Pratt & Whitney JT8D-15

Service difficulty reports · 2,710

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 engine_model_key = 'JT8D15'
  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 FDEA201008102902Skin · misrepairedIMPROPER REPAIR INSTALLED AT STA 1183-1200 S23-24L ACCOMPLISHED REPAIR AT BS 1183-1200 S23-24L, FABRICATED DOUBLER FROM 2024T3 0.080" DIM. 16 3/4 X 17 1/4", FILLER 2024T3 0.071" DIM. 4 1/4" X 9 1/2" AND 7 1/2" X 1" STRUCTURAL FILLER PER SRM 53-30-3 FIG 3A. INSAug 10, 2010 · N487FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201008072867Bleed Valve · lack of lubeWHILE CLIMBING THROGH FL305, NR 2 ENGINE, EXPERINCED ABOUT 5 COMPRESSOR STALLS. ENGING BEHAVED NORMALLY AFTER RETARDING NR 2 THRUST LEVER. ACFT WAS IN CLEAR AIR WITH ENGINE ANTI-ICE CLOSED. ABOUT 5 MINUTES EARLIER ACFT WAS IN MODERATE PRECIPITATION WITH ENAug 7, 2010 · N481FE · Boeing 727227 · Compressor Bleed ValveSDR 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 FDEA201008062869Switch · failedNR 6 LED FAILED TO RETRECT. NR 6 SLAT EXTEND LIGHT ON SO'S PANEL REMAINS ON AT ALL FLAP POSITIONS. WITH THE NR 6 SLAT CONNECTOR PLUG DISCONNECTED THE EXTEND LIGHT WILL EXTINGUISH. WITH THE JUMPER WIRE INSTALLED THE RETRACT REMAINS ON AT ALL FLAP SETTINGS AGAug 6, 2010 · N482FE · Boeing 727227 · Leading Edge Slat Control SystemSDR FDEA201008062885Light · inoperativeEXTERNAL L1 DOOR LOWER EMERGENCY LIGHT INOP. RELAMPED ESCAPE SLIDE LIGHT, NO HELP. R & I EMERGENCY ESCAPE SLIDE LIGHT BATTERY & POWER SUPPLY IAW MM 33-50-051-2-0 . OPS CK'S NORMAL. PREMATURE REMOVAL/INSTALLATION. RELAMPED ESCAPE SLIDE LIGHT, NO HELP.Aug 6, 2010 · N492FE · Boeing 727227 · Emergency LightingSDR FDEA201008062886Battery Pack · inoperativeEMERGENCY LIGHTS GO DIM IN 30 SECONDS. REPLACED BATTERIES COCKPIT O/H EMERGENCY LIGHT PACK IAW MM 33-50-101-2-0. OPS CKS GOOD.Aug 6, 2010 · N492FE · Boeing 727227 · Emergency LightingSDR FDEA201008052850Skin · crackedMCD CUTOUT UPPER SILL BS 485, 487, & 495 SILL UPPER FLANGE HAS CRACK INDICATION AT 3 EA RIVET HOLES. REMOVED DAMAGED MCD UPPER SILL, LOCATED & DRILLED NEW SILL & INSTALLED NEW SILL BEAM IAW EA 7-5310-135582.Aug 5, 2010 · N494FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201008052851Skin · crackedMCD CUTOUT UPPER SILL BS 605 & 615 HAS UPPER FLANGE WITH CRACK INDICATION AT (2 EA) RIVET HOLES. REMOVED DAMAGED MCD UPPER SILL, LOCATED & DRILLED NEW AFT SILL & INSTALLED NEW SILL UPPER SILL BEAM IAW EA 7-5310-135582.Aug 5, 2010 · N494FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201008052855Light · failedCLOSE RT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. R & R SAME IAW MM 33-50-101-2-0. OPS CHECK GOOD, ACFT GOOD FOR CONT SERVICE.Aug 5, 2010 · N486FE · Boeing 727227 · Emergency LightingSDR 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 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 C8GA201000014Control Valve · inoperativeDURING CLIMB OPERATION WITH THE RT PACK ON DMI. THE LT PACK WOULD NOT MAINTAIN CABIN ALTITUDE. ACFT LEVELED OF AT 18,000 FT THE CABIN CONTINUED TO CLIMB AT A RATE OF 500 FT/MIN WITH CARGO HEAT OUTFLOW VALVE AND OUT FLOW VALVE CLOSED. THE ACFT RETURNED TO DEPARAug 3, 2010 · N898AA · Boeing 727223 · Cabin Cooling SystemSDR 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 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 FDEA201007272684Skin · gougedRT INBD FORE FLAP GOUGED AT OTBD LOWER L/E SURFACE. CUT OUT DAMAGED AREA OF SKIN DIM. 1/2" X 1 1/2" IAW SRM 57-50-4 FIG1. FABRICATED REPAIR DOUBLER FROM 2024 T-3 .063" DIM. 3 7/8" X 4 1/2" IAW SRM 57-50-2 FIG 3 AND 57-50-4 FIG 1. INSTALLED REPAIR DOUBLER IAJul 27, 2010 · N487FE · Boeing 727227 · Trailing Edge FlapsSDR FDEA201007262879Seat Track · corrodedSEAT TRACK CORRODED, STA 480-600, BL0, REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178 T6511, DIMS 120" AND INSTALLED IAW P-F SRM 53-10-2 AND SRM 51-30-2.Jul 26, 2010 · N487FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201007242870Seat Track · corrodedSEAT TRACK CORRODED ON BOTH FLANGES STA 380-480 LBL 45. REMOVED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION USING BAC1520- 792 7178-T6 DIMS 136" AND INSTALLED IAW SRM 53-10-5 AND P-F SRM 53-10-2.Jul 24, 2010 · N487FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201007232882Skin · dentedDENT ON LAP SEAM, STA 1112, STR 20R. CUT OUT DAMAGED AREA DIMS 4" X 2 1/4". FABRICATED REPAIR DOUBLER USING 2024T-3 .071 DIMS 11.75" X 9.25", FABRICATED FILLER USING 2024T-3 .080 DIMS 11.5" X 9" , FABRICATED FILLER USING 2024T-3 .080 DIMS 2.25" X 1.3" AND IJul 23, 2010 · N487FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201007202901Skin · misrepairedIMPROPER REPAIR INSTALLED STA 1175 TO 1183, STR'S 23L TO 24L. REMOVED PREVIOUS REPAIR AT STA 1175 TO 1183 STR 23-24L IAW SRM 51-30-2. ACOMPLISHED REPAIR PER EA 7-5330-135578.Jul 20, 2010 · N487FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201007192596Structure · crackedRT WING, INBD FLAP, MID FLAP, AFT CHORD IS CRACKED AT WBL 112. CUTOUT SECTION CHORD CRACKED AT RT WING INBD FLAP MIDFLAP WBL 112 DIM: 47.6250" IAW SRM 51-40-4, FIG 1 AND FABRICATED SECTION CHORD FROM BAC 1503100046 7075T6 DIM: 47.6250 " & SPLICE DIM: 8.5" IAW Jul 19, 2010 · N265FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA201007132500Stringer · corrodedCORROSION ON STR 28L AT STRINGER SPLICE BS 1015.Jul 13, 2010 · N265FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201007062371Skin · corrodedCORROSION - UPPER SKIN, EXTERIOR SURFACE OF WING CTR SECTION FUEL TANK. APPROX BS 825, RBL 12. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-10-6 AND 57-30-1 FIG 4. REPAIRED AREA IAW EA 7-5730-142035.Jul 6, 2010 · N265FE · Boeing 727233 · Wing, Plate/SkinSDR FDEA201006232116Engine · stalledNR 2 ENGINE COMPRESSOR STALL/SURGE AT LEVEL OFF - FL340 EPR WAS OBSERVED TO GO DOWN TO 1.6 EPR WITH ENGINE VIBRATION NOISE ASSOCIATED WITH COMPRESSOR STALL. AIRTURN BACK. R & R NR 2 ENGINE AS PER WORK CARD 70T0002 AND TESTED PER WORK CARD 70T0301-02. ALLJun 23, 2010 · N220FE · Boeing 727233 · Engine (Turbine/Turboprop)SDR 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 C8GA201000010Cover · damagedAFTER STARTING THE TAKEOFF ROLE, THE UPPER YAW DAMPER "OFF" LIGHT ILLUMINATED. THE CREW PERFORMED AN ABORTED TAKEOFF AND RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED NOTING THAT THE LIGHT COVER WAS STUCK IN SOCKET. PERFORMED GROUND TJun 22, 2010 · N898AA · Boeing 727223 · Instrument PanelSDR CA100622024Bolt · shearedA PORTION OF THE BOLT AND A BUSHING (PN NAS72-7E007) WAS DISCOVERED ON A TAXIWAY USED BY ACFT EARLIER IN THE DAY. THE ACFT WAS INSPECTED, AND THE PART WAS FOUND BE MISSING FROM THE LT WING, INBD FLAP, OTBD FLAP CARRIAGE ASSY. THE ACFT WAS TAKEN OUT OF SERVICJun 21, 2010 · Boeing 727247 · Trailing Edge FlapsSDR FDEA201006152014Fire Warning · false activationON CLIMBOUT, GLARESHIELD FIRE WARNING LIGHTS ILLUMINATED DIMLY, FOLLOWED A MINUTE LATER BY AN APU FIRE WARNING LIGHT. FIRE WARNING LIGHTS STAYED ON APPROX 15-20 SECONDS. APU FIRE WARNING REMAINED ON UNTIL IN CHOCKS. PULLED APU FIRE HANDLE, DISCHARGED APU FIRJun 15, 2010 · N284FE · Boeing 727233 · Smoke DetectionSDR FDEA201006041825Fitting · corrodedCORROSION ON LOWER CHORD AT BS 950, STRINGER 30. REMOVED LOWER CHORD SPLICE AT BS950, BL 0, IAW SRM, REV 103, 51-30-2. LOCATED, DRILLED AND DEBURRED LOWER CHORD SPLICE FITTING IAW SRM 51-30-5. INSTALLED LOWER CHORD SPLICE FITTING IAW SRM 51-30-2.Jun 4, 2010 · N267FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR FDEA201006031801Seat Track · corrodedCORROSION SEAT TRACK FLANGE MAIN CABIN BS 680 TO BS 620, LBL 45. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 480 - 690 LBL 45 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 APPROX DIM: 209" .5, FABRICATED SPLICE ANGLES FROM BAC 1503-100122 APPROX DIJun 3, 2010 · N267FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201006021802Structure · corrodedCORROSION AT REINFORCEMENT CHORD, BS 1176, MAIN CABIN, LBL 46. REMOVED REINFORCEMENT CHORD BS 1176, LBL 46, IAW SRM 51-30-2 AND FABRICATED NEW REINFORCEMENT CHORD, MATERIAL PN 65-31773-1 DIM: 33" IAW DWG NR 65-31773. INSTALLED NEW REINFORCEMENT CHORD IAW IAW Jun 2, 2010 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR C8GA201000010AActuator · malfunctionedWHILE ON APPROACH WITH THE GEAR HANDLE IN THE DOWN POSITION THE NLG UNSAFE LIGHT ILLUMINATED. CREW PERFORMED APPROPRIATE CHECKLIST AND RECYCLED GEAR WITH ALL INDICATIONS NORMAL. ACFT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. R & R NLG LOCK AJun 2, 2010 · N899AA · Boeing 727223 · Landing Gear Door Retract SectionSDR FDEA201005241637Skin · gougedRT INBD FOREFLAP OTBD END L/E PREVIOUS REPAIR, GOUGED. REMOVED PREVIOUS REPAIR ON RT INBD FOREFLAP OTBD END IAW SRM 51-30-2 FABRICATED NEW REPAIR IAW SRM 57-50-4, FIG 1, REV 102. INSTALLED NEW REPAIR IAW SRM 51-30-2.May 24, 2010 · N268FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA201005181577Stringer Clip · corrodedCORROSION - STRINGER 26L AT STA 1183 TENSION TIE FITTING, INSIDE CHANNEL. REMOVED SECTION OF STRINGER 26L AT STA 1183, 20" IN LENGTH IAW SRM, REV 102, 51-30-2, 51-10-1, AND 53-10-1 FIG 1. FABRICATED STRINGER USING BAC1498-145, 7075-T6, 20" IN LENGTH. FABRICMay 18, 2010 · N483FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR FDEA201005181576Seat Track · corrodedCORROSION SEAT TRACK FLANGE MAIN CABIN BS. 620, RBL 24. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK AT RBL 24 BS 540+10" FROM BAC 1520-792-7178-T6511 IAW SRM 53-10-5 FIG 1 REV 102 INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.May 18, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201005171769Beam · damagedAFT PIT BS 1183, VERTICAL BEAM AT LBL 17.8 HAS FASTENERS WITH ZERO SPACING. TRIMMED OUT BEAM AFT FLANGES AND BULKHEAD WEB 8 PLACES IAW EA 7-5310-135541. FABRICATED REPAIR DOUBLER, REPAIR ANGLES, FILLERS, BULKHEAD WEB FILLERS, STRAP DOUBLER, STIFFENER SHIMS, May 17, 2010 · N268FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201005141591Stringer · corrodedCORROSION ON STRINGER 27L AT BS 950B 5". CORROSION OUT OF LIMITS. CUT OUT DAMAGED SECTION 18", FABRICATED FILLER USING BAC1498-147 7075T-6 DIMS 18", SPLICES USING BAC1498-131 7075T-6 DIMS 13" AND 12.5" AND INSTALLED IAW SRM 51-30-2, 53-10-1, 53-10-3 AND 51-May 14, 2010 · N268FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201005131535Rib · crackedLT WING NR 2 L/E SLAT INBD & OTBD RIBS ARE CRACKED WHERE ACTUATOR ROD END MOUNTS. R & R INBD & OTBD ACTUATOR RIBS PN 65-17310-3 & 65-17310-4, FABRICATED 1 EA OTBD RIB APPROX WS 251 FROM 7075-O .040 DIM: 16.25" X 6" & FABRICATED NEW ACTUATOR RIB CHANNEL FROMay 13, 2010 · N483FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201005131619Door Frame · crackedL-1 ENTRY DOOR FRAME, STA 303.9, STR 16L, CRACK ON WEB CUTOUT. CUTOUT AREA ON WEB DIM 1.25" X .70" AT BS 303.9 AT STR 16L IAW FEDEX EO 7-5310-7-3362 P7. DRILLED AND LOCATED PARTS FROM FEDEX KIT P/N 5314757 IAW SRM 51-30-5. INSTALLED WEB REPAIR AT BS 303.9 AMay 13, 2010 · N268FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA201005121521Spar · crackedLT WING T/E FALSE SPAR CHORD CRACKED, WBL 118. REPAIRED LT WING T/E FALSE SPAR CHORD WBL 118 IAW DWG NR SR27-57-038, REV C.May 12, 2010 · N268FE · Boeing 727233 · Wing SparSDR FDEA201005121524Floorbeam · corrodedCORROSION FLOORBEAM TOP MAIN CABIN BS 480 BL 0 TO RBL 25. CUT DAMAGE OUT AREA 2.5" X 2", FABRICATED UPPER CHORD FROM BAC 1505-100617 DIM: 14.5" AND INSTALLED FLOORBEAM REPAIR IAW SRM 53-10-8 FIG 3, REV 102 AND SRM 51-30-2.May 12, 2010 · N483FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201005121525Spar · crackedRT WING T/E FALSE SPAR CHORD CRACKED, WBL 118.May 12, 2010 · N268FE · Boeing 727233 · Wing SparSDR FDEA201005121525ABulkhead · crackedCRACK FOUND AT BS 1183 BULKHEAD WEB AT RBL 24, WL 170.May 12, 2010 · N268FE · Boeing 727233 · Fuselage Main, BulkheadSDR FDEA201005121589Skin · damagedMAIN CARGO DOOR AREA, BS 660, STR 3L, NOT ENOUGH DISTANCE BETWEEN FASTENERS. CUT OUT AREA DIM, 2.75" IAW SRM 53-10-3. FABRICATED STRINGER SECTION FROM BAC-1498-139-7075T6 DIM. 2.75", 2 SHIMS FROM 2024T3 .080" DIM. .75" X 4", PLATE FROM 2024T3 .125" DIM 13" X May 12, 2010 · N268FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201005121590Skin · damagedMAIN CARGO AREA, BS 660, STR 3L-4L, DOUBLE DRILLED HOLES ON BONDED STRAP. CUT OUT AREA DIM. 1.5" X 3.5" AND 1" X .75" IAW SRM 53-30-3. FABRICATED FILLER FROM 2024T3 .090" DIM. 19.5" X 8", DOUBLER FROM 2024T3 .080" DIM. 17.6" X 11.5", TRIPLER FROM 2024T3 .May 12, 2010 · N268FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201005121523Spar · crackedRT WING T/E FALSE SPAR CHORD CRACKED, WBL 118. REMOVED LOWER CHORD DIM. 20.5", WEB AND DOUBLER IAW DWG NR SR 27-57-038, REV C. FABRICATED 2 ANGLES FROM 7075-0 .071" DIM. 14.5" X 2.75" AND 12.5" X 2.75" IAW DWG NR SR 27-57-038 REV C. HEAT TREATED ANGLES FROM 7May 12, 2010 · N268FE · Boeing 727233 · Wing SparSDR FDEA201005111505Stringer · crackedSTRINGER 22L CORRODED, BETWEEN STA 1166 - 1183, UPPER SURFACE OF UPPER CHANNEL. CUTOUT DAMAGED SECTION OF STRINGER DIM: 25" .3750 AT STA 1166-1183 IAW SRM 53-10-3, FIG 1. FABRICATED STRINGER REPAIR FROM BAC 1498-143 7075T62 DIM: 25" .3750 & SPLICE FROM BAMay 11, 2010 · N483FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR FDEA201005111506Skin · corrodedCORROSION, EXTERIOR SURFACE - T/E LOWER RADIUS LIP AT LT AFT LAV SERVICE DOOR CUT OUT. APPROX BS 1180, ABOVE STR 22L. REMOVED SKIN TRIPLER AT EXTERIOR SKIN T/E LOWER RADIUS LIP AT AFT LAV SERVICE DOOR BS 1180 STR 22L IAW SRM 51-30-2 AND FABRICATED NEW SKIN TRMay 11, 2010 · N483FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201005101522Seat Track · corrodedUPPER LOWER FLANGE OF MAIN CABIN SEAT TRACK HAS SURFACE CORROSION BS 850 - BS 870 RBL 45. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 850 - BS 870 RBL 45, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-1466-7178T6 DIM: 16" & INSTALLED NEW SEAT TRACK IAW SRM May 10, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201005091518Seat Track · crackedCRACK SEAT TRACK MAIN CABIN RBL 24 BS 995 SECTION OF TRACK IS BS 950, 10" TO BS 1135. REMOVED DAMAGED SEAT TRACK BS 950, 10" TO BS 1135 RBL 24 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK FROM BAC 1520-7927178T6511 DIM: 25' LONG IAW SRM 53-10-5 FIG 1. INSTAMay 9, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201005081517Seat Track · corrodedSURFACE CORROSION MAIN CABIN SEAT TRACK BS 870 - BS 950, LBL 24. REMOVED SEAT TRACK SECTION, FABRICATION NEW SEAT TRACK SEC FROM BAC 1520-792 717896 DIM: 7' 19", INSTALLED NEW SEAT TRACK SECTION, IAW SRM 51-30-2, 53-10-5 FIG 1 AT MAIN CABIN BS 870 - 950 LBL May 8, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
Back to Pratt & Whitney JT8D-15