Boeing 727-2D4

Service difficulty reports · 279

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '7272D4'
  ORDER BY difficulty_date DESC"

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SDR FDEA200903180955Floorbeam · corrodedMAIN CARGO DECK FLOORBEAM UPPER "T " BS 1130 HAS CORROSION BETWEEN LBL25 AND LBL46. CUTOUT CORRODED SECTION IAW SRM 53-10-8 FIG 10 (SHEET 9). HFEC INSPECTED IAW NTM 51-00-19 PT.6, NO CRACK INDICATION NOTED. FABRICATED FILLER FROM 7075-T6 .156. FABRICATED DMar 18, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Floor BeamSDR FDEA200903120909Floorbeam · corrodedMAIN CARGO DECK FLOORBEAM AT STA 720A HAS CORROSION AND SCRIBE MARKS ON UPPER " T " SECTION BETWEEN LBL25 AND RBL25. REMOVED DAMAGED AND CORRODED SECTION IAW SRM 53-10-8 FIG 3, FABRICATED REPAIR PARTS ON TRAVELERS T9/783984,T9/783989,T9/784001,T9/783983,ANDMar 12, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Floor BeamSDR FDEA200903120908Frame · crackedFUSELAGE FRAME STA 890 OUTER CHORD CRACKED AT STRINGER 14R. REMOVED DAMAGE IAW SRM 51-30-2. FABRICATED NEW ANGLE AND NEW DOUBLER IAW SRM 53- 10-2 AND TRAVELERS NR T9/783599 ANDT9/783600, LOCATED AND DRILLED ANGLE AND ANGLE DOUBLER IAW SRM 51-30-2. INSTALLEMar 12, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, FrameSDR FDEA200903110901Seat Track · corrodedSEAT TRACK LBL 25 CORRODED ON NUMEROUS LOCATIONS FROM STA 500-690. REMOVED SEAT TRACK IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK FROM 60-6549/24 BATCH NR 1514987 LOCATED AND DRILLED IAW SRM 51-30-2. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW SEAT TRMar 11, 2009 · N288FE · Boeing 7272D4 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903100879Floorbeam · corrodedMAIN CARGO DECK FLOORBEAM UPPER TEE BS 1130 HAS CORROSION BETWEEN LBL 0 AND LBL 13. REMOVED CORROSION ON FLOORBEAM UPPER TEE BS 1130 BETWEEN LBL 0 AND LBL 13 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-8 FABBED 3 (EA) FILLERS AND NEW ANGLE P/N BAC 1505/100393 IAMar 10, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Floor BeamSDR FDEA200903090875Floorbeam · corrodedLAVATORY AREA FLOORBEAM AT STA 328 HAS CORROSION AT APPROX RBL 36 ON THE UPPER CHORD FWD EDGE (MARKED) REMOVED CORROSION 0.080 ORIGINAL 0.025 MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. CUT OUT DAMAGE AND FABRICATED REPAIR ON TRAVELER T9/783Mar 9, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Floor BeamSDR FDEA200903090874Floorbeam · corrodedMAIN CARGO DECK FLOORBEAM UPPER 'T' BS 1030 HAS CORROSION BETWEEN LBL 0 AND LBL 25 FABRICATED ANGLES REPAIRS FOR FLOORBEAM UPPER 'T' ON MAE TRAVELER T9/783860 IAW WITH SRM 53-10-8, FABRICATED 2 FILLERS BATCH NR 000104977, TREATED AND PRIMED ANGLES REPAIRS, FILMar 9, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Floor BeamSDR FDEA200903080864Bulkhead · corrodedAFT CARGO LT SIDE OF 1183 BULKHEAD FWD FACE DOME NUT AT LBL 27 HAS CORROSION ON IT AND ON SKIN 6 O'CLOCK POS UNDER AIR DUCT (INNER MOST). REMOVED CORROSION IAW SRM 51-10-6 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 1 SH2 NOTE C. FABRICATED REPAIR DOUBLER Mar 8, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, BulkheadSDR FDEA200903080863Seat Track · corrodedSEAT TRACK LBL 45 CORRODED ON NUMEROUS LOCATIONS FROM STA 500 - 690. REMOVED AND REPLACED DAMAGED SEAT TRACK SECTION FROM STA 500 - 690 LBL 45 IAW SRM 51305, FABRICATED FROM PN 60-6549/24 BATCH NR 1514987.Mar 8, 2009 · N288FE · Boeing 7272D4 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903070861Seat Track · corrodedSEAT TRACK LBL 0 CORRODED ON NUMEROUS LOCATIONS FROM STA 500 - 575. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2 BS 500 TO 580, REINSTALLED 4 STRAPS IAW SRM 51-30-2, FABRICATED SEAT TRACK SECTION ON MAE TRAV NR T9/ 82953, BATCH NR 0001541987, LOCATED AND Mar 7, 2009 · N288FE · Boeing 7272D4 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903050850Skin · canningAFT CARGO BILGE SKIN OIL CANNING BETWEEN STA 1100 AND 1130, HAS WORKING RIVETS AT STR 27L, STR 28L, AND STR 29L. CUT-OUT DAMAGED AREA IAW SRM 53-30-3 FIG 3, FABBED FILLERS IAW SRM 53-30-3. FABBED DOUBLER IAW SRM 53-30-3 LOCATED AND DRILLED IAW SRM 51-30-5 ANMar 5, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/SkinSDR FDEA200902270762Bulkhead · crackedNOSE LANDING GEAR BULKHEAD STA NR 351.20 HAS 3 CRACKS MIGRATING FROM 1 FASTENER HOLE ATTACHING THE NOSE GEAR LOCK ACTUATOR FITTING TO BULKHEAD. IN CORRECT TAIL NUMBER ENTERED IN BLOCK 1C, PLEASE SEE SDR 09-0763 FOR AIRCRAFT N482FE.Feb 27, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, BulkheadSDR FDEA200902120513Skin · damagedSKIN DAMAGE FROM STA 560 TO 580 STRINGER'S 27L TO 28R REPAIRED SKIN DAMAGE FROM STA 560 TO 580 STRINGERS 27L TO 28R IAW EA NR 7-5330-126895, FUSELAGE SKIN DENTS BETWEEN BS 560 AND 580 STR 27L AND 28R REPAIR.Feb 12, 2009 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/SkinSDR FDEA200812185195Control Lever · looseFLIGHT TEST OUTBOARD FLAP GAUGE INDICATED BETWEEN 20 DEGREES AND 25 DEGREES AT FLAPS 25 DEGREES AND BETWEEN 25 INCH AND 30 INCH AT FLAPS 30 INCH ALL OTHER POSITIONS OK (REPEAT) PERFORMED ADJUSTMENT AND TEST ON OTBD T/E FLAP POSITION TRANSMITTER REF MM 27-52-01Dec 18, 2008 · N287FE · Boeing 7272D4 · Trailing Edge Flap Control SystemSDR FDEA200812125131Floorbeam · crackedANGLE FOR FLOOR JUST FWD OF FLIGHT DECK DOOR CUT OUT IS CRACKED REMOVED FLOOR SUPPORT AND ATTACH BRACKET, FABRICATED DRILLED, TRIMMED, TREATED AND PRIMED NEW ATTACH ANGLE. INSTALLED FLOOR SUPPORT AND NEW ANGLE. REFERENCE BOEING DWG NR 65-17593/ITEM NR -239Dec 12, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Floor BeamSDR FDEA200812065095Angle · corrodedLWR EXTERIOR FUSELAGE BS 740, LBL6 TO LBL 10, WL 148.5 TO WL 150 JUST AFT OF GROUND A/C HOOK UP DUCT CORRODED REMOVED PANEL, A/C DUCT AND BODY FAIRING, AND HYD LINES FOR ACCESS REF SRM 51-30-02. REMOVED AND FABRICATED L ANGLE AND INSTALLED NEW L ANGLE REF Dec 6, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR FDEA200812055089Bracket · crackedRADAR R/T SHELF TRAY CRACKED AT AFT RT AND LT FOOT REMOVED AND REPLACED RT SHELF REF SRM 51-30-02.Dec 5, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR FDEA200812025041Angle · corrodedEXTERIOR LWR FUSELAGE INSIDE DELTA BEAM BS 740 LBL5 TO RBL 5 WL 148.5 LOWER ANGLE UPPER SURFACE CORRODED. REMOVED AND REPLACED T-ANGLE REF SRM 51-30-2 ORIGINAL MATERIAL THICKNESS .125. REMOVED .025 MATERIAL REMAINING .100 OUT OF LIMITS REF SRM 53-10-1 FIG 1.Dec 2, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04968Rib · crackedLT WING L/E RIB LWR CHORD HAS 2 CRACKS AT 5 INCH AND 18 INCH FROM SPAR, FSS 122. REMOVED PNL 6301 TO FOM. FABRICATED ANGLE REF DWG 64-8342-19 DRILLED-UP, TREATED, PRIMED, AND INSTALLED ANGLE REF SRM 51-30-5, MM 51-20-021, MM 51-20-051, AND SRM 51-30-2. INSTNov 24, 2008 · N287FE · Boeing 7272D4 · Wing, Rib/BulkheadSDR 08FDEA04964Skin Panel · crackedWHILE ACCOMPLISHING "OK TO WORK" STEP ON SNRM (N00791)) FOUND WING L/E SKIN CRACKED (LT WING) AT FSS 122, LWR SURFACE OF SKIN. REMOVED AND REINSTALLED ANTI-ICE DUCT (LT L/E WING ROOT) REF MM 36-00-001-2, LEAK CHECK GOOD. REPAIRED CRACK REF SRM 57-30-4 FIG 8.Nov 24, 2008 · N287FE · Boeing 7272D4 · Wing, Plate/SkinSDR 08FDEA04960Bracket · corrodedRT MLG W/W CUTOUT SEAL BEAM (STR 19R), AREAS OF CORROSION ON TOP SIDE OF BEAM FROM FS 906 TO FS 930, RBL 74, WL 105 REMOVED CORROSION FROM BRACKET, STA 920 ORIG T .094, REMAINING T .071, .023 MATERIAL LOSS OUT OF LIMITS. REPLACED BRACKET STA 920. REMOVED CONov 22, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04947Panel · puncturedFWD CARGO COMPARTMENT, PFM BOX, PUNCTURE JUST BELOW PFM DOOR REPAIRED PUNCTURE IN PFM BOX REF SRM 51-40-20 PAR'S 7, 14, 15, 19, 20, AND FIG'S 8, 211, SRM 51-20-4 AND AMM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 20, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04927Stringer · corrodedAFT PIT S27L LONGERON/FITTING HAS CORROSION AT BS 1130 REMOVED FASTENERS, REMOVED CORROSION, NDT (HFEC) BLENDOUT AREA AND FASTENER HOLES. ALODINED AND CIC, D AREA. WITH NO LIMITS REF EA 7-5310-123810, THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 19, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Longeron/StringerSDR 08FDEA04924Channel · crackedRADAR R/T SHELF, RT SIDE HAT CANNEL ON UPPER SIDE OF SHELF IS CRACKED. REPLACED RT SIDE HAT CHANNEL ON RADAR R/T SHELF IN ACCORDANCE WITH BOEING DRAWING 65C16129 AND SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIRNov 19, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04923Stiffener · corrodedLT MLG WHEEL WELL APU AIR INLET MOUNT FLANGES CORRODED REMOVED CORROSION REF SRM 51-10-1 ORIGINAL THICKNESS .150', REMOVED .018', REMAINING THICKNESS, .132' OUT OF LIMITS REF SRM 53-10-1 FIG 1. REPLACED 323 STIFFENER REF DWG 65-18636, AND SRM 51-30-2 PG 1-10.Nov 19, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04919Frame Splice · damagedAFT CARGO PIT STATION 1030 FRAME SPLICE AT APPROX STRINGER 24L IS DAMAGED. REPLACED FRAME SPLICE REF SRM 51-30-02 AND DRAWING 69-47200. THIS IS CLASSIFIED AS A MAJOR REPAIRNov 19, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 08FDEA04913Frame · dentedAFT CARGO PIT STATION 1050 FUSELAGE FRAME DAMAGED AT STR 26L. REMOVED DAMAGE ON STA 1050 AT STR 26R. REF SRM 51-40-05 PG1 FABRICATED AND INSTALLED DOUBLER FOR FRAME. REF SRM 51-20-1 PG 1 SRM 51-30-02 PG 1-12 FABRICATED AND INSTALLED NEW END ATTACH ANGLE FOR INov 18, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 08FDEA04912Frame · dentedAFT CARGO PIT STATION 1030 FUSELAGE FRAME DAMAGED AT STR 26L. REMOVED FRAME DAMAGE STA 1030 STR 26L REF SRM 51-40-3 FIG 1 PGS 1-6. FORMED DOUBLER REF SRM 51-20-1 PG 1 HEAT TREAT DOUBLER TRACKING 2008-11-129. REMOVED INTERCOSTAL STA 1030, INSTALALED INTERCNov 18, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 08FDEA04911Frame · dentedAFT CARGO PIT STATION 1010 FUSELAGE FRAME DAMAGED AT STRINGER 26L. REPAIRED FRAME REF SRM 51-40-03 FIG1 AND FABRICATED CHANNEL ANGLE REF DWG 65-84827-8 SRM 51-30-02 PG 1-5Nov 18, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 08FDEA04900Support Bracket · crackedMLG WW KEEL BEAM INTERIOR, UPPER BLEED DUCT RT SUPPORT BRACKET IS CRACKED BS 950. REPLACED UPPER BLEED DUCT RT SUPPORT BRACKET BS 950 MLG WW KEEL BEAM INTERIOR IN ACCORDANCE WITH BOEING DRAWING 69-48851 AND SRM 51-20-01 AND 51-30-02. THIS REPAIR IS CLASSIFIENov 17, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04893Skin · corrodedLOWER FWD CARGO PIT BILGE, CORROSION SPOT ON FUSE SKIN AT AFT SIDE OF STA 700, BL- 0" REF DUPLICATE SDR #08-4824. FAA PLEASE DELETE THIS SDR- ADMINISTRATORNov 15, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/SkinSDR 08FDEA04890Support · corrodedEDGE SUPPORT PANEL, BS 1030 TO BS 1166, LBL 19 TO LBL28, UPPER AND LOWER SURFACES CORRODED EDGE SUPPORT FOUND TO BE OUT OF LIMITS REF SRM 53-10-1 PGS 30-31. FABRICATED NEW EDGE SUPPORT REF 65-57570 65-57568. TREATED AND PRIMED NEW EDGE SUPPORT REF SRM 51-10-Nov 15, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04889Angle · crackedMAIN CARGO BAY, GILL LINER MOUNT FRAME CRACKED AT AFT BULKHEAD TOP RT CORNER, FS 1176, 27, WL 292. FABRICATED AND INSTALLED NEW ANGLE REF DRW 25FX1253, SRM 51-30-02 PG 1-12, SRM 51-10-2 PG 7, MM 51-20-151-7 PG 1, THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 15, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04887Support · crackedFUSELAGE UPPER LOBE INTERIOR STRUCTURE CRACKED ON GILL LINER SUPPORT AT STA 1180, RBL 68, STRINGER R 11. REPLACED SUPPORT STRUCTURE REF SRM 51-40-03 PG 1-5. THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 15, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04886Support · corrodedFUSELAGE UPPER LOBE INTERIOR STRUCTURE, CORROSION ON GILL LINER SUPPORT AT STA 1180, RBL68, AT STRINGER R9. REMOVED CORROSION AND INSTALLED REPAR DOUBLER AND FILLER REF SRM 1-40-23 FIG 1.Nov 15, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04885Support · corrodedFUSELAGE UPPER LOBE INTERIOR STRUCTURE FRAME SUPPORT CORROSION AT STA 600 - 620, RBL 47 UPPER AND LOWER SURFACE REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND NEW STRAP, TREATED AND PRIMED AND INSTALLED. CLASSIFIED AS A MINOR REPAIR.Nov 15, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04883Seat Track · chafedFUSELAGE UPPER LOBE STRUCTURE, SEAT TRACK HAS LONG CHAFE AT STA 520, RBL 64 BLENDED CHAFED AREA. MAPPED OUT AND SENT TO EG FOR BLEND ALLOWABLE LIMITS. BLEND IS WITHIN LIMITS. REF EA 7-5310-118317, ALODINED AND PRIMED REF SRM 51-10-02. THIS IS CLASSIFIED ANov 15, 2008 · N287FE · Boeing 7272D4 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04878Web · crackedFWD PIT DOOR CUTOUT FWD FRAME CLOSER WEB LOWER CORNER CRACKED, BS 560 RBL 26, WL 158. REMOVED DAMAGED WEB. FABRICATE NEW WEB. TREATED, PRIMED AND INSTALLED WEB REF: SRM 51-30-02 PG 1-12, SRM 51-1-2, PG 1-7. THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 14, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04870Frame · corrodedFUSELAGE UPPER LOBE INTERIOR STRUCTURE CORROSION AT STA 600 RBL 51 "I" FRAME BOTTOM FLANGE. REPAIRED FRAME IAW EA 7-5310-123811 SEE JPF FOR PARTIAL WORK ACCOMPLISHED, REPAIR CLASSIFIED AS MAJOR.Nov 13, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 08FDEA04862Stiffener · crackedFWD PIT DOOR CUTOUT FWD FRAME CLOSURE WEB FWD LOWER ANGLE STIFFENER CRACKED AT 4 LOWER INTERCOSTAL CUTOUTS BS 555. REMOVED CRACKED STIFFENER, FABRICATED NEW STIFFENER, BACK DRILLED TRIMMED TO FIT. ALSO, FABRICATED NEW FRAME CLIP FOR NEW STIFFENER, CLASSIFINov 12, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04860Support Bracket · crackedRADAR R/T SHELF CENTER LT SUPPORT BRACKET IS CRACKED REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE PER REF SRM 51-30-02, AND DRW NR 66-14848. INSTALLED NEW ANGLE REF SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 12, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04851Floor Panel · corrodedPANEL RACK, AFT PIT FLOOR PANEL SPLICE AT BS 1035 BOTTOM SURFACE CORRODED BLENDED CORROSION. ORIGINAL MATERIAL .125 MATERIAL LOSS OF .030 REMAINING .095, FOUND OUT OF LIMITS REF SRM 53-10-1 PG 30-3. FABRICATED NEW SPLICE PLATE P/N BAC1511-3795 2024-T3. TRENov 11, 2008 · N287FE · Boeing 7272D4 · Fuselage Floor PanelSDR 08FDEA04849Channel · wornPASSENGER CABIN GILL LINER "Z" CHANNEL STA 1148 STR 14L CHAFED INTO FRAME SPLICE BLENDED CHAFED AREA FRAME SPLICE STA 1148 STR 14L REF SRM 53-10-1 ORIG "T" .112 LOSS .040 OUT OF LIMITS REF SRM 53-10-1 P1-2. REPLACED FRAME SPLICE REF SRM 51-30-2, P2 THIS IS CLNov 11, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04825Shear Tie · corrodedLOWER FWD CARGO PIT, CORROSION ON FRAME SHEAR TIE, AFT SIDE OF STA 700, LBL 5 INCH. REPLACED SHEAR TIE IAW DRAWING 69-14871 AND SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.Nov 9, 2008 · N287FE · Boeing 7272D4 · Fuselage Internal Mounting StructureSDR 08FDEA04824Skin · corrodedLOWER FWD CARGO PIT BILGE, CORROSION SPOT ON FUSE SKIN AT AFT SIDE OF STA 700, BL 0". REMOVED DAMAGE FABRICATED REPAIR DOUBLER ANDINSTALLED REPAIR PER REF SRM'S 51-10-6,51-10-2, 51-30-02 AND 53-30-3 FIG1 . THIS IS CLASSIFIED AS A MAJOR REPAIR. CATEGORY "B"Nov 9, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/SkinSDR 08FDEA04818Strap · corrodedFUSELAGE UPPER LOBE INTERIOR STRUCTURE FRAME SUPPORT BETWEEN STA 500 AND STA 520 RBL 45 CORRODED. REMOVED OUTBOARD BLOW OUT PANEL FRAME SEGMENT TO ACCESS CORROSION UNDER THE NUT PLATES, ALSO REMOVED ALL NUT PLATES ON FRAME SUPPORT STRAP FROM STA 520 TO STA 55Nov 9, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04817Rib · crackedRT WING L/E RIB UPPER CHORD HAS SEVERAL CRACKS ALONG EXISTING REPAIRS AT 9 INCHES-20 INCHES FROM SPAR, FSS 122. REMOVED REPAIR, FABRICATED REPAIR DOUBLER REF SRM 51-40-3 FIG 1. INSTALLED RT WING LF RIB CHORD REPAIR REF SRM 51-40-3 FIG 1. THIS IS CLASSIFIED Nov 9, 2008 · N287FE · Boeing 7272D4 · Wing, Rib/BulkheadSDR 08FDEA04816Rib · crackedRT WING L/E RIB UPPER CHORD HAS SEVERAL CRACKS ALONG EXISTING REPAIRS AT 9 INCHES-20 INCHES FROM SPAR, FSS 122. REMOVED REPAIR, FABRICATED REPAIR DOUBLER REF SRM 51-40-3 FIG 1. INSTALLED RT WING LF RIB CHORD REPAIR REF SRM 51-40-3 FIG 1. THIS IS CLASSIFIED Nov 9, 2008 · N287FE · Boeing 7272D4 · Wing, Rib/BulkheadSDR 08FDEA04815Floorbeam · corrodedLOWER FWD CARGO PIT, CORROSION ON UNDERSIDE AT NUTPLATES OF FLOOR SUPPORT STRINGER STA 700 15 INCH, RBL 2.5.Nov 9, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Floor BeamSDR 08FDEA04805Angle · crackedDITCHING PAN AFT ANGLE AT STA 1183 RBL 53 IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED HEAT TREATED NEW ANGLE. INSTALLED AND SEALED NEW ANGLE CLASSIFIED AS A MINOR REPAIR, REF DWG 65-29567, SRM 51-40-02.Nov 8, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
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