANCE DOOR. L1, BEAM NR 1 AFT EDGE AT FWD MAIN ENTRANCE DOOR WAS REPAIR IAW SRM 52-05D, FIG 81, SHEET 3, 51-30-1, 51-30-5 AND 51-10-3, PAR 14.
- [SDR DALA2016022301333](https://openairdocs.org/sdr/DALA2016022301333.md): Intercostal · cracked · Feb 22, 2016 · N926DL · Doug MD88 · Passenger/Crew Doors
  > CRACKED INTERCOSTAL BETWEEN BEAM NR 4 AND NR 5 AND MECHANISM AT FWD MAIN ENTRANCE DOOR, L1. INTERCOSTAL MAIN ENTRANCE DOOR WAS REPLACE IAW SRM 51-30-2.
- [SDR DALA2016022301332](https://openairdocs.org/sdr/DALA2016022301332.md): Access Panel · damaged · Feb 22, 2016 · N926DL · Doug MD88 · Wing, Plate/Skin
  > ELONGATED HOLE ON FUEL ACCESS PLATE NR 1454C. FUEL ACCESS PLATE NR 1454C WAS REPLACED IAW IPC 57-30-00 AND WIL BE INSTALLED UNDER CARD 5710-01110-05, JOB 022-0001.
- [SDR DALA2016022401367](https://openairdocs.org/sdr/DALA2016022401367.md): Beam · cracked · Feb 21, 2016 · N926DL · Doug MD88 · Passenger/Crew Doors
  > CRACKED BEAM NR 4 FWD EDGE AT FWD MAIN ENTRANCE DOOR. L1 BEAM NR 4 WAS REPAIRED IAW SRM 52-05 D FIG 88, SHEET 3, 51-30-1, 51-10-3, PAR 14, 51-10-2 AND 51-30-5.
- [SDR DALA2016022201292](https://openairdocs.org/sdr/DALA2016022201292.md): Door Frame · cracked · Feb 21, 2016 · N926DL · Doug MD88 · Fuselage Main, Structure
  > CRACKED PREVIOUS REPAIR ON NLG DOOR JAMB BS Y=46, X=+18LHZ=-29 AT NLG WHEEL WELL. DOUBLER PREVIOUS REPAIR WAS REPLACED IAW 53-05, FIG 110, 51-10-2, 51-10-4, 51-10-3 AND 51-30-2.
- [SDR DALA2016022201300](https://openairdocs.org/sdr/DALA2016022201300.md): Skin · not reported · Feb 19, 2016 · N926DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING NDT INSPECTION 2 DISCREPANT AREAS, DOUBLER REPAIRS WERE FOUND ON FUSELAGE SKIN AT BS 1271, BETWEEN LONGERON 1 AND 2 RT, ID TAG: "P" 6-25-12 ER/A 504801-14AD AND BS 1193, BETWEEN LONGERON 1 AND 3 LT.
- [SDR DALA2016022801521](https://openairdocs.org/sdr/DALA2016022801521.md): Duct · cracked · Feb 18, 2016 · N926DL · Doug MD88 · Cabin Cooling System
  > CRACKED RATIO RACK EXHAUST DUCT BETWEEN BS Y=256 TO 275 LONG 20LT TO 21LT AT FUSELAGE SKIN. RADIO RACK EXHAUST DUCT WAS REPAIRED IAW ER/A 464964-14 MA, REV C.
- [SDR DALA2016022501445](https://openairdocs.org/sdr/DALA2016022501445.md): Door · corroded · Feb 18, 2016 · N926DL · Doug MD88 · Landing Gear Doors
  > CORROSION ON SEATING AREA OF RUB STRIP AT RT MLG STRUT DOOR. RT MLG STRUT DOOR WAS REPLACED DUE EXCESIVE DAMAGE.
- [SDR DALA2016021801230](https://openairdocs.org/sdr/DALA2016021801230.md): Frame · cracked · Feb 17, 2016 · N926DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME BS 1510. THE FRAME WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3, PAR 21 AND 14.
- [SDR DALA2015101206074](https://openairdocs.org/sdr/DALA2015101206074.md): Wire · loose · Oct 12, 2015 · N926DL · Doug MD88 · Light System Wiring
  > A PASSENGER REPORTED A BROKEN WIRE ALONG THE GROUND NEAR THE SIDEWALL, AT ROW 20 IN THE CABIN. MAINTENANCE FOUND A WIRE FOR THE EMERGENCY LIGHTS AT ROW 20DE TO BE LOOSE AND IT WAS REPAIRED. THE SYSTEM RETURNED TO NORMAL OPERATION.
- [SDR DALA2014112406238](https://openairdocs.org/sdr/DALA2014112406238.md): Release Cable · frayed · Nov 23, 2014 · N926DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE CABLE WAS BULGED AND FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.
- [SDR DALA2014112406237](https://openairdocs.org/sdr/DALA2014112406237.md): Latch · worn · Nov 23, 2014 · N926DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE LT LOWER RELEASE LATCH ASSEMBLY FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE ASSEMBLY WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.
- [SDR DALA2014112406239](https://openairdocs.org/sdr/DALA2014112406239.md): Bracket · worn · Nov 22, 2014 · N926DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE TAILCONE LT AND RT SPRING BRACKETS ARE WORN FROM THE SPRING. THE BRACKETS WERE REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.
- [SDR DALA2014112106236](https://openairdocs.org/sdr/DALA2014112106236.md): Pan · cracked · Nov 20, 2014 · N926DL · Doug MD88 · Fuselage Miscellaneous Structure
  > LEFT FWD OVERWING EMERGENCY DOOR PAN CRACKED AT UPPER AFT SUPPORT BRACKET. REMOVED LINER AND SUPPORT BRACKET. HFEC IAW NDT SPM 06-10-01.001 TO VERIFY CRACK AND MARK ENDS. REMOVED FASTENERS TO PEEL UP INNER SKIN FOR ACCESS. STOP DRILLED ENDS OF CRACK TO 1/4 DI
- [SDR DALA2014111906178](https://openairdocs.org/sdr/DALA2014111906178.md): Receptacle · worn · Nov 18, 2014 · N926DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT ALL OF THE TAILCONE RELEASE SYSTEM GUIDE PIN RECEPTACLES WERE WORN BEYOND ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.
- [SDR DALA14030280926](https://openairdocs.org/sdr/DALA14030280926.md): Battery Pack · inoperative · May 13, 2014 · N926DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THE COCKPIT, L1, AND R1 OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE LIGHTS CHECKED NORMAL.
- [SDR DALA14017350926](https://openairdocs.org/sdr/DALA14017350926.md): Sign · inoperative · Mar 19, 2014 · N926DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT RT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.
- [SDR DALA14017370926](https://openairdocs.org/sdr/DALA14017370926.md): Unknown · odor · Mar 15, 2014 · N926DL · Doug MD88 · Air Distribution System
  > CREW ELECTED TO TURN BACK AFTER TAKEOFF DUE TO BOTH AFT LAVATORY SMOKE DETECTORS SOUNDING AND PASSENGERS REPORT AN ODOR. MAINTENANCE INSPECTED BOTH ENGINES INLETS AND EXHAUST BUT FOUND NO DISCREPANCIES. NO TROUBLE WAS FOUND AND A DUCT BURNOUT WAS PERFORMED. A
- [SDR DALA13060270926](https://openairdocs.org/sdr/DALA13060270926.md): Wire · pulled · Nov 10, 2013 · N926DL · Doug MD88 · Light System Wiring
  > DURING FUNCTIONAL CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT ROW 27DE INOPERATIVE. FOUND A WIRE PULLED LOOSE FROM THE SPLICE CONNECTOR, REPAIRED CONNECTOR & WIRE, AND THE SYSTEM RETURNED TO NORMAL OPERATION.
- [SDR DALA13035140926](https://openairdocs.org/sdr/DALA13035140926.md): Rub Strip · missing · Jul 12, 2013 · N926DL · Doug MD88 · Entrance Stairs
  > PILOT DISCOVERED THAT THE CATWALK IN TAIL SECTION, WOULD NOT RETRACT BECAUSE A RETRACT PANEL WAS BINDING ON THE CEILING PANEL. THE SYS WAS FORWARDED AND PLACARD PROCEDURES WERE COMPLIED WITH. ON 17JUL, IT WAS FOUND THAT THE LT SIDE RUB STRIP WAS MISSING, BUT
- [SDR DALA13026830926](https://openairdocs.org/sdr/DALA13026830926.md): Strap · disconnected · May 31, 2013 · N926DL · Doug MD88 · Escape Slide
  > INSPECTION DISCOVERED EMERGENCY ESCAPE SLIDE COVER SECURING STRAPS DISCONNECTED. THE TAILCONE SLIDE COVER STRAPS WERE REINSTALLED AND AN RII WAS COMPLETED SATISFACTORILY.
- [SDR DALA13026820926](https://openairdocs.org/sdr/DALA13026820926.md): Frame · cracked · May 31, 2013 · N926DL · Doug MD88 · Fuselage Main, Frame
  > BS 1510, FRAME CRACKED. RT UPPER, AT RUDDER PCU ATTACH. REMOVED UPPER RT TAILCONE LATCH, CUTOUT CRACKS, CUTOUT SIZE 1" X 1.375". HFEC INSP AND NO OTHER CRACKS FOUND. FABRICATED AND INSTALLED REPAIR WORK IAW ERA 515449-14, REV ORG ASSOCIATED ER/A 14-515449,
- [SDR DALA13026420926](https://openairdocs.org/sdr/DALA13026420926.md): Skin · cracked · May 28, 2013 · N926DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT BS 1437, BETWEEN LONGERON 2-3R, REPAIRED IAW ERA 515410-14, REV ORIGINAL.
- [SDR DALA13026410926](https://openairdocs.org/sdr/DALA13026410926.md): Skin · cracked · May 28, 2013 · N926DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT BS 1437, BETWEEN LONGERON 2 - 3L. REPAIRED IAW ERA 515409-14, REV ORIGINAL.
- [SDR DALA13024760926](https://openairdocs.org/sdr/DALA13024760926.md): Bushing · worn · May 26, 2013 · N926DL · Doug MD88 · Aerodynamic Fairings
  > DURING AN INSPECTION, MX DISCOVERED THAT THE TAILCONE JETTISON RELEASE PULL-CABLE BUSHINGS, PIN 11, LATCH RECEPTACLE, AND ALIGNMENT PIN RECEPTACLES WERE ALL WORN BEYOND ALLOWABLE LIMITS. THE SYS WAS REPAIRED BY BUSHING REPLACEMENTS IAW AMM 53-53-00/02, SRM 51-
- [SDR DALA13022450926](https://openairdocs.org/sdr/DALA13022450926.md): Battery Pack · inoperative · May 13, 2013 · N926DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT SEAT ROWS 32-34 INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Next page: https://openairdocs.org/deregistered/N926DL-2019-04-08/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 = 'N926DL' AND deregistration_id = 'N926DL-2019-04-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N926DL-2019-04-08/reports

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