N722DH, cancelled Jan 25, 1999
Service difficulty reports · 82
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 = 'N722DH' AND deregistration_id = 'N722DH-1999-01-25' 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 = 'N722DH' AND deregistration_id = 'N722DH-1999-01-25' 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 DHL98722002Trunnion · failedAFTER LANDING, RIGHT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FAILED, CAUSING LANDING GEAR TO SEPARATE FROM THE AIRCRAFT.SDR DHL98722001Pump · failedAFTER TAKEOFF, NR 2 ENGINE FLAMED OUT. DUMPED FUEL, RETURNED FOR LANDING. FORCED TO MAKE GO- AROUND. LANDED AFTER SECOND APPROACH. FOUND FUEL PUMP FAILED.SDR DHL97722006Air Distribution · odorIRRITATING OIL BASED SMELL IN COCKPIT. SUSPECT TO BE FROM F/O SEAT. CLEANED EXCESS SEAT LUBRICANT FROM COCKPIT FLOOR AT F/E AND F/O SEAT PER BMM.SDR DHL97722005Fuel Control · failedNR 1 ENG EPR SPIKED TO 2.5 EPR FOR 1 SECOND DURING TAKEOFF, EPR THEN DECREASED TO APPROX 1.80 EPR ON CLIMB THRUST. ALL ENGINE GAUGES WERE THEN STEADY AT CLIMB THRUST. AFTER CLIMBOUT, THRUST LEVER MOVEMENT WOULD NOT CHANGE THRUST. REMOVED AND REPLACED NSDR DHL97722004Connector · brokenNR 1 ENGINE OIL TEMP 135 TO 140 IN CRUISE, PRESS 46 PSI, 4.2 GAL OIL QUANTITY. FOUND PIN F ON CONNECTOR D356 BROKEN. REPAIRED PER 79-34-01, OPS CHECK OK.SDR DHL97722003Temp Bulb · failedNR 1 ENG OIL TEMP IN YELLOW ON CLIMBOUT. REDUCED THRUST TO MAINTAIN IN LIMITS, ALL OTHER ENG INDICATIONS NORMAL. REMOVED AND REPLACED OIL TEMP BULB, CANNON PLUG TO TEMP BULB, OPS CHECK OK.SDR DHL97722002Skin · crackedFOUND I CRACK IN SKIN AT FWD ENTRY DOOR CUTOUT. C/W EDDY CURRENT INSP, REMOVED RIVETS , ACCOMPLISHED REPAIR PER BOEING S/B 727-53-0198.\SDR DHL97722001Fuel Control · malfunctionedDURING CRUISE, NR 1 ENGINE VIBRATION, WITH ALL ENGINE PARAMETERS NORMAL. INSPECTED ENGINE AND REMOVED AND REPLACED FUEL CONTROL PER MM 73-21-1. PERFORMED ENGINE TRIM AND ENGINE POWER TEST.SDR DHL96722006Engine · vibrationMIDDLE FREQUENCY VIBRATION FELT IN THE NR 1 THRUST LEVER AT ALL POWER SETTINGS ABOVE 1.4 EPR DURING FLIGHT. RETURNED TO DENVER. PERFORMED ENGINE VIBRATION SURVEY ON WING PER MM 72-00 TEST 1, ENGINE WITHIN MANUAL LIMITS. OK FOR CONT SERVICE.SDR DHL96722007Engine · vibrationENGINE NR 1 HAS ABNORMAL VIBRATIONS IN THRUST LEVER AND ENGINE START LEVERS. GROUND RAN NR 1 ENGINE PER JRH 04-02-01, NOT ABNORMAL VIBRATIONS NOTED THROUGHOUT OPERATING RANGE.SDR DHL96722005Csd · reqd serviceGEN NR 2 HAD 2 LIGHT TRIP EN ROUTE NO FAULT, INDICATIONS ON GEN FAULT PANEL. RESIDUAL VOLTS 14 TO 15 VOLTS AND UNSTABLE FREQS UNSTABLE AT 380 TO 382 CPS. FOUND NR 2 CSD OIL QTY LEVEL AT BOTTOM OF OPERATING BAND. SERVICED CSD PER MM 12-13-12, CHECKS NORMAL MSDR DHL9672255CSkin · corrodedAT C-CHECK, NR 5 SLAT UPPER AND LOWER SKIN HAS CORROSION. CUT OUT DAMAGED AREA, INSTALLED EXTERNAL DOUBLER REPAIR PER 57-30-3.SDR DHL9672267CFloor Beam · corrodedAT C-CHECK, FWD CARGO COMPT, LOWER FLANGE OF FLOOR BEAM HAS EXFOLIATED CORROSION AT BS 560, RBL 54. INSTALLED REPAIR PER SRM 53-10-8, 14 BY 2.SDR DHL9672266CStringer · corrodedAT C-CHECK, AFT CARGO COMPT STR 28 LT CORRODED BETWEEN STA 970 AND 990. INSTALLED STRINGER REPAIR PER SRM 53-10-3, 20 LONG.SDR DHL9672256CSeat Track · corrodedAT C-CHECK, SEAT TRACK FLANGE CORRODED AT STA 1032 AND RBL 1. REMOVED AND REPLACED SEAT TRACK FROM STA 1010 TO 1050 PER SRM 53-10-5.SDR DHL9672213CSpacer · crackedAT C-CHECK, NR 2 FLAP TRACK SPACER BLOCK REQUIRES REPAIR. REMOVED AND REPLACED SPACER BLOCK PER S/B 57-125.SDR DHL9672218CFloor Beam · corrodedAT C-CHECK, FOUND HEAVY CORROSION ON TOP FLOOR BEAM CHORD AT STA 400 RBL 4 AND LBL 4. INSTALLED FLOOR BEAM REPAIR AT UPPER CHORD, PER SRM 53-10-8 FROM RBL 4 TO LBL 4.SDR DHL9672265CFitting · crackedAT C-CHECK, WHILE REPLACING 940 FITTING, RT BS 930 FRAME WITH 2 CRACKS BELOW FLOOR LEVEL. REPLACED FRAME FITTING PER S/B 53-130.SDR DHL9672234CRib · crackedAT C-CHECK, LEFT WING RIB AT STA 629.0 HAS A CRACK IN PREVIOUS REPAIR DOUBLER ON LOWER CHORD IN AREA OF STR 6. REMOVED CRACKED REPAIR AT LEFT WING, STOP DRILLED END OF CRACK, INSTALLED REPAIR AT WING RIB PER SRM 57-10-5, 9 BY 4.SDR DHL9672219CFloor Beam · corrodedAT C-CHECK, CABIN FLOOR BEAM HAS CORROSION AT BOTTOM OF UPPER FLANGE BS 1030 RBL 22. CUT OUT DAMAGED SECTION, INSTALLED FLOOR BEAM REPAIR FROM RBL 9 TO RBL 34 PER SRM 53-10-8.SDR DHL9672214CFloor Beam · corrodedAT C-CHECK, CORROSION ON CABIN FLOOR SUPPORT BEAM STA 480 RBL 0 TO RBL 16. CUT OUT DAMAGED AREA, INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8, T-ANGLE 34 INCHES LONG.SDR DHL9672271CFrame · corrosionAT C-CHECK, AFT BAGGAGE COMPT HAS FRAME CORROSION AT STA 950E FLOOR LEVEL AND STR 26R. CUT OUT AREA AND INSTALLED REPAIR PER SRM 51-40-4, 22.5.SDR DHL9672264CFrame · corrodedAT C-CHECK, FOUND CORROSION AFT CARGO NR 2 DOOR FWD CUTOUT FRAME AT BOTTOM ATTACH TO LOWER FRAME. CUT OUT CORRODED AREA OF FRAME FLANGE, INSTALLED REPAIR PER SRM 51-40-4, 22 BY 3.SDR DHL9672238CRib · crackedAT C-CHECK, NR 3 SLAT INBOARD CLOSURE RIB IS CRACKED IN 2 PLACES. REPLACED RIB PER SRM 51-10-1.SDR DHL9672235CRib · crackedAT C-CHECK, LEFT WING RIB AT STA 656.5 CRACKED AT LOWER CHORD AT STR 8 ATTACH BOLT AREA. STOP DRILLED END OF CRACK, INSTALLED WING RIB REPAIR PER SRM 57-10-5, 9 BY 4.SDR DHL9672228CRib · crackedAT C-CHECK, RIGHT WING RIB HAS PREVIOUS REPAIR DOUBLER CRACKED AT LOWER CHORD STA 656.5 AT STR 6. REMOVED REPAIR, REAMED STOP HOLE, CONDUCTED HFEC, INSTALLED REPAIR PER SRM 57-10-5.SDR DHL9672227CRib · crackedAT C-CHECK, RT WING RIB STA 686.5 HAS LOWER CHORD CRACKED AT STR 8. STOP DRILLED, HFEC AND INSTALLED REPAIR PER SRM 57-10-5, 9 BY 4.SDR DHL9672229CRib · crackedAT C-CHECK, RIGHT WING RIB STA 629 CRACKED AT LOWER CHORD IN AREA OF STR 8 ATTACH BOLT. STOP DRILLED, HFEC AND INSTALLED DOUBLER PER SRM 57-10-5, 10.5 BY 3.5.SDR DHL9672236CRib · crackedAT C-CHECK, WING RIB STA 686.5 HAS PREV REPAIR CRACKED AT LOWER CHORD STR 6. REMOVED PREVIOUS REPAIR, INSTALLED NEW REPAIR PER SRM 57-10-5, CHANNEL 8.5 BY 2.5.SDR DHL9672230CRib · crackedAT C-CHECK, WING RIB STA 656.5 CRACKED AT PREVIOUS REPAIR DOUBLER AT STR 6 LOWER CHORD. REMOVED EXISTING REPAIR, INSTALLED WING REPAIR PER SRM 57-10-5, 9 BY 2.25.SDR DHL9672220CFloor Beam · corrodedAT C-CHECK, FOUND CABIN FLOOR BEAM CORRODED AT BS 380 RBL 23. CUT OUT DAMAGED AREA, APPROX 19, INSTALLED REPAIR 24 BY 2.5 PER SRM 53-10-8.SDR DHL9672241CFloor Support · corrodedAT C-CHECK, FLOOR SUPPORT FLANGE AT LBL 20 HAS CORROSION FROM BS 344 TO BS 380. REMOVED AND REPLACED FLOOR SUPPORT FROM BS 344 TO BS 360 AND FROM BS 360 TO BS 380.SDR DHL9672216CSupport · crackedAT C-CHECK, FLOOR SUPPORT FLANGE AT LBL 20 IS CRACKED JUST FWD OF BS 400. INSTALLED NEW FLOOR SUPPORT PER SRM 51-10-1 20.SDR DHL9672215CSeat Track · corrodedAT C-CHECK, FOUND CORROSION ON CABIN SEAT TRACK FLANGE RBL 25 STA 480 TO 520. REMOVED AND REINSTALLED NEW SEAT TRACK PER SRM 51-10-1 FROM STA 480 TO 520.SDR DHL9672203CRib · crackedAT C-CHECK, LEFT WING RIB AT STA 601.5 HAS CRACK IN LOWER CHORD AT STR 6. STOP DRILLED CRACK AND INSTALLED RIB REPAIR PER SRM 57-10-5, 9 INCHES BY 4 INCHES.SDR DHL9672202CRib · crackedAT C-CHECK, LOWER ANGLE CRACKED ON RT WING RIB AT STA 629 AT STR 6. STOP DRILLED CRACK AND INSTALLED RIB REPAIR PER SRM 57-10-5, 9 INCHES BY 4 INCHES.SDR DHL9672272CFloor Beam · corrodedAT C-CHECK, FLOOR BEAM TOP CHORD STA 1130 RBL 24 HAS CORROSION. CUT OUT FLOOR BEAM TOP CHORD, INSTALLED PER SRM 51-40-4. REPAIR USED STRAP 12 BY 1, FILLER 1 BY 1.5 AND L-ANGLE 12 BY 2.5 BY 1 LONG.SDR DHL9672263CSeat Track · corrodedAT C-CHECK, SEAT TRACK FLANGE RBL 24 BETWEEN STA 1010 TO 950B HAS CORROSION. REMOVED AND REPLACED SEAT TRACK FROM STA 955 TO 1020 PER SRM 51-10-1. SEAT TRACK WAS REPLACED BETWEEN STA 950 FRAME PLUS 5 TO STA 1020 AT RBL 24.SDR DHL9672262CSeat Track · corrodedAT C-CHECK, SEAT TRACK FLANGE RBL 46 BETWEEN STA 1070 AND 1030 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK FROM STA 1010 TO 1130 PER SRM 53-10-5.SDR DHL9672244CSeat Track · corrodedAT C-CHECK, SEAT TRACK FLANGE LB 45 STA 1090 TO 1070 CORRODED. REMOVED AND REPLACED SEAT TRACK FROM STA 1060 TO 1130 PER SRM 53-10-5.SDR DHL9672243CSeat Track · corrodedAT C-CHECK, SEAT TRACK FLANGE RBL 53 STA 1130 TO 1070 HAS CORROSION. REPLACED SEAT TRACK PER SRM 51-10-1, 60 LONG.SDR DHL9672223CFloor · corrodedAT C-CHECK, FOUND HEAVY CORROSION ON CABIN FLOOR AT BS 1176 LBL 66. REMOVED CORROSION, INSTALLED NEW CHORD ANGLE LBL 66 TO RBL 66, INSTALLED NEW CHORD ANGLE PER SRM 51-30-2. INSTALLED AFT DOOR THRESHOLD PER SRM 51-30-2.SDR DHL9672222CSeat Track · corrodedAT C-CHECK, SEAT TRACK FLANGE LBL 24 STA 995 HAS CORROSION. CUT OUT SEAT TRACK LBL 24 FROM BS 970 TO BS 1010. INSTALLED SEAT TRACK PER SRM 53-10-1.SDR DHL9672217CWindow Post · crackedAT C-CHECK, X-RAY INSPECTION REVEALED CRACK ON LT SIDE WINDOW POST F TO N. INSTALLED DOUBLER REPAIR PER S/B 53-0086 REV 11.SDR DHL9672206CSkin · corrodedAT C-CHECK, FOUND EXFOLIATION CORROSIION AT STR 20L LAP SEAM, BETWEEN BS 950E AND BS 950F. CUT OUT DAMAGED AREA 4 INCHES BY 2 INCHES 5 INCHES. INSTALLED DOUBLER 11 INCHES BY 7 INCHES AND FILLER 4 INCHES BY 3 INCHES PER SRM 53-30-3.SDR DHL9672270CSkin · tornAT C-CHECK, LOWER RUDDER RT SIDE AT L/E SKIN TORN OFF BELOW PANEL 9507. INSTALLED REPAIR PER SRM 55-40-3, 12 BY 23.25 .SDR DHL9672269CSkin · wornAT C-CHECK, LOWER RUDDER RT SIDE AT L/E FWD SPAR, SKIN WORN THROUGH TO PHENOLIC SUB LAYER JUST BELOW PANL 9507. INSTALLED REPAIR PER SRM 55-40-3, 12 BY 9.SDR DHL9672268CSkin · wornAT C-CHECK, LOWER RUDDER LT SIDE AT FWD SPAR, SKIN WORN THROUGH TO PHENOLOC SUB LAYER MOST OF LENGTH. ACCOMPLISHED RUDDER REPAIR PER SRM 55-40-3. THREE DOUBLERS, 15.5 BY 12.75, 23.375 BY 12.312, 23.375 BY 13.25.SDR DHL9672261CSupport · corrodedAT C-CHECK, CABIN FLOOR SUPPORT CORRODED AT BS 1140 RBL 16 AND BELOW SHEAR WEB AT RBL 23. INSTALLED REPAIR PER SRM 51-40-3 AND PER SRM 51-30-2, 10 BY 25.SDR DHL9672260CFitting · crackedAT C-CHECK, FOUND FRAME FITTING BS 940 RT SIDE CRACKED AT FLOOR LEVEL BEAM ATTACHMENT FLANGE AFT END I/B. ACCOMPLISHED EDDY CURRENT INSP, REPLACED RIGHT SIDE FITTING PER S/B 53-0118 AND DRAWING 65 15732 AND 65C13539.
Back to N722DH, cancelled Jan 25, 1999