N885AA, cancelled Oct 3, 2002

Service difficulty reports · 74

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 = 'N885AA' AND deregistration_id = 'N885AA-2002-10-03'
  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 AALA20011700Light · inoperativeTUL - FOUND VENTRAL STAIRS EMERGENCY LIGHT INOPERATIVE. INSTALLED SERVICEABLE VENTRAL STAIRS EMERGENCY LIGHT PER MM 33-50-061-4 PAGE 403, REPAIRED ON E-58 4012889. (M)Aug 23, 2001 · N885AA · Boeing 727223 · Emergency LightingSDR AALA20011667Web · corrodedTUL - FOUND CORROSION ALONG LINE STATION 1140 FROM APPROX 24 INCHES RBL TO 36 INCHES RBL SEVERAL AREAS. CUTOUT DAMAGED AREA AND INSTALLED WEB REPAIR PER SRM 51-40-2 PAGES 1-6. (M)Aug 19, 2001 · N885AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA20011666Rib · crackedTUL - FOUND STATION 760 RIB CHORD CRACKED BEHIND 760 RIGHT FRAME. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLERS 760 RBL 70.5 IAW SB 727-57-0112 AS EPR CARD 4258 PAGE 2 ITEM 9. (M)Aug 18, 2001 · N885AA · Boeing 727223 · Wing, Rib/BulkheadSDR AALA20011665SkinTUL - FOUND BULGE ABOVE LEFT RAM AIR DOOR MIDWAY ALONG LEFT EDGE OF CUTOUT. REMOVED CORROSION AND INSTALLED .080 17-7 PH DOUBLER PER ESO 11697 DATED 8/15/2001. (M)Aug 17, 2001 · N885AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA20011663Skin · corrodedTUL - FOUND CORROSION UPPER RIGHT HORIZONTAL STAB SKIN T/E BEAM 4 HINGE IN FROM STAB TIP AT ABOUT STAB STATION 115. REPAIRED CORROSION AREA AS PER ESO 11697 DATED 8-16-2001. (M)Aug 16, 2001 · N885AA · Boeing 727223 · Flight Control SystemSDR AALA20011662Beam · corrodedTUL - FOUND CORROSION UPPER RIGHT HORIZONTAL T/E BEAM 3RD ELEVATOR HINGE IN FROM TIP. REPAIRED CORROSION AREA AS PER ESO 11697, 8-16-2001. (M)Aug 16, 2001 · N885AA · Boeing 727223 · Horizontal Stabilizer StructureSDR AALA20011664Skin · corrodedTUL - FOUND LOWER WING LEADING EDGE SKIN CORRODED AFT OF INBOARD FUEL CAP. INSTALLED DOUBLER PER ESO NR 11697 DATED 8-13-2001. (M)Aug 14, 2001 · N885AA · Boeing 727223 · Wing, Plate/SkinSDR AALA20011337Splice · damagedDFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHT AT GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT WIRE SPLICE AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Jul 2, 2001 · N885AA · Boeing 727223 · Light System WiringSDR AALA20010352Light · defectiveDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT MAIN ENTRY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT LEFT SIDE MAIN ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Feb 28, 2001 · N885AA · Boeing 727223 · Emergency LightingSDR AALA20010351Light · inoperativeDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT AFT AIRSTAIR. SYTEM GROUND CHECKED NORMAL OPERATION. (M)Feb 28, 2001 · N885AA · Boeing 727223 · Emergency LightingSDR AALA20010342Light · inoperativeDFW - FOUND DURING OVERNIGHT MAINTENANCE, FLOOR EMERGENCY EXIT LIGHT DIM AT COACH CLASS. REPAIRED EMERGENCY EXIT LIGHT STRIP AT COACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Feb 26, 2001 · N885AA · Boeing 727223 · Emergency LightingSDR AALA20001675Stringer · gougedTUL - FOUND DEEP GOUGE, 1 INCH BY 12 INCHES, IN STRINGER 26L AT STATION 580. REMOVED DAMAGED SECTION OF STRINGER AND REPAIRED USING STRINGER SPLICE PER SRM 53-10-3. (M)Oct 5, 2000 · N885AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA20001633Stringer · corrodedTUL - FOUND STRINGER 27R CORRODED BETWEEN STATION 500-520. REPAIRED STRINGER 27R PER SRM 53-10-3 AND ESO 11697 DATED 10/2/200. FOUND SKIN OUT OF LIMITS. REPAIRED SKIN WITH .100 7075 PLUS 6 DOUBLER PER SRM 53-30-3. (M)Oct 3, 2000 · N885AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA20001631Stringer · splitTUL - FOUND STRINGER 29R IS SPLIT OPEN DUE TO SEVERE CORROSION, 1 INCH BY 3 INCHES, AT STRINGER T-FITTING ATTACHMENT FS 1178 TO 1181. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M)Oct 3, 2000 · N885AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA20001629Structure · crackedTUL - FOUND 2 INCH BY 2 INCHE AREA OF FUSELAGE DENTED/CRACKED BELOW FORWARD LAVATORY SERVICE PANEL STATION 280. INSTALLED REPAIR PER ESO 11697, DATED 29 SEP 00. (M)Oct 2, 2000 · N885AA · Boeing 727223 · Fuselage Main, StructureSDR AALA20001632Stringer · corrodedTUL - FOUND 6 INCH BY 2 INCH AND .100 DEEP AREA OF CORROSION ON STRINGER 29R AT STATION 1010. FABRICATED AND INSTALLED 11 INCH SECTION OF NEW STRINGER WITH NEW FORWARD AND AFT SPLICE AS PER SRM 53-10-3. (M)Sep 27, 2000 · N885AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA20001320Light · inoperativeDFW DURING OVERNIGHT MAINTENANCE AFT STAIR EMERGENCY LIGHT INOPERATIVE. REPLACED AFT STAIR EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.Aug 9, 2000 · N885AA · Boeing 727223 · Emergency LightingSDR AALA20000695Light · inoperativeDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT AT AFT CARGO DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT AT AFT CARGO DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)Apr 24, 2000 · N885AA · Boeing 727223 · Emergency LightingSDR AALA991298Light · failedCCS - FLT 2142 - AFTER TAKEOFF CCS-MIA, FUMES WITH SMELL OF BURNING RUBBER NOTED IN FORWARD AREA OF COACH CABIN. NO VISIBLE SMOKE DETECTED. AIRCRAFT RETURNED TO CCS AND LANDED WITHOUT INCIDENT. SMELL TRACKED TO UPPER FUSELAGE ANTI-COLLISIONS STROBE LIGHT. Aug 29, 1999 · N885AA · Boeing 727223 · Exterior LightingSDR AALA981995Fitting · corrodedTUL - LEFT TRUNNION CORRODED IN BEARING BORE. INSTALLED NEW LEFT TRUNNION FITTING. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Main Landing Gear Attach SectionSDR AALA981994Shear Tie · corrodedTUL - STATION 1166 SHEAR TIE CORRODED AFT SIDE BETWEEN STRINGER 29R-30R. REMOVED AND REPLACED CORRODED SHEAR TIE PER SRM 51-10-6, SRM 51-10-1. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA981993Frame · corrodedTUL - STATION 1166 BELL FRAME SHEAR TIE AFT SIDE OUTBOARD OF STRINGER 29 CORRODED. REMOVED CORROSION PER 51-10-6, TREATED, PRIMED CLEANED AND INSTALLED NEW SHEAR TIE 51-10-1 PAGE 4. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, FrameSDR AALA981992Skin · corrodedTUL - FOUND RIGHT STAB UPPER SKIN HAS CORROSION, ABOVE REAR SPAR AROUND FASTENERS, TOP SURFACE JUST OUTBOARD UPPER SPAR CAP. REMVOED CORROSION AND INSTALLED DOUBLER PER SRM 51-10-1, 2024-T3 .032. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Horizontal Stabilizer, Plate/SkinSDR AALA981991Skin · corrodedTUL - LEFT STABILIZER UPPER SKIN HAS CORROSION TOP SURFACE ABOVE REAR SPAR. INSTALLED DOUBLER PER SRM 51-10-1 2024T3 .032 AFTER CORROSION WAS REMOVED. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Horizontal Stabilizer, Plate/SkinSDR AALA981990Shear Tie · corrodedTUL - FOUND CORROSION ON SHEAR TIE AFT SIDE OF STATION 600, OUTBOARD OF STRINGER 26 LEFT. REMOVED AND REPLACED CORRODED SHEAR TIE, TREATED AND PRIMED AREA PER 51-10-2. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA981989Shear Tie · corrodedTUL - FOUND CORROSION ON SHEAR TIE FORWARD SIDE STATION 600 OUTBOARD, STRINGER 26 LEFT. REPLACED SHEAR TIE, TREATED AND PRIMED AREA PER SRM 51-10-2. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA981988Stringer · corrodedREMOVED CORROSION PER SRM 51-10-6, INSTALLED STRAP PER ESO 11697, DATED 9-15-98. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA981986Stringer · corrodedTUL - STRINGER 27L CORRODED AT STATION 1075 CAUSING 2.5 INCH CRACK IN BELLY SKIN. CUT OUT DAMAGED AREA OF SKIN. REMOVED CORROSION FROM STRINGER 27L PER SRM 51-10-6. INSTALLED DOUBLER ON SKIN PER SRM 53-30-3 FIG 3. INSTALLED 'U' CHANNEL REPAIR ON STRINGER 2Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA981983Frame · gougedTUL - BLENDED OUT GOUGE, HPEC, FLAP PEENED, ALODINE, PRIMED, INSTALLED 17 INCH BY 2 INCH L-ANGLE, 17.7PH STAINLESS STEEL .050 INCH. REPAIRED PER ESO 11697, DATED 9/17/98. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, FrameSDR AALA981982Frame · chafedTUL - WEB OF BELL FRAME DAMAGED, HOLE WORN THROUGH, AFT SIDE STATION 500 ABOVE AND INBOARD OF STRINGER 27R. REMOVED DAMAGED AREA, INSTALLED DOUBLER FROM 2024-T3 .063 INCH ADDED .080 SHIM, WITH 18 FASTENERS, BOLTS. 1875 INCH DIAMETER PER SRM SRM 51-40-2. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, FrameSDR AALA981980Frame · damagedTUL - FOUND STATION 1010 BELL FRAME DAMAGED BELOW STRINGER 25L AND 26L. CUT OUT DAMAGED AREAS AND INSTALLED DOUBLER REPAIRS PER AARD 53-10-7-3 AND SRM 51-40-3, 7075-T6 .071 DOUBLER 4 RIVETS EACH SIDE, DAMAGE 2 ROWS RIVETS INWEB .25 INCH AND .1875 INCH D RIVETOct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, FrameSDR AALA981979Shear Tie · corrodedTUL - STATION 1166 BELL FRAME SHEAR TIE CORRODED AFT SIDE OUTBOARD OF STRINGER 29. REMOVED AND REPLACED CORRODED SHEAR TIE PER SRM 51-10-1 PAGE 4. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA981978Frame · dentedTUL - RIGHT BELL FRAME HAS 3 DENTS STATION 500 BETWEEN STRINGER 24 RT AND 22 RT. INSTALLED DOUBLER ON BELL FRAME PER SRM 51-40-3 FIG 1 PAGE 3, 12 INCH BY .050 DOUBLER 7075-T6 WITH 2 ROWS PAST DAMAGE 1 ROW ON TOP, INSTALLED 27 .1875 MS2047DD RIVETS. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, FrameSDR AALA981975Frame · dentedTUL - BELL FRAME DENTED AND WEB BULGED STAITON 500 BETWEEN STRINGER 24L TO 23L. INSTALLED DOUBLER REPAIR PER ESO 51-40-3 PAGE 3 FIG 1 USING 7075-T6 .063 INCH MATERIAL, 22 UNIVERSAL HEAD 'D' RIVETS .1875 INCH DIAMETER CUTTING OUT 3 INCH OF THE TOP LEG DAMAGED Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, FrameSDR AALA981974Frame · dentedTUL - LEFT BELL FRAME DENTED AND WEB BULGED AT STATION 520 ABOVE STRINGER 24 LEFT. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER .063 INCH 7075-T6 MATERIAL INSTALLED 27 UNIVERSAL HEAD .1875 INCH 'D' RIVETS AND 4 UNIVERSAL HEAD .25 INCH RIVETS PER SRM 51-40-3 PAGOct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, FrameSDR AALA981973Frame · dentedTUL - BELL FRAME DENTED TOP LEG STATION 560 BETWEEN STRINGER 24 LEFT AND 23 LT. INSTALLED DOUBLER .063 INCH 7075-T6 WITH 18 'D' RIVETS .1875 INCH UNIVERSAL HEAD AND 4 'D' RIVETS .25 INCH UNIVERSAL HEAD PER SRM 51-40-3 PAGE 3 FIG 1. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, FrameSDR AALA981972Frame · dentedTUL - FOUND BELL FRAME SPLICE DENTED STATION 600 BETWEEN STRINGER 26 LEFT - 25 RT. INSTALLED 8 INCH DOUBLER 7075 T-6 .063 WITH 20 .1875 MS20470DD RIVETS, 2 ROWS PAST DAMAGE, 1 ROW ON TOP, .75 SPACING PER 51-40-3 FIG 1 PAGE 3. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, FrameSDR AALA981971Frame · dentedTUL - BELL FRAME DENTED STATION 600 ABOVE STRINGER 23 LEFT. INSTALLED 7.5 INCH DOUBLER .063 7075 T-6 WITH 21 .1875 MS20470DD RIVETS, 2 ROWS PAST DAMAGE, 1 ROW ON TOP .75 SPACING PER SRM 51-40-3 FIG 1 PAGE 3. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, FrameSDR AALA981970Frame · dentedTUL - LEFT BELL FRAME DENTED STATION 660 BETWEEN STRINGER 25 LT AND 24 LT. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER FROM 7075-T6 .063 INCH THICK, WITH 15 D RIVETS .1875 DIAMETER AREA 4 D RIVETS .25 INCH DIAMETER UNIVERSAL HEAD PER SRM 51-40-3 PAGE 3 FIG 1.Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, FrameSDR AALA981969Frame · dentedTUL - BELL FRAME DENTED BETWEEN STRINGER 23 LEFT AND 22 LEFT. INSTALLED DOUBLER PER SRM 51-40-3 FIG 1 PAGE 3, 9 INCHES IN LENGTH 2.5 INCHES DEEP, 1 INCH WIDE 22 EACH MS20470DD6 RIVETS AT .780 SPACING 2 ROWS PAST DAMAGE, 1 ROW TOP .063 7075T-6 DOUBLER. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, FrameSDR AALA981968Frame · dentedTUL - RIGHT BELL FRAME DENTED STATION 680 ABOVE STRINGER 24 AND ABOVE STRINGER 23. INSTALLED DOUBLER REPAIR PER SRM 51-40-3, 2.5 INCH WIDE, 1 INCH DEEP, 17 INCH IN LENGTH, TWO ROWS RIVETS ON SIDE, ONE ROW TOP, 46 EACH .1875 RIVETS TOTAL, MS20470 DD6, 2 ROWS POct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, FrameSDR AALA981967Stiffener · crackedTUL - VERTICAL STIFFENER AT STATION 1384 LBL 8 INCHES ABOVE PANEL 5201 AND ABOVE NR 2 ENGINE ANGLE BRACKET HAS CRACK. STOP DRILLED CRACK. INSTALLED STAINLESS 301 HALF HARD ANGLE DOUBLER .080 PER SRM 51-40-4. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA981962Bulkhead · crackedTUL - BULKHEAD 303 AT STRINGER 16L, BELOW DOOR STOP CASTING CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ESO 11697, DATED 10/2/98. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, BulkheadSDR AALA981961Floorbeam · corrodedTUL - TOP OF FLOORBEAM CORRODED OUT OF LIMITS RBL 49 TO RBL 71. REPAIRED 380 FLOORBEAM PER SRM 53-10-08 WITH FILLER ON TOP WHERE CUT OUT AND AN ANGLE ON BOTH SIDES OF FLOORBEAM. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, Floor BeamSDR AALA981960Floorbeam · damagedTUL - REPAIRED 380 FLOORBEAM RBL 7 TO RBL 30 WITH FILLER ON TOP AND ANGLE ON BOTH SIDES PER SRM 53-10-08. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, Floor BeamSDR AALA981959Floorbeam · corrodedTUL - FLOORBEAM UPPER FLANGE CORRODED STATION 400 RBL 21 TO LBL 21. REMOVED CORROSION, INSTALLED FILLER RBL 2 TO 4.5, INSTALLED REPAIR WITH ANGLE ON BOTH SIDES OF FLOORBEAM. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, Floor BeamSDR AALA981958Floorbeam · corrodedTUL - FLOORBEAM CORRODED ON UPPER FLANGE RBL 24 TO RBL 63 AT STATION 480. REPAIRED PER SRM 53-10-8, WITH APPROX 6 INCHES FILLER ON TOP FLANGE WITH ANGLES ON BOTH SIDES OF BEAM. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, Floor BeamSDR AALA981957Floorbeam · corrodedTUL - FOUND UPPER FLANGE OF FLOORBEAM CORRODED. REMOVED AND REPLACED TOP CHORD OF STATION 344 FROM RBL 6 INCHES TO LBL 67 INCHES. DRILLED HOLES ALODINED AND PRIMED PER SRM 51-10-2 AND REINSTALLED TWO WEB STIFFENERS STATION 344 BL 0 AND RBL 8 PER SRM 53-10-8.Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, Floor BeamSDR AALA981956Stringer · crackedTUL - STRINGER 15L CRACKED IN TWO PLACES AT FASTENERS, STATION 720B PLUS 16 INCHES, AFT OF ICE LIGHT. REMOVED DAMAGED AREA OF STRINGER 15L, AFT OF ICE LIGHT STATION 720C. REPAIRED WITH STRINGER SPLICE PER SRM 53-10-3 DETAIL 2. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA981955Stringer · crackedTUL - STRINGER 15R CRACKED AT STATIO N720B PLUS 4 INCH JUST FORWARD OF ICE LIGHT. INSTALLED REPAIR TO STRINGER 15R AT STATION 720B PER SRM 53-10-3 FIGURE 5. (M)Oct 9, 1998 · N885AA · Boeing 727223 · Fuselage Main, Floor Beam
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