N767NC, cancelled Nov 12, 2019
Service difficulty reports · 113
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 = 'N767NC' AND deregistration_id = 'N767NC-2019-11-12' 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA13004240858Connector · looseEMERGENCY EXIT LIGHTS INOPERATIVE ON SEATS 6-8DEF. CONNECTED CONNECTOR BEHIND SIDEWALL PANEL 8F. EMERGENCY EXIT LIGHTS NOW OPS CHECKED NORMAL.SDR DALA13000380858Support Fitting · damagedCOMPLY 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 DALA12014240858Skin · corrodedAFT 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 AFTSDR DALA12014230858Skin · crackedFOUND 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 DALA12014260858Skin · crackedDURING 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 RESDR DALA12013480858Tee Fitting · crackedAFT 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 DALA12000120858Battery Pack · inoperativeDURING 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 DALA1159589858Battery Pack · dischargedDURING LINE CHECK, FOUND EMERGENCY EGRESS AISLE LIGHTING INOP, ROWS 5 THROUGH 9. REPLACED BATTERY PACK AT ROW 7 POWER SUPPLY.SDR DALA1149299858Channel · crackedCRACKED 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 PESDR DALA1138659858Connector · disconnectedDURING 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 DALA1131239858Skin · dentedDURING 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 - WISDR DALA1127659858Intercostal · wornMAIN 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 FLOORSDR DALA1127619858Floorbeam · wornMAIN 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). FABRICATSDR DALA1127529858Seat Track · corrodedSEAT 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 09-5300-3-151SDR DALA1127499858Skin · damagedLOWER 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 MEASUSDR DALA1127469858Skin · dentedCABIN 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 06-10-01.001SDR DALA1127459858Skin · corrodedCABIN 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, ITEMSDR DALA1127449858Skin · damagedCABIN 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. INSTALLSDR DALA1127439858Floorbeam · corrodedCABIN 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 SUPPOSDR DALA1127429858Floor Skin · corrodedMETAL 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 DALA1127419858Floor Support · corrodedCABIN 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 DALA1127409858Skin · damagedCABIN 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, FABRICSDR DALA1127349858Skin · corrodedCABIN 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 DALA1127299858Bracket · crackedFWD 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 DALA12012680858Floorbeam · corrodedFLOORBEAM 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 DALA1131709858Support · corrodedPASSENGER 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, FASDR DALA1126719858Skin · dentedLOWER 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 CHECKEDSDR DALA1126709858Skin · dentedLOWER 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 53-33-0SDR DALA1126589858Floor Panel · crackedCABIN 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 TOPSDR DALA1126579858Channel · damagedPASSENGER 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 DALA1126559858Floorboard · corrodedPASSENGER 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, FASDR DALA1126449858Angle · corrodedFWD 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,-21SDR DALA1128259858Floor Support · crackedCABIN 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 51-1SDR DALA1126659858Floorboard · crackedPASSENGER 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 DALA1126539858Floorboard · corrodedPASSENGER 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 DALA1126529858Floor Panel · dentedCABIN 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 DALA1126519858Floor Panel · damagedFLOOR 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 CRACKSSDR DALA1126509858Floor Panel · dentedCABIN 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 59303SDR DALA1126499858Floor Support · corrodedCABIN 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 DALA1126489858Floor Support · corrodedCABIN 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 DALA1126699858Skin · dentedLOWER 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 DALA1126479858Doubler · crackedBETWEEN 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 000165411SDR DALA1126019858Skin · dentedLOWER 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, INTSDR DALA1126689858Skin · crackedCRACKED 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 IAWSDR DALA1129989858Skin · damagedWEAR 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. TREASDR DALA1129869858Skin · damagedFUSELAGE 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. REPSDR DALA1129649858Skin · damagedFUSELAGE 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 SRSDR DALA1128789858Skin · dentedDENT 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 CUTOUTSDR DALA1127519858Seat Track · crackedFOUND 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 DALA1127509858Fitting · crackedAFT 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
Back to N767NC, cancelled Nov 12, 2019