# Service difficulty reports: N767NC, cancelled Nov 12, 2019 A list on [N767NC, cancelled Nov 12, 2019](https://openairdocs.org/deregistered/N767NC-2019-11-12.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 · 113 reports - [SDR DALA13004240858](https://openairdocs.org/sdr/DALA13004240858.md): Connector · loose · Jan 23, 2013 · N767NC · Doug DC951 · Light System Wiring > EMERGENCY EXIT LIGHTS INOPERATIVE ON SEATS 6-8DEF. CONNECTED CONNECTOR BEHIND SIDEWALL PANEL 8F. EMERGENCY EXIT LIGHTS NOW OPS CHECKED NORMAL. - [SDR DALA13000380858](https://openairdocs.org/sdr/DALA13000380858.md): Support Fitting · damaged · Dec 26, 2012 · N767NC · Doug DC951 · Wing Miscellaneous Structure > COMPLY WITH ERA 510021-14AD, REV ORIG REF AMDS CARDS 5740-01114-01A AND -01B. COMPLIED WITH ERA 510021-14AD, REV ORIG ON RT AND LT MLG RETRACT CYLINDER SUPPORT FITTING BORES. - [SDR DALA12014240858](https://openairdocs.org/sdr/DALA12014240858.md): Skin · corroded · Nov 28, 2012 · N767NC · Doug DC951 · Fuselage Main, Plate/Skin > AFT CARGO DOOR JAMB LOWER CENTER OF OPENING APPROX FS 1088 ACFT SKIN BULGING AND CORROSION FALLS FROM SET SCREW HOLE AND SKIN IS TAPPED (064-15) AD RELATED. R & R LOWER PAN SECTION ON AFT CARGO DOORJAMB LOWER AREA IAW SRM 53-05, FIG 44. R & R SEAL DEPRESOR AFT - [SDR DALA12014230858](https://openairdocs.org/sdr/DALA12014230858.md): Skin · cracked · Nov 28, 2012 · N767NC · Doug DC951 · Fuselage Main, Plate/Skin > FOUND ONE CRACK.281" LONG NOTED AT FWD CARGO DOOR FRAME FWD LOWER CORNER FUSELAGE SKIN. REPAIRED IAW DWG SR09530117 AND RESTORED ACCESS IAW AMM 25-52-01-201, PAGE 3. ACCOMPLISHED PERMANENT REPAIR IAW DWG SR09530117. - [SDR DALA12014260858](https://openairdocs.org/sdr/DALA12014260858.md): Skin · cracked · Nov 22, 2012 · N767NC · Doug DC951 · Fuselage Main, Plate/Skin > DURING L-CHECK, AT THE FWD CARGO DOOR JAMB AFT EDGE, THE SEAL DEPRESSOR AND FUSELAGE SKIN WERE FOUND CRACKED. WORK IAW ER/A 508945-14 AS FOLLOWS: SECTION II - WITHIN EVERY 8,000 CYCLES AFTER SECTION I ASSOCIATED ER/A 13-508945 ADDED. ACCOMPLISHED PERMENANT RE - [SDR DALA12013480858](https://openairdocs.org/sdr/DALA12013480858.md): Tee Fitting · cracked · Nov 16, 2012 · N767NC · Doug DC951 · Cargo/Baggage Doors > AFT CARGO DOOR INTERCOSTAL TEE FITTING ABOVE DOOR CUTOUT IS CRACKED AT BS 1100 L18R. R & R TEE FITTING AT AFT CARGO DOOR INTERCOSTAL ABOVE DOOR CUT-OUT IAW SRM 51-30-5 AND DC-9-A-20-16-00-401-926A. - [SDR DALA12000120858](https://openairdocs.org/sdr/DALA12000120858.md): Battery Pack · inoperative · May 20, 2012 · N767NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THE FIRST THREE EMERGENCY OVERHEAD LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. - [SDR DALA1159589858](https://openairdocs.org/sdr/DALA1159589858.md): Battery Pack · discharged · Oct 23, 2011 · N767NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, FOUND EMERGENCY EGRESS AISLE LIGHTING INOP, ROWS 5 THROUGH 9. REPLACED BATTERY PACK AT ROW 7 POWER SUPPLY. - [SDR DALA1149299858](https://openairdocs.org/sdr/DALA1149299858.md): Channel · cracked · Aug 20, 2011 · N767NC · Doug DC951 · Fuselage Main, Bulkhead > CRACKED J CHANNEL ON APB - CRACKED. PERFORMING INSP OF APB LOWER T SECTION PER 5310-01203-01, FOUND J CHANNEL STIFFENER CRACKED AT STA 25L ON APB JUST ABOVE T ATTACH LOCATION. CAN BE SEEN THRU ACCESS HOLE. REMOVED CRACKED J FRAME. DRILLED NEW J, INST J PE - [SDR DALA1138659858](https://openairdocs.org/sdr/DALA1138659858.md): Connector · disconnected · Jun 8, 2011 · N767NC · Doug DC951 · Light System Wiring > DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT ROW 14, RIGHT SIDE. MAINTENANCE RECONNECTED WIRE CONNECTOR AT ROW 14, RIGHT SIDE. OPERATIONAL CHECK WAS GOOD. AIRCRAFT OK FOR SERVICE. - [SDR DALA1131239858](https://openairdocs.org/sdr/DALA1131239858.md): Skin · dented · May 3, 2011 · N767NC · Doug DC951 · Fuselage Main, Plate/Skin > DURING MAINTENANCE VISIT AT STA-SA, A DENT WAS FOUND ON THE FUSELAGE SKIN AT STA 144 BETWEEN L18L AND L19L. THE DENT WAS SUBSEQUENTLY REPAIRED PER ER/A 491556-14 SECTION I. PERFORM SECTION II INSPECTION PER ER/A 491556-14 AS FOLLOWS: INITIAL INSPECTION - WI - [SDR DALA1127659858](https://openairdocs.org/sdr/DALA1127659858.md): Intercostal · worn · Apr 20, 2011 · N767NC · Doug DC951 · Fuselage Miscellaneous Structure > MAIN CABIN AT STA 617 LT SIDE, UPPER SURFACE OF INTERCOSTAL IS WORN IN SEVERAL SPOTS, AT FLOOR SUPPORT. 60-005. REMOVED 2" ANGLE AND INTERCOSTAL AT STA 617 LT SIDE IAW SRM 51-30-2 PG 1 INSTALLED REPLACEMENT INTERCOSTAL "L" ANGLE AND ATTACHED "Z" ANGLE TO FLOOR - [SDR DALA1127619858](https://openairdocs.org/sdr/DALA1127619858.md): Floorbeam · worn · Apr 20, 2011 · N767NC · Doug DC951 · Fuselage Main, Floor Beam > MAIN CABIN AT STA 636 LT SIDE, UPPER SURFACE OF FLOORBEAM IS WORN IN SEVERAL SPOTS, AT FLOOR LEVEL 60-003. BLENDED OUT DAMAGE MAIN CABIN AT STA 636 LT SIDE LBL 14 IAW SRM 51-10-3 MATERIAL THICKNESS FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1 (PG8). FABRICAT - [SDR DALA1127529858](https://openairdocs.org/sdr/DALA1127529858.md): Seat Track · corroded · Apr 19, 2011 · N767NC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK STA 200 TO 280, RBL 22 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-3 ORIGINAL MATERIAL THICKNESS IS.090" MAT LOSS RANGE FROM.040"-.060" IN SEVERAL AREAS, OUT OF LIMITS. REMOVED SEAT TRACK IAW SRM 51-30-5 FABED SEAT TRACK FROM PN 09-5300-3-151 - [SDR DALA1127499858](https://openairdocs.org/sdr/DALA1127499858.md): Skin · damaged · Apr 19, 2011 · N767NC · Doug DC951 · Fuselage Main, Plate/Skin > LOWER FUSELAGE STA Y390, BETWEEN LONGERON 28RT AND LONGERON 29R SKIN WITH DENT. COLD FORMER SKIN BACK TO ORIGINAL CONTOUR AT LOWER FUSELAGE FABED AND INST INTERNAL REPAIR DOUBLER IAW SRM 53-04, FIG 38 VIEW G NDT CHECK NO CRACKS IAW NDT SPM 06-10-01.001 MEASU - [SDR DALA1127469858](https://openairdocs.org/sdr/DALA1127469858.md): Skin · dented · Apr 19, 2011 · N767NC · Doug DC951 · Fuselage Floor Panel > CABIN FLOOR PANEL 85D HAS SHARP DENTS AND SCREWS PULLED THRU TOP SKIN. REPAIRED PUNCTURE AND CRACKED HAT CHANNELS IAW SRM 53-01, P7, FIG 1. OUT OF LIMITS IAW SRM 51-50-1, PG 1-2, ENDS OF HAT CHANNELS IAW SRM 51-10-2. NDT CHECK FOUND IAW NDT SPM 06-10-01.001 - [SDR DALA1127459858](https://openairdocs.org/sdr/DALA1127459858.md): Skin · corroded · Apr 19, 2011 · N767NC · Doug DC951 · Fuselage Floor Panel > CABIN FLOOR PANEL 32D FWD END IS BENT UP, 1EA RIVET IS HAS CORROSION AROUND SCREW HOLES ON TOP SKIN. REMOVED CABIN FLOOR PANEL. REMOVED CRACKED SECTION AND REPAIRED CABIN FLOOR PANEL IAW 53-05, FIG 1, PG10. TREATED AND PRIMED BARE AREAS IAW SRM 51-10-3, ITEM - [SDR DALA1127449858](https://openairdocs.org/sdr/DALA1127449858.md): Skin · damaged · Apr 19, 2011 · N767NC · Doug DC951 · Fuselage Floor Panel > CABIN FLOOR PANEL 9D HAS PUNCTURE IN TOP SKIN. R & R PANEL 91D FLOOR CABIN AREA IAW SRM 53-05, FIG 2, PG 9 AND 11. NDT FOUND NO CRACKS AT REPAIR AREA IAW NDT SPM 06-10-01-001. FABRICATED REPAIR FILLER AND DOUBLER IAW SRM 51-10-3, PG 31, 32, 40, 41. INSTALL - [SDR DALA1127439858](https://openairdocs.org/sdr/DALA1127439858.md): Floorbeam · corroded · Apr 19, 2011 · N767NC · Doug DC951 · Fuselage Main, Floor Beam > CABIN FLOORBEAM ANGLE STA 200 BL-0 TO RBL 20 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-3, PG 46, OUT OF LIMITS IAW SRM 53-01, PG 8, FIG 1, SHT3. REMOVED CABIN FLOOR SUPPORT ANGLE IAW SRM 51-30-5, PG 29, 30, ITEM 8, FIG 16. FABRICATED CABIN FLOOR SUPPO - [SDR DALA1127429858](https://openairdocs.org/sdr/DALA1127429858.md): Floor Skin · corroded · Apr 19, 2011 · N767NC · Doug DC951 · Fuselage Floor Panel > METAL SUB FLOOR AND EXISTING REPAIR HAS CORROSION STA 188 TO 200 BETWEEN BL-0 AND LBL 22. FABRICATED DOUBLER REPAIR IAW SRM 51-70-4, FIG 2. PG 5 & 9. TREATED & PRIMED IAW SRM 51-10-3, PG 31, PAR 14 & PG 40, PARA 21. INSTALLED 1EA INTERCOSTAL, 2EA T SUPPORT, - [SDR DALA1127419858](https://openairdocs.org/sdr/DALA1127419858.md): Floor Support · corroded · Apr 19, 2011 · N767NC · Doug DC951 · Fuselage Miscellaneous Structure > CABIN FLOOR SUPPORT ANGLE, STA 160 TO 295, BL-0 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-3, PAGE 46, PAR 26, OUT OF LIMITS IAW SRM 53-01, PG 8, REMOVED CABIN FLOOR SUPPORT ANGLE IAW SRM 51-30-5PG. FABRICATED CABIN FLOOR SUPPORT ANGLE IAW SRM 53-13-1. - [SDR DALA1127409858](https://openairdocs.org/sdr/DALA1127409858.md): Skin · damaged · Apr 19, 2011 · N767NC · Doug DC951 · Fuselage Floor Panel > CABIN FLOOR PANEL 840 HAS SHARP DENT AND PULLED SCREW THRU TOP SKIN. INSTALLED REPAIR WASHERS PANEL DAMAGED SCREW HOLE IAW SRM 51-30-1 PAGE 5. OTHER DAMAGE ON FLOOR PANEL, OUT OF LIMITS IAW SRM 53-04 FIG38. CUT OUT DAMAGE IAW SRM 53-05 PG 10 FIG 1, FABRIC - [SDR DALA1127349858](https://openairdocs.org/sdr/DALA1127349858.md): Skin · corroded · Apr 19, 2011 · N767NC · Doug DC951 · Fuselage Floor Panel > CABIN FLOOR PANEL 33D, FWD END UPPER SKIN SCREW HOLES ARE CORRODED, PULLED THRU AND WORN. REMOVED FLOOR PANEL FROM MAIN CABIN IAW MM DC9-A-53-20-01-201-925A-A, REMOVED CORROSION FROM SCREW HOLES AT OTBD SIDE OUT OF LIMITS IAW SRM 51-10-3, PAGE 46, SRM 53-01, - [SDR DALA1127299858](https://openairdocs.org/sdr/DALA1127299858.md): Bracket · cracked · Apr 19, 2011 · N767NC · Doug DC951 · Fuselage Miscellaneous Structure > FWD SERVICE DOOR BEAM NR2 AT AFT FRAME BRACKET CRACKED. VERIFIED CRACK ON BRACKET IAW NDT SPM 06-10-01.001. R & R BRACKET AT FWD SERVICE DOOR BEAM NR2 AT AFT FRAME IAW SRM 51-30-5, PARA 7B, SRM 51-30-2, PARA 8, SRM 51-30-7, PARA 6. COMPLETED AND INSPECTED. - [SDR DALA12012680858](https://openairdocs.org/sdr/DALA12012680858.md): Floorbeam · corroded · Apr 18, 2011 · N767NC · Doug DC951 · Fuselage Main, Floor Beam > FLOORBEAM BS 160 BETWEEN BL-0 AND LBL 22 HAS CORROSION. REMOVED CORROSION CABIN FLOORBEAM. REMOVED FLOORBEAM IAW SRM 51-30-5PG 29. FABRICATED FLOORBEAM. INSTALLED NEW FLOORBEAM IAW SRM 51-30-5 PG 12. - [SDR DALA1131709858](https://openairdocs.org/sdr/DALA1131709858.md): Support · corroded · Apr 17, 2011 · N767NC · Doug DC951 · Fuselage Miscellaneous Structure > PASSENGER CABIN FWD GALLEY DRAIN PAN SUPPORT STRUCTURE IS CORRODED. OUT OF LIMIT IAW DC9 SRM 51-10-3, CUT OUT DAMAGE AREA OF FLOOR WEB STA 160 RBL 52 IAW SRM 51-70-4. FABRICATED REPAIR DOUBLER IAW SRM 51-70-4, 51-10-3, INST REPAIR DOUBLER IAW SRM 51-70-4, FA - [SDR DALA1126719858](https://openairdocs.org/sdr/DALA1126719858.md): Skin · dented · Apr 17, 2011 · N767NC · Doug DC951 · Fuselage Main, Plate/Skin > LOWER FUSELAGE STA Y390 BETWEEN LONGERON 29R AND 30, EXTERNAL SKIN WITH DENT. COLD FORMED SKIN BACK TO ORIGINAL CONTOUR AT LOWER FUSELAGE STA 390 BETWEEN LONG 29R AND 30, FABBED AND INSTALLED INTERNAL REPAIR DOUBLER IAW SRM 53-04 FIG 38 VIEW G AND NDT CHECKED - [SDR DALA1126709858](https://openairdocs.org/sdr/DALA1126709858.md): Skin · dented · Apr 17, 2011 · N767NC · Doug DC951 · Fuselage Main, Plate/Skin > LOWER FUSELAGE STA Y1104, BETWEEN LONG 28R AND LONG 30 SKIN WITH DENT. COLD FORMED SKIN BACK TO ORIGINAL CONTOUR IAW SRM 53-04 FIG 38, HFEC SURFACE INSP PER NDTSPM 06-10-01.001, NO CRACKS, FABBED INTERNAL REPAIR DOUBLER 2EA FROM 2024-T3 0.032" IAW SRM 53-33-0 - [SDR DALA1126589858](https://openairdocs.org/sdr/DALA1126589858.md): Floor Panel · cracked · Apr 17, 2011 · N767NC · Doug DC951 · Fuselage Floor Panel > CABIN FLOOR PNL 95D HAS CRACK AND DENT IN TOP SKIN. FABBED FLOOR PANEL 95D USING MATERIAL SHT 7075-T6.025" BATCH 0001520995 IAW DC9 SRM 53-23-0 PG 9 AND SRM 51-10-4 PG 1, TREATED AND PRIMED IAW DC9 SRM 51-10-3 PG 40-42 AND SRM 51-10-3 PG 31-32, INSTALLED TOP - [SDR DALA1126579858](https://openairdocs.org/sdr/DALA1126579858.md): Channel · damaged · Apr 17, 2011 · N767NC · Doug DC951 · Fuselage Floor Panel > PASSENGER CABIN FLOORBOARD 60-B-50 HAT CHANNEL HAS DAMAGE. ENDS OF ALL 5 HAT CHANNELS DAMAGED & SEVERAL CRACKS IN WEB PART OF PANEL. OUT OF LIMITS PER DC9 SRM 53-05. FABBED FLOOR PANEL ASSY REF DC9 SRM 53-23-0 PG 7 FIG 4 & DWG 9923613, TREATED HAT CHANNELS - [SDR DALA1126559858](https://openairdocs.org/sdr/DALA1126559858.md): Floorboard · corroded · Apr 17, 2011 · N767NC · Doug DC951 · Fuselage Floor Panel > PASSENGER CABIN FLOORBOARD 79-50 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-3 P 46 STEP 26, FOUND TO BE OUT OF LIMITS PER SRM 53-05 PAGE 12, FABRICATED NEW PANEL 79-50 SHEET 7075T6-0.25" BATCH 0001520995 IAW SRM 51-23-0 AND 51-10-4, TREATED AND PRIMED, FA - [SDR DALA1126449858](https://openairdocs.org/sdr/DALA1126449858.md): Angle · corroded · Apr 17, 2011 · N767NC · Doug DC951 · Fuselage Miscellaneous Structure > FWD CARGO DOOR CUTOUT FWD FRAME L-ANGLE BELOW LOWEST STOP FITTING IS CORRODED. REMOVED CORROSION IAW SRM 51-10-3 PARA 26 FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FABBED REPAIR ANGLES WITH SHT 2024-T3.040" BATCH 0001900675, INSTALLED REPAIR ANGLES (2) -19,-21 - [SDR DALA1128259858](https://openairdocs.org/sdr/DALA1128259858.md): Floor Support · cracked · Apr 16, 2011 · N767NC · Doug DC951 · Fuselage Miscellaneous Structure > CABIN FLOOR SUPPORT ANGLE FOUND TO BE CRACKED AT STA 200, LBL 25. REMOVED IAW SRM 51-30-5, PG 1-3, FIG 1, MAT. ID 2652479 EXTRUSION, IAW SRM 53-13-1, PG 25, 26, FIG 11, LOCATED AND DRILLED EXTRUSION IAW SRM 51-10-4, PG 1, PARA 2. TREATED AND PRIMED IAW 51-1 - [SDR DALA1126659858](https://openairdocs.org/sdr/DALA1126659858.md): Floorboard · cracked · Apr 16, 2011 · N767NC · Doug DC951 · Fuselage Floor Panel > PASSENGER CABIN FLOORBOARD 103-50 CORNER IS CRACKED REMOVED DAMAGE IAW SRM 53-05 PG 9-10, FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-05. TREATED AND PRIMED DOUBLER AND FILLER INSTALLED REPAIR DOUBLER AND FILLER ON PASS CABIN FLOORBOARD 103-50 IAW SRM 53- - [SDR DALA1126539858](https://openairdocs.org/sdr/DALA1126539858.md): Floorboard · corroded · Apr 16, 2011 · N767NC · Doug DC951 · Fuselage Floor Panel > PASSENGER CABIN FLOORBOARD NR 21 HAS CORROSION AND IS CRACKED. REMOVED AND REPLACED PASSENGER CABIN FLOORBOARD PANEL 21, (SKIN WEB PANEL REPLACED) IAW DC9 SRM 53-20-0 PAGE 4H AND SRM 53 -05 PAGE 10. - [SDR DALA1126529858](https://openairdocs.org/sdr/DALA1126529858.md): Floor Panel · dented · Apr 16, 2011 · N767NC · Doug DC951 · Fuselage Floor Panel > CABIN FLOOR PNL 50D HAS SCREWS PULLED THRU AND DENT. REMOVED MAIN CABIN FLOOR PNL 50D PER DC9 SRM 51-30-6 PARG 5, CUT OUT DAMAGE PER DC9 53-05 PG 9-12 FABBED DOUBLER AND FILLER USING MAT. 7075-T6.032" BATCH 0001691306 AND 7075-T6.025" BATCH 0001570995 SRM - [SDR DALA1126519858](https://openairdocs.org/sdr/DALA1126519858.md): Floor Panel · damaged · Apr 16, 2011 · N767NC · Doug DC951 · Fuselage Floor Panel > FLOOR PANEL 49D HAS CRACK AT RIVET AND SCREWS ARE PULLED THRU TOP SKIN. REMOVED FLOOR PANEL 49D IAW DC-9 SRM 51-30-1, REMOVED CORR ON SCREW HOLES IAW SRM 51-10-3 PG 26-46, REMOVED HAT CHANNELS FOR REPAIR IAW SRM 51-30-2 AND SRM 53-05 PG 10, NDT INSP NO CRACKS - [SDR DALA1126509858](https://openairdocs.org/sdr/DALA1126509858.md): Floor Panel · dented · Apr 16, 2011 · N767NC · Doug DC951 · Fuselage Floor Panel > CABIN FLOOR PNL 96D HAS SEVERAL SHARP DENTS IN TOP SKIN. REMOVED HAT CHANNELS FROM CABIN FLOOR PANEL, TOP SKIN BS 1003 TO 1068 IAW SRM 51-30-2 PAG 24-26. RECEIVED NEW TOP SKIN 66" X 21" 7075-T6 PER SRM 53-23-0 FIG 6 PNL TYPE C. FABBED NEW SKIN PER DWG 59303 - [SDR DALA1126499858](https://openairdocs.org/sdr/DALA1126499858.md): Floor Support · corroded · Apr 16, 2011 · N767NC · Doug DC951 · Fuselage Miscellaneous Structure > CABIN FLOOR SUPPORT STA 160 TO 200, RBL-44 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-3 PG 46, FOUND TO BE OUT OF LIMITS IAW SRM 53-01 PG 8 FIG 1, REMOVED CABIN FLOOR SUPPORT STA 160 TO 200 RBL-44 IAW SRM 51-30-5 PG 29-30. FABBED CABIN FLOOR SUPPORT IAW - [SDR DALA1126489858](https://openairdocs.org/sdr/DALA1126489858.md): Floor Support · corroded · Apr 16, 2011 · N767NC · Doug DC951 · Fuselage Miscellaneous Structure > CABIN FLOOR SUPPORT ANGLE STA 200 BETWEEN RBL-24 AND RBL-44 HAS CORROSION. BLENDED CORROSION PER DC9 SRM 51-10-3 PG 46, MATERIAL ORIGINAL.070", MATERIAL LOST.015" FOUND TO BE OUT OF LIMITS PER SRM 51-30-5 PG 29, FABBED & DRILLED SUPPORT ANGLE P/N 5265247 9, - [SDR DALA1126699858](https://openairdocs.org/sdr/DALA1126699858.md): Skin · dented · Apr 15, 2011 · N767NC · Doug DC951 · Fuselage Main, Plate/Skin > LOWER FUSELAGE STA Y370, BETWEEN LONG 29R AND LONG 30, EXTERIOR SKIN WITH DENT. MEASURED SKIN OUT OF LIMITS IAW SRM 53-04 FIG 38 PAGE 217. COLD FORMER SKIN BACK TO ORIGINAL CONTOUR AT DENTED AREA IAW SRM 53-04 FIG 38. HFEC SURFACE INSP PER NDT SPM 06-10-01. - [SDR DALA1126479858](https://openairdocs.org/sdr/DALA1126479858.md): Doubler · cracked · Apr 15, 2011 · N767NC · Doug DC951 · Fuselage Miscellaneous Structure > BETWEEN LONGERONS 15R & 16R AT STA 1117 BRACKET-DOUBLER IS CRACKED. REMOVED BRACKET-DOUBLER DAMAGE AND FASTENERS ON STA 1117 BETWEEN LONGERON 15R AND 16R IAW SRM 53-03 PAGE 1. FABBED REPAIR PARTS 1 DOUBLER, 2EA SPLICE WITH SHEET 2014-T6.050" BATCH 000165411 - [SDR DALA1126019858](https://openairdocs.org/sdr/DALA1126019858.md): Skin · dented · Apr 14, 2011 · N767NC · Doug DC951 · Fuselage Main, Plate/Skin > LOWER FUSELAGE BS Y343 BETWEEN LONG 18R AND 19R EXTERNAL SKIN WITH DENT. REMOVED DAMAGED AREA AT LOWER FUSELAGE STA Y343 BETWEEN LONG 18R AND 19R, DIAMETER CUT OUT.550", FABRICATED AND INSTALLED INTERNAL REPAIR FINGER DOUBLER AND EXTERNAL REPAIR DOUBLER, INT - [SDR DALA1126689858](https://openairdocs.org/sdr/DALA1126689858.md): Skin · cracked · Apr 8, 2011 · N767NC · Doug DC951 · Fuselage Main, Plate/Skin > CRACKED SKIN AT FS 1123 BETWEEN STRINGERS 14, 15R. HFEC SURFACE INSPECTED IAW DC9 NDTSPM 06-10-01.001, VERIFIED CRACK MARKED ENDS APPROX 1.5" LONG, CUT OUT SKIN 1.5" LONG FABRICATED DOUBLER, FILLERS REPAIR, MAT'L DMS 1592,.032, TREATED, PRIMED, INSTALLED IAW - [SDR DALA1129989858](https://openairdocs.org/sdr/DALA1129989858.md): Skin · damaged · Apr 6, 2011 · N767NC · Doug DC951 · Fuselage Main, Plate/Skin > WEAR ON EXTERNAL DOUBLER REPAIR AT FUSELAGE SKIN BS 1108, L5R. REMOVED EXISTING EXTERNAL DOUBLER IAW SRM 51-30-2, PG 1EA. REPAIR DOUBLER, SRM 53-04, FIG 3A AND SRM 51-10-4, PARA 2. TRIMMED OUT PYLON L/E INBD EDGE IAW SRM 53-04, FIG 3A, AND SRM 54-02. TREA - [SDR DALA1129869858](https://openairdocs.org/sdr/DALA1129869858.md): Skin · damaged · Apr 6, 2011 · N767NC · Doug DC951 · Fuselage Main, Plate/Skin > FUSELAGE SKIN DOUBLER REPAIR STA 1116 TO STA 1136, BETWEEN LONGERON 16R AND LONGERON 17R, FOUND TO BE WITHIN PROX DISTANCE TO ADJACENT EXTERNAL DOUBLER REPAIR AT STA 1108, LONG 15R, VERTICAL AND HORIZONTAL DISTANCE APPROX 4.5 INCHES. NO ACTION REQUIRED. REP - [SDR DALA1129649858](https://openairdocs.org/sdr/DALA1129649858.md): Skin · damaged · Apr 6, 2011 · N767NC · Doug DC951 · Fuselage Main, Plate/Skin > FUSELAGE SKIN, EXTERNAL DOUBLER REPAIR AT STA 229 TO STA 211, L18L AND L20L FOUND TO BE WITHIN PROXIMITY DISTANCE TO ADJACENT EXT DOUBLER REPAIR, REMOVED EXISTING REPAIR IAW SRM 51-30-8, PG 4, STEP 13. FABED DOUBLER, FILLER, INTERNAL FINGER DOUBLERS IAW SR - [SDR DALA1128789858](https://openairdocs.org/sdr/DALA1128789858.md): Skin · dented · Apr 6, 2011 · N767NC · Doug DC951 · Fuselage Main, Plate/Skin > DENT ON FUSELAGE SKIN EXTERNAL DOUBLER REPAIR BS 222 TO BS 249, BETWEEN L16L AND L18L. REMOVED REPAIR DOUBLERS AND ANGLE SUPPORT FITTING, 2 EA IAW 51-30-8, PG 4 STEP 13. CUTOUT THE SKIN AREA FROM STA 224-STA 257 L17L AND L18L IAW SRM 53-04,. HFEC CUTOUT - [SDR DALA1127519858](https://openairdocs.org/sdr/DALA1127519858.md): Seat Track · cracked · Apr 4, 2011 · N767NC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings > FOUND CRACK IN SEAT TRACK AT RBL 22 AT STA 712. REMOVED SEAT TRACK FROM STA 683.5 TO 721.5, RBL 22 IAW SRM 53-05,. FABED REPAIR SPLICE PLATES AND REPLACEMENT SEAT TRACK SECTION, IAW SRM 53-05, PG 30, FIG 4D. INSTALLED SEAT TRACK AT RBL 22R, STA 683.5 TO 721. - [SDR DALA1127509858](https://openairdocs.org/sdr/DALA1127509858.md): Fitting · cracked · Apr 1, 2011 · N767NC · Doug DC951 · Fuselage Main, Bulkhead > AFT SIDE OF BULKHEAD STA 69, RBL 15 TO WHEEL WELL PRESSURE PANEL VERTICAL FITTING CRACKED IN RADIUS AND LWR ATTACH BOLT HOLE TO EDGE OF FITTING, VIEWED THRU ACCESS 4201A FWD OF RUDDER PEDALS REMOVED IAW SRM 51-30-5, PG 29, FABRICATED NOSE GEAR BEAM ATTACH FIT Next page: https://openairdocs.org/deregistered/N767NC-2019-11-12/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 = 'N767NC' AND deregistration_id = 'N767NC-2019-11-12' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N767NC-2019-11-12/reports --- 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, except the copies of manufacturers’ service documents, which belong to their rights holders.