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 07FDEA03115Stringer Splice · corrodedAFT PIT BILGE BODY FRAME STR SPLICE IS CORRODED, BS 1008-1012, STR 29L, WL 140. REMOVED STRINGER SPLICE, CLEANED DAMAGE HOLE, HFEC STRINGER, FABRICATED STRINGER SPLICE. FABRICATED STRINGER CLIPS, TREATED AND PRIMED PARTS, PERFORMED HIDDEN DAMAGE INSPECTION. Aug 24, 2007 · N286FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 07FDEA03114Floor Support · corrodedFWD CARGO AREA, STA 718, STR 29L, ABOUT LBL 2, FLOOR SUPPORT IS CORRODED ON REPAIR ANGLE REMOVED DAMAGE. FABRICATION REPAIR PART, TREATED AND PRIMED REPAIR PARTS AND INSTALLED. THIS REPAIR IS CLASSIFIED AS MINOR.Aug 24, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA03113Stringer Clip · corrodedFUSELAGE, BS 740, S-27L, 2 STR CLIPS CORRODED REMOVED CLIPS, REMOVED CORROSION AND CLIPS ARE OUT OF LIMITS. FABRICATED NEW CLIPS, TREATED AND PRIMED AND INSTALLED. REF BOEING DOCUMENT DRAWING NR 69-45628/ID NR 0001/FRAME NR 1 CLASSIFIED AS A MAJOR REPAIR.Aug 24, 2007 · N286FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA03112Stringer Clip · corrodedFWD LWR CARGO PIT BILGE STRINGER TIE, ON PRESSURE BULKHEAD HAS CORROSION, STA 740, STR 27R. REMOVED CORRODED STRINGER TIES, FABRICATED NEW STRINGER TIES, AND INSTALLED. REF BOEING DRAWING NR 69-45628 AND SRM 51-30-02. THIS IS CLASSIFIED AS A MAJOR REPAIR.Aug 24, 2007 · N286FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA03111Angle · crackedFWD PIT BILGE BODY SKIN STIFFENER IS BUCKLED/CRACKED, BS 720B PLUS 13" 5", IB OF STR 28R, WL 148. REMOVED DAMAGE SUPPORT ANGLE AND INSTALLED NEW SUPPORT ANGLE, REF BOEING DWG NR 65-54577 AND SRM 51-30-2, THIS IS CLASSIFIED AS A MAJOR REPAIR.Aug 24, 2007 · N286FE · Boeing 727233 · Fuselage Main, StructureSDR 07FDEA03099Angle · corrodedFWD LOWER CARGO BAY REINFORCING ANGLE DOUBLER AT AT BS 740 BULKHEAD STR S-27R IS CORRODED REMOVED CORRODED REINFORCING ANGLE. REMOVED CORROSION AND ANGLE WAS OUT OF LIMITS. FABRICATED NEW REINFORCING ANGLE ON SNRM NR N01045, 8130 FORM TRACKING 2007-06-143. Aug 24, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA03098Stringer · corrodedFWD CARGO AREA, STA 700 TO 705, STR 28R, AT RBL 4 TO RBL 7, STRINGER IS CORRODED REMOVED CORRODED SECTION OF STRINGER FROM STA 680 TO STA 720 AND INSTALLED NEW SECTION REF SRM 51-30-2, AND BOEING DOCUMENT NUMBER 65-54577, ID NR 0004/FRAME NR 1.Aug 24, 2007 · N286FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 07FDEA03095Shear Tie · corrodedLOWER FUSELAGE SKIN ATTACH ANGLE TO FAIRING WEB SUPPORT HAS CORROSION AT BS 720F AND RBL 11-22. REMOVED CORRODED ANGLE AND 65-25577-14 REPLACED. REFERENCE SRM 51-30-02 AND BOEING DOCUMENT NR 65-25577/ID NR 0003/FRAME NR 1, THIS IS CLASSIFIED AS A MINOR REPAIAug 24, 2007 · N286FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 07FDEA03094Web · corrodedAFT UPPER MAIN DECK, CORROSION ON UPPER SHEAR DECK, UNDER FLOORBOARDS, STA 1166 PLUS 8", RBL 17" TO RBL 36" (BETTER VIEW FROM LWR AFT PIT) REMOVED SEAT TRACK AT STA 1128 - 1178, RBL 25 AND 45. REMOVED ATTACHING STRUCTURE FOR SHEAR WEB REMOVAL. REMOVED SHEAAug 24, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA03093Seat Track · corrodedMAIN CABIN FLOOR SEAT TRACK IS CORRODED AT STA 1090, RBL 24 BLENDED CORROSION. ORIGINAL "T" .090", REMOVED .025" OUT OF LIMITS REF SRM 51-10-1 PG 15. FABRICATED REPLACEMENT SEAT TRACK, FABRICATED SPLICE REPAIR PARTS, TREATED AND PRIMED SEAT TRACK AND REPAIR Aug 24, 2007 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA03092Seat Track · corrodedUPPER MAIN CARGO DECK FLOOR STRUCTURE, SEAT TRACK BETWEEN STA 1130 TO 1166 PLUS 8", RBL 25", HAS CORROSION ON LOWER FAYING SURFACE AT AFT END. FABRICATED NEW SEAT TRACK, REF DWG 53FX 976, SEAT TRACK INSTALLED ON N/R N00816. THIS IS CLASSIFIED AS A MAJOR REPAAug 24, 2007 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA03078Frame · failedON AGING, A/C INSP FOUND EXISTING REPAIR ON FRAME AT BS 700 BETWEEN STR 24L AND 26L DID NOT CONFORM TO SRM 51-40-3. REMOVED EXISTING REPAIR, FABRICATED REPAIR, HFEC FRAME TRIM OUT, NO CRACKS EXIST. INSTALLED FORMED REPAIR. REF FED EX EA 7-53-113940. THIS IAug 23, 2007 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA03069Beam · crackedMAIN DECK 1L ENTRY DOOR SN 24, BOTTOM CROSS BEAM WEB IS CRACKED AT AFT STOP FITTING. REMOVED STOP FITTING, REMOVED DAMAGE, REPAIRED WEB. INSTALLED DOUBLER AND REINSTALLED STOP FITTING REF SRM 51-40-2 AND FED EX DWG SR27-52-015, THIS IS CLASSIFIED AS A MAJOR Aug 23, 2007 · N262FE · Boeing 727233 · Passenger/Crew DoorsSDR 07FDEA03067Web · corrodedLWR AFT CARGO PIT DOOR CUTOUT, LWR SILL SLANT WEB HAS CORROSION COMING FROM UNDER THRESHOLD SUPPORT FITTING AT STA 986, WEB ALSO HAS MANY OTHER SPOTS MARKED FWD TO STA 950E PLUS 10". REMOVED THRESHOLD SUPPORT FITTING PER SRM 51-30-2. REMOVED CORROSION PER 51Aug 23, 2007 · N262FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA03055Frame · misrepairedON AGING A/C INSP FOUND EXISTING REPAIR ON FRAME 720A BETWEEN STR 24L AND 25L DID NOT CONFORM TO SRM 51-40-3. REMOVED EXISTING REPAIR, FABRICATED FORMED SECTION REPAIR REF SRM 51-40-3 AND INSTALLED REF FED EX EA NR 7-5310-113941 THIS IS CLASSIFIED AS A MAJOR Aug 22, 2007 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA03052Frame · misrepairedON AGING A/C INSP, FOUND EXISTING REPAIR ON FRAME 680 BETWEEN STR 22L AND 25L DID NOT CONFORM TO SRM 51-40-3. REMOVED EXISTNG REPAIR, REMOVED EXISTING SLICE PLATE AT STR 25L. FABICATED REPAIR AND INSTALLED REF SRM 51-40-3 AND FED EX EO NR 7-5310-113081 THIS Aug 22, 2007 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA03051Intercostal · corrodedFWD PIT FLOOR INTERCOSTAL WEB CORRODED, STA. 580 AT STR. 27R - 28R LOCATED AT BS 582, "Z" OB OF STR 28R REMOVED INTERCOSTAL. REMOVED CORROSION REF SRM 51-10-06. FOUND TO BE OUT OF LIMITS, REF SRM 51-10-01. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER. REFAug 22, 2007 · N262FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA03050Floor Support · corrodedFWD PIT, CARGO FLOOR SUPPORT HAS CORROSION AROUND NUTPLATES AT BS 640-646, LBL 9" FLOOR SUPPORT OUT OF LIMITS AFTER CLEAN UP, NEW FLOOR SUPPORT FABRICATION BY BACK SHOP ON N00727 REF BAC DWG 65-58352 AND HEAT TREATED ON 8130-3 FORM TRACKING NR 2007- 08-106 ANDAug 22, 2007 · N262FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA03043Shear Tie · corrodedAFT LOWER PIT STATION 1148 BILGE AREA, SHEAR TIE FRAME CORRODED, BETWEEN STR 30 AND STR 29L REMOVED CORROSION REF SRM 51-10-01. FOUND TO BE OUT OF LIMITS, ORIGINAL THICKNESS .066" REMAINING THICKNESS .043". REMOVED .023". REMOVED DAMAGE, FAB NEW FRAME REPAIAug 22, 2007 · N262FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 07FDEA03042Skin · corrodedLWR FUSELAGE SKIN IS DETERIORATED AT VHF ANTENNA LOCATION. INTERNAL KIN SURFACE HAS CORROSION, EXTERNAL SKIN SURFACE HAS CORROSION, BS 1030-1050, STR 29R -30, WL140 REMOVED CORROSION AT LWR FUSELAGE INTERNAL SKIN SURFACE, AND EXTERNAL SKIN SURFACE IAW B 727 SAug 22, 2007 · N262FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR PCSA818200701Engine · malfunctionedFLIGHT 861 DEPARTED SJU AND DURING THE TOP OF THE CLIMB THE CREW REPORTED THE NUMBER 1 ENGINE OIL PRESSURE DROPPED TO ZERO, THE NUMBER 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT CONTINUED TO MIA AND LANDED WITHOUT INCIDENT. THE NUMBER 1 ENGINE WAS REMOVED AND REPAug 18, 2007 · N395AJ · Boeing 727233 · Engine (Turbine/Turboprop)SDR 07FDEA03079Controller · malfunctionedCABIN ALT WARNING CLIMBING THROUGH FL270, CABIN ALT SHOWED 10,000, CLOSED CARGO HEAT OUTFLOW VALVE, NO CHANGE IN CABIN ALTITUDE. PERFORMED QRH CABIN ALT WARNING CHECKLIST. THEN PERFORMED FAILURE OF PRESSURIZATION OF CONTROL CHECKLIST. SYSTEM WOULD NOT PRESAug 17, 2007 · N479FE · Boeing 727233 · Cabin Pressure ControllerSDR 07FDEA02962Seat Track · corrodedMID CABIN MAIN FLOOR STRUCTURE STA 856 TO 861, RBL 46 , WL 208, SEAT TRACK I/B FLANGE CORRODED ON UPPER SURFACE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, ORG THICKNESS .100". REMOVED THICKNESS .073", LOSS OF 27 PERCENT, REF SRM 53-10-01 FIG. REMOVED Aug 17, 2007 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02961Bracket · crackedUNDERSIDE OF FRAME 294.5, LBL 10 BRACKET BROKEN BY PULLEYS FABRICATED NEW BRACKET ON UNDERSIDE OF FRAME 294.5, LBL 10, IAW DWG 69-20588 ID 001. TREATED AND PRIMED, INSTALLED IAW B727 SRM 51-10-2 AND 51-30-2. REPAIR IS CLASSIFIED AS MINOR.Aug 17, 2007 · N262FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02929Power Unit · failedENGINE NR 1 AND NR 2 HYDRAULIC LIGHTS ILLUMINATED 22 MINUTES AFTER TAKEOFF, FOLLOWED BY OBSERVING "A" SYSTEM QTY ZERO. FL 260 AT THE TIME AND NO CONTROL INPUTS WERE BEING MADE. COMPLIED WITH QRH, DECLARED AN EMERGENCY AND HAD AN UNEVENTFUL LANDING. FOUND EVAug 16, 2007 · N267FE · Boeing 727233 · Trailing Edge Flap Control SystemSDR 07FDEA02925Web · corrodedFWD CARGO COMPT BETWEEN BS 580-600 S28R OUTER WEB LOWER ANGLE HAS SURFACE CORROSION. REMOVED AND REPLACED WEB IAW SRM 51-30-2. FABRICATED WEB ON TRAVELER T7/695113.Aug 15, 2007 · N254FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02923Web · crackedCABIN FS 1183 BULKHEAD LT OB FLOOR WEB HAS CRACKS. REMOVED AND REPLACED FLOOR WEB IAW SRM 51-30-2. FABRICATED NEW FLOOR WEB .020 ON TRAVELER T7/1695713 IAW SRM 51-30-6 TABLE 1.Aug 15, 2007 · N254FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02922Skin · dentedEXT FUSELAGE SKIN DENT APPROX STA 1153 BETWEEN S-17L - S-19L, REPAIRED IAW SRM 53-30-3.Aug 15, 2007 · N254FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA02924Door Frame · crackedLT AFT SERVICE DOOR FWD UPPER CAM ROLLER FRAME HAS A CRACK. REMOVED AND REPLACED FWD FRAME IAW SRM 51-30-2.Aug 15, 2007 · N254FE · Boeing 727233 · Fuselage Main, StructureSDR 07FDEA02921Beam · crackedNR 1 LWR CARGO DOOR, LWR BEAM ANGLE, 3RD FROM AFT EDGE REMOVED, LOCATED AND DRILLED, AND INSTALLED LOWER BEAM ANGLE REF SRM 51-30-2 PG 1. RESTORED LEVELING COMPOUND REF OM MM 52-36-21,G. 406A. THIS IS CLASSIFIED AS A MAJOR REPAIR.Aug 15, 2007 · N262FE · Boeing 727233 · Fuselage Main, StructureSDR 07FDEA02905Stringer Clip · crackedSTRINGER CLIP CRACKED AT STA 950F AND STR. 9L REMOVED AND REPLACED CLIP REF SRM 51-30-2.Aug 15, 2007 · N262FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02904Stringer Clip · crackedPASSENGER CABIN STA 620, STR 9R, STRINGER CLIP CRACKED REMOVED CRACKED STRINGER CLIP. REPLACED STRINGER CLIP WITH NEW CLIP REF SRM 51-30-02, THIS IS CLASSIFIED AS A MAJOR REPAIR.Aug 15, 2007 · N262FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02898Stringer Clip · crackedSTRINGER CLIP CRACKED AT 970, STR 9L INSTALLED STRINGER CLIP AS PER SRM 51-30-02, THIS IS CLASSIFID AS A MAJOR REPAIR.Aug 15, 2007 · N262FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02897Stringer Clip · crackedSTRINGER CLIP AT STA 720A AND STR. 7L IS CRACKED. REPLACED STRINGER CLIP STA 720A, STR 7L REF SRM 51-30-2.Aug 15, 2007 · N262FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02896Stringer Clip · crackedSTATION 720 AND STR 6L HAS A STRINGER CLIP CRACKED REPLACED STR CLIP AT STA 720, STR 6L REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.Aug 15, 2007 · N262FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02888Stringer Clip · crackedPASSENGER CABIN STA 990 STR 9R, STRINGER CLIP CRACKED. REMOVED AND REPLACED PASSENGER CABIN STRINGER CLIP, AT STA 990 AT STR 9R CLIP IAW SRM 51-30-2.Aug 14, 2007 · N262FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02880Skin · misrepairedON AGING A/C INSP FOUND, EXISTING INTERNAL SKIN REPAIR. REPAIR DID NOT CONFORM TO SRM 53-30-3 FIG 1. [08-28-07] REMOVED AND REPLACED PREVIOUS REPAIR REF. FED EX EA 7-5330-113262, REPLACED CORRODED STRINGER SECTION REF SRM 53-10-3, 51-30-2 TREATED AND PRIMAug 14, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA02878Stringer · crackedPASSENGER CABIN STA 950D, STR 6R, STRINGER CLIP CRACKED. REMOVED STRINGER CLIP THAT WAS EXISTING, IAW SRM 51-30-02. REPLACED WITH NEW STRINGER CLIP IAW SRM 51-30-02. THIS IS CLASSIFIED A MAJOR REPAIR.Aug 14, 2007 · N262FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 07FDEA02870Web · corrodedFWD LWR CARGO PIT, VERTICAL WEB HAS CORROSION AT LWR, BETWEEN STA 700 AND 720 STR 28L. REMOVED AND REPLACED VERTICAL WEB P/N 69-46346-1 REF SRM 51-30-2 DUE TO CORROSION. FASTENER COMMON TO SKIN WILL BE INSTALLED ON N/R N01157. THIS IS CLASSIFIED AS A MINOR Aug 14, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02868Channel · damagedLWR FWD CARGO PIT U-CHANNEL HAS 3 EXTRA HOLES ON UPPER LEG INBD END AT FWD SIDE OF STA 640 BELOW FRAME SPLICE AGAINST SKIN SHEAR TIE, BETWEEN STR 22L AND 23L. REMOVED U CHANNEL, REF SRM 51-30-2. FABRICATED NEW CHANNEL REF DWG 53FX1465 AND SENT FOR HEAT TREATAug 14, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02867Floorbeam · corrodedAFT UPPER MAIN DECK SURFACE OF FLOORBEAM HAS CORROSION AT NUT PLATE HOLE STA 1030, LBL 9". REMOVED CORROSION FROM AFT UPPER MAIN DECK UPPER SURFACE FLOORBEAM STA 1030, LBL 9". FOUND AREAS OF CORROSION REMOVAL TO BE OUT OF LIMITS. REMOVED DAMAGE SECTION OF FAug 14, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02866Stringer · damagedCUSTOMER REQUEST FOR PREVIOUS WORKMANSHIP, BS 680, STR S-23L STRINGER UPPER FLANGE WAS BLENDED, ON AND HAS TOOLING MARK IN AREA UNDER PREVIOUS REPAIR. BLEND OUT TOOLING MARK IAW B727 SRM 51-10-1 FIG 2. INSTALLED STRINGER TYPICAL REPAIR IAW B727 51-10-3-FIG 2Aug 14, 2007 · N286FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 07FDEA02858Rib · crackedLEFT WING LEADING EDGE CAVITY INBOARD OF NR 2 SLAT OUTBOARD TRACK RIB AT SLAT STATION 318 IS CRACKED AT FORWARD LOWER ATTACH FASTENER. REMOVED RIB AND HAD CRACK NDT AND STOP DRILLED CRACK, FORMED DOUBLER AND INSTALLED. REPAIR DOUBLER TO RIB ALODINED, PRIMED Aug 13, 2007 · N262FE · Boeing 727233 · Wing, Rib/BulkheadSDR 07FDEA02857Web · corrodedMAIN DECK FLOOR SHEAR WEB CORRODED STA 1148-1153 RBL 35-38 WL 208 CORROSION REMOVAL RESULTED IN OUT OF LIMITS MATERIAL LOSS. REMOVED DAMAGED PORTION OF WEB. MFG DOUBLER/FILLER REF SRM 51-40-2 INSTALLED REPAIR PARTS AND RIVETS WET.Aug 13, 2007 · N262FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02855Stringer Clip · crackedPASSENGER CABIN STA 950C STR 9R, STRINGER CLIP CRACKED. REPLACED STRINGER CLIP STA 950C STR 9R REF SRM 51-30-2.Aug 13, 2007 · N262FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02853Stringer Clip · crackedPASSENGER CABIN 720E STR 9R, STRINGER CLIP CRACKED. REMOVED BRACKET PER SRM 51-30-2 PG 32 FIG 7. INSTALLED NEW BRACKET REF SRM 51-30-2 PG 1.Aug 13, 2007 · N262FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02852Seat Track · crackedMAIN CABIN FLOOR, SEAT TRACK UPPER FLANGE SPLICE DOUBLERS, BOTH CRACKED IN HALF, BS : 1130, RBL 1 AND LBL: 1 REMOVED CRACKED DOUBLERS AND FABRICATED NEW DOUBLERS AND INSTALLED REF 53FX939, 51-30-2.Aug 13, 2007 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02851Seat Track · corrodedUPPER DECK STA 1110-1122 LBL 1 WL 208 CENTER SEAT TRACK FLANGE HAS AREAS OF CORROSION REMOVED CORROSION FROM SEAT TRACK AND FOUND TO BE OUT OF LIMITS ORIGINAL FLANGE WAS .100 THICKNESS AFTER REMOVAL .053 LEFT SO REMOVED SEAT TRACK FABRICATED NEW SEAT TRACK OAug 13, 2007 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02850Seat Track · corrodedUPPER DECK STA 1086 - 1105 LBL 44 WL 208 SEAT TRACK I/B FLANGE HAS AREAS OF CORROSION. REMOVED CORROSION FROM LBL45 STA 1090-1110, ORIGINAL .080 REMAINING .071 WITHIN LIMITS IAW SRM 53-10-1. TREATED AND PRIMED SEAT TRACK FROM STA 1090-1110; REMOVED CORROSIAug 13, 2007 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02820Unknown · unknownAFT AIRSTAIR LIGHT ILLUMINATED DURING CRUISE FLIGHT AT FL 350 NEGLIGIBLE TURBULENCE. REPEAT WRITE-UP. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 20AUG07 "MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. VERIFY AFT AIRSTAIR ISAug 10, 2007 · N268FE · Boeing 727233 · Central Warning
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