# Service difficulty reports: N965DL, cancelled Dec 30, 2024

A list on [N965DL, cancelled Dec 30, 2024](https://openairdocs.org/deregistered/N965DL-2024-12-30.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 DALA2020031701890](https://openairdocs.org/sdr/DALA2020031701890.md): Tab · punctured · Mar 16, 2020 · N965DL · Doug MD88 · Elevator, Tab Structure
  > WHILE PERFORMING REP INSPN ON LT GEAR TAB MON 1450634, FOUND PUNCTURE DMG ON UPPER SIDE OF TAB. REPLACED LT ELEVATOR GEARED TAB IAW W/C 2730-4130-LH. TAB, ELEVATOR, OFF 09-5525-9-0001 S/N 49956. (LP6953373)
- [SDR DALA2020022101316](https://openairdocs.org/sdr/DALA2020022101316.md): Coffeemaker · odor · Feb 20, 2020 · N965DL · Doug MD88 · Buffet/Galleys
  > ON DESCENT FA REPORTED SMOKE SMELL AROUND FWD GALLEY. WE SMELLED IT IN COCKPIT AT SAME TIME (BURNT POPCORN SMELL). NOTHING WAS IN OVEN. I TURNED OFF GALLEY PWR SMELL DISSIPATED FA REPORTED SMELL WAS AROUND #1 COFFEE MKR. RESTORE GALLEY PWR. TURNED BOTH COFFEE
- [SDR DALA2020020700952](https://openairdocs.org/sdr/DALA2020020700952.md): Duct · blown · Feb 6, 2020 · N965DL · Doug MD88 · Engine Anti-Icing System
  > SHIP 965 -ATB- DUE TO NBR 1 ENGINE FIRE INDICATION. CREW REPORTED FIRE INDICATION PULLED THROTTLE BACK AND FIRE INDICATION EXTINGUISHED. CORRECTIVE ACTION: MAINTENANCE FOUND 13TH STAGE ANTI-ICE DUCT BLOWN AT 12 O'CLOCK POSITION. REPLACED DUCT, ANTI-ICE VALVE,
- [SDR DALA2020012000394](https://openairdocs.org/sdr/DALA2020012000394.md): Lamp · inoperative · Jan 20, 2020 · N965DL · Doug MD88 · Emergency Lighting
  > CAT WALK OVERHEAD EMERGENCY LIGHT INOP. RELAMPED SAME, REF MD88 AMM 33-53. CHECKS GOOD. (LP6394590)
- [SDR DALA2019121437302](https://openairdocs.org/sdr/DALA2019121437302.md): Switch · miswired · Dec 13, 2019 · N965DL · Doug MD88 · Exterior Lighting
  > WHEN WE GOT ON THE GROUND NOSE WHEEL LIGHT PULSED WITH SPEED OF MOTORS. INTERIOR LIGHTS PULSED TOO. BOTH NOSE TAXI LAMPS BLOWN, NO POWER TO EITHER NOSE TAXI LAMP. R &R RT TAXI LAMP SUSPECT INPROPER WIRING "UN MARKED WIRES ON LT NOSE TAXI LAMP."WHILE TROUBLESHO
- [SDR DALA2019100605735](https://openairdocs.org/sdr/DALA2019100605735.md): Frame · cracked · Oct 5, 2019 · N965DL · Doug MD88 · Fuselage Main, Frame
  > TAILCONE CANTED SUPPORT FRAME (1)CRACKED @GUIDE PIN 1:00 (2) CRACKED @5:00 NEAR GUIDE PIN MKD. REMOVED RT. FRAME AND DRILLED NEW FRAME PER BOEING DWG5966769 (458779) BEGAN INSTALLATION OF RT FRAME (ALL FASTENERS THROUGH SKIN INSTALLED) PER BOEING DWG 5966769.
- [SDR DALA2019100605734](https://openairdocs.org/sdr/DALA2019100605734.md): Frame · cracked · Oct 5, 2019 · N965DL · Doug MD88 · Fuselage Main, Frame
  > LOWER FRAME CRACKED AT 7:00 POSITION (MARKED) AT TAILCONE GUIDE PIN.REMOVED LT. FRAME AND DRILLED NEW FRAME PER BOEING DWG 5966769. BEGAN INSTALLATION OF LT. FRAME (ALL FASTENERS THRU SKIN INSTALLED.) PER BOEING DWG 5966769(450401) FINISHED INSTALLATION OF LOW
- [SDR DALA2019093005574](https://openairdocs.org/sdr/DALA2019093005574.md): Pin · disengaged · Sep 30, 2019 · N965DL · Doug MD88 · Escape Slide
  > SVC CHK FOUND L1 DOOR SLIDE PIN NOT ENGAGED. REMOVED L1 DOOR SLIDE REF W/C 2561-4964 INSTALLING NEW SLIDE REF W/C 2561-4964. SLIDE, EVAC, FO OFF 88-2560-9-0003 S/N 03040. (LP5587108)
- [SDR DALA2019100305658](https://openairdocs.org/sdr/DALA2019100305658.md): Door · detached · Sep 28, 2019 · N965DL · Doug MD88 · Doors
  > EXTERNAL POWER DOOR MISSING. INSTALLED EXTERNAL POWER ACCESS DOOR ASSYM PER MD88 CMM 53-30-02.
- [SDR DALA2019082905057](https://openairdocs.org/sdr/DALA2019082905057.md): Smoke Detector · malfunctioned · Aug 28, 2019 · N965DL · Doug MD88 · Smoke Detection
  > F/C LAVATORY SMOKE DETECTOR WILL NOT TURN OFF. SMOKE DETECTOR BEEPING. R AND R F/C LAV SMOKE DET REF MD88 M/M 26-17. CKS GOOD. (LP1244638)
- [SDR DALA2019062433762](https://openairdocs.org/sdr/DALA2019062433762.md): Unknown · odor · Jun 23, 2019 · N965DL · Doug MD88 · Air Distribution System
  > ON TAXI IN FUEL SMELL THROUGH GASPERS IN FWD GALLEY AND COCKPIT. APU RUNNING. T/S PER AMDS W.C. 2120-2367 - NO CONTAMINATION OF FLUIDS FOUND. PERFORMED FULL DUCT BURNOUT PER AMDS W.C. 7100-2619 - NO ODORS DETECTED - ALL PANELS CLOSED. ALL NO GO ODI PREVENTION
- [SDR DALA2019050602813](https://openairdocs.org/sdr/DALA2019050602813.md): Lanyard · defective · May 5, 2019 · N965DL · Doug MD88 · Escape Slide
  > SLIDE FAILED TO DEPLOY WORK CARD # 88-0525-8-0408 SLIDE D29984-213 S/N 1241 MFG DATE MAR 2000. FND LANYARD ON COVER BAD REPLCD SAME. (LP1060688)
- [SDR DALA2019030201363](https://openairdocs.org/sdr/DALA2019030201363.md): Engine · malfunctioned · Mar 1, 2019 · N965DL · Doug MD88 · Engine (Turbine/Turboprop)
  > ON CLIMB OUT BETWEEN 14,500 AND 15,000 FEET WE HEARD A LOUD BANG ACCOMPANIED WITH AN AIRCRAFT SHUTTER AND NOTED LEFT ENGINE NO EPR, NO N1, EGT APPROX. 775, DID IMMEDIATE ACTION ITEMS AND SHUT DOWN LEFT ENGINE PER QRH. STABILIZED AIRCRAFT AT 16,00 FEET RETURNED
- [SDR DALA2018122707421](https://openairdocs.org/sdr/DALA2018122707421.md): Generator · failed · Dec 26, 2018 · N965DL · Doug MD88 · AC Generator-Alternator
  > WITH RIGHT ENGINE GENERATOR ON DEFERRAL, APPROACHING IND, RT BUS LOST POWER, WITH APU RUNNING. RESET APU ON SHORT FINAL AND REGAINED POWER TO RT BUS. AIRPLANE NOT SUITABLE FOR MC FLIGHT. APPROACH WAS SISUAL ONLY WITH AIRSPEED SETTING KNOB NOR RESPONSIVE UNTIL
- [SDR DALA2018112606792](https://openairdocs.org/sdr/DALA2018112606792.md): Horn · corroded · Nov 26, 2018 · N965DL · Doug MD88 · Leading Edge Devices
  > ON WALK AROUND FOUND CORROSION CRACK ON RT WING INBOARD SLAT. REPLACED RT SLAT HORN PER MD88 AMM 27-80. (LP5059545)
- [SDR DALA2018070704417](https://openairdocs.org/sdr/DALA2018070704417.md): Skin · cracked · Jul 6, 2018 · N965DL · Doug MD88 · Passenger/Crew Doors
  > MAIN ENTRY DOOR UPPER AFT CORNER INTERNAL SURFACE IS CRACKED. REMOVED AND REPLACED MAIN ENTRY DOOR IAW AMM 52-11-00.
- [SDR DALA2018070404358](https://openairdocs.org/sdr/DALA2018070404358.md): Skin · gouged · Jul 3, 2018 · N965DL · Doug MD88 · Trailing Edge Flaps
  > RT WING ON NR 3 FLAP VANE IB SIDE UPPER SURFACE GOUGED. REMOVED DAMAGED SKIN (7" X 7") AND ACCOMPLISHED PERMANENT REPAIR ON NR 3 FLAP VANE LEADING EDGE (16.5" X 12.1" DOUBLER) IAW SRM 57-03D PAR 11 AND FIGURE 11.
- [SDR DALA2018070304350](https://openairdocs.org/sdr/DALA2018070304350.md): Longeron Splice · corroded · Jul 2, 2018 · N965DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPT LONGERON 28L SPLICE IS CORRODED AT FS 1202. CORROSION DAMAGE ON AFT CARGO LONGERON 28LT STA 1202 SPLICE FOUND OUT OF LIMITS DUE TO 100% MAT LOSS, ORIG THICKNESS.062" IAW SRM 53-01 FIG 1 AND DRAWING 3914677 REV L. REMOVED AND REPLACED SPLICE IA
- [SDR DALA2018070304349](https://openairdocs.org/sdr/DALA2018070304349.md): Longeron Splice · corroded · Jul 2, 2018 · N965DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPT LONGERON 29L SPLICE IS CORRODED AT FS STA 1202. AFT CARGO LONGERON 29LT SPLICE STA 1202 CORROSION DAMAGE FOUND OUT OF LIMITS DUE TO 100% MAT LOSS, ORIG THICKNESS.062" IAW SRM 53-01 FIG 1 AND DRAWING 3914677 REV L. REMOVED AND REPLACED SPLICE I
- [SDR DALA2018070304348](https://openairdocs.org/sdr/DALA2018070304348.md): Intercostal · corroded · Jul 2, 2018 · N965DL · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT CARGO AT STR 29L BTW STA 1212 AND 1231 INTERCOSTAL O/B SIDE HAS CORROSION. CORROSION DAMAGE ON AFT CARGO INTERCOSTAL AT LONGERON 29LT BETWEEN STA 1212 AND 1231 FOUND OUT OF LIMITS DUE TO 100% MAT LOSS, ORIG THICKNESS.050" IAW SRM 53-01 FIG 1 AND DRAWING 5
- [SDR DALA2018070304332](https://openairdocs.org/sdr/DALA2018070304332.md): Bulkhead · corroded · Jul 1, 2018 · N965DL · Doug MD88 · Fuselage Main, Bulkhead
  > CORROSION FOUND AT AFT PRESSURE BULKHEAD BL0. CORROSION DAMAGE ON AFT PRESSURE BULKHEAD OEM BL0 DOUBLER FOUND OUT OF LIMITS, ORIG THICKNESS.080", MAT LOSS.040", MAT REMAINING.040" IAW DRAWING 5910130 REV ET AND SRM 53-01. REMOVED, FABRICATED NEW, AND INSTAL
- [SDR DALA2018070304331](https://openairdocs.org/sdr/DALA2018070304331.md): Doubler · corroded · Jun 29, 2018 · N965DL · Doug MD88 · Fuselage Main, Plate/Skin
  > AFT CARGO JACK PAD DOUBLER IS CORRODED. FOUND AREA CORRODED ON AFT CARGO JACK PAD DOUBLER WITH ORIGINAL THICKNESS.100 MATT LOSS.060 MATT REMAINING.040 TO BE OUT OF LIMITS IAW SRM 53-01 AFTER CORROSION WAS REMOVED IAW SRM 51-10-3. REMOVED AND INSTALLED NEW D
- [SDR DALA2018070304352](https://openairdocs.org/sdr/DALA2018070304352.md): Repair · departed · Jun 28, 2018 · N965DL · Doug MD88 · Elevator, Tab Structure
  > RT HAND ELEVATOR GEAR TAB (CENTER) HAD BONDED REPAIR THAT HAS DEPARTED AIRCRAFT. REMOVED AND REPLACED RT ELEVATOR GEAR TAB IAW AMM 27-30-04. PERFORMED SATISFACTORY OPS CHECK IAW AMM-27-30-04.
- [SDR DALA2018060403777](https://openairdocs.org/sdr/DALA2018060403777.md): Skin · corroded · Jun 2, 2018 · N965DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE LAV SVC CUTOUT STA 1322 AT L-22L CORROSION. COMPLIED WITH ERA 568960-14 REV B SECTION 1 PERMANENT REPAIR. ALL STEPS IN PRI'S 568960-14 REV O, REV 1, REV 2, REV 3, AND REV 4 MATCH STEPS IN ERA 568960-14 REV B SECTION 1 PERMANENT REPAIR.
- [SDR DALA2018051603378](https://openairdocs.org/sdr/DALA2018051603378.md): Tire · defective · May 16, 2018 · N965DL · Doug MD88 · Tire
  > ON ROTATION IN RDU 3 LOUD BANGS FROM NOSE GEAR AREA ON LANDING, WITH GEAR EXTENDED, NOTICED A DEEP RUMBLE IN FLOOR UNDER PILOTS FEET. EMERGENCY WAS DECLARED. INSPECTED NLG AREA. NO DAMAGED NOTED. R&R BOTH NLG TIRE IAW AMM 32-40. LUBE NLG SYS. A/C OK FOR SVC.
- [SDR DALA2018041102339](https://openairdocs.org/sdr/DALA2018041102339.md): Generator · failed · Apr 10, 2018 · N965DL · Doug MD88 · AC Generator-Alternator
  > RIGHT GENERATOR FAILED. WOULD NOT RESET IN FLIGHT AND A CROSSTIE LOCK-OUT THAT WOULD NOT RESET. AN EMERGENCY WAS DECLARED.
- [SDR DALA2018010300036](https://openairdocs.org/sdr/DALA2018010300036.md): Not Reported · malfunctioned · Dec 4, 2017 · N965DL · Doug MD88 · Aircraft Fuel Distribution System
  > DIVERTED TO BNA DUE TO THE FLIGHT CREW REPORTING THAT FUEL APPEARED NOT TO BE BURNING OUT OF THE LEFT WING TANK. MAINTENANCE VERIFIED THAT THE CROSS-FEEDS AND DEFUEL VALVES WERE OPERATING NORMALLY. THE LEFT TANK FUEL BOOST PUMP OPERATION CHECKED GOOD. A HIGH P
- [SDR DALA2017071005349](https://openairdocs.org/sdr/DALA2017071005349.md): Hydraulic System · leaking · Jul 10, 2017 · N965DL · Doug MD88 · Hydraulic System, Main
  > APU INLET SATURATED WITH HYD FLUID, CABIN HAZE WITH HYD MIST. CLEANED THE APU INLET & BELLY IAW W/C 4900-1184. PERFORMED FULL DUCT BURNOUT IAW W/C 7100-2619, NO SMOKE OR ODOR NOTED.
- [SDR DALA2017052404151](https://openairdocs.org/sdr/DALA2017052404151.md): Actuator · damaged · May 22, 2017 · N965DL · Doug MD88 · Drag Control Actuator
  > AFTER LANDING, THE PREVIOUS FLIGHT CREW REPORTED A SLAT WOULD NOT RETRACT AND RIGHT FLAP INDICATED APPROX. 3 DEG WITH FLAP SET AT ZERO. FOUND THE RT INBD SPOILER ACTUATOR ROD END BROKEN AND BINDING THE FLAPS. REMOVED AND REPLACED THE SPOILER ACTUATOR, OPS AND
- [SDR DALA2017052304111](https://openairdocs.org/sdr/DALA2017052304111.md): Vane · punctured · May 22, 2017 · N965DL · Doug MD88 · Trailing Edge Flaps
  > RT NR 2 FLAP VANE HAS PUNCTURE APPROX 45" FROM INBD EDGE AND 11" FROM TRAILING EDGE MEASURING APPROX 3/4 " X 3/4 ". REMOVED AND REPLACED FLAP VANE REF AMM 27-51-03-201, OPS CKS GOOD.
- [SDR DALA2017041703102](https://openairdocs.org/sdr/DALA2017041703102.md): Cable · frayed · Apr 15, 2017 · N965DL · Doug MD88 · Aerodynamic Fairings
  > TAILCONE CABLE FRAYED. REPLACED THE CABLE IAW AMM 53-53-00.
- [SDR DALA2017032702436](https://openairdocs.org/sdr/DALA2017032702436.md): Floor Panel · damaged · Mar 23, 2017 · N965DL · Doug MD88 · Fuselage Floor Panel
  > CARPET HAS A SOFT SPOT ABOUT 5 BY 5 INCHES. REPLACED CABIN FLOOR PANEL 256C AT CENTER OF F/C CABIN.
- [SDR DALA2016122210030](https://openairdocs.org/sdr/DALA2016122210030.md): Module · failed · Dec 21, 2016 · N965DL · Doug MD88 · Emergency Lighting
  > SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE ROW 30. REPLACED THE LIGHT MODULE AND HARNESS IAW AMM 33-53. CHECKED GOOD.
- [SDR DALA2016120609639](https://openairdocs.org/sdr/DALA2016120609639.md): Tab · damaged · Dec 5, 2016 · N965DL · Doug MD88 · Rudder, Tab Structure
  > RUDDER HAS FLAME SPRAY PEELING AND DAMAGED. REMOVED AND REPLACED RUDDER IAW AMDS 2720-4421.
- [SDR DALA2016120609638](https://openairdocs.org/sdr/DALA2016120609638.md): Tab · damaged · Dec 5, 2016 · N965DL · Doug MD88 · Rudder, Tab Structure
  > RUDDER CONTROL TAB HAS FLAME SPRAY PEELED AND DAMAGED. REPLACED THE RUDDER TAB.
- [SDR DALA2016120609636](https://openairdocs.org/sdr/DALA2016120609636.md): Frame · cracked · Dec 5, 2016 · N965DL · Doug MD88 · Fuselage Main, Frame
  > BS 1510 CANTED FRAME CRACKED APPROXIMATE LOCATION LONGERON 28R AT TAIL CONE ALIGNMENT PIN. REMOVED AND REPLACED CANTED FRAME AND INSTALLED NEW CANTED FRAME IAW DRAWING 9911843.
- [SDR DALA2016120609637](https://openairdocs.org/sdr/DALA2016120609637.md): Frame · cracked · Dec 4, 2016 · N965DL · Doug MD88 · Fuselage Main, Frame
  > BS 1510 CANTED FRAME CRACKED LONGERON 23R. REMOVED AND REPLACED THE FRAME IAW DRAWING 9911843.
- [SDR DALA2016110708302](https://openairdocs.org/sdr/DALA2016110708302.md): Relay · burned · Nov 6, 2016 · N965DL · Doug MD88 · Passenger Compartment Lighting
  > RUBBER SMELL ON TAKEOFF WITH BURNING ODOR. DISSIPATED IN 2-3 MINUTES. UPPER SIDEWALL LIGHTS FLICKERED ON AND OFF (INTERMITTENT USE). COFFEE MAKERS ON AND OFF ALSO. AS PER QRH TURNED GALLEY POWER OFF AISLE LIGHT ON AND SIDEWALL LIGHTS OFF. UPPER SIDEWALL L
- [SDR DALA2016070705158](https://openairdocs.org/sdr/DALA2016070705158.md): Hinge · worn · Jul 7, 2016 · N965DL · Doug MD88 · Fuselage, Door Hinge
  > MID CARGO DOOR FWD AND AFT HINGES LOOSE & WORN, DOOR VERY LOOSE. REPLACED THE WORN PARTS AND ADJUSTED IAW AMM 52-31-02. LEAK CHECKED GOOD.
- [SDR DALA2016070705157](https://openairdocs.org/sdr/DALA2016070705157.md): Release Mech · out of tolerance · Jul 7, 2016 · N965DL · Doug MD88 · Aerodynamic Fairings
  > DURING TAILCONE RELEASE SYSTEM FUNCTIONAL CHECK, OPENING FORCE REQUIRE TO OPEN AFT VENTRAL DOOR IS 30 LBS. PULL TEST OUT OF LIMITS. RIGGED TAILCONE IAW AMDS 5350-01077-0101. ADJUSTED TEE PIN CLIPS, LATCHES, AND LUBED IAW AMDS 5350-01077-0101. PERFORMED TA
- [SDR DALA2016070605126](https://openairdocs.org/sdr/DALA2016070605126.md): Slide · low pressure · Jul 5, 2016 · N965DL · Doug MD88 · Escape Slide
  > ON PRE DOCK, LT AFT SERVICE DOOR SLIDE PRESSURE LOW. REMOVED AND INSTALLED L2 DOOR SLIDE IAW AMDS 2561-4002.
- [SDR DALA2016070605125](https://openairdocs.org/sdr/DALA2016070605125.md): Repair · delaminated · Jul 5, 2016 · N965DL · Doug MD88 · Elevator, Tab Structure
  > RT ANTI-FLOAT TAB, INBD REPAIR IS DIS-BONDED, TOP SURFACE. REMOVED AND INSTALLED RT ANTI-FLOAT TAB ON AMDS 2730-4382.
- [SDR DALA2016070605123](https://openairdocs.org/sdr/DALA2016070605123.md): Vane · damaged · Jul 5, 2016 · N965DL · Doug MD88 · Trailing Edge Flaps
  > RT NR 4 VANE HAS RUBBING MARKS. R & R VANE REF AMM 27-51-03.
- [SDR DALA2016070505098](https://openairdocs.org/sdr/DALA2016070505098.md): Vane · damaged · Jul 3, 2016 · N965DL · Doug MD88 · Trailing Edge Flaps
  > RIGHT NR 3 FLAP VANE HAS A RUBBING AREA WITH A HOLE THROUGH. R & R VANE IAW AMM 27-51-03.
- [SDR DALA2016063005036](https://openairdocs.org/sdr/DALA2016063005036.md): Floor Support · corroded · Jun 30, 2016 · N965DL · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT RT FLOOR SUPPORT CORRODED UNDER FLOORBOARD PANEL 120E. APPROXIMATE STA 160, RBL55. R & R FLOOR SUPPORT IAW SRM 53-30-02.
- [SDR DALA2016062905025](https://openairdocs.org/sdr/DALA2016062905025.md): Bushing · worn · Jun 29, 2016 · N965DL · Doug MD88 · Elevator, Tab Structure
  > RT ANTI-FLOAT TAB, OTBD BEARING IS WORN. R & R WORN BUSHINGS, REF PS 900-9-1, NR 06 REF NR 78 FOR TAB REPLACEMENT.
- [SDR DALA2016061504699](https://openairdocs.org/sdr/DALA2016061504699.md): Slide · defective · Jun 15, 2016 · N965DL · Doug MD88 · Escape Slide
  > L1 DOOR SLIDE PARACHUTE PINS NOT INSTALLED. R & R L1 DOOR SLIDER IAW WC 2561-4964. OK FOR SERVICE.
- [SDR DALA2016053004220](https://openairdocs.org/sdr/DALA2016053004220.md): Fastener · damaged · May 28, 2016 · N965DL · Doug MD88 · Fuselage Structure (General)
  > RIVET HEAD POPPED AT BS 226 AND LONGERON 20-R. REMOVED STRINGER SPLICE AND DAMAGED STRINGER SECTION AT 20R, STA 226, ITEM C/W ON LOG NR 2509285.
- [SDR DALA2016051303906](https://openairdocs.org/sdr/DALA2016051303906.md): Battery Pack · inoperative · May 12, 2016 · N965DL · Doug MD88 · Emergency Lighting
  > RT FORWARD OVERWING EXIT EMERGENCY IDENTIFIER INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY REF AMM 33-53-00. OPS NORMAL.
- [SDR DALA2016051303905](https://openairdocs.org/sdr/DALA2016051303905.md): Power Supply · inoperative · May 12, 2016 · N965DL · Doug MD88 · Emergency Lighting
  > ROWS 16-25, EMERGENCY CEILING LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES FOR APPLICABLE LIGHTS REF AMM 33-53-00. OPS NORMAL.

Next page: https://openairdocs.org/deregistered/N965DL-2024-12-30/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 = 'N965DL' AND deregistration_id = 'N965DL-2024-12-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N965DL-2024-12-30/reports

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