N766NC, cancelled Jun 17, 2014
Service difficulty reports · 206
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 = 'N766NC' AND deregistration_id = 'N766NC-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.
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 = 'N766NC' AND deregistration_id = 'N766NC-2014-06-17' 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 DALA13043040857Power Supply · inoperativeEMERGENCY CEILING LIGHT INOPERATIVE AT ROW 20,21,AND 22. R & R POWER SUPPLY IAW AMM 33-53. OPS CHECKED NORMAL.SDR DALA13025840857Angle · damagedRT PYLON LOWER SURFACE ANGLE INBD OF AFT ENGINE MOUNT VIBRATION ISOLATOR CRACKED, SIX PULLED RIVETS, TWO LOOSE RIVETS. REMOVED ANGLE, TRIMMED OUT DAMAGE AND ACCOMPLISHED REPAIR IAW ER/A 515301-14, REV ORIGINAL.SDR DALA13025090857Power Supply · inoperativeEMERGENCY LIGHTS ROWS 23-26 FAILED TO ILLUMINATE. REPLACED FAULTY EMERGENCY POWER SUPPLY IAW AMM 33-53. OPS CHECKED NORMAL. OK FOR SERVICE.SDR DALA13023950857Frame · crackedAFT PRESSURE BULKHEAD FORMER AT LONGERON 14L CRACKED. INSTALLED DOUBLERS IAW SRM 53-01.SDR DALA13023940857Bulkhead · crackedAFT PRESSURE BULKHEAD FORMER AT LONGERON 12L LWR SKIN CRACKED ON AFT WALL. VERIFIED CRACK WITH HFEC IAW NDT SPM 06-10-01.001. STOP DRILLED CRACK IAW SRM 53-01. CRACK CONTAINED IAW HFEC INSPECTION NDTSPM 06-10-01. FABRICATED DOUBLERS IAW SRM 53-01. INSTASDR DALA13024590857Tee Fitting · crackedTEE FITTING CRACKED AT L14 BS 1167. REMOVED & INSTALLED NEW TEE FITTING IAW SRM 53-03.SDR DALA13024600857Frame · crackedAFT PRESSURE BULK HEAD FRAME CRACKED. APB FRAME REPLACED IAW EM 5310-01203-04E.SDR DALA13012670857Battery Pack · inoperativeEMERGENCY EXIT SIGN AND FIVE SEAT MOUNTED LIGHTS INOPERATIVE. FOUND BATTERIES DEAD. REPLACED BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-53-00. OK FOR SERVICE.SDR DALA13004670857Power Supply · inoperativeSEAT 19-22, EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AT AFT RT OVERWING EMERGENCY EXIT IAW AMM 33-53. OPS CHECK GOOD.SDR DALA12016820857Attach Fitting · damagedLEFT MLG RETRACT ACTUATOR ATTACH FITTING, BORE AND FACE DAMAGED. MACHINED BORE AND FACE TO REMOVE DAMAGE. BORE WITHIN LIMITS BUT FACE IS NOT IAW AA CARD 5740-01114-01A. BORE IS WITHIN LIMITS FOR A .025 O/S BUSHING. REMOVED .017 FROM INBD FACE TO REMOVE CORSDR DALA1256899857Support Fitting · damagedLT MAIN GEAR SUPPORT FITTING BORE AND FACE DAMAGED. REPAIRED IAW ER/A 509731-14AD, REV ORIG.SDR DALA12006330857Skin · damagedLT ELEVATOR UPPER OTBD SKIN HAS A LIGHTNING STRIKE. REMOVED DAMAGE (CUT-OUT) ON LT ELEVATOR UPPER OTBD SKIN, FABRICATED REPAIR DOUBLER FROM CLAD 2024-T3 AND REWORKED TO 0.036. PERFORMED HFEC INSPECTION AND NOTED NO CRACKS AT CUT OUT. LOCATED AND DRILLED REPSDR DALA12006270857Skin · damagedFWD CARGO DOOR HAS OUTER EDGE DAMAGE, WEAR, GOUGES, AND BENDS. DAMAGE ON FWD LWR CARGO DOOR OUTER SKIN FOUND TO BE OUT OF LIMITS IAW MD-88 SRM 52-01 PG 6. PERFORMED PRI 505976-14 REV O, ACCOMPLISHED ER/A 505976-14 REV ORIGINAL AT FWD CARGO DOOR OUTER SKIN ONSDR DALA12006120857Door Frame · corrodedFWD CARGO COMPARTMENT DOOR CUT OUT LOWER FRAME HAS SURFACE CORROSION. REPAIRED FWD CARGO COMPARTMENT DOOR CUT OUT LOWER FRAME.SDR DALA12006100857Door Frame · crackedDURING EDDY CURRENT INSPECTION FWD SERVICE DOOR JAMB FORWARD UPPER CORNER SECT 01B, CRACK INDICATIONS (1 ON SKIN, 2 SUB-SURFACE) WERE DETECTED EMANATING FROM FASTENERS AS MARKED, ALL CRACKS APPROX 1/8 INCH IN LENGTH. REPAIRED FWD SERVICE DOOR JAMB FWD UPPER CSDR DALA12006110857Spar · crackedRIGHT WING REAR SPAR XRS 137, WEB HAS CRACK AT TOP OF LIGHTENING HOLE. REMOVED RT FLAP FORWARD MOVABLE VANE FOR ACCESS, REMOVED DAMAGED WEB ASSEMBLY AT RT WING REAR SPAR. REMOVED ALL SUPPORT ATTACH ANGLES TO RT WING REAR SPAR WEB. FABRICATED RIB LT WING REASDR DALA12001780857Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY ESCAPE LIGHTS IN THE TAIL COMPARTMENT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHT FIXTURES AND RETURNED THE AIRCRAFT TO SERVICE.SDR DALA1219739857Battery · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 5-8 AND 23-26 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.SDR DALA1135919857Coalescer Bag · dirtyENROUTE, FLIGHT DIVERTED, DUE TO A PERSISTENT HOT PLASTIC BURNING ODOR IN THE FORWARD GALLEY BETWEEN MAIN DOOR AND FORWARD LAVATORY. THERE WAS NO VISUAL CONFIRMATION OF SMOKE. MAINTENANCE FOUND THE COALESCER BAGS SATURATED AND DIRTY, REMOVED AND REPLACED THSDR DALA1123319857Connector · disconnectedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING BY THE GALLEY CLOSET AREA WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR BEHIND THE POWER SUPPLY UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.SDR DALA1123159857Outflow Valve · unresponsiveFLIGHT DIVERTED TO BUF WITH A LOSS OF CABIN PRESSURIZE. AT FL330, CABIN WAS CLIMBING 2KFT/MIN AND THE OUTFLOW VALVE SEEMED UN-RESPONSIVE. CREW COMPLIED WITH QRH PROCEDURES, DONNED MASK AND COMMENCED AN EMERGENCY DESCENT. CABIN ALTITUDE REACHED 14K BUT MASKSSDR DALA1113669857Pan · corroded1D/29 FWD CARGO COMPT CARGO DOOR LOWER JAMB PAN HAS EXFOLIATED CORROSION ON SEVERAL AREAS. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1 AND NDT SPM 04-00-06. FABRICATED REPAIR AND INSTALLED REPAIR SPLICES IAW DC9 SRM 51-10-4, 53-05 FISDR DALA1113659857Intercostal · cracked1D/111 FORWARD CARGO COMPT STA 503-522 RBL 48 INTERCOSTAL IN TUNNEL AREA IS CRACKED AND INBD WATER TANK SUPPORT BRACKET HAS 3 SHEARED FASTENERS. REMOVED INTERCOSTAL PART 5919741-6 IAW DC9 SRM 51-30-2 STOP DRILLED CRACKS IAW DC9 SRM 53-01 FIG 2 SHT.3 ACCOMPLISDR DALA1113639857Frame · cracked1F/46 AFT ACCESSORY COMPARTMENT CANTED FRAME 1303 AT RT LOWER END IS CRACKED. REMOVED DAMAGED AREA 1"X1" NDTHFEC USING A2469 ZETEC PER NDT SPM FOUND CRACK FREE AREA. FABRICATED .050 REPAIR DOUBLER & .040 FILLER & INSTALLED IAWDC-9 SRM 51-10-3, 51-70-5 & ER/ASDR DALA1112519857Cargo Track · corrodedFORWARD CARGO COMPT RT SIDE TIEDOWN TRACK BETWEEN FUS STA 218 AND STA 370 HAS CORROSION. REMOVED CORROSION IAW DC9 SRM53-01 FIG 1 ORIG MAT'L .100 REMOVED .027 .073 REMAINING FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1. REMOVED DAMAGED TRACK IAW DC9 SRMSDR DALA1112259857Channel · crackedLT MLG W/W DOOR INTERIOR SIDE FWD ZEE CHANNEL IS CRACKED AT INBD END. REMOVED CHANNEL IAW DC-9 SRM 51-30-2, 51-30-5 AND 51-30-6. LOCATED DRILLED AND INSTALLED NEW CHANNEL IAW DC9 SRM 51-10-4, 51-30-2, 51-30-5 AND 51-30-6, P-205 Q-948 490448. REQUIRED INSPECSDR DALA1112499857Floorbeam · corrodedAFT CARGO COMPARTMENT STA 1167 RBL 50 UPPER FLOORBEAM HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED CORRODED FLOORBEAM ANGLE FABRICATED REPAIR PARTS AND GUSSETUSING TRAVELER NR 2446 N01735 AND 2446N01744. INSTALLED REPAIR PARTS IAW DC9 SRM SDR DALA1112539857Skin · damagedFUSELAGE EXTERIOR STA 475 L27L FASTENER HOLE IN SKIN TORN OUT. REMOVED DAMAGED IAW BOEING DOC NR 5609530001 M1 MAT ID FILLER IAW DC9 SRM 53-30-0 FIG 2 SHT 1 AND 2 AND 51-60-0 FIG1 SHT 1. FINGER DOUBLER .032 IAW BOEING DOC 560950001 M1 PO NR 1120167 FABRICATESDR DALA1112529857Skin · damagedFUSELAGE EXTERIOR STA 489 L27L FASTENER HOLE IN SKIN TORN OUT. REMOVED DAMAGE IAW BOEING DOCUMENT NR 5609530001 M1 NDT NO DAMAGE INDICATION NOTED. MAT ID FILLER .050 IAW DC9 SRM 53-30-0 FIG 2 SHT 1 AND 2 AND 51-60-0 FIG 1 SHT 1 FINGER DOUBLER .032 IAW BOEINGSDR DALA1110899857Floor Support · corrodedMAIN PASSENGER CABIN STA 237, RBL 14 FLOOR SUPPORT CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ORIGINAL MAT .050, REMOVED .049, REMAIN .001 RECEIVED MATERIAL FABRICATED NEW PART LOCATED DRILLED DEBURRED TREATED AND PRIMED AND INSTALLED NEW PARTS IAWSDR DALA1110489857Skin · dentedDURING CURRENT M-CHECK DENTS WERE FOUND ON FUSELAGE SKIN LOCATED BETWEEN STA 1380 TO STA 1401, AND BETWEEN S-27R AND S-29L. ER/A 489003-14 SECTION I ACCOMPLISHED DURING M-CK. SECTION II APPROVAL IS LIMITED TO 12 MONTHS (365DAYS) SERVICE ONLY. ADDITIONAL ER/SDR DALA1110469857Fitting · corrodedFORWARD CARGO COMPARTMENT STA 360 BETWEEN L27R AND L28R TIE DOWN TRACK FITTING HAS CORROSION. REMOVED AND REPLACED TIE DOWN CLIP HAD 100% MATERIAL LOSS IAW DC 9 SRM 53-01 FIG 1. INSTALLED IAW DC9 SRM 51-30-5.SDR DALA1110399857Floor Panel · crackedMAIN PASSENGER CABIN FLOOR PANEL 41 HAS APPROX 10EA CRACKS. FOUND FLOOR PANEL 41 UNREPAIRABLE. FABRICATED NEW PANEL. IDENTIFIED PANEL AS PERMANENT STENCILED PANEL "NOT FOR RESALE" PER ERA 488345-14 AND DC9 SRM 51-10-3.SDR DALA1110329857Door Frame · corrodedFUSELAGE EXTERIOR FORWARD AIR STAIR DOOR FRAME INTERIOR HAS CORROSION. REMOVED AND REPLACED DOOR FRAME IAW DC-9 SRM 51-30-1 AND 51-30-2. REMOVED AND INSTALLED DOOR ASSEMBLY FOR ACCESS IAW MM 52-62-00. PRESSURE LEAK CHECK TO BE ACCOMPLISHED ON SDR DALA1110389857Floor Panel · damagedMAIN PAX CABIN FLOOR PANEL 81 HAS SEVERAL ELONGATED FASTENERS HOLES AT FWD FLANGE BS 851. REMOVED PANEL FOUND UNREPAIRABLE. FABRICATED ALODINED AND PRIMED NEW FLOOR PANEL APPLIED STENCIL & ID TAG 'P' PER ERA 488732-14 INSTALLED PANEL.SDR DALA1110379857Floor Panel · crackedMAIN PAX CABIN FLOOR PANEL 60D HAS 3EA CRACKS AT RIVET HOLES AND PULLED THROUGH RIVETS BS 674. REMOVED FOUND TO BE UNREPAIRABLE FABRICATED ALODINED AND PRIMED NEW FLOOR PANEL. APPLIED STENCIL & ID TAG 'P' PER ERA 488739-14 INSTALLED PANEL 60D.SDR DALA1110369857Floor Panel · damagedMAIN PASSENGER CABIN FLOOR PANEL 101 AFT END 3EA ELONGATED HOLES. FABRICATED NEW FLOOR PANEL 101 FROM ER/A 488734-14. LOCATED DRILLED COUNTERSINK HOLES IAW DC9 SRM 51-10-2, 51-10-3, 51-30-2 & ER/A 488734-14.SDR DALA1110359857Floor Panel · corrodedMAIN CABIN METAL SKIN FLOOR PANEL 84 HAS CORROSION AROUND FASTENER HOLES. REMOVED CORROSION FOUND PANEL TO BE OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1. ORG THICKNESS IS .025 IAW DWG PL9957919. REMOVED, .016.009 REMAINS. FABRICATED NEW PANEL AND HAT CHANNEL DRSDR DALA1110349857Floor Panel · corrodedMAIN CABIN METAL SKIN FLOOR PANEL 5 HAS CORROSION ON SKIN. REMOVED CORROSION IAW DC9 SRM 53-01 FIG 1 SHT 3 OUT OF LIMITS. FABRICATED IAW DWG 9957808 FABRICATED DRILLED DEBURRED & INSTALLED IAW DWG 9957808 & ER/A 488726-14.SDR DALA1110339857Floor Panel · tornMAIN PAX CABIN FLOOR PANEL 60B HAS 1EA TEAR AND SEVERAL PULL THROUGH RIVETS BS 617. REMOVED FLOOR PANEL IAW DC9 SRM 51-30-5. PANEL FOUND TO BE BEYOND REPAIR. OBTAINED MATERIAL TO FABRICATE NEW PANEL PER ER/A 488738-14 DRILLED PANEL AND HAT CHANNELS UP IAW DSDR DALA1109979857Doubler · corrodedFWD CARGO COMPARTMENT, STA 674-697, L28L-L28R INTERNAL DOUBLER CORRODED. GAINED ACCESS, R & R INTERNAL DOUBLER AND RESTORED ACCESS IAW SRM 51-30-1, 51-30-5, AND AMDS CARD 5331-01180-02. REQUIRED INSP COMPLETED.SDR DALA1109969857Skin · crackedFUSELAGE EXTERIOR FWD PASSENGER DOOR JAMB AFT UPPER DOOR STOP SKIN HAS APPROX .250 INCH CRACK RUNNING AFT OF DOOR STOP REF SR09530252-7001 DWG FOR REPAIR. REMOVED DAMAGE 2EA CUTOUTS 3.75" X 1.75" AND 2.1" X 3.75 AND INSTALLED DOUBLER & TRIPLER REPAIR IAW SRM5SDR DALA1109929857Floor Panel · crackedMAIN PASSENGER CABIN FLOOR PANEL NR 75 HAS 1EA CRACKED AT INBD FLANGE AND 1EA ELONGATED HOLE BS775, CORRECTED. FABRICATED FLOOR PANEL 75..SDR DALA1109919857Floor Panel · crackedMAIN CABIN METAL SKIN FLOOR PANEL NR 60A HAS 4 EA HAT CHANNELS CRACKED. FABRICATED FLOOR PANEL 60A IAW ER/A 488737-14 REV ORG P214, CORRECTED.SDR DALA1109899857Frame · crackedAFT ACCESSORY COMPARTMENT CANTED FRAME 1245 CRACKED AT FASTENER HOLE L4L. REMOVED DAMAGED CANTED FRAME 1245 IAW SRM 51-30-2 & 51-30-5. LOCATED, DRILLED, & INSTALLED NEWFRAME IAW SRM 51-30-2, 51-30-5. REQUIRED INSP COMPLETED.SDR DALA1109539857Floor Panel · corrodedMAIN METAL SKIN FLOOR PANEL, NR 67 HAS CORROSION AROUND EDGES. RECEIVED 1EA NEW FLOOR PANEL NR 67 & IAW SRM 53-23-0. DRILLED UP IAW SRM 51-10-4. INSTALLED, 1EA FLOOR PANEL NR 67. REQUIRED INSP COMPLETED.SDR DALA1109529857Floor Panel · corrodedMAIN CABIN METAL SKIN FLOOR PANEL NR 63 HAS CORROSION ON OTBD EDGE. RECEIVED FLOOR PANEL NR 63 IAW SRM 53-23-0, FIG 4 INSTALLED 1EA NEW FLOOR PANEL NR 63.SDR DALA1109519857Floor Panel · corrodedMAIN CABIN METAL SKIN FLOOR PANEL NR 30 HAS CORROSION ON SKIN PREVIOUS REPAIR. REMOVED PANEL NR 30 FROM CABIN FLOOR IAW SRM 51-30-1. FABRICATED FLOOR PANEL NR 30 IAW ER/A 488731-14. INSTALLED FLOOR PANEL NR 30 IAW SRM 51-30-1. REQUIRED INSP COMPLETED.SDR DALA1109509857Floor Panel · corrodedMAIN CABIN METAL SKIN FLOOR PANEL NR 27 HAS CORROSION ON SKIN. FOUND DAMAGED BEYOND REPAIR IAW SRM 53-01, FIG 1. FABRICATED 1EA FLOOR PANEL IAW DWG 9957919 & ER/A 488729-14. INSTALLED 1EA FLOOR PANEL NR 27 IAW DCARD 0590-0020-8M. REQUIRED INSP COMPLETED.SDR DALA1109499857Floor Panel · bentMAIN PASSENGER CABIN FLOOR PANEL NR 85 IS BENT AT FWD FLANGE, BS 851. REMOVED PANEL NR 85 IAW SRM 51-30-1, CUTOUT DAMAGE IAW SRM 53-05, FIG 2. FABRICATED DOUBLER & FILLER IAW SRM 53-05, FIG 2, INSTALLED DOUBLER & FILLER IAW 53-05, FIG 2. COMPLETED.
Back to N766NC, cancelled Jun 17, 2014