# Service difficulty reports: N784NC, cancelled Jun 17, 2014

A list on [N784NC, cancelled Jun 17, 2014](https://openairdocs.org/deregistered/N784NC-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 3 · 122 reports

- [SDR DALA13041330875](https://openairdocs.org/sdr/DALA13041330875.md): Pulley · damaged · Aug 24, 2013 · N784NC · Doug DC951 · Aerodynamic Fairings
  > DURING AMDS 5350-01032-03, DROP CHECK, TAILCONE FAILED RELEASE CHECK. FOUND UPPER LT CABLE PULLEY DAMAGED. INSTALLED SERVICEABLE PULLEY IAW AMM 53-50. DROP CHECKED GOOD OK FOR SERVICE. REQUIRED INSPECTION COMPLETE.
- [SDR DALA13033390875](https://openairdocs.org/sdr/DALA13033390875.md): Wire · damaged · Jul 1, 2013 · N784NC · Doug DC951 · Light System Wiring
  > SEAT MOUNTED EMERGENCY LIGHT AT 7DEF INOPERATIVE. REPLACED PIG TAIL AT SEAT 7D IAW AMM 33-52. OPS CHECKED GOOD.
- [SDR DALA13023980875](https://openairdocs.org/sdr/DALA13023980875.md): Wire · exposed · May 18, 2013 · N784NC · Doug DC951 · Light System Wiring
  > SEAT 6E HAS EXPOSED WIRES. SECURED EMERGENCY LIGHT WIRES IN TRACK, CHECKED GOOD.
- [SDR DALA13022480875](https://openairdocs.org/sdr/DALA13022480875.md): Fuse · blown · May 12, 2013 · N784NC · Doug DC951 · Emergency Lighting
  > EMERGENCY SEAT MOUNTED PATH LIGHTS INOPERATIVE ROWS 9 THROUGH 13. FOUND FUSE BLOWN AT POWER PACK FWD OF LT FWD EMERG EXIT. REPLACED FUSE. OPS CK GOOD.
- [SDR DALA13012660875](https://openairdocs.org/sdr/DALA13012660875.md): Connector · damaged · Mar 19, 2013 · N784NC · Doug DC951 · Light System Wiring
  > EMERGENCY ESCAPE PATH LIGHTS AT ROW'S 7 (WHITE) AND 14 (RED) INOPERATIVE. REPLACED LIGHT ASSY AT ROW 7 AND REPLACED CONNECTOR AT ROW 14 - CHECKED GOOD IAW AMM 33-53.
- [SDR DALA13006910875](https://openairdocs.org/sdr/DALA13006910875.md): Connector · unsecure · Feb 8, 2013 · N784NC · Doug DC951 · Light System Wiring
  > DURING INSPECTION FOUND EMERGENCY PATH LIGHTS SEAT 6-7-8 INOPERATIVE, SECURED CONNECTOR AND TESTED OK.
- [SDR DALA12017200875](https://openairdocs.org/sdr/DALA12017200875.md): Battery Pack · inoperative · Dec 22, 2012 · N784NC · Doug DC951 · Emergency Lighting
  > LT AND RT OVERWING EMERGENCY LIGHTS COME ON WITH EMERGENCY LIGHT SWITCH IS SET TO ARM. TROUBLESHOT AND FOUND THE OVERWING EMERGENCY LIGHT BATTERY PACK IS BAD. R & R THE OVERWING EMERGENCY LIGHT BATTERY PACK AND PERFORMED OPS CHECK. OPS CHECK GOOD REF WDM A-3
- [SDR DALA12017190875](https://openairdocs.org/sdr/DALA12017190875.md): Battery Pack · inoperative · Dec 22, 2012 · N784NC · Doug DC951 · Emergency Lighting
  > LT AND RT OVERWING EMERGENCY LIGHTS COME ON WITH EMERGENCY LIGHT SWITCH IS SET TO ARM. TROUBLESHOT AND FOUND THE OVERWING EMERGENCY LIGHT BATTERY PACK IS BAD. R & R THE OVERWING EMERGENCY LIGHT BATTERY PACK AND PERFORMED OPS CHECK. OPS CHECKED GOOD REF WDM
- [SDR DALA12017180875](https://openairdocs.org/sdr/DALA12017180875.md): Longeron · cracked · Dec 20, 2012 · N784NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > LONGERON CRACKED UNDER FRAME AT BS 389 AND L17R. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-02.
- [SDR DALA12016830875](https://openairdocs.org/sdr/DALA12016830875.md): Longeron · cracked · Dec 13, 2012 · N784NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > LONGERON CRACKED UNDER FRAME AT BS 389 & L17R. R & R LONGERON 17R IAW SRM 53-02, FIG 18. INSTALLED ID REPAIR TAG IAW DPS 900-5-1-NR 4.
- [SDR DALA12000480875](https://openairdocs.org/sdr/DALA12000480875.md): Wire · broken · May 28, 2012 · N784NC · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THE CENTER TAIL SECTION EMERGENCY LIGHT TO BE INOPERATIVE. UPON INSPECTION, MAINTENANCE FOUND THE LIGHT ASSEMBLY WIRE TO BE BROKEN. MAINTENANCE REPAIRED THE WIRE, REPLACED THE LIGHT ASSEMBLY, REMOVED AND REINSTALLED THE BL
- [SDR DALA12000470875](https://openairdocs.org/sdr/DALA12000470875.md): Light · inoperative · May 28, 2012 · N784NC · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT 7D TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION AFTER A FUNCTIONAL CHECK OF THE SYSTEM.
- [SDR DALA1217129875](https://openairdocs.org/sdr/DALA1217129875.md): Fuse · blown · Mar 18, 2012 · N784NC · Doug DC951 · Emergency Lighting
  > EMERGENCY EGRESS AISLE LIGHTING INOP, ROWS 5 THROUGH 8. REPLACED FUSE AT RIGHT OVERWING POWER SUPPLY, CHECKS NORMAL.
- [SDR DALA1209609875](https://openairdocs.org/sdr/DALA1209609875.md): Power Supply · inoperative · Feb 19, 2012 · N784NC · Doug DC951 · Emergency Lighting
  > EMERGENCY EGRESS AISLE LIGHTS INOPERATIVE, ROWS 5 THROUGH 8, AND RIGHT FORWARD OVERWING EXIT SIGN. REPLACED POWER SUPPLY AND LIGHT ASSEMBLY, CHECKED GOOD.
- [SDR DALA1205099875](https://openairdocs.org/sdr/DALA1205099875.md): Fuse · blown · Jan 30, 2012 · N784NC · Doug DC951 · Emergency Lighting
  > LEFT FORWARD OVERWING EXIT VERTICAL SIGN INOPERATIVE. REPLACED FUSE AND BATTERY SET. OPS CHECK GOOD.
- [SDR DALA12015770875](https://openairdocs.org/sdr/DALA12015770875.md): Skin · dented · Sep 3, 2011 · N784NC · Doug DC951 · Fuselage Main, Plate/Skin
  > RT FUSELAGE SKIN IS DENTED BETWEEN STA 239, 6 INCHES BELOW CUSP LINE. DENT MEASURES 1"X 8"X.025" DEEP. EDDY CURRENT DENT NO CRACKS FOUND. P
- [SDR DALA1150469875](https://openairdocs.org/sdr/DALA1150469875.md): Battery · discharged · Aug 26, 2011 · N784NC · Doug DC951 · Emergency Lighting
  > MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT ROWS 5 - 8 AND RIGHT FORWARD EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED BATTERIES AND FUSE ON RIGHT SIDE. LIGHTS RETURNED TO NORMAL OPERATION.
- [SDR DALA1142619875](https://openairdocs.org/sdr/DALA1142619875.md): Power Supply · inoperative · Jul 4, 2011 · N784NC · Doug DC951 · Emergency Lighting
  > MAINTENANCE FOUND THE RIGHT FORWARD EXIT AND ROWS 5 - 8 EMERGENCY EXIT LIGHTS INOPERATIVE. HOUSING WAS ALSO BROKEN ON RIGHT FORWARD EMERGENCY EXIT LIGHT. MAINTENANCE REPLACED THE RIGHT FORWARD EMERGENCY LIGHT POWER SUPPLY PER AMM. OPERATIONAL CHECK WAS OK.
- [SDR DALA1139929875](https://openairdocs.org/sdr/DALA1139929875.md): Fuse · blown · Jun 17, 2011 · N784NC · Doug DC951 · Emergency Lighting
  > MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING FROM SEAT ROWS 5 THROUGH 8 DO NOT ILLUMINATE. MAINTENANCE REPLACED THE FUSE IN RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT PER AMM. AIRCRAFT OK FOR SERVICE.
- [SDR DALA1134269875](https://openairdocs.org/sdr/DALA1134269875.md): Power Supply · inoperative · May 13, 2011 · N784NC · Doug DC951 · Emergency Lighting
  > MAINTENANCE FOUND LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY B5-49 IN ACCORDANCE WITH WDM AND AMM. OPERATIONAL CHECK GOOD.
- [SDR DALA1134109875](https://openairdocs.org/sdr/DALA1134109875.md): Fairing · corroded · May 13, 2011 · N784NC · Doug DC951 · Fuselage Main, Plate/Skin
  > LWR FUSELAGE FROM STA Y851 TO STA Y927 BTWN L20 RT AND 30. FAIRING ATTACH POINTS WITH CORROSION AND MISSING STRAP. REMOVED CORROSION FROM BODY FAIRING ATTACH IAW SRM 51-10-3 IN LIMITS BTWN STA Y911-STA Y931 S21R -26R IN LIMITS BTWN STA Y891 - Y911 S26 DOUBLE
- [SDR DALA1133739875](https://openairdocs.org/sdr/DALA1133739875.md): Floor Panel · cracked · May 12, 2011 · N784NC · Doug DC951 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL NR 17-50 IS CRACKED AND EDGE DAMAGED. FABRICATED AND INSTALLED HAT CHANNELS AND SKIN IAW SAA ERA 491550-14 REV ORIGINAL INST ID TAG IAW PS 900-5-1 NR 4 COMPLETED.
- [SDR DALA1133729875](https://openairdocs.org/sdr/DALA1133729875.md): Floor Panel · delaminated · May 12, 2011 · N784NC · Doug DC951 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL NR 76-50 IS DELAMINATED. FABRICATED AND INSTALLED HAT CHANNELS AND SKIN, DOUBLER AND SUPPORT IAW SAA ERA 491550-14, REV ORIGINAL, FLOOR PANEL 76-50.
- [SDR DALA1133709875](https://openairdocs.org/sdr/DALA1133709875.md): Doubler · corroded · May 12, 2011 · N784NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FWD CARGO COMPARTMENT RT ALT STATIC PORT INTERNAL DOUBLER WITH CORROSION. CORROSION REMOVAL WAS FOUND TO BE OUT OF LIMITS PER SRM 53-01 PG 1-4. REMOVED AND REPLACED T PER SRM 57-30-2 PG 24. AERODYNAMIC TEST FOR STATIC PORT MISMATCH PORT AND RIVETS WAS.001
- [SDR DALA1133529875](https://openairdocs.org/sdr/DALA1133529875.md): Shear Tie · damaged · May 11, 2011 · N784NC · Doug DC951 · Fuselage Internal Mounting Structure
  > SHEAR TIE MISLOCATED AT FS 579 BETWEEN L29R AND L30. REMOVED DAMAGE AT FORMER SHEAR TIE SECTION PER SRM 53-03, FABRICATED NEW SHEAR TIE SECTION PER SRM 53-03, HEAT TREATED SHEAR TIE TRAVELER NR 87360810001 LOCATED AND DRILLED SHEAR TIE SECTION PER SRM 51-10-4
- [SDR DALA1133169875](https://openairdocs.org/sdr/DALA1133169875.md): Seat Track · broken · May 10, 2011 · N784NC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN LT OTBD SEAT TRACK STA 440, HAS A SECTION OF LUG BROKEN OFF OF THE CROWN OF TRACK. FABRICATED SEAT TRACK IAW SRM 53-23-0 FIG 1, CUT OUT DAMAGED AREA LT OTBD SEAT TRACK STA 436-454 IAW SRM 53-05. LOCATED AND DRILLED HOLES 2 NEW SPLICE IAW SRM 51-1
- [SDR DALA1133029875](https://openairdocs.org/sdr/DALA1133029875.md): Hinge · worn · May 10, 2011 · N784NC · Doug DC951 · Wing, Control Surface Attach Fittings
  > RT WING, STA XRS 353, T/E FLAP HINGE BUSHING WORN. REMOVED AND REPLACED RT WING FLAP HINGE IAW AMM 57-40-01-201-925A AND AMM 20-16-00-401-926A-A. REMOVED CABLE BLOCKS ON AILERON RT CTRL CABLES AND TRIM CABLES IAW AMM-57-40-01-201-925A AND AMM-27-10-00-501-9
- [SDR DALA1132979875](https://openairdocs.org/sdr/DALA1132979875.md): Doubler · cracked · May 10, 2011 · N784NC · Doug DC951 · Fuselage Main, Plate/Skin
  > LWR FUSELAGE LT SIDE, STA Y 130.5,-Z22 EXTERNAL EXISTING REPAIR DOUBLER WITH CRACK. REMOVED AND REPLACED DAMAGED LATCH SKIN DOUBLER WITH DOUBLER P/N 09-5300-3-0925, BATCH NR 0002028806 REF SRM 53-04 FIG 24. IDENTIFIED REPAIR PER PS 900-5-1 NR 4.
- [SDR DALA1134069875](https://openairdocs.org/sdr/DALA1134069875.md): Skin · corroded · May 9, 2011 · N784NC · Doug DC951 · Fuselage Main, Plate/Skin
  > LWR FUSELAGE, FROM STA Y468 TO STA Y481, BTWN L29L AND L30, EXT SKIN AND EXT REPAIR DOUBLER WITH CORROSION. REMOVED AND REPLACED EXTERNAL REPAIR FILLER CORROSION REMOVED ON SKIN, REWORK AREA IN LIMITS IAW SRM 53-04, 1EA EXT REPAIR DOUBLER, 1EA REPAIR FILLER,
- [SDR DALA1133539875](https://openairdocs.org/sdr/DALA1133539875.md): Skin · dented · May 9, 2011 · N784NC · Doug DC951 · Fuselage Main, Plate/Skin
  > EXT SKIN DENT AT BS 180 AND L4L L=6", W=1", DEPTH =.064", D/X=15.625. OUT OF LIMITS PER SRM 53-04 FIG 38 DUE TO DEPTH AND PROX TO FRAME AND LONGERON. TRIMMED OUT SKIN EXT REPAIR DOUBLER, INSTALL REPAIR FINGER DOUBLER AND.050" THK REPAIR FILLER INSTALL ON TR
- [SDR DALA1132329875](https://openairdocs.org/sdr/DALA1132329875.md): Floor Panel · cracked · May 9, 2011 · N784NC · Doug DC951 · Fuselage Floor Panel
  > FLOOR PANEL NR 105 CRACK AROUND RIVETS FWD EDGE REMOVED AND INSTALLED FLOOR PANEL NR 105 PER DC-9 AMM 53-20-01. FABRICATED FLOOR PANEL NR 105 IAW DC-9 SRM 53-23-0 FIG 7 PG:11AND TREATED AND PRIMED FLOOR PANEL NR 105 PER SRM 53-10-3 PAR21 AND PG 31 PAR 14.
- [SDR DALA1132089875](https://openairdocs.org/sdr/DALA1132089875.md): Skin · dented · May 7, 2011 · N784NC · Doug DC951 · Fuselage Main, Plate/Skin
  > LT EXTERIOR FUSELAGE DENT AT B STA 256 APPROX AND BETWEEN LONG 15L AND 16L IS WITHIN 1 INCH FROM THE FRAME STRUCTURE. COLD FORMED SKIN BACK TO ORIGINAL CONTOUR TO REMOVE DENTED AREA IAW DC9 SRM 53-04 FIG 38 PG 2/7 TABLE C, FABRICATED, TREATED, PRIMED AND INS
- [SDR DALA1131689875](https://openairdocs.org/sdr/DALA1131689875.md): Floor Panel · corroded · May 5, 2011 · N784NC · Doug DC951 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL NR 79-50 HAS CORROSION. PANEL NR 79-50 REPAIRED IAW DC-9 SRM 53-23-0 PG: 8 FIGURE 5. FABBED NEW WEB PANEL IAW DC-9 SRM 53-23-0 PAGE 8 FIGURE 5. INSTALLED 2 EA HAT CHANNELS.
- [SDR DALA1131219875](https://openairdocs.org/sdr/DALA1131219875.md): Floor Panel · punctured · May 3, 2011 · N784NC · Doug DC951 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 59-50 HAS PUNCTURE. REMOVED HAT CHANNELS 2EA AT IAW DC-9 SRM 51-30-2 PG 24, 26. CUT OUT DAMAGED AREA IAW DC-9 SRM 53-05 PG 10. FABBED DOUBLER AND FILLER IAW DC-9 SRM 53-05 PG 10. TREATED AND PRIMED DOUBLER AND FILLER IAW DC-9 SR
- [SDR DALA1130909875](https://openairdocs.org/sdr/DALA1130909875.md): Support · cracked · May 2, 2011 · N784NC · Doug DC951 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON AFT MOUNT LWR BEAM SUPPORT STRUCTURE CORNER ANGLE CLIP CRACKED, VIEWED THRU ACCESS DOOR PNL 8212. REMOVED ANGLE CLIP PER SRM DC9 51-30-1, FABBED ANGLE CLIP DWG 9915500 TRAVELER 8736011001 LOCATED & DRILLED HOLES PER SRM DC -9 51-10-4 INSTALLED ANG
- [SDR DALA1130789875](https://openairdocs.org/sdr/DALA1130789875.md): Angle · cracked · May 2, 2011 · N784NC · Doug DC951 · Nacelle/Pylon, Bulkhead/Firewall
  > NR 2 STRUT LWR INNER SURFACE, ADJACENT TO AFT ENGINE MOUNT POINT, ANGLE CRACKED AT FASTENER ON AFT FACE OF BULKHEAD. REMOVED ANGLE PER SRM DC-9 51-30-1, FABBED ANGLE IAW 9915500 (-8) PER SRM DC-9 51-10-4 & 51-10-2 INSTALLED ANGLE PER SRM DC-9 51-30-5 PG 1. U
- [SDR DALA1130729875](https://openairdocs.org/sdr/DALA1130729875.md): Skin · dented · May 2, 2011 · N784NC · Doug DC951 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE, STA Y97.25, Z49, LT SIDE EXTERNAL SKIN WITH DENT, MEASURED DENT OUT OF LIMITS IAW SRM 53-04 FIG 38 CONDITION 1A. CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER AND REPAIR FILLER IAW SRM 53-01 FIG 4. HFEC SURFACE NO CRACKS NOTED AT IAW ND
- [SDR DALA1130689875](https://openairdocs.org/sdr/DALA1130689875.md): Floor Panel · corroded · May 2, 2011 · N784NC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 27 METAL THRU PLATE 2 EACH FOR LAV WATER LINES HAS CORROSION ON CABIN FLOOR PANEL 27, REMOVED 2EA. LAV WATER LINE DOUBLER IAW DC9/MD-80 SRM 51-70-02 PARA 6 PAGE 11. FABBED 2EA DOUBLER PLATE PER FSI DWG 94RS481265. BONDED 2EA DOUBLER PLATE
- [SDR DALA1130639875](https://openairdocs.org/sdr/DALA1130639875.md): Floor Panel · corroded · May 2, 2011 · N784NC · Doug DC951 · Fuselage Floor Panel
  > COCKPIT FLOOR PANEL 14 HAS SURFACE CORROSION AND SECURING FASTENERS PULLING THRU AND PUNCTURED. REMOVED COCKPIT PANEL 14 PER MM A-53-20-01-201-925A-A PG 1-4 FOUND PANEL TO BE OUT OF LIMITS PER SRM 53-05 PG 9 PAR 3 FABRICATED PANEL PER SRM 53-05 FIG 1. REINS
- [SDR DALA1130769875](https://openairdocs.org/sdr/DALA1130769875.md): Skin · dented · Apr 29, 2011 · N784NC · Doug DC951 · Fuselage Main, Plate/Skin
  > DURING MCK AT SAT, 4 EA DENTS WERE FOUND ON THE FUSELAGE SKIN, JUST AFT OF THE LOWER AFT CORNER OF THE FWD CARGO DOOR CUTOUT. PERFORM ER/A 491082-14 SECTION II AS FOLLOWS: INITIAL INSPECTION - ON OR BEFORE 25-APR-13 REPEAT INSP - EVERY 24 MOS AFTER THE INITI
- [SDR DALA1130369875](https://openairdocs.org/sdr/DALA1130369875.md): Vane · damaged · Apr 29, 2011 · N784NC · Doug DC951 · Trailing Edge Flaps
  > I/B FLAP FIXED VANE THE AFT ATTACH POINT HAS METAL PEELING UP. REPAIRED DISCREPANT AREA ON I/B FLAP FIXED VANE IAW SRM 51-30-2 PAGE 1, SRM 51-70-2 PARAGRAPH 18(4) PAGE 91&92, SRM 57-50-9 PAGE 5 PER DWG PL591004, SRM 51-70-2 PARAGRAPH 26 PAGE 269-274, SRM 51-7
- [SDR DALA1130349875](https://openairdocs.org/sdr/DALA1130349875.md): Skin · damaged · Apr 29, 2011 · N784NC · Doug DC951 · Fuselage Main, Plate/Skin
  > LWR FUSELAGE FROM STA Y367 TO Y370, BETWEEN LONGERON 26 LT AND 28 LT EXT SKIN WITH TOOL MARKS. CUT OUT DAMAGE AREA AT STA Y368 ABOVE LONGERON 27 LT, NDT INSPECTED AREA NO DAMAGE NOTED. FABRICATE AND INSTALLED FILLER AND INTERNAL REPAIR DOUBLER PER SRM 53-04
- [SDR DALA1130009875](https://openairdocs.org/sdr/DALA1130009875.md): Skin · damaged · Apr 28, 2011 · N784NC · Doug DC951 · Fuselage Main, Plate/Skin
  > LWR FUSELAGE STA Y79 TO STA Y589 BETWEEN LONGERON 21L AND 22L EXTERNAL SKIN WITH TOOL MARKS. REMOVED DAMAGE, NDT NO DAMAGE NOTED. FABRICATED REPAIR PARTS PER SRM 53-04 FIG 38 PG 218L. TREATED AND PRIMED PARTS PER SRM 51-10-3 PARA 14 AND 21. INSTALLED ALL R
- [SDR DALA1129999875](https://openairdocs.org/sdr/DALA1129999875.md): Skin · dented · Apr 28, 2011 · N784NC · Doug DC951 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE STA Y 245 BETWEEN LONGERON 15 RT AND 16 RT EXTERNAL SKIN WITH DENT. CHECKED DENT FROM STA Y 245 BETWEEN LONGERON 15 RT AND 16 RT OUT OF LIMITS PER SRM 53-04 PG: 217 FIG 38 CONDITION 1A COLD FORMED SKIN BACK TO ORIGINAL. CONTOUR IAW SRM 53-04 F
- [SDR DALA1129979875](https://openairdocs.org/sdr/DALA1129979875.md): Floor Support · cracked · Apr 28, 2011 · N784NC · Doug DC951 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT COMPOSITE ANGLE CRACKED STA 200 TO 215 RBL-55. R & R FLOOR SUPPORT COMPOSITE ANGLE WITH PN S4616493-12500, BATCH 0002032988 AT STA 200 TO 215 RBL 55 IAW SRM 51-30-8, PG 3. PRIMED IAW SRM 51-10-3 PG 31, PAR 14..
- [SDR DALA1129969875](https://openairdocs.org/sdr/DALA1129969875.md): Floor Panel · corroded · Apr 28, 2011 · N784NC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 46 HAS SURFACE CORROSION ALONG ROW OD OTBD FASTENER HOLES. BLENDED CORRODED FASTENER HOLES IAW SRM 51-10-3 PG 46-47 ORIG MAT THICKNESS.020 IAW SRM 53-23-0 MAX MAT LOSS.020 OUT OF LIMITS IAW SRM 53-01. REMOVED IAW SRM 51-30-11 AND 51-30-2.
- [SDR DALA1129959875](https://openairdocs.org/sdr/DALA1129959875.md): Floor Skin · dented · Apr 28, 2011 · N784NC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 49 HAS 4 EA DENTS IN UPPER SKIN. DAMAGE IN EXCESS OF 8 INCHES OUT OF LIMITS IAW SRM 53-05. FABRICATED FLOOR PANEL 49 IAW SRM 53-23-0 AND 53-05, REMOVED HAT CHANNELS IAWSRM 53-05 PAINTED AND TREATED FLOOR 49 RE-INSTALLED HAT CHANNELS IAW SR
- [SDR DALA1129949875](https://openairdocs.org/sdr/DALA1129949875.md): Floor Panel · corroded · Apr 28, 2011 · N784NC · Doug DC951 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 25-50 HAS CORROSION. REMOVED CORROSION ON FLOOR PANEL 25-50 SKIN, FOUND TO BE OUT OF LIMITS, REMOVED, FABRICATED, AND INSTALLED NEW SKIN IAW AMM DC-9-A-51-21-03-701-929A-A, SRM 53-23-07 P.7, SRM 51-10-4, SRM 51-10-2, SRM 51-10-3 P.
- [SDR DALA1129939875](https://openairdocs.org/sdr/DALA1129939875.md): Floor Panel · corroded · Apr 28, 2011 · N784NC · Doug DC951 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 98-50 HAS CORROSION. REMOVED CORROSION IAW AMM DC9-A-51-21-03-701-929A-A ORIGINAL OUT OF LIMITS IAW AMM SRM 53-01 PG:5-8. REMOVED 2 EA HAT CHANNELS IAW SRM 51-30-02, PG 24. RECEIVED MATERIAL IAW SRM 53-23-0. TREATED AND PRIMED
- [SDR DALA1129929875](https://openairdocs.org/sdr/DALA1129929875.md): Floor Panel · corroded · Apr 28, 2011 · N784NC · Doug DC951 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 22-50 HAS CORROSION OUT OF LIMITS REF SRM 53-01, PG 8 FIG 1. REMOVED HAT CHANNELS SKIN REF SRM 51-30-2, PG 1-14. FABRICATED SKIN USING 7075T6-.040 BATCH 0001804643 REF SRM 53-23-0, PG 6, FIG 3. TREATED SKIN REF SRM 51-10-3, PG 40

Next page: https://openairdocs.org/deregistered/N784NC-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 = 'N784NC' AND deregistration_id = 'N784NC-2014-06-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N784NC-2014-06-17/reports

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