# Service difficulty reports: N775NC, cancelled Jun 17, 2014

A list on [N775NC, cancelled Jun 17, 2014](https://openairdocs.org/deregistered/N775NC-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 · 156 reports

- [SDR DALA13050020866](https://openairdocs.org/sdr/DALA13050020866.md): Battery Pack · inoperative · Oct 4, 2013 · N775NC · Doug DC951 · Emergency Lighting
  > LEFT AND RIGHT AFT OVERWING EXIT SIGNS NOT WORKING. R & R BATTERY PACK. OPS CHECKED GOOD IAW MM 33-53.
- [SDR DALA12012620866](https://openairdocs.org/sdr/DALA12012620866.md): Skin · dented · Nov 7, 2012 · N775NC · Doug DC951 · Fuselage Main, Plate/Skin
  > DURING LIGHTNING STRIKE INSPECTION, FOUND DENT ON LOWER LT SIDE OF FUSELAGE APPROX 16 IN OTBD OF VHF 2 COMM ANTENNA. REPAIRED IAW SRM 53-04-3, FIG 8.
- [SDR DALA12009920866](https://openairdocs.org/sdr/DALA12009920866.md): Light · broken · Oct 11, 2012 · N775NC · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THE EMERGENCY ESCAPE LIGHTING AT 7D TO BE BROKEN. MX R & R THE LIGHT ASSY AND RETURNED THE ACFT TO SERVICE.
- [SDR DALA12004770866](https://openairdocs.org/sdr/DALA12004770866.md): Slide · low pressure · Aug 3, 2012 · N775NC · Doug DC951 · Escape Slide
  > DURING LINE CHECK, MAINTENANCE FOUND THE 1R DOOR SLIDE PRESSURE AT ZERO. MAINTENANCE REPLACED THE DOOR SLIDE AND RETURNED THE AIRCRAFT TO SERVICE.
- [SDR DALA12002940866](https://openairdocs.org/sdr/DALA12002940866.md): Lanyard · misrouted · Jul 10, 2012 · N775NC · Doug DC951 · Escape Slide
  > DURING LINE CHECK, MAINTENANCE FOUND THE R1 DOOR SLIDE LANYARD TO BE IMPROPERLY ROUTED. MAINTENANCE REINSTALLED THE LANYARD AND RETURNED THE AIRCRAFT TO SERVICE.
- [SDR DALA1223899866](https://openairdocs.org/sdr/DALA1223899866.md): Connector · loose · Apr 17, 2012 · N775NC · Doug DC951 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY ESCAPE LIGHTING IN THE REAR OF THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTION AT THE LIGHT HOUSING ASSEMBLY, TIGHTENED THE CONNECTION AND THE SYSTEM RETURNED TO NORMAL OPERATION
- [SDR DALA1223879866](https://openairdocs.org/sdr/DALA1223879866.md): Battery Pack · discharged · Apr 17, 2012 · N775NC · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS DIM. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS. RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA1157829866](https://openairdocs.org/sdr/DALA1157829866.md): Battery Pack · discharged · Oct 11, 2011 · N775NC · Doug DC951 · Emergency Lighting
  > EMERGENCY EGRESS AISLE LIGHTS TO DIM, ROWS 9 THROUGH 12. REPLACED BATTERY PACK, CHECKS OK.
- [SDR DALA1153849866](https://openairdocs.org/sdr/DALA1153849866.md): Floorboard · cracked · Sep 14, 2011 · N775NC · Doug DC951 · Fuselage Floor Panel
  > CENTER AISLE FLOORBOARD 60D HAS 11 INCH CRACK. P/N 9923615-11 IPC 53-21-00-03G ITEM 200. STA MSP 14SEP11 ATA 5322 ENTR 555596 S POS: CN TASK HRS: 0002.0 TASK ELAPSE TIME HRS: 0002.0 RII: N. REPLACED AISLE FLOORBOARD 60D, ROBBED FROM A/C 9871 PER DC9 AMM 53-2
- [SDR DALA1137199866](https://openairdocs.org/sdr/DALA1137199866.md): Skin · chafed · May 29, 2011 · N775NC · Doug DC951 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STAB LT SKIN CHAFED AFT OF LEADING EDGE. REMOVED AND REPLACED LT SKIN PN H5912130-71 PO 1130960 IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5 P-243.
- [SDR DALA1137169866](https://openairdocs.org/sdr/DALA1137169866.md): Intercostal · bent · May 29, 2011 · N775NC · Doug DC951 · Fuselage Miscellaneous Structure
  > AFT ACC COMPT BETWEEN STA 1314 AND 1326 LT SIDE INTERCOSTAL IS BENT AND ATTACH CLIP AFT END IS CRACKED. REMOVED INTERCOSTAL, REFORMED, INSPECTED, NO CRACKS NOTED, REMOVED ATTACH CLIP AT AFT END, FABED NEW CLIP FROM MAT ID 2024-T3.032, LOCATED, DRILLED, TREA
- [SDR DALA1136699866](https://openairdocs.org/sdr/DALA1136699866.md): Support · cracked · May 26, 2011 · N775NC · Doug DC951 · Fuselage Miscellaneous Structure
  > 6C/281 MAIN PASSENGER CABIN STA 1184 RBL 22 ELEVATOR CONTROL CABLES PULLEY BRACKET MOUNT SUPPORT AFT SIDE OF PULLEY CRACKED. REMOVED SUPPORT, STOP DRILLED CRACK, NDT VERIFIED CRACKS CONTAINED. FABRICATED AND INSTALLED REPAIR PARTS FROM NR 1120665. ALL WORK
- [SDR DALA1136499866](https://openairdocs.org/sdr/DALA1136499866.md): Floor Panel · cracked · May 25, 2011 · N775NC · Doug DC951 · Fuselage Floor Panel
  > MAIN PASSENGER CABIN FLOOR PANEL NR 86LT SIDE IS CRACKED 2 PLACES. CUT OUT DAMAGE SECTION 25 INCHES BY 9 INCHES. NO DEFECTS IAW NDT SPM 06-10-06. FABRICATED AND INSTALLED FILLER.020 7075-T6 AND DOUBLER.032 7075-T6 IAW ERA 491735-14. P-226 REQUIRED INSP CO
- [SDR DALA1136039866](https://openairdocs.org/sdr/DALA1136039866.md): Floor Panel · cracked · May 23, 2011 · N775NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR 85 HAS CRACK INBD AFT END. CUTOUT DAMAGE 2 INCHES BY 1.25 INCHES NO DEFECTS PER NDT SPM 06-10-01. FABRICATED AND INSTALLED FILLER AND DOUBLER FROM.020 7075-T6 PO NR 1120495 IAW DC-9 SRM 53-01 FIG 4, P225. REQUIRED INSPECTION COMPL
- [SDR DALA1136029866](https://openairdocs.org/sdr/DALA1136029866.md): Channel · dented · May 23, 2011 · N775NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR 77 HAS 5 HAT CHANNELS DISBONDED AND IEA HAS DENT. REMOVED HAT CHANNELS IAW SRM 51-10-4. LOCATED AND DRILLED HOLES IN DISBONDED HAT CHANNELS AND INSTALLED HAT CHANNELS IAW SRM 51-30-2 AS PER ENGINEERING. REQUIRED INSPECTION COMPLETE
- [SDR DALA1135889866](https://openairdocs.org/sdr/DALA1135889866.md): Floor Support · cracked · May 20, 2011 · N775NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL 66 HAS 5EA HAT CHANNELS CRACKED. REMOVED AND REPLACED 5 HAT CHANNELS IAW SRM 51-30-2. UPON INSP FOUND 2 CRACKS. CUTOUT DAMAGED AREA 2 INCH BY 1 1/2 INCH. NDT HFEC INSP IAW NDT SPM06-10-01. NO CRACKS NOTED. FABRICATED AND INSTALLE
- [SDR DALA1135599866](https://openairdocs.org/sdr/DALA1135599866.md): Floor Support · cracked · May 18, 2011 · N775NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL 73 HAS BTM SIDE HAS 1 HAT CHANNEL CRACKED APPROX 1/2 IN. CUT OUT DAMAGED HAT CHANNEL (2 INCH LENGTH) IAW SRM 53-05 FIG 1. RECEIVED AND TRIMMED CHANNEL AND INSTALLED IAW SRM 53-05 FIG 1. TAGGED REPAIR IAW DPS 900-5-1 NR 4.
- [SDR DALA1135309866](https://openairdocs.org/sdr/DALA1135309866.md): Skin · damaged · May 18, 2011 · N775NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 73 HAS 1 HOLE ON TOP SKIN. CUT OUT DAMAGE (1") IAW SRM 53-01 FIG, 4. NDT VERIFIED NO CRACK NOTED IAW NDT SPM 06-10-01. ORIG MAT OF PANEL 73 IS.020" 7075-T6 IAW SRM 53-23-0. FABRICATED DOUBLER FROM.032" 7075T6 AND INSTALLED IAW SRM 53
- [SDR DALA1135299866](https://openairdocs.org/sdr/DALA1135299866.md): Structure · chafed · May 18, 2011 · N775NC · Doug DC951 · Fuselage Structure (General)
  > AFT ACC COMPT STA 1190 L17R HOLE CHAFED IN FR OB OF VALVE. CUT OUT DAMAGED AREA 2.5 INCH BY 1 INCH. NO DEFECTS PER NDT SPM 06-10-01.001. FIB FILLER FROM PART NR 9958233-27 AND DOUBLERS FROM.063 7075-T6 PART NR SR09530035-25. INSTALLED YAW DC9 SUM 5304 FIG
- [SDR DALA1135159866](https://openairdocs.org/sdr/DALA1135159866.md): Skin · cracked · May 17, 2011 · N775NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR LT SIDE AIR STAIRS CUTOUT AFT LOWER CORNER HAS APPROX 2 INCH CRACK IN FUSELAGE SKIN. NDT VERIFIED CRACK. TRIMMED OUT SKIN WITH DIMENSIONS OF 1.5 IN BY 1.70 IN IAW DWG NR SR09530031. HFEC INSPECTED IAW NDT SPM 06-10-01.001.CRACK TO BE CONTA
- [SDR DALA1135079866](https://openairdocs.org/sdr/DALA1135079866.md): Floorbeam · cracked · May 17, 2011 · N775NC · Doug DC951 · Fuselage Main, Floor Beam
  > MAIN CABIN OVERWING STA 775 RBL 52 FLOORBEAM CRACKED. REMOVED FLOORBEAM IAW DC9 SRM 51-30-1, 51-30-2, 51-30-05. RECEIVED NEW FLOORBEAM CFE PN NR 9915527 -506. LOCATED, DRILLED AND DEBURRED IAW DOUGLAS DRAWING 9915527. TREATED AND PRIMED IAW SRM 51-10-3.
- [SDR DALA1135069866](https://openairdocs.org/sdr/DALA1135069866.md): Web · cracked · May 17, 2011 · N775NC · Doug DC951 · Fuselage Main, Frame
  > MAIN CABIN OVER WING RBL-44 BETWEEN STA 740 AND 770 WEB TO CENTER TANK ANGLE CRACKED. NDT MARKED ENDS OF CRACK PER NDT SPM 06-10-01. GAINED ACCESS AND REMOVED DAMAGED SECTION OF ANGLE FROM STA 700-780 RBL 44. RECEIVED NEW ANGLE. INSTALLED NEW ANGLE IAW SRM
- [SDR DALA1134969866](https://openairdocs.org/sdr/DALA1134969866.md): Vane · chafed · May 16, 2011 · N775NC · Doug DC951 · Trailing Edge Flaps
  > LEFT WING MOVEABLE VANE INBD EDGE CHAFED AT LOWER END PARTS RACK 82B. -5 ZEE ANGLE AND -21 ANGLE FOUND TO BE OUT OF LIMITS IAW DC-9 SRM 57-01 FIG 1. FABRICATED -21 ANGLE IAW DC9 SRM 51-10-02 MTL.032 2024 T3. TREATED AND PRIMED IAW DC-9 SRM 51-10-3. RECV NEW
- [SDR DALA1134949866](https://openairdocs.org/sdr/DALA1134949866.md): Access Panel · damaged · May 16, 2011 · N775NC · Doug DC951 · Wing, Plate/Skin
  > RIGHT WING FUEL ACCESS 1472A LANDING HAS 1 MIS DRILLED HOLE. REAMED HOLE TO.435. FABRICATED FREEZE PLUG. INSTALLED IAW ERA 491735-14 P-226.
- [SDR DALA1134889866](https://openairdocs.org/sdr/DALA1134889866.md): Frame · gouged · May 16, 2011 · N775NC · Doug DC951 · Fuselage Main, Frame
  > AFT WET AREA-STA 1136 LEFT LONG 4 PYLON BULKHEAD FRAME GOUGED. BLEND GOUGE 1" BY 4" ORIG.050 REMOVED.012 REMAINING.038. FOUND OUT OF LIMITS PER SRM 53-01.FAB AND INSTALLED 2 ANGLES FROM.040 7075-0 IAW SRM 53-02 FIG 2 SHEET 4. HEAT TREATED ON TRAVELER 25
- [SDR DALA1134879866](https://openairdocs.org/sdr/DALA1134879866.md): Frame · cracked · May 16, 2011 · N775NC · Doug DC951 · Fuselage Main, Frame
  > MAIN CABIN STA 734 RIGHT LONG 18 MAIN FRAME CRACKED. REMOVED AND INST NEW FRAME PART NR 9923406-502 IAW 51-30-5, DWG 3924863.P-226. REQUIRED INSPECTION COMPLETED.
- [SDR DALA1134209866](https://openairdocs.org/sdr/DALA1134209866.md): Frame · cracked · May 15, 2011 · N775NC · Doug DC951 · Fuselage Main, Frame
  > MAIN CABIN STA 753 RIGHT LONG 18 MAIN FRAME CRACKED. REMOVED MAIN FRAME AT STA 753 RIGHT LONG 18. RECEIVED NEW FRAME P/N 97-5300-3-0024. INSTALLED NEW FRAME IAW SRM 51-30-5 P226.
- [SDR DALA1134199866](https://openairdocs.org/sdr/DALA1134199866.md): Intercostal · cracked · May 15, 2011 · N775NC · Doug DC951 · Fuselage Miscellaneous Structure
  > COCKPIT BETWEEN STA 148 AND STA 160 LOWER INTERCOSTAL CRACKED AT FWD WIRE CONDUIT. REMOVED WEB ATTACH PLATE AND 2 BRACKETS TO FOM. REMOVED INTERCOSTAL IAW SRM 51-30-2. FABRICATED REPAIR ANGLES FROM 3011/2H.063 PO NR 0722363 IAW SRM 53- 05-51-10-2. INSTAL
- [SDR DALA1134169866](https://openairdocs.org/sdr/DALA1134169866.md): Floor Support · corroded · May 15, 2011 · N775NC · Doug DC951 · Fuselage Main, Floor Beam
  > MAIN CABIN STA 237-302 BL0 FLOOR SUPPORT HAS CORROSION REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-05. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1.
- [SDR DALA1134139866](https://openairdocs.org/sdr/DALA1134139866.md): Cusp Web · cracked · May 15, 2011 · N775NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN BETWEEN STA 1044 AND 1060 LT CUSP WEB CRACKED SEVERAL PLACES. CUTOUT DAMAGE AREA 4.5 INCH BY 29.875 INCH. NO DEFECTS PER NDT SPM 06-10-01. FAB AND INSTALLED REPAIR FROM.032 INCH 7075-T6 IAW DWG SG09530019.P226. REQUIRED INSP.
- [SDR DALA1134079866](https://openairdocs.org/sdr/DALA1134079866.md): Seat Track · corroded · May 15, 2011 · N775NC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN STA 200-285 RBL 22, SEAT TRACK HAS CORROSION. REMOVED CORROSION FROM SEAT TRACK IAW 53-01 FIG 1 OUT OF LIMITS RECEIVED NEW TRACK P/N 27726100. REMOVED AND REPLACED SEAT TRACK IAW DC-9 SRM 51-30-05. REQUIRED INSPECTION.
- [SDR DALA1134219866](https://openairdocs.org/sdr/DALA1134219866.md): Frame · damaged · May 14, 2011 · N775NC · Doug DC951 · Fuselage Main, Frame
  > AFT CARGO COMPT FRAME REPAIR ANGLE HAS SEVERAL IMPROPERLY INSTALLED FASTENER'S SOME PULLED THROUGH AND TOOLING GOUGE'S IN UPPER FWD FLANGE AT STA 908 BETWEEN LONG S29L-29R. REMOVED DAMAGED FRAME REPAIR IAW SRM 51-30-5. FABRICATED AND INSTALLED NEW FRAME SECT
- [SDR DALA1134099866](https://openairdocs.org/sdr/DALA1134099866.md): Pulley Bracket · chafed · May 14, 2011 · N775NC · Doug DC951 · Entrance Stairs
  > AFT ACC COMPT STA 1303 LT PULLEY MOUNT BRACKET AT AIRSTAIR DOOR CUT OUT CHAFED. REMOVED AND REPLACED LT ELEVATOR CONTROL CABLE PULLEY MOUNT BRACKET AT STA 1303 IAW DC-9 SRM 51-30-01. TENSIONED LT ELEVATOR CONTROL CABLES 3B, 4B, IAW MM 27-30-00. FINAL RIGGING
- [SDR DALA1134899866](https://openairdocs.org/sdr/DALA1134899866.md): Keelbeam · corroded · May 13, 2011 · N775NC · Doug DC951 · Fuselage Main, Keel
  > KEEL AREA BETWEEN MAIN GEAR DOORS LANDING FOR PANEL 5501NW HAS CORROSION SEVERAL PLACES. REMOVED CORROSION OUT OF LIMITS IAW DWG 9923459. LOCATED, DRILLED, TREATED, PRIMED, TOP COATED AND INSTALLED NEW WEB SKIN PART NR 9923459-35 ON IAW SRM 51-10-4, 51-10-
- [SDR DALA1133519866](https://openairdocs.org/sdr/DALA1133519866.md): Panel · cracked · May 11, 2011 · N775NC · Doug DC951 · Nacelle/Pylon, Plate/Skin
  > NR 1 ENG PYLON T/E PNL LANDING HAS A CRACK FWD OTBD END COMING PAST PREVIOUSLY REPAIRED STOP DRILL HOLE AT UPPERSIDE. REMOVED PREVIOUS REPAIR DOUBLER PER DC9 SRM 51-30-2. DRILLED STOP HOLE, FABRICATED NEW REPAIR DOUBLER PER DC-9 SRM 54-01 FIG 2 SHEET 3. MAT
- [SDR DALA1133509866](https://openairdocs.org/sdr/DALA1133509866.md): Skin · corroded · May 11, 2011 · N775NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN BETWEEN STA 1151 AND 1167L29L AND L29R PREVIOUS REPAIR HAS CORROSION AROUND DRAIN HOLE. REPAIR HAS CORROSION THAT REQUIRES BLENDING. CANT BLEND ON REPAIR OUT OF LIMITS. REMOVED REPAIR DOUBLER. REQUEST NDT FOR CRACKS, NO CRACKS NOTED
- [SDR DALA1133499866](https://openairdocs.org/sdr/DALA1133499866.md): Longeron · damaged · May 11, 2011 · N775NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > FWD CARGO STA 535 L24R HAS 1 HOLE IN LONGERON LOWER LEG. TRIMMED OUT DAMAGED AREA. NDT VERIFIED DAMAGE NO LONGER EXISTS. FABRICATED REPAIR DOUBLER FROM 7075 T6.063. DRILLED AND DEBURRED, ALODINE AND PRIMED AND INSTALLED IAW SRM 51-10-3, 51-30-2 AND 51-30-
- [SDR DALA1133489866](https://openairdocs.org/sdr/DALA1133489866.md): Stringer · damaged · May 11, 2011 · N775NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > FWD CARGO STA 535 L24L HAS 1 MISS DRILLED HOLE IN RECEIVED.063 7075-T6 IAW SRP DC-9-53-10-04-801-663A-A. FABRICATED, LOCATED AND DRILLED REPAIR ANGLE IAW SRM AND SPM 51-10-4, 51-10-2 AND DC9-A-53-10-04-801-663A-A. TREATED AND PRIMED IAW SRM 51-10-3. INSTAL
- [SDR DALA1133479866](https://openairdocs.org/sdr/DALA1133479866.md): Frame · corroded · May 11, 2011 · N775NC · Doug DC951 · Fuselage Main, Frame
  > AFT CARGO COMPT AFT FACE OF FRAME 1108 SPLICE UNDERNEATH OF UPPER FLANGE HAS CORROSION BETWEEN LONG 27L AND L28L. REMOVED SPLICE IAW 51-30-5. TOOLING MARK ON SPLICEOUT OF LIMITS IAW SRM 53-01 FIG 1. RECEIVED MAT.063 7075-0. RECEIVED FROM HEAT TREAT
- [SDR DALA1133199866](https://openairdocs.org/sdr/DALA1133199866.md): Frame · cracked · May 10, 2011 · N775NC · Doug DC951 · Fuselage Main, Frame
  > MAIN CABIN STA 579 RIGHT LONG 17 FRAME CRACKED. CUT OUT DAMAGE IAW DC-9 SRM 53-03 FIG 32. 1 1/4 INCH BY 3 3/4 INCH NDT VERIFY NO DAMAGE REMAINS. FABRICATED -29 FILLER.063 7075T6 IAW 53-03 FIG 32. FABRICATED -33 ANGLE.071 7075-0 PO 1120609. HEAT TREATED O
- [SDR DALA1133189866](https://openairdocs.org/sdr/DALA1133189866.md): Frame · cracked · May 10, 2011 · N775NC · Doug DC951 · Fuselage Main, Frame
  > MAIN CABIN STA 503 FRAME AT L17L CRACKED AT FASTENER CUT OUT DAMAGED SECTION 1 1/4 BY 3 3/4 IAW DC9 SRM 53-03 FIG 32. NDT VERIFIED DAMAGE REMOVED. FABRICATED 1-32 ANGLE FROM 7075-0.071. HEAT TREATED ON PEMCO TRAVELER NR 2547 NO 1585 TO 7075-T6. FABRICATED
- [SDR DALA1133179866](https://openairdocs.org/sdr/DALA1133179866.md): Floor Panel · cracked · May 10, 2011 · N775NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN-FLOOR PANEL 35 HAS 1 HAT CHANNEL CRACKED IN 2 PLACES. REMOVED CRACKED HAT CHANNEL IAW SRM DC-9 51-30-2. INSTALLED NEW HAT CHANNEL IAW SRM DC9 53-01 FIG 4 PART NR 2912282 LOT NR 1120523, P-245 Q-948 490448 10 MAY 11.
- [SDR DALA1133159866](https://openairdocs.org/sdr/DALA1133159866.md): Frame · cracked · May 10, 2011 · N775NC · Doug DC951 · Fuselage Main, Frame
  > MAIN CABIN STA 560 RIGHT LONG 17 FRAME CRACKED. AT FRAME 560L 17R CUT OUT DAMAGE SECTION 1 1/4 BY 3 3/4 IAW DC9 SRM 53-03 FIG 32. NDT VERIFIED DAMAGE REMOVED. FABRICATED 1-33 ANGLE FROM 7075-0.071. HEAT TREATED ON PEMCO TRAVELER NR 2547 NR 1585 TO 7075-T
- [SDR DALA1133139866](https://openairdocs.org/sdr/DALA1133139866.md): Frame · cracked · May 10, 2011 · N775NC · Doug DC951 · Fuselage Main, Frame
  > MAIN CABIN STA 503 FRAME CRACKED AT L17R 2 FASTENERS. AT FRAME 503 L17R CUT OUT DAMAGED SECTION 3 3/4 IAW DC-9 SRM 53-03 FIG 32 NDT VERIFIED DAMAGE REMOVED. FABRICATED 1EA -33 ANGLE FROM 7075-0 0.071. HEAT TREATED ON PEMCO TRAVELER NR 2547NO1585TO 7075-T6.
- [SDR DALA1133129866](https://openairdocs.org/sdr/DALA1133129866.md): Frame · cracked · May 10, 2011 · N775NC · Doug DC951 · Fuselage Main, Frame
  > MAIN CABIN STA 522 RIGHT LONG 17 FRAME CRACKED. CUT OUT DAMAGE IAW DC9 SRM NR 53-03 F32 NDT VERIFY NO CRACK REMAINS. FAB FILLER IAW 53-03 FIG 2 MAT.063 7075T6.FAB DRILL UP ANGLE -5.O71 70750. HEAT TREATED ON TRAVELER 216DA956. RECEIVED REPAIR ANGLE SR0953
- [SDR DALA1133109866](https://openairdocs.org/sdr/DALA1133109866.md): Frame · cracked · May 10, 2011 · N775NC · Doug DC951 · Fuselage Main, Frame
  > MAIN CABIN STA 541 FRAME AT L17R CRACKED AT FASTENER. CUT OUT DAMAGE AREA 1 1/4 BY 3 3/4 IAW 53-03 FIG 32. NDT VERIFY DAMAGE REMOVED. FAB -33 FILLER IAW 53-03 F.32. MATERIAL.071 7075-0 AND DRILL UP. HEAT TREATED ON TRAVELER 216DA956. RECEIVED ANGLE PN
- [SDR DALA1133099866](https://openairdocs.org/sdr/DALA1133099866.md): Frame · cracked · May 10, 2011 · N775NC · Doug DC951 · Fuselage Main, Frame
  > MAIN CABIN STA 465 FRAME AT L17R CRACKED AT FASTENER. CUT OUT DAMAGE IAW DC-9 SRM 53-03 FIG 32 1 1/4 BY 3 3/4. NDT VERIFY NO DAMAGE. FABRICATED FILLER IAW 53-03 FIG 32.063 7075T6 IAW 53003 FIG 32. FABRICATED -33 ANGLE.071 7075T0 HEAT TREATED ON TRAVELER 21
- [SDR DALA1132949866](https://openairdocs.org/sdr/DALA1132949866.md): Attach Bracket · cracked · May 10, 2011 · N775NC · Doug DC951 · Fuselage Miscellaneous Structure
  > AFT ACC COMPT STA 1314 RT INTERCOSTAL SUPPORT BEAM LOWER END ATTACH BRACKET CRACKED. REMOVED CRACKED BRACKET. FABRICATED NEW BRACKET FROM BAC1505-100437 7075 T6.100. DRILLED AND DEBURED AND ALODINED AND PRIMED AND INST IAW DC9 SRM 51-10-3 AND 51-10-4.
- [SDR DALA1132939866](https://openairdocs.org/sdr/DALA1132939866.md): Floor Support · cracked · May 10, 2011 · N775NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN PASSENGER CABIN STA 313 BL O-LBL 22 FLOOR PANEL SUPPORT IS CRACKED. REMOVED CRACKED FLOOR PNL SUPPORT FROM MAIN PASS CABIN STA 313 BL O-LBL 22. ORIG MAT.050 2024-T3. RECEIVED MAT.050 2024-T3. FABRICATED NEW FLOOR PNL SUPPORT OUT OF.050 2024-T3. LO
- [SDR DALA1132919866](https://openairdocs.org/sdr/DALA1132919866.md): Seat Track · corroded · May 10, 2011 · N775NC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN STA 200 TO 247 LBL 22 SEAT TRACK HAS CORROSION. REMOVED CORROSION FROM MAIN CABIN FLOOR TRACK STA 200 TO 247 LBL22 IAW DC9 SRM 51-10-3. FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-03 FIG 4B-1. REMOVED AND REPLACED LBL 22 SEAT TRACK STA 200 TO 302 IA

Next page: https://openairdocs.org/deregistered/N775NC-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 = 'N775NC' AND deregistration_id = 'N775NC-2014-06-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N775NC-2014-06-17/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.