N278FE, cancelled Aug 27, 2013

Service difficulty reports · 71

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N278FE' AND deregistration_id = 'N278FE-2013-08-27'
  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 FDEA201111114877Unknown · malfunctionedAFTER BLOCK-OUT, COMPASS FLAG CAME INTO VIEW ON CAPTAIN'S HSI. COMPLIED WITH QRH PROCEDURES, RESOLVED COMPASS FLAG NO LONGER IN VIEW. AFTER TAKEOFF COMPASS FLAG REAPPEARED. RETURNED. REPLACED FLIGHT INSTRUMENT ACCESSORY UNIT PER MM 34-62-061-4, CHECKED Nov 11, 2011 · N278FE · Boeing 727233 · Attitude Gyro and Indicating SystemSDR FDEA201006192073Battery Pack · inoperativeEMERGENCY EXIT LIGHT ON BOTH DOORS INOP. REPLACED EMERGENCY EXIT LIGHT BATTERIES. OPS CHECK GOOD FOR SERVICE AT THIS TIME. FINAL CLOSED.Jun 19, 2010 · N278FE · Boeing 727233 · Emergency LightingSDR FDEA201004141182Manifold · failedAFTER T/O NR 1 ENG FIRE LIGHT ON NR 1 FIRE DETECT LOOP. PWR REDUCED ON NR 1 ENG IAW QRH. NR 1 FIRE LIGHT WENT OUT. FIRE DETECT LIGHT REMAINED ON. FIRE DETECT LIGHT OUT WHEN FIRE HANDLE PULLED. NO OTHER ABNORMAL INDICATIONS NOTED. R & R FUEL HEAT MANIFOLD. Apr 14, 2010 · N278FE · Boeing 727233 · Fuel HeaterSDR FDEA201004141180Fire Loop · false activationAFTER T/O NR 1 ENG FIRE LIGHT ON NR 1 FIRE DETECT LOOP. POWER REDUCED ON NR 1 ENG IAW QRH. NR 1 FIRE LIGHT WENT OUT. FIRE DETECT LIGHT REMAINED ON. FIRE DETECT LIGHT OUT WHEN FIRE HANDLE PULLED. NO OTHER ABNORMAL INDICATIONS NOTED. TRACKING NR 10-1182.Apr 14, 2010 · N278FE · Boeing 727233 · Fire DetectionSDR FDEA201001290287Engine · malfunctionedTHRUSH LEVER BROUGHT BACK TO IDLE FOR DESCENT. NR 2 LOW OIL PRESSURE OR FILTER BYPASS LIGHT CAME ON, WENT OUT, CAME BACK ON. AT THAT TIME OIL QTY SLOWLY REDUCED TO 1 GALLON WITH OIL PRESSURE IN YELLOW BAND. FOLLOWED QRH WITH ENG SHUTDOWN. ENG WINDMILLED FOR Jan 29, 2010 · N278FE · Boeing 727233 · Engine Oil PressureSDR FDEA200911053853Relay · false activationAFTER DEPARTING EWR AND CLIMBING THROUGH 16000 FT MAIN CARGO DOOR "B" LIGHT ILLUMINATED. COMPLIED WITH QRH AND RETURNED TO DEPARTURE. RELEASED FOR SERVICE IAW MEL: 52-15-01. REMOVED AND REPLACED CARGO DOOR WARNING SYS "B". RELAY R9107. OPS CHECKS NORMAL INov 5, 2009 · N278FE · Boeing 727233 · Door Warning SystemSDR FDEA200906232245Skin · damaged5 EA OEM HOLES AT RIVET HOLES BETWEEN BS 610 - 600 STR 3L. CUT-OUT DAMAGED AREA (INNER SKIN) DIM: 3.2500" X 1" AND 2.7500" X 1", FAB NEW FILLER FOM 2024T3 .040, PO NR 9008328, DIM: 3.2500" X 1" AND 2.7500" X 1", HFEC AREA WITH NO DEFECT NOTED, TREATED, PRIMEJun 23, 2009 · N278FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200906222202Sill · damagedDRILLED HOLE HAS SHORT "ED" CENTER LONGERON FITTING. DRILLED HOLE FOUND TO BE PART OF P TO F CONVERSION MOD AND FOUND TO BE STRUCTURALLY ACCEPTABLE IAW EA 7-5310-126827 STEP 13.Jun 22, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200906202190Hinge · wornMCD AFT END SECTION OF HINGE HAS PLAY. REMOVED, FABRICATED, AND INSTALLED MCD AFT END SECTION OF HINGE P.O. 79014501, PN NR 5212791, DIM: 42" - UPPER, AND 20" - LOWER. IAW P - F SRM ER 01-049 AND SRM 51- 30-2, 51-30-5, 51-30-8. MCD LEAK AND OPS CHECKED GOODJun 20, 2009 · N278FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA200906202189Hinge · wornMCD FWD END SECTION OF HINGE HAS PLAY REMOVED, FABRICATED AND INSTALLED MCD FWD END SECTION OF HINGE P.O. NR 79014501, PN 5212791, DIM: 45" UPPER, AND 20" LOWER IAW FX P TO F SRM ER-01-049 AND SRM 51-30-2, 51-30-5, 51-30-8. MX LEAK AND OPS CHECKED GOOD IAJun 20, 2009 · N278FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA200906132064Skin · damaged5 EA. OEM HOLES ALONG RIVET LINE BETWEEN BS 610-600 STR 3L. CUT-OUT DAMAGED AREA. FABRICATED NEW FILLERS HFEC INSPECTED AREA WITH NO DEFECTS NOTED, TREATED, PRIMED AND INSTALLED NEW FAB PARTS, ALL IAW EA 7-5310-126827, SRM 51-10-2, AND NDTM 51-00-00 FIG 23 PJun 13, 2009 · N278FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200906122049Sill · damaged1 EA OEM HOLE AT MCK CUT-OUT BS 620 STR 4L. ACCOMPLISHED REPAIR IAW EA 7-5310-126827 BY TRIMING OUT OPEN HOLE IN SKIN BS 620, STR 4L, PERFORMED HFEC INSP OF TRIMMED EDGE TO ENSURE NO CRACKS AND NO FINDINGS NOTED. TRIMMED ADDITIONAL .040 INSURANCE CUT AND FABJun 12, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200906122054Sill · damaged1 EA OEM HOLE AT RIVET HOLE BS 520 S3L. CUT-OUT DAMAGED AREA, FABRICATED NEW FILLER REPAIR, HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 23 PT6. TREATED PRIMED & INSTALLED FILLER REPAIR ALL IAW SRM 51-10-2 & EA 7-5310-126827.Jun 12, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200906122053Sill · damaged7 EA. OEM HOLES ALONG RIVET LINE BETWEEN BS 500-490 S3L. CUT-OUT DAMAGED AREA. FABRICATED NEW FILLER REPAIR, TREATED AND PRIMED, HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 23 PT6 WITH NO DEFECT NOTED. INSTALLED REPAIR FILLERS IAW EA 7-5310-126827 DATED: 06-09Jun 12, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200906122051Sill · damaged1 EA OEM HOLE NEXT TO RIVET HOLE MCD FUSELAGE SKIN BS 560 BETWEEN S2-3L. CUT-OUT DAMAGED, FABRICATED NEW FILLER REPAIR, TREATED AND PRIMED , HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 23 PT 6 WITH NO DEFECTS NOTED & INSTALLED FILLER REPAIR ALL IAW EA 7-5310-12Jun 12, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200906122052Sill · damagedNUMEROUS OEM HOLES ALONG MCK CUT-OUT BS 480 S3-4L. TRIMMED OUT DAMAGED AREA, FABRICATED NEW FILLER, TREATED AND PRIMED IAW SRM 51-10-2. HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 23 PT6 WITH NO DEFECTS NOTED. INSTALLED FILLER REPAIR IAW EA 7-5310-126827 AND SJun 12, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200906041927Web · crackedFORWARD CARGO AREA STA 560 STR 19L PRELOAD SPRING DRUM WEB HAS CRACK. REMOVED AND INSTALLED C1 DOOR MECHANISM SPRING CARTRIDGE ASSY. REMOVED WEB AND FABRICATED NEW WEB, HEAT TREATED TO T6 CONDITION, TREATED, PRIMED & INSTALLED NEW FABRICATED WEB IAW SRM 51-30Jun 4, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200905291854Sill · crackedMAIN CARGO MCK-UPPER SILL, BS 500 STR 3L - 4L CRACK COMING FROM RIVET FASTENER HOLE. REMOVED LOCATED AND INSTALLED LONGERON PN 53FX1467-101 P.O. NR 29052265. SPLICES PN 53FX1467114 PO NR 29057261 TREATED AND PRIMED NEW DRILLED PARTS AND BARE METAL ALL IAW SRMay 29, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200905291853Sill · crackedMAIN CARGO AREA MCK-UPPER SILL STA 600 STR 3L TO 4L, CRACKS ORIGINATING FROM TWO RIVET FASTENERS. REMOVED, LOCATED, TREATED, PRIMED AND INSTALLED MID AND AFT LONGERON SECTION OF MCD UPPER SILL IAW SRM 51-30-2, 51-10-2 AND EA 7-5310-126827 ACCOMPLISHED INSP OFMay 29, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200905291852Sill · crackedMAIN CARGO, MCD-UPPER SILL, BS 490 STR 3L-4L, CRACK COMING FROM FASTENER HOLE. REMOVED AND REINSTALLED MCD HINGE IAW ACCESS, HFEC. INSPECTED AREA IAW NDTM 51-00-00 FIG 23 PT6 AND SRM 51-30-2. REMOVED AND REPLACED MCD UPPER SILL IAW SRM 51-30-2, 51-10-2 AND May 29, 2009 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200905281841Skin · crackedRT FORE FLAP OTBD WBL 442 CRACK ON SKIN ABOVE CARRIAGE ATTACH FITTING. REMOVED RT OTBD FORE FLAP TO FOM REPAIR IAW MM 27-51-011-4. STOPPED DRILLED CRACK IAW SRM 51-10-1. HFEC INSPECTED STOP DRILL AREA IAW NDTM 51-00-00 FIG 3 PT6 NO DEFECTS NOTED. FABRICAMay 28, 2009 · N278FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200905271806Seat Track · crackedCABIN SEAT TRACK HAS CRACK INDICATION AT BS 760 LBL 48 ACCESSED AREA OF INDICATION ON SEAT TRACK IAW SRM 51-30-2. HFEC INSPECTED AREA IAW NDTM PT6. 51-00-00 FIGURE 23. NO DEFECTS NOTED. REINSTALLED 2 EA BOLTS IAW SRM 51-30-2.May 27, 2009 · N278FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200905271805Seat Track · crackedCABIN SEAT TRACK HAS CRACK INDICATION AT BS 760 RBL 48 ACCESSED AREA OF CRACK INDICATION IAW SRM 51-30-2. HFEC INSPECTED AREA IAW NDTM PT6. 51-00-00 FIG 23. NO DEFECTS NOTED. REINSTALLED 2EA BOLTS IAW SRM 51-30-2.May 27, 2009 · N278FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200905231844Attach Angle · corrodedLT WING LE NR 2 SLAT ACTUATOR ATTACH ANGLES MOUNT HOLES CORRODED AND PITTED. REMOVED LT WING FUEL ACCESS PNL 7215 IAW MM 28-11-021-4. REMOVED IB AND OB ATTACH ANGLES IAW EA 7-5750-120824 AND SRM 51-30-2. LOCATED, DRILLED, AND DEBURRED HOLES ON INBD AND OTBD May 23, 2009 · N278FE · Boeing 727233 · Wing, Attach FittingsSDR FDEA200905231861Angle · crackedNR 4 SLAT AFT LOWER ANGLE IS CRACKED AT INBD UPSTOP PAD. REMOVED SLAT COVE PANELS IAW SRM 51-30-2. REMOVED DAMAGED AREA IAW SRM 51-40-4 FIGURE 1. FABRICATED NEW ANGLE IAW SRM 57-50-2 FIG.2 AND 51-30-5, AND 51-30-8. TREATED AND PRIMED ANGLE IAW SRM 51-10-2. INSMay 23, 2009 · N278FE · Boeing 727233 · Leading Edge DevicesSDR FDEA200905231862Angle · crackedNR 8 SLAT AFT LOWER ANGLE IS CRACKED AT INBD AND OUTBD UPSTOP PADS. REMOVED COVE PANELS AT NR 8 SLAT IAW SRM 51-30-2. REMOVED DAMAGED ANGLE IAW SRM 51-30-2 FABRICATED NEW ANGLE IAW SRM 57-50-2 FIG 2, 51-30-5 AND 51-30-8, TREATED AND PRIMED ANGLE IAW SRM 51-May 23, 2009 · N278FE · Boeing 727233 · Leading Edge DevicesSDR FDEA200905221773Skin · gougedLOWER CARGO C3 DOOR OUTER SKIN NUMEROUS DENTS & GOUGES ALL OVER SKIN. REMOVED OUTER SKIN AT C3 DOOR IAW SRM 51-30-2 AND FABRICATED NEW C3 DOOR SKIN IAW EA-7-5230-127967. TREATED AND PRIMED C3 DOOR SKIN IAW SRM 51-10-2 AND INSTALLED C3 DOOR SKIN IAW SRM 51-May 22, 2009 · N278FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA200905221772Frame · dentedAFT CARGO COMPARTMENT FRAME IS DENTED IN UPPER FLANGE AT BS 950C ABOVE STR 26R. REWORKED DENTED AREA TO ORIGINAL CONTOUR. ABOVE STR 26R IAW DWG SR 27-53-139. NDT INSPECTED AREA WITH NO DEFECTED NOTED. FRAME THICKNESS FOUND TO BE .071 IAW SRM 53-10-2 FIG 5.May 22, 2009 · N278FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200905221771Frame · dentedAFT CARGO COMPARTMENT FRAME IS DENTED IN UPPER FLANGE RADIUS AT BS 990 ABOVE STR. 26L. REWORKED DENTED AREA TO ORIGINAL CONTOUR AT BS 990 STR 26L IAW DWG SR 27-53-139. NDT INSPECTED AREA WITH NO DEFECT NOTED IAW NDTM 51-00-00 FIG 23 PART 6. FRAME THICKNESS FMay 22, 2009 · N278FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200905211764Skin · corrodedCORROSION AFT BOLT HEAD FITTING EXTERIOR FUSELAGE, BS 740, STR 26R - 28R. REMOVED BULKHEAD FITTING AT BS 740 STR 26R-28R EXTERIOR FUSELAGE IAW SRM 51-30-2. FABRICATED NEW FITTING IAW DWG NR 69-64841. HEAT TREATED NEW PART TO T6 IAW FAS ENG REPORT NR 2-37153May 21, 2009 · N278FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200905211763Stringer · corrodedSNAKE PIT FWD CARGO, CORROSION AT STR 27 R, STA 740. REMOVED SNAKE PIT FLOOR PANEL TO FOM IAW SRM 51-30-2. CUT OUT SECTION OF STRINGER FOR REPAIR IAW SRM 51-10-1 AND 53-10-3 FIGURE 1. CUT OUT 26.7500 INCH. FABRICATED NEW STRINGER SECTION AND FABRICATED STRINMay 21, 2009 · N278FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200905211762Spar · crackedCRACK ANGLE FALSE SPAR LT WING STA 244 AT NR 7 SPOILER ACTUATOR BRACKET. REMOVED DOUBLER AND WEB SECTION. CUT OUT DAMAGED ANGLE SECTION IAW DWG NR SR27-57-038 REV C. INSTALLED ALL PARTS IAW DRW NR SR27-57-038 REV. C.May 21, 2009 · N278FE · Boeing 727233 · Wing SparSDR 07FDEA04538Duct · blownHEARD LOUD BANG WHILE CLIMBING PAST 32,000 FEET. BANG APPEARED TO BE BELOW AND FORWARD OF THE INSTRUMENT PANEL. DID NOT NOTICE ANY ENGINE OR PRESSURIZATION FLUCTUATIONS. FOUND GASPER AIR DUCT BLOWN. COMPLETED TEMP REPAIR WITH CARGO PIT TAPE PER EA 7-2120-1Oct 9, 2007 · N278FE · Boeing 727233 · Air Distribution SystemSDR 07FDEA00626Bulkhead · crackedCOMPLY WITH FEDEX EA 7-5330-102012, FUSELAGE - BS 11 83 BULKHEAD WEB CRACK REPAIR AT WL 225, BL61. COMPLIED WITH EA 7-5330-102012, RII:575461.Jan 25, 2007 · N278FE · Boeing 727233 · Fuselage Main, BulkheadSDR 07FDEA00124Skin · bulgedRT EXT FUSELAGE STA 288 BELOW STR 21 HAS A SKIN BULGE. REMOVED DAMAGE AND REPAIRED IAW SRM 53-30-2 FIG 3.Jan 16, 2007 · N278FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA00089Floorbeam · corrodedCOMPLIED WITH EA 7-5310-102014 FUSELAGE-BASIC-BS 870 FLOORBEAM UPPER CAP CORROSION, RBL 51-57.Jan 14, 2007 · N278FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA00081Skin · crackedEXT FUSELAGE LOWER HALF BETWEEN STA 680-700 AND BETWEEN 28L - 30. SKIN SURFACE CRACKED AND HOLE NOTED DURING PRESSURIZATION CHECK. REPAIRED AREA AT STA 680 STR 28L IAW SRM 53-30-3 FIG 3A.Jan 12, 2007 · N278FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA03457Module · crackedSHORTLY AFTER LEVELOFF AT FL310, SYS A HYDRAULIC PUMP LIGHTS FLICKERED AND QUANTITY RAPIDLY DROPPED TO (ZERO). COMPLIED W/QRH AND LANDED IN MEM. FOUND HYD PRESS. LINE FROM NR 1 ENG TO "A" SYS MODULE CRACKED. INSTALLED NEW HYDRAULIC LINE AT "A" SYSTEM MODSep 27, 2006 · N278FE · Boeing 727233 · Hydraulic System, MainSDR 06FDEA2924Compressor · stalledAS WE APPLIED T/O POWER (STD POWERS) HEARD A LOUD BANG (COMPRESSOR STALL) AND REJECTED T/O BEFORE T/O POWER WAS SET. MAX SPEED 20KTS WIND 12KT X-WIND. SAT CONFIRMED NR 2 ENGINE COMPRESSOR STALL. C/W AMM 71-00-000-6 3.B. CENTER ENG COMPRESSOR STALL INSPEAug 10, 2006 · N278FE · Boeing 727200 · Turbine Engine Compressor SectionSDR 04FDEA03387Actuator · leakingTOTAL LOSS OF SYS A QUANTITY WITH LANDING GEAR DOWN AND FLAPS AT 30 DEGREE QTY WENT TO 1.0 GALLONS FOR TEN SECONDS THEN WENT IMMEDIATELY TO 0 GALLONS SYS A PRESSURE WENT TO ZERO WITH LOW PRESSURE LIGHTS IMMEDIATELY FOLLOWING QUANTITY LOSS. TROUBLESHOT LEAK TDec 7, 2004 · N278FE · Boeing 727233 · Landing Gear ActuatorSDR 04FDEA02847Indicator · failedHYDRAULIC SYSTEM A QUANTITY INDICATOR WENT TO 0.2 GALLONS ON FLAP RETRACTION. QRH PROCEDURES RECOVERED QTY TO 1.2 GALLONS. ENT BY: 014562 RPT BY: 241937 FACT 29SEP04 11:20, MEM R REMOVED AND REPLACED INDICATOR IAW 727-200 M /M 31-00-011-4. OPS CHECK GOOD. Sep 29, 2004 · N278FE · Boeing 727233 · Hydraulic Indicating SystemSDR 04FDEA00204Seal · out of positionNOSE GEAR DOOR WARNING LIGHT ILLUMINATED WITH GEAR DOWN. AFTER GO-AROUND DOOR LIGHT EXTINGUISHED. VISUALLY INSPECTED BOTH NOSE GEAR DOOR SWITCHES, NO DEFECTS NOTED. FOUND BOTH DOORS WERE DIFFICULT TO OPEN AND CLOSE. WHEN DOORS WERE LATCHED HAD TO BE PUSHEDJan 22, 2004 · N278FE · Boeing 727200 · Landing Gear DoorsSDR 03FDEA01098Control Box · malfunctionedGOT LOWER BODY OVERHEAT LIGHT ON CLIMBOUT UPON DESCENT, LIGHT EXTINGUISHED WITH THROTTLE REDUCTION. T/S IAW 26-14-000-1, FOUND AFT STAIR LT LOOP RUBBING AGAINST STREAMER OF A/C. REPOSITIONED SAME, RERACKED FIRE AND OVERHEAT CONTROL BOX. RAN ENGINES AT GAJul 15, 2003 · N278FE · Boeing 727200 · Detection SystemSDR 02FDEA00191Bulkhead · crackedLEFT W/L BULKHEAD WEB IS CRACKED AT BS 870, LBL 61, WL 162. REMOVED AND REPLACED BULKHEAD WEB PER EA 7-5350-62780.Mar 10, 2002 · N278FE · Boeing 727233 · Fuselage Main, BulkheadSDR 02FDEA00184Frame · dentedDENT IN FRAME AT BS 560 BETWEEN STR 24L AND 25L. REMOVED AND REPLACED FRAME PER SRM 51-10-2, 51-20-151.Mar 6, 2002 · N278FE · Boeing 727233 · Fuselage Main, FrameSDR 02FDEA00146Skin · dentedSKIN DENTED AT BS 1279 TO 1282, BETWEEN STR 20R & 21R. REMOVED AND REPLACED SKIN WITH DOUBLER PER SRM 53-30-3.Feb 27, 2002 · N278FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 02FDEA00149Stringer · crackedSTR 25L CRACKED AT BS 560. REMOVED AND REPLACED STR PER SRM 53-10-3.Feb 25, 2002 · N278FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 02FDEA00142Skin · corrodedCORROSION ON SKIN AND STRINGER AT BS 950D TO 950E, STR 28L. REMOVED AND REPLACED SKIN PER SRM 53-30-3.Feb 23, 2002 · N278FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 02FDEA00148Frame · dentedFRAME DENTED AT BS 420 BETWEEN STR 8L TO 9L. REMOVED AND REPLACED FRAME PER SRM 53-10-4 FIG 1.Feb 23, 2002 · N278FE · Boeing 727233 · Fuselage Main, FrameSDR 02FDEA00212Spar · wornVERT FIN MID SPAR AT FIN STA 230-231 WORN OUT OF LIMITS AT STR 7. REMOVED AND REPLACED MIDSPAR PER EA 7-5510-62791.Feb 19, 2002 · N278FE · Boeing 727233 · Vertical Stabilizer, Spar/Rib
Back to N278FE, cancelled Aug 27, 2013