# Service difficulty reports: N770NC, cancelled Jun 17, 2014

A list on [N770NC, cancelled Jun 17, 2014](https://openairdocs.org/deregistered/N770NC-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 · 111 reports

- [SDR DALA13052070861](https://openairdocs.org/sdr/DALA13052070861.md): Power Supply · inoperative · Oct 13, 2013 · N770NC · Doug DC951 · Emergency Lighting
  > LEFT OVERWING EMERGENCY EVACUATION LIGHT INOPERATIVE. FOUND BAD POWER SUPPLY B5-50 AND REPLACED EMERGENCY LIGHT. OP'S CK GOOD. AMM 33-55-00 OK FOR SERVICE.
- [SDR DALA13045950861](https://openairdocs.org/sdr/DALA13045950861.md): Battery Pack · inoperative · Sep 19, 2013 · N770NC · Doug DC951 · Emergency Lighting
  > DURING NON ROUTINE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY AND FUNCTIONAL CHECKED GOOD.
- [SDR DALA13045580861](https://openairdocs.org/sdr/DALA13045580861.md): Battery Pack · inoperative · Sep 17, 2013 · N770NC · Doug DC951 · Emergency Lighting
  > DURING NON-ROUTINE CHECK, FOUND LT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.
- [SDR DALA13042320861](https://openairdocs.org/sdr/DALA13042320861.md): Strap · cracked · Aug 25, 2013 · N770NC · Doug DC951 · Fuselage Miscellaneous Structure
  > FOUR FASTENERS HAVE CRACK INDICATIONS BELOW STRINGER 3R AT BS 229. REMOVED FASTENERS IAW PRI 518144-14AD, REV O. PERFORMED BHEC AND HFEC IAW STEPS 3 AND 4 OF PRI 518144-14AD, REV O. FOUND FWD FASTENER HOLE CRACKED SPLICE STRAP WITH BHEC, OTHER 3 FASTENER HOL
- [SDR DALA13042010861](https://openairdocs.org/sdr/DALA13042010861.md): Skin · cracked · Aug 25, 2013 · N770NC · Doug DC951 · Fuselage Main, Plate/Skin
  > SKIN HAS CRACK INDICATIONS ABOVE STRINGER 3L BS 229. REPAIRED IAW ER/A 518144-14AD REV ORIGINAL.
- [SDR DALA13042000861](https://openairdocs.org/sdr/DALA13042000861.md): Skin · cracked · Aug 25, 2013 · N770NC · Doug DC951 · Fuselage Main, Plate/Skin
  > SKIN HAS CRACK INDICATIONS ABOVE STRINER 4L BS 224, PERFORMED BHEC AND HFEC IAW STEPS 3 AND 4 OF PRI 518144-14AD, REV O. REPAIRED IAW ER/A 518144-14AD, REV ORIGINAL.
- [SDR DALA13041990861](https://openairdocs.org/sdr/DALA13041990861.md): Skin · cracked · Aug 25, 2013 · N770NC · Doug DC951 · Fuselage Main, Plate/Skin
  > TWO FASTENERS HAVE CRACK INDICATIONS ABOVE STRINGER 4L AT BS 974, ROWS B AND D. PERFORMED BHEC AND HFEC IAW STEPS 3 AND 4 OF PRI 518144-14AD, REV O, FOUND CRACK INDICATION ON FWD FASTENER HOLE SPLICE STRAP AFT HOLE NO ITEMS. STEPPED UP FWD FASTENER HOLE TO
- [SDR DALA13012980861](https://openairdocs.org/sdr/DALA13012980861.md): Light · broken · Mar 24, 2013 · N770NC · Doug DC951 · Emergency Lighting
  > AFT EMERGENCY LIGHT ASSY AT TAIL CONE EXIT HANDLE, BROKEN OFF OF FRAME. INSPECTED FOUND HARDWEAR MISSING, RESECURED LIGHT ASSY IAW SRM 51-30. OPS CHECK GOOD OF LIGHT IAW AMM 33-53-00. OK FOR SERVICE.
- [SDR DALA13009280861](https://openairdocs.org/sdr/DALA13009280861.md): Battery Pack · inoperative · Feb 22, 2013 · N770NC · Doug DC951 · Emergency Lighting
  > EMERGENCY OVERHEAD LIGHTS AT SEAT ROWS 21 AND 23 INOPERATIVE. REPLACED BATTERY PACK IAW ER/A 093314-14 REV ORIG. OPS CHECKED GOOD.
- [SDR DALA12010710861](https://openairdocs.org/sdr/DALA12010710861.md): Wire · broken · Oct 23, 2012 · N770NC · Doug DC951 · Light System Wiring
  > DURING LINE CHECK, MX FOUND THE EMERGENCY ESCAPE PATH LIGHTING AT SEAT 8D TO BE INOPERATIVE. MX FOUND A BROKEN WIRE, REPAIRED IT AND THE LIGHTS RETURNED TO AN OPS CONDITION. ACFT NOW OK FOR SERVICE.
- [SDR DALA12007360861](https://openairdocs.org/sdr/DALA12007360861.md): Skin · cracked · Sep 17, 2012 · N770NC · Doug DC951 · Fuselage Main, Plate/Skin
  > THREE CRACKS WERE FOUND IN THE FUSELAGE SKIN NEAR THE PED JAMB CUTOUT UPPER FORWARD CORNER AT STA 160. THE CRACKS WERE REPAIRED IAW ERA 504604-14AD, SECT I. MX TRIMMED THE INTERNAL DOUBLER TO REMOVE THE CRACK, EXTENDED THE TRIM OUT ONTO THE FUSELAGE SKIN, PE
- [SDR DALA12007580861](https://openairdocs.org/sdr/DALA12007580861.md): Skin · cracked · Sep 14, 2012 · N770NC · Doug DC951 · Fuselage Main, Plate/Skin
  > DURING L CHECK, A CRACK WAS NOTED IN THE FUSELAGE SKIN AT THE PASSENGER ENTRY DOOR CUTOUT, UPPER AFT CORNER, NR 1 DOOR STOP. COMPLIED WITH ERA 504606-14AD, REV ORIGINAL SECTION 1 ON FUSELAGE SKIN LT FWD PASSENGER DOOR JAMB/AFT UPPER CORNER, THIS IS A PERMANEN
- [SDR DALA12007240861](https://openairdocs.org/sdr/DALA12007240861.md): Longeron · cracked · Sep 12, 2012 · N770NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON RIGHT BELOW APU EXHAUST DUCTING L14R BETWEEN BS 1230 TO 1247, REMOVED LONGERON SPLICE, CUT OUT LONGERON AND REMOVED IAW SRM 53-02 FIG 18. REPAIRED LONGERON IAW SRM 53-02 FIG 18.
- [SDR DALA12007370861](https://openairdocs.org/sdr/DALA12007370861.md): Pan · cracked · Sep 3, 2012 · N770NC · Doug DC951 · Cargo/Baggage Doors
  > AD RELATED INSPECTION OF THE FORWARD CARGO DOOR UTILIZING HFEC, DETECTED A CRACK ON THE AFT SIDE DOOR PAN BEND RADII AT THE LOWER (5TH) DOOR STOP PAD APPROX.375 IN. IN LENGTH AND EXTENDS UNDER DOOR STOP PAD. ONE END OF CRACK IS MARKED UNABLE TO DETERMINE END
- [SDR DALA12005790861](https://openairdocs.org/sdr/DALA12005790861.md): Wire · broken · Aug 24, 2012 · N770NC · Doug DC951 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY ESCAPE LIGHTING AT SEAT 6 DEF TO BE INOPERATIVE. MAINTENANCE REPAIRED THE BROKEN WIRE AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. AIRCRAFT NOW OKAY FOR SERVICE.
- [SDR DALA12002340861](https://openairdocs.org/sdr/DALA12002340861.md): Fire Warning · false activation · Jul 1, 2012 · N770NC · Doug DC951 · Fire Detection
  > APU FIRE INDICATOR. RAN QRH PROCEDURE. CREW THEN DISCHARGED BOTH BOTTLES FOR APU. INSPECTED APU COMPARTMENT. NO FIRE DAMAGE OR EVIDENCE FOUND. RAN APU AND INSPECTED AREA. ALL CHECKS GOOD. REMOVED AND REPLACED BOTH FIRE BOTTLES.
- [SDR DALA12001210861](https://openairdocs.org/sdr/DALA12001210861.md): Battery Pack · inoperative · Jun 3, 2012 · N770NC · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THE CEILING EMERGENCY LIGHTS AT ROWS 21 AND 23 TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA1200819861](https://openairdocs.org/sdr/DALA1200819861.md): Pan · cracked · Jan 2, 2012 · N770NC · Doug DC951 · Passenger/Crew Doors
  > WHILE TROUBLESHOOTING DOOR CLOSURE ISSUE, A CRACK WAS NOTED IN THE DOOR PAN UNDER THE LOWER HINGE, APPROXIMATELY 1 INCH IN LENGTH. ERA 498996-14 APPLIED, AND SHIP NON-PRESSURIZED, MAINTENANCE FERRIED TO MSP. REPLACED L1 DOOR.
- [SDR DALA1167379861](https://openairdocs.org/sdr/DALA1167379861.md): Switch · defective · Dec 4, 2011 · N770NC · Doug DC951 · Emergency Lighting
  > WHILE PERFORMING THE SECURE CHECKLIST, PILOT PLACED EMERGENCY EGRESS LIGHT SWITCH IN OFF POSITION, AND ALL EMERGENCY EGRESS LIGHTS ILLUMINATED. REPLACED COCKPIT EMERGENCY EGRESS LIGHT SWITCH, CHECKS OK.
- [SDR DALA1153989861](https://openairdocs.org/sdr/DALA1153989861.md): Connector · damaged · Sep 13, 2011 · N770NC · Doug DC951 · Light System Wiring
  > MAINTENANCE FOUND EMERGENCY EXIT LIGHT AT 1R DOOR INOPERATIVE. MAINTENANCE REMOVED THE LIGHT ASSEMBLY, REPAIRED CONNECTOR, AND REPLACED THE POWER SUPPLY ASSEMBLY. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA1141649861](https://openairdocs.org/sdr/DALA1141649861.md): Skin · corroded · Jun 25, 2011 · N770NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN CORROSION AT WING TO BODY PANEL ATTACHMENT FS 894-908, S26R-28R. REF LOG 0355872. PERMANENT REPAIR ACCOMPLISHED ON FUSELAGE SKIN AT WING TO BODY PANEL ATTACHMENT FS 894-908 S-26R-28R IAW ERA 493500-14 REV ORIGINAL. ALL WORK ACCOMPLISHE
- [SDR DALA1141399861](https://openairdocs.org/sdr/DALA1141399861.md): Membrane · damaged · Jun 24, 2011 · N770NC · Doug DC951 · Fuselage Miscellaneous Structure
  > FOUND HOLES ON SUB FLOOR OF FLOOR PANEL NR 13 LBL 12 STA 160. REMOVED FABRICATED AND INSTALLED WEB UNDER FLOOR PANEL 13 AT STA 160 LBL 12 IAW DC9 SRM 51-30-1 AND DC9 SRM 51-30-2 PARA 7.
- [SDR DALA1141359861](https://openairdocs.org/sdr/DALA1141359861.md): Web · cracked · Jun 24, 2011 · N770NC · Doug DC951 · Fuselage Miscellaneous Structure
  > FOUND CRACK UNDER FLOOR PANEL 13 BL 0 STA 160 WHILE GETTING OK TO INSTALL FLOOR PANEL. REMOVED FABRICATED AND INSTALLED NEW WEB UNDER FLOOR PANEL 13 STA 160 IAW DC9 SRM 51-30-1 PG 1 AND DC9 SRM 51-30-2 PAR 7.
- [SDR DALA1140879861](https://openairdocs.org/sdr/DALA1140879861.md): Seat Track · corroded · Jun 22, 2011 · N770NC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 22 HAS AREAS OF CORROSION FROM STA 200 TO 318. REMOVED CORROSION ON SEAT TRACK LBL 22 AT STA 200 TO 318 PER DC9 SRM 51-10-3 PAGE 35 OUT OF LIMITS PER SRM 53-05 PAGE 24. LOCATED AND DRILLED PAGE 31 AND 40 INSTALLED SEAT TRACK LBL 22 AT STA 200
- [SDR DALA1140869861](https://openairdocs.org/sdr/DALA1140869861.md): Plate · cracked · Jun 22, 2011 · N770NC · Doug DC951 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE NOSE SECTION LT AT HOOK PLATE OF THE FWD PAX DOOR AT FS 130 PLATE IS CRACKED AND DETERIORATED. REMOVED DOUBLER DAMAGED IAW SRM 51-70-2 PG 2 AND SRM 51-30-5 PG 29. LOCATED AND DRILLED NEW DOUBLER IAW SRM 53-04 FIG 24 AND INSTALLED NEW DOUBLE
- [SDR DALA1140859861](https://openairdocs.org/sdr/DALA1140859861.md): Floor Support · cracked · Jun 22, 2011 · N770NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN AT STA 1136.091 FLOOR SUPPORTS ON LEFT AND RIGHT SIDES APPROXIMATELY 12" FROM BL 0 ARE CRACKED AT FWD O/B SIDES. REMOVED AND REINSTALLED CABIN FLOOR SUPPORTS ON LEFT AND RIGHT SIDE STA 1136.091 IAW DC9 SRM 51-30-1 PG 1. REPAIRED CRACKS IAW DC9 SR
- [SDR DALA1140529861](https://openairdocs.org/sdr/DALA1140529861.md): Floor Panel · corroded · Jun 21, 2011 · N770NC · Doug DC951 · Fuselage Floor Panel
  > COCKPIT FLOOR 15 PANEL CORROSION. REMOVED CORROSION PER DC9 SRM 51-10-3 PGS 46-48 OUT OF LIMITS PER DC9 SRM 53-01 PG 8. REMOVED ANGLE BRACKETS PER DC9 SRM 51-30-02 PG 24 PARA 7. LOCATED AND DRILLED NEW PNL PER DC9 SRM 51-10-4 PG 1. COUNTER SUNK PER DC 9 SR
- [SDR DALA1140369861](https://openairdocs.org/sdr/DALA1140369861.md): Floor Panel · damaged · Jun 17, 2011 · N770NC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PNL 20 HAS CORROSION ON BOTTOM SIDE MARKED AND DAMAGED FASTENER HOLES MARKED DOUBLER WASHER NOT TO USE, FLOOR PANEL AND FLOOR PANEL 20 OUT OF LIMITS IAW SRM DC9 53-01 PAGE 8 REPLACED FLOOR PANEL IAW AMM DC9-A-53-20-01-201-925A-A. LOCATED AND DRILL
- [SDR DALA1140359861](https://openairdocs.org/sdr/DALA1140359861.md): Web · chafed · Jun 17, 2011 · N770NC · Doug DC951 · Rudder Miscellaneous Structure
  > RUDDER LOWER SURFACE WEB CHAFING ON NUT PLATE ATTACHMENT. BLENDED DAMAGE AREA OUT OF LIMITS PER SRM 55-40-0 FIG 4. REMOVED AND REPLACED RIB AT RUDDER LWR SURFACE PER SRM 51-30-2. REQUIRED BALANCING THAT SAME NEW PART WAS REPLACED AND THE SAME WEIGHT PER SRM
- [SDR DALA1140319861](https://openairdocs.org/sdr/DALA1140319861.md): Floor Panel · corroded · Jun 17, 2011 · N770NC · Doug DC951 · Fuselage Floor Panel
  > COCKPIT 13 FLOOR PANEL WITH CORROSION. UPON FURTHER EVALUATION FOUND PANEL TO BE EXFOLIATED AND CRACKED REMOVED 9 EA HAT CHANNEL FROM FLOOR PANEL 13, (1 EA) HAT CHANNEL FOUND TO BE CRACKED PER DC9 51-30-2. FABBED PANEL AND 1 EA HAT CHANNEL PER DC9 SRM 53-23-
- [SDR DALA1139699861](https://openairdocs.org/sdr/DALA1139699861.md): Floor Panel · cracked · Jun 13, 2011 · N770NC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 69 HAS A SMALL DENT WITH A CRACK IN SKIN, PNL IS OFF AIRCRAFT PART. CUT OUT DENTED CRACKED AREA ON CABIN FLOOR PANEL 69 IAW DC9 SRM 53-05 PG 10 FIG 7. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW DC-9 SRM 53-05 PG 10 FIG 1 AND DC9
- [SDR DALA1139689861](https://openairdocs.org/sdr/DALA1139689861.md): Floor Panel · corroded · Jun 13, 2011 · N770NC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PNL 26 HAS CORROSION ON UPPER SURFACE OF DOUBLER REPAIR AND ON THE BOTTOM SIDE OF PNL, PNL IS OFF AC PART. REMOVED CORRODED DOUBLER ON CABIN FLOOR PNL 26 IAW DC9 SRM 51-30-2 PG 1. FABRICATED AND INSTALLED DOUBLER ON CABIN FLOOR PANEL 26.
- [SDR DALA1139679861](https://openairdocs.org/sdr/DALA1139679861.md): Floor Panel · punctured · Jun 13, 2011 · N770NC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PNL 89 SMALL PUNCTURE IN SKIN AND A 6 INCH LONG CREASE. REMOVED UPPER SKIN FROM CABIN FLOOR PANEL 89. INSTALLED UPPER SKIN TO CABIN FLOOR 89 IAW SRM 51-30-2 PG 24.
- [SDR DALA1139659861](https://openairdocs.org/sdr/DALA1139659861.md): Longeron · cracked · Jun 13, 2011 · N770NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > MAIN CABIN, STA Y 775, LONG 2 RT WITH CRACK. RII: Y. CUT AND REMOVED DAMAGED SECTION MAIN CABIN 2 RT LONGERON AT STA 775 IAW DC9 SRM 53-02 FIG 18 FABRICATED LONGERON SECTION AND 2 EACH SPLICE SECTION SECTIONS IAW DC9 SRM 53-02 FIG 18 NR 2 RT LONGERON INSTALLE
- [SDR DALA1140309861](https://openairdocs.org/sdr/DALA1140309861.md): Floor Panel · damaged · Jun 12, 2011 · N770NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 71C PUNCTURE TO FLOOR REMOVED DAMAGED FLOOR SKIN AND DAMAGED HAT CHANNEL FROM FLOOR PNL PER DC9 SRM 51-30-2, PG 1-3, FABBED FLOOR SKIN PER DC 9 SRM 53-21-0, PG 14A. FABBED HAT CHANNEL PER DC9 SRM 53-20-0, FIG 3, ITEM 16, TREATED AND PRIM
- [SDR DALA1139599861](https://openairdocs.org/sdr/DALA1139599861.md): Floor Support · corroded · Jun 11, 2011 · N770NC · Doug DC951 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STRUCTURE HAS AREAS OF CORROSION STA 160 BETWEEN LBL 53 AND BL-0. RII: Y. REMOVED CORROSION STA 160 BL-0 TO LBL 53, FOUND CRACK LBL 46. MECHANICALLY MEASURED FOUND MATERIAL LOSS.005. MATERIAL WITHIN LIMITS PER SRM 53-01 FIG 1 PG 8. CUT OUT D
- [SDR DALA1139589861](https://openairdocs.org/sdr/DALA1139589861.md): Skin · dented · Jun 11, 2011 · N770NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FWD CARGO EXTERIOR SKIN SURFACE DENTED. RII: Y. REFORMED DENT AREA ON FWD CARGO DOOR EXTERIOR SKIN IAW SRM 51-10-02 PG:6 FIG 2. HFEC NOTED NO DEFECTS AT REWORK AREA REPAIRED DENT AREA WITH INTERNAL DOUBLER PER SRM 53-04 PG:218K FIG 38 SHEET 22. THIS IS IDEN
- [SDR DALA1139569861](https://openairdocs.org/sdr/DALA1139569861.md): Longeron · cracked · Jun 11, 2011 · N770NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > MAIN CABIN STA Y 764, LONG 3RT WITH CRACK RII: Y. CUT AND REMOVED DAMAGED SECTION MAIN CABIN NR 3 RT LONGERON TO EXISTING SPLICE STA 764 IAW DC-9 SRM 53-02 FIG 18. FABRICATED LONGERON SECTION AND SPLICE IAW SRM 53-02 FIG 18 TO NR 3 RT LONGERON, INSTALLED IAW
- [SDR DALA1139579861](https://openairdocs.org/sdr/DALA1139579861.md): Floor Panel · corroded · Jun 10, 2011 · N770NC · Doug DC951 · Fuselage Floor Panel
  > COCKPIT NR 14 FLOOR PANEL WITH CORROSION. RECEIVED NEW FLOOR PANEL 14 AT COCKPIT. LOCATED AND DRILLED NEW FLOOR PANEL 14 AT COCKPIT IAW DC-9 SRM 51-10-4 PARAGRAPH 2 PG:1.
- [SDR DALA1138309861](https://openairdocs.org/sdr/DALA1138309861.md): Web · cracked · Jun 6, 2011 · N770NC · Doug DC951 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON AFT ENGINE MOUNT LWR SUPPORT STRUCTURE WEB AND EXISTING REPAIR CRACKED STA YN 174 VIEWED THRU ACCESS DOOR 8206A. NDT VERIFIED CRACK IN DOUBLER APPROX 2 INCHES LONG. REMOVED REPAIR DOUBLER PER DC9 SRM 51-30-2. STOP HOLE ON CRACK PER DC9 SRM 54-01
- [SDR DALA1137599861](https://openairdocs.org/sdr/DALA1137599861.md): Hinge · excess play · May 31, 2011 · N770NC · Doug DC951 · Trailing Edge Flaps
  > LT WING NR 4 FLAP HINGE O/B BUSHING HAS PLAY. REMOVED AND REPLACED LT WING NR 4 FLAP HINGE PER DC-9 AMM 20-17-00 -201 PG 1 & 2 AND DC-9 SRM 51-30-1 PG 15 AND 12. GAINED ACCESS PER DC-9 AMM 20-17-00-201. REMOVED AND REPLACED LT WING NR 4 FLAP HINGE PER DC-9
- [SDR DALA1137359861](https://openairdocs.org/sdr/DALA1137359861.md): Doubler · gouged · May 29, 2011 · N770NC · Doug DC951 · Leading Edge Devices
  > GOUGE ON REPAIR DOUBLER AT LEFT WING FLAP, INBD FIXED VANE, STA XF-154. REMOVED REPAIR DOUBLER ON LEFT WING FLAP INBD FIXED VANE LEADING EDGE STA XF 154 IAW DC-9 SRM 51-70-2 PAGE 11 PARA6A. INSTALLED DOUBLER AND FILLER PER DC-9 SRM 57-03 PAGE 27, BONDED REPA
- [SDR DALA1136719861](https://openairdocs.org/sdr/DALA1136719861.md): Floor Panel · damaged · May 26, 2011 · N770NC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PANEL NR 91 THREE SCREWS PULLED THRU SKIN. FABRICATED, TREATED, PRIMED, AND INSTALLED 3 REPAIR DOUBLER WASHERS AT FLOOR PANEL NR 91 PER SRM 51-10-3 PGS 31, 32, 40, AND 42 AND SRM 53-05.
- [SDR DALA1136709861](https://openairdocs.org/sdr/DALA1136709861.md): Floor Panel · damaged · May 26, 2011 · N770NC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PNL NR 53 TWO SCREWS ARE PULLED THRU SKIN. FABRICATED TREATED AND PRIMED AND INSTALLED REPAIR DOUBLER WASHER AT FLOOR PNL NR 53 PER SRM 51-10-3 PGS 31, 32, 40, AND 42 AND SRM 53-05 PG 12 FIG 3.
- [SDR DALA1139819861](https://openairdocs.org/sdr/DALA1139819861.md): Skin · gouged · May 23, 2011 · N770NC · Doug DC951 · Trailing Edge Flaps
  > RT WING FIX VANE MID PANEL FWD SECTION HAS A DEEP GOUGE ON SKIN TO BARE METAL, LOOSE EYE BOLT. CUT OUT GOUGE ON SKIN, IAW SRM 51-70-2, FABBED DOUBLER AND FILLER PER SRM 51-70-2, SRM 57-03, APPLIED ALODINE PER DC9 SRM 51-10-3, PRIMER PER SRM 51-10-3, PG 31-32
- [SDR DALA1138489861](https://openairdocs.org/sdr/DALA1138489861.md): Floor Support · cracked · May 22, 2011 · N770NC · Doug DC951 · Fuselage Miscellaneous Structure
  > CABIN OVERWING STRUCTURE FLOOR SUPPORT CRACKED AT STA 775 AND X-15. REMOVED FLOOR SUPPORT ON MAIN CABIN AT STA 775 AND X-15 IAW DC9 SRM 51-30-02, FABRICATED FLOOR SUPPORT IAW DC9 SRM 53-13-3, PG 26, FIG 11. INSTALLED FLOOR SUPPORT AT STA 775 AND X-15 IAW DC
- [SDR DALA1140299861](https://openairdocs.org/sdr/DALA1140299861.md): Floor Panel · bent · May 21, 2011 · N770NC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PNL 79, FWD END IS BENT UP AND THERE ARE THREE MIS-DRILLED HOLES ALONG I/B AFT EDGE FABED NEW FLOOR PANEL PER DC9 SRM 53-21-0, PG 14B, 14D, SHEET 1-3, AND SRM DC9 51-30-2. TREATED AND PRIMED PER DC9 SRM 51-10-3. ASSEMBLED FLOOR PANEL BY INSTALLI
- [SDR DALA1140279861](https://openairdocs.org/sdr/DALA1140279861.md): Floor Panel · corroded · May 21, 2011 · N770NC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PNL HAS SURFACE CORROSION AT FWD END. REMOVED AND FABRICATED REPLACEMENT FLOOR PANEL WITH SHT 7075T6.032, BATCH 0002057150 IAW DC9 SRM 51-01 PG 3 AND DC9 SRM 51-20-0 PG 4, AND DC9 SRM 51-30-02.
- [SDR DALA1139719861](https://openairdocs.org/sdr/DALA1139719861.md): Doubler · cracked · May 21, 2011 · N770NC · Doug DC951 · Wing Spar
  > LEFT WING REAR SPAR WEB DOUBLER O/B SIDE OF AFT DOUBLER IS CRACKED, REF: EM 5710-00028, SECTION 03 UPON FURTHER INVESTIGATION, ALL WORK TO BE COMPLIED WITH ON WORK CARD 5710-00028-08A (LEFT WING SPAR AND/OR DOUBLER TRIM REPAIR) JOB 000-0009, WO 87938350001.
- [SDR DALA1139639861](https://openairdocs.org/sdr/DALA1139639861.md): Floor Panel · punctured · May 21, 2011 · N770NC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PNL 52, ONE SMALL PUNCTURE ON SKIN 861-KK-82. FABBED & INSTALLED DOUBLER AS PER DC9 SRM 51-30-2, PG 1, 24-26B, PAR 7, MARKED USING REPAIR IDENTIFICATON REQUIREMENTS USING PROCESS STANDARD 900-5-1, NR 4, PG 1-6. INSTALLED REPAIR DOUBLER ON CABIN F

Next page: https://openairdocs.org/deregistered/N770NC-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 = 'N770NC' AND deregistration_id = 'N770NC-2014-06-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N770NC-2014-06-17/reports

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