# Service difficulty reports: N995DL, cancelled Oct 26, 2022

A list on [N995DL, cancelled Oct 26, 2022](https://openairdocs.org/deregistered/N995DL-2022-10-26.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 5 · 225 reports

- [SDR DALA2020052202417](https://openairdocs.org/sdr/DALA2020052202417.md): Panel · out of adjust · May 22, 2020 · N995DL · Doug MD88 · Emergency Exits
  > THE SPRING RETRACT DOOR PANEL RIGHT SIDE ON THE AFT ESCAPE RAMP IS INOPERATIVE. MAINTENANCE ADJUSTED THE DOOR PANEL IAW MD-88 AMM 52-00. OPERATION NOW CHECKS GOOD AT THIS TIME. (LP #6468636)
- [SDR DALA2020042002277](https://openairdocs.org/sdr/DALA2020042002277.md): Battery · discharged · Apr 20, 2020 · N995DL · Doug MD88 · Emergency Lighting
  > THE CEILING EMERGENCY LIGHTS FROM SEAT ROW 22 TO 26 ARE INOPERABLE. MAINTENANCE REPLACED THE BATTERIES ON THE EMERGENCY LIGHT CHARGER ASSEMBLY PER MD88 AMM 33-53, AT SEAT LOCATION 24ED. OPERATIONAL CHECK WAS GOOD. (LP #7183164)
- [SDR DALA2019111506705](https://openairdocs.org/sdr/DALA2019111506705.md): Battery Pack · inoperative · Nov 15, 2019 · N995DL · Doug MD88 · Emergency Lighting
  > DURING SVC FOUND FWD CABIN EMERGENCY LIGHT INOP. T/S PER MD88 AMM:33-50 AND ROBBED EMERGENCY BATTERY FROM A/C 963. OPS CHECK OK A/C OK FOR SVC. (LP6658249)
- [SDR DALA2019082104890](https://openairdocs.org/sdr/DALA2019082104890.md): Fuse · failed · Aug 21, 2019 · N995DL · Doug MD88 · Light System Wiring
  > EXIT ROW LIGHTS OUT FROM ROW 31 AFT. TROUBLE SHOOT TO BAD FUSE IN POWER PACK. REPLACED FUSE IAW CMM 33-21-70. OPS CHECK GOOD. (LP5158525)
- [SDR DALA2019021871017](https://openairdocs.org/sdr/DALA2019021871017.md): Duct · blown · Feb 16, 2019 · N995DL · Doug MD88 · Ice/Rain Protection System
  > RIGHT ENGINE FIRE LIGHT BELLS PASSING APPROX. 800 FT ON TAKEOFF. NO ENGINE INDICATIONS OF FIRE OR DAMAGE. FIRE LIGHT WENT OUT BEFORE BLOWING FIRE BOTTLE OR SHUT DOWN ENGINE. LANDED WITH RIGHT ENGINE AT IDLE PER QRH. FOUND ANTI ICE DUCT BLOWN. NO DAMAGE TO CAS
- [SDR DALA2019012500515](https://openairdocs.org/sdr/DALA2019012500515.md): Slide · failed · Jan 25, 2019 · N995DL · Doug MD88 · Escape Slide
  > RT SLIDE FAIL DEPLOYMENT TEST. FORECAST NR 88-0526-8-0406, MPN. D29982, S/N 0883, DATE, OCT 1986. RT SLIDE REMOVED & REPLACED REF. STK# 97-2561-9-0001, W/C 2561-4964. (LP0917957)
- [SDR DALA2019011300217](https://openairdocs.org/sdr/DALA2019011300217.md): Battery · discharged · Jan 13, 2019 · N995DL · Doug MD88 · Emergency Lighting
  > FWD OVHD EM LIGHTS IN-OP. REPLACED BATTERIES IN EM LT PWR SUPPLY 5-23 IAW AMM 33-55 CKS GOOD. (LP4753077)
- [SDR DALA2018121807253](https://openairdocs.org/sdr/DALA2018121807253.md): Unknown · odor · Dec 17, 2018 · N995DL · Doug MD88 · Air Distribution System
  > BOTH PILOTS SMRLT RUBBER ODER WHEN DEPARTING BHM ON T/O ODER DISSIPATED BEFORE REACHING 10000 FT. REF NO GO ODI LOG 0867036. OPENED SADDLE DUCTS CAPS ON NBR 1 AND NBR 2 ENGINES FOR BOROSCOPE. BOROSCOPE INSPECTED NBR 1 & 2 ENGINE SADDLE DUCTS. NO OIL RESIDUE FO
- [SDR DALA2018121707224](https://openairdocs.org/sdr/DALA2018121707224.md): Unknown · odor · Dec 16, 2018 · N995DL · Doug MD88 · Air Distribution System
  > DURING TO AND INITIAL CLIMB, THE FA AT THE TAILCONE SMELLED AN ODOR. THE RUBBERY ODOR SMELL DISSIPATED 5 MINUTES AFTER TO. IT WAS A NORMAL PWR TO. PACKS ON, ENG ANTI ICE OFF, AND APU OFF. THERE WAS NO SMOKE, ONLY RUBBERY, CHEMICAL ODOR FROM EXIT ROWS AFT TO TH
- [SDR DALA2018120607058](https://openairdocs.org/sdr/DALA2018120607058.md): Rib · cracked · Dec 5, 2018 · N995DL · Doug MD88 · Elevator, Spar/Rib
  > UPPER RIB FORMER IS CRACKED OUT OF RIVET HOLE. ( P/N 9936146-13) UPPER ROW, THIRD HOLE RT FROM CENTER. REPAIRED PER 573506-14 REV O. (LP0852904)
- [SDR DALA2018082905334](https://openairdocs.org/sdr/DALA2018082905334.md): Doubler · worn · Aug 28, 2018 · N995DL · Doug MD88 · Passenger/Crew Doors
  > WORN REPAIR DOUBLER, FWD, UPPER CORNER AT THE L1 DOOR. THE REPAIR DOUBLER WAS REPLACED IAW SRM 52-05, FIG 18A.
- [SDR DALA2018082805308](https://openairdocs.org/sdr/DALA2018082805308.md): Floor Panel · delaminated · Aug 27, 2018 · N995DL · Doug MD88 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 826D IN THE PAX CABIN. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW AMM 53-20-01-201.
- [SDR DALA2018082765254](https://openairdocs.org/sdr/DALA2018082765254.md): Skin · worn · Aug 25, 2018 · N995DL · Doug MD88 · Spoilers
  > WEAR ON THE AFT UPPER SURFACE OF THE RT WING GROUND SPOILER. REPAIRED IAW SRM 51-70-1B, P.11.
- [SDR DALA2018082765248](https://openairdocs.org/sdr/DALA2018082765248.md): Panel · damaged · Aug 25, 2018 · N995DL · Doug MD88 · Fuselage Main, Structure
  > LAVATORY SERVICE PANEL DAMAGED. REPAIRED IAW ER/A 536216-14, REV A, SECT III, AND ETI-88-18-068, REV 2.
- [SDR DALA2018082875314](https://openairdocs.org/sdr/DALA2018082875314.md): Skin · corroded · Aug 24, 2018 · N995DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, AFT LAVATORY SERVICE DOOR CUTOUT BS 1307, LONGERON 22L WAS CORRODED. ACCOMPLISH ERA 536216-14 REV A SECTION IV.
- [SDR DALA2018082705252](https://openairdocs.org/sdr/DALA2018082705252.md): Slide · damaged · Aug 23, 2018 · N995DL · Doug MD88 · Escape Slide
  > BROCKEN SAFETY THREADS AT L1 SLIDE. THE SLIDE WAS REPLACED IAW AMM 25-62-00-201.
- [SDR DALA2018042902888](https://openairdocs.org/sdr/DALA2018042902888.md): Light · inoperative · Apr 28, 2018 · N995DL · Doug MD88 · Emergency Lighting
  > SEAT 14ED EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY IAW AMM 33-53. OPS CHECKED GOOD.
- [SDR DALA2017122608875](https://openairdocs.org/sdr/DALA2017122608875.md): Connector · disconnected · Dec 22, 2017 · N995DL · Doug MD88 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS INOPERATIVE. FOUND THE RT OVERWING EMERGENCY LIGHT NOT CONNECTED. RECONNECTED THE CONNECTOR. ALL LIGHTS CHECKED GOOD.
- [SDR DALA2017112008219](https://openairdocs.org/sdr/DALA2017112008219.md): Battery Pack · inoperative · Nov 17, 2017 · N995DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE, ROW 27 AFT TO REAR DOOR. REPLACED THE BATTERIES IN PAX OVERHEAD BIN 33. OPS CHECKED OK.
- [SDR DALA2017110307924](https://openairdocs.org/sdr/DALA2017110307924.md): Door Frame · cracked · Nov 2, 2017 · N995DL · Doug MD88 · Fuselage Main, Structure
  > DURING A CHECK, FOUND THE RT WHEEL WELL FWD DOOR FRAME CRACKED. VISUALLY INSPECTED AND STOP DRILLED IAW ENGINEERING. REMOVED & REPLACED FWD RT WHEEL WELL DOOR FRAME SECTION IAW DRAWING.
- [SDR DALA2017071405470](https://openairdocs.org/sdr/DALA2017071405470.md): Wheel · undertorqued · Jul 13, 2017 · N995DL · Doug MD88 · Wheel/Ski/Float
  > AFTER LANDING & NORMAL BRAKING, DURING LANDING BOTH BRAKES EXHIBITED SIGNIFICANT SHUDDER DURING STOP ATTEMPTS. AIRPLANE HAD TROUBLE STOPPING DUE TO THE BRAKE CHATTER. BRAKE TEMP AROUND 201 DEG. THIS WAS MORE THAN THE NORMAL BRAKE CHATTER. IT WAS VERY VIOLE
- [SDR DALA2017071005346](https://openairdocs.org/sdr/DALA2017071005346.md): Wire Harness · defective · Jul 9, 2017 · N995DL · Doug MD88 · Light System Wiring
  > ON SERVICE CHECK FOUND SEAT 35C EMERGENCY SEAT LIGHT INOP. REPLACED EMERGENCY LIGHT SEAT HARNESS AT 35C. OPERATION IS NOW NORMAL. OK FOR SERVICE.
- [SDR DALA2017040602773](https://openairdocs.org/sdr/DALA2017040602773.md): Lamp · inoperative · Apr 6, 2017 · N995DL · Doug MD88 · Emergency Lighting
  > ONE RED EMERGENCY LIGHT ON SEAT 24D INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-53. CHECKED GOOD.
- [SDR DALA2016072605568](https://openairdocs.org/sdr/DALA2016072605568.md): Hand Rail · misinstalled · Jul 25, 2016 · N995DL · Doug MD88 · Emergency Exits
  > FUNCTIONAL FAIL ON AFT EMERGENCY DOOR HANDLE. EMERGENCY VENTRAL DOOR HANDLE ASSEMBLIES REMOVED AND INSTALLED CORRECTLY AND FAILURE WAS CORRECTED IAW 52-63-1.
- [SDR DALA2016072605566](https://openairdocs.org/sdr/DALA2016072605566.md): Hinge · worn · Jul 25, 2016 · N995DL · Doug MD88 · Fuselage, Door Hinge
  > FREE PLAY ON FWD & AFT HINGE AT FWD CARGO DOOR. HINGES WERE REMOVED REPAIRED AND INSTALLED IAW ER/A 497387-14 REV B AND FREE PLAY WAS CORRECTED INSTALLATION OF HINGES WAS PERFORMED IAW AMM 52-31-02.
- [SDR DALA2016072605565](https://openairdocs.org/sdr/DALA2016072605565.md): Hinge · worn · Jul 25, 2016 · N995DL · Doug MD88 · Fuselage, Door Hinge
  > FREE PLAY ON FWD & AFT HINGE AT MID CARGO DOOR. FWD. AFT HINGES REMOVED, REPAIRED AND INSTALLED IAW ERA 497387-14MA REV B AND AMM 52-31-02.
- [SDR DALA2016072505535](https://openairdocs.org/sdr/DALA2016072505535.md): Rib · cracked · Jul 25, 2016 · N995DL · Doug MD88 · Wing, Rib/Bulkhead
  > CRACKED RT WING LEADING EDGE RIB XRS 276. RIB WAS REPLACED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.
- [SDR DALA2016072505537](https://openairdocs.org/sdr/DALA2016072505537.md): Angle · cracked · Jul 24, 2016 · N995DL · Doug MD88 · Wing Miscellaneous Structure
  > CRACKED FORMER ANGLES ON FIXED LEADING EDGE COMPARTMENT XOS 354, XOS 361, XOS 251, XOS 257 AND XOS 470 AT LT WING. FORMER ANGLES WERE REPLACED IAW SRM 51-30-2/51-30-5/51-10-4/51-10-3 AND DRAWING 9937589 REV. D, 9919329 REV.T.
- [SDR DALA2016072505536](https://openairdocs.org/sdr/DALA2016072505536.md): Support Fitting · corroded · Jul 24, 2016 · N995DL · Doug MD88 · Fuselage Main, Attach Fittings
  > CORROSION BUSHING BORE AND SPOT FACE AT RIGHT GEAR RETRACT ACTUATOR SUPPORT FITTING. THE REPAIR WAS ACCOMPLISHED IAW ETI-88-16-248 REV 4 AND ER/A 547834-14AD REV ORIG.
- [SDR DALA2016072505534](https://openairdocs.org/sdr/DALA2016072505534.md): Stringer · cracked · Jul 24, 2016 · N995DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK OF 0.250 WAS FOUND ON STRINGER 17R XCW 10, INSIDE CENTER TANK. STRINGER 17 WAS REPAIRED PER ER/A 547822-14 REV. ORIG. 547823-14 REV. ORIG.
- [SDR DALA2016072505533](https://openairdocs.org/sdr/DALA2016072505533.md): Stringer · cracked · Jul 24, 2016 · N995DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK OF 0.312 "WAS FOUND ON STRINGER 17L XCW=12, INSIDE CENTER TANK. STRINGER WAS REPAIRED PER ER/A 547822-14 REV. ORIG. 547823-14 REV. ORIG.
- [SDR DALA2016072505532](https://openairdocs.org/sdr/DALA2016072505532.md): Support Fitting · corroded · Jul 24, 2016 · N995DL · Doug MD88 · Fuselage Main, Attach Fittings
  > CORROSION ON BUSHING BORE OF BEARING AT RIGHT GEAR RETRACT ACTUATOR SUPPORT FITTING. THE REPAIR WAS ACCOMPLISHED IAW ETI-88-16-248 REV 4 AND ER/A 547834-14AD REV ORIG.
- [SDR DALA2016072505531](https://openairdocs.org/sdr/DALA2016072505531.md): Support Fitting · corroded · Jul 24, 2016 · N995DL · Doug MD88 · Fuselage Main, Attach Fittings
  > CORROSION ON BUSHING BORE AND SPOT FACE AT LEFT GEAR, RETRACT ACTUATOR SUPPORT FITTING. THE REPAIR WAS ACCOMPLISHED IAW ETI-88-16-248 REV 4 AND ER/A 547834-14AD REV ORIG.
- [SDR DALA2016072505529](https://openairdocs.org/sdr/DALA2016072505529.md): Pan · cracked · Jul 24, 2016 · N995DL · Doug MD88 · Cargo/Baggage Doors
  > CRACKED PLATE ON AFT EDGE AND BEAM 1 BEHIND STOP NR 1 AT AFT CARGO DOOR. INNER PAN WAS REPAIRED IAW ETI-88-16-254 REV:2 AND ERA 547852-14 REV. ORIGINAL.
- [SDR DALA2016072505528](https://openairdocs.org/sdr/DALA2016072505528.md): Pan · worn · Jul 24, 2016 · N995DL · Doug MD88 · Cargo/Baggage Doors
  > WORN PLATE AND PAN ON AFT EDGE LWR CORNER OUTER SURFACE AT FWD CARGO DOOR. AFT EDGE LWR CORNER WAS REPAIRED I.A.W. DC-9/MD-80 ETI- 88-16-253 REV. 2 AND ERA:547843-14 REV: ORIGINAL.
- [SDR DALA2016072505539](https://openairdocs.org/sdr/DALA2016072505539.md): Skin · cracked · Jul 23, 2016 · N995DL · Doug MD88 · Wing, Plate/Skin
  > DURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND ON LOWER SKIN BETWEEN XRS=163 TO 168 REAR SPAR AT RT WING. REPAIRED IAW ER/A 547818-14 REV. ORIGINAL.
- [SDR DALA2016072505538](https://openairdocs.org/sdr/DALA2016072505538.md): Skin · cracked · Jul 23, 2016 · N995DL · Doug MD88 · Wing, Plate/Skin
  > DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON LOWER SKIN BETWEEN XRS=163 TO 168 REAR SPAR AT LT WING. REPAIRED IAW ER/A 547818-14 REV.ORIGINAL.
- [SDR DALA2016072405524](https://openairdocs.org/sdr/DALA2016072405524.md): Support Fitting · corroded · Jul 23, 2016 · N995DL · Doug MD88 · Fuselage Main, Attach Fittings
  > CORROSION ON BUSHING BORE OF BEARING AT LEFT GEAR RETRACT ACTUATOR SUPPORT FITTING. REPAIR ACCOMPLISHED IAW ETI-88-16-248 REV. 4 AND ER/A 547834-14AD REV ORIG.
- [SDR DALA2016072405523](https://openairdocs.org/sdr/DALA2016072405523.md): Frame · cracked · Jul 23, 2016 · N995DL · Doug MD88 · Fuselage Main, Frame
  > CRACK VISIBLE ON FRAME BS 1510 AFT SIDE NEXT TO UPPER LEFT TAIL CONE LATCH HOOK. REPLACED THE FRAME IAW SRM 51-30-1, 51-30-2, 51-10-4, 51-10-3 AND DWG 9911843 REV AC.
- [SDR DALA2016072405522](https://openairdocs.org/sdr/DALA2016072405522.md): Skin · cracked · Jul 23, 2016 · N995DL · Doug MD88 · Fuselage Main, Plate/Skin
  > TWO CRACKS IN FUSELAGE SKIN BS 1463 -1446. REPAIRED IAW ETI 88-16-255 REV 2 ER/A 547855-14 REV ORG.
- [SDR DALA2016072205482](https://openairdocs.org/sdr/DALA2016072205482.md): Angle · corroded · Jul 21, 2016 · N995DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORRODED ANGLE BS 1350 X 17LT TO 17RT Z 0, LOWER VENTRAL DOOR JAMB ANGLE. LOWER VENTRAL DOOR JAMB WAS REPAIRED IAW SRM 53-05 FIG.34 AND ER/A 547838-14 REV.1.
- [SDR DALA2016072105451](https://openairdocs.org/sdr/DALA2016072105451.md): Intercostal · cracked · Jul 20, 2016 · N995DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL ON BS 1485 AND BTW 1 AND 2 HRS POSITION AT AFT ACCESSORY COMPARTMENT. INTERCOSTAL WAS REPAIRED IAW SRM 53-01, 51-30-2, 51-30-5, AND DWG. 9911875.
- [SDR DALA2016072005443](https://openairdocs.org/sdr/DALA2016072005443.md): Frame · cracked · Jul 19, 2016 · N995DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME BS 1510. FRAME WAS REPLACED IAW DWG 9911843 AND SRM 51-30-2.
- [SDR DALA2016072005442](https://openairdocs.org/sdr/DALA2016072005442.md): Cusp Web · cracked · Jul 19, 2016 · N995DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB BS 459 - 479 AND X -54 TO X -60. REPAIRED IAW SRM 53-05 FIG 131A-14.
- [SDR DALA2016072005441](https://openairdocs.org/sdr/DALA2016072005441.md): Pan · cracked · Jul 19, 2016 · N995DL · Doug MD88 · Cargo/Baggage Doors
  > CRACKED INNER PAN ON AFT EDGE AND BEAM 5 AT FWD CARGO DOOR. PAN REPAIRED IAW SRM 52-03 D FIG 8.
- [SDR DALA2016071905432](https://openairdocs.org/sdr/DALA2016071905432.md): Cargo Track · corroded · Jul 18, 2016 · N995DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED CARGO TRACK BETWEEN BS 1007 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-10-4, 51-10-3 PAR 21 AND 14, 51-30-2, 51-30-1 AND 51-30-5.
- [SDR DALA2016071905434](https://openairdocs.org/sdr/DALA2016071905434.md): Bellcrank · corroded · Jul 17, 2016 · N995DL · Doug MD88 · Rudder Control System
  > CORROSION ON BELLCRANK AT RUDDER THROW-LIMITER. RUDDER BELLCRANK ASSY WAS REPLACED IAW AMM 27-20-03.
- [SDR DALA2016071805375](https://openairdocs.org/sdr/DALA2016071805375.md): Stringer · cracked · Jul 17, 2016 · N995DL · Doug MD88 · Wing, Rib/Bulkhead
  > CRACK ON STRINGER 11 AT THE OUTBOARD FLAP, INBOARD DRIVE HINGE AT STA XRS=160. LH SIDE. CRACKED LH STRINGER 11 AT THE OUTBOARD FLAP, INBOARD DRIVE HINGE AT STA XRS- =160, WAS REPAIRED IN REFERENCE TO CARD 5712 01030-03 AND IN ACCORDANCE WITH SERVICE REWORK DRA
- [SDR DALA2016071805374](https://openairdocs.org/sdr/DALA2016071805374.md): Longeron · corroded · Jul 17, 2016 · N995DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > SEVERAL AREAS OF CORROSION ON LONGERON 22L BETWEEN BS 1287 -- 1309. THE LONGERON WAS REPAIRED IAW SRM 53-02 FIG. 18 / 51-10-3 / 51-30-5.
- [SDR DALA2016071805373](https://openairdocs.org/sdr/DALA2016071805373.md): Doubler · worn · Jul 17, 2016 · N995DL · Doug MD88 · Cargo/Baggage Doors
  > WORN FWD & AFT DOUBLER ON LWR EDGE AT MID CARGO COMPARTMENT DOOR. THE DOUBLER WAS REPLACED IAW SRM 51-30-2 AND AFT DOUBLER WAS CLEANED IAW PSM 900-1-2 AND NO FOUND DAMAGE.

Next page: https://openairdocs.org/deregistered/N995DL-2022-10-26/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 = 'N995DL' AND deregistration_id = 'N995DL-2022-10-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N995DL-2022-10-26/reports

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