N527DA, cancelled Oct 24, 2003

Service difficulty reports · 71

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 = 'N527DA' AND deregistration_id = 'N527DA-2003-10-24'
  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 DL72S011914Battery Pack · dischargedLT O/W FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATT PACK.Dec 9, 2001 · N527DA · Boeing 727232 · Emergency LightingSDR DL72S011770Light · inoperativeRIGHT AFT OVERWING AND LT FWD OVERWING EMERGENCY EXIT LIGHTS INOP ON EXTERIOR OF ACFT. REPLACED LAMPS, RACKS AND BATTERIES. ALL POSITIONS OPERATIONAL EXCEPT LT FORWARD POSITION. RECRIMPED SPLICE 2480 REF WDM 33-51-01. OPS CHECKS GOOD.Nov 7, 2001 · N527DA · Boeing 727232 · Emergency LightingSDR DL72S011007Battery · dischargedEMERGENCY ESCAPE LIGHTS ABOVE AFT STAIRWAY DID NOT COME ON WHEN TESTED. REPLACED BATTERIES IN LIGHT ASSY AND RETESTED, CHECKS NORMAL.Jun 18, 2001 · N527DA · Boeing 727232 · Emergency LightingSDR DL72S010778Beam · crackedTHE RT TORQUE BOX FOR THE AFT VENTRAL STAIRWAY OPENING WAS FOUND WITH A TYPICAL CRACK IN THE UPPER HORIZONTAL BEAM AT FS 1263. THE CRACK IS TYPICAL OF BAC S/B 727-53-0129. THE CRACKED PART WAS REMOVED AND REPLACED WITH A NEW PART PER THE REQUIREMENTS OF THEMay 15, 2001 · N527DA · Boeing 727232 · Fuselage Main, StructureSDR DL72S001983Skin · debondedFROM B-2 LTR CK N/R 63, NR 9 SPOILER PANEL UPPER SURFACE DISBONDED AT FWD I/B CORNER. REPAIRED PER SRM 57-50-6.Oct 11, 2000 · N527DA · Boeing 727232 · SpoilersSDR DL72S001903Warning System · false indicationDISCONTINUED T/O AFTER LEFT BOTTLE DISCHARGE LIGHT CAME ON. VERIFIED BOTH ENG FIRE EXT BOTTLE PRESSURES ALL NORMAL. LIGHT WENT OUT DURING LIGHT TEST. REPLACED LEFT ENGINE FIRE BOTTLE.Sep 29, 2000 · N527DA · Boeing 727232 · Extinguishing SystemSDR DL72S001050Line · damagedEXCESSIVE SMOKE ON LANDING IN CABIN. SUSPECT RT PACK, DURING APU START. REPLACED OIL TANK VENT LINE ON APU.May 29, 2000 · N527DA · Boeing 727232 · Airborne Auxiliary Power Unit (APU) SystemSDR DL72S992451Tire · failedNR 4 MAIN TIRE RECAP CAME APART. DAMAGED RT OUTBOARD GEAR DOOR FLAP ASSY AND FOD NR 3 ENG. REPLACED NR 3 ENGINE. REPLACED FLAP ASSY. REPLACED NR 4 WHEEL.Nov 7, 1999 · N527DA · Boeing 727232 · TireSDR DL72S991893Flap Track · corrodedINBOARD FLAP NR 5 FLAP TRACK AD 90-07-05, AD 90-06-09, CORROSION FOUND AT MLG BEAM ATTACH PAD AND WEAR AT FWD ATTACH LUG FACES. REPAIRED PER ERA 372299-14AD.Aug 20, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S992477Skin · crackedHOLE IN COVE SKIN, 24 FROM I/B FROM I/B END OF FLAP, REPAIRED PER MM 57-52-0 FIG 809.Aug 11, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S991779Skin · gougedTHE FUSELAGE SKIN WAS GOUGED AT FS 990 BETWEEN STRINGERS 24R AND 25R DUE TO GROUND DAMAGE. THE REPAIR WAS ACCOMPLISHED BYERA 333427-14.Aug 6, 1999 · N527DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S991778Skin · crackedTHE FUSELAGE SKIN WAS DAMAGED DUE TO CONTACT WITH THE JETWAY AT FS 380 BETWEEN STRINGERS 17L AND 18L ON 9/13/93 AND A TEMPORARY REPAIR WAS INSTALLED. AT THIS HMV A PERMANENT REPAIR WAS INSTALLED PER ER/A 257628-14.Aug 6, 1999 · N527DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S991777Skin · crackedTHE SKIN ON THE RIGHT SIDE OF THE VERTICAL STABILIZER WAS FOUND CRACKED BETWEEN FS 1203 AND 1211. THIS DAMAGE WAS REPAIRED PER ERA 333422-14.Aug 6, 1999 · N527DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72S991776Shear Tie · crackedTHE FS 1283 FRAME WAS FOUND CRACKED BETWEEN STR 12L AND STR 13L. THIS DAMAGE WAS REPAIRED PER ERA 367856-14.Aug 6, 1999 · N527DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S991775Hinge · wornTHE PIVOT HINGE ON THE REAR SPAR OF THE HORIZONTAL STABILIZER WAS WORN AT RBL 10. THIS DAMAGE WAS REPAIRED PER ER/A 367854-14 AT HMV.Aug 6, 1999 · N527DA · Boeing 727232 · Horizontal Stabilizer StructureSDR DL72S991773Skin · crackedTHE VERTICAL STABILIZER SKIN WAS FOUND CRACKED AT THE FRONT SPAR WHERE THE TORQUE BOX ATTACHES ON THE LEFT HAND SIDE. THE CRACK WAS FOUND AT HMV AND WAS REPAIRED PER ER/A 333420-14.Aug 6, 1999 · N527DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72S991755Skin · crackedDURING HMV INSPECTIONS IT WAS NOTED THAT THE FUSELAGE SKIN WAS CRACKED AT STRINGER 1 BETWEEN FS 1090 AND FS 1110. THIS DAMAGED WAS REPAIRED PER ER/A 333417-14 AND APPROVED BY FAA 8110-3 FORM, DER DESIGNATION DERY-635273-NM.Aug 6, 1999 · N527DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S991676Rib · damagedLWR AFT EXTERNAL SKIN OPENED UP TO FACILITATE REPAIR OF NR 6 RIB. REPAIRED SKIN PER SRM 57-54-0 FIG 801.Jul 25, 1999 · N527DA · Boeing 727232 · Leading Edge DevicesSDR DL72S991674Angle · damagedT ANGLE SUPPORT DAMAGED AT AFT HINGE OF DOOR 3348. REMOVED DAMAGED PORTION OF T ANGLE. BEGAN FABRICATING T ANGLE PER M/M 53-30-1 FIG 804. FABRICATED REPAIR PIECES PER M/M 53-30-1 FIG 804. INSTALLED ANGLE REPAIR PER M/M 53-30-4 FIG 804.Jul 25, 1999 · N527DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S992233Skin · wornLWR L/E SKIN WORN ON I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 803.Jul 24, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S992476Spar · crackedAFT SPAR LWR CAP ANGLE, CRACKED 19 FROM INBD END. REPAIRED PER MM 57-52-0, FIG 802.Jul 19, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S991599Fasteners · missingDURING SHOP INSPECTION, FOUND FASTENERS MISSING. THERE WAS NOT ENOUGH ROOM TO ADD FASTENERS, SO THE SPAR RAIL WAS SPLICED. ON SO 738482, N/R CARD 012493 & 012494.Jul 16, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S992332Angle · crackedDURING SHOP INSPECTION THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED 56 INCHES FROM I/B END OF FLAP. A SECTION OF ANGLE WAS REPLACED AND A DOUBLER INSTALLED PER MM 57-52-0, FIG 802.Jul 15, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S992331Angle · crackedDURING SHOP VISIT, THE AFT LOWER SPAR/CLOSEOUT ANGLE WAS FOUND CRACKED 35 INCHES FROM THE I/B END. A REPLACEMENT SECTION OF ANGLE WAS INSTALLED ALONG WITH A DOUBLER PER MM 57-52-0, FIG 802.Jul 15, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S992330Angle · crackedDURING SHOP VISIT, THE AFT LOWER SPAR/ANGLE WAS FOUND CRACKED 19 INCHES FROM THE I/B END. A REPLACEMENT SECTION OF ANGLE WAS INSTALLED AND A DOUBLER INSTALLED PER MM 57-52-0, FIG 802.Jul 15, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S992289Skin · wornAPPROXIMATELY 3 INCH LONG WEAR AREA, LWR L/E SKIN O/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 803.Jul 14, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S992288Skin · wornLWR L/E SKIN WORN I/B END OF FLAP. REPAIRED OER MM 57-52-0 FIG 803.Jul 14, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S991617Spar · damagedNR 2 MIDFLAP/ UPPER SPAR CHORD / WBL 124.2: ALT FASTENER INSTALLED --- AD 94-07-08. DURING PREVENTATIVE MODIFICATION OF THE UPPER SPAR CHORD PER EO 4-58705-3AD, MTC WAS UNABLE TO INSTALL THE REQUIRED UPPER SPAR CHORD FASTENER COLLAR DUE TO PROXIMITY OF THJul 14, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S991824Skin · wornDURING SHOP VISIT, THE LEADING EDGE SKIN WAS FOUND WORN AT THE I/B END OF THE FLAP. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND FILLER PER 727 MM 57-52-0, FOG 803.Jul 13, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S990927Bracket · crackedNR 8 SLAT ACTUATOR I/B ATTACH BRACKET IS CRACKED. REPAIRED PER M/M 57-20-21 PG 812.Apr 27, 1999 · N527DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S990856Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 57 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND REPAIRED WIApr 17, 1999 · N527DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990855Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 40 CRACKS ALONG THE LENGTH OF THE PANEL. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND REPAApr 17, 1999 · N527DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S982353Megaphone · inopMEGAPHONE INOP. REPLACED MEGAPHONE.Nov 14, 1998 · N527DA · Boeing 727232 · Emergency EquipmentSDR DL72S982192Fitting · corrodedTHE REAR SPAR ATTACHMENT LUG OF THE LT MLG SUPPORT BEAM ATTACH FITTING WAS FOUND WITH CORROSION IN THE LUG HOLE BORE. THE HOLE WAS OVERSIZED TO 1.882 DIA TO REMOVE THE CORROSION AND AN OVERSIZE BUSHING WAS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 3659Oct 22, 1998 · N527DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S982182Support · corrodedWING LT MLG SUPPORT BEAM, OUTBD LUG AND LOWER SURFACE, REPAIR FOR O/S HOLE BORES. THE OUTBD LUG BORE ON THE LT MLG SUPPORT BEAM WAS OVERSIZED AND SPOT FACED TO REMOVE CORROSION. SEVERAL OF THE LOWER SURFACE PANEL ATTACH HOLES WERE ALSO OVERSIZED TO REMOVE Oct 22, 1998 · N527DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S981957Stringer · crackedSTRINGER 8R WAS FOUND WITH A CRACK THROUGH THE INBD FLANGE AT A RIB ATTACH POINT WHICH PROGRESSED TO THE CENTER OF THE STRINGER WEB. THE CRACK WAS REPAIRED WITH TWO ALUMINUM ANGLES PER ER/A 365679-14, REV A.Sep 17, 1998 · N527DA · Boeing 727232 · Vertical StabilizerSDR DL72S981754Strap · out of positionYELLOW BARRIER STRAP CAUGHT HALF WAY OUT L2 DOOR, UNABLE TO RETRACT IN FLIGHT. AIR TURNBACK. REMOVED YELLOW SAFETY STRAP FROM DOOR JAMB.Aug 24, 1998 · N527DA · Boeing 727232 · Service DoorsSDR DL72S980381Support Beam · chaffedFOUND DURING F-1 LETTER CHECK, MLG SIDE BRACE NUT CHAFING MLG SUPPORT BEAM. REPAIRED PER M/M 57-43-0.Feb 13, 1998 · N527DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S971730Actuator · leakingSYSTEM A-HYD FAILURE IN FLT. BOTH A-SYSTEM LOW PRESS LIGHTS CAME ON SIMULTANIOUSLY, FLICKERED THEN STAY ON. REPLACED NR 3 KRUEGER FLAP ACTUATOR FOR LEAKS, SYSTEM OPS CHECKS NORMAL.Sep 4, 1997 · N527DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S972366Spar · crackedCRACKED AFT SPAR RAIL 54 FROM I/B END OF FLAP. REPAIRED ON N/R CARD 02358.Aug 25, 1997 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S972365Spar · bentAFT SPAR RAIL BENT FROM I/B END TO 46 O/B. REPAIRED ON N/R CARD NR 02346.Aug 25, 1997 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S971481Battery Pack · dischargedEMER EXIT LIGHT AFT OF F/C BULKHEAD INOP. REPLACED BATT PACK.Jul 29, 1997 · N527DA · Boeing 727232 · Emergency LightingSDR DL72S971383Stringer · crackedTHE FUSELAGE STR 29R WAS FOUND WITH A CRACK AND CORROSION NEAR STA 950E. THE DAMAGED SECTION OF THE STRINGER HAS BEEN CUT OUT AND REMOVED BETWEEN STA 950D+10 AND 950E+10. A NEW SECTION WAS SPLICED IN AND APPROVED PER FAA/DER FORM 8110-3, DER DESIGNATION SO-8Jul 11, 1997 · N527DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S971284Skin · damagedRIVETS PULLING THROUGH SKIN SEVERAL AREAS. SPLICED SKIN PER SRM 57-50-5, FIG 3.Jul 3, 1997 · N527DA · Boeing 727232 · AileronsSDR DL72S971434Flange · crackedSTA 1010 FRAME UPPER FLANGE, CRACK ABOVE STG 25R. REMOVED DAMAGE PER SRM 53-10-4 FIG 27, FABRICATED REPAIR DOUBLER PER SRM 53-10-4 FIG 27. REPAIRED PER SRM 53-10-4 FIG 27.Jun 27, 1997 · N527DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S971359Frame · dentedFRAME DENTED AFT B/B FS 950 B ABOVE STR 26R. REMOVED DAMAGE PER SRM 53-10-4 FIG 27. DRILLED REPAIR DOUBLER PER SRM 53-10-4 FIG 27. TREATED AND PAINTED FRAME AND DOUBLER PER PS 900-3-6. OK TO INSTALL. INSTALLED DOUBLER PER SRM 53-10-4 FIG 27.Jun 26, 1997 · N527DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S971358Frame · dentedFRAME DENTED AFT B/B FS 950C ABOVE STR 26R. REMOVED DAMAGE AND CHECKED FOR CRACKS PER SRM 53-10-4 PG 110, NO CRACKS FOUND. DRILLED REPAIR PER SRM 53-10-4 FIG 27. TREATED AND PAINTED DOUBLER AND AREA PER PS 900-3-6. OK TO INSTALL. INSTALLED DOUBLER PER SRJun 26, 1997 · N527DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S971357Frame · dentedFRAME DENTED AFT B/B FS 950C FRAME ABOVE STR 26L. REMOVED DAMAGE PER SRM 53-10-4 FIG 27, FABRICATED DOUBLER DRILL HOLES AND ALODINED AND PRIMED IAW SRM 53-10-4 FIG 27. OK TO INSTALL. INSTALLED REPAIR PER SRM 53-10-4 FIG 27.Jun 26, 1997 · N527DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S971356Angle · crackedCRACK STOP DRILLED INSIDE NR 5 SLAT AT OUTBD ACTUATOR ROD END ATTACH ANGLE. FABRICATED DOUBLER PER MM 57-54-0 FIG 804. OK TO INSTALL DOUBLER. INSTALLED REPAIR PER M/M 57-54-1 FIG 804.Jun 26, 1997 · N527DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S962589Bracket · crackedFOUND ON E1 LETTER CK, NR 2 INBD AND OUTBD SLAT ACTUATOR ATTACH BRACKETS CRACKED. REPAIRED PER MM 57-40-0.Nov 25, 1996 · N527DA · Boeing 727232 · Leading Edge Slat Actuator
Back to N527DA, cancelled Oct 24, 2003