Boeing 727-2S2F

Service difficulty reports · 842

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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 = '7272S2F'
  ORDER BY difficulty_date DESC"

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SDR 08FDEA04929Web · misalignedMAIN CABIN SHEAR DECK AT BS 1148 TO 1166 RBL 8-19 NEEDS FABRICATED, SHEAR DECK WILL NOT BE ABLE TO BE INSTALLED AFTER FLOORBEAM REPAIR ON SNRM N00512. NEW DECK WILL BE FABRICATED FROM REF 65-19602. FABRICATED MAIN CABIN SHEAR DECK AT 1148 TO 1166 RBL 8-19 RENov 19, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA04928Fitting · corrodedAFT PIT STRINGER BULKHEAD FITTING STA 1183 STR 19R CORRODED. REMOVED AND REPLACED CORRODED FITTING, REF SRM 51-30-2 PG 1-4,8 THIS IS CLASSIFIED AS A MAJOR REPAIR.Nov 19, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Attach FittingsSDR 08FDEA04922Seat Track · corrodedSEAT TRACK CORRODED, MAIN DECK AT RBL 24 BS 1148 TO 1176.Nov 19, 2008 · N216FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04921Seat Track · corrodedMAIN DECK SEAT TRACK AT LBL 24 BS 1176 TO 1183 IS CORRODED.Nov 19, 2008 · N216FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04920Skin · chafedLOWER RIGHT EXTERIOR FUSELAGE SKIN IS CHAFED AT AFT CARGO PIT DOOR CUTOUT FWD LWR CORNER STA 950E, STR 26-R. REPAIRED FWD LOWER CORNER OF FUSELAGE SKIN AT AFT CAGO DOOR CUT OUT REF EA 7-5330-123818. THIS IS CLASSIFIED AS A MAJOR REPAIR.Nov 19, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 08FDEA04896Skin · misrepairedSKIN AT STA 1290 STR 20R HAS TOOLING MARKS, FASTENERS WITH IMPROPER ED AND THE SKIN IS BULGING. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-02. CUT-OUT DAMAGE PER B727 SRM 51-10-01, FABRICATED REPAIR DOUBLER IAW B727 SRM 53-30-3 & 53-30-2 FIG 3. FABRICATED Nov 16, 2008 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR FDEA200811154884Strap · corrodedAREAS OF CORROSION ON FWD CARGO PIT UPPER FLOORBEAM STABILITY STRAP AS MARKED. REMOVED CORROSION FOUND OUT OF LIMITS REF SRM 53-10-01. FABRICATED STRAP AND SPLICE PLATE REF DWG 65-23638 AND 66-14865. TREATED, PRIMED AND INSTALLED STABILITY STRAP AND SPLICE Nov 15, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA04888Support Angle · corrodedLWR FUSELAGE ANTENNA SUPPORT ANGLES AT FASTENER HOLES HAVE CORROSION, BS 740-760, RBL 6 TO LBL 6. REMOVED CORROSION AT LWR FUSELAGE ANTENNA SUPPORT ANGLES STA 740 - 760, RBL 6 TO LBL 6, REF SRM 51-10-6, MATERIAL LOSS 50 PERCENT OFF, FOUND TO BE OUT OF LIMITS Nov 15, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA04884Strap · corrodedAREAS OF CORROSION ON FWD CARGO PIT UPPER FLOORBEAM STABILITY STRAP AS MARKED. REMOVED CORROSION FOUND OUT OF LIMITS REF SRM 53-10-01. FABRICATED STRAP AND SPLICE PLATE REF DWG 65-23638 AND 66-14865. TREATED, PRIMED AND INSTALLED STABILITY STRAP AND SPLICE Nov 15, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR FDEA200811144879Skin · wornLT EXTERIOR FUSELAGE BS 720D, 12 STR 19L SKIN LAP JUST FWD OF WING LE, SKIN HAS WEAR REPAIRED FUSE SKIN AT STA 720D 12 STR 19L REF SRM 53-30-3 FIG 5. DISPLACED LEFT INBD LEADING EDGE FOR REPAIR AND REINSTALLED REF SRM 51-30-2 PG 1-5. DISCONNECTED LEADING EDGNov 14, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR FDEA200811144880Floor Panel · corrodedMAIN CARGO FLOOR CORROSION ON SEAT TRACK AT STA 740 LBL46, REMOVED BEYOND LIMITS CORRODED SEAT TRACK REF SRM 51-30-2. FABRICATED REPLACEMENT SEAT TRACK REF SRM 53-10-5. FABRICATED TRACK SPLICE REF SRM 53-10-5. INSTALLED SEAT TRACK AND SPLICE REF SRM 53-10-5Nov 14, 2008 · N216FE · Boeing 7272S2F · Fuselage Floor PanelSDR 08FDEA04880Floor Panel · corrodedMAIN CARGO FLOOR CORROSION ON SEAT TRACK AT STA 740 LBL46 REMOVED BEYOND LIMITS CORRODED SEAT TRACK REF SRM 51-30-2. FABRICATED REPLACEMENT SEAT TRACK REF SRM 53-10-5. FABRICATED TRACK SPLICE REF SRM 53-10-5. INSTALLED SEAT TRACK AND SPLICE REF SRM 53-10-5,Nov 14, 2008 · N216FE · Boeing 7272S2F · Fuselage Floor PanelSDR 08FDEA04879Skin · wornLT EXTERIOR FUSELAGE BS 720D 12 STR 19L SKIN LAP JUST FWD OF WING LE, SKIN HAS WEAR REPAIRED FUSE SKIN AT STA 720D 12 STR 19L REF SRM 53-30-3 FIG 5. DISPLACED LEFT INBD LEADING EDGE FOR REPAIR AND REINSTALLED REF SRM 51-30-2 PG 1-5. DISCONNECTED LEADING EDNov 14, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 08FDEA04852Angle · corrodedLWR EXTERIOR FUSELAGE INSIDE DELTA BEAM BS 740 LBL 5 TO RBL 5 WL 149, FWD LOWER CHORD HAS CORROSION AROUND FASTENERS. REMOVED CORROSION FROM TEE ANGLE STA 740 LBL 5 TO RBL 5, FOUND OUT OF LIMITS. REMOVED TEE ANGLE STA 740, FABRICATED NEW TEE ANGLE TREATED ANov 11, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA04847Seat Track · corrodedMAIN CABIN FLOOR CORROSION ON SEAT TRACK FLANGE AROUND FASTENER HOLES STA 560-640 LBL 23 REMOVED CORROSION AT BS 560, REMOVED .030 AREA 1 INCH BY 1 INCH, BS 610 REMOVED .047 AREA 1 INCH BY 1 INCH AND BS 620 REMOVED .045 AREA 1 INCH BY 1 INCH ORIGINAL MATERIAL Nov 11, 2008 · N216FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04846Intercostal · corrodedLOWER AFT CARGO AREA CORROSION ON INTERCOSTAL AT STA 950E 3 RBL 12. REMOVED INTERCOSTAL, REMOVED CORROSION, ORIGINAL "T" .040, REMOVED .010, REMAINING .030, FOUND TO BE OUT OF LIMITS. FABRICATED NEW DOUBLER FOR INTERCOSTAL, INSTALLED NEW INTERCOSTAL AND Nov 11, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA04819Rib · crackedA86-2470, RT WING LE RIB UPPER CHORD IS CRACKED AT EXISTING REPAIR FSS 119, 8 INCHES-18 INCHES FROM SPAR (MKD). INSTALLED AND FABRICATED RT WING LE UPPER CHORD AND SPLICE AT FSS 119. REFS BOEING DWG 64-08342-20, SRM 51-40-03, SRM 51-30-02. TREATED AND PRIMENov 9, 2008 · N216FE · Boeing 7272S2F · Wing, Rib/BulkheadSDR FDEA200811084813Floorbeam · corrodedAFT FLOORBEAM CORRODED RBL 27 AND RBL 43 NUTPLATES STA 1166 WL 208. REPAIRED CORRODED FLOORBEAM REF SRM 53-10-8 FIG 3. SUBSTITUTED "T" CAP MATERIAL REF EA 7-5310-118313. THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR FDEA200811084812Floorbeam · corrodedSTA 1148 FLOORBEAM UPPER FLANGE CORRODED RBL 45-45 AFT SIDE AND 44-47 FWD SIDE WL 208. REPAIRED DAMAGED FLOORBEAM REF SRM 53-10-8 FIG 3, SUBSTITUTED "T" CHORD REF EA 7-5310-118313. THIS IS CLASSIFIED AS A MAJOR REPAIR.Nov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 08FDEA04800Skin · crackedNR 6 FLAP TRACK HINGE FAIRING CRACKED ON LOWER SKIN AT L/E. FABRICATED DOUBLER AND FILLER FOR NR 6 FLAP TRACK PER DWG 65-21795 PG 1 2024-T3 .040 FILLER 2024-T3 .050. DOUBLER INSTALLED, TREATED AND PRIMED AND PAINTED REF SRM 51-10-2 PG 2-7. THIS IS CLASSIFNov 8, 2008 · N216FE · Boeing 7272S2F · Wing Miscellaneous StructureSDR 08FDEA04813Floorbeam · corrodedAFT FLOORBEAM CORRODED RBL 27 AND RBL 43 NUTPLATES STA 1166 WL 208.Nov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 08FDEA04812Floorbeam · corrodedSTA 1148 FLOORBEAM UPPER FLANGE CORRODED RBL 45-45 AFT SIDE AND 44-47 FWD SIDE WL 208.Nov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 08FDEA04811Floorbeam · corrodedAFT PIT FLOOR SUPPORT ON UNDERSIDE AROUND NUTPLATE STA 1166, NO CENTER LINE. SPLICED IN NEW SUPPORT SECTION REF SRM 53-10-5 AND 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 08FDEA04810Floorbeam · corrodedAFT PIT FLOOR SUPPORT CORRODED ON UNDERSIDE AROUND NUTPLATE STA 1166 RBL 7-8. SPLICE IN NEW SUPPORT SECTION REF SRM 53-10-5 AND 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 08FDEA04809Floorbeam · corrodedAFT PIT FLOOR SUPPORT CORRODED ON UNDERSIDE AROUND NUTPLATE STA 1166 RBL 3-4. SPLICED IN NEW SUPPORT SECTION REF SRM 53-10-5 AND 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 08FDEA04808Floorbeam · corrodedAFT PIT FLOOR SUPPORT CORRODED ON UNDERSIDE AROUND NUTPLATE STA 1166 LBL 3-4. SPLICED IN NEW SUPPORT SECTION REF SRM 53-10-5 AND 51-30-2. THIS IS CLASSIFIOED AS A MINOR REPAIR.Nov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 08FDEA04807Floorbeam · corrodedAFT PIT FLOOR SUPPORT CORRODED ON UNDERSIDE AROUND NUTPLATE STA 1166 LBL 11-12. SPLICED IN NEW SUPPORT SECTION REF SRM 53-10-5 AND 51-30-2. CLASSIFIED AS A MINOR REPAIR.Nov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 08FDEA04806Floorbeam · corrodedUNDERSIDE OF AFT PIT FLOOR SUPPORT CORRODED AT STA 1166 RBL 11-12. SPLICED IN NEW SUPPORT SECTION REF SRM 53-10-5 AND 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 08FDEA04804Bulkhead · corrodedFWD CARGO PIT, AFT BULKHEAD LWR BEAM PRESSURE PANEL IS CORRODED APPROXIMATELY 6 INCHES LBL ON UNDER SIDE, AND IN SEVERAL OTHER AREAS OF LWR BEAM AROUND NUTPLATE HOLES. REMOVED CORROSION ON LOWER BEAM FOR BULKHEAD PRESSURE PANELS ON AFT BULKHEAD IN FWD CARGONov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, BulkheadSDR 08FDEA04802Skin · corrodedLOWER AFT CARGO AREA, CORROSION ON SKIN AT STA 950E TO 950F AT LEFT KEEL BEAM. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED FLOOR SUPPORTS, REMOVED, DRILLED, COUNTERSUNK, AND TRIMMED DOUBLER, TREATED AND PRIMED DOUBLER AND SKIN, INSTALLED DOUDLER, INSTANov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 08FDEA04801Rib · crackedRT WING LE RIB LWR CHORD IS CRACKED IS CRACKED FSS 119, 4 INCHES-18 INCHES FROM SPAR VERIFIED MATERIAL ID FOR REPAIR ANGLE AND FILLER. CUT OUT DAMAGE. FABRICATED REPAIR ANGLE AND FILLER. LOCATED, DRILLED AND TRIMMED REPAIR ANGLE. HEAT TREATED REPAIR ANGLE.Nov 8, 2008 · N216FE · Boeing 7272S2F · Wing, Rib/BulkheadSDR 08FDEA04799Web · crackedVERTICAL STRAP UPPER END, ELEVATOR FEEL CONTROL UNIT MOUNT PLATFORM LEFT AND RIGHT VERTICAL WEBS CRACKED AT L/E FASTENERS. VERIFIED VERT WEBS CRACKED. REMOVED LT AND RT VERTICAL WEBS, FABRICATED, TREATED, PRIMED AND INSTALLED LT AND RT NEW VERTICAL WEBS, REFNov 8, 2008 · N216FE · Boeing 7272S2F · Wing Miscellaneous StructureSDR 08FDEA04798Mount · corrodedFWD ELECTRONIC BAY WEATHER RADAR MOUNT SHELF, LT AFT ATTACH BRACKET CRACKED VERIFIED MATERIAL ID. FABRICATED DOUBLER AND NEW LIGHT SWITCH BRACKET. REMOVED ELECTRONIC BAY LIGHT SWITCH BRACKET, STOP DRILLED CRACKS, TREATED, PRIMED AND PAINTED DOUBLER AND NEW LNov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Attach FittingsSDR 08FDEA04797Shear Tie · misinstalledSHEAR TIE AT STA 720A, STR 18 R HAS NO EDGE MARGIN AT FASTENER HOLE REPLACED SHEAR TIE AT STA 720 STR 18R IN ACCORDANCE WITH SRM 51-30-02 AND DRAWING 69-43668. THIS IS CLASSIFIED AS A MAJOR REPAIR.Nov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Internal Mounting StructureSDR 08FDEA04796Skin · damagedLOWER FUSELAGE SKIN, STA 720A, STR 18R, LIGHTNING STRIKE IN SKIN REPAIRED LIGHTING STRIKE IN SKIN STA 720A STR 18R IN ACCORDANCE WITH SRM 53-30-3 FIG 3 REPAIR CLASSIFIED A MAJOR REPAIR.Nov 8, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 08FDEA04766Intercostal · crackedFORWARD LAVATORY BELOW FLOOR WATERLINE 208 APPROX STA 294-312 AND APPROX 41 INCHES INTERCOSTAL WEB BETWEEN FLOORBEAMS IS CRACKED, JUST INBD OF LAV DUMP TUBE. REMOVED INTERCOSTAL FOR REPAIR REF SRM 51-10-2, REPAIRED INTERCOSTAL REF SRM 51-40-03 FIG 1. TREATEDNov 6, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA04754Skin · misrepairedFOUND EXTERNAL FUSELAGE REPAIR LOCATED AT APPROX BS 1164-1178 STR 17R- STR 18R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REMOVED OLD REPAIR REF SRM 51-30-2 PG 1-6. FABRICATED REPAIRNov 5, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 08FDEA04753Angle · crackedDITCHING PAN ANGLE, JUST OTBD OF AIRSTAIR DOOR, LEFT SIDE IS CRACKED AT ALL FASTENER HOLES. REPLACED ANGLE REF DWR 65-29548. THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 5, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA04750Bracket · crackedNR 5 FLAP TRACK FAIRING BRACKET CLIP IS CRACKED LOCATED ON INBD SIDE, 20 INCHES FROM FWD END VERIFIED MATERIAL AS 7075-T6-.063 REF DWR 69-22882. REPLACEMENT MATERIAL SAME AS ORIGINAL, FABRICATED BRACKET FOR INBD SIDE OF NR 5 FLAP TRACK PER DWR 69-22882. TREANov 5, 2008 · N216FE · Boeing 7272S2F · Trailing Edge FlapsSDR 08FDEA04746Bracket · crackedNR 4 FLAP TRACK FAIRING BRACKET CLIP IS CRACKED LOCATED ON OTBD SIDE, 20 INCHES FROM FWD END VERIFIED MATERIAL AS 7075-T6-.063 REF DWR 69- 22882. REPLACEMENT MATERIAL SAME AS ORIGINAL, FABRICATED BRACKET FOR OTBD SIDE OF NR 4 FLAP TRACK PER DWR 69-22882. TRENov 5, 2008 · N216FE · Boeing 7272S2F · Trailing Edge FlapsSDR 08FDEA04740Intercostal · crackedCOCKPIT FLOOR SUPPORT INTERCOSTAL IS CRACKED BS 304, LBL 10, WL 208. REMOVED FIRE EXTINGUISHER BRACKET TO FOM REF SRM 51-30-2 P. 1. REMOVED DAMAGED INTERCOSTAL REF SRM 51-30-2. INSTALLED REPLACEMENT INTERCOSTAL REF SRM 51-30-2. REINSTALLED FIRE EXTINGUISNov 5, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA04739Strap · chafedMAIN CABIN FLOOR CHAFING ON "I" BEAM FLOORBEAM AT STA 740 FROM BL 0 TO RBL 50. REMOVED DAMAGED STRAP REF 51-30-02, FABRICATED REPLACEMENT STRAP REF EA 7-5310-118310. TREATED AND PRIMED REF AMM 51-20-151. INSTALLED NEW STRAP REF EA 7-5310-118310, WORKED WITHNov 5, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA04737Strap · chafedMAIN CARGO FLOOR, CHAFING ON "I" BEAM FLOORBEAM AT STA 740 FROM BL 0 TO BL 50. REPLACED STRAP AT 740, LBL 50 TO RBL 50 REF EA 7-5310-118310, WORKED WITH N/R N00390, THIS IS CLASSIFIED AS A MAJOR REPAIR.Nov 5, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA04703Shear Tie · corrodedLOWER AFT CARGO AREA, CORROSION ON SHEAR TIE AT RBL 11 BS 990, REMOVED CORROSION REF SRM 51-10-6 PG 5. MEASURED ORIGINAL "T" .043, .038 REMAINING REF NDT PART 4 51-00-00 FIG 2. REMOVED .005 OUT OF LIMITS REF SRM 53-10-1 DETAIL IV. REMOVED DAMAGE, FABRICATEDNov 4, 2008 · N216FE · Boeing 7272S2F · Fuselage Internal Mounting StructureSDR 08FDEA04694Stringer Clip · corrodedLOWER AFT CARGO AREA, CORROSION ON STRINGER CLIP AT KEEL BEAM CHORD STA 950E 3. REMOVED STRINGER CLIP, LOCATED AND DRILLED TO SIZE, TREATED AND PRIMED BARE METAL ON KEEL BEAM. INSTALLED NEW STRINGER CLIP REF SRM 51-30-2 PG 1, 51-10-2 PG 1. THIS IS CLASSIFIENov 4, 2008 · N216FE · Boeing 7272S2F · Fuselage Main, Attach FittingsSDR 08FDEA04666Rib · crackedLT WING LE RIB LWR CHORD IS CRACKED FSS 119, 17 INCH FROM SPAR REMOVED CRACKED AREA OF RIB FLANGE, FABRICATED AND INSTALLED REPAIR ANGLE REF SRM 51-40-3 FIG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 1, 2008 · N216FE · Boeing 7272S2F · Wing, Rib/BulkheadSDR 08FDEA04665Strap · crackedUPPER MAIN DECK FLOORBEAM STABILIZER STRAP CRACKED AT STA 324 LBL 23 WL 200. STOP DRILLED CRACK, INSTALLED REPAIR DOUBLER REF SRM 53-10-08 PG 36 FIG 6. THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 1, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA04664Strap · crackedMAIN DECK FLOORBEAM STABILIZER STRAP IS CRACKED BS 344 LBL 23 WL 200 STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER REF SRM 53-10-08 PG 36, FIG 6. THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 1, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA04663Intercostal · corrodedMAIN DECK FLOOR INTERCOSTAL IS CORRODED BS 312-328, LBL 30, WL 208. REMOVED CORROSION AND INTERCOSTAL AT STA 312 ORIGINAL THICKNESS .075 MATERIAL LOSS .025 REMAINING MATERIAL .050, FOUND OUT OF LIMITS. FABRICATED NEW INTERCOSTAL, INSTALLED NEW INTERCOSTAL ANNov 1, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA04662Flange · crackedMAIN DECK FLOOR E/E RACK STANTION SUPPORT INTERCOSTAL VERT FLANGE IS CRACKED BS 371 RBL 2 WL 199. REMOVED ANGLE VERIFIED MATERIAL ID FABRICATED NEW ANGLE INSTALLED NEW ANGLE AND WIRE BUNDLE CLAMP, REF SRM 51-30-2 PG 2, REF DWR 65-24297, REF MM 51-20-151 PG 1-Nov 1, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
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