# Service difficulty reports: N936DL, cancelled Feb 12, 2021

A list on [N936DL, cancelled Feb 12, 2021](https://openairdocs.org/deregistered/N936DL-2021-02-12.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 · 130 reports

- [SDR DALA2018082105162](https://openairdocs.org/sdr/DALA2018082105162.md): Fuse · failed · Aug 19, 2018 · N936DL · Doug MD88 · Emergency Lighting
  > DURING A SERVICE CHECK, FOUND SEAT EMERGENCY LIGHTS, ROWS 30 TO AFT INOPERATIVE. TROUBLESHOT IAW WDM 33-51-14. FOUND TWO BAD FUSES ON CHARGER B5-212, AND LOOSE CONNECTOR AT PAX SEAT 33E. REPLACED FUSES IAW CMM 25-60-03, AND RECONNECTED THE PLUG, IAW AMM 3
- [SDR DALA2018070304329](https://openairdocs.org/sdr/DALA2018070304329.md): Wire · broken · Jun 29, 2018 · N936DL · Doug MD88 · Light System Wiring
  > SEAT MOUNTED EMERGENCY LIGHT INOP FROM ROW 31 TO 36. FOUND BAD FUSE ON BATTERY PACK, REMOVED AND REPLACED- NO HELP, AFTER INSPECTION OF WIRES FOUND BROKEN WIRE TO BATTERY PACK. REPAIRED WIRE/SPLICE IAW SPM 20-50 AND WDM 33-21. OPS CHECK GOOD.
- [SDR DALA2018062304165](https://openairdocs.org/sdr/DALA2018062304165.md): Support Fitting · cracked · Jun 21, 2018 · N936DL · Doug MD88 · Trailing Edge Flaps
  > RT WW TRAPEZOIDAL AND FLAP ACTUATOR SUPPORT FITTING MID-SECTION CRACKED. REMOVED AND REPLACED RT MLG W/W FLAP ACTUATOR SUPPORT FITTING IAW DRAWING 9910155 REV ED, REV DY, 5936030 REV AV, AND SRM 51-30-5. CRACK DIM 2.0".
- [SDR DALA2018062004116](https://openairdocs.org/sdr/DALA2018062004116.md): Skin · dented · Jun 19, 2018 · N936DL · Doug MD88 · Trailing Edge Flaps
  > LT WING NR 1 FLAP VANE LWR SURFACE HAS DENTS. ACCOMPLISHED PERMANENT REPAIR ON LT WING NR 1 FLAP VANE LWR SURFACE IAW SRM 57-03 AND SRM 51-70-2 PAR 18 B.
- [SDR DALA2018110106390](https://openairdocs.org/sdr/DALA2018110106390.md): Floorbeam · corroded · Jun 18, 2018 · N936DL · Doug MD88 · Fuselage Main, Floor Beam
  > CORRODED CEILING ANGLE IN E&E STA 160 APPROX RBL 30. CORROSION DAMAGE ON MAIN CABIN FLOORBEAM STA 160 RBL 30 FOUND OUT OF LIMITS DUE TO 100% MAT LOSS, ORIG THICKNESS.078" IAW SRM 53-01. ACCOMPLISHED A PERMANENT REPAIR TO AREA IAW ER/A 569009-14 REV ORIGINAL.
- [SDR DALA2018061504021](https://openairdocs.org/sdr/DALA2018061504021.md): Skin · corroded · Jun 14, 2018 · N936DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LT AFT FUSELAGE LAV SERVICE ACCESS DOOR LOWER CUTOUT IS CORRODED AT APPROX STA 1312. IN WORK REPAIR.
- [SDR DALA2018061403996](https://openairdocs.org/sdr/DALA2018061403996.md): Doubler · corroded · Jun 13, 2018 · N936DL · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT FRAME 1338 LOWER CHORD AFT SIDE TO APB STA 1361 HAS CORROSION IN BILGE APPROX LBL 10 - RBL 10. CORROSION DAMAGE ON AFT JACK PAD DOUBLER STA 1338 BL0 FOUND TO BE OUT OF LIMITS DUE TO 100% MAT LOSS, ORIG THICKNESS.100" IAW SRM 53-01 AND DRAWING 9915561 REV
- [SDR DALA2018052503605](https://openairdocs.org/sdr/DALA2018052503605.md): Engine · making metal · May 25, 2018 · N936DL · Doug MD88 · Engine (Turbine/Turboprop)
  > FLT 1668 DIVERTED TO CAE DUE TO A RIGHT ENGINE COMPRESSOR STALL ON CLIMB OUT AND ERRATIC ENGINE INDICATIONS. THE FLIGHT CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE ENGINE WAS NOT SHUT DOWN. MAINTENANCE FOUND METAL IN THE TAIL PIPE AND THE 3RD &
- [SDR DALA2018042502809](https://openairdocs.org/sdr/DALA2018042502809.md): Cable · disconnected · Apr 25, 2018 · N936DL · Doug MD88 · Power Lever
  > CREW REPORTED THAT THE RT ENGINE WAS UNRESPONSIVE ON APPROACH. SHUT THE ENGINE DOWN AT 20K DURING DECENT. THE RIGHT ENGINE DID NOT RESPOND. ENGINE WAS STUCK AT IDLE. THE ENGINE BEGAN CREEPING UP TO 1.4 EPR, WHICH WAS TOO MUCH FOR LANDING. THE FLIGHT CREW ELE
- [SDR DALA2018040202049](https://openairdocs.org/sdr/DALA2018040202049.md): Csd · failed · Apr 2, 2018 · N936DL · Doug MD88 · AC Generator-Alternator
  > RIGHT CSD OIL PRESSURE LOW MESSAGE ILLUMINATED DURING FLIGHT & APU WOULD NOT START. DIVERTED. MAINTENANCE FOUND NO OIL IN RIGHT CSD WITH FLUID AROUND FILTER AND SERVICE PORT. REPLACED THE CSD, GENERATOR, AND COOLER IAW AMM. BLED FUEL LINE TO APU AND STARTED
- [SDR DALA2017111608160](https://openairdocs.org/sdr/DALA2017111608160.md): Engine · making metal · Nov 15, 2017 · N936DL · Doug MD88 · Engine (Turbine/Turboprop)
  > DECLARED AN EMERGENCY DUE TO A RIGHT ENGINE OIL STRAINER CLOG MESSAGE. FOUND METAL IN THE OIL FILTER AND ON MCD. RT ENGINE CHANGED.
- [SDR DALA2017110808005](https://openairdocs.org/sdr/DALA2017110808005.md): Light · inoperative · Nov 8, 2017 · N936DL · Doug MD88 · Emergency Lighting
  > SEAT 19DEF EMERGENCY LIGHT INOPERATIVE. REPLACED THE LIGHT ASSY IAW AMM 33-53.
- [SDR DALA2017022301492](https://openairdocs.org/sdr/DALA2017022301492.md): Skin · corroded · Feb 22, 2017 · N936DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AND INTERNAL DOUBLER BS 750 - 759, LONGERON 29L - 29R CORRODED. REPAIRED IAW ERA 555617-14 ISSUED.
- [SDR DALA2016120509608](https://openairdocs.org/sdr/DALA2016120509608.md): Battery Pack · inoperative · Dec 4, 2016 · N936DL · Doug MD88 · Emergency Lighting
  > AFT OVERWING EXIT LIGHTS INOPERATIVE. TROUBLESHOT TO THE BATTERY PACK B5105. R & R BATTERY PACK IAW WDM 33-51.
- [SDR DALA2016120509607](https://openairdocs.org/sdr/DALA2016120509607.md): Fuse · failed · Dec 3, 2016 · N936DL · Doug MD88 · Emergency Lighting
  > FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. FOUND A BAD FUSE AT BATTERY CHARGER BASE. REPLACED THE FUSE IAW AMM 33-51. LIGHTS CHECKED OK.
- [SDR DALA2016101907380](https://openairdocs.org/sdr/DALA2016101907380.md): Fuse · blown · Oct 18, 2016 · N936DL · Doug MD88 · Emergency Lighting
  > EMERGENCY EXIT LIGHTING IN FIRST CLASS INOP. REPLACED FUSE NR 1 ON RT F/C EMERGENCY LIGHT BATTERY PACK, NOW OPS NORMAL. OK FOR SERVICE.
- [SDR DALA2016060204322](https://openairdocs.org/sdr/DALA2016060204322.md): Pan · cracked · Jun 1, 2016 · N936DL · Doug MD88 · Fuselage Main, Structure
  > RIGHT AFT OVERWING EXIT DOOR PAN CRACKED AT FWD UPPER DOOR STOP. R & R DOOR IAW AMM 52-21-00. LEAK CHECKED GOOD.
- [SDR DALA2016060104269](https://openairdocs.org/sdr/DALA2016060104269.md): Tail Cone · out of rig · May 31, 2016 · N936DL · Doug MD88 · Aerodynamic Fairings
  > VAULT DOOR FORCE REQUIRED TO DROP TAIL CONE EXCEEDED 20 LBS TENSION. ADJUSTED TAIL CONE RIG IAW AMM 53-53-00 AND AMDS 5350-01077-0101.
- [SDR DALA2016060104267](https://openairdocs.org/sdr/DALA2016060104267.md): Skin · cracked · May 31, 2016 · N936DL · Doug MD88 · Fuselage Main, Plate/Skin
  > A/C SKIN HAS.3750" LONG CRACK EXTENDING INBD FROM FASTENER HOLE AT BS 1418, 1.5" OTBD OF L2R. ACCOMPLISHED SEC I IAW ERA 547264-14AD. SEC II MONITOR AMOC REQUIRED BY 25 MAY 17. ESTABLISHED ON LOG PAGE 2505537.
- [SDR DALA2016060104265](https://openairdocs.org/sdr/DALA2016060104265.md): Skin · corroded · May 31, 2016 · N936DL · Doug MD88 · Fuselage Main, Plate/Skin
  > POPPED RIVET AND PILLOWING SKIN CORROSION ON BELLY AT BS 217 STR 30. COMPLETED SEC I IAW ERA 546984-14, REV O. SECTION II MONITOR TO BE ACCOMPLISHED AT 8000 CYCLE INTERVALS ESTABLISHED ON LOG PAGE 2509314.
- [SDR DALA2016053004219](https://openairdocs.org/sdr/DALA2016053004219.md): Door Frame · corroded · May 27, 2016 · N936DL · Doug MD88 · Fuselage Main, Structure
  > FWD CARGO DOOR FRAME UNDER ENTRY SCUFF PLATE CORRODED. DOOR FRAME OF SRM LIMITS. REMOVED AND REINSTALLED NEW LOWER PAN. REPAIRED IAW SRM 53-05, FIG 44A.
- [SDR DALA2016052604152](https://openairdocs.org/sdr/DALA2016052604152.md): Attach Fitting · broken · May 25, 2016 · N936DL · Doug MD88 · Fuselage Main, Attach Fittings
  > DUCT JOINT LOWER ATTACH TAB IS BROKEN, AFT OF LT GROUND BLOWER. WELDED TAB IAW ER/A 494638-14MA, REV B.
- [SDR DALA2016041502937](https://openairdocs.org/sdr/DALA2016041502937.md): Battery Pack · inoperative · Apr 15, 2016 · N936DL · Doug MD88 · Emergency Lighting
  > MAINTENANCE FOUND THE AFT CABIN EMERGENCY LIGHTS INOPERATIVE. BATTERY PACK WAS REPLACED AND THE LIGHTS CHECKED OK.
- [SDR DALA2015113007264](https://openairdocs.org/sdr/DALA2015113007264.md): Wire Harness · damaged · Nov 25, 2015 · N936DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 22D IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.
- [SDR DALA2015102306402](https://openairdocs.org/sdr/DALA2015102306402.md): Battery Pack · inoperative · Oct 22, 2015 · N936DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE VENTRAL STAIRWAY ARE VERY DIM. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.
- [SDR DALA2015082005095](https://openairdocs.org/sdr/DALA2015082005095.md): Angle · cracked · Aug 18, 2015 · N936DL · Doug MD88 · Vertical Stabilizer
  > STABILIZER SUPPORT STRUCTURE LT ANGLE CRACKED. REMOVED ANGLE, REPLACEMENT ANGLE WAS FABRICATED FROM.090, 7075-0, HEAT TREATED TO T6 CONDITION. ON RO 702799 IAW DWG 9911808, DRILL AND TRIMMED ANGLE. TREATED AND PAINTED. INSTALLED NEW ANGLE ALL FASTENERS SEC
- [SDR DALA2015082005094](https://openairdocs.org/sdr/DALA2015082005094.md): Angle · cracked · Aug 18, 2015 · N936DL · Doug MD88 · Vertical Stabilizer
  > DURING JACKSCREW INSPECTION FOUND VERTICAL STABILIZER SUPPORT STRUCTURE RT ANGLE CRACKED. ANGLE WAS FABRICATED FROM.090 7075-0 AND HEAT TREATED TO T6 ON RO 702799 IAW DWG 9911808. TREATED AND PAINTED. INSTALLED NEW ANGLE ALL FASTNERS SECURED REF SRM 51-30-
- [SDR DALA2015062403973](https://openairdocs.org/sdr/DALA2015062403973.md): Wire Harness · damaged · Jun 23, 2015 · N936DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FROM THE EXIT ROWS TO THE AFT CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS DUE TO THE WIRES BEING RIPPED FROM THE PINS AT THE CONNECTOR AT AFT CABIN LAST ROW. THE SYSTE
- [SDR DALA2015010800154](https://openairdocs.org/sdr/DALA2015010800154.md): Battery Pack · inoperative · Jan 8, 2015 · N936DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS ABOVE THE AFT OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA14024500936](https://openairdocs.org/sdr/DALA14024500936.md): Release Cable · out of tolerance · Apr 17, 2014 · N936DL · Doug MD88 · Aerodynamic Fairings
  > DURING THE TAILCONE RELEASE SYS FUNCTIONAL CHECK, MAINTENANCE FOUND THAT THERE WAS EXCESSIVE TENSION ABOVE 25 LBS IN THE RELEASE CABLE SYSTEM. THE CABLE RELEASE MECHANISM WAS ADJUSTED AND THE SYSTEM WAS RIGGED TO PULL AT 19 LBS. THE RII STEPS WERE COMPLETED A
- [SDR DALA14024520936](https://openairdocs.org/sdr/DALA14024520936.md): Catwalk · cracked · Apr 16, 2014 · N936DL · Doug MD88 · Fuselage Main, Structure
  > MAINTENANCE DISCOVERED THAT THE TAILCONE CATWALK OVER THE VENTRAL STAIRWAY HAD STRUCTURAL CRACKS IN 3 PLACES. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYSTEM AND COULD HAVE AN ADVERSE AFFECT ON THE EVACUATION ROUTE. THE CATWALK WAS REPAIRED IAW ER/
- [SDR DALA13071130936](https://openairdocs.org/sdr/DALA13071130936.md): Wire Harness · inoperative · Dec 23, 2013 · N936DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, NOTED THE SEAT MOUNTED EMERGENCY LIGHT AT 22DE INOPERATIVE. REPLACED HARNESS AT 22DE IAW AMM 33-52 AND OPERATION THEN CHECKED GOOD.
- [SDR DALA13063500936](https://openairdocs.org/sdr/DALA13063500936.md): Cabin Pressure · malfunctioned · Nov 22, 2013 · N936DL · Doug MD88 · Cabin Pressure Control System
  > PERFORMED AN AIR TURN BACK DUE TO ACFT CABIN WOULD NOT PRESSURIZE DURING CLIMB OUT. FLOW LIGHT ILLUMINATED. NO FAULTS ON EITHER CABIN PRESSURE CONTROLLERS. OUTFLOW VALVE OPERATION CHECKED GOOD. PRESSURIZED ACFT ON EACH PACK WITH NO EXTERNAL LEAKS FOUND. NO
- [SDR DALA13049090936](https://openairdocs.org/sdr/DALA13049090936.md): Ballast · burned · Sep 20, 2013 · N936DL · Doug MD88 · Passenger Compartment Lighting
  > DURING CLIMBOUT, AN ACRID ODOR BEGAN ISSUING FROM AIR CONDITIONING DUCTS. THE ENGINE ANTI-ICE WAS ON AND NORMAL PNEUMATIC CONFIGURATION. SELECTED A COLDER TEMP ON PACKS AND FUMES EVENTUALLY DISSIPATED. FOUND INOPERATIVE LIGHTING BALLAST AT ROW 33ABC. BALL
- [SDR DALA13011990936](https://openairdocs.org/sdr/DALA13011990936.md): Wire · disconnected · Mar 14, 2013 · N936DL · Doug MD88 · Light System Wiring
  > DURING OVERNIGHT MX, THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT ROW 31 WAS FOUND TO BE INOPERATIVE. MX FOUND A WIRE PULLED FROM THE CONNECTOR AT ROW 31. THE CONNECTOR WAS REPLACED IAW STANDARD WIRING PRACTICES MANUAL CHAPTER 20. OPERATION CHECKED GOOD.
- [SDR DALA13001020936](https://openairdocs.org/sdr/DALA13001020936.md): Wire Harness · inoperative · Jan 12, 2013 · N936DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MX FOUND THAT THE EMERGENCY LIGHTING AT SEATS 22 AND 28DE INOPERATIVE. MX REPLACED WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.
- [SDR DALA12016860936](https://openairdocs.org/sdr/DALA12016860936.md): Seat Track · corroded · Dec 19, 2012 · N936DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN, SEAT TRACK CORRODED AND GOUGED, BS 1226 TO 1250, RBL 22. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REPLACED SEAT TRACK IAW SRM 51-30-1.
- [SDR DALA12016810936](https://openairdocs.org/sdr/DALA12016810936.md): Seat Track · corroded · Dec 19, 2012 · N936DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND GOUGES ON MAIN CABIN SEAT TRACK AT LBL 45.5 FROM FS 484 TO 493. REMOVED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-30-5 AND SRM 51-30-1.
- [SDR DALA12016800936](https://openairdocs.org/sdr/DALA12016800936.md): Longeron · damaged · Dec 19, 2012 · N936DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON DOME NUT IN MAIN CABIN BS 250 L1. REPLACED LONGERON 2L SECTION AND SPLICE. REPLACED TWO ATTACH ANGLE FWD AND AFT DOME NUTS BETWEEN BS 227 AND 290. PERFORMED TCAS SELF TEST FOR UPPER TCAS ANTENNA. ALL WORK ACCOMPLISHED IAW SRM 51-30-5, 51-30-2,
- [SDR DALA12016760936](https://openairdocs.org/sdr/DALA12016760936.md): Channel · damaged · Dec 17, 2012 · N936DL · Doug MD88 · Fuselage Miscellaneous Structure
  > E & E BAY BS 218, LONGERON 30 & 29 LT HAS DAMAGE TO LONGERON FLANGE ON BOTH SIDES OF LONGERON HAT CHANNEL. REMOVED DAMAGE ON E/E BAY STA 218, LONGERON 30 AND 29L ON LONGERON FLANGE IAW SRM 51-03, FIG 1. FOUND TO BE WITHIN LIMITS. HFEC INSP DETECTED 1 EA CRACK
- [SDR DALA12016750936](https://openairdocs.org/sdr/DALA12016750936.md): Doubler · corroded · Dec 17, 2012 · N936DL · Doug MD88 · Fuselage Miscellaneous Structure
  > FS 594 BETWEEN L30-L29R, POTABLE WATER BELLY DRAIN DOUBLER CORRODED. REMOVED CORROSION FROM DOUBLER FS 594 L30-29R MID CARGO IAW SRM 51-10-3. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, AND INSTALLED POTABLE WATER FITTING HOSE AND INTERNAL RING DOUBLER
- [SDR DALA12016740936](https://openairdocs.org/sdr/DALA12016740936.md): Attach Angle · cracked · Dec 17, 2012 · N936DL · Doug MD88 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STAB TO FUSELAGE LT SKATE ANGLE AND FASTENERS ARE CRACKED STA 1474 CANT. CUT OUT CRACKED AREA AT VERTICAL STAB TO FUSELAGE LT SKATE ANGLE STA 1474 CANT. FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE IAW SRM 53-05, FIG 23 THE CRACKED FASTENER WAS
- [SDR DALA12016730936](https://openairdocs.org/sdr/DALA12016730936.md): Skin · cracked · Dec 17, 2012 · N936DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING NDT INSPECTION, FWD SERVICE DOOR JAMB CORNER, FOUND ONE CRACK ON UPPER FWD CORNER ON OUTER LAYER OF SKIN. CUT OUT DAMAGE AREA AND REPAIRED IAW SRM 53-05, FIG 112, VIEW D AND ER/A 45.
- [SDR DALA12016480936](https://openairdocs.org/sdr/DALA12016480936.md): Skin · damaged · Dec 16, 2012 · N936DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON CUTOUT AND AROUND FASTENERS, FWD CARGO BAY BS 370 L26R. REPAIRED DAMAGED IAW SRM 51-70-4, PG 1-4.
- [SDR DALA12016080936](https://openairdocs.org/sdr/DALA12016080936.md): Fairing · cracked · Dec 13, 2012 · N936DL · Doug MD88 · Vertical Stabilizer
  > ON INSTALLATION OF VERTICAL STAB TIP FAIRING, FOUND A CRACK ON RT SIDE, EMINATING FROM A RADIUS OF UPPER SKIN. REMOVED FITTING ON RT STAB FAIRING BY ACCESS TO CRACK. NDT VERIFIED END OF CRACK, CHECK STOP DRILL, AND OPEN HOLES. FABRICATED, PRIMERED, TREATED,
- [SDR DALA12015370936](https://openairdocs.org/sdr/DALA12015370936.md): Bulkhead · cracked · Dec 6, 2012 · N936DL · Doug MD88 · Fuselage Main, Bulkhead
  > FS 1007, LBL 18 MLG WW AFT PRESSURE BULKHEAD AFT FACE (ACCESS FROM AFT CARGO BIN) SUSPECTED CRACK NEXT TO U CHANNEL STIFFENER APPROX 2 INCHES FROM TOP OF BULKHEAD (064-68) COMPLIED WITH FINAL ER/A 508338-14 REV ORIGINAL.
- [SDR DALA12015360936](https://openairdocs.org/sdr/DALA12015360936.md): Bulkhead · cracked · Dec 6, 2012 · N936DL · Doug MD88 · Fuselage Main, Bulkhead
  > FS 1007, RBL18, MLG WW AFT PRESSURE BULKHEAD AFT FACE (ACCESS FROM AFT CARGO BIN) SUSPECTED CRACK NEXT TO U-CHANNEL STIFFENER APPROX 2" FROM TOP OF BULKHEAD (064-69). COMPLIED WITH PRI 508338-14, REV 0, COMPLIED WITH PRI 508338-14 REV 1, COMPLIED WITH FINAL E
- [SDR DALA12014850936](https://openairdocs.org/sdr/DALA12014850936.md): Longeron · damaged · Dec 5, 2012 · N936DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > LONGERON 4R CRACKED AT ST 522 AND ST 541 UNDER SUPPORT MOUNT (204-111&112). REMOVED INTERCOSTAL BETWEEN STA 522-541 AT L4R. REMOVED DAMAGE LONGERON AT STA 513 TO 550 AT L4R. HFEC INSPECTION NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED LONGERON AND SPLICES
- [SDR DALA12014840936](https://openairdocs.org/sdr/DALA12014840936.md): Cusp Web · corroded · Dec 5, 2012 · N936DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB FLOOR PANEL, AFT LT CORNER ST 199L AT BL 44L (204-151). CUTOUT CORROSION AND REPAIRED CUSP WEB FLOOR PANEL STA 199 LBL44 IAW SRM 53-01, FIG 4, SHEET 4. COMPLETED AND INSPECTED.
- [SDR DALA12014830936](https://openairdocs.org/sdr/DALA12014830936.md): Skin · corroded · Dec 5, 2012 · N936DL · Doug MD88 · Fuselage Main, Plate/Skin
  > ON REMOVAL OF POTABLE WATER BELLY DRAIN AT FS 594 BETWEEN L30-L29R, EXTERNAL FUSELAGE FOUND CORROSION ON DRAIN CUTOUT AND INTERNAL SKIN. COMPLIED WITH ER/A 508946-14 REV ORIGINAL. COMPLETED AND INSPECTED. ASSOCIATED ER/A 14-508946 ADDED FOR AC 0936.

Next page: https://openairdocs.org/deregistered/N936DL-2021-02-12/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 = 'N936DL' AND deregistration_id = 'N936DL-2021-02-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N936DL-2021-02-12/reports

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