# Service difficulty reports: N773NC, cancelled Jun 17, 2014

A list on [N773NC, cancelled Jun 17, 2014](https://openairdocs.org/deregistered/N773NC-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 5 · 209 reports

- [SDR DALA13012800864](https://openairdocs.org/sdr/DALA13012800864.md): Slide · dislodged · Mar 20, 2013 · N773NC · Doug DC951 · Escape Slide
  > WHEN MAIN CABIN DOOR WAS SHUT FOR DEPARTURE, THE EMERGENCY ESCAPE SLIDE FELL OUT FROM ITS COMPARTMENT. INSTALLED L1 DOOR SLIDE IAW AMM 25-62.
- [SDR DALA13011630864](https://openairdocs.org/sdr/DALA13011630864.md): Slide · dislodged · Mar 9, 2013 · N773NC · Doug DC951 · Escape Slide
  > R1 DOOR SLIDE CAME OUT OF BOX ON LANDING. INSTALLED SLIDE. CHECKED GOOD.
- [SDR DALA12006350864](https://openairdocs.org/sdr/DALA12006350864.md): Ground Wire · damaged · Sep 5, 2012 · N773NC · Doug DC951 · Light System Wiring
  > ON SERVICE CHECK, FOUND SEAT ROWS 1-4 EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE FOUND EMERGENCY LIGHT BATTERIES DEAD. REPLACED BATTERIES WITH SPARE ONE. LIGHTS WOULD NOT EXTINGUISH AFTER TEST. FOUND GROUND WIRE PINCHED BETWEEN ROW 1 AND ROW 2. REPAI
- [SDR DALA12006340864](https://openairdocs.org/sdr/DALA12006340864.md): Fuse · inoperative · Sep 1, 2012 · N773NC · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEATS 1 THRU 4 AND SERVICE DOOR TO BE INOPERATIVE. MAINTENANCE REPLACED THE FUSE AT THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA12005710864](https://openairdocs.org/sdr/DALA12005710864.md): Skin · cracked · Aug 22, 2012 · N773NC · Doug DC951 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING AD RELATED TASK CARD 5330-01142-02 EDDY CURRENT INSPECTION, FWD PASSENGER DOOR JAMB SKIN CORNERS AND DOOR STOPS SECTION 02 1. CRACK INDICATION ON SKIN WAS DETECTED EMANATING FROM NR 7 DOOR STOP. REMOVED DAMAGE ON DOOR STOP SKIN NR 7 AFT,
- [SDR DALA12005700864](https://openairdocs.org/sdr/DALA12005700864.md): Strap · corroded · Aug 20, 2012 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > UPON CLEANING OF AREA ON N/R 2 ZONE 1E IN AFT CARGO PIT FOUND STRAP TO BE CORRODED. DOUBLER STRAP WAS REMOVED AND REPLACED PER DC9 SRM.
- [SDR DALA12005640864](https://openairdocs.org/sdr/DALA12005640864.md): Bulkhead · corroded · Aug 17, 2012 · N773NC · Doug DC951 · Fuselage Main, Bulkhead
  > UPON CLEANING OF AREA ON NR 2 ZONE 1 FOUND AFT CARGO AFT BULKHEAD AREA STA 1167 BL0 T-ANGLE TO HAVE CORROSION. T-ANGLE EXFOLIATED AND CRACKED FOUND TO BE OUT OF LIMITS. REMOVED ON NRC NR 2 ZONE 1E AFT CARGO PIT AFT BULKHEAD AREA STA 1167 BL-0 TEE ANGLE. LOC
- [SDR DALA12000130864](https://openairdocs.org/sdr/DALA12000130864.md): Cable · binding · May 18, 2012 · N773NC · Doug DC951 · Entrance Stairs
  > DURING LINE CHECK, MAINTENANCE FOUND THE CATWALK STUCK IN THE LOWERED POSITION WITH THE AFT AIRSTAIRS LOWERED. ON INSPECTION, MAINTENANCE FOUND THE RIGHT RETRACT CABLE JAMMED. MAINTENANCE REPLACED THE FITTING CRANK ASSEMBLY AND RETRACT CABLE AND RETURNED THE
- [SDR DALA1109059864](https://openairdocs.org/sdr/DALA1109059864.md): Panel · delaminated · Feb 7, 2011 · N773NC · Doug DC951 · Wing, Plate/Skin
  > RT WING T/E FIXED PANEL INBD OF AILERON IS DELAMINATED. APPROX 36 SQ INCHES. R & R PANEL IAW SRM 51-30-01 AND 51-30-2. REPAIRED UPPER T/E SPAR IAW ERA 488339-147. REQUIRED INSP COMPLETED.
- [SDR DALA1108589864](https://openairdocs.org/sdr/DALA1108589864.md): Floor Panel · damaged · Feb 5, 2011 · N773NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 19 FASTENER HOLES ELONGATED IN FLOOR PANEL RACK. FABRICATED FLOOR PANEL 19 IAW DOUGLAS DRAWING 9957823 AND ER/A 488722-14. REQUIRED INSPECTION COMPLETED.
- [SDR DALA1108679864](https://openairdocs.org/sdr/DALA1108679864.md): Cusp Web · corroded · Feb 4, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN LT SIDE BETWEEN STA 693-712 BATHTUB FITTING LBL 55 UNDER FLOOR CUSP WEB HAS CORROSION. REMOVED FITTING MATCH DRILLED AND INSTALLED 2EA FREEZE PLUGS ON TRAVELER 2311N01993. INSTALLED FITTING PER ERA 487368-14. REQUIRED INSPECTION COMPLETED.
- [SDR DALA1108629864](https://openairdocs.org/sdr/DALA1108629864.md): Skin · dented · Feb 4, 2011 · N773NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR STA 238 APPROX 3" BELOW L18L SKIN HAS DENT. CUT OUT SECTION OF SKIN 4"X 5"; NO DAMAGE PER NDT SPM 06-10-01. FABRICATED AND INSTALLED NEW SECTION OF SKIN.050 AND FINGER DOUBLERS.025 IAW DC-9 SRM 53-04 FIG 12C P-226. REQUIRED INSPECTION COM
- [SDR DALA1108129864](https://openairdocs.org/sdr/DALA1108129864.md): Web · cracked · Feb 2, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN PASSENGER CABIN STA 1130 RBL 47 REPAIR DOUBLER IS CRACKED. REMOVED DAMAGED DOUBLER IAW SRM 51-30-2, IAW DWG 5609530019 AND SRM 51-10-4. INSTALLED MEMBRANE REPAIR IAW SRM 51-30-2 AND 51-30-5. P-127 REQUIRED INSPECTION COMPLETED.
- [SDR DALA1108039864](https://openairdocs.org/sdr/DALA1108039864.md): Pan · damaged · Feb 1, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT, STA 427, LOWER DOOR PAN SPLICE FASTENER HOLES ELONGATED IN FRAME. GAINED ACCESS IAW SRM51-30-2. REMOVED FRAME IAW SRM 51-30-5 AND 51-30-2. RECEIVED NEW FRAME, INSTALLED AND RESTORED ACCESS IAW DWG 9912453. R & R DOOR PAN IAW SRM 53-05
- [SDR DALA1108019864](https://openairdocs.org/sdr/DALA1108019864.md): Bulkhead · cracked · Feb 1, 2011 · N773NC · Doug DC951 · Fuselage Main, Bulkhead
  > RT MLG, STA 851, BULKHEAD RBL 58, 3 INCHES FROM TOP WEB IS CRACKED. CUT OUT DAMAGE SECTION 2.5" X 3". DAMAGE CONTAINED IAW NDT SPM 06-10-01,.001. FABRICATED AND INSTALLED FILLER.050 DOUBLER.032 AND SPLICE DOUBLER.071 IAW ERA 488374-14, P-226, Q-953, 18
- [SDR DALA1107019864](https://openairdocs.org/sdr/DALA1107019864.md): Frame · cracked · Jan 29, 2011 · N773NC · Doug DC951 · Fuselage Main, Frame
  > FWD CARGO COMPT STA 674, LONG 29 LT FRAME IS CRACKED. REMOVED DAMAGED FRAME AT STA 674, L25L TO L25R IAW SRM 51-30-05. LOCATED, DRILLED & DEBURRED FRAME IAW SRM 51-10-4. TREATED AND PRIMED NEW FRAME IAW SRM 51-10-3. INSTALLED FRAME IAW SRM 51-30-02 & SRM 5
- [SDR DALA1106709864](https://openairdocs.org/sdr/DALA1106709864.md): Pan · corroded · Jan 27, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > FWD PIT-CARGO DOOR JAMB PAN HAS CORROSION 375-421 AROUND CORENUTS AND UNDER 2 EA STOP FITTINGS. REMOVED CORROSION.5" X 4" FROM PAN IAW SRM 51-10-3. ORIG MAT.050 IAW SRM 53-13-2,.038. FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1. R & R PAN IAW SRM 53-13-2, 5
- [SDR DALA1106469864](https://openairdocs.org/sdr/DALA1106469864.md): Floor Panel · cracked · Jan 26, 2011 · N773NC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PANEL NR 29, 1 EA CRACK. 31 IN AFT TOP. FABRICATED NEW PANEL IAW DWG 995720 AND ERA 488344-14, REV ORIG STENCILED AND IDENTIFIED IAW PS 900-5-1, NR4 P-117 25 JAN 11. CORRECTED..
- [SDR DALA1106459864](https://openairdocs.org/sdr/DALA1106459864.md): Floor Support · cracked · Jan 26, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN PASSENGER CABIN STA 636, LBL 8, FLOOR SUPPORT CRACKED. REMOVED FLOOR SUPPORT AT STA 636 THAT WAS CRACKED IAW SRM 51-30-5. FORMED, TRIMMED, DRILLED, DEBURRED NEW FLOOR SUPPORT APPLIED ALODINE TREATMENT AND PRIMED IAW SRM 51-10-3. INSTALLED NEW FLOOR SUP
- [SDR DALA1106449864](https://openairdocs.org/sdr/DALA1106449864.md): Floor Panel · cracked · Jan 26, 2011 · N773NC · Doug DC951 · Fuselage Floor Panel
  > MAIN PASSENGER CABIN PANEL NR61 TOP SKIN CRACKED TRIMMED OUT DAMAGED AREA 3.2500" X 2.5". FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-01, FIG 4 SHEET 1, 51-10-4 AND 51-10-3. REQUIRED INSPECTION COMPLETED.
- [SDR DALA1106439864](https://openairdocs.org/sdr/DALA1106439864.md): Cusp Web · cracked · Jan 26, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN PAX CABIN RT SIDE CUSP WEB HAS 1 EA CRACK AND ELONGATED HOLES UNDERNEATH OF OTBD SEAT TRACK AT STA 229, RBL 46. REMOVED DAMAGED CUSP WEB. FABRICATED NEW CUSP WEB IAW DWG09530019 IAW SRM 53-13-2. CUT OUT ADDITIONAL DAMAGE AT STA 237. FABRICATED AND INS
- [SDR DALA1106129864](https://openairdocs.org/sdr/DALA1106129864.md): Floor Panel · corroded · Jan 25, 2011 · N773NC · Doug DC951 · Fuselage Floor Panel
  > MAIN PASSENGER CABIN STA 148-160, FLOOR PANEL 14B HAS CORROSION. MFG FLOOR PNL NR14 IAW DWG 9957826, REV ORIGINAL AND ER/A 488341-14 REV ORIGINAL. STENCILED AND IDENTIFIED PANEL IAW PS 900-5-1, NR 04 P-117 25 JAN 11. REQUIRED INSP COMPLETED.
- [SDR DALA1106119864](https://openairdocs.org/sdr/DALA1106119864.md): Floor Panel · corroded · Jan 25, 2011 · N773NC · Doug DC951 · Fuselage Floor Panel
  > MAIN PASSENGER CABIN STA 148-160, FLOOR PANEL NR15 HAS CORROSION. MFG FLOOR PANEL NR15 IAW DWG 9957825, REV ORIGINAL AND ER/A 488340-14 REV ORIGINAL. STENCILED AND IDENTIFIED PANEL IAW PS900-5-1, NR 04, P-117. CORRECTED. REQUIRED INSPECTION COMPLETED.
- [SDR DALA1106109864](https://openairdocs.org/sdr/DALA1106109864.md): Floor Panel · cracked · Jan 25, 2011 · N773NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR105 CRACKED TOP SIDE IN FLOOR PANEL RACK. MFG FLOOR PNL NR105 IAW DWG 9915532, REV ORIGINAL AND ER/A 488724-14 REV ORIGINAL. CORRECTED. REQUIRED INSPECTION COMPLETED.
- [SDR DALA1106099864](https://openairdocs.org/sdr/DALA1106099864.md): Floor Panel · damaged · Jan 25, 2011 · N773NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL, 30 HOLES BROKE OUT AND ELONGATED IN FLOOR PANEL RACK. FABRICATED NEW NR 30 FLOOR PANEL IAW DWG 9957915. INSTALLED 5 EA HAT CHANNELS IAW SRM 51-30-7. TAGGED REPAIR IAW DPS 900-5-1 AND IAW ERA 488746-14. REQUIRED INSPECTION COMPLETED.
- [SDR DALA1106069864](https://openairdocs.org/sdr/DALA1106069864.md): Longeron · damaged · Jan 25, 2011 · N773NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT STA 674, L29L BOTTOM SIDE OF TOP LEG DAMAGE. REMOVED DAMAGE FROM STA 674, L29L, ORIG MAT.080, LOSS MAT.050, REMAINING.030. FOUND TO BE OUT OF LIMITS IAW SRM 53-01. REMOVED L29 FROM STA 647 TO 698 IAW SRM 51-30-5, 51-30-2,51-30-1. INSTALLE
- [SDR DALA1108789864](https://openairdocs.org/sdr/DALA1108789864.md): Web · corroded · Jan 24, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING M-CK, CORROSION WAS FOUND ON THE WEB AT STA 1108 BETWEEN L24R & L26R. ONCE BLENDED OUT, THE PART DAMAGE WAS OUT OF SRM LIMITS. WORK IAW ER/A 488329-14 AS FOLLOWS: SECT I, SECT II - ON OR BEFORE 3,000 CYCLES AFTER SECTION I, SECT III - WITHIN EVERY 3,0
- [SDR DALA1105789864](https://openairdocs.org/sdr/DALA1105789864.md): Floor Panel · chafed · Jan 24, 2011 · N773NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PNL 62 FASTENER HOLES ELONGATED, CHAFED AND BROKE OUT. ORIG MATERIAL THICKNESS.025 IAW SRM 53-23-0. MATERIAL LOSS MAXIMUM.009 MATERIAL REMAINING.016 IAW SRM 53-01, FIG 1. RECEIVED MATERIAL FOR WEB AND HAT CHANNEL IAW DWG 9957919. DRILLE
- [SDR DALA1105739864](https://openairdocs.org/sdr/DALA1105739864.md): Door Frame · corroded · Jan 24, 2011 · N773NC · Doug DC951 · Fuselage Main, Structure
  > FWD CARGO DOOR JAMB WEB STA 370-427 HAS CORROSION AT CORENUTS. REMOVED CORROSION ORG MAT.040. REMOVED.013, REMAINING.027 FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. R & R WEB IAW SRM 51-30-2 AND 51-30-5. REQUIRED INSP COMPLETED.
- [SDR DALA1105479864](https://openairdocs.org/sdr/DALA1105479864.md): Attach Angle · cracked · Jan 23, 2011 · N773NC · Doug DC951 · Nacelle/Pylon, Attach Fittings
  > NR 2 ENG PYLON FWD LOWER ATTACH ANGLE FOR PANEL 8220NW HAS APPROX 1 IN CRACK AT FWD END. REMOVED & FABRICATED NEW ANGLE IAW SRM 54-04, FIG 10 PRIMED IAW SRM 51-10-3 INSTALLED IAW SRM 51-30-5 & 54-04 FIG 10 & 51-30-2. REQUIRED INSP COMPLETED.
- [SDR DALA1105469864](https://openairdocs.org/sdr/DALA1105469864.md): Skin · damaged · Jan 23, 2011 · N773NC · Doug DC951 · Fuselage Main, Plate/Skin
  > FWD CARGO BS 522-541, L24R, FUSELAGE SKIN HAS 3EA FASTENER HOLES KNIFE EDGED. CUT SECTION OUT FOR SKIN REPAIR STA 516-550. RT STATIC PORT IAW SRM 53-04, FIG 12C FABRICATED NEW SECTION, TREATED & PRIMED IAW SRM 53-04 FIG.12C, 51-10-3 FABRICATED FINGER DOUBLER
- [SDR DALA1105049864](https://openairdocs.org/sdr/DALA1105049864.md): Web · corroded · Jan 23, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > AFT CARGO STA 1106 TO 1116 BETWEEN L24R AND L26R WEB HAS CORROSION. REPAIRED WEB IAW ERA 488337-14 WEIGHT OF DOUBLER IAW 30-10-7 IS 63 GRAMS TOOL NR 9513 INSTALLED & EDGE SEALED, ID TAG IAW DPS 900-5-1. CUTOUT DAMAGE 7." X 15.5 CORRECTED BY LOVE 490448.
- [SDR DALA1105459864](https://openairdocs.org/sdr/DALA1105459864.md): Fitting · cracked · Jan 21, 2011 · N773NC · Doug DC951 · Vertical Stabilizer
  > AFT ACCESORY COMPARTMENT STA 1258 VERTICAL STAB. RT SIDE FITTING CRACKED. RECEIVED NEW FITTING IAW TRAVELER 2311NO21922, OK TO TREAT HOLES. TREATED AND PRIMED HOLES IAW SRM 51-10-3. INSTALLED NEW FITTING IAW SRM 51-30-1 AND SRM 51-30-5. REQUIRED INSPECTI
- [SDR DALA1105349864](https://openairdocs.org/sdr/DALA1105349864.md): Floor Support · corroded · Jan 21, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN PASSENGER CABIN BETWEEN STA 1151-1167, RBL 18 FLOOR SUPPORT CORRODED. REMOVED CORROSION AND FABRICATED NEW SUPPORT. HEAT TREATED ON TRAVELER 2311NO2233. INSTALLED SUPPORT IAW SRM 51-30-1 AND 51-01,P-226, REQUIRED INSPECTION COMPLETED.
- [SDR DALA1105329864](https://openairdocs.org/sdr/DALA1105329864.md): Floor Support · damaged · Jan 21, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING REPAIR ON SUPPORT STA 1151-1167, RBL 18, NR 6C/230, FOUND SUPPORT CHANNEL WITH MULTIPLE DOUBLE DRILLED HOLES AND ELONGATED HOLES. FABRICATED NEW SUPPORT FROM.050. HEAT TREATED ON TRAVELER 2311 NR 02266. INSTALLED SUPPORT IAW SRM 51-01 AND 51-30-1.P-2
- [SDR DALA1105299864](https://openairdocs.org/sdr/DALA1105299864.md): Floor Panel · cracked · Jan 21, 2011 · N773NC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PANEL NR 75 CRACKED AND PUNCTURED AT AFT INBD SIDE. CUT OUT DAMAGE 2EA PLACES 1" X 2". NO DEFECTS IAW NDT SPM 06-10-01. FABRICATED AND REINSTALLED 2EA FILLERS AND 1EA DOUBLER FROM.025, 7075-T6 PO 1120034 IAW SRM 53-01, FIG 4, SHEET 4.
- [SDR DALA1105279864](https://openairdocs.org/sdr/DALA1105279864.md): Doubler · cracked · Jan 21, 2011 · N773NC · Doug DC951 · Fuselage Main, Plate/Skin
  > MAIN PASSENGER CABIN STA 237, LBL 55 DOUBLER CRACKED. GAINED ACCESS & REMOVED EXISTING PREVIOUSLY REPAIRED CUSP WEB AT FS218 TO 237, LBL 44-55 IAW SRM 51-10-4,51-30-2 & 51-30-5. FABRICATED NEW WEB IAW DWG 9910699 REV M IAW SRM 51-10-2 & 51-10-4. HFEC INSP
- [SDR DALA1105149864](https://openairdocs.org/sdr/DALA1105149864.md): Longeron · damaged · Jan 21, 2011 · N773NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT BETWEEN STA 522-541 RT SIDE LONGERON 24 HAS 2EA CUTOUTS IN TOP LEG OF LONGERON. REMOVED SECTION OF LONGERON 24 RT SIDE FROM STA 491 TO STA 569. NDT NO CRACKS NOTED. REPLACED WITH NEW SECTION OF LONGERON LOCATED, DRILL AND INSTALLED IAW SRM 5
- [SDR DALA1105019864](https://openairdocs.org/sdr/DALA1105019864.md): Intercostal · damaged · Jan 21, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR JAMB, 5 EA INTERCOSTALS HOLES ELONGATED. REMOVED AND INSTALLED (5EA) INTERCOSTALS IAW SRM 51-30-05. REQUIRED INSPECTION COMPLETED.
- [SDR DALA1104999864](https://openairdocs.org/sdr/DALA1104999864.md): Threshold · damaged · Jan 21, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FS 427 TO 370 STEEL THRESHOLD HAS 31EA (PREVIOUS REPAIR) DRILLED OUT HOLES. REMOVED THRESHOLD & CLIP. RECEIVED NEW PART. LOCATED AND INSTALLED IAW SRM51-10-4-51-30-2 AND 51-30-5, 53-13, 53-05. REQUIRED INSPECTION COMPLETED.
- [SDR DALA1104979864](https://openairdocs.org/sdr/DALA1104979864.md): Frame · cracked · Jan 21, 2011 · N773NC · Doug DC951 · Fuselage Main, Frame
  > MAIN PASSENGER CABIN STA 1136 OTBD BETWEEN LONGERON FRAME CLIP IS CRACKED. R & R FRAME CLIPS IAW SRM51-30-5. REMOVED AND INSTALLED FASTENERS FOR ACCESS IAW SRM 51-30-5. CLEANED UP MINOR SCRATCHES ON SURROUNDING AREA IAW SRM 53-01 & SRM 51-10-3 AND FABRICATED
- [SDR DALA1103999864](https://openairdocs.org/sdr/DALA1103999864.md): Floor Panel · cracked · Jan 19, 2011 · N773NC · Doug DC951 · Fuselage Floor Panel
  > FLOOR PANEL NR 68, 1 EA CRACK ON FASTENER HOLE. REMOVED CRACK IAW SRM 53-01, FIGURE 2. FABRICATED DOUBLER AND FILLER IAW SRM 53-01, FIG 2. INSTALLED DOUBLER AND FILLER IAW SRM 51-30-2. REQUIRED INSP COMPLETED.
- [SDR DALA1103989864](https://openairdocs.org/sdr/DALA1103989864.md): Intercostal · cracked · Jan 19, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > LT FWD OVERWING EMERGENCY EXIT DOOR PAN FWD SIDE AT FS712, L12 INTERCOSTAL CLIP IS CRACKED. REMOVED CLIP IAW SRM 51-30-2 AND DWG 5910537-18. FABRICATED AND TRIMMED, PICKED HOLES IAW SRM 51-10-2 AND DWG 5910537-18. INSTALLED NEW CLIP IAW SRM 51-30-05. REQUI
- [SDR DALA1104179864](https://openairdocs.org/sdr/DALA1104179864.md): Web · chafed · Jan 18, 2011 · N773NC · Doug DC951 · Emergency Exits
  > RT AFT OVER WING EMERGENCY EXIT ABOVE DOOR LOCK WEB IS CHAFED. CHAFED OUT OF LIMITS. CUT OUT 1" X 2" IAW SRM 09-00-01. FABRICATED AND DRILLED IAW SRM 51-70-4. DAMAGE CONTAINED IAW NDT SPM 06-10-01.001. INSTALLED IAW SRM 51-30-5. REQUIRED INSPECTION COMPL
- [SDR DALA1104139864](https://openairdocs.org/sdr/DALA1104139864.md): Brace · damaged · Jan 18, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN PASSENGER CABIN BETWEEN STA 218-237, LBL 55, 2EA FASTENERS MISSING IN BRACES. REMOVED REMAINING FASTENERS IAW SRM 51-30-2. FABRICATED RADIUS FILLERS IAW EO 94FS481230. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED FASTENERS, FILLERS, AND BRACES IAW SRM
- [SDR DALA1104079864](https://openairdocs.org/sdr/DALA1104079864.md): Web · cracked · Jan 18, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN CABIN-STA 712, L12L CLOSEOUT WEB CRACKED AT TOP FASTENERHOLE. GAINED ACCESS STA 712 CABIN WINDOW NR26. REMOVED FRAME AND DAMAGED CLOSEOUT WEB. LOCATED, DRILLED, DEBURRED, ALODINED. PRIMED AND INSTALLED NEW CLOSEOUT WEB IAW SRM 51-10-2, 51-10-4, 51-30-
- [SDR DALA1104129864](https://openairdocs.org/sdr/DALA1104129864.md): Floor Panel · corroded · Jan 17, 2011 · N773NC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 21 CORRODED IN FLOOR PANEL RACK. RECEIVED NEW FLOOR PANEL NR 21. TO BE INSTALLED ON JOB CARD 0590-4010-8M. LOCATED AND DRILLED, LOCATED AND DEBURRED FLOORPANEL NR 21 IAW SRM 51-10-4 TO BE INSTALLED ON WORK CARD 2311R68.
- [SDR DALA1103719864](https://openairdocs.org/sdr/DALA1103719864.md): Attach Fitting · cracked · Jan 15, 2011 · N773NC · Doug DC951 · Fuselage Main, Attach Fittings
  > MAIN PASSENGER CABIN STA 1136 OTBD BETWEEN LONG 14-15L, FRAME CLIP IS CRACKED. REMOVED AND INSTALLED NEW FRAME CLIP IAW SRM 51-30-2 AND 51-30-5. RESTORED ACCESS. REQUIRED INSP COMPLETED.
- [SDR DALA1103669864](https://openairdocs.org/sdr/DALA1103669864.md): Floor Support · cracked · Jan 15, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous Structure
  > MAIN PASSENGER CABIN STA 313, LBL 1, FLOOR SUPPORT, Z-ANGLE CRACKED. REMOVED FLOOR SUPPORT IAW SRM 51-30-2. FABRICATED & INSTALLED FLOOR SUPPORT IAW SRM 51-30-5. REQUIRED INSP COMPETED.
- [SDR DALA1103439864](https://openairdocs.org/sdr/DALA1103439864.md): Shear Tie · cracked · Jan 14, 2011 · N773NC · Doug DC951 · Fuselage Internal Mounting Structure
  > MAIN PASSENGER CABIN STA 1116 BELOW LONG 14 FRAME NEAR TIE IS CRACKED. REMOVED, FABRICATED, & INSTALLED SHEAR TIE IAW SRM 51-30-2, SRM 51-30-5 & DWG 9957739. REQUIRED INSP COMPLETED.

Next page: https://openairdocs.org/deregistered/N773NC-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 = 'N773NC' AND deregistration_id = 'N773NC-2014-06-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N773NC-2014-06-17/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.