# Service difficulty reports: N914DL, cancelled Jan 24, 2020

A list on [N914DL, cancelled Jan 24, 2020](https://openairdocs.org/deregistered/N914DL-2020-01-24.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 · 142 reports

- [SDR DALA2018062704235](https://openairdocs.org/sdr/DALA2018062704235.md): Wire · unsecure · Jun 22, 2018 · N914DL · Doug MD88 · Light System Wiring
  > SEAT MOUNTED EMERG. LIGHT AT 32D IS INOP. SECURED WIRE TO EMER LIGHT AT SEAT 32D REF SPWM CH 20 OPS CKS GOOD.
- [SDR DALA2018012200328](https://openairdocs.org/sdr/DALA2018012200328.md): Door Frame · corroded · Jan 22, 2018 · N914DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION FOUND ON THE R1 DOOR FRAME, AFT SIDE OF THE FRAME AT THE CUSP. REPAIRED IAW SRM 53-05, FIG 55.
- [SDR DALA2018011900299](https://openairdocs.org/sdr/DALA2018011900299.md): Structure · cracked · Jan 18, 2018 · N914DL · Doug MD88 · Vertical Stabilizer
  > OPEN HOLE INSPECTION IAW NDTSPM 06-10-01.003 OF SEVENTH HOLE FROM BOTTOM OF REPAIR INDICATES A CRACK. REPAIRED IAW ERA 565018-14, REV ORG.
- [SDR DALA2017122808941](https://openairdocs.org/sdr/DALA2017122808941.md): Battery Pack · inoperative · Dec 27, 2017 · N914DL · Doug MD88 · Emergency Lighting
  > EMERGENCY OVERHEAD LIGHTS INOPERATIVE FROM ROWS 27 - 36. REPLACED THE BATTERY PACK AT ROW 29 IAW AMM 33-50. ALL EMERGENCY LIGHTS OPS CHECKED GOOD.
- [SDR DALA2017092207053](https://openairdocs.org/sdr/DALA2017092207053.md): Battery · defective · Sep 22, 2017 · N914DL · Doug MD88 · Emergency Lighting
  > DURING SERVICE CHK FOUND FWD OVERWING EMER EXIT SIGNS NOT LIGHTING UP. T/S AND FOUND BAD BATTERY CELL FOR FWD OVERWING EMERGENCY EXIT SIGNS IAW AMM 33-50 SYSTEM CHECKS GOOD.
- [SDR DALA2017030701845](https://openairdocs.org/sdr/DALA2017030701845.md): Skin · damaged · Mar 7, 2017 · N914DL · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STAB LEADING EDGE, 5TH FASTENER HOLE FROM LOWER EDGE IS OUT OF ROUND. REPAIRED IAW ER/A 556179-14.
- [SDR DALA2017030701844](https://openairdocs.org/sdr/DALA2017030701844.md): Spar Cap · damaged · Mar 7, 2017 · N914DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STAB LT SIDE FRONT SPAR CAP FWD FLANGE 5TH FASTENER ABOVE VSS ZFS 52.267 HOLE IS OUT OF ROUND. REPAIRED IAW ER/A 556179-14AD.
- [SDR DALA2017030601775](https://openairdocs.org/sdr/DALA2017030601775.md): Bracket · cracked · Mar 5, 2017 · N914DL · Doug MD88 · Aerodynamic Fairings
  > TAIL CONE RIGHT UPPER BAYONET FITTING BRACKETS CRACKED. DRILLED REPLACEMENT BRACKETS. TREATED, PRIMED & PAINTED PART. INSTALLED THE BRACKETS IAW SRM 51-30-02.
- [SDR DALA2017030501772](https://openairdocs.org/sdr/DALA2017030501772.md): Former · broken · Mar 3, 2017 · N914DL · Doug MD88 · Wing Main, Frame Structure
  > FOUND RT WING UPPER FILLET PANEL MOUNT FORMER BROKEN AT WS 886. REMOVED AND REPLACED THE FORMER IAW DWG 9951259.
- [SDR DALA2017030301731](https://openairdocs.org/sdr/DALA2017030301731.md): Frame · cracked · Mar 2, 2017 · N914DL · Doug MD88 · Fuselage Main, Frame
  > F/AS REPORTED VIBRATION AT 25DE. HYDRAULIC PUMPS OFF OR ON DOES NOT CHANGE VIBRATIONS. LOAD AND VIBRATING ALL PHASES NO VISIBLE FAILURES. FOUND A CRACK ON THE RT MLG WHEEL WELL AREA. REMOVED DAMAGED FRAME. FOUND SEALS JUST FWD OF MLG DOORS VERY LOOSE AND
- [SDR DALA2016110608271](https://openairdocs.org/sdr/DALA2016110608271.md): Cap · unsecure · Nov 4, 2016 · N914DL · Doug MD88 · APU Oil System
  > PERFORMED ATB DUE TO REPORTED SMOKE IN CABIN AFTER TAKEOFF. FOUND APU OIL CAP NOT SECURE. APU COMPARTMENT AND INLET CLEANED. LEAK CHECKED GOOD. PERFORMED DUCT BURNOUT PROCEDURE WC 7100-2619. NO ODOR PRESENT.
- [SDR DALA2015121007486](https://openairdocs.org/sdr/DALA2015121007486.md): Skin · damaged · Dec 9, 2015 · N914DL · Doug MD88 · Trailing Edge Flaps
  > AWR DAMAGE T, WEAR ON INBD GUIDE VANE LWR SKIN AT LT WING. INBD GUIDE VANE AT LT WING WAS R & R AND INSTALLED IAW AMM 27-51-03-201, PAR 3A, B, AND SRM 57-03D, PAR II AND ACFT 0914, CARD 2000-8149-8149-03.
- [SDR DALA2015120907464](https://openairdocs.org/sdr/DALA2015120907464.md): Frame · cracked · Dec 8, 2015 · N914DL · Doug MD88 · Fuselage Main, Frame
  > ELONGATED HOLE ON FRAME BS 1380 BETWEEN LONGERON 12 LT TO 13 LT AT AFT ACCESSORY COMPARTMENT. PARTS REPAIR WERE FABRICATED, TREATED, PAINTED, SHEAR CLIP AND SHIM WERE INSTALLED IAW SR 51-10-3, PAR 14, 21, 51-30-5, ETI-88-15-425, REV 2 AND ER/A 541544-14 REV O
- [SDR DALA2015120907463](https://openairdocs.org/sdr/DALA2015120907463.md): Frame · cracked · Dec 8, 2015 · N914DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME, BS 1388 LONG 2RT AT AFT ACC COMPARTMENT. REPAIR SPAR FRAME BS 1388 WAS ATTENDED WITH ER/A N; 541564-14, REV ORIGINAL.
- [SDR DALA2015120807452](https://openairdocs.org/sdr/DALA2015120807452.md): Frame · cracked · Dec 7, 2015 · N914DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME BS 1485 AT AFT ACCCOMPARTMENT. FRAME WAS REPAIRED IAW SRM 53-03, FIG 49, SHEET 2, 3 AND SRM 51-10-3, PARA 21, 14 AND SRM 51-30-5 AND SRM 51-30-2.
- [SDR DALA2015120707432](https://openairdocs.org/sdr/DALA2015120707432.md): Skin · damaged · Dec 6, 2015 · N914DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON FUSELAGE SKIN AT AFT UPPER CORNER LT WINDOW BELT BETWEEN BS 693 AND 712. LIGHTNING STRIKE WAS REPAIRED AND DIMENTIONS AS FOLLOW: (UT) WAS ACCOMPLISHED IAW NDT-SPM 04-00-07, PARA 5, FIG. 5, ON AFT UPPER CORNER ORIGINAL THICKNESS 0.090 AND R
- [SDR DALA2015120707431](https://openairdocs.org/sdr/DALA2015120707431.md): Skin · damaged · Dec 6, 2015 · N914DL · Doug MD88 · Fuselage Main, Plate/Skin
  > TWO LIGHTNING STRIKES ON FUSELAGE SKIN AT AFT LOWER CORNER LT WINDOW BELT BETWEEN BS 617 AND 636. REPAIRED IAW ER/A 541573-14 REV ORIGINAL., UT WAS ACCOMPLISHED IAW NDT-SPM, 04-00-07, PAR. 5, FIG 3
- [SDR DALA2015120707430](https://openairdocs.org/sdr/DALA2015120707430.md): Skin · damaged · Dec 6, 2015 · N914DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKES, 3 EAS, ON FUSELAGE SKIN AT FWD LOWER CORNER LT WINDOW BELT BETWEEN BS 636 AND 655. LIGHTNING STRIKES WERE REPAIRED AND DIMENTIONS AS FOLLOW: UT WAS ACCOMPLISHED IAW NDT-SPM 04-00-07, PARA 5, FIG 3, ON FWD LWR CORNER, ORIGINAL THICKNESS 0.0
- [SDR DALA2015120707429](https://openairdocs.org/sdr/DALA2015120707429.md): Skin · damaged · Dec 6, 2015 · N914DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKES ON FUSELAGE SKIN AT FWD UPPER CORNER LT WINDOW BELT BETWEEN BS 655 AND 674. LIGHTNING STRIKES WERE REPAIRED AND DIMENTIONS AS FOLLOW: UT, WAS ACCOMPLISHED IAW NDT-SPM, 04-00-07, PARA 5, FIG 3, ON FWD UPPER CORNER ORIGINAL THICKNESS 0.135" AN
- [SDR DALA2015120707427](https://openairdocs.org/sdr/DALA2015120707427.md): Structure · damaged · Dec 5, 2015 · N914DL · Doug MD88 · Fuselage Main, Structure
  > TWO FASTENERS IN THE FWD TAB ON EITHER SIDE OF THE CUT LINE OF LT APB LOWER CHORD. REPAIRED IAW ER/A 541560-14, REV ORIG.
- [SDR DALA2015120507392](https://openairdocs.org/sdr/DALA2015120507392.md): Support · cracked · Dec 4, 2015 · N914DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ON AFT FACE FRAME, BS 1437, LONG 1 AT AFT ACCESSORY COMPARTMENT. SUPPORT WAS REPLACED IAW SRM 53-30-5, 51-10-3 AND DWG 9911840-115, REV DC.
- [SDR DALA2015121807671](https://openairdocs.org/sdr/DALA2015121807671.md): Skin · damaged · Dec 3, 2015 · N914DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CREASE ON EDGE OF CUT OUT BS 1211 AND LONGERON PROJECTION 23 TO 24 RT. EDGE OF CUT OUT ON BS 1211 AND LONGERON PROJECTION 23 TO 24 RT WAS REPAIRED IAW SRM 53-05, FIG 155, OPTION 1.
- [SDR DALA2015120507393](https://openairdocs.org/sdr/DALA2015120507393.md): Door Frame · cracked · Dec 3, 2015 · N914DL · Doug MD88 · Fuselage Main, Structure
  > CRACK ON FWD INBD DOOR JAMB OF RT MLG. CHANNEL WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4 AND DWG 5930584.
- [SDR DALA2015120507391](https://openairdocs.org/sdr/DALA2015120507391.md): Duct · worn · Dec 3, 2015 · N914DL · Doug MD88 · Wing Structure
  > WEAR AT FUEL VENT DUCT, RT WING. EDGE OF CUTOUT ON Y=1211 AND LONGERON 23 TO 24 RT WAS REPAIRED IAW SRM 53-05, FIG 155, OPTION 1.
- [SDR DALA2015120307354](https://openairdocs.org/sdr/DALA2015120307354.md): Door Frame · cracked · Dec 2, 2015 · N914DL · Doug MD88 · Fuselage Main, Structure
  > CRACK ON FWD OTBD DOOR JAMB OF RT MLG, W/W, SM. FWD OTBD DOOR JAMB WAS REPLACED IAW SRM 51-30-2. DIMENTION CRACK IS 2.875".
- [SDR DALA2015120207308](https://openairdocs.org/sdr/DALA2015120207308.md): Wire Harness · broken · Dec 1, 2015 · N914DL · Doug MD88 · Electrical Power System Wiring
  > BROKEN WIRING BUNDLES ON RT AILERON BUS CONTROL CABLE 35C, REF CARD 85, ZONE 10. CONTROL CABLE SEGMENT 35C WAS REMOVED IAW AMM 20-10-17 AND WILL BE INSTALLED AND ADJUSTED UNDER CARD 2000-9000-02.
- [SDR DALA2015120107289](https://openairdocs.org/sdr/DALA2015120107289.md): Beam · cracked · Nov 30, 2015 · N914DL · Doug MD88 · Fuselage Main, Structure
  > CRACKED BEAM NR 1 AFT SIDE AT FWD SERVICE DOOR. INNER SKIN CAP PLATE, HANDLE, FWD, AFT SUPPORT, INTERCOSTALS, AND BEAM WERE REMOVED. NEW BEAM WAS DRILLED, TREATED, AND PAINTED. BEAM, INNER SKIN CAP PLATE, HANDLE, FWD, AFT SUPPORT, INTERCOSTALS WERE INSTALLE
- [SDR DALA2015120107288](https://openairdocs.org/sdr/DALA2015120107288.md): Pan · cracked · Nov 30, 2015 · N914DL · Doug MD88 · Service Doors
  > CRACKED PAN ON FWD SERVICE DOOR AFT UPPER CORNER, TREATED AND PAINTED IAW SRM 51-10-4, 51-10-3 PAR 21 AND 14 DWG REV.
- [SDR DALA2015120107287](https://openairdocs.org/sdr/DALA2015120107287.md): Pan · cracked · Nov 30, 2015 · N914DL · Doug MD88 · Service Doors
  > CRACKED PAN AT FWD SERVICE DOOR. SECTION WEB, STRAP WERE REMOVED, REPAIR PARTS WERE FABRICATED, TREATED, PAINTED, SECTION WEB, STRAP AND REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2, 51-30-4, 51-30-5, 52-03D, FIG 3, 51-10-3, PAR 21 AND 14. CRACK. 0.180".
- [SDR DALA2015112807241](https://openairdocs.org/sdr/DALA2015112807241.md): Skin · cracked · Nov 28, 2015 · N914DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN BS 1474 LONGERON 15L,. SKIN WAS REPARED IAW SRM 53-01, FIG 4, 51-30-2, AND 51-10-3, PAR 14 AND 21.
- [SDR DALA14001950914](https://openairdocs.org/sdr/DALA14001950914.md): Frame · cracked · Jan 9, 2014 · N914DL · Doug MD88 · Fuselage Main, Frame
  > FRAME WEB CRACKED AT BS 1485, LBL 20. REPAIRED IAW PRI 522045-14, REV 0. COMPLIED WITH ER/A 522045-14, REV O.
- [SDR DALA14001390914](https://openairdocs.org/sdr/DALA14001390914.md): Skin · cracked · Jan 7, 2014 · N914DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT BS 1418. REPAIRED IAW ER/A 522025-14, REV. ORIG.
- [SDR DALA2016102807865](https://openairdocs.org/sdr/DALA2016102807865.md): Door Frame · corroded · Jan 6, 2014 · N914DL · Doug MD88 · Fuselage Main, Structure
  > MID CARGO DOOR OPENING LOWER FRAME CORRODED. REPAIR IAW SRM 53-05 FIG 123.
- [SDR DALA1248140914](https://openairdocs.org/sdr/DALA1248140914.md): Wire · loose · Sep 9, 2012 · N914DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT SEAT 32 WAS INOPERATIVE. MAINTENANCE FOUND A LOOSE NUT AND WIRE ON THE TERMINAL STRIP. THE NUT WAS REPLACED AND THE WIRE WAS SECURED. THE SYSTEM RETURNED TO NORMAL OPERATIO
- [SDR DALA1247180914](https://openairdocs.org/sdr/DALA1247180914.md): Skin · cracked · Aug 26, 2012 · N914DL · Doug MD88 · Fuselage Main, Plate/Skin
  > INDICATION OF CRACK AT FASTENER HOLE THRU SKIN BS 1416 INBOARD OF L2R. REPAIRED PER ERA 505959-14 ORIG.
- [SDR DALA1247170914](https://openairdocs.org/sdr/DALA1247170914.md): Frame · corroded · Aug 26, 2012 · N914DL · Doug MD88 · Fuselage Main, Frame
  > AFT CARGO FRAME BS 1117 ANGLE CORRODED L29L TO L29R. REPAIRED PER ERA 505970-14 REV ORIG.
- [SDR DALA1247130914](https://openairdocs.org/sdr/DALA1247130914.md): Frame · corroded · Aug 25, 2012 · N914DL · Doug MD88 · Fuselage Main, Frame
  > AFT ACCESORY COMPARTMENT BS 1406 BETWEEN LONG 25 LT AND AFT ENTRANCE STAIRWAY DOOR CUTOUT SUPPORT CHANNEL WITH CORROSION. REPLACED FRAME IAW MD-88 SRM 51-30-2.
- [SDR DALA1246990914](https://openairdocs.org/sdr/DALA1246990914.md): Skin · corroded · Aug 23, 2012 · N914DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LOWER BILGE SKIN BUTT SPLICE STRAP HAS CORROSION AT BS 1184 FROM L-26L TO L-29R. REPAIRED PER ER/A 505963-14REV ORIG.
- [SDR DALA1246980914](https://openairdocs.org/sdr/DALA1246980914.md): Skin · gouged · Aug 23, 2012 · N914DL · Doug MD88 · Cargo/Baggage Doors
  > FWD CARGO DOOR INNER SKIN GOUGED AT AFT LOWER END ABOVE LATCH. REPAIRED PER ER/A 505965-14 REV ORIG.
- [SDR DALA1246970914](https://openairdocs.org/sdr/DALA1246970914.md): Torque Box · corroded · Aug 23, 2012 · N914DL · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT CARGO TORQUE BOX UPPER WEB FS 1146 L30-L26R UPPER SURFACE CORRODED, ER/A 493766-14MA REV ORIG.
- [SDR DALA1246960914](https://openairdocs.org/sdr/DALA1246960914.md): Strap · corroded · Aug 23, 2012 · N914DL · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT CARGO TORQUE BOX LWR INTERNAL BEAM AT L 29R LWR H2 FLANGE HAS A CORRODED STRAP FS 1167-1177. REPAIRED PER ER/A505658-14 REV A.
- [SDR DALA1246010914](https://openairdocs.org/sdr/DALA1246010914.md): Seat Track · corroded · Aug 15, 2012 · N914DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK STA 798 TO 1032 LBL HAS CORROSION AND GOUGES THROUGHOUT. REPAIRED IAW MD-88 SRM 51-30-5.
- [SDR DALA1246000914](https://openairdocs.org/sdr/DALA1246000914.md): Cargo Track · corroded · Aug 15, 2012 · N914DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO LEFT TIE DOWN TRACK STA 1007 TO 1221 CORRODED. REPAIRED IAW MD-88 SRM 51-30-2.
- [SDR DALA1245990914](https://openairdocs.org/sdr/DALA1245990914.md): Floorbeam · corroded · Aug 15, 2012 · N914DL · Doug MD88 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM STA 1309 HAS CORROSION AND ELONGATED FASTENER HOLES AT LBL 18 AND RBL 18. REPAIRED IAW MD-88 SRM 51-70-5.
- [SDR DALA1245980914](https://openairdocs.org/sdr/DALA1245980914.md): Panel · corroded · Aug 15, 2012 · N914DL · Doug MD88 · Wing, Plate/Skin
  > RT WING PNL 1456C LANDING AREA HAS PITTING. BLENDED AREA AND FOUND WITHIN LIMITS IAW MD-88 SRM 57-32-4.
- [SDR DALA1245970914](https://openairdocs.org/sdr/DALA1245970914.md): Support Channel · corroded · Aug 15, 2012 · N914DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON 2 GIRT BAR FITTING SUPPORT CHANNELS FOR SERVICE DOOR ON CUSP WEB STA 1142 AND 1165. REPAIRED IAW MD-88 SRM 51-30-5.
- [SDR DALA1245960914](https://openairdocs.org/sdr/DALA1245960914.md): Panel · corroded · Aug 15, 2012 · N914DL · Doug MD88 · Wing, Plate/Skin
  > RT WING FUEL PNL 1462C LANDING HAS PITTING ALL. BLENDED AREA AND FOUND WITHIN LIMITS IAW MD-88 SRM 57-32-4.
- [SDR DALA1245950914](https://openairdocs.org/sdr/DALA1245950914.md): Cusp Web · corroded · Aug 15, 2012 · N914DL · Doug MD88 · Fuselage Miscellaneous Structure
  > MAIN CABIN RT CUSP WEB STA 1174 HAS CORROSION. REPAIRED IAW MD-88 SRM 51-30-01.
- [SDR DALA1245930914](https://openairdocs.org/sdr/DALA1245930914.md): Skin · dented · Aug 15, 2012 · N914DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE STA Y157.5 BELOW LONG 21 RT EXTERNAL SKIN WITH DENT. REPAIRED IAW MD-88 SRM 53-04-3.
- [SDR DALA1245920914](https://openairdocs.org/sdr/DALA1245920914.md): Cusp Web · corroded · Aug 15, 2012 · N914DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON MAIN CABIN LT CUSP WEB BETWEEN STA 389-408. REPAIRED IAW MD-88 SRM 51-30-01.

Next page: https://openairdocs.org/deregistered/N914DL-2020-01-24/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 = 'N914DL' AND deregistration_id = 'N914DL-2020-01-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N914DL-2020-01-24/reports

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