N403DA, cancelled Aug 15, 2013

Service difficulty reports · 65

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 = 'N403DA' AND deregistration_id = 'N403DA-2013-08-15'
  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.

SDR DL72S001117Actuator · failedDURING FLIGHT BETWEEN DFW AND SEA AT FLT LEVEL 310, CREW EXPERIENCED AN A-SYSTEM LOW HYDRAULIC PRESSURE LIGHT FLICKERING. CREW THEN NOTICED THE A-SYSTEM QUANTITY INDICATION WAS AT ZERO. DIVERTED TO SLC. WHEN LOWERING FLAPS WITH ALTERNATE SYSTEM, CREW COULD Jun 8, 2000 · N403DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S000905Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC INSPECTION ALONG THE LENGTH OF THE PANEL CONFIRMED A SINGLE CRACK LOCATION BETWEEN FS 360 & 380. THE CRACK WAMay 4, 2000 · N403DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S000555Actuator · leakingLOST A SYSTEM HYD QTY DURING CLIMBOUT. FOUND NUMBER 6 LEADING EDGE FLAP ACTUATOR LEAKING. REPLACED NR 6 LEADING EDGE FLAP ACTUATOR AND A SYS CASE DRAIN AND PRESS FILTERS.Mar 21, 2000 · N403DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72S000537Bulb · failedAFT LT OVERWING EMERGENCY LIGHT INOP. FOUND SEVERAL BULBS INOP. REPLACED BAD BULBS AFT LT OVERWING EMER EXIT SIGN, NOW CHECKS OK. ONLY BULBS INOP WERE ONES THAT LIGHT SIGN AT ALL TIMES.Mar 20, 2000 · N403DA · Boeing 727232 · Emergency LightingSDR DL72S992601Oven · contaminatedFORWARD GALLEY WORK LIGHT C/B POPPED. F/A REPORTED LIGHT PLASTIC SMELL. NO SMOKE NOTED. BREAKER WAS NOT RESET. ON CHECK, FOUND GALLEY WORK LIGHT C/B POPPED AND COLLARED BY PREVIOUS ENG ORDER. CHKD OPS OF OVENS, COFFEEMAKER. ALL ELEC OPERATIONS NORMAL. FONov 25, 1999 · N403DA · Boeing 727232 · Buffet/GalleysSDR DL72S992429Bracket · crackedA .125 INCH CRACK IN NR 2 L/E FLAP ACTUATOR SUPPORT BOX INBD LWR BRACKET. INSTALLED DOUBLER PER M/M 57-20-21.Nov 2, 1999 · N403DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S992428Frame · crackedFOUND ON C2 LETTER CHECK, 1.5 INCH CRACK ON R-1 DOOR FWD FRAME AT THE LOWER STOP CASTING. REPAIRED PER ERA AND MM 52-12-0.Nov 2, 1999 · N403DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990716Frame · crackedFOUND ON C1 LETTER CK, AFT RT ENTRY DOOR FRAME CRACKED. REPAIRED PER SRM 53-10-9.Mar 31, 1999 · N403DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990560Skin · crackedLFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. HFEC INTERNAL INSPECTION CONFIREMD SEVERAL CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE LENGTH OF THE PAMar 10, 1999 · N403DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990549Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 REVEALED A CRACK BETWEEN FS 660 AND 681 IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERNAL INSPECTION OF THE ENTIRE PANEL CONFIRMED THE SINGLE CRACK. THE CRACK WAS ROUTED OUT OMar 9, 1999 · N403DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990548Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERNAL INSPECTION OF THE ENTIRE SKIN PANEL CONFIRMED ONE CRACK BETWEEN FS 400 AND 420. THE CRACK AREA WAS ROUTED OUTMar 9, 1999 · N403DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990356Light · inopON LAYOVER CK, FOUND R-1 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY PER M/M, CKS OK.Feb 22, 1999 · N403DA · Boeing 727232 · Emergency LightingSDR DL72S982389Actuator · failedA-SYS HYD FAILURE ON APPROACH. FOUND THE NR 4 L/E SLAT ACT FAILED. REPLACED SAME.Nov 18, 1998 · N403DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S981781Bulkhead Web · crackedTWO CRACKS OF .75 INCH LENGTH OR LESS WERE FOUND IN THE FS 1183 BULKHEAD WEB AT RBL 18 BETWEEN WL 166 AND 169 AND ONE .375 INCH CRACK WAS FOUND IN THE WEB AT LBL 25, WL 169. THE CRACKS WERE REPAIRED WITH A DOUBLER PER ER/A 365537-14 AND SET UP FOR REPETITIVE Aug 26, 1998 · N403DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S981620Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED IN 21 PLACES AT I/B CUTOUT FOR I/B AFT FLAP DRIVE. THE ANGLE WAS REPAIRED BY STOP DRILLING THE CRACKS AND INSTALLING A DOUBLER PER 727 MM 57-52-0, PG 807.Jun 26, 1998 · N403DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S981183Actuactor · leakingIN CRUISE FLIGHT LEVEL 310 A SYSTEM QTY RAPIDLY DECREASED TO ZERO FOLLOWED BY A SYSTEM PRESSURE DECREASING TO ZERO. WHILE RUNNING POM OUTBOARD FLAPS FAILED TO ALT EXTEND. REPLACED NR 3 LED FLAP ACUTATOR. REPLACED NR 1 AND NR 2 HYD CASE DRAIN FILTERS. LEAK Jun 3, 1998 · N403DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S980406Rib · crackedNR 6 SLAT RIB CRACKED. REPAIRED PER M/M 57-54-0.Feb 19, 1998 · N403DA · Boeing 727232 · Leading Edge DevicesSDR DL72S980243Fitting · mislocatedWHILE PERFORMING A REPAIR TO WING STR 9 PER MM 57-13-0, FIG 802 AT WS656.5 AN EXISTING HOLE ON THE TOP FLANGE OF THE RIB CHORD ASSY FALLS OUT IN THE RADIUS OF THE STRINGER TO RIB ATTACHMENT ANGLE. REWORKED PER ERA 331251-14AD.Jan 29, 1998 · N403DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S980220Frame · crackedTHE 65C20303-13 REPLACEMENT WEB PREVIOUSLY INSTALLED AS PART OF THE 65C20303-25 FRAME REPAIR KIT WAS FOUND CRACKED. THE -25 KIT WAS INSTALLED BY ERA 111762-14, CIRCA 6/86. THE CRACK IS LOCATED AT APPROX WL216. REPAIRED PER ERA 331194-14AD.Jan 26, 1998 · N403DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S980204Skin · damagedFUSELAGE SKIN DAMAGE AT BS 1030 AND S3L OCCURRED. REPAIRED PER ERA 331249-14.Jan 23, 1998 · N403DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S980147Stringer · corrodedSTRINGER 30 WAS CORRODED NEAR FS 990. THE STRINGER WILL BE CUT AT FS 990 AND A REPLACEMENT SECTION SPLICED IN. REPAIR PER ERA331185-14.Jan 19, 1998 · N403DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S980403Skin · crackedDURING SHOP INSPECTION, THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY INSTALLING A REPAIR ANGLE.Dec 31, 1997 · N403DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S980120Angle · damagedTEMPORARY REPAIR STA 1343 BL 0 AFT AIRSTAIR OPENING AFT EDGE LWR SIDE. REMOVED REPAIR, CHORD ANGLE, NR 2 ENG FIREWALL PNL. BEGAN DRILLED NEW CHORD AND SKIN. COMPLETED DRILLING CHORD. OK TO INST CHORD. BEGAN INSTALLING CHORD. FINISHED INSTALLING CHORD. CDec 27, 1997 · N403DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S980189Skin · wornDURING SHOP VISIT INSPECTION, THE MIDFLAP LEADING EDGE WAS FOUND WORN BEYOND SRM LIMITS AT THE IB END OF FLAP. THE LEADING EDGE WAS REPAIRED PER 727 MM 57-52-0 BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER.Dec 23, 1997 · N403DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S980168Rib · crackedITEM: AT HMV2 FOUND R/W STA 656-5 UPPER STRINGER TO RIB ATTACH IS CRACKED LOC 2ND STRINGER FWD OF REAR SPAR. PLUGGED HOLE PER ERA 33125-14AD STOP DRILLED/REPAIR PART PER MM 57-13-0 FABD PART PER ERA.Dec 23, 1997 · N403DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S980109Web · crackedNR 6 L/E SLAT INTERNAL WEB CRACKED ON O/B SIDE OF SLAT TRACK MT FITTING. REPAIRED PER MM 57-40-00.Dec 23, 1997 · N403DA · Boeing 727232 · Leading Edge DevicesSDR DL72S980054Stringer · crackedITEM: LH WING HFEC INSP SHOWS CRACK INDICATION AT UPPER STRINGER-TO-RIB NO. 8 AT W.S. 546.5. CORRECTION: COMPLETED STEPS #1 THRU 4 PER MM 57-13-0 FIG 802. FINISHED DRILLING REPAIR ANGLES PER MM 57-13-0 FIG 802. OK TO INSTALL. BEGAN INSTALLING REPAIR PER MM 57Dec 23, 1997 · N403DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S980052Stringer · crackedRIGHT WING STA 656.6 UPPER STRINGER TO RIB ATTACH IS CRACKED LOC AT FWD VENT BOX AFT LUG. PROVIDED CUTOUT IN VENT STRINGER FOR ACCESS AS PER DETAIL I M/M 57-13-0 PG 806. FORWARD ANGLE IN PLACE, NEED TO DRILL UP TO VENT BOX STRINGER. DRILLED UP FWD AND REPADec 23, 1997 · N403DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S980051Stringer · crackedRT WING HFEC INSP SHOWS CRACK INDICATION AT NO 13 STRINGER-TO-RIB HOLE AT WS 629.0. DRILLED ACCESS HOLE PER M/M 57-13-0. DRILLED REPAIR PARTS PER M/M 57-13-0. OK TO INSTALL. INSTALLED REPAIR PER M/M 57-13-0.Dec 23, 1997 · N403DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S980030Stringer · crackedLEFT WING STA 601.5 UPPER STRINGER TO RIB ATTACH IS CRACKED. FIRST STRINGER FWD OF REAR SPAR. REPAIRED PER MM 57-13-0.Dec 23, 1997 · N403DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S980108Web · crackedWEB CRACKED VERTICAL STAB INTERIOR, WEB CRACKED LT SIDE OF VERTICAL, APPROX STA 1303 ABOVE S-DUCT. REPAIRED PER SRM 53-10-4.Dec 22, 1997 · N403DA · Boeing 727232 · Vertical StabilizerSDR DL72S980107Web · crackedWEB CRACKED VERTICAL STAB INTERIOR, WEB CRACKED RT SIDE OF VERTICAL APPROX STA 1303. REPAIRED PER SRM 53-10-4.Dec 22, 1997 · N403DA · Boeing 727232 · Vertical StabilizerSDR DL72S980053Frame · crackedSTA 930 FRAME AT STR 14 FRAME CRACK AND VERTICAL SKIN STRAP CRACK AT SAME LOCATION. REMOVED FASTENERS AND CUT OUT REPAIR AREA PER SRM 53-10-4 PG 7. ALSO, PERFORMED DYE PENETRANT CHECK PER PS 900-6-3 NR 1. DYE CHECK OK. BEGAN DRILLING REPAIR ANGLES, FINISHDec 22, 1997 · N403DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S980050Web · crackedWEB CRACKED NR 1 SLAT ACTUATOR ATTACH HOUSING WEBS BOTH CRACKED I/B AND O/B SIDE. FABRICATED AND DRILLED I/B REPAIR PER M/M 57-54-0 FIG 804. FABRICATED AND DRILLED UP O/B REPAIR AS PER M/M 57-40-0 FIG 804. OK TO INSTALL. INSTALLED REPAIRS PER M/M 57-54-0 Dec 22, 1997 · N403DA · Boeing 727232 · Leading Edge DevicesSDR DL72S980029Skin · crackedS-DUCT INTERIOR SKIN CRACKED AND BENT UPWARD FROM 10 O'CLOCK TO 1 O'CLOCK POSITION. REMOVED DAMAGED SECTION OF SKIN. FAB REPAIR DOUBLER AND FILLER PER ERA 331180-14. INSTALLED DOUBLER PER ERA 331180. INSTALLED TAPERED SHIM AND CLOSED OUTER SKIN PER ERA 331Dec 22, 1997 · N403DA · Boeing 727232 · Nacelle/Pylon StructureSDR DL72S980056Stringer · crackedSTR 18L, INDICATIONS FOUND 3 EA ON TOP ROW, 2ND HOLE FROM FRONT. ON BOTTOM ROW 1ST AND 3RD HOLE FROM FRONT. REFERENCE SUPPLEMENTAL CARD - ATTACHMENT A OPN 250. CLEANED HOLES. REAMED HOLE IN STRINGER 2ND HOLE FROM FRONT ON BOTTOM TO 542. BEGAN DRILLING REPDec 20, 1997 · N403DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S980055Bracket · crackedBRACKET CRACKED, ACT ATTACH BRACKET NR 3 KRUEGER FLAP OUTBD SIDE. BEGAN MANUFACTURING ANGLE REPAIR DOUBLER AS PER M/M 57-20-21 FIGURE 807. FINISH MFG ANGLE REPAIR DOUBLER PER MM 57-20-21 FIG 807. OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER M/M 57-20-21 FIDec 20, 1997 · N403DA · Boeing 727232 · Leading Edge DevicesSDR DL72S980028Frame · dentedFRAME DENTED FS 1050 BETWEEN STR 25L AND 26L. REMOVED DAMAGE AND DYE-CHECKED PER SRM 53-10-4. NO CRACKS FOUND AROUND CUTOUT. DRILLED UP DOUBLER AS PER SRM 53-10-4 FIG 27. OK TO INSTALL, BEGAN INSTALLING REPAIR. INSTALLED PER SRM 53-10-4.Dec 20, 1997 · N403DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S980027Support · crackedSUPPORTS CRACKED NR 6 L/E FLAP ACTUATOR SUPPORTS ARE CRACKED. VERIFIED CRACKS TO BE PRESENT PER PS 900-6-3. REMOVED CRACKED SUPPORTS FROM A/C. FABRICATED REPAIR PARTS PER M/M 57-20-32 FIG 807. OK TO TREAT AND PAINT TREATED AND PAINTED PER PS 900-3-6 ASSEMDec 20, 1997 · N403DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S972714Frame · dentedFRAME DENTED FS 1030 AT STR 26L. REPAIRED PER SRM 53-10-4 FIG 27.Dec 20, 1997 · N403DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S980026Liner · crackedNR 2 ENG INLET ASSY (DOGHOUSE) ACCOUSTICAL LINER 12 O'CLOCK POS AFT CRACKED AND SEPARATING. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND FILLER AS PER SRM 54-10-3 FIG 13. BEGAN INSTALLATION OF REPAIR PER SRM 54-10-3 FIG 13. COMPLETE REPAIR PER SRM 54-10-3 FDec 19, 1997 · N403DA · Boeing 727232 · Engine Cowling SystemSDR DL72S972621Web · crackedFOUND DURING A-2 LETTER CHECK, .75 INCH CRACK LT LWR TORQUE BOX WEB STA 1227 UPPER EDGE OF VERT WEB. REPAIRED PER M/M 53-11-0.Dec 12, 1997 · N403DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S972620Frame · wornFOUND DURING A-2 LETTER CHECK, ANGLE WORN THROUGH 11 INCHES, 6 O'CLOCK POSITION FS 1352 FRAME. REPAIRED PER ERA 363434.Dec 12, 1997 · N403DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S972619Skin · crackedFOUND DURING A-2 LETTER CHECK, 1.75 INCH CRACK IN RT ELEVATOR UPPER SKIN AT DOUBLER BETWEEN O/B 2 ELEVATOR HINGES. REPAIRED PER ERA 363435-14.Dec 12, 1997 · N403DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S972079Actuator · failedSYS-A HYDRAULIC QTY DECREASED TO ZERO IN FLT. FOUND NR 3L SLAT ACTUATOR FAILED IN RETRACT POSITION. SEALS BLOWN AT ACTUATOR ROD.Oct 16, 1997 · N403DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S971871Tach Gen Housing · leakingOIL TEMP NR 3 STEADILY INCREASED REACHING A MAX OF RED RADIAL. NR 3 OIL QTY STEADILY DECREASED TO APPROX 2 GALLONS. NR 3 OIL PRESSURE DROPPED TO 20 PSI SHUT DOWN ENGINE IAW CHECK LIST. FOUND OIL PUDDLED IN INTAKE. REPLACED N1 TACH GEN HOUSING AND O-RING. Sep 19, 1997 · N403DA · Boeing 727232 · Engine RPM Indicating SystemSDR DL72S971799Battery · dischargedAFT DOOR SLIDE LIGHTS INOP. REPLACED BATT PACK, ALL EMERG LIGHTS NOW OP NORMAL.Sep 14, 1997 · N403DA · Boeing 727232 · Emergency LightingSDR DL72S971111Accessory Unit · failedBOTH PACKS OVERHEATED AND SMOKED CABIN. PACK FAN CONTROL C/B POPPED AND WOULD NOT RESET. REPLACED LANDING GEAR ACCY UNIT.Jun 9, 1997 · N403DA · Boeing 727232 · Landing Gear Position and WarningSDR DL72S962774Spar · crackedDURING INSPECTION, FOUND NR 2 MID FLAP AFT SPAR RAIL CRACKED. THE RAIL WAS REPAIRED PER MM 57-52-0, PG 807.Sep 19, 1996 · N403DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S962773Spar · crackedNR 2 MID FLAP AFT LOWER SPAR RAIL WAS FOUND CRACKED DURING INSPECTION. REPAIRED PER MM 57-52-0, PAGE 807.Sep 19, 1996 · N403DA · Boeing 727232 · Trailing Edge Flaps
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