N884AA

Service difficulty reports not matched to an aircraft · 77

They name N884AA, 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 = 'N884AA' 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 AALA20011741Beam · corrodedTUL - FOUND CORROSION ON RIGHT HORIZONTAL STAB UPPER T/E BEAM INBOARD OF NR 7 ELEV HINGE. INSTALLED DOUBLER PER ESO 11697. (M)Sep 6, 2001 · N884AA · Boeing 727223 · Horizontal Stabilizer StructureSDR AALA20011742Skin · dentedTUL - FOUND DENT WITH CREASE IN FUSELAGE SKIN. CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER PER 53-30-3 FIG 3 PAGE 13 AND 53-30-3 PART 1 DETAIL 1. (M)Sep 5, 2001 · N884AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA10011743SkinTUL - FOUND BUBBLE IN FUSELAGE SKIN STATION 1013 ABOVE STRINGER 28 LEFT. CUT AND REMOVED DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3A. (M)Aug 31, 2001 · N884AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA20011493Connector · defectiveDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS VERY DIM. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT CONNECTORS AT FIRST CLASS FORWARD PARTITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Jul 23, 2001 · N884AA · Boeing 727223 · Light System WiringSDR AALA20002022Skin · corrodedTUL - FOUND AREA OF CORROSION ON LOWER SURFACE 1.5 INCH BY 1.5 INCH, CENTER WING SKIN ABOVE LOUVERS AFT OF RIGHT PRIMARY HEAT EXCHANGER. INSTALLED DOUBLER PER SRM 57-30-3. (M)Nov 18, 2000 · N884AA · Boeing 727223 · Wing, Plate/SkinSDR AALA20001571Valve · leakingDFW - FLT 0608 - ON CLIMB-OUT, PASSENGER REPORTED FUEL LEAKING FROM LEFT WING. CONFIRMED LEAK BY VISUAL INSPECTION FROM CABIN BY FLIGHT ENGINEER, RETURNED TO DFW, LANDED WITHOUT INCIDENT. INSPECTED LEFT WING WITH NO FUEL LEAKS NOTED. EXCESSIVE FUEL IN SURGESep 15, 2000 · N884AA · Boeing 727223 · Aircraft Fuel Distribution SystemSDR AALA20000253Brake Assy · malfunctionedIAH - FLT 393 - ON LANDING, AIRCRAFT PULLED TO LEFT WITH BRAKES APPLIED. RESET BRAKE DEBOOSTERS, BLED BRAKES AND TAXIED AIRCRAFT WITHOUT FURTHER INCIDENT. SYSTEM GROUND CHECKED NORMAL OPERATION. LEFT ANTI-SKID CONTROL VALVE CHANGE IN MIA ON 2/5/2000. (M)Mar 28, 2000 · N884AA · Boeing 727223 · Landing Gear Brake SystemSDR AALA991646Light · inoperativeDFW - DURING OVERNIGHT MAINTENANCE, SEAT 6D AND 8D EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Oct 31, 1999 · N884AA · Boeing 727223 · Emergency LightingSDR AALA991427Light · dirtyMIA - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED ELECTRICAL CONTACTS TO BATTERY FOR AFT AIRSTAIRS EMERGNCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Sep 21, 1999 · N884AA · Boeing 727223 · Emergency LightingSDR AALA990924Battery · dirtyMIA - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED CONTACTS ON BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Jun 22, 1999 · N884AA · Boeing 727223 · Emergency LightingSDR AALA982207Stringer · crackedTUL - FOUND STRINGER END CRACKED FROM FAST HOLE 720B PLUS INCHES. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-10-3 FIG 1. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA982206Stringer · crackedTUL - FOUND STRINGER 15L CRACKED AT FS 720B PLUS 15 INCHES. REPAIRED STRINGER 15L AT FS 720C PLUS 15 INCHES PER SRM 53-10-3 FIG 1. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA982205Floorbeam · corrodedTUL - FOUND CORROSION ON FLOORBEAM AT FS 380 RBL 20 TO RBL 45. CUT OUT CORRODED PORTION OF UPPER AREA OF FLOORBEAM AND REPAIRED PER FLOORBEAM REPAIR SRM 53-10-8. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Floor BeamSDR AALA982204Stringer · corrodedTUL - FOUND CORROSION ON STRINGER 29 LT STATION 950C - 950E. CORROSION ON STRINGER 29 RT STATION 950F - 970. REMOVED CORROSION AND INSTALLED REPAIRS PER ECO 11697, DATED 11-12-98. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA982203Stringer · crackedTUL - FOUND STRINGER 15R CRACKED AT STATION 720B PLUS 4 INCH. CUT OFF CRACKED PORTION OF STRINGER AND INSTALLED STRINGER AND SPLICE PER SRM 53-10-3 PAGE 3-4B. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA982201Frame · bentTUL - FOUND STATION 1070 UPPER FLANGE BENT AND WEB CREASED STRINGER 25R. CUTOUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-4 PAGE 3-5 FIG 1 7075 T-6 .080, 2.5 INCH BY 17 INCH L 19 .1875 INCH HI-LOCKS UPPER FLANGE, 16 .25 AND 15 .1875 HI-LOCKS IN WEB. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982200Frame · crackedTUL - FOUND CRACK IN FRAME AT FS 930 ABOVE STRINGER 14R. INSTALLED Z-FRAME REPAIR AT FS 930 STRINGER 14R IAW 53-10-4 FIG 1. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982199Frame · bentTUL - STATION 1050 UPPER FLANGE BENT AND WEB IS DEFORMED AT STRINGER 24-25L. CUT OUT DAMAGE SECTION AND INSTALLED DOUBLER PER SRM 53-10-4 PG 3-5. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982196Stringer · corrodedTUL - STRINGER 29R HAS CORROSION ON OUTBOARD FLANGE AND EXTENDING FROM UNDER SEALANT STATION 950 E TO 950F. BLENDED OUT CORROSION, TREATED, PRIMED AND INSTALLED DOUBLERS PER ESO 11697 DATED 11-12-98. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA982194Floorbeam · corrodedTUL - TOP OF FLOORBEAM CORRODED STATION 400 RBL 3 TO RBL 4. CUT OUT UPPER PORTION OF FLOORBEAM TO REMOVED CORROSION AND INSTALLED FLOORBEAM DOUBLER REPAIR PER SRM 53-10-8 PAGE 9 A AND B. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Floor BeamSDR AALA982193Stringer · corrodedTUL - FOUND CORROSION AT STRINGER 26R BETWEEN STATION 680-700. REMOVED CORRODED SECTION OF STRINGER. INSTALLED SPLICE REPAIR IAW SRM 53-10-3. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR AALA982192Frame · dentedTUL - STATION 580 FRAME DENTED BETWEEN STRINGER 22L-25L. REPAIRED FRAME PER SRM 51-40-3 AND D224655 11-18-98 AARD 53-10-7-3. CUT OUT DAMAGED AREA 4 INCH BY 3 INCH. INSTALLED .050 7075-T6 DOUBLER WITH MS204720 MS 204260, RIVETS (FLANGE) 4 EACH FASTENERS BOTHDec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982190Frame · dentedTUL - STATION 500 BELL FRAME DENTED STRINGER 23R-25R. CUT OUT DAMAGE. INSTALLED .050 7075-T6 DOUBLER 18 INCH PER SRM 51-40-3 AND AARD 53-10-7-3. 36 .1875 MS20470D RIVETS, 4 .25 INCH MS 20470D RIVETS (4 RIVETS EACH SIDE DAMAGE) 3 ROWS. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982189Frame · crackedTUL - FOUND CRACK IN ANGLE OF FRAME TO STRINGER ATTACH POINT STATION 805, STRINGER 14R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-40-3 PAGE 3, 3A. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982187Frame · dentedTUL - STATION 680 BELL FRAME DENTED BETWEEN STRINGER 22R AND 21R. INSTALLED DOUBLER PER SRM 51-40-3 FIG 3, .050 7075-T6 3 ROWS OF MS20470D RIVETS (11 EACH) AND ONE ROW .1875 OF MS20426 D RIVETS (6 EACH) .1875, DOUBLER 8 INCHES LONG. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982186Frame · dentedTUL - STATION 660 BELL FRAME DENTED BETWEEN STRINGER 22R-25R. CUTOUT DAMAGE, INSTALLED DOUBLER PER SRM 51-40-3 PAGE 3 .050 7075-T6 17 INCH BY 2.5 INCH, 24 .1875 MS 20470D RIVETS, 15 MS20426D RIVETS .1875 INCH, 1 MS20470D .25 INCH RIVET. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982185Frame · dentedTUL - STATION 620 BELL FRAME DENTED BETWEEN STRINGER 23L-25L. CUT OUT DAMAGE. INSTALLED DOUBLER PER SRM 51-40-3 PAGE 3, .050 7075-T6 21 MS20426D .1875 RIVETS, 40 MS20470D .1875 RIVETS, 5 MS20470D .25 RIVETS, 4 FASTENERS PAST DAMAGE, 2 ROWS IN WEB. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982184Frame · dentedTUL - STATION 700 BELL FRAME DENTED BETWEEN STRINGER 25R AND 22R. DYE CHECKED, NO CRACKS FOUND. INSTALLED DOUBLER 30 INCH LONG .050 7075-T6 USING BAC B30FM HI-LOCKS 3 ROWS, AND NAS 8603-2 FASTENERS ONE ROW PER SRM 54-10-3 AND 53-10-4. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982183Frame · crackedTUL - BELL FRAME CRACKED AT FS 804.95 STRINGER 14L. REPAIRED BELL FRAME IAW SRM 51-40-3 PAGE 1-6. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982181Frame · dentedTUL - STATION 950E FRAME HAS DENT ON UPPER FLAGNE WITH WEB DEFORMED ABOVE STRINGER 26. INSTALLED REPAIR DOUBLER PER SRM 51-40-3 USING MAT 7075-T6, SIZE 12 INCH BY 4 INCH, WITH 2 ROWS ON SIDE WEB HAVING 12 .25 INCH BAC B30 FP8 1 ROW AND 13 .1875 BAC B30 FP6 OTDec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982180Frame · dentedTUL - BELL FRAME DENTED STATION 680 BETWEEN STRINGER 22L AND 24L. CUT OUT DAMAGED AREA 4.5 L BY .5 W INSTALLED .050 DOUBLER 7075-T6 13 INCHES LONG. INSTALLED 17 FASTENERS THROUGH BELL FRAME UPPER FLANGE ON .75 INCH SPACING, 20 FASTENERS THROUGH SIDE ON 1 INCDec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982179Frame · dentedTUL - STATION 950F FRAME HAS LARGE DENT IN UPPER FLANGE WITH CREASE IN WEB BETWEEN STRINGER 23L TO 24L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-40-4. 3 ROWS OF 4 RIVETS ON EACH SIDE OF DAMAGE 7075-T6 .071, 17 438D .25 INCH, 14 BAC015CE6 20 EACHDec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982178Frame · dentedTUL - STATIN 1030 FRAME HAS DENT IN UPPER FLANGE WITH FORWARD WEB DEFORMED, STRINGER 25-26R. INSTALLED DOUBLER MADE OF .070 7075 F6 APPROX 13 INCHES LENGTH BY 4 INCHES WITH 2 ROWS OF .25 INCH HI-LOCKS HAVING 4 FASTENERS EACH SIDE OF DAMAGE AND 1 ROW OF .1875 Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982176Angle · crackedTUL - ANGLES CRACKED IN RIGHT LOWER TORQUE BOX IN VENTRAL STAIRS STATION 1273 UNDER A/S ACT. ANGLES REPLACED UNDER AIRSTAIRS ACT AND WEB REPLACES STATION 1273. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR AALA982175Frame · dentedTUL - STATION 620 BELL FRAME DENTED BETWEEN STRINGER 23L AND 25L. REPAIRED BELT FRAME PER SRM 51-40-3 PAGE 3, STATION 620 BETWEEN STRINGER 23L AND 25L. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982174Frame · dentedTUL - STATION 720A FRAME UPPER FLANGE DENTED BETWEEN STRINGER 24L AND 25L. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3. INSTALLED DOUBLER OVER DAMAGED AREA, DENT .050 FRAME, DOUBLER MATERIAL .050. SAME TYPE MATERIAL FASTENERS BAC 830 FM6 BACDec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982173Floorbeam · corrodedTUL - STATION 1130 FLOORBEAM HAS CORROSION AROUND CLIP NUT PLATE HOLES IN LOWER FLANGE BL 0 TO APPROX LBL 40. INSTALLED DOUBLER PER ESO 11697 DATED 11-19-98. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Floor BeamSDR AALA982172Skin · gougedTUL - TWO GOUGES IN SKIN INSIDE, BETWEEN STATION 1148-1166 RIGHT SIDE ABOVE STRINGER 27R. INSTALLED REPAIRED DOUBLER IAW SRM 53-30-3 PAGE 151 FIG 24. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Aerodynamic FairingsSDR AALA982171Skin · crackedTUL - FOUND CRACK EXTENDING FROM RIVET RIGHT SIDE STRINGER 1 AT STATION 1100, FUSE SKIN. INSTALLED DOUBLER REPAIR PER SB NR 727-53A0204 AND SRM 53-30-3 PAGE 3. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA982170Skin · wornTUL - SKIN LAP WORN STRINGER 19R STATION 720D PLUS 12 INCHES TO 720D PLUS 14 INCHES AT WIG WRAP AROUND PANEL L/E. REMOVED DAMAGED AREA. INSTALL FLUSH DOUBLER REPAIR PER SRM 53-30-3 FIG 6. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA982168Skin · corrodedTUL - FUSELAGE SKIN IS CORRODED AFT SIDE OF STATION 720A. INSTALLED 8 INCHES BY 12 INCHES EXTERNAL DOUBLER PER SRM 53-30-3 FIG 3 SHEET 1 THROUGH 4. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA982167Skin · corrodedTUL - FOUND FUSELAGE SKIN IS CORRODED OUTBOARD OF STRINGER 27R STATION 520. INSTALLED DOUBLER AS PER SRM 53-30-3 PAGE 12-14A. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA982166Skin · dentedTUL - FOUND 22 INCH LONG DENT IN SKIN STATION 418 TO 440 STRINGER 20R. REMOVED DAMAGED AREA AT SKIN AND INSTALLED DOUBLER PER 53-30-3 FIG 2. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA982165Skin · dentedTUL - FOUND FUSELAGE SKIN DENT .375 INCH BY 4 INCH APPROX 40 INCHES BELOW THE L3 WINDOW. TRIMMED OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3 PAGES 5-8 FIG 1. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA982164Skin · dentedTUL - FOUND 3.5 INCH DENT IN SKIN AT STATION 308 STRINGER 22R. CUT OUT 3 INCH BY 4 INCH AREA AT STRINGER AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 24. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA982163Skin · damagedTUL - FOUND DEEP TOOLING MARKS ON INNER SKIN STATION 356 BETWEEN STRINGER 9R AND 10R. BLENDED GOUGES AND INSTALLED DOUBLER PER SRM 53-30-3 PAGE 508 SRM 53-30-3 PAGE 3B AND AARD 53-30-03-3 PAGE 1. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA982162Skin · damagedTUL - FOUND LARGE DOUBLER INSTALLED ON OUTERSKIN AND DAMAGE NOT REMOVED AND DOUBLER DENTED. REPLACED DOUBLER AS PER SRM 53-30-3 FIG 5. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA982160Skin · dentedTUL - FOUND 2 INCH DENT WITH SCRATCHES STATION 363 STRINGER 20R. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW SRM 53-30-3 PAGE 3-C. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR AALA982010Frame · wornTUL - BELLFRAME STATION 990 HAS SPOT INBOARD OF STRINGER 8L. REPAIRED FRAME PER SRM 53-10-4 FIG 2. (M)Dec 11, 1998 · N884AA · Boeing 727223 · Fuselage Main, FrameSDR AALA982159Skin · corrodedTUL - FOUND AREA OF CORROSION ON LOWER WING SKIN UNDER AREA OF LEFT PRIMARY HEAT EXCHANGER. REMOVED CORROSION, TREATED AND INSTALLED REPAIR DOUBLER PER ESO NR 11697 DATED 11-17-98 AND REF BOEING MESSAGE AAL-TUL-98 1122RR DATED 17 NOV 98. (M)Dec 10, 1998 · N884AA · Boeing 727223 · Wing, Plate/Skin
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