N205AU, cancelled May 30, 2018

Service difficulty reports · 61

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 = 'N205AU' AND deregistration_id = 'N205AU-2018-05-30'
  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 F3LA99119Axle · corrodedDEN - DURING C-4 CHECK, INSPECTION REPORTED DAMAGE FROM CORROSION PITTING ON NOSE LANDING GEAR RT AXLE. REPLACED INNER CYLINDER ASSY PER BOEING MM 32-21-11. (M)Sep 4, 1999 · N205AU · Boeing 737201 · Nose/Tail Landing Gear Strut/AxleSDR F3LA99115Wire · failedDEN - DURING C-4 CHECK INSPECTION, REPORTED EMERGENCY EXIT SIGN INOPERATIVE AT ROW 9 LEFT SIDE. MAINTENANCE REPAIRED WIRING AT SEAT 9C FOR EMERGENCY EXIT SIGN. (M)Aug 22, 1999 · N205AU · Boeing 737201 · Light System WiringSDR F3LA99043Drag Brace · crackedDEN - DURING SERVICE CHECK, INSPECTION REPORTED NOSE LANDING GEAR UPPER DRAG BRACE BEARING MIGRATING AT ACTUATOR ATTACH POINT. UPON FURTHER INSPECTION, FOUND 1 INCH CRACK IN NOSE GEAR UPPER DRAG BRACE A-FRAME ON RT SIDE OF WEB. MAINTENANCE INSTALLED NEW DRAJun 4, 1999 · N205AU · Boeing 737201 · Nose/Tail Landing GearSDR F3LA99004Wire · brokenDEN - DURING A-6 CHECK, INSPECTION REPORTED FLOOR PROXIMITY LIGHTING AT ROWS 16, 17 AND 18 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRING AND SYSTEM CHECKED OK. (M)Feb 17, 1999 · N205AU · Boeing 737201 · Light System WiringSDR F3LA99001Skin · damagedDEN - FLT 850 - UPON ARRIVAL, MAINTENANCE REPORTED HOLE IN FUSELAGE, AFT OF FORWARD LAV SERVICE DOOR STATION 328, STRINGER 24R TO STRINGER 25R. MAINTENANCE FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-5. (M)Jan 5, 1999 · N205AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA98163Skin · crackedDEN - DURING SERVICE CHECK, MAINTENANCE REPORTED A 3 INCH CRACK IN NOSE WHEEL WELL SKIN, BS 245.6 TO 248.6, WL 168.5. A .125 INCH CRACK AT RIVET, BS 244.1, W 165.5, AND A .125 INCH CRACK AT BS 243.1, WL 164.3. MAINTENANCE REPAIRED DAMAGED AREAS PER SRM 51-40Aug 29, 1998 · N205AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA98080Gcu · failedPHX - FLT 429 - DURING DESCENT INTO PHX, FLIGHT CREW REPORTED NR 1 GENERATOR OFF BUS LIGHT ILLUMINATED FOLLOWED BY THE SMELL OF ELECTRICAL SMOKE WITH A SMALL AMOUNT OF VISIBLE SMOKE NOTICED. COMPLIED WITH SMOKE REMOVAL CHECKLIST AND SMOKE DISSIPATED. AIRCRAFJun 14, 1998 · N205AU · Boeing 737201 · AC RegulatorSDR F3LA98089Angle · corrodedPAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON MAIN EQUIPMENT BAY RIGHT INTERCOSTAL LOWER OUTBOARD SUPPORT ANGLE AT BS 353, RBL 12, WL 146. MAINTENANCE REPAIRED PER EO 98-0502. (M)Jun 5, 1998 · N205AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR F3LA98088Frame · crackedPAE - DURING C-CHECK INSPECTION REPORTED CRACK IN FORWARD CARGO DOOR LOWER FORWARD FRAME IN OUTBOARD RADIUS OF LATCH ARM. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SB 737-52-1100 AND MM 52-31-0. CYCLES: 2,451. (X)May 29, 1998 · N205AU · Boeing 737201 · Cargo/Baggage DoorsSDR F3LA98087Skin · crackedPAE - DURING C-CHECK INSPECTION, REPORTED CRACK ABOVE NR 2 LEADNG EDGE PYLON. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM'S 51-10-1, 51-30-2, AND 57-30-4. CYCLES: 2,451.0. (X)May 29, 1998 · N205AU · Boeing 737201 · Wing, Plate/SkinSDR F3LA98086Splice · crackedPAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN BS 727 BULKHEAD TO FLOORBEAM SUPPORT SPLICE AFT FLANGE, LBL 25, WL 202. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-1, 51-10-2, 51-20-1 AND 51-30-2. (M)May 29, 1998 · N205AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR F3LA98084Doubler · corrodedPAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON INNER MOUNTING DOUBLER FOR FORWARD LAVATORY DRAIN TUBE, BS 270, STRINGER 23R. MAINTENANCE REMOVED DAMAGED DOUBLER, FABRICATED REPLACMENT PART AND REPAIRED PER SRM 51-20-4, 51-30-2 AND 53-10-1. (M)May 29, 1998 · N205AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR F3LA98083Intercostal · crackedPAE - DURING C-CHECK INSPECTION, REPORTED CRACK ON INTERCOSTAL, AFT SIDE AT BS 294.5 STRINGER 7L. MAINTENANCE REMOVED INTERCOSTAL, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-10-3 FIG 2. (M)May 29, 1998 · N205AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR F3LA98081Skin · crackedPAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN FORWARD ENTRY DOOR OUTER SKIN, LOWER HINGE CUTOUT, UPPER AFT CORNER. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SB 737-52-1096 AND SRM 51-30-2. (M)May 29, 1998 · N205AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA98079Stringer · crackedPAE - DURING C-CHECK, INSPECTION REPORTED CRACK 1 INCH ABOVE STRINGER 12L, BS 294.5. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, 51-30-2, 51-40-3, FIG 1 AND 53-10-4. (M)May 29, 1998 · N205AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA98078Stringer · crackedPAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN CROWN OF STRINGER 7L, BS 295. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-10-3, FIG 1. (M)May 29, 1998 · N205AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA98077Skin · crackedPAE - DURING C-CHECK, INSPECTION REPORTED 1 INCH CRACK IN SKIN ABOVE NR 1 ENGINE PYLON, LEFT WING LEADING EDGE. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 57-30-04. (M)May 29, 1998 · N205AU · Boeing 737201 · Wing, Plate/SkinSDR F3LA98076Frame · corrodedPAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON FRAME AND SHEAR TIE AT BS 360, RBL 8-13, BETWEEN STRINGER 27R AND 28R. MAINTENANCE REMOVED DAMAGED AREA (6 INCH BY 4 INCH BY .006 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-1May 29, 1998 · N205AU · Boeing 737201 · Fuselage Main, FrameSDR F3LA98070Shear Tie · crackedPAE - DURING C-CHECK INSPECTION, REPORTED 1.8 INCH CRACK IN SHEAR TIE AT BS 294 BETWEEN STRINGER 12L AND 14L. MAINTENANCE FABRICATED NEW SHEAR TIE AND REPAIRED PER SRM 51-10-2 AND 51-30-2. (M)May 29, 1998 · N205AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR F3LA98062Skin · crackedPAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN AFT SERVICE DOOR SKIN ABOVE LOWER HINGE CUTOUT AT BS 949, STRINGER 14R, WL 220. MAINTENANCE REMOVED DAMAGED AREA, 1.5 INCH BY 2.5 INCH. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 52-00-3. (M)May 29, 1998 · N205AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA980529Frame · crackedPAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN FORWARD CARGO DOOR UPPER AFT FRAME. MAINTENANCE REMOVED DAMAGED FRAME. FABRICATED REPLACEMENT PART AND REPAIRED PER SRM 51-30-2. (M)May 29, 1998 · N205AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR F3LA98052Skin · corrodedPAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON INTERNAL SKIN AT BS 353-356, RBL 3. MAINTENANCE REPAIRED SKIN PER SRM 53-30-3, FIG 28. (M)May 26, 1998 · N205AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA98012Skin · crackedDEN - PRIOR TO DEPARTURE, MAINTENANCE REPORTED ONE .25 INCH CRACK IN LEFT WING LEADING EGE SKIN AT WBL 165.0. MAINTENANCE REPAIRED DAMAGED AREA PER SRM 57-30-4, PAGE 4. (M)Apr 1, 1998 · N205AU · Boeing 737201 · Wing, Plate/SkinSDR F3LA98009Wire · loosePHX - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 4 A, B, C INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SECURED WIRING HARNESS AND SYSTEM CHECKED OK. (M)Mar 17, 1998 · N205AU · Boeing 737201 · Light System WiringSDR F3LA98006Line · failedSFO - ON INBOUND FLIGHT TO SFO, FLIGHT CREW REPORTED LOSS OF 'A' SYSTEM HYDRAULIC PRESSURE AND FLUID. USED ALTERNATE FLAP SYSTEM AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE 'A' SYSTEM HYDRAULIC PRESSURE LINE IN AFT FLAP WELL, BOTH 'A' SYSTEM HMar 8, 1998 · N205AU · Boeing 737201 · Hydraulic System, MainSDR F3LA97157Light · inoperativeDEN - DURING SERVICE CHECK, MAINTENANCE REPORTED AFT RT EMERGENCY EXIT LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. REPLACED LIGHT ASSEMBLY AND CHECKED OK. (M)Nov 16, 1997 · N205AU · Boeing 737201 · Emergency LightingSDR F3LA97150Control Panel · failedOMA - UPON ARRIVAL, FLIGHT CREW REPORTED ELECTRICAL ODOR IN COCKPIT. REPLACED AUTOPILOT CONTROL PANEL AND CHECKED OK. (M)Sep 27, 1997 · N205AU · Boeing 737201 · Autopilot SystemSDR F3LA97149Line · failedAIR TURN BACK. UPON ROTATION, FLIGHT CREW REPORTED LOSS OF 'A' SYSTEM HYDRAULI CS AND DECLARED AN EMERGENCY. AIRCRAFT LEFT RUNWAY UPON LANDING AND GOT STUCK IN THE MUD. PASSENGERS WERE EVACUATED. REPLACED NR 2 ENGINE HYDRAULIC PRESSURE LINE IN PYLON AND BOSep 24, 1997 · N205AU · Boeing 737201 · Hydraulic System, MainSDR F3LA97131Wire · brokenDEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 4L INOPERATIVE. MAINTENANCE SPLICED BROKEN WIRE UNDER SEAT WITH BUTT CONNECTOR AND SECURED WIRE ROUTING UNDER SEAT FRAME. SYSTEM CHECKED OKAY. AIRFRAME TOTAL TIME: 72,075.1 HRJun 21, 1997 · N205AU · Boeing 737201 · Light System WiringSDR F3LA97133Wire · failedDEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 7A INOPERATIVE. MAINTENANCE INSTALLED NEW BUTT SPLICE SYSTEM CHECKED OKAY. (X)Jun 6, 1997 · N205AU · Boeing 737201 · Light System WiringSDR F3LA97129Battery Pack · dischargedDEN - FLT 18 - UPON ARRIVAL, FLIGHT CREW REPORTED FORWARD SECTION OF FLOOR PROXIMITY LIGHTING INOPERATIVE. REPLACED BATTERY PACK AND SYSTEM CHECKED OK. (M)Jun 6, 1997 · N205AU · Boeing 737201 · Emergency LightingSDR F3LA97098Bulb · failedDEN - UPON ARRIVAL, FLIGHT CREW REPORTED L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED LAMP AND CHECKED OK. (M)Mar 16, 1997 · N205AU · Boeing 737201 · Emergency LightingSDR F3LA97097Skin · dentedFUSELAGE DENTS BETWEEN BS 360 AND 409. REMOVED SKIN FROM BS 360 TO 440, STRINGER 19R TO 24R. FABRICATED AND INSTALLED REPLACEMENT SKIN AND REPAIR IAW EWO 97-0080. REF WORK ORDER 214932 FUSELAGE 153/7-133 AND SRM. (M)Mar 7, 1997 · N205AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA97096Skin · crackedPAE - A .5 INCH CRACK IN THE UPPER FORWARD CORNER OF THE FORWARD ENTRY DOOR CUTOUT SKIN. WHILE ACCOMPLISHING EA 53-737-023 INADVERTENTLY OVERSIZED 34 HOLES ABOVE ALLOWABLE LIMITS IN BOEING SB 737-53-1163. REPAIRED DAMAGED HOLES IAW TRAMCO EWO 97-0140 BY OVERMar 7, 1997 · N205AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA97093Skate Angle · crackedRIGHT VERTICAL STAB AFT MOUNT LUG INBOARD SKATE ANGLE CRACKED. REMOVED RIGHT VERTICAL STAB AFT MOUNTING LUG INBOARD SKATE ANGLE. FABRICATED REPAIR ANGLE FROM MATERIAL OF 7075-0 .071 AND HEAT TREATED BY GIDDENS INDUSTRIES, INC TO 7075-T6, PO NR 1ML212756. INFeb 26, 1997 · N205AU · Boeing 737201 · Vertical StabilizerSDR F3LA97052Bracket · corrodedPAE - FOUND CORROSION (C53-107-01) ON AFT AIRSTAIR HINGE SUPPORT BRACKET AT BS 982, LBL 40, WL 208. REMOVED CORROSION FROM AFT AIRSTAIR HINGE SUPPORT BRACKET IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. FABRICATED FLOOR SUPPORT PLATE AND FILLFeb 10, 1997 · N205AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR F3LA97051Skin · crackedPAE - FORWARD SERVICE DOOR LOWER HINGE CUTOUT UPPER CORNER IS CRACKED .125 INCH IN LENGTH. REPAIRED CRACK BY STOP DRILLING AND INSTALLING EXTERNAL DOUBLER IAW TRAMCO EWO 97-0094. (M)Feb 10, 1997 · N205AU · Boeing 737201 · Service DoorsSDR F3LA97048Floor Beam · corrodedPAE - FLOOR BEAM UPPER CHORD AT BS 277 HAS TWO .625 INCH DIAMETER HOLES AT LBL 17 AND LBL 24, WL 208. CORROSION WAS DISCOVERED AT BS 277 LBL 17, LBL 20, AND LBL 25 WL 208. REMOVED CORROSION ON FLOOR BEAM FOUND TO BE OUT OF LIMITS, IAW 53-10-1, REPAIRED FLOORFeb 10, 1997 · N205AU · Boeing 737201 · Fuselage Main, Floor BeamSDR F3LA97049Seat Track · corrodedPAE - WHILE WORKING INTERIOR 00171, FOUND CORROSION ON SEAT TRACK AT RBL 25, BS 344-BS 360. REMOVED CORROSION ON SEAT TRACK AT RBL 25, BS 344-BS 360, WL 208, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED SEAT TRACK FROM BS 344-BS 360, FABRICATED SEAT TRFeb 9, 1997 · N205AU · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR F3LA97053Stringer · crackedPAE - AT STATION 500B PLUS 2.5, STRINGER 16L IS CRACKED, LENGTH OF CRACK .25 INCH. CUTOUT DAMAGED AREA AND REPAIRED PER TRAMCO EWO NR 97-0115 AND BOEING SB 737-53-1145. WORK ACCOMPLISHED ON TRAMCO WORK ORDER NR INTERIOR 262. (M)Feb 8, 1997 · N205AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA97046Floor Beam · corrodedPAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD, BS 360, RBL 1 TO LBL 11, WL 208.1. FOUND CORROSION BEYOND LIMITS. REMOVED BS 360, WL 208.1 CHORD FROM LBL 13 TO RBL 15. FABRICATED AND INSTALLED REPAIR. ALL WORK DONE IAW SRM 53-10-1, 53-10-9, 5Feb 6, 1997 · N205AU · Boeing 737201 · Fuselage Main, Floor BeamSDR F3LA97037Floor Beam · corrodedPAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD BS 344, RBL 9 TO LBL 65. FOUND CORROSION BEYOND LIMITS PER SRM 52-10-1. REMOVED CHORD FROM LBL 65 TO RBL 65. FABRICATED AND INSTALLED NEW CHORD. ALL WORK PERFORMED IAW SRM 51-10-6, 53-10-2, 53-10Feb 6, 1997 · N205AU · Boeing 737201 · Fuselage Main, Floor BeamSDR F3LA97036Floor Beam · corrodedPAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD BS 328, RBL 60 - LBL 30, WL 208.1. REMOVED CORROSION ON FLOOR BEAM UPPER CHORD BS 328. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED UPPER CHORD AND REPAIR ANGLES FROM 7075-T6 .090 T-ANGLEFeb 5, 1997 · N205AU · Boeing 737201 · Fuselage Main, Floor BeamSDR F3LA97035Skin · gougedPAE - AFT CARGO DOOR EXTERNAL SKIN GOUGED 28 INCH FROM FWD EDGE. BLENDED GOUGED AREA IN EXTERNAL SKIN OF AFT CARGO DOOR 28 INCH IN FROM FORWARD EDGE AND 21 INCH DOWN FROM EDGE. DAMAGED AREA FOUND TO BE OUT LIMITS IAW SRM 52-00-2. REMOVED, FABRICATED DOUBLERFeb 4, 1997 · N205AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA97034Seat Track · corrodedFOUND CORROSION (C53-107-01), ON SEAT TRACK BS 344-360, LBL 45, WL 208. BLENDED OUT CORROSION AT BS 344-360, LBL 45, WL 208. BLENDED OUT CORROSION AT BS 344-360, LBL 45, WL 208 IN AN AREA 6 INCH BY 1 INCH BY .020 INCH. ORIGINAL THICKNESS . 270 INCH OF SEAT Feb 4, 1997 · N205AU · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR F3LA97033Floor Beam · corrodedPAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD BS 294, LBL 21 TO RBL 60, WL 208.1. REMOVED CORROSION ON FLOOR BEAM UPPER CHORD BS 294, LBL 21 TO RBL 60, WL 208.1 IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED UPPER CHORD FFeb 4, 1997 · N205AU · Boeing 737201 · Fuselage Main, Floor BeamSDR F3LA97032Access Door · crackedAPU ACCESS DOOR MOST AFT RIB RIGHT CORNER CRACKED. STOP DRILLED CRACK END USING .125 INCH DRILL, CRACK WAS FOUND TO BE 2 INCHES IN LENGTH. REMOVED DAMAGED AREA AND INSTALLED FABRICATED REPAIR PARTS FROM STOCK MATERIAL OF 2024-T3 .050 IAW SRM 51-10-1, 52-40-1Feb 4, 1997 · N205AU · Boeing 737201 · Auxiliary Power Unit (APU) DoorsSDR F3LA97031Skin · dentedPAE - FORWARD CARGO DOOR EXTERNAL SKIN DENTED 18-20 INCHES DOWN FROM TOP EDGE AND 15-16 INCHES IN FROM AFT EDGE. DENT IN FORWARD CARGO DOOR EXTERNAL SKIN 18-20 INCHES DOWN FROM TOP EDGE AND 15-16 INCHES IN FROM AFT EDGE. FOUND TO BE OUT OF LIMITS IAW SRM 52-Feb 4, 1997 · N205AU · Boeing 737201 · Cargo/Baggage DoorsSDR F3LA97030Skin · dentedPAE - DENT ON SKIN AT BS 388.5, 4 INCH ABOVE STRINGER 19L. REMOVED DAMAGED SKIN ON BS 388.5, 4 INCHES ABOVE STRINGER 19L. FABRICATED THE DOUBLER FROM 2024-T3 .050 MATERIAL. SEALED AND INSTALLED WITH RIVETS PER SRM 53-30-3. (M)Jan 31, 1997 · N205AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA97029Skin · dentedPAE - DENT IN SKIN AT BS 875-879, BETWEEN STRINGER 17R-18R. FOUND DENT TO BE OUT OF LIMITS IAW SRM 53-30-01. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER FROM 2024-T3 .063 SHEET STOCK. DOUBLER INSTALLED WET SEALANT. ALL WORK DONE IAW SRM 53-30-3 FIG Jan 30, 1997 · N205AU · Boeing 737201 · Fuselage Main, Plate/Skin
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