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"

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 C8GA2010000026Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP, CORROSION WAS NOTED ON THE STRINGER 29L STATION 950B. REMOVED CORROSION FROM STRINGER, FABRICATED REPAIR STRAP FROM 7075 T6 .063" 8.5" INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 24, 2010 · N755DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR C8GA2010000025Shear Tie · corrodedWHILE IN HEAVY MX PERFORMING INSP CORROSION WAS NOTED ON THE SHEAR TIE FRAME STA 950B STRINGER 29L. REMOVED CORROSION FROM SHEAR-TIE, FABRICATED REPAIR STRAP FROM 7075 T6 .063" INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 24, 2010 · N755DH · Boeing 727225 · Fuselage Internal Mounting StructureSDR C8GA2010000024Support Angle · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE AFT CARGO, AFT BULKHEAD , RT SIDE, OTBD CEILING FLOOR TO BULKHEAD ATTACH SUPPORT HAS CORROSION. REMOVED AND FABRICATED NEW FLOOR TO BULKHEAD SUPPORT ANGLE FROM 2024-0 HEAT TREATED TO T3 AND INSTALLED ANGLAug 24, 2010 · N755DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR C8GA2010000023Support · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE AFT CARGO, AFT BULKHEAD , RT SIDE, OTBD CEILING FLOOR TO BULKHEAD ATTACH SUPPORT HAS CORROSION. REMOVED AND FABRICATED NEW FLOOR TO BULKHEAD SUPPORT ANGLE FROM 2024-0 HEAT TREATED TO T3 AND INSTALLED ANGLAug 24, 2010 · N755DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR C8GA2010000022Attach Fitting · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE AFT CARGO, AFT BULKHEAD , RT SIDE, OTBD CEILING FLOOR TO BULKHEAD ATTACH SUPPORT HAS CORROSION. R & R SUPPORT FITTING. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Aug 24, 2010 · N755DH · Boeing 727225 · Fuselage Main, Attach FittingsSDR C8GA2010000021Skin · corrodedWHILE IN HEAVY MX, PERFORMING INSP, IT WAS NOTED THAT THE LOWER FUSELAGE LT SIDE AT BS 950C - 1010. REMOVED DAMAGED AREA BS 950E TO 950F, STR 25L-26L 3" X 1" & 2" X 1", ALSO 950 F TO 970 BETWEEN BETWEEN STRINGER 24L-25L 7" X 2.5" AND 970 TO 990 BETWEEN 24L-25Aug 24, 2010 · N755DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR C8GA2010000020Duct · corrodedWHILE IN HEAVY MX INSP, IT WAS NOTED THAT CORROSION WAS NOTED ON THE CTR ENGINE AIR DUCT AT THE LOWER PRODUCTION BREAK. FABRICATED NEW SPLICE STRAP FROM 301.2500 HD .063" NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 24, 2010 · N755DH · Boeing 727225 · Engine Air Intake SystemSDR C8GA2010000019Support Fitting · crackedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE RT WING LANDING GEAR REAR TRUNNION SUPPORT BEAM AT REAR SPAR ATTACH POINT FITTING IS CRACKED APPROX. .4375". MODIFIED FITTING IAW THE SB 57-0153, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 24, 2010 · N755DH · Boeing 727225 · Wing, Landing Gear Attach FittingsSDR C8GA2010000018Failsafe · corrodedWHILE IN HEAVY MX PERFORMING INSPECTIONS, IT WAS NOTED THAT THE RT SIDE OF HORIZ STABILIZER REAR SPAR UPPER CHORD FAIL SAFE STRAP HAS SURFACE CORROSION. R & R STRAP PN 65-16876-50. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Aug 23, 2010 · N755DH · Boeing 727225 · Horizontal Stabilizer StructureSDR C8GA2010000017Skin · dentedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE FUSELAGE HAS (2EA) DENTS LOCATED BETWEEN BS 196 TO 203 AT S 23L. CUT OUT DAMAGED AREA 9.75" BY 2.75", PERFORMED NDT INSP, FABRICATED DOUBLER FROM 2024 T3 .050" 13" X 9" AND INSTALLED DOUBLER REPAIR NO OTAug 23, 2010 · N755DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR C8GA2010000016Skin · corrodedWHILE IN HEAVY MX PERFORMING INSPECTIONS CORROSION WAS NOTED AT THE LT WING, LOWER SKIN FWD OF FRONT SPAR WS 250-287 BEHIND THE NR1 & NR2 KRUGER FLAP. CORROSION FOUND TO BE OUT OF LIMITS. PERFORMED BLEND-OUT IAW RES-W1 NR 2002564-12 LOSS OF MATERIAL IS .095"Aug 23, 2010 · N755DH · Boeing 727225 · Wing, Plate/SkinSDR ABXR2010081100037Intercostal · damagedDURING A STORM DAMAGE REPAIR MX EVENT & DURING A SKIN REPLACEMENT AN INTERCOSTAL WAS DISCOVERED WITH MULTIPLE HOLES IN THE RADIUS. FABRICATED NEW INTERCOSTAL AND INSTALLED. ITEM RETURNED TO SERVICE.Aug 11, 2010 · N801EA · Boeing 727225 · Fuselage Miscellaneous StructureSDR ABXR2010081100036Skin · dentedDURING A STORM DAMAGE REPAIR MX EVENT A DENT WAS DISCOVERED ON THE RT WING L/E. DENT WAS SMOOTH AND FREE FROM SHARP CREASES LOCATED ON THE LOWER SURFACE AND MEASURED 4.00" LONG X 1.20' WIDE 0.162 DEEP. THE DENT WAS COLD WORKED BACK TO ITS ORIGINAL SHAPE AND CAug 11, 2010 · N801EA · Boeing 727225 · Wing, Plate/SkinSDR ABXR2010081100035Fairing · crackedDURING A HEAVY MX INSP, EVENT THE RT WING OTBD FLAP, OTBD FLAPTRACK AFT FAIRING WAS FOUND TO BE CRACKED AND DENTED. R & R FAIRING. ITEM RETURNED TO SERVICE.Aug 11, 2010 · N801EA · Boeing 727225 · Trailing Edge FlapsSDR ABXR2010081100034Fairing · crackedDURING A HEAVY MX EVENT THE RT WING OTBD FLAP, INBD FLAP TRACK, FWD FAIRNG WAS FOUND TO BE CRACKED AND DENTED. R & R FAIRING. ITEM RETURNED TO SERVICE.Aug 11, 2010 · N801EA · Boeing 727225 · Trailing Edge FlapsSDR ABXR2010081100033Fairing · cracked(ABXR) DURING A HEAVY MX INP EVENT, THE RT WING OTBD FLAP, INBD FLAP TRACK, FWD FAIRING WAS FOUND TO BE CRACKED AND DENTED. R & R FAIRING. ITEM RETURNEDTO SERVICE.Aug 11, 2010 · N801EA · Boeing 727225 · Trailing Edge FlapsSDR ABXR2010081100032Bracket · misalignedDURING A HEAVY MX, THE NR 7 SLAT ACTUATOR NOT ALIGNING WITH NR 7 SLAT MOUNT POINT DUE TO SLAT ACTUATOR MOUNTING BRACKET HOLE LOCATIONS WITH INCORRECT DIMENSIONS. R & R BRACKET. ITEM RETURNED TO SERVICE.Aug 11, 2010 · N801EA · Boeing 727225 · Wing, Attach FittingsSDR FDEA201008062865Stringer · misrepairedILLEGAL REPAIR (STRINGER) STR 27L BS 540 - BS 560 FWD PIT. CUT OUT STRINGER SECTION FROM STA 550 TO 590 STR 27L IAW SRM 53-10-3 FIG 1. FAB REPAIR PARTS HAT SECTION MAT USED BAC1498-141 7075-T6 2 EA DIM 21" LONG AND 22" LONG. 2 EA SPLICERS, MAT USED BAC1498-13Aug 6, 2010 · N466FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR CA100810005Clamp · damaged(CAN) WHILE CLIMBING THROUGH 4500 FT, ENGINE FIRE/WHEEL WELL FIRE BELL RANG. THERE WERE NO FIRE INDICATION LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO DEPARTURE. TROUBLESHOOTING WAS PERFORMED BY MAINTENANCE PERSONNEL AND IDENTIFIED THE NR 1 ENGINE PYLON CLAug 5, 2010 · Boeing 727225 · Pneumatic Distribution SystemSDR CA100810004Line · leaking(CAN) WHILE PERFORMING THE ACFT DAILY INSP, MX DISCOVERED A HYD LEAK IN THE NR 2 ENGINE "A" SYS RETURN HYDR LINE AT THE ENGINE FIREWALL BULKHEAD IN THE RT AFT AIRSTAIRS AREA. THE HYD LINE WAS R & R WITH A TEMPORARY FLEXIBLE LINE IAW THE ACFT MM AND COMPANY PRAug 5, 2010 · Boeing 727225 · Hydraulic System, MainSDR FDEA201008042813Stringer · corrodedFWD CARGO COMPARTMENT STR 23R CORRODED BELOW FRAME AT BS 720E. FOUND DURING CLEANING. CUT OUT DAMAGED SECTION OF STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER REPAIR FROM BAC 1498 -144, 7075-T6 DIM 16 1/4", SPLICES FFROM BAC 1498-132, 7075-T6, DIM 16 1/Aug 4, 2010 · N466FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201008032789Skin · gougedMCD INNER SURROUND SKIN GOUGED STA 620-630, STR 16L. REPAIRED MCD INNER SURROUND SKIN IAW EA 7-5330-135571.Aug 3, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201008032934Skin · crackedLT HORIZ STAB HAS PROTRUDING DENT AT ELEV STA 140 WITH CRACK INDICATION. CUTOUT DAMAGED AREA DIM .7500" X .7500" AND FABRICATED REPAIR DOUBLER FROM 2024-T3, 0.032" DIM. 3" X 3" IAW SRM 55-20-3, FIG 4. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIRAug 3, 2010 · N466FE · Boeing 727225 · Horizontal Stabilizer, Plate/SkinSDR FDEA201007312747Skin · crackedBS 1290 LIGHTNING HOLE HAS CRACK LBL18 TRIMMED OUT DAMAGE DIM. 1" X 1" AND FABRICATED REPAIR DOUBLER FROM 7075-T6 0.032" DIM. 3 1/2" X 21/2" IAW SRM 51-40-2 FIG. 1. TREATED, PRIMED AND INSTALLED DOUBLER AT BS 1290 LIGHTING HOLE LBL 18 IAW SRM 51-10-2, 51-30-2,Jul 31, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201007312853Seat Track · corrodedSEAT TRACK AT BS 760 TO 789 RBL 45 IS CORRODED. REMOVED SEAT TRACK AND TEE SECTION BS 760 TO BS 848 RBL 45 IAW SRM 51-30-2. LOCATED AND DRILL NEW TEE SECTION FROM BAC1506-1108 7075-T6 DIM. 110" LONG IAW SRM 53-10-2 FIG. 7 AND 51-30-5. TREATED AND PRIMED NEW Jul 31, 2010 · N466FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201007302734Support · crackedMAIN CARGO COMPARTMENT INNER UPPER, DOOR FRAME SUPPORT FASTENER HOLE CRACKED STA 620. REPAIRED MAIN CARGO COMPARTMENT INNER UPPER DOOR FRAME SUPPORT STA 620 IAW EA 7-5310-135576.Jul 30, 2010 · N466FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA201007302733Skin · gougedMCD INNER SURROUND SKIN GOUGED STA 620 STR 4L. REMOVED MCD INNER SKIN AFT UPPER SECTION BS 620 STR4L IAW SRM 51-30-2. FABRICATED NEW MCD INNER SKIN SECTION FROM 2024 T3 0.125" DEMINSION 79" X 48" IAW SRM 53-10-2 FIGURE 3A REV J. TREATED AND PRIMED AND INSTALLJul 30, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201007302732Floorbeam · damagedFLOORBEAM HAS DOUBLE DRILL HOLES BS 480 LBL 45. OVERSIZED HOLES TO 5/32" AND INSTALLED FASTENERS IAW SRM 51-30-5. WITHIN LIMITS IAW SRM 53-10-1 FIGURE 4B.Jul 30, 2010 · N466FE · Boeing 727225 · Fuselage Main, Floor BeamSDR FDEA201007292715Seat Track · corrodedSEAT TRACK CORRODED STA 620 - 660 LBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792 7178-T651 DIM. 17.5 FT. IAW SRM 53-*10-2 FIG 7A REV J AND SRM 51-30-5. TREATED, PRIMED AND INSTALLED MAIN CABIN SEAT TRACK SECTIJul 29, 2010 · N466FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201007292714Frame · corrodedCORROSION ON UPPER FLANGE OF FRAME AT BS 1148 BETWEEN STRINGER 27L AND 26L. REMOVED CORROSION. ORIGINAL MATERIAL THICKNESS .063, MATERIAL LOSS .003. FOUND WITHIN LIMITS IAW SRM 53-10-1 AND 53-10-2.Jul 29, 2010 · N466FE · Boeing 727225 · Fuselage Main, FrameSDR FDEA201007292720Skin · gougedMCD INNER SURROUND SKIN GOUGED STR 620 STR 8L. BLENDED OUT DAMAGE AND FOUND ORIGINAL MAT 0.125", REMAINING MATERIAL 0.115", MATERIAL LOSS 0.010", REMOVED INNER SKIN SPLICE AND FABRICATED NEW SECTION FROM 2024-T3 0.125" DEMENSION 22"X11" IAW SRM 51-30-2 AND SRJul 29, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201007282738Skin · chafedBS 720B, 8" RBL 2 RAM AIR DUCT STIFFENING BOLT CHAFING HOLE IN FUSELAGE SKIN. CUT OUT DAMAGED AREA FUSELAGE SKIN BS 720C 8 RBL2. DIMENSIONS (1 3/8" X 1 3/8") IAW SRM 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER MAT USED 2024 T3 .125" DIM (12 1/4" X 9 7/8") ANDJul 28, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201007282703Skin · misinstalledFWD CARGO COMPARTMENT, STRINGER 25L HAS SEVERAL FASTENERS IMPROPERLY INSTALLED FROM STA 540-600. CUT-OUT SKIN DOUBLER AND TRIPLER (6EA) BS 560 - 620 STR 25L DIM. 2 3/4" X 2 1/8" AND FABRICATED REPAIR FILLER FROM 2024-T3 0.125" DIM. 71.5" X 11.5", REPAIR DOJul 28, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201007282702Skin · corrodedFUSELAGE SKIN STA 1070 STR 28L HAS CORROSION AND FASTENER NO E.D. CUTOUT DAMAGED AREA DIMENSION 5 1/8" X 2 7/8" AND 4 1/8" X 1 1/8" AND FABRICATED REPAIR DOUBLER FROM 2024T3 .063 DIMENSION 28 1/2" X 9 1/2" AND FILLERS FROM 2024T3 .050 DIMENSION 5 1/8" X 2Jul 28, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201007272713Stringer · corrodedCORROSION ON STRINGER 27L AT BS 1100. REMOVED CORROSION. EVALUATED AREA ORIGINAL .063 MATERIAL LOSS .015 MATERIAL REMAINING .048 FOUND AREA TO BE OUT OF LIMITS. CUTOUT DAMAGED AREA APPROX DIM: 5". FABRICATED STRINGER FILLER FROM BAC 1498-145 7075T6 APPROX DIJul 27, 2010 · N466FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201007262704Stringer · damagedFASTENER HOLE IS ELONGATED IN STR 25L AT BS 520. CUT OUT DAMAGED SECTION OF STRINGER DIM. 16" LONG IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER REPAIR PARTS USING BAC1498-139 7075 T6 DIM 16" 7075 T6 .050" DIM. 10 1/4" X 5/8" (4 EACH), BAC1493-412 7075 T6 DIM Jul 26, 2010 · N466FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201007262687Stringer · corrodedCORROSION ON STRINGER 27L AT BS 720B. CUT OUT DAMAGED STRINGER SECTION DIMENSION 14" LONG AND FABRICATED NEW STRINGER SECTION FROM BAC 1498-145 DIMENSION 14" LONG AND 2EA SPLICES FROM BAC 1498-131 DIMENSION 10" LONG EACH, TREATED AND PRIMED AND INSTALLED ATJul 26, 2010 · N466FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201007262688Skin · canningRT FUSELAGE SKIN STR 17R BETWEEN BS 1303 TO BS 1323 IS OIL CANNED. CUTOUT DAMAGED AREA ( DIM: 6" X 3") AND FABRICATED REPAIR DOUBLER FROM 2024T3 .071 DIMENSION 15" X 10" IAW SRM 53-30-3, FIG 1 & 53-30-2, FIG 3. TREATED AND PRIMED AND INSTALLED REPAIR DOUJul 26, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201007222701Skin · gougedMAIN CARGO DOOR INNER SURROUND SKIN GOUGED STA 460-48- STR 4L. REMOVED MAIN CARGO DOOR INNER SKIN FWD UPPER SECTION IAW SRM 51-30-2. FABRICATED NEW INNER SKIN IAW DWG 53FX2022, REV C AND 53FX1535 REV H, TREATED AND PRIMED IAW SRM 51-10-2 AND INSTALLED NEW IJul 22, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR CA100625005Adjuster · missing(CAN) AFTER LANDING THE FLIGHT CREW NOTICED THAT THE AIRCRAFT BRAKES WERE ABNORMALLY HOT. UPON CLOSER INSPECTION OF THE NR 4 BRAKE ASSEMBLY THE FLIGHT CREW NOTICED THAT THE BALL AND TUBE ADJUSTER ASSEMBLY WAS MISSING. THE NR 4 BREAK ASSEMBLY WAS REPLACED WITJun 23, 2010 · Boeing 727225 · Landing Gear Brake SystemSDR FDEA201006182051Line · leakingLOST "A" SYSTEM HYDRAULICS AT FL 250. ENG 1 & 2 FLUID SHUTOFF CLOSED FOR 30 MINUTES WITH ENGINE NR 1 & 2 OPERATING. FOUND SPOILER HYD FLUID RETURN LINE NEAR WING STATION 546.5 BROKEN REPLACED SPOILER RETURN LINE PER SPM. LEAK CK`S NORMAL. SYSTEM A PRESSUJun 18, 2010 · N464FE · Boeing 727225 · Hydraulic System, MainSDR K11A2010062472401Skin · corrodedEVIDENCE OF SKIN CORROSION 12 X 12 INCH.Jun 10, 2010 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201004131198Rib · crackedNR 3 SLAT 2ND FROM INBD RIB IS CRACKED AT SLAT STA 128. REMOVED CRACKED RIB, FABRICATED NEW RIB USING 7075-O .032 DIMS 18" X 6", HEAT TREATED TO T6 CONDITION IAW ENG REPORT 2-37153-801 REV A, LOCATED, DRILLED AND INSTALLED RIB IAW SRM 51-30-2, 51-20-1, AND 51Apr 13, 2010 · N464FE · Boeing 727225 · Leading Edge DevicesSDR FDEA201004041077Stringer · damagedAFT PIT STRINGER HAS DOUBLE DRILLED HOLES STA 970 STR 28L REMOVED PREVIOUS REPAIR SPLICE AND PRODUCTION SPLICE, REMOVED DAMAGED STRINGER SECTION, LOCATED AND DRILLED NEW STRINGER SECTION USING BAC1498-145 7075T-6 PO 29057141 DIMS 43.1250" AND INSTALLED NEW STRApr 4, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201003301031Skin · gougedUPON REMOVAL OF INTERCOSTAL FOUND GOUGE IN FUSELAGE SKIN FWD OF BS 970 BTWN STR 30 AND STR 29R. REMOVED GOUGE AND CORROSION AND FOUND OUT OF LIMITS, REMOVED PREVIOUS REPAIR IAW SRM 51-30-2, CUT OUT DAMAGED AREAS DIMS 2.3750" X 4", 2 3/8" X 5.3125" AND 1" X 3"Mar 30, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003281121Skin · damagedMAIN CARGO AREA STA 660 BETWEEN STR 3L AND 4L NO EDGE DISTANCE ON FASTENERS. CUT OUT DAMAGED AREA DIMS 3" X 3.4", FABRICATED TRIPLER USING 2024T-3 .100 PO 9009120 DIMS 10 7/8" X 11 3/8", FABRICATED DOUBLER USING 2024T-3 .080 PO 9009327 DIMS 11 5/8" X 13 1/2",Mar 28, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003271026Floorbeam · damagedSTA 1166 FLOORBEAM HAS DOUBLE DRILLED HOLES LBL 25. CUT OUT DAMAGED AREA, FABRICATED NEW UPPER CHORD USING BAC1505-100617 7075T-73 PO 29103139 DIMS 11 5/8" X 2", FABRICATED 2 EACH SUPPORT ANGLES USING BAC1490-2831 7075T-62 PO 9006081 DIMS 11 1/2" X 3" AND BMar 27, 2010 · N464FE · Boeing 727225 · Fuselage Main, Floor BeamSDR FDEA201003271021Skin · damagedRT WING OTBD FORE FLAP, INBD L/E WBL 309 TO WBL 314 HAS 2 DEEP GOUGES FROM CONTACT WITH SPOILER PULLEY BOLTS. GOUGES OUT OF LIMITS IAW SRM 57-50-2 ,CUT OUT 2 DAMAGED AREAS DIMS .5" EACH IAW SRM 57-50-4, FABRICATED DOUBLER REPAIR USING 2024T-3 .050 DIMS 7" XMar 27, 2010 · N464FE · Boeing 727225 · Trailing Edge FlapsSDR FDEA201003261016Structure · corrodedCORROSION ON NOSE WHEEL WELL RT MID-CHORD, REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD, LOCATED AND DRILLED NEW CHORD PN 65-19862-20 PO 20017288 AND INSTALLED IAW SRM 51-30-5, 53-10-1 AND 51-30-2.Mar 26, 2010 · N464FE · Boeing 727225 · Fuselage Main, StructureSDR FDEA201003261017Sill · damagedC-2 DOOR CUT-OUT LOWER SILL HAS PILLOWING AT BS 970. REMOVED PREVIOUS REPAIR, REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD IAW SRM 51-30-2, LOCATED AND DRILLED NEW CHORD PN 65-56129Y10 IAW SRM 51-30-5 AND INSTALLED CHORD IAW SRM 51-30-2.Mar 26, 2010 · N464FE · Boeing 727225 · Fuselage Miscellaneous Structure
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