Boeing 727-232

Service difficulty reports · 6,539

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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 = '727232'
  ORDER BY difficulty_date DESC"

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SDR DL72S950596Rib · crackedRIB CRACKED, 3RD RIB OUTBOARD OF ACTUATOR MOUNT ON NR 6 L/E SLAT. FOUND DURING INSP AT HMV2 IN ATL. REPAIRED PER MM 57-54-0 PG 819.Feb 1, 1995 · N492DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950595Angle · crackedLOWER CHORD ANGLE CRACKED AT 2ND RIB O/B OF ACTUATOR FITTING ON NR 6 L/E SLAT. FOUND DURING INSP AT HMV2 IN ATL. REPAIRED PER MM 57-54-0 PG 816.Feb 1, 1995 · N492DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950594Stringer · crackedSTRINGER CRACKED AT FS 133.800, STR 9L CRACKED AT RIB. FOUND DURING INSPECTION AT HMV2 IN ATL. REPAIRED PER MM 55-30-0 PG 803.Feb 1, 1995 · N492DA · Boeing 727232 · Vertical StabilizerSDR DL72S950593Rib · crackedOUTBOARD RIB CRACKED ON NR 5 L/E SLAT. FOUND DURING INSPECTION AT HMV2 IN ATL. REPAIRED PER MM 57-54-0 PG 819.Feb 1, 1995 · N492DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950592Stops · wornINBOARD AND OUTBOARD STOP WORN ON NR 5 L/E SLAT. FOUND DURING INSPECTION AT HMV2 IN ATL. REPAIRED STOPS PER MM27-81-11 PG 803.Feb 1, 1995 · N492DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950591Rib · crackedRIB CRACKED, 2ND RIB FROM OUTBOARD END OF NR 5 L/E SLAT. FOUND DURING INSPECTION AT HMV2 IN ATL. REPAIRED PER M/M 57-54-0 PG 819.Feb 1, 1995 · N492DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950588Stringer · crackedDURING HMV, FOUND STRINGER 15 LEFT CRACKED AT LOWER RIVET STA 380, REPAIRED PER 53-10-3 FIG 1.Feb 1, 1995 · N492DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S950586Le Rib · crackedDURING HMV, FOUND RIB CRACKED ON INBD SIDE OF INBD TRACK ON NR 7 L/E SLAT AND A RIB CRACKED ON OUTBD SIDE OF INBD TRACK NR 7 SLAT, REPAIRED PER MM 57-54-0 PG 805 ON INBD SIDE AND OUTBD SIDE PER MM 57-57-0 PG 805.Feb 1, 1995 · N492DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950585Rib · crackedDURING HMV, FOUND RIB CRACKED ON O/B SIDE OF NR 6 L/E SLAT TAI DUCT AND A RIB CRACKED NEXT RIB O/B OF ITEM NR 1, REPAIRED BYSTOP DRILLING CRACK AND FABRICATING REPAIR DOUBLER PER SRM 57-50-3 PG 25, INSTALLED REPAIR PER SRM 57-50-3 PG 25.Feb 1, 1995 · N492DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S950573Seat Track · crackedFWD SUPPORT LUG OF SEAT TRACK CRACKED, LOC STA760 RT O/B SEAT TRACK. REPAIRED PER SRM 53-10-8 PG 47-49 FIG 11. THIS ITEM WAS FOUND DURING INSPECTION AT HMV2.Feb 1, 1995 · N492DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950572Frame · crackedFUSELAGE FRAME CRACKED AT TWO FASTENER HOLES STA 312 AT STR 13R. FABRICATED REPAIR ANGLES PER SRM 53-10-4. INSTALLED REPAIR PER SRM 53-10-4. ITEM FOUND DURING INSPECTION AT HMV 2.Feb 1, 1995 · N492DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S950508Stringer · crackedDURING INSPECTION FOUND FUSELAGE STRINGER 18A LEFT SIDE, CRACKED ON HORIZONTAL FLANGE AT FS 950. REPAIRED PER MM 53-12 PG 818 ITED LEVEL 2 REPAIR.Feb 1, 1995 · N400DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S950499Stringer · crackedDURING HMV, FOUND RT WING WS 656 STRINGER 11 ABOVE TANK PLATE CRACKED. REPAIRED PER M/M 57-13-0 FIG 804.Feb 1, 1995 · N492DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S950480Aft Trnvrse Beam · crackedDURING ROUTINE INSPECTION AT LETTER CHECK, THE RT TORQUE BOX HAD STIFFENERS CRACKED AT FS 1263. IN ACCORDANCE WITH B727 S/B 53-0129, REV 4, THE PART WAS REPLACED.Feb 1, 1995 · N539DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950449Door Frame · crackedFOUND ON CV2 CHECK, .5 INCH CRACK EXTENDING FROM LOWER AFT STOP CASTING IN FWD SVC DOOR FRAME REPAIRED PER M/M 52-12-0.Feb 1, 1995 · N411DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950876Le Skin · wornDURING SHOP VISIT LE WAS FOUND WORN 17 INCHES AND 22 INCHES FROM IB END. A REPAIR DOUBLER WAS INSTALLED PER SRM 57504 AFTER IT WAS DETERMINED THAT WEAR EXCEEDED ALLOWABLE DAMAGE LIMITS OF SRM 57-50-01 FOR NR 3 FORE FLAP.Jan 31, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950827Skin · delaminatedAT HMV, NR 2 FORE FLAP WAS FOUND WITH TOP SKIN DELAMINATED AT 44 INCHES FROM THE I/B END. REPAIRED PER SRM 57-50-4, WITH REF TO SRM 51-40-06.Jan 31, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950749Skin · disbondedLEVELING COMPOUND DISBONDED AND LIFTING O/B STR 27R AFT STA 480 FOUND AT HMV. CUT OUT DAMAGE AND REPAIRED PER SRM 53-30-3 FIG 3A.Jan 31, 1995 · N492DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S950748Skin · corrosionSEVERAL AREAS OF LT CORR BET STR 27 AND 28 RT JUST AFT OF STA 480 FRAME FWD B/B FOUND AT HMV. CUT OUT CORR AREA FAB REPAIR DOUBLER PER SRM 53-30-3 INSTALLED REPAIR PER ERA 301155-14Jan 31, 1995 · N492DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S950732Skin · corrodedSKIN CORRODED BETWEEN STR 27 AND 28 RIGHT AFT OF STA 480 FWD BB REMOVED CORROSION, FABRICATED DOUBLER PER SRM 53-30-3. REPAIRED PER ERA 301155-14, FOUND AND REPAIRED AT HMV.Jan 31, 1995 · N492DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S950587Stringer · crackedDURING HMV, FOUND FUEL TANK UPPER STRINGER NR 17 CRACKED AT WS 338.50, REPAIRED PER SRM 57-10-4 FIG 6 AND ERA 301143-14 REV A.Jan 31, 1995 · N492DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S950512Skin · damagedHOLE IN LOWER SKIN PANEL 9 IN FROM O/B END OF LT AILERON. ITEM FOUND DURING INSPECTION AT HMV2 IN ATL. ITEM REPAIRED PER SRM 57-50-5.Jan 31, 1995 · N492DA · Boeing 727232 · Wing, Plate/SkinSDR DL72S950500Hinge Bushing · looseDURING HMV, FOUND NR 5 FLAP TRACK, FWD BUSHING HINGE FOR STRUT DOOR BUSHING IS LOOSE AND WORKING IN BORE, REPAIRED PER M/M 57-43-0 FIG 804.Jan 31, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950488Skin · crackedAT HMV, FOUND CRACK IN LOWER SKIN PANEL OF LEFT WING OUTBOARD AILERON. REPAIRED PER SRM 57-50-5.Jan 31, 1995 · N492DA · Boeing 727232 · AileronsSDR DL72S950455Stiffener · crackedFOUND ON F1 LETTER CHECK 1. 2 IN CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NR 7 SLAT OUTBD TRACK INBD ANGLE LOWER END 2. 1 .5 INCH CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NR 7 SLAT OUTBD TRACK OUTBD ANGLE LOWER END, REPAIR - 1. REPLACED STIFFENER PER Jan 31, 1995 · N494DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S950454Stiffener · crackedFOUND ON F1 LETTER CHECK, 1. 3 IN CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NBR 7 SLAT INBD TRACK INBD ANGLE LOWER END 2. 3 IN CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NBR7 SLAT INBD TRACK OUTBD ANGLE LOWER END, REPAIRED PER MM 57-20-21 PG 813.Jan 31, 1995 · N494DA · Boeing 727232 · Wing SparSDR DL72S950451Stiffener · crackedFOUND ON F1 LETTER CHECK, 3 IN CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NR 6 SLAT OUTBD TRACK INBD ANGLE LOWER END, REPAIR. INSTALLED NEW ANGLE PER M/M 57-20-21 PG 813.Jan 31, 1995 · N494DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S951806Te Flap · crackedAFT I/B CONTROL ROD CUTOUT HAS CRACKED O/B CORNER (MARKED). MANUFACTURED AND INSTALLED DOUBLER PER MM 57-52-0 PAGE 819 FOR NR 3 MID FLAP AT HMV, SHOP INSPECTION.Jan 30, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951401Spar Rail · crackedTHE NR 2 MID FLAP DURING HMV TO SHOP, WAS FOUND TO HAVE A CRACKED AFT SPAR RAIL 41 INCHES FROM O/B END OF FLAP. CRACK WAS REPAIRED PER MM 57-52-0 PG 807.Jan 30, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951400Spar Rail · crackedTHE NR 2 MID FLAP DURING HMV TO SHOP, WAS FOUND TO HAVE AN CRACKED AFT LOWER RAIL AT I/B AFT FLAP TRACK O/B CORNER. CRACK WAS REPAIRED PER MM 57-52-0 PG 807.Jan 30, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951399Spar Rail · carckedTHE NR 2 MID FLAP DURING HMV TO SHOP, WAS FOUND THAT THE AFT LOWER RAIL HAS TWO CRACKS I/B AFT FLAP DRIVE CUTOUT. THIS CRACKS WERE REPAIRDED PER MM 57-52-0 PG 807.Jan 30, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951398Skin · crackedTHE NR 2 MID FLAP DURING HMV SHOP INSP, WAS FOUND TO HAVE A CRACKED COVE SKIN AT THE I/B DRIVE ROD CUT OUT. THIS CRACK WAS REPIRED PER MM 57-52-0 PG 819.Jan 30, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951005Mid Flap · corrodedNR 4 MID FLAP, I/B AND O/B THRUST BEARING BORES CORRODED. REPAIRED PER SRM 575004, MACHINED THRUST BORES AND INSTALLED BUSHINGS.Jan 30, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950898Rib · crackedNR 1 MID FLAP, I/B AFT RIB CRACKED. REPAIRED PER SRM 575200 INSTALLED DOUBLER.Jan 30, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950897Thrust Bearing · corrodedNR 1 MID FLAP, O/B THRUST BEARING BORE CORRODED. REPAIRED PER SRM 575004 FIG 15. MACHINED OVERSIZE AND INSTALLED BUSHING.Jan 30, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950896Support · corrodedNR 1 MID FLAP, O/B CARRIAGE SUPPORT FITTING, THURST BEARING RETAINER UPPER I/B AND O/B BOLT HOLES CORRODED ALSO LOWER I/B BOLT HOLE CORRODED. REPAIRED PER SRM 575004 FIG 14. OVERSIZED HOLES AND INSTALLED BUSHINGS.Jan 30, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950895Retainer · corrodedNR 1 MID FLAP, I/B CARRIAGE SUPPORT FITTING, THRUST BEARING RETAINER UPPER BOLT HOLES CORRODED. REPAIRED PER SRM 575004 FIG. 14, OVERSIZED HOLES AND INSTALLED BUSHINGS.Jan 30, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950674Le Skin · crackedAT HMV SHOP INSPECTION, NR 1 FORE FLAP L/E SKIN WAS FOUND CRACKED AT O/B CUT OUT PAN. REPAIRED PER SRM 57-50-04.Jan 30, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950566Le Skin · dentedAT HMV SHOP INSPECTION, THE RIGHT WING NR 4 AFT FLAP LEADING EDGE SKIN WAS FOUND DENTED AT 64 INCHES FROM THE I/B END OF FLAP. REPAIRED PER SRM 57-50-4.Jan 30, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950875Skin · dentedDURING INSPECTION TOP SKIN FOUND DENTED AT 46 INCHES AND 60 INCHES FROM I/B END. RT WING NR 3 FORE FLAP. REPAIRED PER SRM 57-50-4.Jan 29, 1995 · N492DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L951017Angle · wornNR 6 SLAT, ITEM NR 1, INNER CLOSE OUT PANEL LOWER ATTACH ANGLE HAS ELONGATED HOLE 4.5 INCHES FROM I/B END. ITEM NR 2, REPAIR INSUFFICIENT AT LOWER ATTACH ANGLE T-DUCT CUTOUT. REPAIRED BOTH ITEMS PER SRM 57-54-0 FIG 805A.Jan 29, 1995 · N507DA · Boeing 727232 · Leading Edge DevicesSDR DL72L951016Rib · crackedNR 6 SLAT, SECOND RIB FROM I/B END CRACKED AT LOWER END. INSTALLED DOUBLER PER M/M 57-54-0 FIG 814. DAMAGE FOUND DURING SHOP INSPECTION.Jan 29, 1995 · N507DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950403Uplock Frame · crackedDURING E-1 LETTER CHECK, FOUND RT MLG UPLOCK FRAME CRACKED AT FS 913.5, ABOVE RADIUS BLOCK. REPAIRED PER MM 53-11-0 PG 834-837.Jan 27, 1995 · N403DA · Boeing 727232 · Landing Gear Retraction/Extension SystemSDR CAL950073Hyd Line · leakingMIA - FLT 334 - THE 'A' SYSTEM HYDRAULIC QUANTITY DECREASED TO .1250 GALLON WHILE IN FLIGHT. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND THE ACFT WAS DIVERTED TO MIA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP PJan 27, 1995 · N27783 · Boeing 727232 · Hydraulic System, MainSDR DL72S950438Fairing · crackedDURING INSPECTION, FOUND FUSELAGE TO WING BODY FAIRING RIGHT SIDE WITH A 7 INCH CRACK FS 720E PLUS 12 INCHES. REPAIRED PER SRM 53-30-3.Jan 26, 1995 · N401DA · Boeing 727232 · Aerodynamic FairingsSDR DL72S950380Angle · crackedDURING CORROSION INSPECTION, RIGHT WING NR 6 SLAT WAS FOUND WITH A .5 INCH CRACK IN O/B ATTACH ANGLE, JUST I/B OF O/B STOP. REPAIRED PER MM 57-54-0 PG 816.Jan 26, 1995 · N411DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950379Rib · crackedDURING CORROSION INSPECTION, RIGHT WING NR 6 SLAT WAS FOUND WITH A 1 INCH CRACK IN L/E RIB, JUST OUTBOARD OF INBOARD SLAT TRACK. REPAIRED PER MM 57-54-0 PG 815-815A.Jan 26, 1995 · N411DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950378Skin · crackedDURING CORROSION INSPECTION, RT WING NR 6 SLAT WAS FOUND WITH A 2.25 INCH CRACK IN LOWER AFT SKIN. REPAIRED PER MM 57-54-0 PG 801.Jan 26, 1995 · N411DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950377Angle · crackedDURING CORROSION ISNPECTION, FOUND NR 6 SLAT WITH A .5 INCH CRACK IN ATTACH ANGLE BELOW ANTI-ICE DUCT TEE. REPAIRED PER MM 57-54-0 PG 807A.Jan 26, 1995 · N411DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950371Web · corrosionCORROSION WAS FOUND ON THE SKIN CLIP AND WEB JUST O/B OF THE LT NOSE CHORD AT STA 303.9. THE DAMAGE WAS REPAIRED PER MM 53-30-0 FIG 806. DAMAGE FOUND DURING SPECIAL INSPECTION.Jan 26, 1995 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
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