N272AU, cancelled Aug 22, 2003

Service difficulty reports · 73

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 = 'N272AU' AND deregistration_id = 'N272AU-2003-08-22'
  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 USAASB01174Charger · failedBWI - MAINTENANCE FOUND THE AFT OVERHEAD EMERGENCY LIGHT BETWEEN ROW 19 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 9008-3-5A) AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)Jun 15, 2001 · N272AU · Boeing 7372B7 · Emergency LightingSDR USAASB01154Fuse · blownTPA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE FORWARD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THE FUSE IN THE POWER SUPPLY BLOWN. REMOVED AND REPLACED FUSE. OPS CHECK GOOD. (M)Jun 2, 2001 · N272AU · Boeing 7372B7 · Emergency LightingSDR USAASB99170Epr Transmitter · failedCLE - FLT 8027 - APPROXIMATELY 7 MINUTES AFTER TAKEOFF, CREW ENCOUNTERED PROBLEMS WITH THE NR 2 ENGINE EPR AND THE AUTOTHROTTLE DISCONNECTING. WITH FUEL FLOW AT 5.3, NR 1 ENGINE EPR WAS AT 1.78 AND THE NR 2 ENGINE AT 1.41. WHEN AUTOTHROTTLE WAS RE-ENGAGED, TJul 13, 1999 · N272AU · Boeing 7372B7 · Engine Pressure Ratio (EPR)SDR USAASB99126Switch · failedBWI - MAINTENANCE FOUND THE CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL SWITCH IN THE COCKPIT. OPERATIONAL CHECK GOOD. (M)May 16, 1999 · N272AU · Boeing 7372B7 · Emergency LightingSDR USAA990438Skin · crackedTPA - DURING CX-2 CHECK, FOUND .375 INCH LONG SKIN CRACK, LEFT FUSELAGE, 2 INCH AFT OF BS 727B AT LOWER EDGE OF STRINGER 18L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. DOUBLER MADE OF 2024T3 - .063 PER BOEING SRM 53-30-3 FIG 1. (M)May 7, 1999 · N272AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA990135Gusset · crackedCLT - DURING DROP IN VISUAL INSPECTION, FOUND A 1 INCH CRACK IN UPPER RADIUS OF GUSSET AT TOP OF N/G WELL. REPAIRED PER SRM 51-10-1. (M)Feb 18, 1999 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAASB99025Connector · shortedBOS - FLT 1241 - DURING CLIMB-OUT FROM BOS AT FL 200, THE CREW RECEIVED A NR 2 ENGINE FIRE WARNING LIGHT AND HORN. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND IMMEDIATELY SHUT DOWN THE NR 2 ENGINE AND FIRE BOTH FIRE EXTINGUISHING BOTTLES. AN EMJan 31, 1999 · N272AU · Boeing 7372B7 · Fire DetectionSDR USAA980193Skin · crackedROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK IN SKIN FORWARD SIDE OF LOWER HINGE CUTOUT AT FORWARD ENTRY DOOR. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 31. (M)May 12, 1998 · N272AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980192Skin · scratchROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 3 INCH SCRATCH APPROX .025 INCH DEEP IN CROWN SKIN STATON 687, STRINGER 1L. BURNISHED AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)May 12, 1998 · N272AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB97340Pitot Probe · malfunctionedCLT - FLT 8026 - FLIGHT DIVERTED TO CLT DUE TO A 10 KNOT DIFFERENCE BETWEEN CAPTAINS AND FIRST OFFICERS AIRSPEED INDICATORS. INDICATED AIRSPEED APPEARS TO BE 10 KNOTS HIGHER ON FIRST OFFICERS SIDE BETWEEN 70-150 KNOTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT.Dec 17, 1997 · N272AU · Boeing 7372B7 · Pitot/Static SystemSDR 98ZZZM111Adc · malfunctionedCLT - FLT 8026 - FLIGHT DIVERTED TO CLT DUE TO A 10 KNOT DIFFERENCE BETWEEN CAPTAINS AND FIRST OFFICERS AIRSPEED INDICATORS. INDICATED AIRSPEED APPEARS TO BE 10 KNOTS HIGHER ON FIRST OFFICERS SIDE BETWEEN 70-150 KNOTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT.Dec 17, 1997 · N272AU · Boeing 7372B7 · Air Data ComputerSDR USAASB97088Anti-Ice Tube · failedCLT - FL 775 - ON CLIMB-OUT FROM CLT, AT 10,000 FEET, THE NR 1 ENGINE OVERHEAT ILLUMINATED. CAPTAIN ACCOMPLISHED ENGINE OVERHEAT CHECKLIST. WHEN THRUST WAS REDUCED, LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NOMar 22, 1997 · N272AU · Boeing 7372B7 · Engine Anti-Icing SystemSDR USAASB97049Battery Pack · dischargedCLE - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN INOP AT THE CENTER CABIN CEILING. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)Feb 16, 1997 · N272AU · Boeing 7372B7 · Emergency LightingSDR USAASB96263Detection Loop · failedPIT - FLT 1212 - FLIGHT DIVERTED TO PIT DUE TO A RIGHT WING BODY OVERHEAT LIGHT. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE STRUT CAVITY OVERHEAT DETECTION LOOP. RAN ENGINE. ADec 17, 1996 · N272AU · Boeing 7372B7 · Overheat DetectionSDR USAA951372Intercostal · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1.5 INCH BY 1 INCH, BY STATION 947 TO STATION 967, RBL 45 INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA951317Seat Track · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 3 INCH CORRODED AREA BS 986.5 RBL 24. REPLACED SEAT TRACK, WT CHANGE LESS THAN 1 LB. REPAIRED PER SRM 51-10-1 AND SRM 53-10-5. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA951316Floor Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK LBL 25 LONGITUDINAL FLOOR BEAM WEB (LOWER) STATION 707, WL 203. INSTALLED WEB REPAIR (WT .3 LBS), REPAIRED PER SRM 51-40-2. (M)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA951315Floor Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BL 0 STATION 708 AND BS 710. INSTALLED WEB REPAIR, REPAIRED PER DWG 65C34537. (M)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA951314Skin · gougedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH GOUGE IN OUTER SKIN OF AFT CARGO DOOR TOP AFT CORNER OF DOOR (6 INCH BY 6 INCH DOUBLER). INSTALLED EXT SKIN DOUBLER, REPAIRED PER SRM 52-00-3. (M)Dec 6, 1995 · N272AU · Boeing 7372B7 · Cargo/Baggage DoorsSDR USAA951313Fitting · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK, BL 0 LONGITUDINAL FLOOR BEAM SUPPORT FITTING FORWARD RADIUS, STATION 727, WL 202.5. INSTALLED REINFORCING ANGLES, RADIUS FILLERS, SHIMS AND SEALED. REPAIRED PER EO 5394G176. (M)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA951312Angle · crackINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK RIGHT WING TO BODY SUPPORT ANGLE BS 540-522. REPLACED ANGLE, LESS THAN 1 LB WEIGHT CHANGE, REPAIR PER EA 25375 AND SRM 51-40-3. (M)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA951311Stringer · crackINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK S-16R, BETWEEN STATION 500B AND 520, ON STRINGER. INSTALLED STRINGER REPAIR, REPAIRED PER EO 5393X228. (M)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA951310Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STRINGER 16 L, BETWEEN STATION 500B AND STATION 520, ON STRINGER. INSTALLED STRINGER REPAIR, REPAIRED PER EO 5393X228. (M)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA951309Hinge · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT AFT END OF HINGE, FRONT CABIN SERVICE DOOR LOWER GATE HINGE. REPLACED HINGE, REPAIR PER EA 40350. (M)Dec 6, 1995 · N272AU · Boeing 7372B7 · Service DoorsSDR USAA951308Stringer · gougedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH GOUGE IN STRINGER OUTBOARD 'J' SECTION, STATION 1044 STRINGER 27L. INSTALLED REPAIR DOUBLER UNDER 'J' LEG OF STRINGER, AFTER SMOOTHING GOUGE. REPAIRED PER SRM 53-10-3 FIG 1. (M)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA951307Skin · damagedINT - DURING 'Q-3' CHECK VISUAL INSPECTION (PREVIOUS REPAIR NOT PER SRM), FOUND UNKNOWN DAMAGED DOUBLER, 8 INCHES BY 9.50 INCHES, BS 227 TO BS 235, S19R TO S20R. INSTALLED DOUBLER PER SRM, REPAIRED PER SRM 53-30-3. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA951306Floor Beam · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH LONG CRACK IN UPPER RADIUS OF BEAM CAP, STA 520, FLOOR BEAM RBL 25. INSTALLED FLOOR BEAM REPAIR, .8 POUNDS AT BS 520, REPAIRED PER SB 737-53-1120, EA 40385. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA951305Stringer · gougedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND DEEP GOUGE .25 INCH BY 2 INCHES IN UPPER INBOARD LEG OF S26L, BS 1044. INSTALLED STR REPAIR, LESS THAN 1 POUND ADDED, REPAIRED PER SRM 53-10-3, FIGURE 1. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA951304Angle · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1.50 INCH CRACK, BS 727, RBL 24.5 ON ANGLE. INSTALLED REPAIR ANGLE, REPAIRED PER EA 40453. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA951303Attach Angle · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK, STA 639, STUB BEAM ATTACH ANGLE, RBL 45, WL 207. REPLACED ATTACH ANGLE, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA951302Frame · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK, STA 616, RIGHT FRAME INBOARD CHORD, FIRST FASTENER ABOVE CENTER WING SKIN. INSTALLED FILLER ANGLE, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER EA 40391. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA951301Frame · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK, STA 616, LT FRAME INBOARD CHORD, FIRST FASTENER ABOVE CENTER WING SKIN. INSTALLED FILLER AND ANGLE, WEIGHT CHANGE LESS THAN 1 POUND. REPAIRED PER EA 40391. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA951300Support · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK, SEAT TRACK SUPPORT CHANNEL, STA 520, LBL 45, WL 207.5. INSTALLED FLOOR BEAM REPAIR, REPAIRED PER SB 737-53-1120, EA 40385, .8 POUNDS AT BS 520. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA951298Floor Beam · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK, RBL 24.5, STA 675, IN FLOOR BEAM. CRACK CONTAINED AT AILERON QUADRANT CUT-OUT. INSTALLED REPAIR CHANNEL AMD DOUBLERS, AND RADIUS FILLERS AS REQUIRED PER CO 5791G632 AND EA 40396. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA951297Floor Beam · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK, LBL 24.5, STA 675, IN FLOOR BEAM. CRACK CONTAINED BY FASTENER HOLE AND CUT-OUT INSTALL REPAIR CHANNEL, DOUBLERS, AND RADIUS FILLER AS REQUIRED BY EO 5791G632 AND EA 40396. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA951296Skin · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH LONG CRACK IN OUTER SKIN AT UPPER HINGE CUT-OUT AT ENTRY DOOR. INSTALLED EXTERIOR SKIN REPAIR. REPAIRED PER EA 40360. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Passenger/Crew DoorsSDR USAA951295Doubler · damagedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH SLOT IN BEAR STRAP - DOUBLER PREVIOUSLY INSTALLED, BUT NOT PER SRM BS 794 AT S23R. REMOVED PREVIOUSLY INSTALLED DOUBLER AND INSTALLED REPAIR PER EA. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA951293Seat Track · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 3.50 INCH BY 1 INCH AND 2 INCHES BY 1 INCH, BS 990 AND BS 1015 AT RBL 8 INCHES ON SEAT TRACK. REPLACED TRACK, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSIODec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA951292Intercostal · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES, STA 328 TO 340, LBL 12 INCHES ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-10. CORROSION LEVEL 2. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA951290Floor Beam · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 2 INCHES, STA 312 RBL 35 INCHES ON FLOOR BEAM. REPLACED T-CAP FROM LBL 6 TO RBL 36, REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA951289Floor Beam · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH BY .50 INCH CORRODED AREA FLOOR BEAM BS 1016, LBL 15. REMOVED CORROSION AND INSTALLED REPAIR STRAP, REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA951288Intercostal · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 1 INCH, STA 986.5 TO 1006 BL ZERO ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA951287Intercostal · corrosionINT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION 1.50 INCHES BY 1 INCH, STA 947 TO STA 967, RBL 45 ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA951286Floor Beam · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA AROUND NUTPLATE HOLES .25 INCH BY .25 INCH, BS 967 LBL 4, RBL 5, RBL 18 RBL 26, RBL 47, ON FLOOR BEAM. INSTALLED TEE SECTION ANGLES AND STRAPS. REPAIRED PER TR 53-10-05 C. CORROSION TASK NR C53-1Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA951285Stringer · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 12 INCH BY 1 INCH AT S-26 R, BS 974 TO BS 986 ON STRINGER. SPLICED NEW STRINGER SECTION IN, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA951284Stringer · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 5 INCH BY 1 INCH S-25 L BS 968 ON STRINGER. INSTALLED DOUBLER WEIGHT CHANGE LESS THAN 1 LB. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA951283Stringer · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 6 INCH BY 1 INCH S-27 L, BS 1004 TO BS 1010 ON STRINGER. SPLICED IN NEW STRINGER SECTION WEIGHT CHANGE LESS THAN 1 LB. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA951282Angle · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 24 INCH FORWARD ENTRY DOOR TRANSITION ANGLE. INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M)Dec 6, 1995 · N272AU · Boeing 7372B7 · Passenger/Crew DoorsSDR USAA951281Intercostal · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION, 1 INCH BY 3 INCHES, STA 312 TO STA 328, LBL 12 INCHES, ON INTERCOSTAL. REPLACED INTERCOSTAL, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-01. CORROSION LEVEDec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA951280Floor Beam · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION, 2 INCHES BY 4 INCHES, STA 344, BL ZERO TO LBL 8 INCHES, ON FLOOR BEAM. CUT OUT FLOOR BEAM SECTION, FABRICATED NEW T-CAP, AND REPAIRED DOUBLERS AND INSTALLED PER TR 53-10-13. CORROSION TASK NR C53-1Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor Beam
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