N770NC, cancelled Jun 17, 2014

Service difficulty reports · 111

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA13052070861Power Supply · inoperativeLEFT 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.Oct 13, 2013 · N770NC · Doug DC951 · Emergency LightingSDR DALA13045950861Battery Pack · inoperativeDURING NON ROUTINE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY AND FUNCTIONAL CHECKED GOOD.Sep 19, 2013 · N770NC · Doug DC951 · Emergency LightingSDR DALA13045580861Battery Pack · inoperativeDURING NON-ROUTINE CHECK, FOUND LT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.Sep 17, 2013 · N770NC · Doug DC951 · Emergency LightingSDR DALA13042320861Strap · crackedFOUR 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 HOLAug 25, 2013 · N770NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA13042010861Skin · crackedSKIN HAS CRACK INDICATIONS ABOVE STRINGER 3L BS 229. REPAIRED IAW ER/A 518144-14AD REV ORIGINAL.Aug 25, 2013 · N770NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA13042000861Skin · crackedSKIN 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.Aug 25, 2013 · N770NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA13041990861Skin · crackedTWO 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 Aug 25, 2013 · N770NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA13012980861Light · brokenAFT 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.Mar 24, 2013 · N770NC · Doug DC951 · Emergency LightingSDR DALA13009280861Battery Pack · inoperativeEMERGENCY OVERHEAD LIGHTS AT SEAT ROWS 21 AND 23 INOPERATIVE. REPLACED BATTERY PACK IAW ER/A 093314-14 REV ORIG. OPS CHECKED GOOD.Feb 22, 2013 · N770NC · Doug DC951 · Emergency LightingSDR DALA12010710861Wire · brokenDURING 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.Oct 23, 2012 · N770NC · Doug DC951 · Light System WiringSDR DALA12007360861Skin · crackedTHREE 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, PESep 17, 2012 · N770NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA12007580861Skin · crackedDURING 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 PERMANENSep 14, 2012 · N770NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA12007240861Longeron · crackedCRACKED 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.Sep 12, 2012 · N770NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA12007370861Pan · crackedAD 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 Sep 3, 2012 · N770NC · Doug DC951 · Cargo/Baggage DoorsSDR DALA12005790861Wire · brokenDURING 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.Aug 24, 2012 · N770NC · Doug DC951 · Light System WiringSDR DALA12002340861Fire Warning · false activationAPU 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.Jul 1, 2012 · N770NC · Doug DC951 · Fire DetectionSDR DALA12001210861Battery Pack · inoperativeDURING 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.Jun 3, 2012 · N770NC · Doug DC951 · Emergency LightingSDR DALA1200819861Pan · crackedWHILE 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.Jan 2, 2012 · N770NC · Doug DC951 · Passenger/Crew DoorsSDR DALA1167379861Switch · defectiveWHILE 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.Dec 4, 2011 · N770NC · Doug DC951 · Emergency LightingSDR DALA1153989861Connector · damagedMAINTENANCE 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.Sep 13, 2011 · N770NC · Doug DC951 · Light System WiringSDR DALA1141649861Skin · corrodedFUSELAGE 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 ACCOMPLISHEJun 25, 2011 · N770NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1141399861Membrane · damagedFOUND 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.Jun 24, 2011 · N770NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1141359861Web · crackedFOUND 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.Jun 24, 2011 · N770NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1140879861Seat Track · corrodedSEAT 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 Jun 22, 2011 · N770NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1140869861Plate · crackedEXTERNAL 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 DOUBLEJun 22, 2011 · N770NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1140859861Floor Support · crackedMAIN 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 SRJun 22, 2011 · N770NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1140529861Floor Panel · corrodedCOCKPIT 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 SRJun 21, 2011 · N770NC · Doug DC951 · Fuselage Floor PanelSDR DALA1140369861Floor Panel · damagedCABIN 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 DRILLJun 17, 2011 · N770NC · Doug DC951 · Fuselage Floor PanelSDR DALA1140359861Web · chafedRUDDER 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 SRMJun 17, 2011 · N770NC · Doug DC951 · Rudder Miscellaneous StructureSDR DALA1140319861Floor Panel · corrodedCOCKPIT 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-Jun 17, 2011 · N770NC · Doug DC951 · Fuselage Floor PanelSDR DALA1139699861Floor Panel · crackedCABIN 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 DC9Jun 13, 2011 · N770NC · Doug DC951 · Fuselage Floor PanelSDR DALA1139689861Floor Panel · corrodedCABIN 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.Jun 13, 2011 · N770NC · Doug DC951 · Fuselage Floor PanelSDR DALA1139679861Floor Panel · puncturedCABIN 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.Jun 13, 2011 · N770NC · Doug DC951 · Fuselage Floor PanelSDR DALA1139659861Longeron · crackedMAIN 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 INSTALLEJun 13, 2011 · N770NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA1140309861Floor Panel · damagedMAIN 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 PRIMJun 12, 2011 · N770NC · Doug DC951 · Fuselage Floor PanelSDR DALA1139599861Floor Support · corrodedFLOOR 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 DJun 11, 2011 · N770NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1139589861Skin · dentedFWD 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 IDENJun 11, 2011 · N770NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1139569861Longeron · crackedMAIN 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 Jun 11, 2011 · N770NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA1139579861Floor Panel · corrodedCOCKPIT 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.Jun 10, 2011 · N770NC · Doug DC951 · Fuselage Floor PanelSDR DALA1138309861Web · crackedNR 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 54-01Jun 6, 2011 · N770NC · Doug DC951 · Nacelle/Pylon Miscellaneous StructureSDR DALA1137599861Hinge · excess playLT 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 May 31, 2011 · N770NC · Doug DC951 · Trailing Edge FlapsSDR DALA1137359861Doubler · gougedGOUGE 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 REPAMay 29, 2011 · N770NC · Doug DC951 · Leading Edge DevicesSDR DALA1136719861Floor Panel · damagedCABIN 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.May 26, 2011 · N770NC · Doug DC951 · Fuselage Floor PanelSDR DALA1136709861Floor Panel · damagedCABIN 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.May 26, 2011 · N770NC · Doug DC951 · Fuselage Floor PanelSDR DALA1139819861Skin · gougedRT 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 31-32May 23, 2011 · N770NC · Doug DC951 · Trailing Edge FlapsSDR DALA1138489861Floor Support · crackedCABIN 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 DCMay 22, 2011 · N770NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1140299861Floor Panel · bentCABIN 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 INSTALLIMay 21, 2011 · N770NC · Doug DC951 · Fuselage Floor PanelSDR DALA1140279861Floor Panel · corrodedCABIN 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.May 21, 2011 · N770NC · Doug DC951 · Fuselage Floor PanelSDR DALA1139719861Doubler · crackedLEFT 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.May 21, 2011 · N770NC · Doug DC951 · Wing SparSDR DALA1139639861Floor Panel · puncturedCABIN 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 FMay 21, 2011 · N770NC · Doug DC951 · Fuselage Floor Panel
Back to N770NC, cancelled Jun 17, 2014