# Service difficulty reports: N764NC, cancelled Jun 17, 2014

A list on [N764NC, cancelled Jun 17, 2014](https://openairdocs.org/deregistered/N764NC-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 5 · 233 reports

- [SDR DALA13048260855](https://openairdocs.org/sdr/DALA13048260855.md): Frame · damaged · Sep 26, 2013 · N764NC · Doug DC951 · Fuselage Main, Frame
  > FOUND FRAME DAMAGE BS 1190 BETWEEN L16-17R. COMPLIED WITH ERA/PRI 519084-14, REV 0.
- [SDR DALA13046530855](https://openairdocs.org/sdr/DALA13046530855.md): Wire Harness · damaged · Sep 23, 2013 · N764NC · Doug DC951 · Light System Wiring
  > EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT ROW 15. REPLACED LIGHT WIRE HARNESS IAW AMM33-53. OPS CHECKED GOOD.
- [SDR DALA13012990855](https://openairdocs.org/sdr/DALA13012990855.md): Wire · exposed · Mar 24, 2013 · N764NC · Doug DC951 · Light System Wiring
  > EXPOSED WIRES IN SEAT TRACK DIRECTLY UNDERNEATH SEAT 6F. SECURED WIRES IN RACEWAY.
- [SDR DALA13006900855](https://openairdocs.org/sdr/DALA13006900855.md): Power Supply · inoperative · Feb 7, 2013 · N764NC · Doug DC951 · Emergency Lighting
  > DURING INSPECTION, FOUND EMERGENCY PATH LIGHTS SEAT 9-13 AND LEFT OVER WING EXIT INOPERATIVE, REPLACED POWER SUPPLY AND TESTED OK.
- [SDR DALA12008090855](https://openairdocs.org/sdr/DALA12008090855.md): Lanyard · broken · Sep 19, 2012 · N764NC · Doug DC951 · Escape Slide
  > R1 DOOR SLIDE LANYARD BROKEN. MX ATTACHED THE LANYARD. ACFT IS NOW OK FOR SERVICE.
- [SDR DALA12006400855](https://openairdocs.org/sdr/DALA12006400855.md): O-Ring · damaged · Sep 3, 2012 · N764NC · Doug DC951 · APU Engine Fuel and Control
  > FLIGHT CREW NOTED FUEL FUMES IN AIRCRAFT AFTER STARTING AND RUNNING THE APU. ON INSPECTION, MAINTENANCE REPLACED THE O-RING AT THE ATOMIZER B-NUT AND PERFORMED A PNEUMATIC DUCT BURNOUT. AIRCRAFT IS NOW OKAY FOR SERVICE.
- [SDR DALA12005350855](https://openairdocs.org/sdr/DALA12005350855.md): Frame · damaged · Aug 13, 2012 · N764NC · Doug DC951 · Fuselage Main, Frame
  > RT MLG WHEEL WELL DOOR CUTOUT HAS FRAME WITH CHAFE/GOUGES IN 2 AREAS BY DOOR PROX SENSORS. GAINED ACCESS, REMOVED DAMAGE PER PR/I 505955-14, PERFORMED HFEC INSPECTION AT THE TRIMMED EDGE OF THE FORMER PER NDT SPM 06-10-01.003, NO CRACK NOTED. PERFORMED DVI O
- [SDR DALA12005270855](https://openairdocs.org/sdr/DALA12005270855.md): Skin · delaminated · Aug 12, 2012 · N764NC · Doug DC951 · Leading Edge Devices
  > LT WING SLAT PANEL 1142A IS DELAMINATED AND HAS CORROSION. ACCOMPLISHED REPAIR OF LT WING SLAT PANEL NR 1142A IAW PRI 505669-14 REVISION O, PRI NR 505669-14 REV 1 AND ERA NR 505669-14 REV ORIGINAL SECTION 1.
- [SDR DALA12005260855](https://openairdocs.org/sdr/DALA12005260855.md): Skin · cracked · Aug 12, 2012 · N764NC · Doug DC951 · Fuselage Main, Plate/Skin
  > A CRACK INDICATION WAS DETECTED ON SKIN EMANATING FROM FASTENER AT SHEAR CLIP AT BS 160 BETWEEN LONGERONS 2L AND 3L. REMOVED DAMAGE (CUT OUT) ON SKIN UPPER FUSELAGE FROM FASTENERS AT SHEAR CLIP AT STA Y160 BETWEEN LONGERONS 2L AND 3L PER DWG SR 09530129. DIM
- [SDR DALA12002930855](https://openairdocs.org/sdr/DALA12002930855.md): Lanyard · frayed · Jul 9, 2012 · N764NC · Doug DC951 · Escape Slide
  > DURING LINE CHECK, MAINTENANCE FOUND THE R1 DOOR SLIDE LANYARD TO BE FRAYED. MAINTENANCE REPLACED THE R1 DOOR SLIDE AND RETURNED THE AIRCRAFT TO SERVICE.
- [SDR DALA12001840855](https://openairdocs.org/sdr/DALA12001840855.md): Lock · binding · Jun 19, 2012 · N764NC · Doug DC951 · Entrance Stairs
  > ON WALK AROUND, MAINTENANCE FOUND THE AFT STAIRS DOWN AND THE CATWALK BLOCKING THE REAR EXIT. MAINTENANCE FOUND THE AFT VENTRAL STAIR LOCK BINDING AND FREED IT. AIRCRAFT NOW OKAY FOR SERVICE.
- [SDR DALA12000300855](https://openairdocs.org/sdr/DALA12000300855.md): Fuse · inoperative · May 22, 2012 · N764NC · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT SIGN TO BE INOPERATIVE. MAINTENANCE REPLACED THE FUSE AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA12000040855](https://openairdocs.org/sdr/DALA12000040855.md): Battery Pack · inoperative · May 12, 2012 · N764NC · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY CEILING LIGHTS BETWEEN ROWS 16 AND 19 TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIVE CONDITION.
- [SDR DALA1217819855](https://openairdocs.org/sdr/DALA1217819855.md): Wire · broken · Mar 22, 2012 · N764NC · Doug DC951 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE TAIL COMPARTMENT HAD ALL THREE CATWALK LIGHTS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT THE HINGE LINE AND REPAIRED IT. THE SYSTEM RETURNED TO NORMAL OPERATION.
- [SDR DALA1171009855](https://openairdocs.org/sdr/DALA1171009855.md): Tire · odor · Dec 22, 2011 · N764NC · Doug DC951 · Tire
  > BURNING RUBBER SMELL - VERY STRONG IN COCKPIT AND THROUGHOUT THE CABIN, ON TAKEOFF AND CLIMB, CONTINUED TO DESTINATION UNEVENTFULLY. REMOVED EXCESS RUBBER FROM TIRES SUSPECTED FROM HYDROPLANING.
- [SDR DALA1148709855](https://openairdocs.org/sdr/DALA1148709855.md): Battery · discharged · Aug 19, 2011 · N764NC · Doug DC951 · Emergency Lighting
  > MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING AT ROWS 14-19 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES PER AMM. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA1126649855](https://openairdocs.org/sdr/DALA1126649855.md): Floor Support · corroded · Mar 29, 2011 · N764NC · Doug DC951 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT ANGLE AND UPPER CHORD OF FLOORBEAM HAS CORROSION STA 237, BL-0 TO RBL 22. CORR OUT OF LIMITS IAW SRM 51-01, REMOVED CORR ON FLOORBEAM UPPER CHORD IN LIMITS IAW SRM 51-01, PAGE 8. HFEC SURFACE INSP PER NDT SPM 06-10-01.001, NO CRACKS NOTED
- [SDR DALA1105709855](https://openairdocs.org/sdr/DALA1105709855.md): Support · chafed · Jan 24, 2011 · N764NC · Doug DC951 · Fuselage Miscellaneous Structure
  > AFT ACCESSORY.9910087-5 SUPPORT CHAFED. RECEIVED -5 SUPPORT. LOCATED AND DRILLED HOLES, INSTALLED -5 SUPPORT IAW SRM 51-30-5, 51-30-2 S.
- [SDR DALA1105699855](https://openairdocs.org/sdr/DALA1105699855.md): Intercostal · damaged · Jan 24, 2011 · N764NC · Doug DC951 · Fuselage Miscellaneous Structure
  > AFT ACCESSORY INTERCOSTAL AT -27 ATTACH POINT ELONGATED HOLES, 3 EA. REMOVED DAMAGED.75"X2.5". FABBED DOUBLER FOR -3 AT -27 INTERCOSTAL IAW SRM 53-01, FIG 4 AND INSTALLED REPAIR DOUBLER SRM 51-30-2. REQUIRED INSPECTION COMPLETED.
- [SDR DALA1105489855](https://openairdocs.org/sdr/DALA1105489855.md): Wedge · cracked · Jan 22, 2011 · N764NC · Doug DC951 · Fuselage Main, Attach Fittings
  > INCOMING RUDDER HAS A 2" CRACK UPPERMOST T/E WEDGE. CUTOUT DAMAGED SECTION 10" FABRICATED LOCATED DRILLED & INSTALLED T/E SECTION. CUSTOMER FURNISHED & SPLICE IAW SRM 53-03, FIG 6, P205. REQUIRED INSPECTION COMPLETED.
- [SDR DALA1105179855](https://openairdocs.org/sdr/DALA1105179855.md): Doubler · damaged · Jan 22, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/Skin
  > AFT CARGO DOOR JAMB LOWER INTERIOR DOUBLER HAS INCOMING DRILL STARTS AND NUMEROUS HOLES FROM PREVIOUS REPAIRS. CUTOUT INNER DOOR JAMB DOUBLER STA 1068-1108 AT L24R. LOCATED AND DRILLED NEW DOUBLER 5910158-25 IAW SRM 51-10-2. HFEC INSP AREA IAW NDT SPM 06-10
- [SDR DALA1105169855](https://openairdocs.org/sdr/DALA1105169855.md): Doubler · damaged · Jan 22, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FWD CARGO DOORJAMB LOWER INTERIOR DOUBLER HAS INCOMING DRILL STARTS AND NUMEROUS HOLES FROM PREVIOUS REPAIRS. CUTOUT INNER DOOR JAMB DOUBLER STA 340-440 AT L25R. LOCATED AND DRILLED NEW DOUBLER 9962455-25 IAW SRM 51-10-2. HFEC INSP AREA IAW MDT SPM 06-10-
- [SDR DALA1105159855](https://openairdocs.org/sdr/DALA1105159855.md): Doubler · damaged · Jan 22, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FWD CARGO DOORJAMB LOWER INTERIOR DOUBLER HAS INCOMING DRILL STARTS AND NUMEROUS HOLES FROM PREVIOUS REPAIRS. CUTOUT INNER DOOR JAMB DOUBLER STA 340-440 AT L25R LOCATED AND DRILLED NEW DOUBLER 9962455-25 IAW SRM 51-10-2. HFEC INSP AREA IAW NDT SPM 06-10-0
- [SDR DALA1105119855](https://openairdocs.org/sdr/DALA1105119855.md): Longeron · misrepaired · Jan 22, 2011 · N764NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > AFT ACCY COMP CANTED FRAME STA 1245 AT LONGERON 3L, 4EA FASTENER HOLES ARE MISDRILLED. REMOVED APPROX 12" OF L3L PERFORMED DETAILED VISUAL INSP USING 10X MAGNIFYING GLASS NDT SPM 09-10-06 HFEC INSP CUTOUT IAW NDT SPM 06-10-01.001, A2700. NO INDICATIONS NOTED
- [SDR DALA1105089855](https://openairdocs.org/sdr/DALA1105089855.md): Longeron · misrepaired · Jan 22, 2011 · N764NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > AFT ACCESSORY CANTED FRAME AT STA 1245, L4L OTBD FRAME TO LONGERON ATTACH FASTENER HAS MISDRILLED HOLE. REMOVED DAMAGED SECTION OF LONGERON IAW SRM 53-02, FIG 18. HFEC INSP IAW NDT SPM 06-10-01 VERIFIED DAMAGE REMOVED. FABRICATED NEW LONGERON AND SPLICES I
- [SDR DALA1104959855](https://openairdocs.org/sdr/DALA1104959855.md): Frame · cracked · Jan 22, 2011 · N764NC · Doug DC951 · Fuselage Main, Frame
  > AFT ACCESSORY COMPARTMENT RT CANTED FRAME 1314, CRACKED BELOW AIRSTAIR ACTUATOR. CUTOUT DAMAGED AREA 2" X 2" AREA NDT VERIFIED DAMAGE. REMOVED IAW NDT SPM 06-10-01 FABBED & INSTALLED FILLER & DOUBLER IAW SRP DC9-A-53-10-17-801-663A-A. REQUIRED INSPECTION CO
- [SDR DALA1105059855](https://openairdocs.org/sdr/DALA1105059855.md): Frame · misrepaired · Jan 21, 2011 · N764NC · Doug DC951 · Fuselage Main, Frame
  > AFT ACCY COMPARTMENT CANTED FRAME, STA 1245, L3R, FRAME TO LONGERON ATTACH FASTENERS HAVE MISDRILLED HOLES. REMOVED DAMAGE APPROX 15.5". HFEC INSP IAW NDT SPM 06-10-01. VERIFIED DAMAGE REMOVED. LOCATED, FABRICATED AND DRILLED NEW SECTION OF LONGERON AND 2E
- [SDR DALA1104459855](https://openairdocs.org/sdr/DALA1104459855.md): Door Frame · damaged · Jan 20, 2011 · N764NC · Doug DC951 · Fuselage Main, Structure
  > FWD CARGO DOOR CUTOUT-STA 364 FRAME BETWEEN 26L-25 DOOR JAMB WEB HAS 2 EA ELONGATED HOLES. REAMED UP HOLES TO.371. FABED FREEZE PLUGS ON TRAVELER 2312NO2175. FABBED STRAPS IAW EA 488328-14. REQUIRED INSP COMPLETED.
- [SDR DALA1104209855](https://openairdocs.org/sdr/DALA1104209855.md): Battery Pack · inoperative · Jan 19, 2011 · N764NC · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT THE EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND RELAMPED THE LIGHT. SYS RETURNED TO AN OPS CONDITION.
- [SDR DALA1103969855](https://openairdocs.org/sdr/DALA1103969855.md): Shear Tie · cracked · Jan 19, 2011 · N764NC · Doug DC951 · Fuselage Internal Mounting Structure
  > AFT ACCESSORY COMPARTMENT RT SIDE STA 1190 SHEAR ANGLE CRACKED JUST BELOW L14R. REMOVED CRACKED SHEAR TIE IAW SRM 51-30-2 AND 51-30-5. FABRICATED NEW SHEAR TIE IAW SRM 51-10-2 AND 53-13-4. HEAT TREATED SHEAR TIE ON TRAVELER 2312N02136. INSTALLED NEW SHEAR TI
- [SDR DALA1103959855](https://openairdocs.org/sdr/DALA1103959855.md): Frame · cracked · Jan 19, 2011 · N764NC · Doug DC951 · Fuselage Main, Frame
  > AFT ACCESSORY RT SIDE CANTED FRAME 1245 CRACKED 3EA PLACES BETWEEN L3R AND L7R. REMOVED CRACKED FRAME IAW SRM 51-30- 1, 51-30-2 AND 51-30-5. LOCATED, DRILLED AND INSTALLED NEW FRAME IAW DWG SRO9530086. REQUIRED INSP COMPLETED.
- [SDR DALA1104169855](https://openairdocs.org/sdr/DALA1104169855.md): Frame · damaged · Jan 18, 2011 · N764NC · Doug DC951 · Fuselage Main, Frame
  > FWD CARGO DOOR CUTOUT STA 364, FRAME BETWEEN L26L-25. UPPER FLANGE FRAME HAS 2 EACH ELONGATED HOLES. REAMED UP HOLE TO CLEAN AND ROUND. FABRICATED AND INSTALLED FREEZE PLUGS. FABRICATED STRAPS AND INSTALLED REPAIR PARTS IAW EA NR 488328-14. REQUIRED INSP
- [SDR DALA1104089855](https://openairdocs.org/sdr/DALA1104089855.md): Floor Panel · corroded · Jan 18, 2011 · N764NC · Doug DC951 · Fuselage Floor Panel
  > MAIN PASSENGER CABIN FLOOR PANEL NR34, BL 0, STA 313, HAVE REMOVED CORROSION IAW SRM 51-10-3. MATERIAL LOSS OUT OF LIMITS IAW SRM 53-01.FABRICATED AND INSTALLED HAT CHANNELS AND WEB IAW ERA 488311-14. REQUIRED INSP COMPLETED.
- [SDR DALA1104049855](https://openairdocs.org/sdr/DALA1104049855.md): Longeron · damaged · Jan 18, 2011 · N764NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > AFT ACC COMPT LONGERON 5L CANTED STA 1245 HAS EXISTING DOUBLE DRILLED HOLE. CUT OUT APPROX 15" OF LONGERON 5L, STA 1245. LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW SRM 51-10-2, 51-30-5, 53-02, FIG 18, SHT 2, 51-10-3, 51-10-4. REQ
- [SDR DALA1104069855](https://openairdocs.org/sdr/DALA1104069855.md): Shear Tie · cracked · Jan 17, 2011 · N764NC · Doug DC951 · Fuselage Internal Mounting Structure
  > CABIN STA 1136 BULKHEAD BETWEEN LONGERON 14L-15L SHEAR TIE CRACKED. REMOVED CRACKED SHEARTIE IAW SRM 51-30-5. RECEIVED REPAIR KIT FOR SHEAR TIE. LOCATED AND DRILLED NEW SHEAR TIE IAW SRM 51-10-4. INSTALLED SHEAR TIE IAW SRM 51-30-5. REQUIRED INSPECTION CO
- [SDR DALA1104159855](https://openairdocs.org/sdr/DALA1104159855.md): Stop Fitting · damaged · Jan 16, 2011 · N764NC · Doug DC951 · Cargo/Baggage Doors
  > FWD CARGO DOOR CUTOUT AFT LOWER DOOR STOP T-FITTING ON BACKSIDE OF DOOR STOP DAMAGED. REMOVED DAMAGED FITTING IAW SRM 51-30-5. FABRICATED NEW FITTING IAW SRM 51-10-1 AND 51-10-4 AND DWG 9957909. INSTALLED NEW FITTING IAW SRM 51-30-5.
- [SDR DALA1104149855](https://openairdocs.org/sdr/DALA1104149855.md): Frame · damaged · Jan 16, 2011 · N764NC · Doug DC951 · Fuselage Main, Frame
  > FWD CARGO STA 427 L26R-L25R FRAME HAS DRILL HOLE NEXT TO CORE NUT HOLE. REAMED HOLE TO.625 IAW DWG 5912461. RECEIVED 3 EA FREEZE PLUGS ON TRAV 2312NO2114. INSTALLED 3 EA FREEZE PLUGS IAW ER/A NR 487380-14. FAB 2 EA REPAIR STRAPS. INSTALLED LOWER AND UP
- [SDR DALA1103829855](https://openairdocs.org/sdr/DALA1103829855.md): Rib · damaged · Jan 15, 2011 · N764NC · Doug DC951 · Wing, Rib/Bulkhead
  > LT WING T/E, FOUND TOO MARK O LOWER ANGLE OF RIB NR7 OUT OF LIMITS. REMOVED DAMAGED T-ANGLE IAW SRM 51-30-2. FABBED AND INSTALLED NEW T-ANGLE IAW SRM 51-30-2.
- [SDR DALA1103819855](https://openairdocs.org/sdr/DALA1103819855.md): Door Frame · cracked · Jan 15, 2011 · N764NC · Doug DC951 · Flight Compartment Windows
  > FUSELAGE EXTERIOR FWD SERVICE DOOR FRAME, FWD UPPER CORNER HAS.1250" CRACK AT FASTENER. REPAIR IAW EM5330-01134-01B, CUTOUT DAMAGED AREA 2.125" X 3". NDT VERIFIED DAMAGE, REMOVED, FABBED AND INSTALLED FILLER IAW SRM 53-05, FIG 112 AND DWG SRO9530172. REQUI
- [SDR DALA1103809855](https://openairdocs.org/sdr/DALA1103809855.md): Skin · damaged · Jan 15, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN STA 370, LONG 26L SKIN REQUIRES 53-04, FIG 12C REPAIR TO FACILITATE EA 487370-14 CUT OUT DAMAGED AREA 18.5"X 15.5" NDT VERIFIED DAMAGE, REMOVED IAW NDT SPM 06-10-01. FABBED AND INSTALLED REPAIR PARTS IAW SRM 53-04, FIG 12C. REQUIED INSP COMPLET
- [SDR DALA1103799855](https://openairdocs.org/sdr/DALA1103799855.md): Skin · damaged · Jan 15, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR STA 1060 AT LONG 26R SKIN REQUIRES REPAIR DUE TO EXISTING REPAIR FASTENER HOLES CUTOUT SKIN SECTION IAW SRM 53-04 FIG 12C. HFEC AREA NO DEFECTS NOTED. FABRICATED AND INSTALLED NEW SKIN SECTION AND REPAIR PARTS IAW SRM 53-04, FIG 12C. REQUIR
- [SDR DALA1103649855](https://openairdocs.org/sdr/DALA1103649855.md): Angle · cracked · Jan 14, 2011 · N764NC · Doug DC951 · Wing Miscellaneous Structure
  > MAIN CABIN STA 748 TO 760, RBL 44, WEB TO CTR WING TANK, ATTACH ANGLE CRACKED. REMOVED DAMAGED ANGLE IAW SRM 51-30-5 AND 51-30-2. INSTALLED NEW ANGLE PN 591046424, PO 1032365 IAW SRM 51-10-4 AND 51-30-5.
- [SDR DALA1103639855](https://openairdocs.org/sdr/DALA1103639855.md): Skin · damaged · Jan 14, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN-STA 1108, L26R SKIN REQUIRES 53-04, FIG 12C, REPAIR TO FACILITATE EA 487369-14. CUT OUT AREA STA 1108 TO 1125, BETWEEN L23R TO 26R (16",18") FROM.071 2024-T3 AND FINGER DOUBLER.025 2024-T3, 6 EA DOUBLERS AND 7 EA STRAPS FROM.071 2024-T3 AND F
- [SDR DALA1103559855](https://openairdocs.org/sdr/DALA1103559855.md): Floorbeam · damaged · Jan 14, 2011 · N764NC · Doug DC951 · Fuselage Main, Floor Beam
  > MAIN PASSENGER CABIN STA 180, BL 0, RBL 45, FLOORBEAM REQUIRE REMOVAL FAB REINSTALL IAW CUSTOMER. REMOVED, FABRICATED, & INSTALLED NEW FLOORBEAM IAW SRM 51-10-3, 51-30-5.
- [SDR DALA1103509855](https://openairdocs.org/sdr/DALA1103509855.md): Floor Panel · corroded · Jan 14, 2011 · N764NC · Doug DC951 · Fuselage Floor Panel
  > MAIN PASSENGER CABIN CORROSION ON FLOOR PANEL PN37, SEVERAL PLACES. REMOVED CORROSION IAW SRM 51-10-3. ORIGINAL THICKNESS WAS.025 AFTER MATERIAL IS.005. OUT OF LIMITS IAW SRM 53-01. FABRICATED FLOOR PANEL WEB FROM 7075-T6.025 AND HAT CHANNELS FROM S2912
- [SDR DALA1103049855](https://openairdocs.org/sdr/DALA1103049855.md): Bulkhead · damaged · Jan 13, 2011 · N764NC · Doug DC951 · Nacelle/Pylon, Bulkhead/Firewall
  > MAIN CABIN STA 1136 LT PYLON BULKHEAD FWD SIDE UPPER END 2 FASTENERS HAVE NO EDGE DISTANCE. TRIMMED OUT DAMAGED AREA.450 X.680 IAW E-88 NR 8134 IAW SRM 53-01, FIG 4. FABRICATED & INSTALLED 1 EA DOUBLER AND 2 EA FILLERS IAW E88 NR 8134 IAW SRM 53-04, FIG 4
- [SDR DALA1103019855](https://openairdocs.org/sdr/DALA1103019855.md): Attach Angle · cracked · Jan 13, 2011 · N764NC · Doug DC951 · Wing, Attach Fittings
  > MAIN CABIN STA 756 LBL 44 WEB TO CTR WING TANK ATTACH ANGLE CRACKED. CUTOUT CRACKED AREA 1" X 12" IAW SRM 53-01, FIG 2, FABRICATED 1EA FILLER, 2EA REPAIR ANGLES IAW SRM 53-01, FIG 2. REMOVED & INSTALLED NEW T ANGLE AND 2EA SHIMS IAW DWG NR 9919689. INSTALL
- [SDR DALA1102669855](https://openairdocs.org/sdr/DALA1102669855.md): Cusp Web · cracked · Jan 12, 2011 · N764NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 237, RBL 55, CUSP WEB IS CRACKED IN 2EA PLACES STOP DRILLED CRACK IAW DC-9 A53-10-16. FABRICATED REPAIR DOUBLER IAW SRP DC9-A-53-10-16-801-663A -A. INSTALLED DOUBLER IAW SRP DC-9-A-53-10-16-801-663A-A.P-134 10 JAN 11. REQUIRED INSPECTION COMPLE
- [SDR DALA1102659855](https://openairdocs.org/sdr/DALA1102659855.md): Cusp Web · cracked · Jan 12, 2011 · N764NC · Doug DC951 · Fuselage Miscellaneous Structure
  > CABIN STA 237, RBL 55, BENEATH CUSP WEB CRACKED DOUBLER AT FASTENER HOLE. REMOVED 1EA FRAME FITTING IAW SRM 51-30-5. REMOVED FASTENERS & REPAIR IAW SRM 51-30-5. CUT-OUT DAMAGED AREA IAW SRM 53-10-16-801-663A-A, NDT VERIFIED DAMAGE. REMOVED IAW NDT SPM 0
- [SDR DALA1102649855](https://openairdocs.org/sdr/DALA1102649855.md): Floor Panel · damaged · Jan 12, 2011 · N764NC · Doug DC951 · Fuselage Floor Panel
  > MAIN PASSENGER CABIN SEVERAL WASHERS PULLING THROUGH SKIN OF FLOOR PANEL NR84. FABRICATED FLOOR PANEL WEB AND HAT CHANNELS FROM IAW DWG 9957919. ASSEMBLED PANEL WEB AND HAT CHANNELS IAW SRM 51-30-2 AND ERA 488336-14. REQUIRED INSPECTION COMPLETED.

Next page: https://openairdocs.org/deregistered/N764NC-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 = 'N764NC' AND deregistration_id = 'N764NC-2014-06-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N764NC-2014-06-17/reports

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