N703DH, cancelled Jun 11, 2013
Service difficulty reports · 110
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 = 'N703DH' AND deregistration_id = 'N703DH-2013-06-11' 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 = 'N703DH' AND deregistration_id = 'N703DH-2013-06-11' 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 DHL2001703003Switch · faultyUPON FIRST GEAR EXTENSION INTO CVG NOSE GEAR GREEN LIGHT WAS INTERMITTENT. RECYCLED LANDING GEAR AND ALL INDICATIONS NORMAL. REMOVED AND REPLACED NOSE POSITION SWITCH IAW B727 MM 32-61-21, OPS CHECK OK.SDR DHL2001703002Indicator · inoperativeA-SYSTEM HYDRAULIC QUANTITY INDICATOR INOP. PLACED ON DEFERRAL PER DMI 4858. MEL REF 29-14 CAT C.SDR DHL2001703001Skin · corrodedSTRINGER 19 RIGHT AT FS 369 TO FS 400 LAP SEAM HAS BULGING SKIN AROUND SEVERAL FASTENERS. CUT OUT DAMAGED AREA, INSTALLED DOUBLER AND FILLER 12.55 X 7.05 INCH DOUBLER. REWORKED LAP AT STA 360 TO 390 WORK DONE IAW SRM 53-30-3.SDR DHL2000703007Reservoir · lowDURING TAXI WITH FLAPS EXTENDED "A" HYD SYS QUANTITY DECREASED TO 1.9 GALLONS, ON RETURN TAXI QUANTITY INCREASED TO 2.4 GALS WITH FLAPS RETRACTED. C/W A VISUAL INSP OF THE WING FLAP SYS (NO EXTERNAL LEAKS NOTED) FOUND RESERVOIR QUANTITY LOW. SERVICED RESERVSDR DHL2000703006Tire · failedO/B LEFT MAIN TIRE BLOWN. REPLACED LEFT MAIN O/B AND I/B TIRES PER M/M 32-40.SDR DHL2000703005Adc · intermittentINTERMITTENT GYRO FLAG ON CAPTAINS ADI AND FLIGHT DIRECTOR FLAGS ON BOTH CAPTAINS AND F/OS. REMOVED AND REPLACED FLIGHT DIRECTOR COMPUTER.SDR DHL2000703004Gyro · failedINTERMITTENT GYRO FLAG AND FLIGHT DIRECTOR FLAG. REMOVED AND REPLACED VERTICAL GYRO AND FLIGHT INSTRUMENT AMPLIFIER.SDR DHL2000703003Brake · malfunctionedAFTER ROTATION PRIOR TO GEAR RETRACTION THE LEFT I/B AND RIGHT O/B ANTI SKID RELEASE LIGHTS ILLUMINATED. PLACED ANTI SKID SYS ON DMI 2456 PER MEL 32-5. TROUBLESHOT SYS PER M/M 32-42-0, SYS CHKS OK. SWAPPED TRANSDUCERS FOR T/S. TEST OK PER M/M 32-42-0.SDR DHL2000703002Bullet · contaminatedNR 3 ENGINE EPR READS HIGH N1 AND N2 LOW NR 3 THROTTLE 3 & 1/2 BEHIND NR 1 AND NR 2. BLEW DEBRIS FROM NR 3 BULLET. PERFORMED ENGINE RUN. OPS CHECK GOOD.SDR DHLA200070301Stringer · corrodedFOUND LOCALIZED CORROSION AT STATION 650 STRINGER 18R IN LAP JOINT. INSTALLED FLUSH DOUBLER REPAIR ON LAP SEAM AT STR 18 RIGHT FROM BS 615 TO BS 621. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 53-30-3 FIG 15A. MATERIAL USED 7075-T6 0.080 SIZED 14 X 4 INCHESSDR DHL9970334CTrack · crackedAT C CHECK, NR 3 FLAP TRACK MOVABLE FAIRING O/B TRACK CRACKED. REMOVED AND REPLACED TRACK PER SRM 51-30-2, N/R 5107.SDR DHL9970342CHinge Fitting · crackedAT C CHECK, RT TAIL SKID DOOR HINGE FITTING CRACKED. REMOVED AND REPLACED RT TAIL SKID DOOR HINGE FITTING PER SRM 51-30-2, N/R 3198.SDR DHL9970341CHinge Fitting · crackedAT C-CHECK, LEFT TAIL SKID DOOR HINGE FITTING CRACKED. REMOVED AND REPLACED LEFT TAIL SKID DOOR HINGE FITTING AS PER SRM 51-30-2, N/R 3197.SDR DHL9970336CBulkhead Skin · crackedAT C CHECK, CRACK AT BS 1183 BULKHEAD SKIN AFT CARGO COMPT WL 182 LBL 15. REMOVED FASTENERS AND STOP DRILLED CRACK PER SRM 51-30-2, AND 51-10-1 PG NR 7. PERFOMRED HFEC INSPECT. NO CRACK IND PAST STOP DRILLS. CUT OUT DAMAGED AREA PER SB 727-53-0175. REMOVESDR DHL9970335CBulkhead Skin · crackedC-CK, CRACK BS 1183 BULKHEAD SKIN, AFT BAG COMPT WL 182 RBL 15. OVERSIZED HOLE BY .015625 TO REMOVE INDAT WL190 RBL 15.5 AND ACCOMP PER SRM 51-10-1, VERIFIED CRACK NOT VISIBLE NDT PROCEDURE HFEC B727, PER NDT MANUAL PART 6510000 FIG 4. NO CRACK IND. DRILLEDSDR DHL9970348CBulkhead · damagedAT C CHECK, REPLACED TEMP REPAIR WITH PERMANENT REPAIR BS 870 BULKHEAD WEB. REF: AVITAS ENG LETTER 98 PMS 1.213D-1. REMOVED TEMPORARY REPAIR AT BS 870. REMOVED OLD PRIMER AND PRC AROUND DAMAGED AREA. PERFORMED HFEC INSP OF STOP DRILL AT BS 870 AND WEB IAW NSDR DHL9970347CSkin · damagedAT C CHECK, LT INBD HORIZONTAL STABILIZER LEADING EDGE DAMAGED. REMOVED LEADING EDGE FOR APPROX STA 20 LE TO LE STA 147.32 PER SRM 51-30-2. REMOVED RIBS TO AID IN MAINTAINING CONTOUR OF LEADING EDGE IAW SRM 51-30-2. CUT OUT DAMAGED AREA AT LT LEADING I/B HOSDR DHL9970344CAngle · crackedC-CK, LT WING BS 930 LBL 64 VERT ANG CRACKED. R & R FITTING AT LT STA 930 LBL 64, ALOD & PRIM. INSTALL SPLICES STA 920 STR 15/16 RT. INSTALL REPAIR STR 14 & SUB FLOOR WEBS STA 930-940 & 920-930. REPLACED FLOOR PANEL, INSTALL LT W/W EMERG GEAR EXTEN AND FASSDR DHL9970328CBolts · crackedAT C CHECK, 2 EA SLAT ROLLER BOLTS CRACKED AT LUBE HOLE AND 6 EA SLAT ROLLER BOLTS WORN. REPLACED PER MM 27-81-11, N/R 2074.SDR DHL9970329CSkin · crackedAT C CHECK, RT WING FIXED LEADING EDGE CUT OUT FOR THE NR 5 SLAT INBD TRACK IS CRACKED. REMOVED SEALS TO GAIN ACCESS TO BACKSIDE OF LEAD EDGE OF WING PER SRM 57-30-4, MADE EXTERNAL DOUBLER PICKED UP EXISTING HOLES 2 EA NEW HLOES ONTO NEW DOUBLER PER SRM 57-30SDR DHL9970330CHinge · crackedAT C CHECK, LW NR 7 SPOILER PANEL CENTER HINGE CASTING OUTBOARD LEG CRACKED AT AFT HOLE. CUT OUT CRACK FROM HINGE CASTING 2 LONG PER SRM 51-10-1, DYE PENETRANT INSPECTED CUTOUT PER MIL 68-66B. NO CRACK NOTED, INSTALLED FILLER AND REINFORCING STRAP AT LEFT WISDR DHL9970317CTail Cone · delaminatedAT C CHECK, TAIL CONE HAS DELAMINATION AT LEFT TOP AREA. REMOVED VERTICAL STABILIZER TAILCONE PER SRM 51-30-2. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8 FIG 1, USED RESIN 50-A AND CLOTH STYLE 720 10 INCH BY 6 INCH, PRIMED ALL REAS PER SRM 51-10-2.SDR DHL9970345CDoor · corrodedAT C CHECK, GALLEY DOOR UPPER FLAP HINGE HAS CORROSION. REMOVED GALLEY DOOR UPPPER FLAP PER MM 20-10-1. INSTALLED GALLEY DOOR UPPER FLAP (GATE ASSY) PER MM 52-12-0. REMOVED AND REPLACED PIN STOP ON GALLEY DOOR UPPER FLAP PER 52-12-0. SEALED OUTSIDE OF DOORSDR DHL9970332CBulkhead Panel · crushedAT C CHECK, RT BS 1183 BULKHEAD PANEL IS CRUSHED AT LOWER END. REPLACED RT STA 1183 BLKHD PANEL PER 53-20-11 MATERIAL USED P/N AE4155-81162, APPROXIMATELY 7X4N/R 5118.SDR DHL9970331CMount · crackedAT C CHECK, ENGINE NR 1 GEARBOX FWD MOUNT CRACKED. REMOVED G/B PER MM-72-00, INSTALLED O/H G/B PER MM-72-0. INSTALLED FUEL LINE FROM FUEL OIL COOLER PER MM 28-40-3, LEAK CHECK, NO LEAK FOUND. OPS CHECKED ENGINE RUN AND TRIM, N/R 6179.SDR DHL9970325CLongeron · crackedAT C CHECK, NR 1 LOWER COWL OUTBOARD LONGERON IS CRACKED UNDER RUB PLATE BY NR 3 LATCH V-BOLT CUTOUT. ALSO, SKIN IS BENT AND CRACKED AROUND CUTOUT. REWORKED SKIN AT NR 1 ENG LOWER COWL NR 3 LATCH U-BOLT CUT OUT PER SRM 51-10-1. NO SIGNIFICANT MATERIAL LOSSSDR DHL9970320CSkin · corrodedAT CHECK, RT WING UPPER SURFACE SKIN BULGES ALONG ROW OF FASTENERS JUST FWD OF THE NR 8 SPOILER PANEL. REMOVED PANEL FOR REAIR, CLEANED MATING SURFACE ON WING, NO CORROSION NOTED, TREATED AND PRIMED AREA PER SRM 51-10-2. INSTALLED BONDED REPAIR AT R/WING UPPSDR DHL9970319CBracket · crackedAT C CHECK, FWD CARGO DOOR UPLOCK SUPPORT BRACKET IS CRACKED. REMOVED FWD CARGO DOOR UP LOCK SUPPORT BRACKET PER SRM 51-30-2. REPLACED FWD CARGO DOOR UPLOCK SUPPORT BRACKET PER SRM 51-30-2 AND 51-40-2, MATERIAL USED 2024T3 .040 6 BY 3, ALODINED AND PRIMED PESDR DHL9970318CStructure · crackedAT C CHECK, FWD ENTRY DOOR INTERIOR FWD UPPER CORNER IS CRACKED. REMOVED INTERIOR FWD ENTRY DOOR PER SRM 51-30-2, FABRICATED NEW LINER SUPPORT FWD CORNER PER SRM 52-10-1 FIG 1 USED .050 2024-0 HEAT TREATED TO 2024T3 PER 99PMSI 247 PG-01. ALODINED AND PRIMED PSDR DHL9970316CFairing · delaminatedAT C CHECK, V STABILIZER HAS FAIRING DELAMINATED ON BOTH SIDES BELOW TAIL CONE. INSTALLED BONDING REPAIR AT VERTICAL STABILIZER FAIRINGS BELOW TAIL CONE PER SRM 51-20-3 FIG 1, MATERIAL USED EPOCAST 1652 A/B, N/R 4127.SDR DHL9970314CCowl · chaffAT C CHECK, NR 1 TOP COWL OUTBOARD LONGERON HAS DEEP CHAFED SPOTS AT 46 AND 54 INCHES FROM AFT EDGE. REPLACED COLGERON SECTION PER SRM 51-40-2 AND 54-10-2 ON NR 1 TOP COWL, USED 2024T3 .050 20 BY 4, TREATED AND PRIMED AREA PER SRM 51-10-2, N/R 6206.SDR DHL9970313CSkin · chafedAT C CHECK, ENGINE NR 2 FWD RT COWL LOWER FWD INSIDE CORNER DOUBLER CHAFFED THROUGH. REMOVED FASTENER AND DAMAGED DOUBLER PER SRM 51-30-2, CLEANED AND PRIMED ARE PER SRM 51-10-2. REPLACED DOUBLER PER SRM 51-30-2 USED .040 14 BY 5 2024-0 HEAT TREATED TO 2024TSDR DHL9970310CDepressor · damagedAT C CHECK, SEAL DEPRESSOR AT MCD AFT OF NR 6 LATCH HAS A SQUARE .25 OF MATERIAL MISSING REQUIRES REPAIR. SMOOTHED DAMAGED SECTION PER SRM 51-40-1. ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED L ANGLE REPAIR PER SRM 51-40-3 FIG 1 USING .063 2024-0 HEAT TSDR DHL9970308CPanel · crackedAT C CHECK, V STAB ACCESS PANEL NR 9774 HAS REPAIRS CRACKING UP L/S. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8 FIG 1 USING RESIN 1304, 6 INCH BY 4 INCH, N/R 4128.SDR DHL9970305CFairing · corrodedAT C CHECK, LEFT WING NR 1 MOVABLE FAIRING SKIN CORRODED AT FWD I/B SIDE AT FAIRING ATTACH POINT. REMOVED PAINT FROM SKIN CORRODED AREA PER MM 51-20-0, CUT 6 INCH BY 5 INCH SECTION OF SKIN AWAY AND INSTALLED REPAIR SKIN AND SPLICE PLATE PER SRM 53-50-1 FIG 1 SDR DHL9970340CCarriage · looseLS NR 4 FLAP CARRIAGE HAS THRUST NUT LOOSE, IT HAS EXCESS CLEARANCE BETWEEN SHIMS AND FLAP FITTING. REMOVED LEFT INBOARD FLAP ASSY PER MM 27-51-3. FOUND LEFT INBOARD THRUST BEARING CASTING OUT OF LIMITS PER MM 27-51-3. REMOVED CARRIAGES FROM OLD FLAP AND TRSDR DHL9970339CAngle · crackedAT C-CHECK, LEFT WING LEADING EDGE CAVITY AREA FSS 115.0 VERTICAL ANGLE CRACKED LOSER SECTION. CUTOUT DAMAGED SECTION 3 BY 2 PER SRM 51-40-3. FABRICATED NEW VERTICAL ANGLE PER SRM 51-40-3 FIGURE 1, MATERIAL USED 7075-0 .071 3 BY 8, .375 INCH, HEAT TREATED 7SDR DHL9970327CSkin · damagedAT C CHECK, LW TOP SKIN PANEL HAS FIBERGLASS REPAIR NOT FINISHED BETWEEN WING AND FUSELAGE. REMOVED LW TOP SKIN PANEL LOCATED BETWEEN WING AND FUSELAGE PER SRM 51-30-2. INSTALLED BONDED REPAIR AT LW TOP PANEL PER SRM 51-40-6 FIG 1 MAT USED 2024 T3 .020 , 202SDR DHL9970326CStiffener · crackedAT C CHECK, LW VERT STIFFENER IS CRACKED AT LOWER END AT FALSE SPAR BELOW NR 5 SPOILER O/B SIDE. STOP DRILLED 1 CRACK PER SRM 57-50-6. REMOVED APPROX 6 OF FASTENERS PER SRM 57-50-6, MADE NEW L ANGLE DOUBLER PER SRM 57-50-6. PICKED UP EXISTING FASTENER HOLESDR DHL9970323CBolt · shearedAT C CHECK, LT WING NR 3 LE SLAT ACTUATOR TIE DOWN BOLT IB LOWER BOLT SHEARED. REPLACE THE IB LOWER BOLT ON NR 3 LE SLAT ACTUATOR PER MM 20-80-1, N/R 1199.SDR DHL9970322CSkin · corrodedAT C CHECK, RT WING INBOARD FORE FLAP HAS SURFACE CORROSION ON LOWER SKIN APPROXIMATELY 12 FROM OUTBD END. REMOVED CORROSION AT RT WING PER SRM 51-10-6, OUT OF LIMITS PER SRM 57-50-1 FIG 3 DETAIL 3. INSTALLED FG OVERLAY REPAIR PER SRM 51-40-8 FIG 1 ON RT WINSDR DHL9970321CSkin · delaminatedAT C CHECK, RT WING UPPER SURFACE SKIN BULGES ALONG PANEL 10 FORWARD OF NR 9 AND NR 10 SPOILER PANEL. REMOVED FASTENERS AT RT WING PANEL PER SRM 51-30-2. FOUND DELAMINATED SKIN IN UPPER PANEL, CLEANED MATING SURFACE ON AIRCRAFT TRATED AND PRIMED. NO CORROSISDR DHL9970315CPlate · crackedAT C CHECK, MAIN CARGO DOOR INTERIOR LOWER PLATE COVER FWD TO AFT SECTION HAS SEVERAL CRACKS AND DENTS ON SURFACE. REMOVED PLATE AT MAIN CARGO DOOR INTERIOR LOWER PLATE COVER REPAIRED PER SRM 51-30-2 AND 51-10-1. ALODINED AND PRIMED PER SRM 51-10-2 USED 2024SDR DHL9970312CLongitudinal · crackedAT C CHECK, E3 ELECTRONIC RACK UPPER RT LONGITUDINAL IS CRACKED 2 PLACES. STOP DRILLED CRACKS PER SRM 51-10-1 2 PLACES. INSTALLED DOUBLER PER SRM 51-40-2 FIG 1 USING 2024T3 .050 6 BY 4 2 EA, ALODINED AND PRIMED PER SRM 51-10-2, N/R 3126.SDR DHL9970309CFloor · crackedAT C CHECK, NOSE W/W PRESS FLOW HAS CRACK AT BS 284.5. REMOVED FLOOR PANEL AT FWD PER SRM 51-30-2. REMOVED 2 EACH OLD DOUBLERS PER SRM 51-30-2. CUT OUT DAMAGED AREA AT BS 284.5 4 BY 1 PER S/B 53-0145, HFEC INSPECTED CUTOUT IAW 51-00-0 FIG 4. NO CRACKS NOTESDR DHL9970307CAngle · crackedAT C CHECK, RT WING TRAILING EDGE COVER PANEL INBOARD SUPPORT ANGLE IS CRACKED AT WS 447.90 JUST INBOARD OF NR 11 SPOILER ACTUATOR. REMOVED AND REPLACED SUPPORT ANGLE AT RT WING AT WS 447.90 PER SRM 51-10-1 PAR 4 AND 51-30-2, N/R 2044.SDR DHL9970302CAngle · crackedAT C CHECK, RT WING TRAILING EDGE COVE PANEL OUTBOARD SUPPORT ANGLE IS CRACKED AT WS 498.08 INBOARD OF THE NR 12 SPOILER ACTUATOR. REPLACED COVER PANEL OUTBRD SUPPORT WS 498.08 PER SRM 51-30-2, 51-10-1 PAR 4 N/R 2045.SDR DHL9970301CCircumferential · crackedAT C CHECK, FWD CARGO COMPT, CRACK AT CIRCUMFERENTIAL STA 640 STRINGER 26L. REMOVED OLD REPAIR, STOP DRILLED CRACK, HFEC. INSTALLED REPAIR PARTS PER SRM 53-10-4, 12 BY 6, N/R 3121.SDR DHL9970338CBulkhead · crackedAT C-CHECK, CRACK AT 1183 BULKHEAD SKIN AFT CARGO COMPT WL 172 RBL 8. REMOVED FASTENERS AND STOP DRILL CRACK AT 1183 BLKD WL 172 RBL 8. PERFORMED HFEC INSPECTION PER NDT MANUAL PART 6 51-00-00 FIG 4. NO CRACK IND PAST STOP DRILLS, CUT OUT DAMAGED AREA PER SSDR DHL9970311CReceptacle · crackedAT C CHECK, BARRIER NET ATTACH RECEPTACLE AT BS 364 BETWEEN STRINGERS 5L AND 6L UPPER MOUNT BRACKET MISSING ATTACH RIVET AND CRACKED. REMOVED BRACKET SUPPORT PER SRM 51-30-2. REPLACED BRACKET SUPPORT PER SRM 51-30-2 USED 7075T0 .071 AND 2024T3 .050, ALODINED
Back to N703DH, cancelled Jun 11, 2013