Boeing 727-223

Service difficulty reports · 5,313

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = '727223'
  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 C8GA20080100Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 656.50. REPAIRED L/WING TANK FUEL VENT LINE AT WBL 656.50 IAW COTNEY ED NR EDAG52-1. FABRICATED DOUBLER FROM 2024 0.040 INCH DIM 1.625 INCH BNov 17, 2008 · N715AA · Boeing 727223 · Fuel StorageSDR C8GA20080098Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 601.50. REPAIRED LT WING TANK FUEL VENT LINE AT WBL 601.50 IAW COTNEY ED NR EDAG52-1. FABRICATED DOUBLER FROM 2024 0.040 INCH DIM 1.625 INCH Nov 17, 2008 · N715AA · Boeing 727223 · Fuel StorageSDR C8GA20080097Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 519. REPAIRED LT WING TANK FUEL VENT LINE AT WBL 519 IAW COTNEY ED NR EDAG52-1. FABRICATED DOUBLER FROM 2024 0.040 INCH DIM 1.625 INCH BY 4.2Nov 17, 2008 · N715AA · Boeing 727223 · Fuel StorageSDR C8GA20080096Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT TOP CLAMP WBL 442. REPAIRED LT WING TANK FUEL VENT LINE AT WBL 442 IAW COTNEY ED NR EDAG52-1. FABRICATED DOUBLER FROM 2024 0.040 INCH DIM 1.625 INCH BYNov 17, 2008 · N715AA · Boeing 727223 · Fuel StorageSDR C8GA20080095Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 383.50. REPAIRED LT TANK FUEL VENT LINE AT WBL 383.50 IAW COTNEY ED NR EDAG52-1. FABRICATED DOUBLER FROM 2024 0.040 INCH DIM 1.625 INCH BY 4.Nov 17, 2008 · N715AA · Boeing 727223 · Fuel StorageSDR C8GA20080094Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT TOP OF CLAMP WBL 348.00. REPAIRED LT WING TANK FUEL VENT LINE AT WBL 348 IAW ED NR EDAG52-1. LEAK CHECK GOOD. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RENov 17, 2008 · N715AA · Boeing 727223 · Fuel StorageSDR C8GA20080093Fitting · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE AFT I BEAM SUPPORT SHACKLE FITTING HAS EXFOLIATING CORROSION AT BS 307-0. REMOVED FITTINGS AND FABRICATED 2 NEW FITTINGS. INSTALLED NEW FITTINGS IAW DWG NR 69-45947-1-1 AND 51-30-1. NO ONov 17, 2008 · N715AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR C8GA20080092Skin · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING L/E WS 530 AT HOOK CUTOUT AFT REPAIR HAS CRACK. REMOVED PREVIOUS REPAIR, FABRICATED NEW PLATE FROM AISI 301 1/2 HARD .020 INCH DIM 8 INCH BY 6 INCH. INSTALLED REPAIR IAW SRM 57-30Nov 17, 2008 · N715AA · Boeing 727223 · Wing, Plate/SkinSDR C8GA20080091Intercostal · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE INTERCOSTAL WEB AT BS 490-510 STR 28R HAS CORROSION. REMOVED INTERCOSTAL AND FABRICATED ANGLE FROM 7075 T6 DIM 18.5". INSTALLED INTERCOSTAL AND FABRICATED ANGLE IAW B727 SRM 53-10-2, 51-3Nov 17, 2008 · N715AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR C8GA20080087Skin · dentedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS 2 EA DENTS WERE NOTED AT BS 575-583 BETWEEN STR. 26R-27R. CUT OUT 2 EA DAMAGED AREAS, FABRICATED DOUBLER, AND SHIMS. PERFORMED HFEC INSPECTION NO DEFECTS NOTED. INSTALLED REPAIR IAW DWG AG52-53-101. NO OTHER Nov 17, 2008 · N715AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR C8GA20080085Intercostal · brokenWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE INTERCOSTAL SKIN ATTACH FLANGE WAS BROKEN AT BS 950A - 950B STR 28L. REMOVED BROKEN INTERCOSTAL AND FABRICATED NEW. INSTALLED FABRICATED INTERCOSTAL IAW SRM 53-10-2 AND 51-20-1. NO OTHENov 17, 2008 · N715AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR C8GA20080086Skin · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT FUSELAGE SKIN IS CORRODED BELOW STR 28R AT BS 490-510.CORROSION OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED DOUBLER, FABRICATED 2 FILLERS. INSTALLED REPAIR IAW SRM 53-30-3. NO OTHER DEFECTS NNov 17, 2008 · N715AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR DHLA200800127Light · malfunctionedL1 DOOR EMERGENCY EXIT LIGHT REMAINS ON WHEN SWITCH IS IN THE OFF POSITION.Nov 15, 2008 · N752DH · Boeing 727223 · Emergency LightingSDR C8GA20080070Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT STRINGER 29L STA 950C - 1000 IS CORRODED. REMOVED AND REPLACED STRINGER 29L P/N 65-56441-7. INSTALLED STRINGER IAW SB 727-53-0179. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Nov 5, 2008 · N715AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR C8GA20080067Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STRINGER 29R WAS CORRODED UNDER BS 950E FRAME EXTENDING TO BS 1000. CORROSION AT STR. 29R WAS OUT OF LIMITS. CUT OUT DAMAGED STR 29R AT BS 950 TO 1006. INSTALLED NEW STRINGER P/N 65-56441-8. WORK PERFORMED IANov 5, 2008 · N715AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR C8GA20080064Stringer · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT STR. 27R LOCATED AT BS. 1010-1030 HAD EXFOLIATED CORROSION. REMOVED CORROSION, CORROSION AFTER CLEAN UP FOUND TO BE BEYOND LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR AT BS 950E-1010 PER EA ENov 5, 2008 · N715AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR C8GA20080084Structure · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE LOWER CHORD RUNNING ALONG STR 27R BY THE C2 DOOR IS CORRODED AND CRACKED AT BOTH ENDS, STA 950E-1010. CUT OUT DAMAGED AREA, PERFORMED HFEC INSPECTION AND FABRICATED REPAIR ANGLE FROM 7075Nov 1, 2008 · N715AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR C8GA20080083AIntercostal · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS SURFACE CORROSION WAS NOTED ON INTERCOSTAL BS 695 STR 27R. DAMAGED INTERCOSTAL WAS REMOVED, A NEW INTERCOSTAL WAS FABRICATED. INSTALLED REPAIR IAW SRM 53-10-2 AND 51-10-3. NO OTHER DEFECTS NOTED. AIRCRAFT WOct 29, 2008 · N715AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR C8GA20080083Frame · corrodedWHILE IN HEAVY PERFORMING INSPECTIONS IT WAS NOTED THAT THE FRAME WAS DENTED AT BS 1110 JUST ABOVE STR 26R CUT OUT DAMAGED FRAME AND FABRICATED NEW FRAME FROM 7075-O .063 INCH 23 INCH BY 4.5 INCH. HEAT TREATED FRAME TO T6. INSTALLED REPAIR IAW SRM 53-10-2 ANOct 29, 2008 · N715AA · Boeing 727223 · Fuselage Main, FrameSDR C8GA20080031Slat · malfunctionedFLT 715 FROM MEM TO TOL. DURING CLIMB OPERATION ON FLAP RETRACTION THE NR 7 LEADING EDGE DEVICE WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO MEM WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION OF THE NR 7 LEADING EDGE POSITION SWITCH WAS PERFORMED AOct 28, 2008 · N708AA · Boeing 727223 · Leading Edge Slat Control SystemSDR C8GA20080080Shear Tie · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT SHEAR TIE LOCATED AT STATION 580 STRINGER 26R-27R WAS CORRODED. REMOVED DAMAGED SHEAR TIE. FABRICATED NEW SHEAR TIE FROM 7075-O .071 INCH (8 INCHES X 2 INCHES) HEAT TREATED TO T6. INSTALLED NEOct 27, 2008 · N715AA · Boeing 727223 · Fuselage Internal Mounting StructureSDR C8GA20080074Support Angle · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE SUPPORT ANGLE LOCATED ABOVE STRINGER 26R AT BS 558 HAS SURFACE CORROSION. REMOVED CORRODED SUPPORT ANGLE AND FABRICATED SUPPORT ANGLE FROM 7075 O -.040 INCH (9 INCHES X 4.5 INCHES) HEAT TREATED TO T6. INSOct 27, 2008 · N715AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR C8GA20080069Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STRINGER 22L STA, 1183 ATTACH FITTING HAS EXFOLIATION CORROSION. REMOVED AND REPLACED ATTACH FITTING. PN 65-24276-29 IAW SRM 51-30-2. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Oct 24, 2008 · N715AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR C8GA20080068Stringer · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT STRINGER 22L WAS CORRODED AT B.S. 1177. DAMAGE WAS OUT OF LIMITS. CUT OUT DAMAGED AREA AT STR. 22L AT B.S 1177, FABRICATED 2 EA STR. REPAIR MATERIALS FROM BAC 1498-143 7075T6 (14 3/8" & 9 1/4")Oct 24, 2008 · N715AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR DHLA20087521022BWedge · delaminatedRIGHT WING INBD T/E FLAP ASSY MID FLAP T/E HAS AREA OF DELAMINATION AT OUTER T/E. 337 FILED AND MP9 FILED NR 26945. ALL REPAIR WORK COMPLIED WITH IAW BOEING SRM 51-40-20 PARA 7, 8, 10, 14, 20, 22. REMOVED DAMAGED AREA APPROX 4 INCH BY 4 INCH AND FABRICATED Oct 22, 2008 · N752DH · Boeing 727223 · Trailing Edge FlapsSDR DHLA20087521022AWedge · delaminatedLEFT WING INBD T/E FLAP ASSY INBD MID FLAP T/E APPROX 64 INCHES FROM OUTBOARD EDGE HAS AREA OF DELAMINATION AT PREVIOUS REPAIR. 337 FILED AND MP9 NR 26944 FILED. ALL REPAIR WORK COMPLIED WITH IAW BOEING SRM 51-40-20 PARA 7, 8, 9, 10, 14, 20, 22. AREA OF DAMOct 22, 2008 · N752DH · Boeing 727223 · Trailing Edge FlapsSDR C8GA20080076Angle · corrodedWHILE IN HEAVY MX, PERFORMING INSP IT WAS NOTED THAT AN L-ANGLE LOCATED AT STA 740 STR 27R-28R WAS CORRODED. REMOVED DAMAGED ANGLE AND FABRICATED NEW ANGLE FROM 7075-O .190 INCH (12 INCH X 10.5 INCH) HEAT TREATED TO T6. INSTALLED L-ANGLE IAW 727 DRAWING NR 65-Oct 20, 2008 · N715AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR C8GA20080075Angle · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE L-ANGLE LOCATED BETWEEN STRINGER 27L - 28L IS CORRODED AT STA 740. REMOVED CORRODED L-ANGLE AND FABRICATED NEW FROM 7075 O -.090" (10.6250 INCH X 7.6258 INCH)HEAT TREATED TO T6. INSTALLED (L) ANGLE. IAW DOct 20, 2008 · N715AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR C8GA20080072Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STRINGER 28L STA 492 HAD CORROSION. CUT OUT DAMAGE AT STA 492 FABRICATED NEW ANGLE SUPPORT FROM 7075 T6 18, .5 INCH, FABRICATED STRINGER REPAIR STA. 480 -510 FROM P/N BAC 1498-141 7075 T6, FABRICATED 2EA SPLOct 16, 2008 · N715AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR C8GA20080063Stringer · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT STR 28R LOCATED AT BS. 490-510 HAD CORROSION. REMOVED DAMAGED SECTION OF STR 28R FROM BS 480-508. FABRICATED NEW STRINGER, FABRICATED 2 EA SPLICES. INSTALLED NEW PARTS IAW SRM 53-10-3, 51-30-Oct 16, 2008 · N715AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR C8GA20080081Shear Tie · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT SHEAR TIE LOCATED AT STA 990 STRINGER 29R WAS CRACKED. REMOVED DAMAGED SHEAR TIE. FABRICATED NEW SHEAR TIE FROM 7075-O .063 INCH (4.380 INCH X 2 INCH) HEAT TREATED TO T6. INSTALLED NEW SHEAR TIE IAW 53-10-4, Oct 15, 2008 · N715AA · Boeing 727223 · Fuselage Internal Mounting StructureSDR C8GA20080071Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT STRINGER 26L STATION 540 - 560 IS CORRODED. CUT OUT DAMAGE AT STA 533-550. FABRICATED STRINGER FROM BAC 1498-143 7075T6, 16 INCH, FABRICATED 2 EA SPLICE PLATES FROM BAC 1498-132 7075 T6, 13 INCHES INSTALLED Oct 15, 2008 · N715AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR C8GA20080066Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT RIVETS WERE PULLING THROUGH THE SKIN EXTERIOR AT BS 1010 STR 28R. CORROSION ON STR 28R TO BE OUT OF LIMITS. CUT OUT DAMAGED STR 28R AT B.S 1010 TO + 11.375. FABRICATED NEW STRINGER REPAIR SPLICE FROM BAC 1498Oct 13, 2008 · N715AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR C8GA20080061Seat Track · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE MAIN CABIN SEAT TRACK LOCATED AT BS. 760-850, LBL 45.5 HAD CORROSION. REMOVED SEAT TRACK FROM STATION 760-850, FABRICATED NEW SEAT TRACK, INSTALLED NEW SEAT TRACK IAW SRM 53-10-2, 53-10-5 Oct 13, 2008 · N715AA · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR C8GA20080079Shear Tie · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT SHEAR TIE LOCATED AT STA 660 STRINGER 26R-27R WAS CORRODED. REMOVED DAMAGED SHEAR TIE. FABRICATED NEW SHEAR TIE FROM BAC 1506-1630 7075-T6 (6.5 INCH) INSTALLED SHEAR TIE IAW 51-30-2, 51-10-2. NO OTHER DEFECTSOct 10, 2008 · N715AA · Boeing 727223 · Fuselage Internal Mounting StructureSDR C8GA20080078Shear Tie · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT SHEAR TIE LOCATED AT STA 640 STRINGER 26L-27L WAS CORRODED. REMOVED DAMAGED SHEAR TIE. FABRICATED NEW SHEAR TIE FROM BAC 1506-1630 7075-T6 (6.75 INCH) INSTALLED SHEAR TIE IAW 51-30-2, 53-10-2. NO OTHER DEFECTOct 10, 2008 · N715AA · Boeing 727223 · Fuselage Internal Mounting StructureSDR C8GA20080077Shear Tie · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT SHEAR TIE LOCATED AT STA 620 STRINGER 26L-27L WAS CORRODED. REMOVED DAMAGED SHEAR TIE. FABRICATED NEW SHEAR TIE FROM BAC 1506-1630 7075-T6 (6.75 INCHES) INSTALLED SHEAR TIE IAW 51-30-2, 53-10-2. NO OTHER DEFEOct 10, 2008 · N715AA · Boeing 727223 · Fuselage Internal Mounting StructureSDR DHL2008F00046Bracket · crackedNR 4 SLAT ACTUAROT MOUNT BRACKET CRACKED AT BOTTOM SIDE LWS 410. R&R MOUNT BRACKET IAW SRM 51-10-1 AND 51-30-2. OPS AND LEAK CHECKED OK IAW MM 27-81-32 & 28-11-21.Oct 1, 2008 · N780DH · Boeing 727223 · Leading Edge DevicesSDR C8GA20080062Stringer · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT STR 25R LOCATED AT BS 720E +4 , HAD EXFOLIATED CORROSION. REMOVED DAMAGED SECTION OF STR. FABRICATED NEW STRINGER, FABRICATED SPLICE, INSTALLED NEW PARTS IAW SRM 53-10-3, 53-10-2 NO OTHER DEFESep 30, 2008 · N715AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR C8GA20080060Seat Track · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE MAIN CABIN SEAT TRACK LOCATED AT BS. 760-850, LBL 45.5 HAD CORROSION. REMOVED SEAT TRACK FROM STATION 760-850, FABRICATED NEW SEAT TRACK, INSTALLED NEW SEAT TRACK IAW SRM 53-10-2, 53-10-5 Sep 29, 2008 · N715AA · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR C8GA20080041Skin · misrepairedWHILE IN HEAVY MAINTENANCE PERFORMING VISUAL INSPECTION FOR DTA. EXISTING EXTERNAL DOUBLER/TRIPLER REPAIR AT BS 950E TO 990 29R IS NON-COMPLIANT. REMOVED EXISTING REPAIR CLEANED AND VERIFIED CRACK CONTAINMENT. FABRICATED TRIPLER AND FABRICATED DOUBLER. FABRICASep 13, 2008 · N713AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR C8GA20080037Skin · crackedWHILE IN HEAVY MAINTENANCE PERFORMING MFEC INSPECTION MULTIPLE FASTENER HOLES WERE NOTED AS CRACKED AT UPPER FUSELADGE SKIN LAP SEAM 4R BETWEEN BS 481-681. CUT OUT UPPER AND LOWER SKINS, VERIFIED CRACK CONTAINMENT. FABRICATED LAP SEAM FILLER, REPAIR DOUBLER ANSep 6, 2008 · N713AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR C8GA20080034Nose Cowl · dentedWHILE IN HEAVY MAINTENANCE PERFORMING VISUAL INSPECTION ON THE NR 1 ENGINE NOSE COWL A DENT WAS NOTED AT THE 1 O'CLOCK POSITION. EVALUATED DENT AND FOUND A/Y RATIO OUT OF LIMITS. CUT OUT DAMAGED AREA AND FABRICATED INTERNAL DOUBLER OF 2024 T3 .040, FABRACATED Sep 4, 2008 · N713AA · Boeing 727223 · Nacelle/Pylon, Plate/SkinSDR C8GA20080035Skin · damagedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION A CRACK WAS NOTED ON THE EXTERIOR OF THE FUSELAGE BS 254 STRINGER 10 LEFT. CUT OUT DAMAGED SKIN, VERFIED CRACK CONTAINEMENT WITH NDT. FABRICATED FILLE AND FABRICATED DOUBLER. INSTALLED FILLER AND DOUBLER IAW SRMSep 3, 2008 · N713AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR C8GA20080057Support · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE RIGHT WING IB AILERON TAB HAS DELAMINATION. REMOVED DAMAGED AREA, FABRICATED CORE. FABRICATED DOUBLER. INSTALLED REPAIR HOT BONDED & SEALED CORE AND DOUBLER. IAW SRM 51-40-20. NO OTHER DEFEAug 25, 2008 · N713AA · Boeing 727223 · Aileron TabsSDR C8GA20080052Skin · gougedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT IB FOREFLAP AT THE UPPER SURFACE HAS A 10" GOUGE. REMOVED DAMAGED SKIN, FABRICATED CORE. FABRICATED DOUBLER. HOT BONDED CORE AND DOUBLER SEALED EDGES IAW SRM 51-40-20. NO OTHER DEFECTS NAug 25, 2008 · N713AA · Boeing 727223 · Trailing Edge FlapsSDR C8GA20080050Tab · dentedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION LEFT WING OUTBOARD AILERON TAB HAD A DEEP DENT. REMOVED DAMAGE AND FABRICATED CORE & HOT BONDED. FABRICATED DOUBLER, HOT BONDED AND SEALED DOUBLER IAW SRM 51-40-20. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED Aug 25, 2008 · N713AA · Boeing 727223 · Aileron TabsSDR C8GA20080045Seat Track · elongatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION NOTED THAT THE MAIN CABIN SEAT TRACK HAS ELONGATED SLOTS AT BS. 720B-740 LBL 45.0. REMOVED 2 EA SEAT TRACK AT LBL 45 BS. 640-740 DISPLACED SPLICE PER DWS 2902 INSTALLED NEW SEAT TRACK IAW SRM 51-30-2, 53-10-5. NAug 24, 2008 · N713AA · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR C8GA20080044Seat Track · damagedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION NOTED THAT THE MAIN CABIN SEAT TRACK HAS ELONGATED HOLES AT BS. 720A -720D LBL 24.75. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2, 53-10-5. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.Aug 24, 2008 · N713AA · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR C8GA20080043Structure · damagedWHILE IN HEAVY MAINTENANCE EXISTING REPAIR AT BS 1133 BETWEEN STR. 21R - 22R REQUIRES REPLACEMENT. REMOVED EXISTING REPAIR, CUT OUT DAMAGE, FABRICATED FILLER, FABRICATED DOUBLER. INSTALLED REPAIR IAW SRM 53-30-2, 53-30-8. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RAug 24, 2008 · N713AA · Boeing 727223 · Fuselage Main, Structure
Back to Boeing 727-223