Boeing 737-2B7

Service difficulty reports · 1,360

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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 aircraft_model_key = '7372B7'
  ORDER BY difficulty_date DESC"

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SDR USAA960522Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CRACK .375 INCHSTATION 917 BETWEEN STRINGERS 21L AND 22L SKIN. INSTALLED DOUBLER, REPAIREDPER SRM 53-30-3. (M)Jul 19, 1996 · N283AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA960521Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 90INCHES AT STATION 986 FLOOR BEAM UPPER CHORD. INSTALLED NEW SECTION WITHREPAIR ANGLES AND STRAPS, REPAIRED EA 41317. CORROSION TASK NR C53-107-02,CORROSION LEVEL 1. (M)Jul 19, 1996 · N283AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960520Stringer · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 7 INCHCORRODED AREA AT INBOARD SIDE STRINGER BS 960-967 STRINGER 26R. INSTALLEDSTRINGER SPLICE/REPAIR. REPAIRED PER SRM 53-10-3 PAGE 10 FIG 1. CORROSIONTASK NR C53-202-01, CORROSION LEVEL 1. (M)Jul 19, 1996 · N283AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA960519Floor Beam · chaffingINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 10 INCHESCHAFFING STATION 720 RHS KEEL BEAM LOWER CORD OUTBOARD FLANGE. INSTALLEDREPAIR STRAP, REPAIRED PER EA 41322. (M)Jul 19, 1996 · N283AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960518Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCHCORRODED AREA ON TOP OF FLOOR BEAM BS 1016 LBL 16 LBL 5. INSTALLED FLOORBEAM REPAIR, REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-017-02,CORROSION LEVEL 1. (M)Jul 19, 1996 · N283AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960517Skin · dentedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH INDENTEDAREA STABILIZER SKIN STATION 111.1 APPROX 12 INCHES FORWARD OF AFT SPAR.INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3. (M)Jul 19, 1996 · N283AU · Boeing 7372B7 · Horizontal Stabilizer, Plate/SkinSDR USAA960516Frame · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCHBY 1 INCH FRAME STATION 990 WL 208. INSTALLED FRAME REPAIR AND REPLACED 'Z'ANGLE, REPAIRED PER SRM 51-40-03, 51-10-2. CORROSION TASK NR 53-107-02,CORROSION LEVEL 1. (M)Jul 19, 1996 · N283AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAASB96132Downlocksensor · failedMCO - FL 1145 - ON DESCENT INTO MCO, LANDING GEAR WAS LOWERED,NOSE GEAR RED LIGHT FLICKERED ON. CAPTAIN WENT THROUGH MANUAL GEAREXTENSION PROCEDURE. NOSE GEAR SHOWED DOWN AND LOCKED IN VIEW FINDER.EMERGENCY EQUIPMENT WAS CALLED OUT. ABOUT FOUR MINUTES FROM Jul 17, 1996 · N286AU · Boeing 7372B7 · Landing Gear Position and WarningSDR USAASB96130Retract Mech · lack of lubePIT - FLT 1589 - DURING APPROACH TO PIT AND LANDING GEAR LOWERED, NOSE GEAR RED LIGHT STAYED ON. CREW RECYCLED GEAR, BUT NOSE GEAR RED LIGHT STILL SHOWED RED FOR APPROXIMATELY 20 SECONDS, THEN TURNED GREEN. FLIGHT LANDED SAFELY WITH NO FURTHER INCIDENT. MAIJul 16, 1996 · N286AU · Boeing 7372B7 · Landing Gear Retraction/Extension SystemSDR USAASB96129Fuel Hose · failedBWI - FLT 1176 - EN ROUTE FROM MCO TO BDL, CAPTAIN NOTICED WHAT APPEARED TO BE A FUEL LOSS AND SUSPECTED A FUEL LEAK. CAPTAIN DECLARED AN EMERENCY AND THE FLIGHT DIVERTED TO BWI. AFTER LANDING SAFELY AND EXITING RUNWAY, FIRE DEPARTMENT TOLD CREW A BAD FUEL LJul 15, 1996 · N276AU · Boeing 7372B7 · Aircraft Fuel Distribution SystemSDR USAASB96126Fuel Control · out of trimCLT - FLT 560 - TAKEOFF ROLL-OUT OF PIT WAS NORMAL. UPON PASSING 100 KNOTS, THE THROTTLES SPLIT UNTIL CLIMB POWER WAS REACHED. ALL INDICATIONS SHOWED NORMAL THEN. CREW CONTACTED MAINTENANCE CONTROL VIA ARINC. DECISION WAS MADE TO DIVERT TO CLT WHERE THE FLJul 12, 1996 · N281AU · Boeing 7372B7 · Fuel Control/Turbine EnginesSDR USAASB96125Light · failedLAS - FL 623 - FLOOR TRACK EMERGENCY LIGHTS INOP AT ROW 22 DEF.MAINTENANCE REPLACED THE EMERGENCY LIGHT LENSE P/N 07912 AND BULB P/N0L3071BPEGPL AT ROW 22 DEF. OPS CHECK GOOD.(M)Jul 11, 1996 · N529AU · Boeing 7372B7 · Emergency LightingSDR USAASB96120Downlock Sensor · out of adjustCLT - FLT 1126 - ON GEAR EXTENSION, NOSE GEAR RED LIGHT REMAINED ILLUMINATED. CREW CYCLED GEAR WITH NO HELP. GEAR VISUAL CHECK INDICATED GEAR WAS DOWN. RED LIGHT FINALLY WENT OUT AND GREEN LIGHT ILLUMINATED. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTEJul 5, 1996 · N286AU · Boeing 7372B7 · Landing Gear Position and WarningSDR USAA960490Floor Beam · corrodedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS ON FLOOR BEAM UPPER FLANGE BS 986.5 LBL 27 INCHES TO RBL 52 INCHES. INSTALLED T-SECTION WITH REPAIR ANGLES AND STRAPS, REPAIRED PER EA NR 41243. (X)Jun 22, 1996 · N278AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960489Floor Beam · corrodedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS 1 INCH BY 1 INCH ON FLOOR BEAM BS 947.5 LBL 37 INCHES TO RBL 35 INCHES. INSTALLED T-CAP WITH REPAIR ANGLES, REPAIRED PER SRM 53-10-9. (X)Jun 22, 1996 · N278AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960488Stringer · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 5 INCH BY 3 INCH CORRODED AREA STR 27L BS 967 TO BS 972. INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3, FIGURE 1. CORROSION TASK NR: C53-208-01. CORROSION LEVEL: 2. (X)Jun 22, 1996 · N278AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA960487Floor Beam · corrodedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS ON FLOOR BEAM UPPER FLANGE BS 967 LBL 27 INCHES TO RBL 52 INCHES. INSTALLED T-SECTION WITH REPAIR ANGLES AND STRAPS, REPAIRED PER EA NR 41242. (X)Jun 22, 1996 · N278AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960486Floor Beam · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED SCREW HOLES ON FLOOR BEAM BS 328 22 INCHES RBL 36 INCHES RBL AND 42 INCHES RBL. REPLACED SECTION OF FLOOR BEAM AND INSTALLED ANGLES. REPAIRED PER TR 53-10-13. (X)Jun 22, 1996 · N278AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960485T-Cap · corrosionINT - DURING Q-CHECK VISUAL INSPECTION, FOUND T-CAP SURFACE CORROSION AT LBL 15, STA 1016. REMOVED PRE-EXISTING REPAIR, FABRICATED NEW REPAIR AND REPAIRED PER SRM 53-10-9. (X)Jun 22, 1996 · N278AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960484Keel Beam · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND FRETTING CORROSION 55 INCHES RIGHT KEEL BEAM LOWER CORD STA 672 TO STA 727. INSTALLED REPAIR STRAP, REPAIRED PER EA 41232. CORROSION TASK NR: C53-212-01. CORROSION LEVEL: 2. (X)Jun 22, 1996 · N278AU · Boeing 7372B7 · Fuselage Main, KeelSDR USAA960483Stringer · corrodedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 7 INCH BY 3 INCH CORRODED AREA, STR 25L, BS 967 TO BS 974. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR: C53-202-01. CORROSION LEVEL: 2. (X)Jun 22, 1996 · N278AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA960475Skin · crackedGSO - DURING 'WALKAROUND' VISUAL INSPECTION, FOUND .50 INCH CRACK IN EXTERIOR SKIN FORWARD GALLEY DOOR OUTER SKIN AT THE FORWARD UPPER CORNER OF THE LOWER HINGE CUT OUT. INSTALLED DOUBLER, REPAIRED PER TYPICAL REPAIR 52-10-01 A. (X)Jun 21, 1996 · N287AU · Boeing 7372B7 · Galley DoorsSDR USAASB96106Battery Pack · dischargedRDU - MAINTENANCE FOUND THE FORWARD ENTRY AND SERVICE DOOR EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE BATTERY PACK. (M)Jun 14, 1996 · N281AU · Boeing 7372B7 · Emergency LightingSDR USAASB96098Lamp · burned outRSW - FLT 989 - ON APPROACH INTO RSW AT GEAR EXTENSION, CAPTAIN FAILED TO GET NOSE GEAR LIGHT. CAPTAIN DID A GO-AROUND AND RELAMPED NOSE GEAR DOWNLIGHT. GEAR WAS CYCLED WITH NORMAL GEAR INDICATION. RELAMPED NOSE GEAR LIGHT. (X)Jun 10, 1996 · N286AU · Boeing 7372B7 · Landing Gear Position and WarningSDR USAASB96097Sensor · failedPIT - FLT 1898 - AT APPROXIMATELY 8,000 FEET, THE NR 4 LE SLAT GREEN LIGHT CYCLED ON AND OFF AFTER FLAPS WERE RETRACTED. CREW RECYCLED FLAPS WITH NO CHANGE. CAPTAIN DECIDED TO RETURN TO FIELD. FLT LANDED IN PIT WITH NO FURTHER INCIDENT. MAINTENANCE REPLACEJun 1, 1996 · N281AU · Boeing 7372B7 · Leading Edge Slat Position Indicating SystemSDR USAASB96095Engine · bird strikeMCI - FL 800 - FLIGHT WAS CLIMBING OUT OF MCI WHEN THE A/C STRUCK A DUCK AT 3,500 FEET WITH THE RIGHT ENGINE. FLIGHT RETURNED TO FIELD AS A PRECAUTIONARY MEASURE. ALL ENGINE INDICATIONS WERE NORMAL. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FUMay 30, 1996 · N266AU · Boeing 7372B7 · Turbine Engine Compressor SectionSDR USAASB96094Controller · malfunctionedPIT - FLT 1297 - AT 31,000 FEET, CREW RECEIVED A PRESSURIZATION WARNING HORN ON THE AUTOMATIC SYSTEM. CREW SWITCHED TO MANUAL PRESSURIZATION CONTROL AND DESCENDED TO 10,000 FEET. NO EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AND LANDED WITH NO FURTHERMay 30, 1996 · N271AU · Boeing 7372B7 · Cabin Pressure ControllerSDR 96ZZZM1015Outflow Vlv · malfunctionedPIT - FLT 1297 - AT 31,000 FEET, CREW RECEIVED A PRESSURIZATION WARNING HORN ON THE AUTOMATIC SYSTEM. CREW SWITCHED TO MANUAL PRESSURIZATION CONTROL AND DESCENDED TO 10,000 FEET. NO EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AND LANDED WITH NO FURTHERMay 30, 1996 · N271AU · Boeing 7372B7 · Pressure Regulator/Outflow ValveSDR USAA960463Skin · dentedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO 3 INCH DIAMETER DENTS IN EXT FUSELAGE SKIN BS 877-STRINGER 18R. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)May 25, 1996 · N279AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA960462Skin · creaseINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND CREASE IN EXTERIOR DOOR SKIN 6 INCHES LONG AFT CARGO DOOR (NEAR HANDLE). INSTALLED EXTERIOR SKIN REPAIR, REPAIRED PER TR 52-10-01 A. (X)May 25, 1996 · N279AU · Boeing 7372B7 · Cargo/Baggage DoorsSDR USAA960461Stringer · out of limitsINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND FASTENER HOLE EDGE DISTANCE OUT OF LIMITS (SHORT EDGE MARGIN) STR 18A, STA 727L, AFT LOWER HOLE. INSTALLED REPAIR ANGLE, REPAIRED PER EA 41124. (X)May 25, 1996 · N279AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA960460Keel Beam · corrosionINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 1 INCH BY 64 INCHES OF EROSION/FRETTING CORROSION ON LT/RT KEEL BEAM BS 663 - BS 727 W/W CUT OUT PANEL ATTACH FLANGES. INSTALLED REINFORCING/CHAFE STRIPS. REPAIRED PER EA 41139 SRM 51-10-1. (X)May 25, 1996 · N279AU · Boeing 7372B7 · Fuselage Main, KeelSDR USAA960459Frame · crackedINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND .50 INCH CRACKED FRAME, STA 312, STR 5L. INSTALLED DOUBLER, REPAIRED PER SRM 53-40-3, FIGURE 1. (XMay 25, 1996 · N279AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA960458Skin · crackedINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 1 INCH CRACK AT LOWER HINGE CUT OUT ON A/C AFT SERVICE DOOR SKIN. INSTALLED FUSELAGE SKIN REPAIR AND REPAIRED PER SRM 53-30-3. (X)May 25, 1996 · N279AU · Boeing 7372B7 · Service DoorsSDR USAA960457Stringer · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 9 INCH CORRODED AREA AFT CARGO BS 967-987 STRINGER 25L. INSTALLED STRINGER SPLICE AND REPAIRED PER SRM 53-10-3. (M)May 25, 1996 · N279AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA960456Stringer · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 10 INCH CORRODED AREA STRINGER 27L BS 948. CUT OUT CORRODED SECTION OF STRINGER FABRICATED NEW SECTION AND SPLICED BACK IN, REPAIRED PER SRM 53-10-3. (M)May 25, 1996 · N279AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA960455Skin · crackedINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 2.5 INCH LONG CRACK IN FUSELAGE SKIN AT LOWER AFT CORNER OF FORWARD SERVICE DOOR CUT OUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER TR 53-10-19, REV A. (X)May 25, 1996 · N279AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA960454Floor Beam · corrosionINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND CORROSION AT NUTPLATE ON T-CAP .50 INCH BY 1 INCH, STA 294.5 AT BL ZERO, T-CAP OF FLOOR BEAM. REMOVED CORRODED SECTION OF T-CAP, FABRICATED AND SPLICED IN NEW SECTION PER TR 53-10-04 B. (X)May 25, 1996 · N279AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960453Floor Beam · corrodedINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 1 INCH BY 2.50 INCH CORRODED AREA BS 328, RLB 21, FLOOR BEAM CAP. INSTALLED DOUBLER, REPAIRED PER TR 53-10-01 A. (X)May 25, 1996 · N279AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960452Cargo Door · dentedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH DENT BS 807 STRINGER 20R SKIN ON CARGO DOOR. INSTALLED DOUBLER REPAIRED PER SRM 52-00-3. (M)May 25, 1996 · N279AU · Boeing 7372B7 · Cargo/Baggage DoorsSDR USAA960451Web · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AFT ENTRY DOOR 3RD STOP FROM BOTTOM AFT END WEB. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. (M)May 25, 1996 · N279AU · Boeing 7372B7 · Passenger/Crew DoorsSDR USAA960450Floor Beam · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 986.5 FLOOR BEAM T-CAP 44 INCH LBL. INSTALLED STRAP REPAIR, REPAIRED PER TR 53-10-01A. (M)May 25, 1996 · N279AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAASB96084Ballast · failedFLT NR 1005 - MEM - AT CRUISE ALT AN ELECTRICAL SMELL DEVELOPED IN THE AFT GALLEY. CAPTAIN CONFIRMED UPON INSPECTION AND DIRECTED FA'S TO PULL ALL AFT GALLEY CIRCUIT BREAKERS. SMELL DISIPATED. DIVERTED TO MEM. MAINTENANCE REMOVED AND REPLACED BALLAST FOR NMay 11, 1996 · N269AU · Boeing 7372B7 · Buffet/GalleysSDR USAASB96078Fairing · not sealedFLT NR 2009 - CLT - HARMONIC SURGE FELT IN AIRFRAME DURING CLIMB-OUT AND TO A LESSER EXTENT IN CRUISE. THIS SURGE FELT MORE PRONOUNCED AT 180 TO 250 KNOTS. MX RESEALED WING TO BODY FAIRING LEFT SIDE. INSPECTED FLIGHT CONTROLS, FUSELAGE, AND GEAR. NO DEFECTMay 4, 1996 · N270AU · Boeing 7372B7 · Aerodynamic FairingsSDR USAA960417Floor Beam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROX 2 INCH BY 5 INCH AREA OF SURFACE CORROSION, FLOOR BEAM UPPER T-CAP, STATION 1016, RBL 1 TO RBL 6. CUT OFF ENTIRE T-CAP, FABRICATED NEW PART AND INSTALLED PER EA 41077. (M)Apr 30, 1996 · N277AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960416Floor Beam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 3 INCH BY 40 INCH AREA OF SURFACE CORROSION, FLOOR BEAM T-CAP STATION 967, LBL 22 TO RBL 32. REPLACED T-CAP, REPAIRED PER TR 53-10-05C. (M)Apr 30, 1996 · N277AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960415Floor Beaam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 40 INCH AREA OF SURFACE CORROSION, FLOOR BEAM UPPER T-CAP AT STATION 986.5 LBL 45 TO RBL 45. INSTALLED T-CAP SPLICE, REPAIRED PER SRM 53-10-05C. (M)Apr 30, 1996 · N277AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960414Skin · dentedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH BY .50 INCH DEEP DENT IN SKIN AT BS 891 BETWEEN STRINGER 22R AND STRINGER 23R. CUT OUT DAMAGE AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M)Apr 30, 1996 · N277AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA960413Skin · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK LOWER AFT CORNER FORWARD SERVICE DOOR CUTOUT OUTER SKIN AND BEAR STRAP, BS 324 WL 210 RBL 68. INSTALLED DOUBLERS, REPAIRED PER SRM 53-30-3 FIG 26. (M)Apr 30, 1996 · N277AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA960412Skin · dentedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND DENT 6 INCHES BY 1 INCHES AREA FUSELAGE SKIN BS 397 BETWEEN STRINGER 22L AND STRINGER 23L. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M)Apr 30, 1996 · N277AU · Boeing 7372B7 · Fuselage Main, Plate/Skin
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