Boeing 727-232

Service difficulty reports · 6,539

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '727232'
  ORDER BY difficulty_date DESC"

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SDR DL72S950761Web · crackedDURING INSPECTION, THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A 0.25 INCH CRACK AT STA 285. THE DAMAGED PORTION OF THE WEB WILL BE TRIMMED OUT AND A REPAIR DOUBLER AND FOUR STRAPS WERE INSTALLED IN ACCORDANCE WITH S/B 727-53-145.Feb 8, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950670Skin · dentedAT HMV, FOUND LEFT INBOARD AILERON WITH A DENT ON THE UPPER SKIN. THE DENT WAS REPAIRED BY INSTALLING A FLUSH REPAIR PER SRM 57-50-5 FIG 1.Feb 8, 1995 · N543DA · Boeing 727232 · AileronsSDR DL72S950611Rib · crackedDURING INSPECTION OF THE NR 4 LEADING EDGE SLAT, RIB MARKED NR 18 WAS FOUND TO HAVE A CRACK. THE RIB WAS REPAIRED PER MM 57-54-0 FIG 805.Feb 8, 1995 · N532DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950557Blkhd Beam · crackedDURING LETTER CHECK, FOUND FS 1183 BULKHEAD VERTICAL BEAM AT RBL 8 WITH A 1 INCH CRACK. REPAIRED PER MM 53-11-0.Feb 8, 1995 · N516DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950556Skin Clip · corrodedDURRING LETTER CHECK, FOUND FS 1090 FRAME TO SKIN SHEAR TIE CORRODED ON ITS FWD SIDE AT STRINGERS 29R AND 28R. REPAIRED PER M/M 53-11-0 FIG 815.Feb 8, 1995 · N516DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR 95FDEA00113Fire Warning · activatedAFTER T/O FIREBELL RANG MOMENTARILY AND ONE RED LT FLASHED, WAS OVER BEFORE WE COULD DETERMINE SOURCE. TESTED ENG AND W/W FIRE WARNING. CKS NORMAL. NO HISTORY NOTED. SYSTEM OK FOR SERVICE.Feb 8, 1995 · N498FE · Boeing 727232 · Fire DetectionSDR DL72S950773Floor Support · crackedFOUND ON LTR CK - 1 INCH CRACK THROUGH MOUNT BOLT HOLE FLOOR PANEL SUPPORT CHANNEL FWD SIDE STA 950C BL 18R - REPAIR - REPAIRED PER SRM 53-10-5 AND I.D. PER P.S. 900-5-1 NR 4.Feb 7, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950552Skin · scratchedDURING INSPECTION, FOUND OUTER FUSELAGE SKIN SCRATCHED BEYOND LIMITS AFT OF FORWARD ENTRY DOOR JUST BELOW FLOOR LINE AT FS 380. REPAIRED PER SRM 53-30-3.Feb 7, 1995 · N528DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S950535Skin · crackedFOUND ON LTR CK, .4375 INCH BY .25 INCH SECTION OF FUSELAGE SKIN ROUTED OUT AT AFT CORNER OF ACCESS PLATE 3903. REPAIRED PER M/M 53-30-0 PG 804.Feb 7, 1995 · N420DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S950534Web · crackedDURING LETTER CHECK, FOUND A .4375 INCH LONG CRACK IN VERTICAL WEB AFT STAIRWELL AREA LEFT SIDE FS 1276. REPAIRED PER SRM 53-11-0 PG 832.Feb 7, 1995 · N420DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950821Angle · crackedDURING CV-2 CK, FOUND CRACK ON NR 3 SLAT I/B TRACK O/B VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED STIFFENER.Feb 6, 1995 · N467DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S950819Angle · crackedDURING CV-2 CK, FOUND CRACK ON NR 2 SLAT O/B TRACK O/B VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED ANGLE PER MM 57-20-21 PG 813.Feb 6, 1995 · N467DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950818Angle · crackedDURING CV-2 CK, FOUND CRACK ON NR 2 SLAT OUTBOARD TRACK INBOARD VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED ANGLE PER M/M 57-20-21 PG 813.Feb 6, 1995 · N467DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S950793Stringer · corrodedFOUND ON CV2 CK - CORROSION INSIDE STRINGER 27L FWD STA 720F - REPAIR - REPLACED SECTION OF STRINGER PER SRM 53-10-3 FIG 1.Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S950789Clip · corrodedFOUND ON CV2 CK - CORROSION AT LOWER FWD FUSELAGE SKIN CLIP STA 303 AT NOSE W/W CHORD - REPAIR - REPAIRED PER SRM 51-40-3 FIG 1.Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950788Floor Beam · corrodedFOUND ON CV2 CK - CORROSION AT FLOOR BEAM AT BL 0 TO LBL 16 STA 1110 - REPAIR - INSTALLED REPAIR ANGLE PER MM 53-20-11 FIG 804A.Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S950787Floor Beam · corrodedFOUND ON CV2 CK - CORROSION AT FLOOR BEAM TOP SIDE AND BOTTOM WHERE CLIP NUTS ATTACH STATION 380 RBL 12 TO 63 - REPAIR - REPLACED TEE CAP PER SRM 53-10-8.Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S950786Seat Track · corrodedFOUND ON CV2 CK - CORROSION AT SEAT TRACK STA 344 TO 360 AT LBL 22 - REPAIR - REPLACED SEAT TRACK PER SRM 53-10-5 FIG 7.Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950785Seat Track · corrodedFOUND ON CV2 CK - CORROSION AT SEAT TRACK STA 480 LBL 22 - REPAIR - REPLACED DAMAGED SEAT TRACK FROM 440-480 PER SRM 53-10-5 FIG 7.Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950537Pcu · failedDURING CLIMB THROUGH 18,000 FEET BOTH 'A' SYSTEM HYDRAULIC PUMPS FAILED, LANDED LAX. FOUND LOWER RUDDER PCU FAILED, CAUSING A SYSTEM FAILURE. REPLACED PCU AND BOTH 'A' SYSTEM PUMPS AND FILTERS.Feb 6, 1995 · N546DA · Boeing 727232 · Rudder Control SystemSDR DL72S950525Skin · damagedDURING SHOP INSPECTION THE LEFT WING NR 1 FORE FLAP WAS FOUND WITH THE LEADING EDGE SKIN DAMAGED AT 7 INCHES TO 12 INCHES FROM THE INBOARD END OF FLAP. REPAIRED PER SRM 57-50-4.Feb 6, 1995 · N496DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950519Rib · crackedDURING SHOP INSPECTION, FOUND LEFT WING NR 3 SLAT WITH THE LOWER CHORD DAMAGED OUBOARD OF THE INBOARD UP STOP FITTING AND RIB NR 10 CRACKED AT ITS LOWER END, OUTBOARD OF ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0.Feb 6, 1995 · N475DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950763Rear Spar · crackedDURING INSPECTION, THE RT ELEVATOR REAR SPAR WAS FOUND TO HAVE A CRACK EMANATING .25 INCH FROM INBD SIDE OF THE SHEAR PLATE AT THE SECOND FROM OUTBD TAB HINGE FITTING-TO-REAR SPAR ATTACHMENT. IN ACCORDANCE WITH B727 S/B 55-0087, THE CRACK WAS STOP DRILLED ANDFeb 4, 1995 · N532DA · Boeing 727232 · Elevator, Spar/RibSDR DL72S950589Skin · puncturedDURING HMV, FOUND C-2 DOOR HAS HOLE PUNCHED IN IT ABOVE AFT LOWER CORNER, REPAIRED PER SRM 52-00-3 FIG 3.Feb 4, 1995 · N492DA · Boeing 727232 · Cargo/Baggage DoorsSDR DL72K950760Angle · crackedDURING INSPECTION, A .875 INCH CRACK WAS FOUND IN THE ANGLE OF THE FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1263 IN ACCORDANCE WITH B727 S/B 53-0129, REV. 4, THE BEAM WILL BE REPLACED.Feb 4, 1995 · N479DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950721Seat Track · corrosionDURING HMV, FOUND SEAT TRACK CORROSION AT STA 344 LEFT I/B TRACK, REPAIRED BY REPLACING SEAT TRACK LT I/B FROM STA 380 FWD PER MM 53-20-11 FIG 802.Feb 3, 1995 · N492DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950502Flap · crackedFOUND ON LETTER CHECK, 1 IN CRACK I/B END OF NR 6 L/E FLAP, REPAIR. INSTALLED DOUBLER PER M/M 57-53-0 PG 804.Feb 3, 1995 · N532DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950497Cover · crackedFOUND ON LETTER CK -1. .5 IN CRACK ON NR 5 L/E SLAT I/B TRACK COVER SKIN - 2. .5 IN CRACK ON NR 6 L/E SLAT I/B TRACK COVER SKIN - 1. AND 2. REPAIRED PER M/M 57-54-0 PG 820.Feb 3, 1995 · N532DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950496Web · crackedFOUND ON LETTER CHECK, LIGHTNING HOLES DAMAGED LEFT AT STA 1290 1330 IN STAIR WELL VERTICAL WEB, REPAIR. INSTALLED DOUBLER AT STA 1330 PER M/M 53-11-0.Feb 3, 1995 · N532DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K950503Stair Web · crackedFOUND ON LETTER CHECK, A .875 INCH CRACK IN DOUBLER AT HORIZ STIFFENER STA 1263 BELOW VENTRAL STAIR ACT - 2. .75 INCH CRACK AT LIGHTENING HOLE UPPER STA 1266 BELOW VENTRAL STAIR ACT - REPAIR - 1. REPAIRED PER ERA 301128-14 CODE 4-53-10 - 2. REPAIRED PER M/MFeb 3, 1995 · N479DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S951857Skin · delaminatedNR 2 MID FLAP DURING HMV SHOP INSP, WAS FOUND TO BE DELAMINATED FROM 0 TO 3 FROM O/B END AND POTTING COMPOUND DETERIOIATED. REPAIRD PER SRM 57-50-4 .Feb 2, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951140Panel · delaminatedLARGE DELAMINATION LOWER SKIN, ON WING SPOILER PANEL. MADE BONDED REPAIR PER 727 SRM 57-50-6 DAMAGE FOUND DURING SHOP INSPECTION.Feb 2, 1995 · N470DA · Boeing 727232 · SpoilersSDR DL72S950817Rib · crackedDURING CV-2 CK, FOUND RIB CRACKED 1 INCH ON NR 3 SLAT JUST OUTBD OF OUTER TRACK. REPAIRED PER SRM 57-50-3 FIG 9.Feb 2, 1995 · N467DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950751Floor Beam · corrodedSTA 360 FLOOR BEAM NUT CLIP HOLES CORRODED MANY PLACES FOUND AT HMV. REPAIRED PER SRM 53-10-8 FIG 1.Feb 2, 1995 · N492DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S950689Rib · crackedAT HMV, FOUND NR 2 LEADING EDGE SLAT WITH CRACKED RIB AT 2ND LOCATION FROM THE OUTBD END OF SLAT. REPAIRED PER SRM 57-54-0 PG 819.Feb 2, 1995 · N492DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950551Floor Beam · corrodedAT HMV, FOUND FS 400 CABIN FLOOR BEAM UPPER CAP WITH CORROSION DAMAGE ALONG ITS LENGTH. REPAIRED PER SRM 53-10-8 FIG 3 AT RBL 10 TO LBL 10 AND SRM 53-20-11.Feb 2, 1995 · N492DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S950550Floor Beam · corrodedAT HMV, FOUND FS 1070 CABIN FLOOR SUPPORT BEAM UPPER CAP CORRODED, OUTBOARD OF RT OUTBOARD SEAT TRACK. REPAIRED PER MM 53-20-11 FIG 804 A.Feb 2, 1995 · N492DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S950501Clip · crackedDURING HMV, FOUND SKIN CLIP CRACKED AT FS 1050 BETWEEN STR 30 AND 29L, REPAIRED PER M/M 53-11-0 FIG 815.Feb 2, 1995 · N492DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950495Clip · corrodedAT HMV, FOUND FS 950F FRAME TO SKIN SHEAR TIE CORRODED AT STRINGER 29R. REPAIRED PER MM 53-11-0 FIG 815.Feb 2, 1995 · N492DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950478Clip · brokenAT HMV, FOUND FS 980 FRAME TO SKIN CLIP CRACKED BETWEEN STRINGERS 29R AND 30. REPAIRED PER MM 53-11-0 FIG 815.Feb 2, 1995 · N492DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950477Clip · crackedAT HMV, FOUND FS 950A FRAME TO SKIN SHEAR TIE CRACKED BETWEEN STRINGERS 28-27R. REPAIRED PER MM 53-11-0 FIG 815.Feb 2, 1995 · N492DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L950511Skin · punctureDURING SHOP INSPECTION, NR 1 ENGINE NOSE COWL OUTER SKIN WAS FOUND WITH PUNCTURE DAMAGE AT 7 O'CLOCK POSITION. REPAIRED PER SRM 54-30-3.Feb 2, 1995 · N502DA · Boeing 727232 · Engine Cowling SystemSDR DL72S950696Frame · crackedFWD B/B STA 600 FRAME CRACKED AT STR CLIPS STR 23 AND 24 LEFT. REPAIRED PER SRM 53-10-4 PG 88-90. DAMAGE FOUND AND REPAIRED AT HMV VISIT.Feb 1, 1995 · N492DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S950695Rib · crackedAT HMV, NR 3 L/E SLAT WAS FOUND WITH CRACKED RIBS JUST INBOARD OF THE INBOARD SLAT TRACK AND OUTBOARD OF TAI DUCT. REPAIRED PER MM 57-54-0 PG 807.Feb 1, 1995 · N492DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950694Rib · crackedAT HMV, FOUND NR 3 L/E SLAT WITH RIBS NR 1 AND NR 2 CRACKED. REPAIRED PER SRM 57-50-3 FIG 9 AND MM 57-54-0 PG 819.Feb 1, 1995 · N492DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950691Channels · wornCHANNELS WORN FWD B/B AFT BULKHEAD TWO VERTICAL SUPPORT CHANNELS ARE WORN (LOC OVER STG 26L AND 26R) AT FLEX JOINTS. ALSO, RIVETS SHEARED LEFT SUPPORT AT CEILING. FOUND AT HMV, REPAIRED PER SRM 53-10-9 FIG 8, REPLACED RIVETSFeb 1, 1995 · N492DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S950690Rib · crackedAT HMV, FOUND RT WING NR 6 SLAT WITH THE 2ND RIB FROM THE INBOARD END CRACKED AND 2 CRACKS IN RIB ON THE OUTBARD SIDE OF THE INBOARD TRACK. REPAIRED PER SRM 57-50-3 PG 25.Feb 1, 1995 · N492DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950622Stringer · crackedAT HMV, FOUND FUSELAGE STRINGER 7R, CRACKED FORWARD OF FS 560, REPAIRED PER SRM 51-10-3.Feb 1, 1995 · N492DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S950599Stringer · crackedAT HMV, FOUND STRINGER 9 LT CRACKED AT 3RD BULHEAD UP FROM ACCESS PANEL INSIDE VERTICAL STABILIZER. REPAIRED PER SRM 55.Feb 1, 1995 · N492DA · Boeing 727232 · Vertical StabilizerSDR DL72S950598Stringer · crackedAT HMV, FOUND STRINGER 4 LT. CRACKED AT 5TH BULKHEAD FROM ACCESS PANEL IN VERTICAL STABILIZER. REPAIRED PER SRM 55.Feb 1, 1995 · N492DA · Boeing 727232 · Vertical Stabilizer
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