# Service difficulty reports: N779NC, cancelled May 16, 2017

A list on [N779NC, cancelled May 16, 2017](https://openairdocs.org/deregistered/N779NC-2017-05-16.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 · 165 reports

- [SDR DALA13037350870](https://openairdocs.org/sdr/DALA13037350870.md): Wire · broken · Jul 31, 2013 · N779NC · Doug DC951 · Light System Wiring
  > SEAT MOUNTED EMERGENCY LIGHT AT 6DE INOPERATIVE. FOUND BROKEN WIRE AND REPAIRED IAW CHAPTER 20 WSPM AND EWIS.
- [SDR DALA13000860870](https://openairdocs.org/sdr/DALA13000860870.md): Wire · broken · Jan 10, 2013 · N779NC · Doug DC951 · Light System Wiring
  > EMERGENCY LIGHT BLACK WIRE BROKEN & HANGING LOOSE UNDER SEAT 9F. SECURED BROKEN WIRE IAW SWPM 20-20-03. OPS CHECKED NORMAL. OK FOR SERVICE.
- [SDR DALA12013490870](https://openairdocs.org/sdr/DALA12013490870.md): Connector · unsecure · Nov 19, 2012 · N779NC · Doug DC951 · Light System Wiring
  > EMERGENCY PATHWAY LIGHT INOPERATIVE AT SEAT 6R. SECURED CONNECTOR UNDER SEAT. CHECKED GOOD.
- [SDR DALA12005370870](https://openairdocs.org/sdr/DALA12005370870.md): Slide · unserviceable · Aug 15, 2012 · N779NC · Doug DC951 · Escape Slide
  > DURING LINE CHECK, MAINTENANCE FOUND THE 1R DOOR SLIDE PRESSURE READING ZERO. MAINTENANCE REPLACE THE DOOR SLIDE AND RETURNED THE AIRCRAFT TO SERVICE.
- [SDR DALA12000490870](https://openairdocs.org/sdr/DALA12000490870.md): Fastener · loose · May 25, 2012 · N779NC · Doug DC951 · Aerodynamic Fairings
  > DURING LINE CHECK, MAINTENANCE FOUND THE LOCK FASTENER LOOSE ON THE TAIL CONE DOOR HATCH. MAINTENANCE REPLACED THE RECEPTICAL, SECURED THE FASTENER AND RETURNED THE AIRCRAFT TO SERVICE.
- [SDR DALA1170639870](https://openairdocs.org/sdr/DALA1170639870.md): Battery · discharged · Dec 20, 2011 · N779NC · Doug DC951 · Emergency Lighting
  > EMERGENCY EGRESS AISLE LIGHTS INOP AT ROWS 19, 20, 21, 22 AND 2R LOWER EXIT SIGN. REPLACED POWER SUPPLY BATTERIES, CHECKS OK.
- [SDR DALA1167049870](https://openairdocs.org/sdr/DALA1167049870.md): Light · inoperative · Dec 4, 2011 · N779NC · Doug DC951 · Emergency Lighting
  > EMERGENCY EGRESS AISLE LIGHTS INOP AT ROWS 13, 14 AND 16. REPLACED AISLE LIGHT ASSEMBLY, CHECKS OK.
- [SDR DALA1160479870](https://openairdocs.org/sdr/DALA1160479870.md): Battery Pack · discharged · Oct 26, 2011 · N779NC · Doug DC951 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST FOUND PATH LIGHT ROW 9 TO ROW 13 AND FORWARD OVER WING EXIT SIGN INOP. THE BATTERY PACK AND FUSE WERE REPLACED AND TESTS OK.
- [SDR DALA1154699870](https://openairdocs.org/sdr/DALA1154699870.md): Connector · disconnected · Sep 19, 2011 · N779NC · Doug DC951 · Light System Wiring
  > DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING AT ROW 17 INOPERATIVE. MAINTENANCE RECONNECTED THE ROW 17 EMERGENCY ESCAPE PATH LIGHT WIRE CONNECTOR. OPERATIONAL CHECK WAS NORMAL.
- [SDR DALA1125959870](https://openairdocs.org/sdr/DALA1125959870.md): Power Supply · inoperative · Apr 15, 2011 · N779NC · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT IDENTIFIER AT THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM.
- [SDR DALA1123829870](https://openairdocs.org/sdr/DALA1123829870.md): Cusp Web · damaged · Apr 1, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN PASSENGER CABIN R1 DOOR PAN REQUIRE CUT FOR R1 DOOR CUSP REPAIR. CUT OUT DOOR PAN IAW DC-9 SRM 53-05 FIG 55. RECEIVED NEW PAN PN 5912492-1. LOCATED, DRILLED AND INSTALLED NEW PAN IAW DC-9 SRM 53-05 FIG 55. WEIGHT FOR REPAIR 8.3 OZ NDT VERIFIED DAMAGE
- [SDR DALA1123819870](https://openairdocs.org/sdr/DALA1123819870.md): Door Frame · damaged · Apr 1, 2011 · N779NC · Doug DC951 · Fuselage Main, Structure
  > MAIN PASSENGER CABIN FWD SERVICE DOOR JAMB REPAIR 53-05 FIG 55 DOOR SPLICE -43 SPLICE HOLES FALL IN RADIUS. FAB -43 SPLICE FROM MAT.071 2024-0. HEAT TREATED TO.071 2024-T42 ON PEMCO TRAVELER 2469NO1540. DRILLED AND INSTALLED -43 SPLICE IAW DC9 ERA 490833-
- [SDR DALA1123809870](https://openairdocs.org/sdr/DALA1123809870.md): Cusp Web · corroded · Apr 1, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN CUSP ANGLE UNDER R-1 DOOR PAN HAS CORROSION. LOSS OUT OF LIMITS IAW DC-9 SRM 51-10-3. REMOVED CUSP ANGLE FROM STA 164-227 RBL 59. LOCATED AND DRILLED NEW ANGLE AND INSTALLED ANGLE IAW DC-9 SRM 53-05 FIG 55 WEIGHT OF REPAIR PARTS IS 7.8 INSTALLED
- [SDR DALA1123799870](https://openairdocs.org/sdr/DALA1123799870.md): Floor Panel · corroded · Apr 1, 2011 · N779NC · Doug DC951 · Fuselage Floor Panel
  > CORROSION ON CABIN FLOOR PNL 21. REMOVED CORROSION IAW DC9 SRM 51-10-3 FIG 1. AFTER BLEND THICKNESS IS.005, OUT OF LIMITS IAW DC9 SRM 53-01. CUT OUT DAMAGE IAW DC9 SRM 53-01. (1) HFEC INSP IAW NDT SPM 06-10-01.001. NO CRACKS NOTED A2700. FABRICATED AND I
- [SDR DALA1123499870](https://openairdocs.org/sdr/DALA1123499870.md): Floor Panel · cracked · Mar 31, 2011 · N779NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 97 IS CRACKED AT FASTENER HOLE AFT END OF PANEL. REMOVED DAMAGE AT AFT END OF PNL IAW SRM 53-01, FIG 4. HFEC INSP IAW NDT SPM 06-10-01.001. FOUND DAMAGE REMOVED. REPAIRED PANEL IAW SRM 53-01, FIG 4, ERA 490832-14 & MFG DWG 9919600.
- [SDR DALA1123049870](https://openairdocs.org/sdr/DALA1123049870.md): Channel · broken · Mar 29, 2011 · N779NC · Doug DC951 · Fuselage Floor Panel
  > MAIN PASSENGER CABIN FLOOR PANEL 70 AFT END HAT CHANNEL BROKEN AT FASTENER HOLE. REMOVED & REPLACED 4 EA HAT CHANNELS IAW DC-9 SRM 51-30-2 & ERA 490831-14. REMOVED PREVIOUS MISDRILLED REPAIR & REPAIRED PANEL IAW DC-9 SRM 53-05 FIG 1 & 51-30-2. INSTALLED 2 E
- [SDR DALA1123019870](https://openairdocs.org/sdr/DALA1123019870.md): Floor Panel · corroded · Mar 29, 2011 · N779NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 37 HAS CORROSION ON TOP OF PANEL. REMOVED CORR. 6X1 INCH IAW DC-9 SRM 53-01 FIG 1 AND CARD 5100-01570-01. ORIG MATERIAL.020 REMOVED.013 REMAINING MAT.007 OUT OF LIMITS. FABBED NEW PNL FROM.025 7075-T6 IAW DWG9957918 AND ERA 490827-
- [SDR DALA1122789870](https://openairdocs.org/sdr/DALA1122789870.md): Floor Panel · cracked · Mar 28, 2011 · N779NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 60C HAS 4EA HAT CHANNELS CRACKED ON BOTTOM OF PANEL. REMOVED 5EA HAT CHANNELS IAW SRM 51-30-2. FOUND WEB CRACKED, FABRICATED, LOCATED, DRILLED AND DEBURRED TO SKIN WITH.025 7075-T6 IAW ERA 490830-14. TRIMMED, LOCATED, DRILLED AND DEB
- [SDR DALA1122739870](https://openairdocs.org/sdr/DALA1122739870.md): Frame · cracked · Mar 28, 2011 · N779NC · Doug DC951 · Fuselage Main, Frame
  > AFT ACCESSORY COMPARTMENT CANTED FRAME 1243 IS CRACKED AT L4R. REMOVED CANTED FRAME AT STA 1243 IAW DC-9 SRM 51-30-5 AND 51-30-2. LOCATED AND DRILLED NEW FRAME P/N SR09530086-81 IAW DC9 SRM 51-10-4. INSTALLED NEW FRAME IAW DC9 SRM 51-30-5 P-102.
- [SDR DALA1122539870](https://openairdocs.org/sdr/DALA1122539870.md): Floor Panel · damaged · Mar 27, 2011 · N779NC · Doug DC951 · Fuselage Floor Panel
  > MAIN PASSENGER CABIN FLOOR PANEL 72 TOP SKIN HOLE PUNCH CUTOUT DAMAGE IAW DC9 SRM 53-01. HFEC INSP IAW NDT SPM 06-10-01.001. NO CRACKS NOTED. FABRICATED FILLER AND DOUBLER FROM 7075-T6.025 LOT 1120200 IAW DC9N SRM 53-01. INSTALLED FILLER AND DOUBLER IAW D
- [SDR DALA1122459870](https://openairdocs.org/sdr/DALA1122459870.md): Keelbeam · corroded · Mar 27, 2011 · N779NC · Doug DC951 · Fuselage Main, Keel
  > LEFT KEEL AREA STA 712 BETWEEN L29L AND L30 FRAME HAS CORROSION. REMOVED CORROSION IAW DC9 SRM 51-10-3. 100 PERCENT MATERIAL LOSS. REMOVED FRAME IAW DC-9 SRM 51-30-2. LOCATED, DRILLED AND INSTALLED NEW FRAME P/N 9957740-3 IAW DC9 SRM 51-10-4, 51-30-2 AND 51
- [SDR DALA1122569870](https://openairdocs.org/sdr/DALA1122569870.md): Support Bracket · cracked · Mar 26, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN STATION 200 L4L CRACKED. REMOVED L4L STA 160-228 AND 2 EA SPLICES STA 160-180 & 116-228. INTERCOSTAL SUPPORT BRACKET AND ATTACHMENT CLIP TO GO IN ACCESS. LOCATED, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW 51-10-4, 51-20-2, 51-30-2. RE
- [SDR DALA1122529870](https://openairdocs.org/sdr/DALA1122529870.md): Cusp Web · cracked · Mar 25, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 1132 LBL 44 LEFT SIDE CUSP WEB CRACKED APPROX 2 INCHES UNDER SEAT TRACK. REMOVED DAMAGED AREA 12"X 12". NDT VERIFIED DAMAGE REMOVED IAW NDT SPM 06-10-01.001. FABRICATED, LOCATED, DRILLED, DEBURRED AND INSTALLED NEW WEB AND SPLICE. INSTALLED
- [SDR DALA1122509870](https://openairdocs.org/sdr/DALA1122509870.md): Longeron · cracked · Mar 25, 2011 · N779NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > MAIN CABIN STATION 200 LONGERON L2L CRACKED. REMOVED 32 INCHES OF L2L & 2 EA SPLICES. REMOVED CENTER AC DUCT STA 180 FOR ACCESS. RECEIVED NEW CAST FORM MAT P/N S2777922-3, LOCATE, DRILL, TRIM, DEBURRED, TREAT, PRIME & INSTALL IAW SRM 51-10-2, 51-30-2, 51-30
- [SDR DALA1121939870](https://openairdocs.org/sdr/DALA1121939870.md): Floor Support · corroded · Mar 24, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 200 RBL 47 TO 57 FLOOR SUPPORT HAS CORROSION. REMOVED FLOOR SUPPORT IAW DC-9 SRM 51-30-5. REMOVED CORROSION IAW DC-9 SRM 51-10-3. ORIG MAT.060 MAT REMOVED.050 MAT REMAIN.010. FOUND TO BE OUT OF LIMITS L=8.00 W: 1.75D=.050 IAW DC-9 SRM 53-
- [SDR DALA1121879870](https://openairdocs.org/sdr/DALA1121879870.md): Cusp Web · cracked · Mar 23, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN PAX CABIN RT SIDE CUSP WEB HAS 1EA CRACKED AT RBL 40 AFT 1 INCH FROM FLOORBEAM BS 239. REMOVED DAMAGE FROM WEB IAW DC9 SRM 53-10-16-801-663A FIG 2. HFEC INSP IAW DC9 NDT SPM 06-10-01. FOUND DAMAGE REMOVED INSTALLED 1EA REPAIR DOUBLER.020 7075T6 CLAD I
- [SDR DALA1121869870](https://openairdocs.org/sdr/DALA1121869870.md): Angle · broken · Mar 23, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 225 RBL 56 Z-ANGLE BROKEN OUT AT FASTENER HOLE. REMOVED Z-ANGLE IAW DC-9 SRM 51-30-2. RECEIVED NEW Z-ANGLE IAW DC-9 SRM 51-10-1. LOCATED, DRILLED & DEBURRED Z-ANGLE IAW DC-9 SRM 51-10-4. INSTALLED NEW Z-ANGLE IAW DC-9 SRM 51-30-5.
- [SDR DALA1121819870](https://openairdocs.org/sdr/DALA1121819870.md): Frame · damaged · Mar 23, 2011 · N779NC · Doug DC951 · Fuselage Main, Frame
  > MAIN PAX CABIN/GALLEY HOLE IN EXISTING FRAME REPAIR BLOWN OUT AT STA 1151 AND L-17-L. REMOVED EXISTING REPAIR IAW SRM 51-30-2, 51-30-5. FABBED NEW REPAIR PLATE.063 7070-T6. FABBED REPAIR ANGLE & FILLER.050 7075-0. TREATED & PRIMED IAW DC-9 SRM 51-10-3.
- [SDR DALA1121579870](https://openairdocs.org/sdr/DALA1121579870.md): Gusset · gouged · Mar 22, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 832 LBL-10 GUSSET GOUGED. REJECTED FOR GUSSET IMPROPERLY INSTALLED. FABBED, LOCATED, DRILLED, COUNTERSUNK AND DEBURRED GUSSET IAW DC9 SRM 51-10-4 & DOUGLAS DWG 4915719. INSTALLED GUSSET IAW DC9 SRM 51-30-2.
- [SDR DALA1121559870](https://openairdocs.org/sdr/DALA1121559870.md): Floor Support · corroded · Mar 22, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 160 TO 200 RBL 44 FLOOR SUPPORT HAS CORROSION. REMOVED 1 EA FLOOR SUPPORT IAW SRM 51-30-5. REMOVED CORR IAW SRM 53-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-01. FABBED 1 EA FLOOR SUPPORT MAT S2652479-7075-T6511. LOCATED, DRILLED & DEBUR IAW
- [SDR DALA1121549870](https://openairdocs.org/sdr/DALA1121549870.md): Diaphragm · damaged · Mar 22, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN - FASTENER HOLE IN DIAPHRAGM TORN STA 172 RBL 44. REMOVED DAMAGE IN 3 EA PLACES.400" IN DIAMETER IAW DC9 SRM 53-01. HFEC INSP IAW NDT SPM 06-10-01.001. NO CRACKS NOTED. FABBED DOUBLER 7075-T6 IAW DC-9 SRM 53-13-1 FIG 11. TREATED & PRIMED DOUBL
- [SDR DALA1121539870](https://openairdocs.org/sdr/DALA1121539870.md): Diaphragm · damaged · Mar 22, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE IN DIAPHRAGM AT STA 198 AND RBL 46. REMOVED DAMAGE IN 1EA PLACE.500 IN DIAMETER IAW DC-9 SRM 53-01. HFEC INSP IAW NDT SPM 06-10-01.001. NO CRACK NOTED. FABBED DOUBLER 7075-T6 IAW DC-9 SRM 53-13-1 FIG 11. TREATED AND PRIMED DOUBLER IAW DC-9
- [SDR DALA1121279870](https://openairdocs.org/sdr/DALA1121279870.md): Frame Splice · corroded · Mar 21, 2011 · N779NC · Doug DC951 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT FRAME AT STA 1116 HAS CORROSION ON LOWER AFT FLANGE SPLICE ANGLE BETWEEN LONG 28L AND LONG 30. FOUND SPLICE OUT OF LIMITS IAW DC9 SRM 53-01. REMOVED SPLICE IAW DC9 SRM 51-30-5. FABBED NEW SPLICE FROM 7075-0.050. HEAT TREATED TO TO 7075T6
- [SDR DALA1121269870](https://openairdocs.org/sdr/DALA1121269870.md): Attach Bracket · corroded · Mar 21, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > FWD CARGO STA 365 RBL 6 SURFACE CORROSION. REMOVED CORR 1 X 3 INCHES ON SURFACE OF ATTACH BRACKET. ORIG MAT.100 REMOVED.035 REMAINING.065. FOUND TO BE OUT OF LIMITS. RECEIVED, SEALED AND INSTALLED NEW BRACKET P/N 3457317-1. ALL WORK ACCOMPLISHED IAW DC
- [SDR DALA1121249870](https://openairdocs.org/sdr/DALA1121249870.md): Cusp Web · cracked · Mar 21, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN PASSENGER CABIN STA 435 LT CUSP WEB CRACKED. CUT OUT DAMAGED AREA 2"X 3.5". NDT VERIFIED DAMAGE REMOVED IAW NDT SPM 06-10-01. FABBED AND INSTALLED DOUBLER AND FILLER FROM 7075-T6.025 & 7075T6.020 IAW DC9 SRM 53-10-16.
- [SDR DALA1121239870](https://openairdocs.org/sdr/DALA1121239870.md): Floor Panel · corroded · Mar 21, 2011 · N779NC · Doug DC951 · Fuselage Floor Panel
  > CORROSION ON CABIN FLOOR PNL 16. FABRICATED NEW FLOOR PANEL IAW ER/A 490110-14 AND DC08 SRM 51-10-2. ASSEMBLED FLOOR PANEL IAW DC9 SRM 51-30-2. TREATED AND PRIMED PANEL IAW DC9 SRM 51-10-3. DRILLED AND COUNTERSUNK HOLES IAW DC-9 SRM 51-10-4.
- [SDR DALA1121229870](https://openairdocs.org/sdr/DALA1121229870.md): Floor Panel · cracked · Mar 21, 2011 · N779NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 84 CRACKED AT FWD I/B EDGE. STOP DRILLED CRACK IAW DC9 SRM 53-01. NDT VERIFIED CRACK CONTAINED IAW NDT SPM 06-10-01. FABBED AND INSTALLED REPAIR DOUBLER FROM 7075 T6.020 IAW DC-9 SRM 53-01.
- [SDR DALA1121219870](https://openairdocs.org/sdr/DALA1121219870.md): Longeron Splice · corroded · Mar 21, 2011 · N779NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT LONG 28L SPLICE HAS EXFOLIATED CORROSION BETWEEN BS 237 AND BS 229. REMOVED DAMAGED SPLICE. SEALED AND REPLACED WITH NEW SPLICE IAW DC9 SRM 51-30-2, 51-10-4, 51-10-3, 51-20-0, 51-30-5.
- [SDR DALA12012260870](https://openairdocs.org/sdr/DALA12012260870.md): Skin · cracked · Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR BS 1209 BETWEEN L13-14R SKIN CRACKED AT FASTENER. CUTOUT DAMAGED AREA 1.5"X 1.5" NDT VERIFIED CRACK REMOVED IAW NDT SPM 06-10-01. FABBED AND INSTALLED FILLER AND DOUBLER FROM.040" 7075-T6 PO#1023415 IAW SRM 53-01 FIG 4. REPAIR INSTALLED WITH
- [SDR DALA1120699870](https://openairdocs.org/sdr/DALA1120699870.md): Hinge · cracked · Mar 18, 2011 · N779NC · Doug DC951 · Trailing Edge Flaps
  > LT WING NR 3 FLAP HINGE FLAP HALF OF THE HINGE IS CRACKED. REMOVED AND REPLACED NR 3 FLAP HINGE HALF IAW CARD 5753-9893M-LT.
- [SDR DALA1120649870](https://openairdocs.org/sdr/DALA1120649870.md): Skin · cracked · Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR CANTED FRAME STA 1292 BETWEEN LONG 13-14L SKIN CRACKED AT FASTENER. REMOVED DAMAGE 1 5/8"X 1 1/16". NDT VERIFIED DAMAGE REMOVED IAW NDT SPM 06-10-01. FABBED FILLER AND DOUBLER FROM.040" 7075-T6 AND.050" 7075-T6. INSTALLED DOUBLER AND FI
- [SDR DALA1120639870](https://openairdocs.org/sdr/DALA1120639870.md): Skin · gouged · Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR STAIRS CONTROL CUTOUT SKIN BELOW HINGE GOUGED. NDT FOUND CRACK CONTAINED AT FASTENER HOLE. REMOVED STAIR CONTROL DOOR. FABBED DOUBLER FROM.032" 2024-T3 AND INSTALLED DOUBLER AND DOOR IAW SRM 53-01 FIG 4.
- [SDR DALA1120609870](https://openairdocs.org/sdr/DALA1120609870.md): Floor Panel · corroded · Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 45 HAS CORROSION ALONG FWD I/B EDGE REMOVED CORR. ORIG. MAT. 020" REMOVED.015" FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. CUT OUT DAMAGE 5.75 X 1.75 INCHES NDT INSP VERIFIED DAMAGE REMOVED IAW NDT SPM 06-10-01. FABBED DOUBLER AND
- [SDR DALA1120599870](https://openairdocs.org/sdr/DALA1120599870.md): Structure · misrepaired · Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 785 RBL 50 PREVIOUS REPAIR NOT MEETING FASTENER REQUIREMENT. REMOVED EXISTING REPAIR IAW SRM 51-30-2. FABBED AND INSTALLED FILLER.040" 7075-T6 AND DOUBLER.050" 7075-T6 IAW SRP DC-9 A-53-10-16-801-663A-A.
- [SDR DALA1120589870](https://openairdocs.org/sdr/DALA1120589870.md): Floor Panel · corroded · Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Floor Panel
  > CORROSION ON CABIN FLOOR PANEL 20. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. CUT OUT DAMAGED SECTION OF FLOOR PANEL 1.5"X 4". FABBED AND INSTALLED NEW SECTION OF PANEL FROM.032" 2024-T3 IAW DWG 9957828 AND SRM 53-01 FIG 4.
- [SDR DALA1120559870](https://openairdocs.org/sdr/DALA1120559870.md): Floor Panel · corroded · Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 33 HAS CORROSION ON TOP AROUND FASTENER HOLES. REMOVED CORR OUT OF LIMITS IAW SRM 53-01 FIG 1. CUT OUT DAMAGE IN 4EA PLACES IAW SRM 53-5 FIG 1. FABBED 4EA DOUBLERS AND FILLERS FROM.025 INCH 7075-T-6 AND.032" 7075-T6. INSTALLED DOUBL
- [SDR DALA1120509870](https://openairdocs.org/sdr/DALA1120509870.md): Gusset · gouged · Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 832 LBL-10 GUSSET GOUGED. GOUGE FOUND TO BE OUT OF LIMITS 90 PERCENT MAT. LOSS IAW SRM 53-01 FIG 1. REMOVED GUSSET, FABBED NEW ONE FROM.032" 7075-0 AND HEAT TREATED TOT6 ON TRAVELER #24961416. INSTALLED NEW GUSSET IAW SRM 51-30-5 AND 51-10-3
- [SDR DALA1120499870](https://openairdocs.org/sdr/DALA1120499870.md): Support Channel · cracked · Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous Structure
  > NLG STA 106 RIGHT LONG 28 DOOR CUTOUT SUPPORT CHANNEL CRACKED APPROX 1.25 INCH. RECEIVED FORMER P/N 5913421023. REMOVED CRACKED FORMER AND REPLACED IAW SRM 51-30-05 AND 51-10-3.
- [SDR DALA1119509870](https://openairdocs.org/sdr/DALA1119509870.md): Stinger · damaged · Mar 16, 2011 · N779NC · Doug DC951 · Horizontal Stabilizer, Spar/Rib
  > HORIZONTAL STABILIZER STRINGER LT SIDE UPPER ANGLE HAS ELONGATED HOLES. REPLACED ANGLE, FABBED OUT OF.032 2024-T3 IAW SRM 55-31-00 FIG 8. SUBED 2024T43 FOR 2024-T3 IAW DC-9 SRM 51-60-0 FIG.1. LOCATED AND DRILLED IAW DC-9 SRM 51-10-04, 51-30-02 AND 51-30-05
- [SDR DALA1119499870](https://openairdocs.org/sdr/DALA1119499870.md): Cargo Track · damaged · Mar 16, 2011 · N779NC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO STA 446 LT TIE DOWN TRACK HAS 2EA HOLES IN EDGE OF SPLICE. REMOVED DAMAGED SPLICE IAW DC9 SRM 51-30-05. FOUND SPLICE TO BE MISS LOCATED ON TIE DOWN TRACK IAW DWG 5932875. FABBED 2EA SPLICE ANGLES IAW DC9 SRM 53-03. TRIMMED TO FIT & LOCATED & DRIL

Next page: https://openairdocs.org/deregistered/N779NC-2017-05-16/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 = 'N779NC' AND deregistration_id = 'N779NC-2017-05-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N779NC-2017-05-16/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.