# Service difficulty reports: N780NC, cancelled Jun 17, 2014

A list on [N780NC, cancelled Jun 17, 2014](https://openairdocs.org/deregistered/N780NC-2014-06-17.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 · 153 reports

- [SDR DALA13069740871](https://openairdocs.org/sdr/DALA13069740871.md): Fuse · failed · Dec 16, 2013 · N780NC · Doug DC951 · Emergency Lighting
  > SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED FUSE IN SERVICE DOOR EXIT SIGN IAW AMM 33-52. OPS CHECKED GOOD.
- [SDR DALA13059960871](https://openairdocs.org/sdr/DALA13059960871.md): Fuse · inoperative · Nov 8, 2013 · N780NC · Doug DC951 · Emergency Lighting
  > FIRST CLASS SEATS EMERGENCY LIGHTS OUT. REPLACED FUSE IN BATTERY PACK. OPS CHECKED GOOD IAW WDM 33-51-04.
- [SDR DALA13045940871](https://openairdocs.org/sdr/DALA13045940871.md): Battery Pack · inoperative · Sep 19, 2013 · N780NC · Doug DC951 · Emergency Lighting
  > DURING NON ROUTINE CHECK, FOUND OVERWING EXIT SIGN AFT DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES ON AFT LT AND RT EMERGENCY EXIT LIGHTS AND FUNCTIONAL CHECK WAS NORMAL.
- [SDR DALA13044970871](https://openairdocs.org/sdr/DALA13044970871.md): Tee Fitting · cracked · Sep 14, 2013 · N780NC · Doug DC951 · Fuselage Main, Bulkhead
  > DURING INSPECTION, FOUND AFT PRESSURE BULKHEAD TEE CAP BETWEEN STR 13 TO 14L HAS CRACK INDICATION MEASURED THE TOTAL LENGTH IS 4". REMOVED DAMAGED BULKHEAD TEE SECTION FROM APB LONGERON 7-17 LT. LOCATED & DRILLED NEW TEE SECTION. INSTALLED NEW TEE SECTION A
- [SDR DALA13049340871](https://openairdocs.org/sdr/DALA13049340871.md): Tee Fitting · cracked · Sep 13, 2013 · N780NC · Doug DC951 · Fuselage Main, Bulkhead
  > DURING INSPECTION, THE AFT PRESSURE BULKHEAD TEE WAS FOUND WITH A.5" LONG CRACK AT L14L. REPAIRED IAW ER/A 516484-14AD.
- [SDR DALA13019820871](https://openairdocs.org/sdr/DALA13019820871.md): Battery Pack · inoperative · Apr 28, 2013 · N780NC · Doug DC951 · Emergency Lighting
  > LAST 4 ROWS OF SEAT MOUNTED EMERGENCY LIGHTS INOP. REPLACED BATTERYS AT EMERGENCY EXIT SIGN IAW AMM 33-52. OPS CKS GOOD.
- [SDR DALA13017990871](https://openairdocs.org/sdr/DALA13017990871.md): Wire · exposed · Apr 17, 2013 · N780NC · Doug DC951 · Light System Wiring
  > EMERGENCY LIGHT WIRES EXPOSED BENEATH 12 D AND E. SECURED WIRE RUN.
- [SDR DALA12016450871](https://openairdocs.org/sdr/DALA12016450871.md): Skin · damaged · Dec 14, 2012 · N780NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FS 370 L24-26R, FORWARD EDGE OF FWD CARGO DOOR CUT-OUT, ACFT SKIN DAMAGED IN 4 PLACES. ACCOMPLISHED REPAIR AT FS 370 L24-26R FORWARD EDGE OF FORWARD CARGO DOOR CUT-OUT 4 EA PLACES IAW ERA 509300-14, REV O.
- [SDR DALA12015950871](https://openairdocs.org/sdr/DALA12015950871.md): Skin · damaged · Dec 12, 2012 · N780NC · Doug DC951 · Cargo/Baggage Doors
  > DURING L CHECK, EDGE DAMAGE WAS FOUND AT THE FORWARD EDGE OF THE FORWARD CARGO DOOR BETWEEN L-24R AND L-26R. DAMAGE WAS REPAIRED IAW ER/A 509300-14.
- [SDR DALA12016460871](https://openairdocs.org/sdr/DALA12016460871.md): Skin · bulged · Nov 29, 2012 · N780NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FS 106 - 110 L27R, BELLY SKIN BULGED. ONE PROTRUDING FASTENER HEAD AND ONE FASTENER HEAD PULLING THROUGH SKIN. ACCOMPLISHED REPAIR IAW ERA 509303-14 REV O.
- [SDR DALA12003630871](https://openairdocs.org/sdr/DALA12003630871.md): Wire · broken · Jul 18, 2012 · N780NC · Doug DC951 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTING AT SEAT 11C TO BE INOPERATIVE. MAINTENANCE RETERMINATED THE BROKEN WIRE AND RETURNED THE AIRCRAFT TO SERVICE.
- [SDR DALA12003620871](https://openairdocs.org/sdr/DALA12003620871.md): Wire Harness · inoperative · Jul 18, 2012 · N780NC · Doug DC951 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTING AT SEAT 7C TO BE INOPERATIVE. MAINTENANCE REPLACED THE SEAT WIRE HARNESS AND RETURNED THE AIRCRAFT TO SERVICE.
- [SDR DALA1170509871](https://openairdocs.org/sdr/DALA1170509871.md): Light · inoperative · Dec 19, 2011 · N780NC · Doug DC951 · Emergency Lighting
  > FOUND TWO AFT CATWALK EMERGENCY EGRESS PATH LIGHTS INOP. REPLACED BULBS, CHECK OK.
- [SDR DALA1151469871](https://openairdocs.org/sdr/DALA1151469871.md): Battery · discharged · Sep 1, 2011 · N780NC · Doug DC951 · Emergency Lighting
  > MAINTENANCE FOUND CABIN EMERGENCY CEILING LIGHTS ABOVE SEATS 5, 7 AND 9 WOULD NOT ILLUMINATE. MAINTENANCE REPLACED BATTERIES IN RESPECTIVE EMERGENCY BATTERY PACK PER AMM. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA1129579871](https://openairdocs.org/sdr/DALA1129579871.md): Frame · cracked · Apr 27, 2011 · N780NC · Doug DC951 · Fuselage Main, Frame
  > MAIN CABIN RT STA 734 MAIN FRAME CRACKED APPROX 2.5 INCHES. R & R MAIN FRAME, MAIN CABIN RT STA 734 L0R-L18R IAW SRM 51-10-4, 51-30-2, 51-30-5 & 51-30-8. NEW FRAME PN 9923406-502N 26 APR11 P-138 REQUIRED INSP.
- [SDR DALA1129029871](https://openairdocs.org/sdr/DALA1129029871.md): Keelbeam · damaged · Apr 26, 2011 · N780NC · Doug DC951 · Fuselage Main, Keel
  > KEEL BEAM AREA BETWEEN GEAR DOORS THRU ACCESS 5501 UPPER LT ANGLE CRACKED APPROX 2 INCHES. CUT AND REMOVED DAMAGED SECTION OF ANGLE. NDT IAW NDT SPM 06-10-01, A2700 CHECKED GOOD. FAB (1) REPAIR SECTION 7075 0.063. HEAT TREAT TO T6 ACCOMP ON TRAVELER N
- [SDR DALA1129019871](https://openairdocs.org/sdr/DALA1129019871.md): Support Angle · cracked · Apr 26, 2011 · N780NC · Doug DC951 · Fuselage Miscellaneous Structure
  > AFT ACCESSORY STA 1258, RT FAN INBD VERTICAL SUPPORT ANGLE CRACKED AT BOTTOM FASTENER. FABRICATED REPAIR DOUBLERS RT FAN INBD VERTICAL SUPPORT ANGLE AFT ACCY STA 1258 IAW SRM 51-10-4, 51-10-2 & 53-01, FIG 2..025 2024-T3 IAW DWG 9911840. TREATED AND PRIMED
- [SDR DALA1128939871](https://openairdocs.org/sdr/DALA1128939871.md): Cusp Web · corroded · Apr 26, 2011 · N780NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN RT CUSP WEB BETWEEN STA 370 AND 389 HAS CORROSION. CPCP TASK 58-53309 GAINED ACCESS. R & R RT CUSP WEB STA 370-389 FROM.032 7075T6. RESTORED AREA IAW SRM 51-30-1, 51-30-5, 51-30-2, 51-30-3, DWG SG09530019.P-125. REQUIRED INSP COMPLETED.
- [SDR DALA1128899871](https://openairdocs.org/sdr/DALA1128899871.md): Frame · chafed · Apr 26, 2011 · N780NC · Doug DC951 · Fuselage Main, Frame
  > AFT ACCESSORY STA 1209, LT LONG 4 VALVE CHAFING INTO PREVIOUS REPAIR ON WEB. REMOVED EXISTING REPAIR IAW SRM51-30-2. FABRICATED NEW DOUBLER.032 7075-T6 IAW SRM 53-01, FIG 4. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED DOUBLER IAW SRM 53-01, FIG 4, 51-30-
- [SDR DALA1128819871](https://openairdocs.org/sdr/DALA1128819871.md): Fitting · corroded · Apr 25, 2011 · N780NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN BETWEEN STA 693 AND 712 RT LONG 19 BATH TUB FITTING HAS CORROSION. CORROSION FOUND OUT OF LIMITS IAW SRM 53-01. REMOVED OLD FITTING, LOCATED, DRILLED & INSTALLED NEW FITTING PN 5913055-508 IAW SRM 51-10-5, 51-70-2 & ERA 490847-14 P-205, REQUIRED IN
- [SDR DALA1128799871](https://openairdocs.org/sdr/DALA1128799871.md): Doubler · dented · Apr 25, 2011 · N780NC · Doug DC951 · Fuselage Main, Plate/Skin
  > DENT IN UPPER WINDOW BELT DOUBLER, STA 712, LT SIDE. DENT MEASURES.017" X 7" DX=41 TOOL H9340. DENT FOUND TO BE OUT OF LIMITS IAW SRM 53-04, FIG 38. R & R WINDOW BELT AT STA 712, PN 9-5300-3-1772, PO 1098W037 IAW SRM 51-30-2 & 51-30-1, 51-30-5.
- [SDR DALA1128729871](https://openairdocs.org/sdr/DALA1128729871.md): Door Frame · corroded · Apr 25, 2011 · N780NC · Doug DC951 · Fuselage Main, Structure
  > E & E COMPARTMENT AFT LOWER END OF AIRSTAIR DOOR CUTOUT HAS CORROSION. CORR ON CORNER ANGLE FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG.1 75% MAT LOSS.CUT ACCESS HOLE STA 207 IN WEB TO GAIN ACCESS TO ANGLE FASTENERS 5"X 5" AREA IAW SRM 51-70-4 DEBURRED AND I
- [SDR DALA1128709871](https://openairdocs.org/sdr/DALA1128709871.md): Frame · chafed · Apr 25, 2011 · N780NC · Doug DC951 · Fuselage Main, Frame
  > FS 1190 AT L16R FRAME HAS HOLE CHAFED THRU BY ORIGINAL AUG VALVE. CUT OUT DAMAGED AREA 1 1/2"X 3/4" IAW SRM 53-03 FIG4. NDT VERIFIED DAMAGE REMOVED. NO CRACKS IAW NDT SPM 06-10-01.001 REC REPAIR ANGLE. LOCATED, DRILLED IAW SRM 51-10-4. FABRICATED DOUBLER PL
- [SDR DALA1128699871](https://openairdocs.org/sdr/DALA1128699871.md): Frame · corroded · Apr 25, 2011 · N780NC · Doug DC951 · Entrance Stairs
  > E & 3 COMP AIRSTAIR DOOR LOWER INTERIOR FRAME HAS 2EA SPOTS OF CORROSION. RECEIVED AND REPLACED WITH SERVICEABLE DOOR PER SRM 51-30-1.
- [SDR DALA1128219871](https://openairdocs.org/sdr/DALA1128219871.md): Bracket · cracked · Apr 19, 2011 · N780NC · Doug DC951 · Fuselage Miscellaneous Structure
  > AFT ACC COMPT FS1258 CTR, VERTICAL BRACKET IS CRACKED. LOWER RT SIDE RADIUS GAINED ACCESS. STOP DRILLED CRACK. NDT VERIFIED CRACK CONTAINMENT. FABRICATED AND INSTALLED 2 EA REPAIR ANGLES FROM.032 7075T6. RESTORED AREA. IAW SRM 51-30-1, 51-30-5, 53-01, FIG 2
- [SDR DALA1127539871](https://openairdocs.org/sdr/DALA1127539871.md): Spar · cracked · Apr 19, 2011 · N780NC · Doug DC951 · Elevator, Spar/Rib
  > LT ELEVATOR OTBD T/E SPAR CRACKED, OTBD HOLE IN SPAR ELONGATED. CUT OUT DAMAGED SECTION OF CHANNEL 7" LONG IAW SRM 51-70-5. NDT TO VERIFY DAMAGED CONTAINED. ORIG MAT 2024T3.025 IAW SRM 51-70-5. FABBED 1EA CHANNEL MAT 2024T3, PO 1120031. MAT FOR SPLICE 20
- [SDR DALA1127379871](https://openairdocs.org/sdr/DALA1127379871.md): Web · damaged · Apr 19, 2011 · N780NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN-INNER WEB ABOVE AFT LT ESCAPE DOOR STA 753-775 HAS DAMAGE TO FASTENER HOLE. HEAT TREATED WEB TO 2024-T3. LOCATED, DRILLED, DEBURRED NEW WEB IAW DRW 5910537 AND 51-10-2, 51-10-4. INSTALLED ON SAME CARD. REQUIRED INSP COMPLETED.
- [SDR DALA1127319871](https://openairdocs.org/sdr/DALA1127319871.md): Shear Tie · cracked · Apr 19, 2011 · N780NC · Doug DC951 · Fuselage Internal Mounting Structure
  > CABIN FRAME STA 1116 BETWEEN LONGERONS 15-14L SHEAR TIE CRACKED. REMOVED,FABED AND REINSTALLED NEW SHEAR TIE IAW SRM 51-30-2, 51-30-5, 51-13-3,51-10-2, 51-10-3, DWG 9957917. REQUIRED INSP COMPLETED.
- [SDR DALA1127309871](https://openairdocs.org/sdr/DALA1127309871.md): Frame · cracked · Apr 19, 2011 · N780NC · Doug DC951 · Fuselage Main, Frame
  > AFT ACCESSORY, RT STA 1209, FRAME WEB IS CRACKED MULTIPLE PLACES BETWEEN L9R AND L13R. REMOVED WEB AT STA 1209, BL L9R-L13R IAW SRM 51-30-2. RECEIVED MAT FOR DOUBLER & REPAIR.032, 7075-T6, PO 1022537 &.040 7075-T6 IAW SRM 51-70-4 FIG 1 FABRICATED, LOCATED
- [SDR DALA1128269871](https://openairdocs.org/sdr/DALA1128269871.md): Attach Angle · cracked · Apr 18, 2011 · N780NC · Doug DC951 · Fuselage Main, Attach Fittings
  > CABIN, CTR WING, STA 712, RBL 45. L-ANGLE CRACKED. FLOORBEAM TO TANK ATTACH ANGLE. REMOVED AND INSTALLED ANGLE IAW SRM 51-30-5 & 51-30-1 FABED ANGLE FROM 7075-0.090 IAW DWG 5910464 HEAT TREATED ON TRAVLER 2504N01781 TO T6. REQUIRED INSPECTION COMPLETED.
- [SDR DALA1127029871](https://openairdocs.org/sdr/DALA1127029871.md): Skin · damaged · Apr 18, 2011 · N780NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FUSELAGE EXT DRILL START IN SKIN AT STA 1116 L14L CUT OUT DAMAGE. 1" AREA IAW SRM 53-04, FIG 46, NDT VERIFIED NO CRACKS IAW BDT SPM 06-10-01.001. FABED REPAIR DOUBLER.032 6AL-4V TITANIUM IAW SRM 53-04, FIG 46. FABED -5 FILLERS.03, 6AL-4V TITANIUM & PASSIV
- [SDR DALA1126899871](https://openairdocs.org/sdr/DALA1126899871.md): Fitting · corroded · Apr 18, 2011 · N780NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN BETWEEN STA 693 AND 712 LEFT LONGERON 19 BATH TUB FITTING HAS CORROSION CPCP TASK 53-53300. REMOVED FITTING IAW DC-9 SRM 51-30-5. LOCATED, DRILLED AND INSTALLED NEW FITTING P/N 5913055-507 PO 1040W001 IAW DC-9 SRM 51-10-4 & 51-30-5 P-205.
- [SDR DALA1126859871](https://openairdocs.org/sdr/DALA1126859871.md): Doubler · gouged · Apr 18, 2011 · N780NC · Doug DC951 · Cargo/Baggage Doors
  > FWD CARGO DOOR FWD LATCH MECHANISM CUT OUT AND DOUBLER GOUGED. REMOVED OLD DOUBLER AND FABRICATED NEW DOUBLER IAW DC9 SRM 52-05 FIGURE 26B. MATERIAL.032 TY301 1/2. INSTALLED IAW DC9 SRM 52-05 FIGURE 26B. INSTALLED ID TAG IAW PS 900-5-1. WEIGHT IAW TOPP 30
- [SDR DALA1127059871](https://openairdocs.org/sdr/DALA1127059871.md): Skin · gouged · Apr 17, 2011 · N780NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FUSELAGE EXT LT SIDE FUSELAGE SKIN HAS A GOUGE APPROX 2" LONG AT BS 1087 AND ABOVE LONG 15L. REMOVED GOUGE IAW 53-33 FIG 3. MAT ID.032 6AL-HV PO 1120167. FABBED FILLER & DOUBLER IAW SRM 53-04, FIG 4. TREATED & PRIMED & TOP COATED IAW SRM 51-10-3. INSTALLED
- [SDR DALA1126739871](https://openairdocs.org/sdr/DALA1126739871.md): Bearing · loose · Apr 16, 2011 · N780NC · Doug DC951 · Trailing Edge Flaps
  > LEFT NR 4 FLAP HINGE FLAP SIDE BEARING LOOSE AT PIVOT POINT. REMOVED AND REPLACED WITH NEW NR 4 FLAP HINGE P/N 5912153-501 IAW DC-9 SRM 51-30-5 P241.
- [SDR DALA1126639871](https://openairdocs.org/sdr/DALA1126639871.md): Floor Panel · damaged · Apr 16, 2011 · N780NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 19 I/B EDGE FWD FASTENER HOLE HAS NO EDGE LEFT. FABRICATED NEW FLOOR PANEL SKIN AND HAT CHANNELS IAW ERA 4890838-14 FROM.040" 7075-T6, AND P/N S2912282. INSTALLED HAT CHANNELS TO SKIN AND STENCILED IAW ERA 4890838-14 TAGGED REPAIR IAW
- [SDR DALA1126729871](https://openairdocs.org/sdr/DALA1126729871.md): Support Angle · cracked · Apr 15, 2011 · N780NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 775 BL-0 VERTICAL SUPPORT ANGLE BELOW FLOOR CRACKED. REMOVED AND INSTALLED 2EA SUPPORT ANGLE AND 1EA ATTACH ANGLE BRACKET IAW DC9 SRM 51-30-02 AND 51-30-5. FABBED SUPPORT ANGLE P/N S2912538 EXTRUSION DRAWING 9923415 AND FABBED ATTACH BRACKET U
- [SDR DALA1126009871](https://openairdocs.org/sdr/DALA1126009871.md): Floor Panel · sheared · Apr 14, 2011 · N780NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 62 SEVERAL FASTENERS SHEARED OFF AND LOOSE ON AFT END. REMOVED TEN EA SHEARED OFF AND LOOSE FASTENERS ON MAIN CABIN FLOOR PNL 62 IAW SRM DC9 51-30-2. REPAIRED DISBONDED HAT CHANNEL 78 EA FASTENER HOLES IAW SRM DC9 51-10-4. TREATED AND
- [SDR DALA1125999871](https://openairdocs.org/sdr/DALA1125999871.md): Cusp Web · damaged · Apr 14, 2011 · N780NC · Doug DC951 · Fuselage Miscellaneous Structure
  > CUSP WEB STATION 693-753 HAS CRACKS AND CORROSION THROUGHOUT PANEL. FOUND ON FURTHER OPEN UP FOR FRAME 734 REPLACEMENT CARD 6C/176. FABRICATED NEW CUSP WEB & RING DOUBLERS IAW BOEING DRAWING S609530019. TREATED AND PRIMED IAW DC9 SRM 51-10-3. WEIGHT OF DOU
- [SDR DALA1125989871](https://openairdocs.org/sdr/DALA1125989871.md): Angle · broken · Apr 14, 2011 · N780NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 1079 TO 1118 LBL 56 Z-ANGLE BROKEN SEVERAL PLACES AT FASTENER HOLES CPCP TASK 58-53310. REMOVED & REPLACED SECTION OF Z-ANGLE STATION 1079-1125 LBL 56 IAW DC9SRM 51-30-02 & 51-30-05 P/N 4616493. FABBED REPAIR SPLICE FO Z-ANGLE FROM.050 7075T6
- [SDR DALA1125979871](https://openairdocs.org/sdr/DALA1125979871.md): Skin · cracked · Apr 14, 2011 · N780NC · Doug DC951 · Fuselage Main, Plate/Skin
  > AFT CARGO ABOVE DOOR CUTOUT AT APPROXIMATELY STATION 1108 PREVIOUS STOP DRILL IS CRACKED. REMOVED EXISTING REPAIR. CUT OUT DAMAGED AREA 2"X 2". HFEC INSP IAW DC-9 NDT SPM 06-10-01.001. NO FURTHER DAMAGE NOTED. OBTAINED FILLER MAT.020 7075-T6 AND DOUBLER
- [SDR DALA1125969871](https://openairdocs.org/sdr/DALA1125969871.md): Frame · cracked · Apr 14, 2011 · N780NC · Doug DC951 · Fuselage Main, Frame
  > AFT ACCESSORY CANTED FRAME 1303 CRACKED AT L16L LT SIDE. REMOVED CRACK IAW 53-03 FIG 4. CRACK REMOVED HFEC USING ZETECPER NDT SPM 06-10-01. RECEIVED MAT.040 7075T6 MAT ID.050 7075T6 MAT ID.063 7075T6. FABBED FILLER, ANGLE SPLICE IAW 53-03 FIG 4. TREAT
- [SDR DALA1127479871](https://openairdocs.org/sdr/DALA1127479871.md): Intercostal · cracked · Apr 13, 2011 · N780NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN-FS 764 BELOW RT AFT EMERGENCY EXIT VERTICAL INTERCOSTAL IS CRACKED. REMOVED 1 EA VERTICAL INTERCOSTAL, STOPPED DRILLED CRACK.25 DIA HFEC INSP STOP DRILL, CRACK, CONTAINED, NDT SPM 06-10-01-001, MAT I/D 7075-T6.063 FAB 2EA REPAIR DOUBLER 7075-T6.0
- [SDR DALA1125869871](https://openairdocs.org/sdr/DALA1125869871.md): Static Wick · damaged · Apr 13, 2011 · N780NC · Doug DC951 · Static Discharge System
  > LT ELEVATOR AT O/B STATIC WICK BASE ATTACH POINT OB OF STATIC WICK BASE AFT END CAP DOUBLER HAS A MISDRILLED RIVET, INCOMING DAMAGE, FOUND ON INVESTIGATION OF DAMAGE AT STATIC WICK BASE DOUBLER. REMOVED END CAP IAW DC-9 SRM 51-30-2. ORIGMAT.020 2024-T42 IAW
- [SDR DALA1125859871](https://openairdocs.org/sdr/DALA1125859871.md): Skin · damaged · Apr 13, 2011 · N780NC · Doug DC951 · Elevator, Plate/Skin
  > LT ELEVATOR OTBD T/E SKIN UPPER AND LOWER SURFACE OF SKIN HAS 3 EA MISDRILLED HOLES. CUT OUT DAMAGED AREA ON UPPER AND LOWER SURFACE. UPPER CUT OUT 2" X 1/2". LOWER 2.75" X.75" IAW SRM 55-01, FIG 4. NDT TO VERIFIED CRACKS CONTAINED. MAT USED TO FAB DOUBL
- [SDR DALA1125849871](https://openairdocs.org/sdr/DALA1125849871.md): Structure · cracked · Apr 13, 2011 · N780NC · Doug DC951 · Elevator Structure
  > LT ELEVATOR AT OTBD STATIC WICK BASE ATTACH POINT, STATIC WICKBASE DOUBLER CRACKED UPPER SURFACE. REMOVED STATIC WICK BASED DOUBLER IAW SRM 51-30-2. ORIG. MAT.020 2024 FAB NEW DOUBLER MAT.020 2024-T3 IAW SRM 51-10-4. INSTALLED NEW DOUBLER IAW SRM 51-30-2.
- [SDR DALA1125839871](https://openairdocs.org/sdr/DALA1125839871.md): Wedge · cracked · Apr 13, 2011 · N780NC · Doug DC951 · Elevator, Plate/Skin
  > LT ELEVATOR OTBD T/E WEDGE CRACKED. FOUND ON REMOVAL OF STATIC WICK BASE DOUBLER. REMOVED T/E WEDGE IAW SRM 51-30-2. REPAIRED USING REPAIR KIT IAW SRM 51-70-1. INSTALLED IAW SRM 51-30-2. WEIGHT AND BALANCE TO BE ACCOMPLISHED.
- [SDR DALA1125819871](https://openairdocs.org/sdr/DALA1125819871.md): Floor Panel · damaged · Apr 13, 2011 · N780NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 54 HAS SEVERAL MISSING AND LOOSE FASTENERS AND FIBER DAMAGE ON TOP FWD SURFACE OF PANEL. FABRICATED NEW FLOOR PANEL USING S2912282 HAT CHANNELS.025 7075-T6 IAW ERA 490836-14. REQUIRED INSP COMPLETED.
- [SDR DALA1125809871](https://openairdocs.org/sdr/DALA1125809871.md): Floorbeam · cracked · Apr 13, 2011 · N780NC · Doug DC951 · Fuselage Main, Floor Beam
  > MAIN CABIN FS 598, LBL 0-22 FLOOR SUPPORT IS CRACKED. REMOVED CRACKED FLOOR SUPPORT IAW SRM 51-30-05. FAB NEW FLOOR SUPPORT. MAT ID.050 2024 T3 IAW SRM 53-12-2 FIG 4. CUT, RIMMED, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED FLOOR SUPPORT IAW SRM 51-10-4
- [SDR DALA1125799871](https://openairdocs.org/sdr/DALA1125799871.md): Longeron · cracked · Apr 13, 2011 · N780NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > AFT ACCESSORY CANTED STA 1260, L7L CRACKED NDT VERIFIED. REMOVED LONGERON L7L FROM STA 1254 TO 1286. LOCATED AND DRILLED NEW LONGERON PN 2777922-4 AND SPLICE PN 7637813-3. INSTALLED LONGERON AND SPLICE IAW SRM 53-02, FIG 18. REQUIRED INSP COMPLETED.

Next page: https://openairdocs.org/deregistered/N780NC-2014-06-17/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 = 'N780NC' AND deregistration_id = 'N780NC-2014-06-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N780NC-2014-06-17/reports

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