N890AA

Service difficulty reports not matched to an aircraft · 69

They name N890AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N890AA' AND registry_match IS NULL
  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 AALA20011677Light · inoperativeDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING IN AFT STAIRWELL INOPERATIVE. REPLACED AFT STAIRWELL LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Aug 21, 2001 · N890AA · Boeing 727223 · Emergency LightingSDR AALA20011593Light · inoperativeDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING IN AFT STAIRWELL INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Aug 5, 2001 · N890AA · Boeing 727223 · Emergency LightingSDR AALA20011007Valve · failedBNA - FLT 1216 - EN ROUTE DFW-PHL, AIR INTERRUPTED BNA, AFTER NR 3 ENGINE FLAME OUT AND NO FUEL TRANSFER FROM NR 2 TANK. REPLACED NR 2 CROSSOVER FEED VALVE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)May 14, 2001 · N890AA · Boeing 727223 · Fuel Transfer ValveSDR AALA20010988Rib · crackedTUL - FOUND DURING SCHEDULED C-CHECK INSPECTION, A CRACK WAS FOUND IN THE LBL 70.5 UPPER RIB CHORD AT BS 760. INSTALLED THE PREVENTATIVE MODIFICATION 65C33202-99 PER BOEING 727 SB 727-57-0112 WITH DEVIATION PER ESO 11697 DATED 5-9-2001. (M)May 13, 2001 · N890AA · Boeing 727223 · Wing, Rib/BulkheadSDR AALA20010847Skin · crackedTUL - FOUND FORWARD ENTRY DOOR LOWER HINGE CUTOUT SKIN CRACKED, FS 303. TRIMMED OUT CRACK, INSTALLED DOUBLER IAW SB 727-53-0198 FIG 4. (M)Apr 19, 2001 · N890AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA20010846Skin · crackedTUL - FOUND FORWARD ENTRY DOOR UPPER HINGE CUTOUT CRACKED. INSTALLED DOUBLER IAW SB 727-53-0198 FIG 4, TRIMMED OUT CRACK. (M)Apr 18, 2001 · N890AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA20010845Beam · corrodedTUL - FOUND LEFT HORIZONTAL T/E BEAM CORRODED AT OUTBOARD END. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697 DATED 4/17/01. (M)Apr 18, 2001 · N890AA · Boeing 727223 · Horizontal Stabilizer StructureSDR AALA20010844Stiffener · crackedTUL - FOUND AFT BULKHEAD 1183 RIGHT BL 9 VERTICAL STIFFENER HAS CRACK UNDER OUTBOARD TOWER RADIUS BLOCK. STOP DRILLED CRACK AND INSTALLED REPAIR AS PER SB 727-53-0175. (M)Apr 18, 2001 · N890AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA20010848Skin · gougedTUL - FOUND 1.5 INCH BY .125 INCH GOUGE LOCATION NEAR RIGHT NLG DOOR. DAMAGE IS APPROX 12 INCHES AFT AND 18 INCHES ABOVE AFT AND OF RIGHT NLG DOOR. REMOVED AREA DAMAGED AND INSTALLED DOUBLER JUST AFT AND ABOVE AFT RIGHT NLG DOOR PER SRM 53-30-3 PAGE 13 PART Apr 17, 2001 · N890AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA2000562Channel · damagedTUL - FOUND ELONGATED HOLE IN VERTICAL CHANNEL AT OUTBOARD HINGE OF NR 2 SPOILER. REMOVED VERTICAL CHANNEL AND INSTALLED NEW PART USING FIRST OVERSIZE HI-LOCKS SRM 51-10-1 PAGE 4. (M)Mar 28, 2000 · N890AA · Boeing 727223 · SpoilersSDR AALA20000227Light · inoperativeDFW - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD CENTER CEILING INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT FORWARD CENTER CEILING. SYSTEM GROUND CHECK NORMAL OPERATION. (M)Feb 6, 2000 · N890AA · Boeing 727223 · Emergency LightingSDR AALA20000224Light · inoperativeDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IN AFT AIRSTAIR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)Feb 3, 2000 · N890AA · Boeing 727223 · Emergency LightingSDR AALA991290Connector · defectiveDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 17D, 20D, AND 24D INOPERATIVE. REPLACED CONNECTORS TO EMERGENCY EXIT FLOOR PATH LIGHTS STRIPS AT SEATS 17D, 20D, AND 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Aug 27, 1999 · N890AA · Boeing 727223 · Emergency LightingSDR AALA990590Beam · corrodedTUL - FOUND CORROSION ON LIGHTENING HOLE ON BOTTOM OF DELTA BEAM AT STATION 786 TO 790. REPAIRED WITH DOUBLER IAW SRM 51-40-2 AND 51-20-0. (M)Apr 20, 1999 · N890AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA990584Frame · corrodedTUL - FOUND OUTBOARD SIDE STRINGER 26R AFT SIDE 620 FRAME LOWER CHORD ANGLE CORRODED. REPAIRED CHORD ANGLE PER SRM 51-40-3. (M)Apr 20, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990565Skin · corrodedTUL - FOUND CORROSION AROUND INNER SKIN AROUND ICE LIGHT HOUSING LANDING AT BS 720B-720C AND STRINGER 14L-16L. REPAIRED PER SRM 53-30-3 AREA AROUND ICE LIGHT HOUSING, AND ESO 11697 (PAN HEAD HI-LOCKS) 2 EACH, 4-9-99. (M)Apr 20, 1999 · N890AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA990606Stringer · crackedTUL - REF E58 NR 3150893, STRINGER 15L CRACKED AT BS 720B PLUS 15 INCHES AT AFT EDGE OF ICE LIGHT HOUSING. REPAIR STRINGER 15L BS 720B PLUS 15 INCHES AT AFT EDGE OF ICE LIGHT PER SRM 53-10-3. (M)Apr 19, 1999 · N890AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA990566Spar · corrodedTUL - FOUND LEFT HORIZ STAB REAR SPAR CHORD UPPER END HAS 1 INCH AREA OF CORROSION BETWEEN NR 6 AND NR 7 ELEV HINGE BEARING. REPAIRED AREA OF CORROSION REMOVAL PER ESO 11697, DATED 3/30/99. (M)Apr 19, 1999 · N890AA · Boeing 727223 · Horizontal Stabilizer, Spar/RibSDR AALA990594Frame · dentedTUL - FOUND BELL FRAME FLANGE DENTED STATION 1110, STRINGER 27 AND 25R. INSTALLED DOUBLER PER SRM 51-40-3. (M)Apr 16, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990596Angle · corrodedTUL - FOUND OUTBOARD SIDE STRINGER 26R AFT SIDE 620 FRAME LOWER CHORD ANGLE CORRODED. REPAIRED CHORD ANGLE PER SRM 51-40-3 DOUBLER 17-7 MATERIAL .063 THICK 2.5 INCH BY 2.5 INCH BY 15 INCH WITH BAC30FQ6 FASTENERS AND 44 BACC30MB COLLARS. (M)Apr 15, 1999 · N890AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA990574Strap · corrodedTUL - FOUD STRINGER 614-619 ABOVE STRINGER 26R UPPER CHORD ANGLE LOWER TAPERED STRAP DOUBLER CORRODED AROUND 3 NUT PLATES. REMOVED AND REPLACED TAPERED STRAP. (M)Apr 14, 1999 · N890AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA990593Frame · bentTUL - FOUND STATION 1030 BELL FRAME BENT (FLANGE/WEB) STRINGER 26-25 LEFT. REMOVED DAMGED SECTIONS, 1 INCH BY 2.8125 INCH BY 1 INCH BY 1.3125 INCH FROM BELL FRAME FLANGE, DYE CHECKED FOR CRACKS, NONE FOUND. INSTALLED DOUBLER PER SRM 51-40-3. (M)Apr 13, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990573Floorbeam · corrodedTUL - FOUND CORROSION AT FASTENER HOLES FOR CEILIG PANEL ATTACHMENT. REMOVED CORROSION AND REPAIRED PER ESO 11697 DATED 4-9-99 USING 7075T6 .080 1 INCY BY 16.5 INCH OAL. (M)Apr 12, 1999 · N890AA · Boeing 727223 · Fuselage Main, Floor BeamSDR AALA990599Spar · corrodedTUL - RIGHT WING FSS 213-216 LOWER CHORD ANGEL LOWER LEFT HAS EXFOLIATING CORROSION, UPPER SURFACE AROUND AND UNDER STRUT ROD MOUNT BRACKET. REMOVED AND BLENDED CORROSION PER SRM 57-10-1. REPAIRED PER AARD 57-30-00-2. (M)Apr 9, 1999 · N890AA · Boeing 727223 · Wing SparSDR AALA990611Frame · bentFOUND BELL FRAME BENT IN WEB STATION 1130, STRINGER 26R TO STRINGER 25R. CUT OUT DAMGED AREA AND INSTALLED DOUBLER REPAIR PER 51-40-5 (AARD 53-10-07-3). (M)Apr 8, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990592Frame · bentTUL - FOUND BELL FRAME BENT FLANGE AND WEB STATION 1030 STRINGER 26R TO STRINGER 25R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLERS PER SRM 51-40-3. (M)Apr 8, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990591Splice · crackedTUL - FOUND BELL FRAME (SPLICE) STRAP CRACKED STATION 1030 BETWEEN STRINGER 24L AND 25L. REPLACED (SPLICE) STRAP PER 51-10-1. (M)Apr 7, 1999 · N890AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA990572Shear Tie · corrodedTUL - FOUND CORROSION ON SHEAR TIE AFT OF FS 1130 AT STRINGER 29 LEFT. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE USING ORIGINAL FASTENER LOCATIONS. FASTENER THROUGH FRAME .1875 HI-LOCKS. FASTENERS THROUGH SKIN ORIGINAL SIZE ADN TYPE REF 51-10-1Apr 7, 1999 · N890AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA990571Shear Tie · corrodedTUL - FOUND CORROSION ON SHEAR TIE AFT SIDE FS 1130, STRINGER 28 LEFT OUTBOARD. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE USING ORIG FASTENER LOCATIONS. FASTENERS THROUGH FRAME .1875 INCH HI-LOCKS. FASTENERS THROUGH SKIN RIVET ORIGINAL SIZE ANDApr 7, 1999 · N890AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA990570Shear Tie · corrodedTUL - FOUND CORROSION ON SHEAR TIE FS 1130 AT STRINGER 30. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE USING ORIGINAL FASTENER LOCATIONS. FASTENERS THROUGH FRAME .1875 INCH HI-LOCKS. FASTENERS THROUGH SKIN ORIGINAL SIZE AND TYPE REF 51-10-1. (M)Apr 7, 1999 · N890AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA990598Frame · corrodedTUL - FOUND STATION 1070 BELLFRAME FLANGE AND WEB STRINGER 26 AND 25 LEFT. INSTALLED DOUBLER PER SRM 51-40-3. (M)Apr 6, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990597Frame · bentTUL - FOUND STATION 1050 BELLFRAME FLANGE 8 WEB BENT STATION 1050, STRINGER 26 AND 25 LEFT. REPAIRED BELLFRAME PER SRM 51-40-3. (M)Apr 6, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990605Stringer · crackedTUL - CUT OUT CRACK AND REPAIRED STRINGER 15R FORWARD SIDE OF WING SCANNING LIGHT. MATERIAL PER SRM 53-10-3 FIG 5. FASTENERS SIX .1875 HI-LOCKS THROUGH SKIN AND STRINGER THREE .1875 HI-LOCKS THROUGH SIDE OF U-CHANNEL PER SIDE, TWO .15625 HI-LOCKS THROUGH STRApr 4, 1999 · N890AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA990604Stringer · damagedTUL - CUT OUT DAMAGE AT FS 720A PLUS 10 INCHES SPLICED IN NEW STRINGER. MATERIAL PER SRM 53-10-3 FIG 5. FASTENERS THROUGH SKIN FOUR .1875 HI-LOCKS PER SIDE OF SPLICE ALSO THROUGH LIP OF STRINGER. FOUR .15625 HI-LOCKS THROUGH SIDE OF 'J' CHANNEL PER SIDE, EAApr 4, 1999 · N890AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA990595Frame · bentTUL - FOUND BELL FRAME FLANGE/WEB BENT. INSTALLED DOUBLER PER SRM 51-40-3. (M)Apr 4, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990576Stringer · corrodedTUL - FOUND STRINGER 30 CORRODED AT STATION 1177. INSTALLED NEW SECTION OF STRINGER STATION 1156-1183 WITH NEW SPLICE BETWEEN STATION 1148 AND 1166 PER SRM 51-10-3 PAGE 3, NEW END FITTING INSTALLED AT 1183 ALODINED AND PRIMERED ALL PARTS. (M)Apr 3, 1999 · N890AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA990577Stringer · corrodedTUL - FOUND STRINGER 29L CORRODED AROUND FASTENER, OUTBOARD LEG AFT OF STATION 950B TO 950B PLUS 1 INCH. REPAIRED PER ESO 11697 DATED 4-1-99 USING GENERAL GUIDE LINES OF SRM 51-40-4. INSTALLED STRAP REPAIR. (M)Apr 1, 1999 · N890AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA990567Frame · damagedTUL - REMOVED DAMAGE BY CUTTING OUT. INSTALLED DOBULER AND FILLER SRM 51-40-3 DOUBLER MATERIAL 7075-T6 .063 INCH THICK FILLER .050 INCH 7075-T6 FASTENERS (10 EACH) .1875 PROTRUDING HD HI-LOCKS (4) .1875 100 DEGREES COUNTERSUNK HD HI-LOCKS WITH TOTAL 14 INCH TApr 1, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990580Frame · dentedTUL - FOUND STATION 560 BELLFRAME DENTED IN BETWEEN STRINGERS 24L AND 25L. CUT OUT DAMAGE 1 INCH BY 1.25 INCH AND INSTALLED DOUBLER PER SRM 51-40-3 PAGE 1-5. MATERIAL .063 INCH 7075T-6, 9 INCH LONG USING 27MS20470D, .1875 INCH RIVETS, 3 ROWS PAST DAMAGE, 1 OMar 31, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990568Sill · corrodedTUL - FOUND STATION 970 STRINGER 27 RIGHT DOOR CUT OUT CORRODED CHORD ANGLE, SILL PLATE LOWER. BLENDED CORROSION, HFEC FASTENER HOLES. LIGHTLY SPOTFACED FASTENERS HOLES, AND FLAP PEENDED REWORK AREA PER ESO11697, DATED 3/29/99. (M)Mar 31, 1999 · N890AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA990609Frame · bentTUL - BELT FRAME, BENT FLANGE AND WEB STATION 950F BETWEEN 26L AND 25L. INSTALLED DOUBLER ON BELT FRAME AT STATION 950F BETWEEN STRINGER 25L AND 26L IAW AARD 53-10-07-3. DAMAGED AREA OF FREE FLANGE AT WEB CUT OUT WAS 1 INCH BY 1.5 INCH. DOUBLER USED WAS 2024Mar 30, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990588Frame · bentTUL - FOUND STATION 1070 BETWEEN STRINGER 26R-25R, BELLFRAME BENT IN WEB. REMOVED 3.5 INCH BY 1.25 INCH DAMAGED AREA. INSTALLED .071 T6 DOUBLER PER SRM 51-40-3. INSTALLED DOUBLER WITH 11BACB30FP8-4, 11 BACC30M8, 11 BACBB30FP6-3, 19 BACC30M6, 8 BACB30F06-3 HIMar 30, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990569Frame · damagedTUL - STATION 950A STIRNGER 19R, BELT FRAME HAS DEEP WEAR FROM CEILING PANEL, DAMAGE ON FREE FLANGE. INSTALLED DOUBLER PER 51-40-3. NO CUT OUT REQUIRED. DOUBLER PUT ON TOP OF FREE FLANGE AND WEB WAS .063 7075 MATERIAL 5.5 INCH LONG. 1 ROW OF 6 HI-LOCKS BACMar 30, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990602Floorbeam · corrodedTUL - FOUND TOP OF FLOORBEAM AT BS 380 IS CORRODED FROM RBL 48 TO 64 RBL. FLOORBEAM REPAIR COMPLETE AFT FLANGE OF UPPER CHORD STATION 380 RBL 48 TO 65 AS PER AARD 53-10-07-02 PAGE 1-3 FIG 1. (M)Mar 29, 1999 · N890AA · Boeing 727223 · Fuselage Main, Floor BeamSDR AALA990589Angle · crackedTUL - FOUND ANGLE ON FRAME CRACKED AT FASTENER HOLE AT ATTACH POINT TO STRINGER 14R. REMOVED CRACKED PART AND INSTALLED NEW PART WITH HI-LOCKS. (M)Mar 29, 1999 · N890AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA990586Frame · dentedTUL - FOUND STATION 990 BELL FRAME FLANGE AND WEB BENT LEFT STRINGER 25-27. CUT OUT 6.75 INCH BY 1.25 INCH DAMAGED AREAS. INSTALLED .071 T-6 DOUBLER PER SRM 51-40-3, 25 MS20470, 25MS 20470 D6-6 (RIVETS), 16 BACR15CE6D6 RIVETS, 3 BACB30FP6-3 (RIVETS), 3BAC30MMar 29, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990581Frame · dentedTUL - FOUND STATION 580 BELLFRAME DENTED FROM STRINGER 24L TO 22L. REMOVED AND CUTOUT 3 DAMAGED AREAS (SIZES NOTED ABOVE). INSTALLED .063 DOUBLER, 7075-T6, 20 INCH LONG. INSTALLED 55-MS20470D, .1875 RIVETS AND 4 MS20470D, .25 INCH RIVETS, 3 ROWS TOTAL PER SMar 29, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990578Frame · bentTUL - FOUND STATION 680 BELLFRAME BENT BETWEEN STRINGER 24L AND 23L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-40-3. (M)Mar 29, 1999 · N890AA · Boeing 727223 · Fuselage Main, FrameSDR AALA990564Skin · corrodedTUL - HEAVY CORROSION ON OUTER SKIN OF NR 2 FUEL CELL AT STATION 847, LBL 28, WING CENTER SECTION. REMOVED 4 FASTENERS, BLENDED CORROSION. REMOVED .051 THICKNESS. REAMED HOLES 2ND OVER, COLD WORKED HOLES. INSTALLED 4 4 EACH 2ND OVERSIZE HI-LOCKS (SEALER) TMar 29, 1999 · N890AA · Boeing 727223 · Wing, Plate/SkinSDR AALA990583Frame · dentedTUL - FOUND FRAME 660 DENTED FROM STATION 24L TO 23L. REMOVED TWO DAMAGED AREAS, .75 INCH BY 6.5 INCH, .75 INCH BY .75 INCH. INSTALLED DOUBLER (7075 T-6, .063) 18 INCHES LONG, WITH 3 ROWS OF RIVETS, 1 ROW ON TOP, 2 ROWS ON SIDE WITH 41 .1875 D-RIVETS AND FOUMar 26, 1999 · N890AA · Boeing 727223 · Fuselage Main, Frame
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