Boeing 727-233

Service difficulty reports · 3,034

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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 = '727233'
  ORDER BY difficulty_date DESC"

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SDR FDEA200909223350Skin · gougedMCD DOOR AFT LWR SIDE GOUGED AT OLD REPAIR REMOVED OLD DOUBLER OUT OF LIMITS IAW SRM 51-30-2, FAB NEW DOUBLER USING MAT 301.1/2HD .063 PO NR 29067392, DIM: "8.5 X 4.8750" IAW PF SDMCER 01-049 REV H AND 52-30-2 FIG 2A. PAINTED IAW SRM 51-10-2, INSTALLED NEW DOSep 22, 2009 · N286FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA200909173428Skin · chafedFWD ENTRY DOOR FRAME AT BS 303.9, STR 15 AND16 WEB CUT OUTS HAS JAGGED EDGES AND RUBBING AGAINST DOOR STRAP. TRIMMED OUT EDGE UPPER SECTION ON FRAME STR 15L DIM: .063 AND STR 16L DIM: .090 IAW SRM 51-10-1 AND EA 7-5310-126849. HFEC AREA IAW NDTM 51-00-00, Sep 17, 2009 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200909173317Angle · crackedLT INBD MID FLAP LWR T/E ON ACT ROD CUTOUT WBL 106 ANGLE IS CRACKED. REMOVED ANGLE CRACKED FROM LT I/B MID FLAP IAW SRM 51-30-2, FABRICATED NEW ANGLE IAW SRM 51-40-4 FIG 1 SRM 57-50-2 FIG 5. INSTALLED NEW ANGLE IAW SRM 51-30-2 SRM 57-20-2 INSTALLED LOWER SKISep 17, 2009 · N286FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200909173363Skin · misinstalledMAIN CARGO AREA, STA 660, STR 4L, ABOVE STRINGER, RIVETS WITH NO SPACING. CUT OUT DAMAGED AREA OF STRAP, FABRICATED DOUBLER, TRIPLER, STRUCTURAL FILLER, 2 FILLERS, TEAR STRAP REPAIR, SHIMS, AND INSTALLED PARTS IAW SRM 51-30-2, 53-30-3, 51-30-5 AND 53-30-Sep 17, 2009 · N286FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200909173362Skin · misinstalledMAIN CARGO AREA, STA 660, STR 4L, BELOW STR, RIVETS WITH NO SPACING. CUT OUT DAMAGED AREA OF STRAP DIMS 3 INCHES X 5.5 INCHES, CUT OUT DAMAGED AREA OF SKIN, FABRICATED DOUBLER, TRIPLER, STRUCTURAL FILLER, 2 FILLERS, TEAR STRAP REPAIR, SHIMS, AND INSTALLED PARSep 17, 2009 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200909173319Doubler · gougedRT WING INBD FORE FLAP OTBD L/E HAS DEEP GOUGE FROM LONG SCREW IN WING LWR T/E. STOP DRILLED DEEP GOUGE AT RT WING INBD FORE FLAP OTBD L/E IAW SRM 51-10-1 REV 101. HFEC INSPECTED AREA IAW NDTM 51-00-00, FIG 23 PART 6, NO DEFECTS NOTED. FABRICATED REPAIR PSep 17, 2009 · N286FE · Boeing 727233 · Leading Edge DevicesSDR FDEA200909173318Angle · crackedRT WING INBD MID-FLAP, AFT LWR CHORD ANGLE IS CRACKED IN 2 PLACES AT WBL 100. REMOVED LWR SKIN PANEL IAW SRM 51-30-2. REMOVED LWR CHORD ANGLE ON IB MID FLAP IAW SRM 51-30-2 REV 101. FABRICATED NEW CHORD ANGLE 5 FT X 1.5 INCHES FROM BAC1503-100046 7075 T6, Sep 17, 2009 · N286FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200909173316Skin · crackedRT MLG WING DOOR SKIN CRACKED UNDER UPPER SEAL RETAINER AFT HINGE AREA. REPAIRED MLG WING DOOR IAW EO 7-5280-7-4301 PART 4.Sep 17, 2009 · N286FE · Boeing 727233 · Landing Gear DoorsSDR FDEA200909163384Frame · damagedAFT PIT BS 1090 FRAME IS PUNCTURED IN THE UPPER FLANGE ABOVE STR 27L. CUT-OUT DAMAGED AREA IAW SRM 51-10-1 REV 101. FABRICATED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1. HEAT TREATED 7075-0 TO T6 CONDITION IAW ER 2-37153-801 REV A. CW CONDUCTIVITY TEST IAW NDTMSep 16, 2009 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200909163434Support Fitting · missingMAIN CABIN SEAT TRACK SUPPORT FITTING MISSING, STA 1183, RBL 24.75. INSTALLED MISSING MAIN CABIN SEAT TRACK SUPPORT FITTING PART IAW SRM 51-30-2, 51-30-5 AND DWG 65-19606.Sep 16, 2009 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909163431Seat Track · corrodedCORROSION AT SEAT TRACK STA 740 TO STA 870, LBL 24. REMOVED OLD SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED IAW DWG 65-16279 AND SRM 51-30-2.Sep 16, 2009 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909163383Frame · puncturedAFT PIT BS 1050 FRAME PREVIOUS REPAIR DOUBLER IS PUNCTURED ABOVE STR 27R. REMOVED PREVIOUS REPAIR DOUBLER, FABRICATED NEW DOUBLER, HEAT TREATED DOUBLER TO T-6 CONDITION IAW FASI FORM 2-37153- 801 REV A, AND INSTALLED IAW SRM 51-40-3, 53-10-2 AND 51-30-2.Sep 16, 2009 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200909153429Skin · gougedMAIN CARGO AREA, STA 620-640, STR 4L, INNER SKIN HAS DEEP GOUGE. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED PARTS IAW SRM 51-10-1 AND EA 7-5310-126850.Sep 15, 2009 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200909153345Skin · damagedLT SIDE OF FUSELAGE, OUTER SKIN, SCRATCHES BETWEEN STA 1070 TO STA 1130, AND STR 23L TO STR 27L. REPAIRED LT SIDE OF FUSELAGE OUTER SKIN STA. 1086 TO 1097 BETWEEN STR 24L TO 25L IAW SRM 53-30-3 FIG 1 REV 101, 53-30-3, FIG 1, AND 51-30-2..Sep 15, 2009 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200909123346Web · crackedAFT AIRSTAIR STA 1275 LIGHTNING HOLE LT SIDE OF AIRSTAIR CRACKED. TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER FROM 7075-T6 .032 PO NR 9008186 APPROX DIM: 4 INCHES X 2.3750 INCHES AND INSTALLED NEW REPAIR DOUBLER AT BS 1275 LH AFT AIRSTAIR WEB IAW SRM 5Sep 12, 2009 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200909123315Spar · crackedRT WING LWR T/E, FALSE SPAR IS CRACKED AT INBD END, WBL 118. REMOVED LWR CHORD SECTION IAW DWG 27-57-038 REV C & DOUBLER IAW DWG SR27-57-038 REV C. TRIMMED OUT INBD AREA IAW DWG SR27-57-038, REV C & FABRICATED 2 ANGLES & HEAT TREATED ANGLES TO T6 IAW ER NR 2Sep 12, 2009 · N286FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200909123314Spar · crackedLT WING LOWER T/E, FALSE SPAR IS CRACKED AT INBD END, WBL 118. REMOVED DOUBLER, CUT-OUT LOWER CHORD, FABRICATED NEW WEB, 2 EACH ANGLES, NEW LWR CHORD, NEW DOUBLER, STRAPS, 2 FILLERS AND INSTALLED PARTS IAW DWG SR27-57-038 REV C.Sep 12, 2009 · N286FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200907182662Controller · malfunctionedON INITIAL TAKEOFF ROTATION THE DFFERENTIAL PRESSURE MOMENTARILY STUCK AT ZERO AND THEN JUMPED TO 3.6 PSID WHILE THE CABIN ALTITUDE CONTINUED TO CLIMB NORMALLY. HOWEVER PASSING 15000 FT CABIN ALTITUDE EXCEEDED 5600 FT WHICH WAS SET IN CABIN ALTITUDE WINDOW.Jul 18, 2009 · N257FE · Boeing 727233 · Cabin Pressure ControllerSDR FDEA200907142620Accessory Unit · failedAFTER TAKE OFF, THE LANDING GEAR LEVER LATCH FAILED TO RELEASE. LANDING GEAR LEVER COULD ONLY BE RAISED TO OFF POSITION. HORN SOUNDED WHEN FLAPS RETRACTED FROM 5 DEG. TO 2 DEG. REMOVED AND REPLACED M831 AIR SENSING SENSOR PER AMM 32-09-221-4 AND PERFORMJul 14, 2009 · N269FE · Boeing 727233 · Landing Gear Retraction/Extension SystemSDR FDEA200907112582Power Unit · leakingSYS B HYD SYS FAILED INFLT B HYD INDICATED ZERO GAL & PRESSURE BEGAN TO DECREASE BELOW 200 PSI. EVALUATION SHOWS LEAK FROM UPPER RUDDER AREA. F/E NOTED DECREASING "B" SYS QTY & MONITORED QTY & PRESSURE. AS PRESSURE DECREASED, AS SOON AS NR 2 "B" PUMP LOW PJul 11, 2009 · N258FE · Boeing 727233 · Hydraulic System, MainSDR FDEA200907102578Angle · corrodedFUSELAGE LWR BODY AT PANEL CUTOUT BTW STA 277 AND STA 351 CORROSION SKIN AND NUTPLATES. REMOVED NUTPLATES AND CORROSION IAW SRM 51-10-6 AND 51-30-2 AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG1. REMOVED T-ANGLE AND FABRICATED NEW T-ANGLE IAW DWG NR 65-10936. Jul 10, 2009 · N284FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200907072515Skin · gougedRT OTBD FOREFLAP WBL 442, GOUGE FWD OF ATTACH FITTING BURNISHED AREA IAW SRM 51-10-1 AND FOUND OUT OF LIMITS IAW SRM 57-50-1 FIG 23. REMOVED FOREFLAP BRACKET FOR ACCESS IAW SRM 51-30-4, FIG 4. CUT DAMAGED AREA IAW SRM 57-50-4, FIG 4 FABRICATED 2 EA DOUBLERS Jul 7, 2009 · N284FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200906242279Seat Track · gougedCABIN FLOOR SUPPORT GOUGE AT SEAT TRACK STA 1090 NR RBL 24.5. BLENDED OUT DAMAGE AND FOUND OUT OF LIMITS IAW SRM 51-10-1 AND 53-10-1 FIG 3. REMOVED DAMAGED SEAT TRACK AND FABRICATED NEW TRACK SECTION. TREATED AND PRIMED NEW TRACK AND INSTALLED IAW SRM 51-30Jun 24, 2009 · N284FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200906232245Skin · damaged5 EA OEM HOLES AT RIVET HOLES BETWEEN BS 610 - 600 STR 3L. CUT-OUT DAMAGED AREA (INNER SKIN) DIM: 3.2500" X 1" AND 2.7500" X 1", FAB NEW FILLER FOM 2024T3 .040, PO NR 9008328, DIM: 3.2500" X 1" AND 2.7500" X 1", HFEC AREA WITH NO DEFECT NOTED, TREATED, PRIMEJun 23, 2009 · N278FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200906222202Sill · damagedDRILLED HOLE HAS SHORT "ED" CENTER LONGERON FITTING. DRILLED HOLE FOUND TO BE PART OF P TO F CONVERSION MOD AND FOUND TO BE STRUCTURALLY ACCEPTABLE IAW EA 7-5310-126827 STEP 13.Jun 22, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200906202190Hinge · wornMCD AFT END SECTION OF HINGE HAS PLAY. REMOVED, FABRICATED, AND INSTALLED MCD AFT END SECTION OF HINGE P.O. 79014501, PN NR 5212791, DIM: 42" - UPPER, AND 20" - LOWER. IAW P - F SRM ER 01-049 AND SRM 51- 30-2, 51-30-5, 51-30-8. MCD LEAK AND OPS CHECKED GOODJun 20, 2009 · N278FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA200906202189Hinge · wornMCD FWD END SECTION OF HINGE HAS PLAY REMOVED, FABRICATED AND INSTALLED MCD FWD END SECTION OF HINGE P.O. NR 79014501, PN 5212791, DIM: 45" UPPER, AND 20" LOWER IAW FX P TO F SRM ER-01-049 AND SRM 51-30-2, 51-30-5, 51-30-8. MX LEAK AND OPS CHECKED GOOD IAJun 20, 2009 · N278FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA200906172140Attach Fitting · crackedMAIN CABIN UPPER FUSELAGE RT SIDE AT STA 360, STR 7 R AT 9G BULKHEAD ATTACHMENT TO STRINGER - STR 7R IS CRACKED AT LWR END RADIUS. REMOVED FASTENERS ON STRINGER ACESS AND STRAP SUPPORT IAW SRM 51-30-2. STOP-DRILLED CRACK IAW SRM 53-10-3 FIG 2. C/W HFEC-VERIFJun 17, 2009 · N284FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR FDEA200906152116Stiffener · misinstalledAFT PIT - VERTICAL STIFFENER HAS 3 EACH PLACES WHERE FASTENERS AVE NO EDGE DISTANCE AT BS 1183, LBL 17.8. REPAIRED IAW EA 7-53-126832 - FUSELAGE AD 98-11-03 R1, BS 1183 BULKHEAD, VERTICAL BEAM WITH UNSUFFICIENT FASTENER SPACING AT LBL 20 BELOW WL 190 REPAIR.Jun 15, 2009 · N284FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200906132064Skin · damaged5 EA. OEM HOLES ALONG RIVET LINE BETWEEN BS 610-600 STR 3L. CUT-OUT DAMAGED AREA. FABRICATED NEW FILLERS HFEC INSPECTED AREA WITH NO DEFECTS NOTED, TREATED, PRIMED AND INSTALLED NEW FAB PARTS, ALL IAW EA 7-5310-126827, SRM 51-10-2, AND NDTM 51-00-00 FIG 23 PJun 13, 2009 · N278FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200906122049Sill · damaged1 EA OEM HOLE AT MCK CUT-OUT BS 620 STR 4L. ACCOMPLISHED REPAIR IAW EA 7-5310-126827 BY TRIMING OUT OPEN HOLE IN SKIN BS 620, STR 4L, PERFORMED HFEC INSP OF TRIMMED EDGE TO ENSURE NO CRACKS AND NO FINDINGS NOTED. TRIMMED ADDITIONAL .040 INSURANCE CUT AND FABJun 12, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200906122054Sill · damaged1 EA OEM HOLE AT RIVET HOLE BS 520 S3L. CUT-OUT DAMAGED AREA, FABRICATED NEW FILLER REPAIR, HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 23 PT6. TREATED PRIMED & INSTALLED FILLER REPAIR ALL IAW SRM 51-10-2 & EA 7-5310-126827.Jun 12, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200906122053Sill · damaged7 EA. OEM HOLES ALONG RIVET LINE BETWEEN BS 500-490 S3L. CUT-OUT DAMAGED AREA. FABRICATED NEW FILLER REPAIR, TREATED AND PRIMED, HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 23 PT6 WITH NO DEFECT NOTED. INSTALLED REPAIR FILLERS IAW EA 7-5310-126827 DATED: 06-09Jun 12, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200906122051Sill · damaged1 EA OEM HOLE NEXT TO RIVET HOLE MCD FUSELAGE SKIN BS 560 BETWEEN S2-3L. CUT-OUT DAMAGED, FABRICATED NEW FILLER REPAIR, TREATED AND PRIMED , HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 23 PT 6 WITH NO DEFECTS NOTED & INSTALLED FILLER REPAIR ALL IAW EA 7-5310-12Jun 12, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200906122052Sill · damagedNUMEROUS OEM HOLES ALONG MCK CUT-OUT BS 480 S3-4L. TRIMMED OUT DAMAGED AREA, FABRICATED NEW FILLER, TREATED AND PRIMED IAW SRM 51-10-2. HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 23 PT6 WITH NO DEFECTS NOTED. INSTALLED FILLER REPAIR IAW EA 7-5310-126827 AND SJun 12, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200906041927Web · crackedFORWARD CARGO AREA STA 560 STR 19L PRELOAD SPRING DRUM WEB HAS CRACK. REMOVED AND INSTALLED C1 DOOR MECHANISM SPRING CARTRIDGE ASSY. REMOVED WEB AND FABRICATED NEW WEB, HEAT TREATED TO T6 CONDITION, TREATED, PRIMED & INSTALLED NEW FABRICATED WEB IAW SRM 51-30Jun 4, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR PCSA2009060401Flange · corrodedCORROSION FOUND ON RT MAIN WHEEL WELL OTBD AFT FLANGE AT STA 930 RBL 72 ABOVE MANUAL EXTENSION TORQUE TUBE. REMOVED SUPPORT FITTING FOR ACCESS. REMOVED CORROSION IAW SRM 51-30-2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW EO SIE-AJ-N495AJ-05-09 REV 1R. REPLACJun 1, 2009 · N495AJ · Boeing 727233 · Fuselage, Landing Gear Attach FittingsSDR FDEA200905291854Sill · crackedMAIN CARGO MCK-UPPER SILL, BS 500 STR 3L - 4L CRACK COMING FROM RIVET FASTENER HOLE. REMOVED LOCATED AND INSTALLED LONGERON PN 53FX1467-101 P.O. NR 29052265. SPLICES PN 53FX1467114 PO NR 29057261 TREATED AND PRIMED NEW DRILLED PARTS AND BARE METAL ALL IAW SRMay 29, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200905291853Sill · crackedMAIN CARGO AREA MCK-UPPER SILL STA 600 STR 3L TO 4L, CRACKS ORIGINATING FROM TWO RIVET FASTENERS. REMOVED, LOCATED, TREATED, PRIMED AND INSTALLED MID AND AFT LONGERON SECTION OF MCD UPPER SILL IAW SRM 51-30-2, 51-10-2 AND EA 7-5310-126827 ACCOMPLISHED INSP OFMay 29, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200905291852Sill · crackedMAIN CARGO, MCD-UPPER SILL, BS 490 STR 3L-4L, CRACK COMING FROM FASTENER HOLE. REMOVED AND REINSTALLED MCD HINGE IAW ACCESS, HFEC. INSPECTED AREA IAW NDTM 51-00-00 FIG 23 PT6 AND SRM 51-30-2. REMOVED AND REPLACED MCD UPPER SILL IAW SRM 51-30-2, 51-10-2 AND May 29, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200905281841Skin · crackedRT FORE FLAP OTBD WBL 442 CRACK ON SKIN ABOVE CARRIAGE ATTACH FITTING. REMOVED RT OTBD FORE FLAP TO FOM REPAIR IAW MM 27-51-011-4. STOPPED DRILLED CRACK IAW SRM 51-10-1. HFEC INSPECTED STOP DRILL AREA IAW NDTM 51-00-00 FIG 3 PT6 NO DEFECTS NOTED. FABRICAMay 28, 2009 · N278FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200905271806Seat Track · crackedCABIN SEAT TRACK HAS CRACK INDICATION AT BS 760 LBL 48 ACCESSED AREA OF INDICATION ON SEAT TRACK IAW SRM 51-30-2. HFEC INSPECTED AREA IAW NDTM PT6. 51-00-00 FIGURE 23. NO DEFECTS NOTED. REINSTALLED 2 EA BOLTS IAW SRM 51-30-2.May 27, 2009 · N278FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200905271805Seat Track · crackedCABIN SEAT TRACK HAS CRACK INDICATION AT BS 760 RBL 48 ACCESSED AREA OF CRACK INDICATION IAW SRM 51-30-2. HFEC INSPECTED AREA IAW NDTM PT6. 51-00-00 FIG 23. NO DEFECTS NOTED. REINSTALLED 2EA BOLTS IAW SRM 51-30-2.May 27, 2009 · N278FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200905231844Attach Angle · corrodedLT WING LE NR 2 SLAT ACTUATOR ATTACH ANGLES MOUNT HOLES CORRODED AND PITTED. REMOVED LT WING FUEL ACCESS PNL 7215 IAW MM 28-11-021-4. REMOVED IB AND OB ATTACH ANGLES IAW EA 7-5750-120824 AND SRM 51-30-2. LOCATED, DRILLED, AND DEBURRED HOLES ON INBD AND OTBD May 23, 2009 · N278FE · Boeing 727233 · Wing, Attach FittingsSDR FDEA200905231861Angle · crackedNR 4 SLAT AFT LOWER ANGLE IS CRACKED AT INBD UPSTOP PAD. REMOVED SLAT COVE PANELS IAW SRM 51-30-2. REMOVED DAMAGED AREA IAW SRM 51-40-4 FIGURE 1. FABRICATED NEW ANGLE IAW SRM 57-50-2 FIG.2 AND 51-30-5, AND 51-30-8. TREATED AND PRIMED ANGLE IAW SRM 51-10-2. INSMay 23, 2009 · N278FE · Boeing 727233 · Leading Edge DevicesSDR FDEA200905231862Angle · crackedNR 8 SLAT AFT LOWER ANGLE IS CRACKED AT INBD AND OUTBD UPSTOP PADS. REMOVED COVE PANELS AT NR 8 SLAT IAW SRM 51-30-2. REMOVED DAMAGED ANGLE IAW SRM 51-30-2 FABRICATED NEW ANGLE IAW SRM 57-50-2 FIG 2, 51-30-5 AND 51-30-8, TREATED AND PRIMED ANGLE IAW SRM 51-May 23, 2009 · N278FE · Boeing 727233 · Leading Edge DevicesSDR FDEA200905221773Skin · gougedLOWER CARGO C3 DOOR OUTER SKIN NUMEROUS DENTS & GOUGES ALL OVER SKIN. REMOVED OUTER SKIN AT C3 DOOR IAW SRM 51-30-2 AND FABRICATED NEW C3 DOOR SKIN IAW EA-7-5230-127967. TREATED AND PRIMED C3 DOOR SKIN IAW SRM 51-10-2 AND INSTALLED C3 DOOR SKIN IAW SRM 51-May 22, 2009 · N278FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA200905221772Frame · dentedAFT CARGO COMPARTMENT FRAME IS DENTED IN UPPER FLANGE AT BS 950C ABOVE STR 26R. REWORKED DENTED AREA TO ORIGINAL CONTOUR. ABOVE STR 26R IAW DWG SR 27-53-139. NDT INSPECTED AREA WITH NO DEFECTED NOTED. FRAME THICKNESS FOUND TO BE .071 IAW SRM 53-10-2 FIG 5.May 22, 2009 · N278FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200905221771Frame · dentedAFT CARGO COMPARTMENT FRAME IS DENTED IN UPPER FLANGE RADIUS AT BS 990 ABOVE STR. 26L. REWORKED DENTED AREA TO ORIGINAL CONTOUR AT BS 990 STR 26L IAW DWG SR 27-53-139. NDT INSPECTED AREA WITH NO DEFECT NOTED IAW NDTM 51-00-00 FIG 23 PART 6. FRAME THICKNESS FMay 22, 2009 · N278FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200905211764Skin · corrodedCORROSION AFT BOLT HEAD FITTING EXTERIOR FUSELAGE, BS 740, STR 26R - 28R. REMOVED BULKHEAD FITTING AT BS 740 STR 26R-28R EXTERIOR FUSELAGE IAW SRM 51-30-2. FABRICATED NEW FITTING IAW DWG NR 69-64841. HEAT TREATED NEW PART TO T6 IAW FAS ENG REPORT NR 2-37153May 21, 2009 · N278FE · Boeing 727233 · Fuselage Main, Plate/Skin
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