# Service difficulty reports: N923DL, cancelled Apr 8, 2019

A list on [N923DL, cancelled Apr 8, 2019](https://openairdocs.org/deregistered/N923DL-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 · 172 reports

- [SDR DALA2017121808668](https://openairdocs.org/sdr/DALA2017121808668.md): Lamp · inoperative · Dec 17, 2017 · N923DL · Doug MD88 · Emergency Lighting
  > BOTH FWD CABIN DOOR EMERGENCY LIGHTS OUT. RELAMPED BOTH FWD CABIN DOOR EMERGENCY LIGHT ASSYS PER MD88 AMM 33-53. OPS CHECKED GOOD. (LP3869586)
- [SDR DALA2017092507064](https://openairdocs.org/sdr/DALA2017092507064.md): Engine · failed · Sep 25, 2017 · N923DL · Doug MD88 · Engine (Turbine/Turboprop)
  > AT APPROXIMATELY 85 KTS DUE TO HEARING A BANG & THE NR 2 ENGINE EGT AT 750 DEGREES. ABORTED TAKEOFF. STOPPED ON RUNWAY, FIRE DEPT SPRAYED THE NR 2 ENGINE AS PRECAUTION. FOUND METAL IN TAIL PIPE AND TURBINE DAMAGE. ENGINE CHANGE COMPLETED.
- [SDR DALA2017022501572](https://openairdocs.org/sdr/DALA2017022501572.md): Skin · corroded · Feb 24, 2017 · N923DL · Doug MD88 · Fuselage Main, Plate/Skin
  > BULGING FUSELAGE SKIN BS 680 - 700 BETWEEN LONGERONS 29L-29R. THE SKIN WAS REPAIRED IAW ETI-88-17-068 REV. 6, AND ER/A 554161-14 REV. ORIGINAL.
- [SDR DALA2017022501571](https://openairdocs.org/sdr/DALA2017022501571.md): Access Panel · corroded · Feb 24, 2017 · N923DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON ACCESS PANEL ON RT WING. THE ACCESS PANEL WAS REPAIRED IAW SRM 51-22-2A, PAR 6, CONDITION II (C).
- [SDR DALA2017022401527](https://openairdocs.org/sdr/DALA2017022401527.md): Access Panel · corroded · Feb 23, 2017 · N923DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON FUEL TANK ACCESS PANEL. CORROSION MEASURED AND FOUND OUT OF LIMITS. REPLACED THE ACCESS PANEL IAW SRM 51-22-2A CONDITION II.
- [SDR DALA2017022401526](https://openairdocs.org/sdr/DALA2017022401526.md): Access Panel · corroded · Feb 23, 2017 · N923DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON ACCESS PANEL. CORROSION MEASURED AND FOUND OUT OF LIMITS. REPLACED IAW SRM 51-22-2A CONDITION II.
- [SDR DALA2017022301493](https://openairdocs.org/sdr/DALA2017022301493.md): Support · cracked · Feb 22, 2017 · N923DL · Doug MD88 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED CONNECTOR SUPPORT ON FIRE LOOP AT FLANGE "J" BTW 6 TO 7 HRS POSITION, RT NACELLE. FIRE DETECTOR LOOP SUPPORT ASSY WAS REMOVED IAW AMM 26-10-04 AND REPLACED IAW AMM 26-10-04. TESTED IAW AMM 26-00-00-201.
- [SDR DALA2017022301489](https://openairdocs.org/sdr/DALA2017022301489.md): Doubler · worn · Feb 22, 2017 · N923DL · Doug MD88 · Fuselage Main, Plate/Skin
  > WORN TITANIUM DOUBLER AT BS 1309 BETWEEN LONGERONS 18 & 23L. THE DOUBLER WAS REPLACED IAW ETI-88-17-067 R4 AND ER/A 554160-14 REV ORIGINAL.
- [SDR DALA2017022301487](https://openairdocs.org/sdr/DALA2017022301487.md): Doubler · corroded · Feb 22, 2017 · N923DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL CUTOUT DOUBLER AT AFT LAVATORY SERVICE PANEL LOWER AFT CORNER. REPAIRED IAW ETI-88-17-067 REV.4 AND ER/A 554160-14 REV.ORIG.
- [SDR DALA2017022101364](https://openairdocs.org/sdr/DALA2017022101364.md): Frame · cracked · Feb 20, 2017 · N923DL · Doug MD88 · Fuselage Main, Frame
  > AFT ACCESORIES COMPARTMENT. CRACKED FRAME BS 1474 BETWEEN LONGERONS 23 - 25R. THE FRAME WAS REPAIRED IAW SRM 53-01, FIG. 2, 51-30-2,AND 51-30-5.
- [SDR DALA2017022001360](https://openairdocs.org/sdr/DALA2017022001360.md): Frame · cracked · Feb 19, 2017 · N923DL · Doug MD88 · Fuselage Main, Frame
  > AFT ACCESSORY BAY HAD CRACKS ON FRAME BS 1510. THE FRAME WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, AND 51-30-8.
- [SDR DALA2017021901354](https://openairdocs.org/sdr/DALA2017021901354.md): Skin · cracked · Feb 18, 2017 · N923DL · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STABILIZER CRACKED ON THE RAM AIR ACCESS CUTOUT 6301A. REPAIRED IAW SRM 55-05, PAR. 6, FIG. 3.
- [SDR DALA2017021901358](https://openairdocs.org/sdr/DALA2017021901358.md): Angle · corroded · Feb 17, 2017 · N923DL · Doug MD88 · Fuselage Miscellaneous Structure
  > E& E BAY HAD CORROSION ON AN ANGLE, BS 150 AND LONGERON 28R. THE ANGLE WAS REPLACED IAW DWG 9911550 REV: E.
- [SDR DALA2017021701313](https://openairdocs.org/sdr/DALA2017021701313.md): Skin · damaged · Feb 16, 2017 · N923DL · Doug MD88 · Passenger/Crew Doors
  > L1 DOOR SKIN BENDED THE SKIN WAS REPLACED IAW SRM 52-05, FIG 64.
- [SDR DALA2017021701311](https://openairdocs.org/sdr/DALA2017021701311.md): Pan · cracked · Feb 16, 2017 · N923DL · Doug MD88 · Passenger/Crew Doors
  > L1 DOOR HAS A CRACKED PAN AT FWD UPPER CORNER. THE PAN WAS REPAIRED IAW SRM 52-05, FIG 18A.
- [SDR DALA2017021701309](https://openairdocs.org/sdr/DALA2017021701309.md): Angle · cracked · Feb 16, 2017 · N923DL · Doug MD88 · Passenger/Crew Doors
  > L1 DOOR HAS A CRACKED TEE ANGLE AT FWD PASSENGER DOOR INTERNAL STRUCTURE BETWEEN BEAMS 4 AND 5 AND BS 168. THE TEE ANGLE WAS REPLACED IAW DWG 9955763 REV: K, SRM 51-30-2, AND 51-30-5.
- [SDR DALA2017021601275](https://openairdocs.org/sdr/DALA2017021601275.md): Stringer · cracked · Feb 15, 2017 · N923DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > PAX CABIN CRACKED LONG 3L ON STA Y=160. ACCOMPLISH WHIT WORK CARD 5330-01204-04. LONGERON 3L ON STA Y=160 WAS REPAIRED PER SRM 53-02 FIG18 AND 5330-01204-04 JOB 100-0001.
- [SDR DALA2016060704399](https://openairdocs.org/sdr/DALA2016060704399.md): Wire · loose · Jun 6, 2016 · N923DL · Doug MD88 · Light System Wiring
  > FLIGHT CREW REPORTED SMOKE IN THE COCKPIT ON APPROACH; DONNED O2 MASKS. SMOKE WAS COMING FROM UNDERNEATH THE CAPTAINS TAXI LIGHT CONTROL PANEL. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND A LOOSE TERMINAL WIRE AT THE LANDING LIGHT/GROUND FLOOD LIGHT SWITCH P
- [SDR DALA2015082005147](https://openairdocs.org/sdr/DALA2015082005147.md): Battery Pack · inoperative · Aug 20, 2015 · N923DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROWS 2-10 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECKED GOOD.
- [SDR DALA2015071104299](https://openairdocs.org/sdr/DALA2015071104299.md): Skin · cracked · Jul 10, 2015 · N923DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION AND CRACKED BELLY SKIN AT BS 680, STRINGERS 29 - 30L, REPAIRED THE SKIN IAW ERA 537463-14, REV ORIG.
- [SDR DALA2015012200527](https://openairdocs.org/sdr/DALA2015012200527.md): Web · corroded · Jan 20, 2015 · N923DL · Doug MD88 · Fuselage Main, Structure
  > C-1 DOOR AFT CUTOUT WEB CORRODED APPROXIMATELY STA 27-434, LONGERONS L-27 AND L-25. BURNISHED AREA C-1 DOOR CUT-OUT WEB STA 427 TO 434, LONGERON L-27 TO L-25 AND ALODINED AREA. C/W UT OF AREA WITH ORIG 0.040 REM MAT 0.030 IAW NDTM P. 4 CA 04-00-07 A 9710. EVAL
- [SDR DALA2015011500337](https://openairdocs.org/sdr/DALA2015011500337.md): Pulley Bracket · worn · Jan 14, 2015 · N923DL · Doug MD88 · Aerodynamic Fairings
  > LEFT PULLEY BRACKET, TAIL CONE RELEASE CABLE, GUARD PIN HOLE WORN. R & R PULLEYS BRACKET FOR TAIL CONE RELEASE CABLE AT LOWER LEFT IAW SRM 51-30-02 AND SRM 51-30-01.
- [SDR DALA2015012200539](https://openairdocs.org/sdr/DALA2015012200539.md): Frame · cracked · Jan 8, 2015 · N923DL · Doug MD88 · Passenger/Crew Doors
  > DOOR FRAME CRACKED INSIDE L-1 DOOR AT UPPER AFT CORNER. REMOVED L-1 DOOR IAW AMM 52-11-00-401, STEP 1A-2A5. INSTALLED SERVICEABLE L1 DOOR IAW AMM 52-11-00-501. PERFORMED SATISFACTORY RIG & LEAK/PRESSURE CHECK IAW AMM 52-11-00.
- [SDR DALA2015012600636](https://openairdocs.org/sdr/DALA2015012600636.md): Skin · damaged · Dec 27, 2014 · N923DL · Doug MD88 · Fuselage Main, Plate/Skin
  > SKIN FOUND DENT AND SCRATCH AT BS 239 BELOW STRINGER 17L. REPAIRED IAW ERA 531743-14, REV A SEC III.
- [SDR DALA2014070203845](https://openairdocs.org/sdr/DALA2014070203845.md): Wire · broken · Jul 1, 2014 · N923DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROW 6DEF WAS INOPERATIVE. MAINTENANCE FOUND WIRES BROKEN AT THE LIGHT RECEPTACLE. REPLACED THE LIGHT ASSEMBLY AND THE SYSTEM RETURNED TO NORMAL.
- [SDR DALA2015031102095](https://openairdocs.org/sdr/DALA2015031102095.md): Skin · corroded · Apr 30, 2014 · N923DL · Doug MD88 · Fuselage Main, Plate/Skin
  > SIGNS OF CORROSION FOUND ON FUSELAGE LOWER SKIN AND INTERNAL C2 DOOR SURROUND DOUBLER. DAMAGE LOCATED AT STA 617-636 AND BETWEEN LONGERONS 29L AND 29R. DAMAGE CUT OUT AND REPAIRED IAW SECTION I OF ER/A 525291-14.
- [SDR DALA2015031102096](https://openairdocs.org/sdr/DALA2015031102096.md): Skin · corroded · Apr 14, 2014 · N923DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON SKIN AT TCAS ANTENNA LOCATION. PERMANENT REPAIR ACCOMPLISHED IAW ER/A 525060-14.
- [SDR DALA14010450923](https://openairdocs.org/sdr/DALA14010450923.md): Light · inoperative · Feb 15, 2014 · N923DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHT IN COCKPIT AND AT DOORS L1 & L2 WERE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLIES, REPLACED BULBS, AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.
- [SDR DALA13062390923](https://openairdocs.org/sdr/DALA13062390923.md): Wire · shorted · Nov 17, 2013 · N923DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT IN AFT CABIN. MAINTENANCE FOUND A SHORT IN THE WIRES IN THE TAIL AND REPAIRED WIRES.
- [SDR DALA13042520923](https://openairdocs.org/sdr/DALA13042520923.md): Bulkhead · cracked · Aug 30, 2013 · N923DL · Doug MD88 · Fuselage Main, Bulkhead
  > MX DISCOVERED THAT THE EMERGENCY ESCAPE PATH TAILCONE RELEASE ALIGNMENT PIN BULKHEAD SKIN WAS CRACKED. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYS AND COULD HAVE AN ADVERSE AFFECT ON THE EVACUATION ROUTE IF IT PREVENTED PROPER DEPLOYMENT OF THE TAI
- [SDR DALA13042500923](https://openairdocs.org/sdr/DALA13042500923.md): Pin · worn · Aug 30, 2013 · N923DL · Doug MD88 · Aerodynamic Fairings
  > MX DISCOVERED THAT THE RELEASE LATCH "TEE PIN" FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE T-PINS WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.
- [SDR DALA13042490923](https://openairdocs.org/sdr/DALA13042490923.md): Release Cable · frayed · Aug 30, 2013 · N923DL · Doug MD88 · Aerodynamic Fairings
  > MX DISCOVERED THAT THE TAILCONE KEVLAR RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.
- [SDR DALA13042480923](https://openairdocs.org/sdr/DALA13042480923.md): Spring · missing · Aug 30, 2013 · N923DL · Doug MD88 · Fuselage Miscellaneous Structure
  > MX DISCOVERED THAT THE TEE PIN SPRINGS WERE MISSING AND REQUIRED REPLACEMENT.
- [SDR DALA13042730923](https://openairdocs.org/sdr/DALA13042730923.md): Release Cable · broken · Aug 29, 2013 · N923DL · Doug MD88 · Aerodynamic Fairings
  > MX DISCOVERED THAT THE EMERGENCY ESCAPE PATH TAILCONE RELEASE CABLE WAS BROKEN. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYS AND COULD HAVE AN ADVERSE AFFECT ON THE EVACUATION ROUTE IF IT PREVENTED PROPER DEPLOYMENT OF THE TAILCONE. THIS NOT IN COMP
- [SDR DALA13042510923](https://openairdocs.org/sdr/DALA13042510923.md): Arm · out of rig · Aug 29, 2013 · N923DL · Doug MD88 · Aerodynamic Fairings
  > MX DISCOVERED THAT THE TAILCONE RELEASE ARM WAS OUT OF ALLOWABLE RIG LIMITS. THE AFT TAILCONE RELEASE ARM WAS ADJUSTED TO GET PIN CLEARANCE FROM THE DOOR STOP AND THE SYSTEM WAS RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.
- [SDR DALA13040390923](https://openairdocs.org/sdr/DALA13040390923.md): Connector · loose · Aug 20, 2013 · N923DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MX FOUND EMERGENCY LIGHTS AT ROW 18D IN CABIN INOPERATIVE. FOUND CONNECTOR LOOSE, CONNECTED IT, AND FUNCTIONALLY CHECKED SYSTEM.
- [SDR DALA13040380923](https://openairdocs.org/sdr/DALA13040380923.md): Power Supply · inoperative · Aug 20, 2013 · N923DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND OVERHEAD EMERGENCY PATHWAY LIGHTING FOR CATWALK IN TAIL WAS INOPERATIVE. MX REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA13026850923](https://openairdocs.org/sdr/DALA13026850923.md): Battery · inoperative · Jun 3, 2013 · N923DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT BOTH THE FWD AND THE AFT OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MX REPLACED THE BATTERIES IN BOTH BATTERY PACKS AND THE LIGHTS RETURNED TO AN OPS CONDITION.
- [SDR DALA1213210923](https://openairdocs.org/sdr/DALA1213210923.md): Longeron Splice · cracked · Mar 4, 2012 · N923DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > LONGERON 29L SPLICE IS CRACKED AT STA 1193-1211. REMOVED SPLICE ON LONGERON 29L AT STA 1193-1211 IAW MD80 SRM 51-30-5 PG 12 AND 29. TP BE REPAIRED ON NRC 202495.
- [SDR DALA1218500923](https://openairdocs.org/sdr/DALA1218500923.md): Fitting · chafed · Feb 28, 2012 · N923DL · Doug MD88 · Nacelle/Pylon, Bulkhead/Firewall
  > NR 2 PYLON AT NAC 201 I/B LOWER SIDE BULKHEAD FITTING EXTERIOR CHAFED. BLENDED DAMGAED AREA, FOUND TO BE OUT OF LIMITS. REPAIR TO BE ACCOMPLISHED PER PRI 501029-14 REV 0 & 1.
- [SDR DALA1216570923](https://openairdocs.org/sdr/DALA1216570923.md): Frame · cracked · Feb 27, 2012 · N923DL · Doug MD88 · Fuselage Main, Frame
  > MAIN CABIN STA 1117 LONGERON 7L FRAME IS CRACKED. CUT OUT DAMAGED AREA IAW MD80 SRM 53-03D FIG 4. FABRICATED REPAIR PART 2 EA ANGLE REPAIR AND FILLER REPAIR IAW MD80 SRM 53-03D FIG 4 AND INSTALLED PER MD80 SRM 51-30-2 PARA 1 PG 1, MD80 SRM 51-30-5 PARA 1 PG
- [SDR DALA1212910923](https://openairdocs.org/sdr/DALA1212910923.md): Cusp Web · corroded · Feb 27, 2012 · N923DL · Doug MD88 · Fuselage Miscellaneous Structure
  > LT CUSP WEB AT STA 834 LBL 58 IN MAIN CABIN IS CORRODED. FOUND TO BE OUT OF LIMITS IAW MD80 SRM 53-01 PG 8 FIG 1. FABRICATED AND INSTALLED FILLER SPLICE DOUBLER AND RING DOUBLER PER MD80 SRM 51-30-2 PG 24 DURING HMV ON NRC 197383.
- [SDR DALA1212520923](https://openairdocs.org/sdr/DALA1212520923.md): Floor Support · corroded · Feb 26, 2012 · N923DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON MAIN CABIN FLOOR SUPPORT ATTACH ANGLE STA 200 RBL 42. FOUND TO BE OUT OF LIMITS IAW MD80 SRM 53-01 PG 8 FIG 1. FABRICATED AND INSTALLED FLOOR SUPPORT ANGLE ON MAIN CABIN AT STA 200 RBL 42 IAW MD80 SRM 51-30-01 FIG 1 PGS 1, 2 AND 3 AT SAA DURING
- [SDR DALA1215450923](https://openairdocs.org/sdr/DALA1215450923.md): Longeron · cracked · Feb 24, 2012 · N923DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > IN CABIN FUSELAGE LONGERON 3L IS CRACKED AT STA 160. BLENDED DAMAGE SECTION, FABRICATED AND INSTALLED LONGERON REPAIR AND SPLICE IAW DC9/MD80 SRM 53-02 DURING HMV.
- [SDR DALA1212510923](https://openairdocs.org/sdr/DALA1212510923.md): Floor Support · corroded · Feb 23, 2012 · N923DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON MAIN CABIN FLOOR SUPPORT MOUNT TRACK STA 188 RBL 4. FOUND FLOOR SUPPORT STA 188 RBL 44 OUT OF LIMITS IAW MD80 SRM 53-01 FIG 1 SHEET 3 PG 8. FABRICATED AND INSTALLED FLOOR SUPPORT AT STA 188 RBL 44 IAW MD80 SRM 51-30-5 PG 12 AT DURING HMV ON.
- [SDR DALA1213190923](https://openairdocs.org/sdr/DALA1213190923.md): Cusp Web · corroded · Feb 21, 2012 · N923DL · Doug MD88 · Fuselage Miscellaneous Structure
  > MAIN CABIN RT CUSP WEB HAS CORROSION FROM STA 503-525 INCLUDING THE PREVIOUS REPAIR DOUBLER AT STA 511. REMOVED CORROSION CUSP WEB AREA FROM STA 503-525. MATERIAL LOST FOUND TO BE OUT OF LIMITS IAW MD80 SRM 53-01 FIG 1 SHEET 3. CUT OUT DAMAGE AREA IAW DWG S
- [SDR DALA1212900923](https://openairdocs.org/sdr/DALA1212900923.md): Seat Track · corroded · Feb 20, 2012 · N923DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK AT RBL 22 HAS CORROSION FROM SEAT TRACK PLUG AT STA 433-797. FOUND STA 498.5-499.5 AND STA 597-598 TO BE OUT OF LIMITS IAW MD80 SRM 51-10-01 FIG 26. INSTALLED NEW SECTION OF TRACK RBL 22 STA 493-609 AND 2 EA SPLICES AND REPAIR PLATES IA
- [SDR DALA1212870923](https://openairdocs.org/sdr/DALA1212870923.md): Floor Support · gouged · Feb 20, 2012 · N923DL · Doug MD88 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE IS GOUGED AT STA 826 LBL 17-RBL 17. FOUND TO BE OUT OF LIMITS IAW DC9/MD80 SRM 53-01 FIG 1 PG 8. FABRICATED AND INSTALLED FLOOR SUPPORT IAW DC9/MD80 SRM 51-30-5 PARAGRAPH 7 ON NRC 202315. (NRC 202315)
- [SDR DALA1212530923](https://openairdocs.org/sdr/DALA1212530923.md): Seat Track · corroded · Feb 19, 2012 · N923DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN STA 1098-1088 BL22L SEAT TRACK HAS CORROSION. FOUND OUT OF LIMITS IAW MD80 SRM 53-05 FIG 4B 1 SECTION D-D SHEET 2 PG 28. REPAIR TO BE ACCOMPLISHED ON NRC 202469.
- [SDR DALA1210750923](https://openairdocs.org/sdr/DALA1210750923.md): Seat Track · corroded · Feb 19, 2012 · N923DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN STA 454 TO 456 BL L22 SEAT TRACK HAS CORROSION. REMOVED CORROSION AT STA 454-456 L22 SEAT TRACK, FOUND TO BE OUT OF LIMITS.

Next page: https://openairdocs.org/deregistered/N923DL-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 = 'N923DL' AND deregistration_id = 'N923DL-2019-04-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N923DL-2019-04-08/reports

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