Boeing 727-233

Service difficulty reports · 3,034

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 = '727233'
  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 FDEA200902200614Skin · gougedC2 DOOR LOWER AFT CORNER IS GOUGED BS 990 S26R. ROUTED OUT DAMAGED EDGE IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER & 2 FILLERS IAW SRM 52-00-03 FIG 4 & 52-30-1 FIG 8. HFEC INSPECTION PERFORMED IAW NDTM PT6 & 51-00-00 FIG 11. NO CRACKS NOTED. OVERSIZED CRIFeb 20, 2009 · N258FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA200902200613Frame · crackedFRAME CRACKED BS 970 ABOVE STR 26L AFT PIT. REMOVED INTERCOSTAL AND PREVIOUS REPAIR FOR ACCESS IAW SRM 51-30-2, CUTOUT DAMAGED AREA ON FRAME IAW SRM 51-10-1. FABRICATED FILLERS & DOUBLER IAW SRM 53-102 FIG 5 AND 51-40-3 FIG 1. HEAT TREATED FILLERS & DOUBLER Feb 20, 2009 · N258FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200902200612Frame · crackedFRAME CRACKED BS 990 ABOVE STR 26L AFT PIT. CUTOUT DAMAGED AREA IAW SRM 51-10-1, FABRICATED FILLER & DOUBLER IAW SRM 53-10-2 FIG 5 & 51-40-3 FIG 1. HEAT TREATED FILLER & DOUBLER TO 7075 T-6 IAW FAS ENG REPORT 2-37153-001 REV A. LOCATED DRILLED, DEBURRED FILLFeb 20, 2009 · N258FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200902190584Skin · dentedOIL CANNING RT FUSELAGE SKIN BS 675 BETWEEN STR 22R AND STR 23R. CUT-OUT DAMAGE AREA IAW SRM 53-30-3 FIG 1. FABRICATED DOUBLER REPAIR IAW SRM 53-30-3 FIG 1 AND 53-30-2 FIG 2. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2. INSTALLED PARTS IAW SRM 51-30-2 ANDFeb 19, 2009 · N258FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200902190587Hinge · crackedEXTERIOR FUSELAGE MCD AFT HINGE AFT END HAS LARGE CRACK TO ATTACH SCREW HOLE, FROM LOBE. REPLACED HINGE SEGMENT IAW SRM 51-30-5, 51-30-2 & IAW DWG 52FX1433 REV E & INSTALLED NEW HINGE PIN IAW SRM 51-30-2 & DRAWING 52FX1433 REV E. OPS CHECK GOOD IAW MM 52-34-0Feb 19, 2009 · N258FE · Boeing 727233 · Fuselage, Door HingeSDR FDEA200902190585Skin · corrodedEXTERIOR FUSELAGE, CORROSION ON SKIN LAP AT BS 690 STR 26R. REMOVED CORROSION IAW SRM 51-10-6. OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT-OUT DAMAGED AREA, FABRICATED DOUBLER, & FILLER. TREATED AND PRIMED ALL REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR IAFeb 19, 2009 · N258FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200902180572Plate · damagedON CLIMB-OUT ACFT UNUSUAL VIBRATION PASSING 11,000 FT & ACCELERATING THROUGH 335 KIAS. DECREASED AIRSPEED & VIBE STOPPED AT 315 KIAS. ACCELERATED AGAIN & AT FL 180, 325 KIAS VIBE RETURNED, DEPLOYED SPOILERS & VIBE SMOOTHED OUT. STOWED SPOILERS & VIBE RETURNFeb 18, 2009 · N274FE · Boeing 727233 · Trailing Edge Flap Control SystemSDR FDEA200902120511Intercostal · damagedMCD INNER CENTER BEAM HAS MISDRILLED HOLE AND GOUGED INTO INTERCOSTAL REMOVED DAMAGE INTERCOSTAL IAW SRM 51-30-2, FABRICATED NEW INTERCOSTAL IAW HAYES INTERNATIONAL CORP DRAWING NR 52FX518 REV A, HEAT TREATED PART IAW FAS ENGINEERING REPORT NR 2-37153-801 REV Feb 12, 2009 · N279FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA200902120510Door Frame · crackedCORRECTION OF SDR 09-0481 FWD CARGO DOORWAY STA 620 LOWER INNER CHORD CRACKED. FABRICATED CHORD ON MAE TRAVELER T9/778261. FABRICATED SPLICE ON MAE TRAVELER T9/779262. CHORD REMOVED AND NEW INSTALLED IAW SRM 51-30-2 AND SRM 51-40-4. MAJOR REPAIR, RII, RDFeb 12, 2009 · N269FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200902090484Stringer · corrodedFWD CARGO AREA BS 720F TO 740 S-26L STRINGER SEVERAL ROW OF RIVETS CORRODED REPAIRED STRINGER IAW SRM 53-10-3. FABRICATED STRINGER ON MAE TRAVILER T9/778825. MAJOR REPAIR, RII, RDR AND SDR.Feb 9, 2009 · N269FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA200902070482Seat Track · corrodedMCD SEAT TRACK FLANGE HAS CORROSION AT LBL24 APPROX FROM STA 370 TO 460. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. FABRICATED TRACK AND SPLICES ON MAE TRAVELER T9/779235 AND T9/779236. MAJOR REPAIR, RII, RDR AND SDR.Feb 7, 2009 · N269FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902070481Structure · crackedFWD CARGO DOORWAY STA 620 LOWER INNER CHORD CRACKED. FABRICATED CHORD ON MAE TRAVELER T9/778261. FABRICATED SPLICE ON MAE TRAVELER T9/779262. REPAIRED CHORD IAW SRM 53-10-2. MAJOR REPAIR, RII, RDR AND SDR.Feb 7, 2009 · N269FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200902060476Skin · crackedTWO CRACKS ON FWD ENTRY DOOR HINGE CUT OUT BODY SKIN EDGE RADII, LOWER HINGE. REPAIRED CRACKS IAW EO 7-5330-7-2345F PART 2.Feb 6, 2009 · N279FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200902030436Hinge · crackedMCD AFT HINGE LAST LUG CRACKED FROM EDGE TO FASTENER HOLE. REMOVED MCD AFT UPPER HINGE IAW FX DWG 52FX1433 REV E AND B727 SRM 51-30-2. LOCATED SHAPED AND DRILLED NEW HINGES SEGMENT 48 INCH BY 4 INCH IAW B727 SRM 51-30-5. TREATED AND PRIMED NEW PART IAW B7Feb 3, 2009 · N281FE · Boeing 727233 · Fuselage, Door HingeSDR FDEA200901310407Skin · crackedRIGHT WING NR 8 SLAT OTBD TRACK SKIN IS CRACKED. STOP DRILLED CRACK IAW DRAWING SR27-57-034 REV A AND SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024-T3 0.071 DIM 9 1/2" BY 6" IAW DRAWING SR27-57-034 REV A. INSTALLED DOUBLER IAW DRAWING SR27-57-034 REV A AJan 31, 2009 · N279FE · Boeing 727233 · Leading Edge DevicesSDR FDEA200901290389Structure · corrodedPOSSIBLE CORROSION AT DOG HOUSE LOWER LEFT CHORD STA 312 UNDER LEVELING COMPOUND. REMOVED LEVELING COMPOUND AND CORROSION FROM AREA IAW SRM 51-10-6 AND SOPM 20-30-03, FOUND CHORD OUT OF LIMITS IAW SRM 53-10-1 FIG 1, REMOVED AND REPLACED CHORD IAW SRM 51-30-Jan 29, 2009 · N279FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200901290386Angle · crackedRIGHT WING LOWER CHORD ANGLE CRACKED AT NR 8 SPOILER FITTING.Jan 29, 2009 · N279FE · Boeing 727233 · Wing, Attach FittingsSDR FDEA200901290385Angle · crackedLEFT WING LOWER CHORD ANGLE CRACKED AT NR 7 SPOILER FITTING.Jan 29, 2009 · N279FE · Boeing 727233 · Wing Miscellaneous StructureSDR FDEA200901290384Skin · canningC1 DOOR LOWER AFT SKIN IS OIL CANNED. CUT OUT DAMAGED AREA IAW 52-00-03 FIG 3. FABRICATED DOUBLER REPAIR IAW SRM 52-00-03 FIG 3 AND 52-30-01 FIG. 7. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.Jan 29, 2009 · N279FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA200901290383Structure · crackedCRACK ON LEFT INBD MID FLAP CHORD AT WBL 114. CUT OUT DAMAGED AREA IAW SRM 51-40-3 FIG 1. FABRICATED LOWER SECTION USING EXTRUSION AND SPLICE IAW SRM 51-40-3 FIG 1 AND 57-50-2 FIG 5. INSTALLED REPAIR PARTS IAW SRM 51-30-2.Jan 29, 2009 · N279FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200901290382Frame · gougedFWD PIT FRAME AT BS 520 STRINGER 22L IS GOUGED AT RADIUS. CUT OUT DAMAGED IAW SRM 51-40-3 FIG. 1. FABRICATED REPAIR DOUBLER, STRUCTURAL FILLER, AND 1 FILLER IAW SRM 53-10-2 FIG. 3 AND 51-40-3 FIG. 1. HEAT TREATED PART FROM 7075-O TO 7075-T6 IAW FAS ENGINEERINJan 29, 2009 · N279FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200901290380Skin · gougedRIGHT WING INBD FORE FLAP IS GOUGED AT OTBD LEADING EDGE IN TWO PLACES. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED NEW REPAIR PARTS IAW SRM 57-50-2 FIG 3 AND 57-50-4 FIG 1. INSTALLED NEW REPAIR IAW SRM 51-30-2.Jan 29, 2009 · N279FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200901280343Angle · crackedLEFT WING LOWER CHORD ANGLE CRACKED AT NR 7 SPOILER FITTING. REMOVED AND DISCARDED DOUBLER IAW FEDEX DRAWING SR27-57-038 REV C. TRIMMED WEB AND LOWER CHORD IAW FEDEX DRAWING SR27-57-038 REVC. FABRICATED NEW WEB FROM 7075-T6 0.032 DIM. 12 1/8" BY 9 1/2". Jan 28, 2009 · N279FE · Boeing 727233 · SpoilersSDR FDEA200901280347Frame · crackedNR 1 ENGINE NOSE COWL AFT EDGE IS CRACKED AND SECTION TORN AT 4 O'CLOCK POSITION BS 1200 CUT OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED REPAIR PARTS AND 1 FILLER IAW SRM 54-10-2 FIG 1 AND 54-10-3 FIG 3. INSTALLED REPAIR PARTS IAW SRM 51-30-2.Jan 28, 2009 · N279FE · Boeing 727233 · Nacelle/Pylon, Main FrameSDR FDEA200901280344Skin · damagedLEFT AFT EMERGENCY EXIT HATCH HAS DEEP SCRATCH ON OUTER SKIN. CUT OUT DAMAGED AREA IAW SRM 52-00-03 FIG 3. FABRICATED REPAIR DOUBLER IAW SRM 52-00-03 FIG 3 AND 52-20-01 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.Jan 28, 2009 · N279FE · Boeing 727233 · Emergency ExitsSDR FDEA200901280342Angle · crackedRIGHT WING LOWER CHORD ANGLE CRACKED AT NR 8 SPOILER FITTING. REMOVED AND DISCARDED DOUBLER IAW DRAWING SR27-57-038 REV C. TRIMMED WEB AND LOWER CHORD IAW DRAWING SR27-57-038 REV C. FABRICATED NEW INBD WEB, FABRICATED NEW INBD LOWER CHORD, FABRICATED NEW STJan 28, 2009 · N279FE · Boeing 727233 · Wing Miscellaneous StructureSDR FDEA200901280345Skin · damagedRIGHT FWD EMERGENCY EXIT HATCH OUTER SKIN HAS DEEP SCRATCH. CUT OUT DAMAGED AREA DIM 4 1/4 BY 1 1/4 INCH IAW B727 SRM 52-00-03 FIG 3. FABRICATED DOUBLER REPAIR MAT USED 2024-T3 0.080" PO NR 9008077 DIM 11 1/8 BY 7" IAW B727 SRM 52-00-03 FIG 3 AND 52-20-01 Jan 28, 2009 · N279FE · Boeing 727233 · Emergency ExitsSDR FDEA200901240316Valve · malfunctionedTHE LEFT BRAKE WILL NOT MODULATE. A GREAT DEAL OF PEDAL EFFORT IS REQUIRED TO ACTIVATE AND THEN MAX BRAKING IS RESULT. REMOVED AND REPLACED LT BRAKE METERING VALVE OPS CHECKED GOOD AS PER MM 32-41-011-4.Jan 24, 2009 · N262FE · Boeing 727233 · Landing Gear Brake SystemSDR FDEA200901200269Panel · dentedE/E BAY UPPER CHORD SKIN STRUCTURE HAS BULGE AT BS 328 BL 0. EVALUATED BULGE ON NLG WW UPPER SKIN BS 328 BL0 AS AN OIL CANNING DENT. DETERMINED TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. DRILLED 1 INCH ROUND HOLE TO REMOVE DAMAGE IAW B727 SRM 51-10-1. Jan 20, 2009 · N281FE · Boeing 727233 · Fuselage Main, BulkheadSDR FDEA200901190246Web · dentedE/E BAY UPPER STRUCTURE HAS BULGE AT BS 328 BL0. EVALUATED BULGE ON N/W/W UPPER SKIN BS 328 BL0 AS AN OIL CANNING DENT DETERMINED TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 1. DRILLED 1" INCH ROUND HOLE TO REMOVE DAMAGE IAW SRM 51-10-1. FABRICATED REPAIR DOUBLJan 19, 2009 · N281FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200901180230Spar · crackedCRACK ANGLE FALSE SPAR AT NR 7 SPOILER ACTUATOR CUT-OUT. CRACKED ANGLE OUT OF LIMITS IAW SRM 57-10-1 FIG 1. REMOVED SUPPORT FITTING & VERTICAL STRUCTURE IAW DWG SR27-57-038 & SRM 51-30-2. TRIMMED AFT WEB AT CUT LINE IAW DWG SR27-57-038 REV C. REMOVED CRACKJan 18, 2009 · N281FE · Boeing 727233 · Wing SparSDR CA090113005Cabin Pressure · unknown(CAN) ENROUTE YOW FROM YVO, THE CREW OBSERVED THE CABIN ALTITUDE CLIMBING BEYOND THE PRESET VALUE. THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER PROBLEM. (TC NR 20090113005)Jan 11, 2009 · Boeing 727233 · Cabin Pressure Control SystemSDR FDEA200901110124Stringer · corrodedCORROSION AT ATTACHING RIVET HEADS STA 950-1010 STR 27L IN AFT PIT. FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED STRINGER 27L FROM BS 950A TO BS 1010 IAW SRM 51-30-2. FABRICATED NEW STRINGER AND SPLICES IAW SRM 53-10-3. INSTALLED REPAIR PARTS IAWJan 11, 2009 · N277FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA200901110123Stringer · corrodedCORROSION AT ATTACHING RIVET HEADS STA 1010-1090 STR 27L IN AFT PIT. FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1, REMOVED STRINGER 27L FROM BS 1010 TO BS 1090 IAW SRM 51-30-2. FABRICATED NEW STRINGER AND SPLICES IAW SRM 53-10-3. INSTALLED REPAIR PARTS IJan 11, 2009 · N277FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA200901100120Valve · failedTOTAL LOSS OF A HYDRAULICS UPON GEAR RETRACTION, (LEVEL AND PRESSURE 0). A PUMPS RAN AMAX OP 3 MINS BEFORE SHUTOFF. REMOVED AND REPLACED LT GEAR LOCK SEQUENCE VALVE IAW MM 32-32-031-4. PERFORMED GEAR SWING IAW AMM 32-32-00-005. REMOVED BOTH NR1 AND NR 2 HYJan 10, 2009 · N286FE · Boeing 727233 · Hydraulic Pump (Electric/Engine), MainSDR FDEA200901090104Indication Sys · inoperativeDURING CLIMB-OUT, NR 1 CSD "RISE" OUT OF LIMITS. QRH DIRECTED US TO DISCONNECT NR 1 CSD. REPLACED TEMP BULB. NO HELP TRIED NEW OUT TEMP BULB NO HELP. SWAPPED IND CONN & PROBLEM FOLLOWED. DURING NR 1 ENG RUN, RISE 10 DEG & NR 2 AND 3 WERE AT 1 DEG. NR 1 RJan 9, 2009 · N219FE · Boeing 727233 · Central WarningSDR FDEA200901090107Actuator · failedAFTER TAKEOFF WHILE RAISING FLAPS NR 1 LEADING EDGE DEVICE REMAINED EXTENDED AT 2 DEG AND 0 DEG FLAP SETTING. RAN QRH PROBLEM REMAINED. RETURNED TO BASE FOR NORMAL LANDING. LEADING EDGE DEVICE RETRACTED ON SCHEDULE AFTER LANDING CLEAN UP. VISUAL INSPECTION Jan 9, 2009 · N279FE · Boeing 727233 · Leading Edge Slat ActuatorSDR FDEA200901080103Actuator · failedAFTER TAKEOFF WHILE RAISING FLAPS NR 1 LEADING EDGE DEVICE REMAINED EXTENDED AT 2 DEG AND 0 DEG FLAP SETTING. RAN QRH PROBLEM REMAINED. RETURNED TO BASE FOR NORMAL LANDING. LED RETRACTED ON SCHEDULE AFTER LANDING CLEAN UP. VISUAL INSPECTION OF NR 1 LEADINGJan 8, 2009 · N279FE · Boeing 727233 · Leading Edge Slat ActuatorSDR FDEA200901070064Stringer · corrodedFWD CARGO PIT, CORROSION INSIDE CHANNEL STRINGER 23R AT STA. 720E - 720F. REMOVED ACCESS PANEL 3440 IAW SRM 51-30-2. CUT-OUT DAMAGE STR 23R BETWEEN STA 720E TO 740 IAW SRM 53-10-3 FIG 1 DETAIL I. FABRICATED REPAIR FILLER AND 2 EA SPLICES IAW SRM 53-10-3 FIJan 7, 2009 · N277FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200901050042Stringer · corrodedFWD CARGO CORROSION AT STR 27R AND STA 620 INSIDE THE STRINGER CHANNEL. REMOVED CORROSION IAW SRM 51-10-2 AND UT AREA IAW NDTM 51-00-00 FIG 2 PART 4. FOUND TO BE OUT-OF-LIMITS IAW SRM 53-10-1 FIG 1. REMOVED RIBS AT STA. 606 & 612, AND STRINGER TIES IAW SRM Jan 5, 2009 · N277FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA200901050026Skin · dentedDENT STA 1180 STR 17R. FOUND DENT OUT OF LIMITS, CUT OUT DAMAGED SKIN DIMS 3.2 INCH X 3.0 INCH, FABRICATED REPAIR DOUBLER USING 2024-T3 .090 DIMS 10.5 INCH X 8.750 INCH AND FILLER USING 2024-T3 .080 DIMS 3.2 INCH X 3.0 INCH, INSTALLED REPAIR DOUBLER AND FILLEJan 5, 2009 · N257FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200901030009Skin · crackedNR 6 SLAT HAS A BROKEN BOLT AT INBD HOOK AT AFT MOUNT AND BROKEN RIVET AND HAS CRACK INDICATIONS. HFEC VERIFIED 4 CRACKS ALL TERMINATE AT FASTENER HOLES OR SKIN EDGE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-50-3 AND 51-30-2.Jan 3, 2009 · N277FE · Boeing 727233 · Leading Edge DevicesSDR FDEA200901030008Skin · crackedNR 6 SLAT HAS A CRACK AT OTBD HOOK AFT OF MOUNT BOLT. HFEC VERIFIED CRACK TERMINATES AT FASTENER HOLE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-50-3 AND SRM 51-30-2.Jan 3, 2009 · N277FE · Boeing 727233 · Leading Edge DevicesSDR FDEA200812305318Stringer · corrodedFWD CARGO COMPT STRINGER 28L IS CORRODED FROM BS 600-620. CUTOUT DAMAGED STRINGER. FABRICATED STRINGER REPAIR FILLER, REPAIR SPLICE. CUTOUT DAMAGED SKIN & FABRICATED REPAIR DOUBLER. INSTALLED REPAIR PARTS IAW SRM 53-10-3, 53-10-2, 53-30-2 AND 51-30-2.Dec 30, 2008 · N257FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA200812305317Skin · dentedDENT STA 390 STR 8L. DENT FOUND TO BE OUT OF LIMITS, REWORKED DENT TO ORIGINAL CONTOUR IAW SRM 51-40- 1 HFEC INSPECTED IAW NDTM 51-00-00 WITH NO DEFECTS NOTED.Dec 30, 2008 · N257FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200812295313Shear Tie · corrodedAFT CARGO COMPARTMENT - CORROSION ON SHEAR TIE AT BS 1166 AFT SIDE BETWEEN STRINGERS 29L AND 28L. CORROSION ON SHEAR TIE 100% MATERIAL LOSS & OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED SHEAR TIE IAW SRM 51-30-2 AND FABRICATED NEW PART IAW SRM 51-20-1 FIGDec 29, 2008 · N276FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR FDEA200812245290Web · crackedAFT AIRSTAIR, RT LWR TORQUE BOX INBD VERTICAL WEB IS CRACKED AT 02 PLACES AT LIGHTING HOLE STA 1218. REMOVED AFT AIRSTAIRS FLOOR PANEL AND ANGLE FOR ACCESS IAW SRM 51-30-2. CUTOUT DAMAGED AREA IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR PARTS FROM 2024T3, 0.032 Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200812245288Skin · damagedFUSELAGE, FASTENER INSTALLED AT SEAM AT STA 550, STR 21L REMOVED SUBJECT FASTENER AND TRIMMED OUT DAMAGED AREA IAW EA NR 7-5330-126879. REPAIRED IAW EA NR 7-5330-126879, FUSELAGE, PLATES AND SKIN AD 98-11-03 R1 MCD CUTOUT PLATING REPAIR AT STA 554.Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200812245284Skin · dentedGOUGE AND DENT ON FUSELAGE SKIN STA 1030, STR 28L. FOUND GOUGE OUT OF LIMIT IAW B727 SRM 53-30-1 FIG 1 AND 2. CUTOUT DAMAGED AREA IAW B727 SRM 53-30-3 FIG 3. FABRICATED DOUBLER FROM 2024T3, 0.071 AND A FILLER FROM 2024T3, 0.063 INCH IAW B727 SRM 53-30-3 FIGDec 24, 2008 · N277FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200812245282Stringer · corrodedFWD CARGO HAS CORROSION AT STRINGER 28R AND STA 680 ON STRINGER CHANNEL UNDER LEVELING COMPOUND. REMOVED STRINGER SPLICE IAW SRM 51-30-2. FABRICATED NEW STR SPLICE IAW SRM 53-10-2FIG 9 AND 53-10-3 FIG 1. TREATED AND PRIMED AND INSTALLED NEW SPLICE AT FWD CADec 24, 2008 · N277FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
Back to Boeing 727-233