# Service difficulty reports: N909DL, cancelled Dec 6, 2018

A list on [N909DL, cancelled Dec 6, 2018](https://openairdocs.org/deregistered/N909DL-2018-12-06.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 · 119 reports

- [SDR DALA2015030601920](https://openairdocs.org/sdr/DALA2015030601920.md): None · none · Mar 5, 2015 · N909DL · Doug MD88 · Standard Practices/Structures
  > DURING THE LANDING, THE ACFT SKIDDED TO THE LT AND DEPARTED THE RUNWAY. MAINTENANCE AND DAMAGE EVALUATION IS IN PROGRESS.
- [SDR DALA2015010200010](https://openairdocs.org/sdr/DALA2015010200010.md): Eyebolt · unsecure · Jan 1, 2015 · N909DL · Doug MD88 · Elevator Control System
  > CREW PERFORMED AN AIR TURN BACK FOLLOWING EXCESSIVE CONTROL PRESSURES REQUIRED ON THE ELEVATOR AND STABILIZER TRIM, NOSE DOWN TO MAINTAIN INTENDED LONGITUDINAL FLIGHT. MAINTENANCE FOUND THE RT ELEVATOR POWER BOOST CYLINDER EYEBOLT NOT SECURED TO THE ELEVATOR.
- [SDR DALA2014110706003](https://openairdocs.org/sdr/DALA2014110706003.md): Connector · unsecure · Nov 7, 2014 · N909DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 16D IN THE CABIN WAS INOPERATIVE. MAINTENANCE CORRECTED A LOOSE CONNECTION AND THEN OPERATIONALLY CHECKED THE SYSTEM.
- [SDR DALA2014092105152](https://openairdocs.org/sdr/DALA2014092105152.md): Spar Cap · cracked · Sep 18, 2014 · N909DL · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > RT HORIZONTAL STABILIZER REAR SPAR UPPER CAP INBD END, 1EA CRITICAL FASTENER HOLE, UPPER-OTBD, HAS A CRACK APPROXIMATELY.2500" LONG. REMOVED REAR, UPPER & LOWER SPAR ASSY AT RT HORIZONTAL STABILIZER CUT REAR UPPER SPAR SECTION, 34". MATCH DRILLED, TRIMMED
- [SDR DALA2014092105151](https://openairdocs.org/sdr/DALA2014092105151.md): Spar · cracked · Sep 18, 2014 · N909DL · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > HORIZONTAL STABILIZER REAR SPAR FOUND CRACKED. HFEC AREA ONE CRACK, NOTED, REMOVED UPPER & LOWER REAR SPAR ASSY, CUT DAMAGED AREA DIM: 34", MATCH DRILL & TRIMMED NEW UPPER CHORD SECTION -13, REPLACEMENT. LOCATED, DRILLED, DEBURRED, TREATED, PRIMED & INSTALLE
- [SDR DALA2014092505241](https://openairdocs.org/sdr/DALA2014092505241.md): Skin · dented · Sep 11, 2014 · N909DL · Doug MD88 · Passenger/Crew Doors
  > L1 DOOR EXTERIOR, SKIN DENTED. CUT OUT DAMAGE. FABRICATED REPAIR DOUBLER, FILLER, TREATED AND PRIMED REPAIR. INSTALLED IAW 52-05, FIG 37, SHEET 1, SRM 51-10-03, SRM 51-10-04.
- [SDR DALA2014071404095](https://openairdocs.org/sdr/DALA2014071404095.md): Battery Pack · inoperative · Jul 13, 2014 · N909DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING FROM THE L2 DOOR TO ROW 27 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECKED GOOD.
- [SDR DALA14031870909](https://openairdocs.org/sdr/DALA14031870909.md): Wire · damaged · May 23, 2014 · N909DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT 22D WAS INOPERATIVE. MAINTENANCE REPLACED THE PIGTAIL AT 22D AND THE LIGHTS RETURNED TO AN OPERATIVE STATE.
- [SDR DALA14000910909](https://openairdocs.org/sdr/DALA14000910909.md): Power Supply · inoperative · Jan 7, 2014 · N909DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS IN ROWS 17-20 INOPERATIVE. REPLACED THE POWER SUPPLY AND OPS CHECKED GOOD.
- [SDR DALA13063530909](https://openairdocs.org/sdr/DALA13063530909.md): Battery Pack · inoperative · Nov 23, 2013 · N909DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, NOTED EMERGENCY LIGHTS ABOVE AFT OVER WING EXIT DOORS INOPERATIVE. REPLACED BATTERY PACK IN POWER SUPPLY IAW AMM 33-53 AND OPS CHECKED NORMALLY.
- [SDR DALA13038250909](https://openairdocs.org/sdr/DALA13038250909.md): Battery Pack · inoperative · Aug 6, 2013 · N909DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING FOR ROWS 1-4 AND 27-31 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.
- [SDR DALA13013980909](https://openairdocs.org/sdr/DALA13013980909.md): Pan · corroded · Mar 29, 2013 · N909DL · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT LAV SERVICE PANEL PAN CORRODED AT TWO SPOTS ALONG LOWER EDGE. REPAIR INSTALLED IAW STEP 6 OF ER/A 513184-14, REV 2.
- [SDR DALA13013800909](https://openairdocs.org/sdr/DALA13013800909.md): Longeron · corroded · Mar 28, 2013 · N909DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED MX, LONGERON 22L END FITTING WAS FOUND TO BE CORRODED. REPLACED LONGERON FITTING IAW DWG 4914954-1.
- [SDR DALA13013100909](https://openairdocs.org/sdr/DALA13013100909.md): Clamp · loose · Mar 24, 2013 · N909DL · Doug MD88 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MX, THE CABLE CLAMPS FOR THE TAILCONE CABLE CONDUIT WERE FOUND TO BE LOOSE AT BS 1510 AT THE 7:00 POSITION. REPLACED CLAMPS IAW AMM 53-53-00.
- [SDR DALA13013620909](https://openairdocs.org/sdr/DALA13013620909.md): Cam · worn · Mar 21, 2013 · N909DL · Doug MD88 · Aerodynamic Fairings
  > DURING SCHEDULE MX, TAILCONE CAM BASE RAMP WAS FOUND TO BE WORN & GROOVED. INSTALLED SERVICEABLE CAM ASSY AND RIGGED IAW AMM 53-53-02 AND AMDS CARD 5350-01077-0101, STEP 7.
- [SDR DALA13013140909](https://openairdocs.org/sdr/DALA13013140909.md): Bracket · worn · Mar 21, 2013 · N909DL · Doug MD88 · Aerodynamic Fairings
  > DURING SCHEDULED MX, THE TAILCONE SPRING MOUNT BRACKET ON LT SIDE WAS FOUND TO BE WORN AT THE LT SPRING MOUNT. REPLACED THE LT TAILCONE SPRING MOUNT BRACKET IAW SRM 51-30.
- [SDR DALA13013130909](https://openairdocs.org/sdr/DALA13013130909.md): Pin · loose · Mar 21, 2013 · N909DL · Doug MD88 · Aerodynamic Fairings
  > DURING SCHEDULED MX, THE TAILCONE GUIDE PIN WAS FOUND TO BE LOOSE AT THE 2:00 POSITION AT STA 1510. RETORQUED TAILCONE GUIDE PIN AT 2:00 POSITION IAW AMM 20-30-01. REQUIRED INSPECTION COMPLETED.
- [SDR DALA13013120909](https://openairdocs.org/sdr/DALA13013120909.md): Receptacle · worn · Mar 21, 2013 · N909DL · Doug MD88 · Aerodynamic Fairings
  > DURING SCHEDULED MX, THE TAILCONE RECEPTACLES WERE FOUND TO BE WORN OR LOOSE IN SEVERAL LOCATIONS. CORRECTIVE ACTION: REMOVED AND REPLACED TAILCONE RECEPTACLES PER MD88 SRM 51-30. REQUIRED INSPECION COMPLETED (LP 0790899)
- [SDR DALA13013110909](https://openairdocs.org/sdr/DALA13013110909.md): Latch · worn · Mar 21, 2013 · N909DL · Doug MD88 · Aerodynamic Fairings
  > DURING SCHEDULED MX, THE TAILCONE LOWER LATCHES ON LT AND RT SIDE WERE NOTED TO BE WORN AND DO NOT RETURN TO THEIR LOCKED POSITION. R & R SPRINGS ON LT AND RT LOWER LATCHES IAW AMM 53-53-00. REQUIRED INSPECTIONS COMPLETED.
- [SDR DALA13009370909](https://openairdocs.org/sdr/DALA13009370909.md): Door Frame · damaged · Feb 24, 2013 · N909DL · Doug MD88 · Fuselage Main, Structure
  > RIGHT WHEEL WELL FWD MLG DOOR FRAME HAS 3 INCH CRACK BELOW DOOR PROXIMITY SENSOR. REMOVED RT MLG FWD DOOR FRAME DAMAGED SECTION. INSTALLED RT MLG FWD DOOR FRAME SECTION IAW DWG 5930584. R & R RT MLG DOOR OPEN SENSOR IAW AMM32-60.
- [SDR DALA1228730909](https://openairdocs.org/sdr/DALA1228730909.md): Tail Cone · out of limits · Apr 22, 2012 · N909DL · Doug MD88 · Aerodynamic Fairings
  > DURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM, MAINTENANCE FOUND THE GAP BETWEEN PIN AND ROD WAS BEYOND ALLOWABLE LIMITS. THE PIN WAS ADJUSTED AND BROUGHT WITHIN LIMITS AND THE RII COMPLETED.
- [SDR DALA1228720909](https://openairdocs.org/sdr/DALA1228720909.md): Release Cable · out of limits · Apr 22, 2012 · N909DL · Doug MD88 · Aerodynamic Fairings
  > PERFORMED TAILCONE RELEASE SYSTEM OPERATIONAL CHECK (6908) AND FOUND THE TAILCONE EXTERIOR RELEASE CABLE WAS OUT OF ALLOWABLE LIMITS. THIS DISCREPANCY WAS LOCATED AT THE CLAMP TO THE INTERIOR RELEASE CABLE SYSTEM. THE CABLE WAS ADJUSTED AND RIGGED BACK INTO
- [SDR DALA1162360909](https://openairdocs.org/sdr/DALA1162360909.md): Connector · loose · Nov 8, 2011 · N909DL · Doug MD88 · Light System Wiring
  > SEAT 23D AND 28D EMERGENCY LIGHTS INOPERATIVE. FOUND LOOSE CONNECTORS AT LIGHT ASSEMBLIES. SECURED CONNECTORS. OPS CHECK GOOD.
- [SDR DALA1157330909](https://openairdocs.org/sdr/DALA1157330909.md): Skin · cracked · Oct 9, 2011 · N909DL · Doug MD88 · Fuselage Main, Plate/Skin
  > STA 1437 SKIN CRACKED AT 4 LOCATIONS BETWEEN L2L-L5L BELOW VERTICAL ATTACH ANGLES. REPAIRED ON N/R 105 PER ERA 496705-14 REV O.
- [SDR DALA1157320909](https://openairdocs.org/sdr/DALA1157320909.md): Tee Fitting · bent · Oct 9, 2011 · N909DL · Doug MD88 · Fuselage Main, Bulkhead
  > DURING PSV CHECK THE APB TEE 5910130-387 WAS FOUND DEFORMED AND BENT UPWARD. REPAIRED PER ERA 496691-14.
- [SDR DALA1157230909](https://openairdocs.org/sdr/DALA1157230909.md): Skin · cracked · Oct 8, 2011 · N909DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT STA 1437 FROM L-2R TO L-5R 2 EACH CRACKS. DAMAGED REMOVED AND PERMANENT REPAIR INSTALLED PER ER/A 496706-14.
- [SDR DALA1156840909](https://openairdocs.org/sdr/DALA1156840909.md): Skin · bent · Oct 4, 2011 · N909DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING PSV, FOUND FUSELAGE SKIN AT C3 CARGO DOOR CUTOUT BS 1211 BETWEEN L22-24R, BENT OUTWARD. REPAIRED IAW ERA 496767-14.
- [SDR DALA1156830909](https://openairdocs.org/sdr/DALA1156830909.md): Tee Fitting · damaged · Oct 4, 2011 · N909DL · Doug MD88 · Fuselage Main, Bulkhead
  > DURING PSV, FOUND DAMAGE TO AFT PRESSURE BULKHEAD TEE, CUT AND REMOVED SECTION OF ANGLE. REPAIRED IAW ERA 496732-14.
- [SDR DALA1124080909](https://openairdocs.org/sdr/DALA1124080909.md): Line · leaking · Apr 3, 2011 · N909DL · Doug MD88 · Engine Thrust Reverser
  > DURING TAKEOFF AND CLIMB THE CREW REPORTED AN ACRID/OIL SMELL IN CABIN AND COCKPIT AND SMOKE IN THE COCKPIT. NO OVERHEAT INDICATIONS INDICATED FOR ENGINES OR PACKS. SMOKE CLEARED PRIOR TO LANDING. MAINTENANCE FOUND LEAKING LINE ON LEFT T/R CONTROL VALVE. M
- [SDR DALA1119100909](https://openairdocs.org/sdr/DALA1119100909.md): Battery · dislodged · Mar 14, 2011 · N909DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK MAINTENANCE FOUND EMERGENCY PATH LIGHTS AT 26ED INOPERATIVE AND LEFT AND RIGHT AFT OVERWING EXIT SIGNS INOPERATIVE. MAINTENANCE FOUND THE BATTERY DISLODGED FROM ASSEMBLY AND RE-INSTALLED THE BATTERY. OPERATION OF LIGHTS NOW CHECKS GOOD.
- [SDR DALA1115820909](https://openairdocs.org/sdr/DALA1115820909.md): Slide · misrouted · Mar 6, 2011 · N909DL · Doug MD88 · Escape Slide
  > DURING LINE CHECK, MX FOUND L1 DOOR SLIDE LANYARD MISROUTED. MX REROUTED THE LANYARD IAW MM.
- [SDR DALA1115810909](https://openairdocs.org/sdr/DALA1115810909.md): Slide · misrigged · Mar 6, 2011 · N909DL · Doug MD88 · Escape Slide
  > DURING LINE CHECK MX, FOUND L2 DOOR SLIDE LANYARD NOT ATTACHED TO GIRT BAR. MX REATTACHED THE SLIDE LANYARD IAW MM.
- [SDR DALA1103280909](https://openairdocs.org/sdr/DALA1103280909.md): Guard · misinstalled · Jan 17, 2011 · N909DL · Doug MD88 · Wing Main, Frame Structure
  > DURING LINE MX CHECK FOUND A FLIGHT CONTROL CABLE GUARD INCORRECTLY INSTALLED AND WITH HARDWARE MISSING. 4 CONTROL CABLES THAT RUN NEXT TO THE LT SIDE CATWALK ON THE AFT 48 SECTION. WERE ROUTED THRU THE OUTSIDE OF THE CABLE GUARD INSTEAD OF THE INSIDE. THE
- [SDR DALA1100010909](https://openairdocs.org/sdr/DALA1100010909.md): Longeron · corroded · Jan 1, 2011 · N909DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV4, FOUND AFT CARGO STA 1285-1308 LONG 22L HAS MAJOR CORROSION. REMOVED CORROSION FROM L22L IAW SRM 53-01, FIG 1 (.5 X 1.5) ORIGINAL MAT.125 IAW SRM 53-14-3, FIG 4 AND 51-10-1, FIG 15. REMOVED 0.075. REMAINING MAT.050. FOUND TO BE OUT OF LIMITS.
- [SDR DALA1053590909](https://openairdocs.org/sdr/DALA1053590909.md): Shear Tie · cracked · Dec 29, 2010 · N909DL · Doug MD88 · Fuselage Internal Mounting Structure
  > DURING HMV4, FOUND AFT ACCESSORY STA 1437 L2L VERTICAL STAB FITTING OTBD SHEAR TIE CRACKED AT FASTENERS. R & R SHEAR TIE FABBED FROM 7075-T6 0.071 INSTALLED SHEAR TIE.
- [SDR DALA1053570909](https://openairdocs.org/sdr/DALA1053570909.md): Pan · cracked · Dec 29, 2010 · N909DL · Doug MD88 · Fuselage Miscellaneous Structure
  > DURING HMV4, FOUND NR3 CARGO DOOR INNER PAN CRACKED AT NR4 BEAM FWD SIDE. STOPPED DRILLED CRACK NDT HFEC INSPECTED STOP DRILL IAW NDT 06-10-01.001. NO CRACK NOTED, A2700 RECEIVED REPAIR DOUBLER FROM HEAT TREAT ON TRAVELER 2310N02631. INSTALLED IAW SRM 52-05
- [SDR DALA1053560909](https://openairdocs.org/sdr/DALA1053560909.md): Rib · cracked · Dec 29, 2010 · N909DL · Doug MD88 · Leading Edge Devices
  > DURING HMV4, FOUND LT WING NR4 SLAT CUTOUT RIB IS CRACKED. ACCOMPLISHED PERMANENT REPAIR IN COMPLIANCE WITH ER/A 472719-14MA AND DWG AMR0957267. TAGGED AND EDGE SEALED REPAIR IAW DPS 900-5-1 NR 04.
- [SDR DALA1053550909](https://openairdocs.org/sdr/DALA1053550909.md): Cusp Web · corroded · Dec 29, 2010 · N909DL · Doug MD88 · Fuselage Miscellaneous Structure
  > DURING HMV4, FOUND MAIN PASSENGER CABIN BETWEEN STA 1041 AND 1060 RT CUSP WEB HAS CORROSION UPPER AND LOWER SURFACE. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER AFTER REMOVING DAMAGE IAW SRM 53-14-3, FIG 12 AND DRD 53-05D.
- [SDR DALA1053540909](https://openairdocs.org/sdr/DALA1053540909.md): Skin · dented · Dec 29, 2010 · N909DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV4, FOUND FUSELAGE EXTERIOR STA 1090 BETWEEN L16L AND L17L SKIN HAS DENT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER IAW DWG SG0953002.
- [SDR DALA1053530909](https://openairdocs.org/sdr/DALA1053530909.md): Skin · cracked · Dec 29, 2010 · N909DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV4, FOUND FUSELAGE EXTERIOR STA 1429 BETWEEN L2R AND L3R SKIN CRACKED AT FASTENER. STOP DRILLED CRACK AND REPAIR DOUBLER MADE IAW SRM 53-01, FIG 2, FABBED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW SRM 53-01, FIG 2, 51-30-5, 51-30-02.
- [SDR DALA1053520909](https://openairdocs.org/sdr/DALA1053520909.md): Longeron · corroded · Dec 29, 2010 · N909DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV4, FOUND AFT ACCESSORY STA 1380, 1401, 1418 L24L HAS CORROSION AND CRACKS. REMOVED DAMAGED SECTION OF LONGERON BETWEEN 1380 AND 1429 DUE TO 100PERCENT MAT LOSS. REPLACED DAMAGED LONGERON FROM 1380 TO 1428, L24L IAW SRM 51-10-4.
- [SDR DALA1053510909](https://openairdocs.org/sdr/DALA1053510909.md): Frame · corroded · Dec 29, 2010 · N909DL · Doug MD88 · Fuselage Main, Frame
  > DURING HMV4, FOUND AFT CARGO STA 1287, L28-30R HAS CORROSION. REMOVED CORROSION ON L28 AND L29 FOUND TO BE WITHIN LIMITS IAW SRM 53-01, FIG 1. FOUND L30 TO BE OUT OF LIMITS. FABBED U CHANNEL REPAIR IAW SRM 53-02, FIG 19. LOCATED, DRILLED AND DEBURRED IAW S
- [SDR DALA1053500909](https://openairdocs.org/sdr/DALA1053500909.md): Longeron · corroded · Dec 29, 2010 · N909DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV4, FOUND AFT CARGO COMPT STA 1206-1200 L28L, INBD AND OTBD BOTTOM CORRODED. REMOVED CORROSION IAW SRM 51-10-3, 100 PERCENT MAT LOSS. R & R LONGERON 28L IAW SRM 51-10-4, 51-30-5, 51-30-2.
- [SDR DALA1053490909](https://openairdocs.org/sdr/DALA1053490909.md): Frame · cracked · Dec 29, 2010 · N909DL · Doug MD88 · Fuselage Main, Frame
  > DURING HMV4, FOUND MAIN PASSENGER CABIN STA 1312 RT SIDE LONGERON 17, FRAME CRACKED. R & R FRAME PN 9958238U7 IAW SRM 53-03D, FIG 32, SHT 2-3.
- [SDR DALA1053480909](https://openairdocs.org/sdr/DALA1053480909.md): Longeron · corroded · Dec 29, 2010 · N909DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV4, FOUND AFT CARGO STA 1321, L25L HAS CORROSION UNDER FRAME. REMOVED CORROSION UNDER FRAME STA 1321 L25L FOUND OUT OF LIMITS. REPLACED L25L AT STA 1276 TO 1338 IAW SRM 51-30-2, 51-30-5
- [SDR DALA1053470909](https://openairdocs.org/sdr/DALA1053470909.md): Longeron · corroded · Dec 29, 2010 · N909DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV4, FOUND AFT CARGO L23L HAS CORROSION STA 1308 ON BOTTOM OF LONGERON. REMOVED CORROSION, FOUND OUT OF LIMITS, R & R LONGERON AT STA 1308 IAW SRM 51-30-2, 51-30-5. FASTENERS INSTALLED ALSO IAW DWG 5936667 SHT1.
- [SDR DALA1053450909](https://openairdocs.org/sdr/DALA1053450909.md): Skin · corroded · Dec 29, 2010 · N909DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV4, FOUND CORROSION BETWEEN LONGERONS 29L AND 29R AT STA 750-765 ON THE FUSELAGE SKIN INNER SURFACE. REMOVED INNER DOUBLER, FOUND TO BE OUT OF LIMITS, FOUND OUTER SKIN TO BE OUT OF LIMITS. CUT OUTER SKIN AND REMOVED DAMAGED AREA IAW DWG SG0953002.
- [SDR DALA1053440909](https://openairdocs.org/sdr/DALA1053440909.md): Cusp Web · corroded · Dec 29, 2010 · N909DL · Doug MD88 · Fuselage Miscellaneous Structure
  > DURING HMV4, FOUND MAIN CABIN STA 1142 GIRT BAR FITTING SUPPORT LT CUSP WEB HAS CORROSION. REMOVED CORROSION 100 PERCENT MAT LOSS. CUTOUT 3"X3.5" IAW DWG SG09530019. FABRICATED DOUBLER FROM 0.040 A286 STAINLESS AND FILLER FROM 0.063 7075-T6 IAW DWG SG0953001
- [SDR DALA1053150909](https://openairdocs.org/sdr/DALA1053150909.md): Skin · gouged · Dec 29, 2010 · N909DL · Doug MD88 · Cargo/Baggage Doors
  > DURING HMV4, FOUND AFT LOWER CARGO DOOR LWR AFT CORNER REPAIR (DOUBLER) CHAFED EXTERIOR BOTTOM END. REMOVED AFT DOUBLER, REMOVED CORROSION FROM DOOR SKIN DOUBLER AREA ORIG MAT THICKNESS 0.050, LOSS 0.006, REMANING 0.044, DOOR SKIN FOUND TO BE WITHIN LIMITS TR
- [SDR DALA1053140909](https://openairdocs.org/sdr/DALA1053140909.md): Skin · gouged · Dec 29, 2010 · N909DL · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > DURING HMV4, FOUND VERTICAL STAB LT SIDE STA YV-170 AND ZV-174 SKIN CUTOUT GOUGED IN RADIUS. MEASURED DEPTH OF GOUGE,.046 MEASURED ORIG MAT. 0.062 IAW SRM 55-32-00, FIG 3, SHT 2. REMAINING MAT. 0.016, FOUND TO BE OUT OF LIMITS IAW SRM 55-01, FIG 1, RECEIVED

Next page: https://openairdocs.org/deregistered/N909DL-2018-12-06/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 = 'N909DL' AND deregistration_id = 'N909DL-2018-12-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N909DL-2018-12-06/reports

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