# Service difficulty reports: N951DL, cancelled Jan 24, 2020

A list on [N951DL, cancelled Jan 24, 2020](https://openairdocs.org/deregistered/N951DL-2020-01-24.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 · 102 reports

- [SDR DALA2019010200018](https://openairdocs.org/sdr/DALA2019010200018.md): Position Switch · out of adjust · Jan 1, 2019 · N951DL · Doug MD88 · Leading Edge Slat Position Indicating System
  > SLAT DISAGREE AT FLAPS 15. T/S FLAP/SLAT HANDLE POS SEITCH REF AMM 22-80 FOUND SWITCH OUT OF ADJUSTMENT, REQUIRES MAINTENANCE. REMOVED AND REPLACED FLAP HANDLE SWITCH PACK ASSY PER AMM 27-80. PERFORMED NR 1 & NR 2 RTS BOTH "GO". SDR REPORTED DUE TO DECLARED EM
- [SDR DALA2018121877255](https://openairdocs.org/sdr/DALA2018121877255.md): Brake · odor · Dec 17, 2018 · N951DL · Doug MD88 · Landing Gear Brake System
  > AFTER LANDING BURNING RUBBER SMELL IN CABIN AND COCKPIT, NO HAZE. FOUND NBR 4 TIRE FLAT SPOT. R/R NBR 4 MLG WHEEL ASSY AND BRAKE ASSY PER MD88 AMM 32-40,32-42. T/S ANTISKID PER MD88 AMM 32-43. CKS GOOD. PERFORMED NO GO ODI PREVENTION SECTION 2172. C/W WC 2120-
- [SDR DALA2018120306970](https://openairdocs.org/sdr/DALA2018120306970.md): Regulator Valve · malfunctioned · Dec 2, 2018 · N951DL · Doug MD88 · Cabin Pressure Control System
  > SHIP 951- PRESS - FLOW LIGHT IN CRUISE. DURING DESCENT PRESSURIZATION COULD NOT KEEP UP. AT 10,000 FEET AIRCRAFT WAS COMPLETELY DEPRESSURIZED UNTIL LANDING. CORRECTIVE ACTION: REPLACED LEFT PRESSURE REGULATING VALVE AND LEFT A/C PILOT PRESSURE REGULATOR. (LP48
- [SDR DALA2018090705496](https://openairdocs.org/sdr/DALA2018090705496.md): Splice · defective · Sep 5, 2018 · N951DL · Doug MD88 · Light System Wiring
  > EMERGENCY LIGHT INOP ROW 25 TO 28 SEATS. FOUND SPLICE BAD AT ROW 28 RT AND 25 RT. REPAIRED BOTH SPLICE IAW AMM 20-50 AND AMM WDM 33-51 OPS CHECK GOOD.
- [SDR DALA2018052003452](https://openairdocs.org/sdr/DALA2018052003452.md): Frame · cracked · May 19, 2018 · N951DL · Doug MD88 · Fuselage Main, Frame
  > WHILE WORKING RT HYD PRESSURE PROBLEM FOUND RT FWD WHEEL WELL FRAME CRACKED 4" BELOW PROX SENSOR. REMOVED DAMAGED FRAME AND BEGAN DRILLED NEW FRAME PER DWG 5930584. INSTALLED NEW FRAME PER DWG 5930584.
- [SDR DALA2018021700972](https://openairdocs.org/sdr/DALA2018021700972.md): Light · inoperative · Feb 17, 2018 · N951DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHT 24ED INOPERATIVE. R & R THE LIGHT ASSY. OPS NORMAL IAW AMM 33-52.
- [SDR DALA2017112108256](https://openairdocs.org/sdr/DALA2017112108256.md): Pin · detached · Nov 20, 2017 · N951DL · Doug MD88 · Escape Slide
  > L1 DOOR SLIDE PIN NOT ATTACHED. R & R THE DOOR SLIDE IAW JIC 5200-0652.
- [SDR DALA2017100507316](https://openairdocs.org/sdr/DALA2017100507316.md): Pin · disengaged · Oct 5, 2017 · N951DL · Doug MD88 · Escape Slide
  > DURING INSPECTION OF THE L1 DOOR MOUNTED ESCAPE SLIDE PIN ENGAGEMENT, PIN NOT ENGAGED. REPLACED THE DOOR SLIDE IAW 2561-4964.
- [SDR DALA2017071705511](https://openairdocs.org/sdr/DALA2017071705511.md): Slide · damaged · Jul 16, 2017 · N951DL · Doug MD88 · Escape Slide
  > FOUND SLIDE PACK UNFOLDING. REMOVED AND REPLACED THE TAILCONE SLIDE PACK.
- [SDR DALA2017032402372](https://openairdocs.org/sdr/DALA2017032402372.md): Unknown · odor · Mar 23, 2017 · N951DL · Doug MD88 · Air Distribution System
  > PASSING 6,000 MSL FLIGHT ATTENDANT CALLED TO REPORT A STRONG PLASTIC BURNING SMELL IN CABIN THAT GOT STRONGER FURTHER BACK IN CABIN. NO SMOKE OR HAZE OBSERVED. FAINT OILY SMELL OBSERVED IN FLIGHT DECK. RAN QRH PAGE 8.6 FOR SMOKE, FIRE OR FUMES. RETURNED TO CVG
- [SDR DALA2017013100762](https://openairdocs.org/sdr/DALA2017013100762.md): Duct · disconnected · Jan 30, 2017 · N951DL · Doug MD88 · Airfoil Anti/De-ice System
  > FLIGHT RETURNED TO ATL DUE TO ODOR AND VISIBLE HAZE IN FIRST CLASS GALLEY AREA. CREW REPORTED WHEN AIRFOIL ANTI-ICE WAS SELECTED ON, A LOUD NOISE WAS HEARD, FOLLOWED BY RUSHING AIR NOISE WITH ASSOCIATED SMOKE/ODOR. AIRFOIL ANTI-ICE WAS SELECTED OFF AND NOISE C
- [SDR DALA2017011800480](https://openairdocs.org/sdr/DALA2017011800480.md): Fitting · cracked · Jan 17, 2017 · N951DL · Doug MD88 · Spoilers
  > DURING LUBRICATION OF GROUND SPOILER ACTUATORS, THE HINGE SUPPORT WAS FOUND CRACKED AT LT WING. HINGE SUPPORT FITTING. THE FITTING WAS REPLACED IAW AMM 20-30-01 AND DC9/MD80 SRM 51-30-1, 51-30-2 AND 51-30-5.
- [SDR DALA2017011700383](https://openairdocs.org/sdr/DALA2017011700383.md): Door Frame · corroded · Jan 16, 2017 · N951DL · Doug MD88 · Fuselage Main, Structure
  > MID CARGO BAY HAD CORROSION ON THE LOWER DOOR FRAME BS 636 - 693. THE DOOR FRAME WAS REPAIRED IAW SRM 53-05 PAR. 140 FIG. 123.
- [SDR DALA2017011600361](https://openairdocs.org/sdr/DALA2017011600361.md): Skin · cracked · Jan 15, 2017 · N951DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACKED SKIN AT FWD AIRSTAIR DOOR FRAME AT AFT LWR CORNER. THE SKIN WAS REPAIRED IAW DWG SR09530031 REV K.
- [SDR DALA2017011500359](https://openairdocs.org/sdr/DALA2017011500359.md): Door Frame · corroded · Jan 14, 2017 · N951DL · Doug MD88 · Fuselage Main, Structure
  > AFT CARGO BAY HAD CORROSION ON LOWER DOOR FRAME BS 1155 - 1212. THE DOOR FRAME WAS REPAIRED IAW SRM 53-05 PAR 140 FIG. 123.
- [SDR DALA2017011500358](https://openairdocs.org/sdr/DALA2017011500358.md): Stringer · cracked · Jan 14, 2017 · N951DL · Doug MD88 · Wing, Longeron/Stringer
  > A CRACK WAS FOUND ON STRINGER 11 LT WING STA XRS =160. THE STRINGER WAS REPAIRED IAW DRAWING SR09570100.
- [SDR DALA2017010900210](https://openairdocs.org/sdr/DALA2017010900210.md): Frame · cracked · Jan 8, 2017 · N951DL · Doug MD88 · Fuselage Main, Frame
  > CRACK ON RT AFT WHEEL WELL FRAME. THE FRAME WAS REPLACED IAW SRM 51-30-2.
- [SDR DALA2016072905652](https://openairdocs.org/sdr/DALA2016072905652.md): Wire Harness · inoperative · Jul 28, 2016 · N951DL · Doug MD88 · Light System Wiring
  > DURING SERVICE CHECK, FOUND SEAT 15E EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY IAW CMM 33-50-63. OPS NORMAL.
- [SDR DALA2016071605362](https://openairdocs.org/sdr/DALA2016071605362.md): Structure · cracked · Jul 15, 2016 · N951DL · Doug MD88 · Wing Miscellaneous Structure
  > CRACK FOUND IN RT WING L/E AT NR 2 SLAT LOCATION. C/W ERA 548916-14 REV ORIGINAL ACCOMPLISHED SEC 1 TIME LIMITED REPAIR. SECTION 2 PERMANENT REPAIR DUE WITHIN 760 DAYS.
- [SDR DALA2016070305057](https://openairdocs.org/sdr/DALA2016070305057.md): Slide · malfunctioned · Jul 2, 2016 · N951DL · Doug MD88 · Escape Slide
  > CABIN SERVICE DEPLOYED TAIL CONE ASSY AND SLIDE DID NOT BLOW. REPLACED TAILCONE EVACUATION SLIDE IAW WC 5350-4287.
- [SDR DALA2016061304603](https://openairdocs.org/sdr/DALA2016061304603.md): Lamp · inoperative · Jun 12, 2016 · N951DL · Doug MD88 · Emergency Lighting
  > DURING SERVICE CHECK, LT OVERWING EMERGENCY LAMP WAS NOT ILLUMINATING. REPLACED THE LAMP AND OPS CHECKED NORMAL.
- [SDR DALA2016061304602](https://openairdocs.org/sdr/DALA2016061304602.md): Battery Pack · inoperative · Jun 12, 2016 · N951DL · Doug MD88 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND OVERWING EMERGENCY LIGHTS REMAINED ILLUMINATED AFTER EMERGENCY POWER REMOVED. REPLACED OVERWING EMERGENCY LIGHTS BATTERY PACK.
- [SDR DALA2016050903840](https://openairdocs.org/sdr/DALA2016050903840.md): Connector · disconnected · May 9, 2016 · N951DL · Doug MD88 · Light System Wiring
  > THE CREW OF FLIGHT 2459, FOUND SEAT 14D EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESEATED A PLUG PIN AND THE LIGHT CHECKED OK.
- [SDR DALA2015102806541](https://openairdocs.org/sdr/DALA2015102806541.md): Light · inoperative · Oct 27, 2015 · N951DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 19D IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.
- [SDR DALA2015010200009](https://openairdocs.org/sdr/DALA2015010200009.md): Intercostal · cracked · Jan 1, 2015 · N951DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL BETWEEN BS 1148 - 1153, LONGERONS 29 - 30R. THE INTERCOSTAL WAS REPLACED IAW DWG 5930483, REV AL, SRM 51-30-2, 51-30-5, AND 51-10-3 PAR 14 AND 21.
- [SDR DALA2015010200008](https://openairdocs.org/sdr/DALA2015010200008.md): Lanyard · frayed · Jan 1, 2015 · N951DL · Doug MD88 · Escape Slide
  > INSPECTION DISCOVERED THAT THE L1 DOOR EMERGENCY ESCAPE SLIDE LANYARD WAS FRAYED. THE SLIDE LANYARD WAS REPLACED.
- [SDR DALA2014122606769](https://openairdocs.org/sdr/DALA2014122606769.md): Cusp Web · corroded · Dec 25, 2014 · N951DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON LEFT CUSP WEB X 54 - 60, BETWEEN BS 859 - 864. CUSP WEB REPARED IAW SRM 51-10-3, PAR 14, 21, 26, 38. 53-05 FIG 131A-1 AND ER/A 511165-14 MA AND 51-30-2.
- [SDR DALA2014072404204](https://openairdocs.org/sdr/DALA2014072404204.md): Channel · broken · Jul 17, 2014 · N951DL · Doug MD88 · Fuselage Miscellaneous Structure
  > MAINTENANCE DISCOVERED THAT THE TAILCONE CATWALK OVER THE VENTRAL STAIRWAY HAD GOTTEN STUCK HALF WAY THROUGH TRANSITION WHEN LOWERING THE STAIRS. CAUSE OF BINDING WAS BROKEN CHANNEL EXTRUSION ON THE STAIR AREA SIDEWALL. THIS IS CONSIDERED A DEFECT IN THE EME
- [SDR DALA14032320951](https://openairdocs.org/sdr/DALA14032320951.md): Battery Pack · inoperative · May 27, 2014 · N951DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT SEVERAL OF THE OVERHEAD EMERGENCY PATHWAY LIGHTS IN THE FWD CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.
- [SDR DALA14007810951](https://openairdocs.org/sdr/DALA14007810951.md): Acm · odor · Feb 7, 2014 · N951DL · Doug MD88 · Cabin Cooling System
  > DURING CLIMB, CREW BEGAN DETECTING FUMES. THE ODOR INCREASED AT CRUISE FLIGHT AND WAS WORSE IN THE REAR CABIN AREA. FLIGHT WAS DIVERTED, WHEN THE FUMES INFILTRATED COCKPIT TO SUCH A DEGREE THAT THE FLIGHT CREW DONNED MASKS. MAINTENANCE REPLACED THE LT AIR CY
- [SDR DALA13062890951](https://openairdocs.org/sdr/DALA13062890951.md): Power Supply · inoperative · Nov 22, 2013 · N951DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, CEILING EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 10-15. REPLACED POWER SUPPLY AND OPS CHECKED GOOD IAW AMM 33-53.
- [SDR DALA13036150951](https://openairdocs.org/sdr/DALA13036150951.md): Skin · cracked · Jul 24, 2013 · N951DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACKED FUSELAGE SKIN BELOW RAM AIR SCOOP BS 1418 BETWEEN LONG 1 AND 2 RT. (VHS) (T0 286773). DAMAGE WAS REMOVED, FILLERS & DOUBLERS WERES FABRICATED, REPAIR PARTS WERE INSTALLED, REPAIR WAS IDENTIFIED, REPAIR WAS ACCOMPLISHED IAW ER/A 516239-14AD REV ORIG
- [SDR DALA13036140951](https://openairdocs.org/sdr/DALA13036140951.md): Heater Blanket · out of limits · Jul 23, 2013 · N951DL · Doug MD88 · Airfoil Anti/De-ice System
  > DURING UT INSPECTION 1 VOID AREA 271 SQ " WAS FOUND ON LT HEATER BLANKET AND IS OUT OF LIMITS IAW CARD 5700-2232, JOB 001-0843, FIG 1, STEP 1(B) (LW) REF (T0 286220) (CARD 21, ZONE 13). LT HEATER BLANKET PANEL WAS REPLACED IAW AMM 30-80-02, PAGE BLOCK 401. R
- [SDR DALA2015011607845](https://openairdocs.org/sdr/DALA2015011607845.md): Skin · cracked · Jul 22, 2013 · N951DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV4, A SID INSPECTION FOUND A TWO INCH CRACK AT BS 1418 BETWEEN L1 AND L2R. THE CRACK WAS REPAIRED. SID AD 2004-11-07 APPLIES. ACCOMPLISH ER/A 88-516239-14 SECTION II DTA REQUIREMENT WITHIN 18 MONTHS OF SECTION I ACCOMPLISHMENT. ASSOCIATED ER/A 88-
- [SDR DALA13035110951](https://openairdocs.org/sdr/DALA13035110951.md): Longeron · cracked · Jul 17, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 2L AT BS 1418 IN AFT ACCESORY COMPARTMENT. CRACKED LONGERON WAS REMOVED AND A NEW LONGERON WAS INSTALLED WITH THE PREVIOUS REPAIR SPLICE, 53-02 FIG 18.
- [SDR DALA13035100951](https://openairdocs.org/sdr/DALA13035100951.md): Longeron · corroded · Jul 17, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 29LT BETWEEN BS 1287 TO 1298 AT AFT CARGO COMPARTMENT. CORROSION REMOVED IAW SRM 51-10-3 PAR 26. AREA FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1 (SHEET 3). DAMAGE AREA WAS REMOVED AND NEW LONGERON SECTION AND REPAIRS WERE INSTALLED IAW 5
- [SDR DALA2014102406956](https://openairdocs.org/sdr/DALA2014102406956.md): Skin · damaged · Jul 16, 2013 · N951DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV 4 A LIGHTNING STRIKE WAS FOUND AND REPAIRED AT FS 906 AND L-3R. THIS REPAIR AFFECTS A PSE.
- [SDR DALA13035650951](https://openairdocs.org/sdr/DALA13035650951.md): Skin · damaged · Jul 16, 2013 · N951DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTING STRIKE ON OUTER FUSELAGE SKIN BETWEEN LONGERON 3-4R BS 693, DAMAGE WAS BLEND OUT AND WAS FOUND OUT OF LIMITS AND AREA WAS REPAIR IAW ER/A 516241-14, REV ORIG AND SRM 53-04-1, PAR 6 (UT) WAS ACCOMPLISHED.
- [SDR DALA13034570951](https://openairdocs.org/sdr/DALA13034570951.md): Longeron · cracked · Jul 14, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 14LT BS 1380 IN AFT ACCESSORY COMPARTMENT. CRACKED LONGERON WAS REMOVED, NEW LONGERON SECTION AND SPLICE WERE INSTALLED. REPAIR LONGERON WAS IDENTIFIED, REPAIR WAS ACCOMPLISHED IAW SRM 53-02, FIG 18.
- [SDR DALA13034560951](https://openairdocs.org/sdr/DALA13034560951.md): Longeron · cracked · Jul 14, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 11LT BS 1380, IN AFT ACCESSORY COMPARTMENT. LONGERON WAS REMOVED, NEW LONGERON AND SPLICE WERE INSTALLED, REPAIR LONGERON WAS IDENTIFIED, REPAIR WAS ACCOMPLISHED IAW SRM 53-02, FIG 18.
- [SDR DALA13034410951](https://openairdocs.org/sdr/DALA13034410951.md): Longeron · damaged · Jul 9, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 2R AT BS 693 AT CABIN FUSELAGE STRUCTURE. DAMAGE LONGERON REMOVED. NEW LONGERON INSTALLED IAW SRM 53-02 FIG 18.
- [SDR DALA13034400951](https://openairdocs.org/sdr/DALA13034400951.md): Longeron · cracked · Jul 9, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 18 RT AT BS 1380 IN AFT ACCESSORY COMPARTMENT. LONGERON WAS REMOVED FROM BS 1370 TO 1395 SPLICES WERE FABRICATED AND INSTALLED. REPAIR WAS IDENTIFIED AND ACCOMPLISHED IAW SRM 53-02, FIG 18.
- [SDR DALA13034390951](https://openairdocs.org/sdr/DALA13034390951.md): Longeron · corroded · Jul 9, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 27 LT BETWEEN BS 1287 TO 1309 AT AFT CARGO COMPARTMENT. DAMAGED LONGERON REMOVED IAW SRM 53-02, FIG 18. NEW SECTION LONGERON AND REPAIR SPLICE INSTALLED IAW SRM 53-02, FIG 18.
- [SDR DALA13034010951](https://openairdocs.org/sdr/DALA13034010951.md): Longeron · cracked · Jul 8, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK AND INADEQUATE SCREW HOLES ON LONGERONS 1 AND 2 LT FROM STA Y=256 TO 275. (FCS) REF (T0 286313) (CARD 204 ZONE 58). LONGERONS 1 & 2 WERE REMOVED, NR 1 FROM STA 256 TO 320 AND NR 2 FROM STA 256 TO 275, NEW LONGERONS AND REPAIR SPLICES WERE INSTALLED IAW S
- [SDR DALA13034080951](https://openairdocs.org/sdr/DALA13034080951.md): Lever · worn · Jul 7, 2013 · N951DL · Doug MD88 · Aerodynamic Fairings
  > DURING A CHECK OF TAILCONE RELEASE SYS, MX FOUND THE LOCKPIN LEVER AND LATCH LEVER WERE WORN BEYOND ALLOWABLE LIMITS. MX REPLACED THE TAILCONE LOCK SYS. THE RII COMPLETED FOLLOWING MX.
- [SDR DALA13033990951](https://openairdocs.org/sdr/DALA13033990951.md): Turnbuckle · corroded · Jul 4, 2013 · N951DL · Doug MD88 · Aerodynamic Fairings
  > MX DISCOVERED THAT THE EMERGENCY ESCAPE PATH TAILCONE RELEASE CABLE HAD CORRODED HARDWARE (TURNBUCKLES). 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
- [SDR DALA13034100951](https://openairdocs.org/sdr/DALA13034100951.md): Cam · worn · Jul 3, 2013 · N951DL · Doug MD88 · Aerodynamic Fairings
  > MX DISCOVERED THAT THE TAILCONE RELEASE CAM BASE WAS WORN OUT OF ALLOWABLE LIMITS. THE CAM BASE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII WAS SATISFACTORY.
- [SDR DALA13034020951](https://openairdocs.org/sdr/DALA13034020951.md): Longeron · cracked · Jul 1, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON NR 3LT AND 4LT, STA Y=160 OF FUSELAGE INTERNAL STRUCTURE. DAMAGED SECTION OF LONGERONS 4LT AND 3LT WERE REMOVED AND NEW SECTIONS OF LONGERONS WERE INSTALLED. REPAIRS WERE IDENTIFIED IAW SRM 53-02, FIG 18 AND 51-10-4. RII COMPLETED.
- [SDR DALA13031880951](https://openairdocs.org/sdr/DALA13031880951.md): Cusp Web · corroded · Jun 26, 2013 · N951DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON RT CUSP WEB UPPER SURFACE BETWEEN BS 1136 AND 1231 X=-54 TO X=-60. CORROSION WAS REMOVED FROM BS 1155 AND 1174. FOUND OUT LIMITS IAW ER/A 511165-14 MA REV A.
- [SDR DALA13035120951](https://openairdocs.org/sdr/DALA13035120951.md): Skin · worn · Jun 22, 2013 · N951DL · Doug MD88 · Fuselage Main, Plate/Skin
  > STRUCTURE STA 953-958 AT RT MLG DOOR. PREVIOUS REPAIR DOUBLER WAS REMOVED IAW SRM 51-30-2. NEW DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, PAR 14, 21.

Next page: https://openairdocs.org/deregistered/N951DL-2020-01-24/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 = 'N951DL' AND deregistration_id = 'N951DL-2020-01-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N951DL-2020-01-24/reports

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