Boeing 727-225

Service difficulty reports · 4,226

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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 = '727225'
  ORDER BY difficulty_date DESC"

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SDR FOTR2101904398Skin · debondedRT WING T/E NR 10 SPOILER UPPER SKIN IS DEBONDED. REMOVED DAMAGE, SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20, PARA 7, 11, 14, 15, AND 18. FABRICATED REPAIR FILLER 13.5" X 3.5" AND DOUBLER 15" X 5" FROM 7075T6 .025 PO 90010605 IAW SRM 51-40-20, PARA 8.Feb 21, 2011 · N815EA · Boeing 727225 · SpoilersSDR FDEA201102070486Altimeter · failedCLIMBING THROUGH 20,000 MSL STANDBY ALTIMETER INDICATED AN ALTITUDE THAT WAS 10,000 HIGHER THAN THE ACTUAL ALTITUDE AS INDICATED ON THE CAPTAIN'S AND F/O'S ALTIMETERS. REMAINED IN ERROR THROUGHOUT THE FLIGHT. UPON ARRIVAL FOUND STANDBY ALTIMETER INDICATINGFeb 7, 2011 · N469FE · Boeing 727225 · Altimeter, Barometric/EncoderSDR CA110106009Check Valve · frozenAIRCRAFT FAILED TO PRESSURIZE ON DEPARTURE. DUMPED FUEL AND RETURNED. MAINTENANCE GROUND RAN AIRCRAFT, CARRIED OUT PRESSURIZATION CHECKS, NO FAULTS FOUND. AIRCRAFT PRESSURIZED NORMALLY TO MAX DIFF SUBSEQUENT FLIGHTS COMPLETED WITH NO FURTHER PROBLEMS SUSPEJan 5, 2011 · Boeing 727225 · Cabin Pressure Control SystemSDR FDEA201012294773Battery Pack · inoperative"EMERGENCY EXIT LIGHTS BATTERIES ARE DEAD. LIGHTS WON'T TEST." REPLACED BATTERIES IN BOTH PORTABLE EMERGENCY LIGHT ASSY IAW AMM 33-50-101-2-0. (CLOSED)Dec 29, 2010 · N462FE · Boeing 727225 · Emergency LightingSDR FDEA201012244751Switch · out of adjustAFT AIRSTAIR " LIGHT ILLUMINATED FOR 10 MINS, THEN BECAME INTERMITTENT NO BUFFET FELT AT ANY TIME. FOUND UPPER DOOR HANDLE SWITCH OUT OF ADJUSTMENT. ADJUSTED IAW MM 52-70-001-5. CHECKED GOOD.Dec 24, 2010 · N469FE · Boeing 727225 · Door Warning SystemSDR FDEA201012244750Switch · out of adjustAT FL 360" AFT AIRSTAIR " LIGHT ILLUMINATED FOR 10 MINS, THEN BECAME INTERMITTENT NO BUFFET FELT AT ANY TIME. FOUND UPPER DOOR HANDLE SWITCH OUT OF ADJUSTMENT. ADJUSTED IAW MM 52-70-001-5. CHECKED GOOD.Dec 24, 2010 · N469FE · Boeing 727225 · Door Warning SystemSDR FDEA201012014531Control Valve · failedACFT DID NOT PRESSURIZE AFTER TAKEOFF. OUTFLOW VALVE SHOWED CLOSED, CARGO HEAT OUTFLOW CLOSED. ALL DOOR LIGHTS INDICATED CLOSED. PRESSURIZATION SYS APPEARED TO BE WORKING, NORMAL OTHERWISE. ALSO COULD NOT GAIN CONTROL IN STBY MODE. RESEALED NOSE GEAR ADec 1, 2010 · N466FE · Boeing 727225 · Cabin Pressure Control SystemSDR FDEA201011274497Flap System · malfunctionedAT FLAPS 2 POSITION THE AMBER L/E FLAPS LIGHT STAYS ILLUMINATED. L/E DIVICES POSITION INDICATOR SHOWS NORMAL LED CONFIGURATION. RELEASED FOR SERVICE IAW MEL: 27-06-C CATEGORY: C EXPIRATION: 07DEC10 "MEL 27-06-C: AMBER L/E FLAPS LIGHT ON THE FWD INSTRUMENTNov 27, 2010 · N466FE · Boeing 727225 · Leading Edge Slat Control SystemSDR FDEA201011174401Window · crackedL-1 WINDOW CRACKED AND ARCED AT FL 210 DURRING CLIMB OUT. NO WEATHER AS AN ISSUE. SMOOTH AIR AND CLEAR SKIES. 3-4 CRACKS ALL ON OUTER PANE. REMOVED AND REPLACED L-1 WINDOW IAW AMM 56-11-011-4. WINDOW HEAT TEST CHECKED NORMAL IAW 30-41-033-4 RII 236332 R/C ANov 17, 2010 · N463FE · Boeing 727225 · Flight Compartment WindowsSDR C8GA2010000075Warning Light · false activationAFTER TAKE-OFF, 30 MINUTES INTO FLIGHT THE NR 3 ENGINE OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED AND REMAINED ON. THE OIL PRESSURE, TEMPERATURE AND QUANTITY WERE ALL WITHIN LIMITS ENGINE WAS SHUTDOWN IN FLIGHT. POSITIVE OIL PSI WAS MAINTAINED AND THE ACFT LNov 17, 2010 · N755DH · Boeing 727225 · Engine Oil Indicating SystemSDR C8GA2010000074Filter · warning lightDURING CRUISE OPERATION AT FL320 THE NR3 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. ENGINE WAS SHUTDOWN, POSITIVE OIL PRESSURE WAS MAINTAINED AND ACFT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. R & R MAIN OIL FILTER, DRAINED AND FLUSHED ENGINE Nov 15, 2010 · N755DH · Boeing 727225 · Engine Oil Indicating SystemSDR C8GA2010000073Indicator · malfunctionedON TAKEOFF ROLL, THE NR1 EPR INDICATION PEGGED. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE BLOCKS. HIGH ENERGY INSP WAS PERFORMED. R & R THE NR1 EPR INDICATOR, OPS CHECK GOOD. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Nov 10, 2010 · N815EA · Boeing 727225 · Engine Pressure Ratio (EPR)SDR FDEA201010264174Valve · inoperativeRT AIR MIX VALVE STUCK FULL COLD. FOLLOWED BY LOSS OF CABIN PRESSURIZATION. RAN PACKS INDIVIUALY AND TOGETHER. PERFORMED LEAK CK OF DUCTS, PACKS, MIX VLVS. NO DEFECTS NOTED. PERFORMED BITE TEST OF 35 DEG VALVE AND WATCHED VALVES OPERATE. PULLED C/B ON Oct 26, 2010 · N466FE · Boeing 727225 · Cabin Pressure Control SystemSDR FDEA201010244160Structure · crackedLEFT WING, I/B FLAP, MID FLAP T/E LWR CHORD HAS A CRACK , O/B OF NO. 4 FLAP TRACK. REMOVED CRACKED T/E LOWER CHORD SECTION DIM 69 1/2" IN LENGTH IAW SRM 51-30-2 LOCATED AND DRILLED NEW CHORD SECTION FROM BAC1503-100046 7075 T6 DIM 69 1/2" IN LENGTH IAW SROct 24, 2010 · N467FE · Boeing 727225 · Trailing Edge FlapsSDR FDEA201010234157Stringer · corrodedCORROSION ON STRINGER 27R BSTA 1083. CUT-OUT DAMAGED STRINGER 27R SECTION DIM. 53 7/8" LONG BETWEEN BS 1079 TO 1133. FABRICATED NEW STRINGER SECTION FROM BAC 1498-145 7075T62 DIM. 53 7/8" AND FABRICATED 3EA SPLICE REPAIRS FROM BAC 1498-131 7075T6 DIM. 14" ANDOct 23, 2010 · N467FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201010184171Skin · gougedMCD INNER SURROUND SKIN GOUGED STA 480 STR 16L. CUT-OUT DAMAGED AREAS APPROX DIM. 1.1" X 0.900", FABRICATED FILLERS APPROX DIM. 1.1" X 0.900" AND REPAIR DOUBLER APPROX DIM. 14" X 3.2", INSTALLED FILLERS AND REPAIR DOUBLER IAW EA 7-5330-143910 AT MCD INNER SUOct 18, 2010 · N467FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201010184170Skin · gougedMCD INNER SURROUND SKIN HAS NUMEROUS GOUGES STA 620 STR 12L TO 17L. CUT-OUT DAMAGED AREAS 1.25" X 1.1", FABRICATED FILLERS APPROX DIM. 1.25" X 1.1" AND DOUBLER REPAIR APPROX DIM. 18.5" X 3.1", INSTALLED FILLERS AND DOUBLER REPAIR IAW EA 7-5330-143910 AT MCD Oct 18, 2010 · N467FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201010184107Skin · gougedMCD INNER SURROUND SKIN GOUGED STA 480, STR 8L. REMOVED GOUGED INNER SKIN DIM. 22" X 11" AT BS 480 STR 8L IAW SRM 51-30-2. FABRICATED NEW INNER SKIN FROM 2024 T-3 0.125" DIM. 22" X 11" IAW SRM 53-10-2 FIG 3A. INSTALLED NEW INNER SKIN IAW SRM 51-30-2 REV 103.Oct 18, 2010 · N467FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201010174106Skin · gougedMCD INNER SURROUND SKIN HAS NUMEROUS GOUGES STA 620 STR 4L TO 8L. REMOVED MAIN CARGO DOOR INNER SKIN UPPER AFT SECTION IAW SRM 51-30-2, FABRICATED INNER SKIN MATERIAL USED 2024T3 .125" PO 20110320 DIM 79" X 48" IAW SRM 53-10-2 FIG 3A. TREATED AND PRIMED IAOct 17, 2010 · N467FE · Boeing 727225 · Cargo/Baggage DoorsSDR FDEA201010154102Frame · damagedFUSELAGE INTERIOR BS 1176 -9 CHORD HAS 4 OPEN FASTENER HOLES BETWEEN LBL 17.5 AND RBL 17.5 WITH LOW EDGE DISTANCE AND NO EDGE DISTANCE. COMPLIED WITH EA 7-5310-143902 , INSTALLED NEW CHORD SECTION P/N 5310212 DIM. 65.5" LONG, AND FABRICATED AND INSTALLED 2Oct 15, 2010 · N467FE · Boeing 727225 · Fuselage Main, BulkheadSDR FDEA201010144066Seat Track · corrodedSEAT TRACK AT BS 1050 RBL 45.5 HAS CORROSION. REMOVED, FABRICATED, AND REPLACED NEW SEAT TRACK SECTION BS 1000 TO 1070 RBL 45.5 APPROX DIM 69.50" FROM BAC1520-792 7178T6 AND SPLICE REPAIR IAW SRM 53-10-5 FIG 1 AND 51-30-2. INSTALLED REPAIR PARTS IAW SRM 51-3Oct 14, 2010 · N467FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010134098Stringer · corrodedAFT PIT BS 1173 STRINGER AT 22L IS CORRODED. REMOVED DAMAGED STRINGER SECTION DIM. 25 3/8" IAW B727 SRM 53-10-3 AND 51-30-2. FABRICATED NEW STRINGER SECTION FROM BAC1498-144 7075T6 DIM. 25 3/8" AND SPLICE FROM BAC1498-132 7075T6 DIM. 14 3/4" IAW SRM 53-10-2Oct 13, 2010 · N467FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201010124032Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 1166 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED CORRODED SHEAR TIE AT BS 1166, STRINGER 28R TO 27R IAW SRM 51-30-2 REV 103Oct 12, 2010 · N467FE · Boeing 727225 · Fuselage Internal Mounting StructureSDR FDEA201010124024Web · gougedC-1 DOOR CUTOUT AFT FRAME BS 620 WEB IS GOUGED ON FWD SIDE AT STR 22R BETWEEN DOOR STOPS NR 3 AND NR 4. REMOVED C-1 DOOR AFT FRAME WEB IAW SRM 51-30-2 FABRICATED NEW FRAME WEB FROM 7075 T6 .071" DIM 106" X 6" IAW 53-10-2 FIG 3 AND 51-30-5 INSTALLED NEW FOct 12, 2010 · N467FE · Boeing 727225 · Fuselage Main, StructureSDR FDEA201010124099Skin · corrodedBULGE EXTERIOR FUSELAGE BS 1183-1176 STR 22L AT AFT LAV SERVICE PANEL. REMOVED INNER DOUBLER IAW SRM 51-30-2. FABRICATED NEW INNER DOUBLER FROM 7075T6 0.071" DIM. 20" X 20" IAW SRM 51-30-5 AND DWG 65-25607. INSTALLED NEW INNER DOUBLER IAW SRM 51-30-2 AT EXTOct 12, 2010 · N467FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201010124031Frame · corrodedCORROSION AT FASTENER HOLE ON UPPER FLANGE OF FRAME AT BS 950C BETWEEN STRINGERS 28R AND 27R. CUT OUT DAMAGED AREA DIM 1 1/4" X 1" IAW SRM 51-40-3 FIG 1, FORMED REPAIR DOUBLER IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1 INSTALLED REPAIR DOUBLER IAW SRM 5Oct 12, 2010 · N467FE · Boeing 727225 · Fuselage Main, FrameSDR FDEA201010124030Frame · puncturedAFT CARGO COMPARTMENT, FRAME AT BS 1090 ABOVE STR 27R HAS PUNCTURE IN THE UPPER FLANGE WITH MATERIAL LOSS ON THE LOWER SURFACE .5" IN DIAMETER. CUT OUT DAMAGED AREA OF FRAME DIM 1" X 1" IAW SRM 51-40-3 FIG 1 FORMED FRAME REPAIR DOUBLER IAW SRM 51-40-3 FIG 1Oct 12, 2010 · N467FE · Boeing 727225 · Fuselage Main, FrameSDR FDEA201010124022Skin · corrodedCORROSION ON SKIN AT BS 660 BETWEEN STRINGERS 28L AND 28R CUT OUT DAMAGED AREA DIM. (8" X 73/4") IAW SRM 53-30-3 FIG 1. FABRICATED DOUBLER IAW SRM 53-30-3 FIG 1 AND 53-30-2 FIG 2, TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED REPAIR PARTS, DOUBLER AND FILLER IOct 12, 2010 · N467FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR C8GA201000054AIndicator · inoperativeFLT 719 FROM FLL TO TOL. DURING CLIMB OPERATION THE AIRCRAFT WOULD NOT PRESSURIZE. THE AIRCRAFT RETURNED TO FLL WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED NOTING THAT THE AFTER ENTRY DOOR WAS UNLATCHED. DOOR WAS CLOSED,AND IDENTIFIOct 1, 2010 · N801EA · Boeing 727225 · Door Warning SystemSDR C8GA201000047Skin · dentedWHILE IN HEAVY MX PERFORMING INSP, A DENT WAS NOTED AT LAP SEAM STA 520, STRINGER 26R. REMOVED DAMAGED AREA, PERFORMED HFEC INSP, NO CRACKS NOTED. FABRICATED DOUBLER 12" X 11" FROM 2024 T3 .090" AND FILLERS 4" X 3" (2) FROM 2024 T3 .080". INSTALLED REPAIR, Sep 12, 2010 · N755DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201009023244Relay · burnedDURING COCKPIT PREFLIGHT, NOTICED HEAVY WHITE SMOKE COMING FROM OVERHEAD CONTROL PANEL. ADVISED 2ND OFFICER TO REMOVE ELECTRICAL POWER FROM ACFT. ADVISED CREW TO EVACUATE. INSP O/H PANEL AREA & FOUND NO SIGNS OF BURNED WIRES, SWITCHES, CONNECTOR'S OR RELAYSSep 2, 2010 · N469FE · Boeing 727225 · Light System WiringSDR FDEA201008313206Light · looseEMERGENCY EXIT LIGHT IN COCKPIT POPS OUT OF ITS HOUSING ON ROTATION AND LANDING. FOUND LIGHT NOT PROPERLY SET, RE-SET SAME, OPS CHECK NORMAL AND NOW IS SECURE. ACCOMPLISHED IAW MM 33-50-101-2-0.Aug 31, 2010 · N465FE · Boeing 727225 · Emergency LightingSDR FDEA201008313205Light · damagedCOCKPIT EMERGENCY EXIT LIGHT DOES NOT TEST ON PRE-FLIGHT. R & R COCKPIT EMERGENCY LIGHT ASSY IAW AMM 33-50-101-2-0, OPS CHECKS GOOD. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION. R & R COCKPIT EMERGENCY LIGHT ASSY IAW AMM 33-50-101-2-0, OPS CHECKS GOOD. Aug 31, 2010 · N465FE · Boeing 727225 · Emergency LightingSDR C8GA201000046Doubler · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT 2 EA DOUBLER'S REQUIRE REPLACEMENT IAW SB 53A0198R3, AD 2007-12-14 ON THE FUSELAGE AT THE FWD ENTRY DOOR UPPER AND LOWER HINGE CUTOUTS. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 30, 2010 · N755DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR C8GA201000045Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STRINGER 24 R IS CORRODED AT STA 316 TO 335. CUT OUT DAMAGED AREA, FABRICATED NEW STRINGER FROM BAC1498-140. INSTALLED REPAIR PARTS, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 30, 2010 · N755DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR C8GA201000043Web · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT IN THE AFT CARGO COMPARTMENT NR 2 DOOR 2ND WEB FROM LOWER EDGE, APPROX 24" FROM FWD EDGE OF DOOR IS CORRODED. CUT OUT DAMAGE 10" X 4.5"' FABRICATED FILLER FROM 7075 T6 .063"10" X 4.5", FABRICATED DOUBLER FROMAug 30, 2010 · N755DH · Boeing 727225 · Cargo/Baggage DoorsSDR C8GA201000042Web · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT LT AFT CABIN FLOOR WEB AT STA 1170, LBL 26 IS CORRODED. REMOVED DAMAGE, FABRICATED DOUBLER FROM 7075 T6 .071" DIM 12" X 22". INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 30, 2010 · N755DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR C8GA201000041Keelbeam · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT CTR FUSELAGE FWD KEELBEAM AT STA 777.65 AT WEB HOLE EDGE CORRODED. ROUTED OUT DAMAGE, FABRICATED DOUBLER REPAIR FROM 7075-0 .125" HEAT TREATED TO 7075 T6, INSTALLED REPAIR. NO OTHER DEFECTS NOTED. ACFT WAAug 30, 2010 · N755DH · Boeing 727225 · Fuselage Main, KeelSDR C8GA201000040Floor Support · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT FLOORBEAM BELOW FLOOR SUPPORT HAS CORROSION AT STA 1130 AT RBL 0. FABRICATED NEW ANGLE REPAIR FROM 7075 T6 .050" 12" X 3". INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 30, 2010 · N755DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR C8GA201000039Frame · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT FRAME IS CORRODED AT STA 1149 BETWEEN STRINGER 25L-26L. REMOVED DAMAGE, FABRICATED REPAIR FROM 7075-0 HEAT TREATED TO T6 2" X 12", INSTALLED REPAIR. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 30, 2010 · N755DH · Boeing 727225 · Fuselage Main, FrameSDR C8GA201000038Stringer Clip · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE STRINGER TIE FITTING IS CORRODED AT STRINGER 18L STA 1183. REMOVED, FABRICATED AND INSTALLED TIE CLIP. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 30, 2010 · N755DH · Boeing 727225 · Fuselage Main, Attach FittingsSDR C8GA201000037Attach Fitting · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSP, IT WAS NOTED THAT FLOOR SUPPORT FITTING TO BULKHEAD AT STA 1183 RBL 28 BELOW FLOOR IS CORRODED. FABRICATED NEW PLATE FROM 7075 T6 .090" 6" X 12", INSTALLED REPAIR NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICEAug 30, 2010 · N755DH · Boeing 727225 · Fuselage Main, Attach FittingsSDR C8GA201000036Stringer Clip · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT STRINGER 18R & 19R HAVE 2EA STRINGER TIES THAT ARE CORRODED. TIES ARE OUT OF LIMITS, R & R STRINGER END FITTINGS AT 1183. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 30, 2010 · N755DH · Boeing 727225 · Fuselage Main, Attach FittingsSDR C8GA201000035Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STRINGER 28L IS CORRODED OUT OF LIMITS AT STA 680-700. CUT OUT DAMAGED AREA OF STRINGER, FABRICATED REPAIR SPLICE FROM BAC 1498-131 12.25" & 16" LONG, STRINGER 65-56236-22. INSTALLED REPAIRS, NO OTHER DEFECTAug 30, 2010 · N755DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR C8GA201000034Skin · dentedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT A 2 EA DENTS ON THE RT WING UPPER L/E STA 160 ARE OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED FILLER AND DOUBLER FROM 2024 T3 .050" 2" X 3" & 2.5" X 5.25". INSTALLED REPAIRS, NO OTHER DEFECTS NOTED. ACFT WAS Aug 30, 2010 · N755DH · Boeing 727225 · Wing, Plate/SkinSDR C8GA201000033Skin · dentedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT A DENT AT FUSELAGE STA 495, STRINGER 27R IS OUT OF SRM LIMITS. FABRICATED DOUBLER FROM .063" 2024 T3 DIM 9.25" X 7.5", INSTALLED REPAIR NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 30, 2010 · N755DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR C8GA201000032Beam · corrodedWHILE IN HEAVY MX, PERFORMING INSP IT WAS NOTED THAT THE RT MLG BEAM AND OTBD SUPPORT FITTING BORES ARE CORRODED. REMOVED CORROSION, HFEC, SHOT PEENED, INSTALLED BUSHING AND SPACER. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 30, 2010 · N755DH · Boeing 727225 · Wing, Landing Gear Attach FittingsSDR C8GA2010000029Bulkhead · corrodedWHILE IN HEAVY MX PERFORMING INSP, THE INTERNAL CABIN AFT PRESSURE BULKHEAD RT STATION 1183 LOWER LOBE WEB WAS CORRODED. FABRICATED LOWER LOBE WEB FROM 2024 T3 .040" R & R LOWER LOBE, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 24, 2010 · N755DH · Boeing 727225 · Fuselage Main, BulkheadSDR C8GA2010000028Hinge · crackedWHILE IN HEAVY MX PERFORMING INSP, THE MAIN CARGO DOOR AFT HINGE LOBE IS CRACKED. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 24, 2010 · N755DH · Boeing 727225 · Fuselage, Door HingeSDR C8GA2010000027Support Fitting · corrodedWHILE IN HEAVY MX PERFORMING INSP, CORROSION WAS NOTED ON THE SUPPORT FITTING ATTACHED TO THE SHEAR WEB LOWER SIDE STA 1175 LBL 30. REMOVED AND FABRICATED NEW SUPPORT FITTING FROM BAC1520-792. INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SAug 24, 2010 · N755DH · Boeing 727225 · Fuselage Miscellaneous Structure
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