N948DL, cancelled Aug 22, 2019
Service difficulty reports · 103
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 = 'N948DL' AND deregistration_id = 'N948DL-2019-08-22' 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 = 'N948DL' AND deregistration_id = 'N948DL-2019-08-22' 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 DALA2019011500259Smoke Detector · malfunctionedSMOKE DETECTOR WENT OFF IN AFT RT SIDE LAV ON DESCENT. LEAD F/A FOLLOWED PROCEDURE TO SILENCE IT. PERFORMED GVI OF LAV FOR INDICATIONS OF SMOKE NON NOTED. REMOVED AND REPLACED RT AFT LAV SMOKE DETECTOR PER AMM 26-13. PERFORMED LAV SMOKE DETECTION TEST PER AMM SDR DALA2018113006931Paint · missingRUDDER TAB MISSING PAINT. REMOVED RUDDER TAB REF MD88 AMM 27-20-02. INSPECTED AREA & ATTACHMENTS, OK TO INSTALL TRIM TAB. INSTALLED NEW RUDDER TAB REF AMM 27-20-02. INSPECTED INSTALLATION/SAFETY & ADJUSTMENT PER AMM 27-20-02. (LP5243521)SDR DALA2018092405720Power Supply · inoperativeDURING SERVICE CHECK MAINTENANCE FOUND ROW 24-30 LOWER EMERGENCY LIGHTS TO BE INOPERATIVE. THEY REPLACED THE POWER SUPPLY PER AMM 33-53. AND THE OPERATIONAL CHECK IS GOOD.SDR DALA2018082105163Battery Pack · inoperativeEMERGENCY CEILING LIGHTS AT 11A,13A/B,14A,22A,24 A/D, & 25A INOPERATIVE. REMOVED & REPLACED THE BATTERY PACKS ROW 12 & 24 IAW AMM 33-55. OPS CHECKED GOOD.SDR DALA2018060703863Cable · out of positionTAILCONE UNSAFE MESSAGE. FOUND INTERIOR CABLE DISCONNECTED, OUT OF RETAINING MECHANISM. SECURED THE CABLE AND PERFORMED ODI TEST IAW AMM 53-53-00. OPS NORMAL ACFT OK FOR SERVICE. THE TAILCONE SLIDE REARMED. INSPECTION AND RIGGING OK IAW AMM 53-53.SDR DALA2018060403774Light · inoperativeSEAT 19 EMERGENCY LIGHT NOT WORKING. REMOVED AND REPLACED EMERGENCY LIGHT ON SEAT 19 REF AMM 33-53 OPS CHECK GOOD.SDR DALA2018052403541Engine · failedAT 27,000 FT LEFT ENGINE PRODUCED A LOUD BANG AND IMMEDIATELY FOLLOWING THE EPR, N1, N2 ROLLED BACK TO IDLE. WE CONDUCTED THE ENGINE SEVERE DAMAGE QRH AND LANDED WITH THE LEFT ENGINE AT IDLE. THE RIGHT ENGINE NEVER EXCEEDED ANY LIMITS DURING THE FAILURE. REF SDR DALA2018032201837Battery Pack · dischargedTOP AFT LEFT AND RIGHT OVER WING EMERGENCY DOOR EMERGENCY LIGHT INOP. T/S TOP AFT LT/RT OVER WING EXIT DOOR EMERGENCY LIGHT PER AMM 33-50. R&R EMERGENCY BATTERY PACK. OPS CK GOOD. OK FOR SVC.SDR DALA2018031501725Wire · brokenSEAT MOUNTED EMERGENCY LIGHT AT 28DE INOP, TERMINAL PLUG WIRE BROKEN. RETERMINATED TERMINAL PLUG AT SEAT 28DE PER SPWM CHAPTER 20 AND EWIS OPS CKS GOOD.SDR DALA2018012500419Clamp · failedRETURNED TO DEPARTURE DUE TO A TAIL COMPARTMENT TEMP HIGH MESSAGE. PERFORMED QRH AND MESSAGE EXTINGUISHED WITH LEFT ENGINE AT IDLE. DURING THE RETURN, THE CABIN PRESSURE WAS LOST AND PASSENGER OXYGEN MASKS DEPLOYED. AN EMERGENCY WAS DECLARED. DURING AN EMESDR DALA2018012600429Bracket · crackedON ''A'' CHECK FOUND ATTACH BRACKET FOR HANDRAIL IN TAIL COMP CRACKED. ROBBED HAND RAIL ATTACH BRACKET P/N 5930556-15. INSTALLED BRACKET PER MD88-AMM53-40.SDR DALA2017092507085Battery · dischargedOVERWING EXIT SIGN LIGHTS OVER FWD DOORS INOP. R&R BATTERIES IAW AMM 33-53-00.SDR DALA2017070305173Wire · defectiveSEAT MOUNTED EMERGENCY LIGHTS AT 14D AND 28D INOP. REPLACED PIG TAIL AT 14D AND RETERMINATED CONNECTOR AT 28D PER AMM 33-52 AND EWIS. OPS CKS GOOD.SDR DALA2017041703101Door · looseLT FWD OVERWING EXIT DOOR NOT FLUSH WITH FUSELAGE AND LOOSE. ADJUSTED LT FWD OVERWING EXIT DOOR IAW AMM 52-21-00, OK FOR SERVICE.SDR DALA2017032802472Guide · wornBAD VIBRATION AT FRONT OF AIRPLANE CLIMBING OUT ABOVE 300 KNOTS. PERFORMED GVI FOUND EXCESSIVE PLAY ON RADOME GUIDE PIN HOLES R&R RADOME REF AMM 53-51.SDR DALA2016122009994Door Frame · crackedCRACKED DOOR FRAME FWD ACCESSORY COMPARTMENT, THE DOOR FRAME WAS REPAIRED IAW ER/A 552876-14 REV. ORIGINAL AND ETI -88-16-484 REV. 2.SDR DALA2016121909966Skin · dentedDENTS ON UPPER SKIN AT LT ELEVATOR CONTROL TAB. ELEVATOR CONTROL TAB P/N 5910413-511; S/N 49533 (OFF) WAS REMOVED AND INSTALLED SERVICEABLE CONTROL TAB P/N 5910413-507; S/N 49983 (ON).SDR DALA2016121509881Skin · damagedNICKS ON LOWER SKIN AT INBOARD LT WING FLAP. THE FLAP WAS REPAIRED IAW SRM 57-01-FIG.5.SDR DALA2016121509878Longeron · corrodedCORROSION ON LONGERON 29L BETWEEN BS 1271 - 1309. REPAIRED IAW SRM. 53-02, FIG 18.SDR DALA2016121409846Pan · crackedCRACKED MAIN ENTRANCE DOOR PAN ON FWD UPPER CORNER PAN ON FWD UPPER CORNER OF MAIN L1 DOOR. REPAIRED IAW SRM 52-05 FIG. 18A.SDR DALA2016121209791Lanyard · brokenPAX CABIN, BROKEN WIRES ON L2 SLIDE LANYARD. LANYARD WAS REPLACED PER AMM 25-62-00 PARAGRAPH D-4.SDR DALA2016121209783Pan · crackedDOOR, CRACK ON FWD PAN BTW NR 3 AND 4 BEAMS AT R1 DOOR. PAN BTW BEAMS NR 3 AND 4 WAS REPAIRED PER SRM 52-03 D FIG 3.SDR DALA2016121009780Longeron · crackedPAX CABIN CRACKED LONGERON 3 LT ON STA Y=180. FASTENER WAS REMOVED AND INSTALLED PER SRM 51-30-5 AND HFEC INSPECTION WAS ACCOMPLISHED PER NDT SPM 06-10-01.001 AND NO CRACKS WERE FOUND.SDR DALA2016120909772Support · crackedDOOR, CRACKED SUPPORT ON LT INBD MLG DOOR STA Y=962-970 AND X=30. LANDING GEAR DOOR WAS REPLACED.SDR DALA2016120509547Actuator · leakingDURING APPROACH, FLIGHT ATTENDANTS REPORTED A BURNING ODOR IN THE FORWARD GALLEY. MAINTENANCE FOUND HYDRAULIC FLUID IN THE APU INLET. DETERMINED THE SOURCE TO BE A LEAKING VENTRAL AIR STAIR ACTUATOR. THE ACTUATOR WAS REPLACED AND DUCT CLEANING AND BURNOUT WAS SDR DALA2016113009420Battery Pack · dischargedLT AND RT OVERHEAD, OVERWING EXIT LIGHTS W/N ILLUMINATE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-53.SDR DALA2016112809292Tab · missingFLAME SPRAY MISSING ON RUDDER TAB. REMOVED & REPLACED RUDDER TAB. OK FOR SERVICE.SDR DALA2016112809291Structure · missingFLAME SPRAY MISSING ON RUDDER. REMOVED & REPLACED RUDDER. OK FOR SERVICE.SDR DALA2016080505788Light · brokenSEAT 24E EMERGENCY LIGHT BROKEN. R AND R SEAT 24E LOWER DOOR EMERGENCY LIGHT ASSY IAW AMM 33-50, OPS CKS GOOD.SDR DALA2016062404912Wire · disconnectedCREW REPORTS LOOSE WIRES AT SEAT 35D & 35E. FOUND EMERGENCY PATH LIGHTING WIRING DISCONNECTED AT SEVERAL SPLICES FROM SEAT 32D AND 32E TO 35D AND 35E. REPAIRED WIRING IAW WDM CHP 20 AND REPOSITIONED WIRING IN CHANNEL. ALL EMERGENCY PATH LIGHTS OPERATING FROSDR DALA2016060204323Wire · misinstalledDURING SERVICE CHECK FOUND ROW 24-30 EMERGENCY LIGHTS IN THE AISLE INOPERATIVE. R & R POWER SUPPLY 55-107 IAW MM 33-53-00. NO HELP. REPLACED FUSE FOR POWER SUPPLY B5-212. NO HELP. INSPECTED WIRING FOUND DISCONNECTED WIRE THAT WAS NOT SEATED CORRECTLY IN THE SDR DALA2016051603936Handle · no testTAILCONE FUNCTIONAL IAW AMDS 5350-01077-0101, STEP 11D. FAILED INTERIOR HANDLE PULL TEST 37LBS. SEE NR FOR ADDITIONAL INFORMATION 036-0001:5350-01077-0101/007 00009 REINSTALLED AND TESTED TAIL CONE IAW AMM 53- 53-00, WITHIN LIMITS, 27LBS.SDR DALA2016051603935Release Mech · failedTAILCONE RELEASE MECHANISM CAM FAILED TORQUE CHECK OF AMDS 5350-01077-0101, STEP NR 12. SEE NR FOR ADDITIONAL INFORMATION 036-0001:5350-01077-0101/005 00007. REPLACED IAW AMM 53-53-02, AJUSTED AND TORQUED.SDR DALA2016021901307Door · out of adjustF/A REPORTS LOUD HISSING & SQUEAL IN FLIGHT 1L DOOR. FOUND APPROXIMATELY 2" SPLIT IN LOWER FWD CORNER OF 1L DOOR. ACFT PRESSURIZED TO 4PSI. REMOVED L1 DOOR IAW AMM 52-11. INSTALLED AND ADJUSTED DOOR IAW AMM 52-11-00. SLIDE INSTALLED ON CARD 2561-4964.SDR DALA2015102006260Connector · brokenDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 28DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE IN THE CONNECTOR. THE CONNECTOR WAS REPAIRED AND THE SYSTEM RETURNED TO NORMAL OPERATION.SDR DALA2015042002812Wire · brokenDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT ROW 28 INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE ON THE OTBD SEAT RAIL. THE CONNECTOR WAS REPLACED AND THE WIRE WAS REPAIRED. THE SYSTEM RETURNED TO NORMAL OPERATION.SDR DALA14032520948Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY PATHWAY LIGHTING SYSTEM WOULD NOT TURN OFF WHEN SELECTED TO. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND OPERATIONAL CHECKED GOOD.SDR DALA14001410948Fan · failedCREW NOTED STRONG ELECTRICAL FUMES THROUGHOUT CABIN DURING CRUISE FLIGHT. GALLEY POWER, CABIN LIGHTING, AND CIRCUIT BREAKERS FOR AIR RECIRCULATION FAN WERE ALL SECURED. FUMES THEN DIMINISHED AND THE FLIGHT CONTINUED TO SCHEDULED DESTINATION WITHOUT FURTHER PSDR DALA13044020948Cable · wornMX FOUND THAT THE TAILCONE RELEASE CABLE INNER SHEATH WAS WORN OUT OF ALLOWABLE LIMITS. THE INTERIOR TELEFLEX CABLE WAS REPLACED, ADJUSTED, AND RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FOLLOW-UP CHECK WAS SUCCESSFUL.SDR DALA13044010948Cable · wornMX FOUND THAT THE TAILCONE RELEASE CABLE SHEATH WAS WORN OUT OF ALLOWABLE LIMITS. THE CABLE WAS REPLACED, ADJUSTED, AND RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FOLLOW-UP CHECK WAS SUCCESSFUL.SDR DALA13039430948Connector · disconnectedDURING LINE CHECK, MX FOUND THAT THE SEAT MOUNTED EMERGENCY LIGHTS AT ROW 23 IN THE CABIN WAS INOPERATIVE. MX FOUND A CONNECTOR IN THE WIRE HARNESS AT THE SEAT SIDEWALL UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYS.SDR DALA13024360948Rub Strip · damagedRT FWD LOWER FUSELAGE RUB STRIP STA 820 FOR NR 370, FOUND DEEP PREVIOUS BLENDS. .032" MATERIAL LOSS IS FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1. EXISTING REPAIR FOUND AT 6" AND NEEDS TO BE INCORPORATED WITH NEW REPAIR IAW SRM 53-04, PARA 57 C. (4). FABRICATESDR DALA13023310948Door Frame · corrodedAFT CARGO DOOR FRAME HAS CORROSION AROUND RIVETS & FACE OF DOOR FRAME BS 1155-1212 BETWEEN L28-29. NO DAMAGE NOTED UNDER STRAP, FABRICATED AND INSTALLED STRAP IAW SRM 53-05, FIG 123, OPTION 1, 51-30-05 & 51-10-3.SDR DALA13023290948Door Frame · corrodedCENTER CARGO BAY LOWER DOOR FRAME BS 674 IS CORRODED. FABRICATED AND INSTALLED NEW SPACER AT BS 674 IAW SRM 51-30-05, 53-01, FIG 1-53-05, FIG 123 (OPTION 1), 51-10-3.SDR DALA13023270948Skin · dentedFUSELAGE SKIN BS 256 L17L DENTED. REPAIRED IAW SRM 53-04-3, PG 108, ITEM 8A.SDR DALA13023230948Skin · dentedFUSELAGE SKIN BS 237, L18L DENTED. FABRICATED DOUBLER, INSTALLED REPAIR PARTS IAW SRM 51-30-2, 53-04-5, PARA 4, 53-04-5 FIG 5, 51-10-3 & PSM 900-5-1, NR 4. THIS IS A CLASS 2 REPAIR IAW SRM 53-04-5, FIG 5 INSPECTION REQUIREMENTS IAW 53-04-5, TABLE 2.SDR DALA13023180948Frame · corrodedAFT ACCESSORY COMPARTMENT FRAME AT BS 1380 LOWER RT SIDE SHOWS EVIDENCE OF CORROSION AROUND FASTENERS. REPLACED FRAME WITH FABRICATED IAW SRM 51-30-02, PARA 1, SRM 53-01, PARA 3, SRM 51-20-0, PARA. 4, DWG 9912246-109 & 9912246-121, SRM 51-10-4, PARA 2, SRM 51SDR DALA13023220948Longeron · crackedLONGERON 4L IS CRACKED FROM FASTENER HOLE TO EDGE BS 200. REMOVED, FABRICATED, AND INSTALLED LONGERON REPAIR.SDR DALA13023210948Longeron · crackedLONGERON 3L IS CRACK AT AND THROUGH FASTENER HOLE TO EDGE BS 160. CUT OUT LONGERON 3L, AND REMOVED BETWEEN BS 148 TO 170 IAW SRM 51-30-02 AND 53-02, FIG 18. FABRICATED REPAIR SPLICE AND INSTALLED LONGERON REPAIR IAW SRM 51-30-05, 51-30-02, AND 53-02 FIG 18.SDR DALA13022780948Longeron · crackedLONGERON 2 LT IS CRACKED AT AND THROUGH FASTENER HOLE TO EDGE APPROX STA 160 "MARKED" MRB 53-038-05. REMOVED EXISTING LONGERON 2L REPAIR IAW SRM 51-30-02 AND 53-02 FIG 18, TOTAL 19" REMOVED. INSTALLED REPAIR STA 148 TO 120 IAW SRM 51-30-02, 51-30-05, AND 53-
Back to N948DL, cancelled Aug 22, 2019