# Service difficulty reports: N918DL, cancelled Apr 8, 2019

A list on [N918DL, cancelled Apr 8, 2019](https://openairdocs.org/deregistered/N918DL-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 · 177 reports

- [SDR DALA2018070904425](https://openairdocs.org/sdr/DALA2018070904425.md): Pin · pulled · Jul 7, 2018 · N918DL · Doug MD88 · Escape Slide
  > L1 DOOR SLIDE PINS PULLED. REPLACED L1 DOOR SLIDE PER JIC 2561-4964 A/C OK FOR SERVICE.
- [SDR DALA2018070504362](https://openairdocs.org/sdr/DALA2018070504362.md): Wire · broken · Jul 5, 2018 · N918DL · Doug MD88 · Light System Wiring
  > SEAT ROWS 35DE AND 36 DE EMERGENCY LIGHTS OUT. FOUND BROKEN WIRE AT AMPHENOL CONNECTOR UNDER SEAT TRACK. RETERMINATED AND INSTALLED CONTACT INTO CONNECTOR PER SWPM 20-31 OPS NML.
- [SDR DALA2018041102329](https://openairdocs.org/sdr/DALA2018041102329.md): Lamp · inoperative · Apr 9, 2018 · N918DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT 26ED INOPERATIVE. REPLACED THE LAMPS AND PERFORMED AN OPS CHECK IAW AMM 33-53. CHECKED OK.
- [SDR DALA2018012200329](https://openairdocs.org/sdr/DALA2018012200329.md): Door · missing · Jan 19, 2018 · N918DL · Doug MD88 · Auxiliary Power Unit (APU) Doors
  > PASSING APPROXIMATELY 25,000, FT, THE AIRCRAFT BEGAN TO VIBRATE. SPEED WAS 300 KIAS. SLOWING REDUCED, BUT DID NOT ELIMINATE THE VIBRATION. DURING DESCENT AND LEVELING AT 17K, 280 KIAS, THE VIBRATION SUDDENLY STOPPED. INSPECTED THE ACFT AND FOUND THE RT APU D
- [SDR DALA2018011700255](https://openairdocs.org/sdr/DALA2018011700255.md): Door Frame · cracked · Jan 14, 2018 · N918DL · Doug MD88 · Fuselage Main, Structure
  > CRACK IN FWD ACCESSORY COMPARTMENT DOOR JAMB. FWD ACCESSORY COMPARTMENT DOOR JAMB WAS REPAIR AS A PERMANENT REPAIR PER ER/A 564870-14 REV ORIGINAL AND ETI-88-18-001 REV 2.
- [SDR DALA2018011000171](https://openairdocs.org/sdr/DALA2018011000171.md): Frame · cracked · Jan 9, 2018 · N918DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME ON STA Y= 1510 CANT AT 3 AND 5 HRS POSITION, AFT ACCESSORIES COMPARTMENT. FRAME ON STA Y=1510 CANT WAS REPLACED PER SRM 51-30-2.
- [SDR DALA2018010700113](https://openairdocs.org/sdr/DALA2018010700113.md): Angle · cracked · Jan 6, 2018 · N918DL · Doug MD88 · Service Doors
  > CRACKED ANGLE AT THE R1 DOOR INSTERNAL STRUCTURE, A NEW ANGLE WAS FABRICATED IAW DWG 9911579, REV L AND REPLACED IAW SRM 51-30-4, 51-30-5.
- [SDR DALA2017101107436](https://openairdocs.org/sdr/DALA2017101107436.md): Cover · broken · Oct 10, 2017 · N918DL · Doug MD88 · Exterior Lighting
  > FLIGHT CREW REPORTED THE CAPTAIN GOT SHOCKED WHEN TURNING ON NOSE LANDING LIGHTS. FOUND SWITCH COVER UNDER GLARESHIELD BROKEN. REMOVED AND REPLACED COVER. ACFT OK FOR SERVICE IAW AMM 33-41.
- [SDR DALA2017071805533](https://openairdocs.org/sdr/DALA2017071805533.md): Line · leaking · Jul 17, 2017 · N918DL · Doug MD88 · Hydraulic System, Main
  > AFTER TAKE OFF, PASSENGERS AND AFT FLIGHT ATTENDANTS REPORTED AN ODOR OF HYDRAULIC FLUID AND A LIGHT A HAZE IN CABIN. THE ODOR AND HAZE DISIPATED QUICKLY. NO ABNORMAL HYD INDICATIONS IN FLIGHT DECK. PERFORMED WORKCARD 2120-2367. AFTER INSPECTION OF APU, AP
- [SDR DALA2017041703106](https://openairdocs.org/sdr/DALA2017041703106.md): Battery Pack · inoperative · Apr 16, 2017 · N918DL · Doug MD88 · Emergency Lighting
  > TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACKS IAW AMM 33-53.
- [SDR DALA2017040702853](https://openairdocs.org/sdr/DALA2017040702853.md): Tire · failed · Apr 7, 2017 · N918DL · Doug MD88 · Tire
  > AFTER TAKEOFF, AIRFRAME VIBRATION AND BURNING RUBBER ODOR FOLLOWED BY LEFT MAIN GEAR UNSAFE INDICATION WITH GEAR STILL EXTENDED. CHECKED LANDING GEAR VISUALLY AND NOW HAVE 3 GREEN DOWN AND LOCKED GEAR SAFE LIGHTS. FOUND THE NR 2 MAIN TIRE BLOWN AND RECAP SEP
- [SDR DALA2017032102262](https://openairdocs.org/sdr/DALA2017032102262.md): Cam · worn · Mar 21, 2017 · N918DL · Doug MD88 · Aerodynamic Fairings
  > FOUND BASE OF THE TAILCONE RELEASE MECHANISM CAM WORN. REPLACED TAILCONE RELEASE MECHANISM CAM BASE IAW AMM 53-53-02.
- [SDR DALA2016112809294](https://openairdocs.org/sdr/DALA2016112809294.md): Battery Pack · inoperative · Nov 27, 2016 · N918DL · Doug MD88 · Emergency Lighting
  > COCKPIT AND FWD ENTRY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK. OPS CHECKED OK IAW AMM 33-50.
- [SDR DALA2016092306798](https://openairdocs.org/sdr/DALA2016092306798.md): Power Supply · inoperative · Sep 23, 2016 · N918DL · Doug MD88 · Emergency Lighting
  > FIRST CLASS AISLE EMERGENCY LIGHTS INOPERATIVE. FOUND FIRST CLASS POWER SUPPLY BAD. REMOVED & REPLACED POWER SUPPLY IAW AMM 33-53. BATTERY NOT REPLACED. OPS CHECKED OK.
- [SDR DALA2016050403621](https://openairdocs.org/sdr/DALA2016050403621.md): Wire · shorted · May 3, 2016 · N918DL · Doug MD88 · Light System Wiring
  > THE FLIGHT CREW FOUND THAT THE EMERGENCY LIGHTING BETWEEN ROWS 32 AND 36 WERE INOPERATIVE. THE TAIL COMPARTMENT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE FOUND THE TAILCONE INTERIOR HANDLE LIGHT SHORTED AND REPAIRED THE WIRES. THE EMERGENCY LIGHTS
- [SDR DALA2016031501956](https://openairdocs.org/sdr/DALA2016031501956.md): Structure · missing · Mar 9, 2016 · N918DL · Doug MD88 · Rudder, Plate/Skin
  > FLAME SPRAY MISSING FROM CRITICAL ZONES ON RUDDER IAW SRM 55-03, PAGE 91 AND 92. RUDDER REQUIRES REPLACEMENT. RUDDER ASSY, PN 5955501-1, SN 0327 REMOVED. INSTALLED RUDDER IAW AMDS WC 2720-4421 AND 2720-7454. OK FOR SERVICE.
- [SDR DALA2015122007682](https://openairdocs.org/sdr/DALA2015122007682.md): Skin · damaged · Dec 18, 2015 · N918DL · Doug MD88 · Wing, Plate/Skin
  > SEVERAL GOUGES ON FIXED L/E BETWEEN BS XIS=83 AND XIS=73 AT RT WING. FIXED L/E BETWEEN BS XIS=83 AND XIS=73 AT RT WING WAS REPAIRED IAW ER/A 541584-14, REV ORIGINAL AND SLAT TRACK NR 3 WAS REMOVE/INSTALL IAW AMM 27-80-01; AFTER BLEND OUT, ORIGINAL THICKNESS
- [SDR DALA2015121707650](https://openairdocs.org/sdr/DALA2015121707650.md): Skin · cracked · Dec 15, 2015 · N918DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL FUSELAGE SKIN BETWEEN LONGERONS 2 - 3RT BS 1437. REPAIRED IAW ER/A 541550-14, REV ORIG SECTION I.
- [SDR DALA2015121607648](https://openairdocs.org/sdr/DALA2015121607648.md): Skin · cracked · Dec 15, 2015 · N918DL · Doug MD88 · Cargo/Baggage Doors
  > CRACKED FWD CARGO DOOR OTBD SKIN AROUND OTBD HANDLE. CRACK ON FWD CARGO DOOR OTBD SKIN AROUND OTBD HANDLE, C1 WAS REPAIRED IAW ER/A 591590-14 REV ORIGINAL.
- [SDR DALA2015121507606](https://openairdocs.org/sdr/DALA2015121507606.md): Skin · damaged · Dec 14, 2015 · N918DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKES ON FWD, AFT UPPER CORNER AT WINDOW BELT NR 59 EXTERNAL FUSELAGE SKIN. LIGHTNING STRIKES ON WINDOW BELT NR 59 EXTERNAL FUSELAGE SKIN WERE BLENDED OUT AND ARE WITHIN LIMITS IAW SRM 53-05, FIG 111 AND ER/A 541585-14, REV.A.
- [SDR DALA2015121507605](https://openairdocs.org/sdr/DALA2015121507605.md): Skin · damaged · Dec 14, 2015 · N918DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON RT WINDOW BELT BETWEEN BS 788 - 807 AT FWD AREA. LIGHTNING STRIKE ON RT WINDOW BELT WAS BLENDED OUT, POLISHED, MEASURED AND TREATED IAW SRM 53-05, FIG 111 AND ER/A 541586-14 REV ORIGINAL.
- [SDR DALA2015121507604](https://openairdocs.org/sdr/DALA2015121507604.md): Door Frame · cracked · Dec 14, 2015 · N918DL · Doug MD88 · Fuselage Main, Structure
  > CRACKED TEE ON AFT DOOR JAMB AT LT MLG. TEE ON AFT DOOR JAMB AT LT MLG WAS REPAIRED IAW SRM 53-05, FIG 141.
- [SDR DALA2015121407584](https://openairdocs.org/sdr/DALA2015121407584.md): Longeron · cracked · Dec 13, 2015 · N918DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 4L AT BS 200. THE LONGERON WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND 53-02, FIG 18.
- [SDR DALA2015121407582](https://openairdocs.org/sdr/DALA2015121407582.md): Longeron · corroded · Dec 13, 2015 · N918DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > SEVERAL CORROSION POINTS ON LONGERON 30 FROM BS 1287 - 1295. THE LONGERON WAS REPLACED IAW SRM 53-02, FIG 18.
- [SDR DALA2015121307581](https://openairdocs.org/sdr/DALA2015121307581.md): Skin · worn · Dec 13, 2015 · N918DL · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > WEAR ON RT SKIN BETWEEN BS ZFS 180 AND ZFS 165 AT VERTICAL STABILIZER. RT SKIN WAS REPLACED DUE EXCESSIVE WEAR IAW SRM 55-32-0, FIG 3 AND DWG 5936143, REV.
- [SDR DALA2015121407586](https://openairdocs.org/sdr/DALA2015121407586.md): Frame · corroded · Dec 12, 2015 · N918DL · Doug MD88 · Fuselage Main, Frame
  > SEVERAL CORROSION POINTS ON FRAME CLIPS BS 1288 FROM LONGERON 28L - 28R. FRAME CLIP AND SPLICES WERE REPLACED BY EXCESS COROOSION IAW SRM 53-03, FIG 3.
- [SDR DALA2015121407585](https://openairdocs.org/sdr/DALA2015121407585.md): Skin · cracked · Dec 12, 2015 · N918DL · Doug MD88 · Leading Edge Devices
  > CRACK ON RT SLAT PANEL NR 1 XIS=133 APPROXIMATELY CRACK WAS FOUND OUT OF LIMITS 2.750" IN REF ERA 519116-14MA, REV ORIGINAL THEREFORE SLAT PANEL NR 1 AT RT WING WAS REMOVED AND WILL BE INSTALLED AND ADJUSTED UNDER JIC CARD 2700-4224-RH-01, JOB 000-0011.
- [SDR DALA2015121307580](https://openairdocs.org/sdr/DALA2015121307580.md): Rib · cracked · Dec 12, 2015 · N918DL · Doug MD88 · Wing, Rib/Bulkhead
  > CRACKED CLIP AND RIB L/E AREA BS XRS=414.100 APPROXIMATELY LT WING. RIB AND CLIP WERE REPLACED IAW DWG 9919329-7, REV T AND SRM 51-30-2 AND 51-30-5.
- [SDR DALA2015121207577](https://openairdocs.org/sdr/DALA2015121207577.md): Web · cracked · Dec 11, 2015 · N918DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK ON MEMBRANE BS 200, X=-22, Z=0 AT CEILING OF ELECTRONIC EQUIPMENT COMPARTMENT. MEMBRANE WAS REPAIRED IAW SRM 51-30-2, SRM 51-70-4, SRM 51-10-3 PAR 14, 21, SRM 51-30-8.
- [SDR DALA2015121007536](https://openairdocs.org/sdr/DALA2015121007536.md): Skin · damaged · Dec 10, 2015 · N918DL · Doug MD88 · Ailerons
  > EXPOSED COMPOUND MATERIAL ON RT AILERON ON TABS. REPAIRED IAW SRM 51-70-1D, PAR 3.
- [SDR DALA2015121007490](https://openairdocs.org/sdr/DALA2015121007490.md): Spacer · corroded · Dec 9, 2015 · N918DL · Doug MD88 · Fuselage Main, Structure
  > SEVERAL CORROSION POINTS ON AFTER CARGO COMPARTMENT LOWER DOOR JAMB SPACER. SPACER WAS REPLACED IAW SRM 53-05, FIG 123, 51-30-5, 51-10-3 PAR 14, 21 AND 38.
- [SDR DALA2015120907465](https://openairdocs.org/sdr/DALA2015120907465.md): Structure · cracked · Dec 9, 2015 · N918DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED RADIO RACK EXHAUST BS 256-275. RADIO RACK EXHAUST BS 256-275 WAS REPAIRED IAW ER/A 464964, 14 MAR, REV C.
- [SDR DALA2015121007489](https://openairdocs.org/sdr/DALA2015121007489.md): Rib · cracked · Dec 8, 2015 · N918DL · Doug MD88 · Wing, Rib/Bulkhead
  > CRACK ON RIB OF RT WING FIXED L/E STA XRS= 418 APPROXIMATELY RIB WAS REPLACED IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-4, SRN 51-10-3, PAR14 AND 21.
- [SDR DALA2015062904051](https://openairdocs.org/sdr/DALA2015062904051.md): Lanyard · frayed · Jun 28, 2015 · N918DL · Doug MD88 · Escape Slide
  > KEVLAR CABLE IN TAIL CONE FRAYED, RII: N ENTR 448527 W, R & R KEVLAR TAILCONE SLIDE DEPLOYMENT LANYARD IAW AMM REF 25-62-01.
- [SDR DALA2015060703610](https://openairdocs.org/sdr/DALA2015060703610.md): Access Panel · corroded · Jun 6, 2015 · N918DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON LT MAIN FUEL TANK ACCESS PLATE NR 1361C COUNTERSINK HOLES AND SETTLEMENT AREA. CORROSION ON COUNTERSINKS AND SETTLEMENT AREA WAS REMOVED, COUNTERSINKS WERE MEASURED AND MAXIMUM DIAMETER ALLOWABLE IS.532" AND WAS FOUND 3 COUNTERSINKS OUT OF LIMIT
- [SDR DALA2014081204441](https://openairdocs.org/sdr/DALA2014081204441.md): Battery Pack · inoperative · Aug 8, 2014 · N918DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT ROWS 22-25 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. OPS CHECKED GOOD.
- [SDR DALA2014063003817](https://openairdocs.org/sdr/DALA2014063003817.md): Battery Pack · inoperative · Jun 30, 2014 · N918DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.
- [SDR DALA2014061803673](https://openairdocs.org/sdr/DALA2014061803673.md): Battery Pack · inoperative · Jun 15, 2014 · N918DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THE OVERWING EXIT LIGHTS WERE INOPERATIVE ON THE RT AND LT AT ROW 25. MAINTENANCE REPLACED THE BATTERIES FOR THE OVERWING EXIT LIGHTS AND THE LIGHTS BECAME OPERATIONAL.
- [SDR DALA14019750918](https://openairdocs.org/sdr/DALA14019750918.md): Fuse · failed · Mar 30, 2014 · N918DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 31-36 IN CABIN AND CATWALK IN TAIL, WERE INOPERATIVE. MAINTENANCE REPLACED THE FAILED FUSE AT THE POWER SUPPLY AND THE BULBS IN TAILCONE HANDLE. THE LIGHTS RETURNED TO AN OPS CONDITION.
- [SDR DALA14000700918](https://openairdocs.org/sdr/DALA14000700918.md): Battery Pack · inoperative · Jan 4, 2014 · N918DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING IN THE COCKPIT AND AT DOORS L1 & R1 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND OPS CHECKED GOOD.
- [SDR DALA13072590918](https://openairdocs.org/sdr/DALA13072590918.md): Slide · misinstalled · Dec 31, 2013 · N918DL · Doug MD88 · Escape Slide
  > INSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE WAS IMPROPERLY INSTALLED. THIS CONFIGURATION OF THE SLIDE WOULD HAVE PREVENTED PROPER DEPLOYMENT OF THE ESCAPE SYSTEM AND IS NOT IN COMPLIANCE WITH 14 CFR, PART 121.703. THE TAILCONE SLIDE
- [SDR DALA13072490918](https://openairdocs.org/sdr/DALA13072490918.md): Clamp · obstructed · Dec 28, 2013 · N918DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE TAILCONE LOCKING CABLE CLAMP DOES NOT CLEAR THE CONDUIT BY.5. CLAMPS REPLACED AND THE CONDUIT ADJUSTED IAW MM.
- [SDR DALA13072480918](https://openairdocs.org/sdr/DALA13072480918.md): Fitting · worn · Dec 28, 2013 · N918DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE TAILCONE EXTERNAL RELEASE HANDLE FITTINGS WERE WORN. FITTINGS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.
- [SDR DALA13072470918](https://openairdocs.org/sdr/DALA13072470918.md): Cable · frayed · Dec 28, 2013 · N918DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE RT RELEASE LATCH CABLE FOR THE TAILCONE WAS FRAYED BEYOND ALLOWABLE LIMITS. CABLE REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.
- [SDR DALA13042570918](https://openairdocs.org/sdr/DALA13042570918.md): Ground Wire · loose · Aug 30, 2013 · N918DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MX FOUND THAT THE CEILING MOUNTED EMERGENCY EXIT LIGHTS AT SEAT ROWS 16, 18, AND 20 WERE TOO DIM TO PROVIDE ESCAPE GUIDANCE. MX FOUND THE POWER SUPPLY GROUND TERMINAL LOOSE AND RE-SECURED IT. THE LIGHTS RETURNED TO AN OPS CONDITION.
- [SDR DALA13039450918](https://openairdocs.org/sdr/DALA13039450918.md): Cabin Pressure · low · Aug 13, 2013 · N918DL · Doug MD88 · Cabin Pressure Control System
  > FLIGHT CREW DIVERTED THE ACFT, FOLLOWING THE LOSS OF CONTROL OF CABIN PRESSURIZATION AT FL330. PASSENGER O2 MASKS DID NOT DEPLOY BUT ACFT WAS REQUIRED TO DESCEND TO 10,000 FT AND DECLARED AN EMERGENCY. MX FOUND BOTH PACKS SHUTTING OFF AT CRUISE POWER SO BOTH
- [SDR DALA13016650918](https://openairdocs.org/sdr/DALA13016650918.md): Cable · broken · Apr 13, 2013 · N918DL · Doug MD88 · Aerodynamic Fairings
  > MX DISCOVERED THAT THE TAILCONE RETRACT CABLE WAS BROKEN AT THE TURN-BUCKLE. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.
- [SDR DALA13000590918](https://openairdocs.org/sdr/DALA13000590918.md): Battery Pack · inoperative · Jan 9, 2013 · N918DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE COCKPIT AND AT DOORS L1 & R1 WERE INOPERATIVE. MX REPLACED THE BATTERIES. OPS CHECKED GOOD.
- [SDR DALA12015390918](https://openairdocs.org/sdr/DALA12015390918.md): Battery · inoperative · Dec 6, 2012 · N918DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT MULTIPLE OVERHEAD EMERGENCY PATHWAY LIGHTING WAS INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER PACKS B5-100 & B5-102, AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA12013910918](https://openairdocs.org/sdr/DALA12013910918.md): Battery · failed · Nov 26, 2012 · N918DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE COCKPIT HAD FAILED. MX REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Next page: https://openairdocs.org/deregistered/N918DL-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 = 'N918DL' AND deregistration_id = 'N918DL-2019-04-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N918DL-2019-04-08/reports

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