Boeing 727-2A1

Service difficulty reports · 502

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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 = '7272A1'
  ORDER BY difficulty_date DESC"

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SDR UPS01234805Structure · crackedINSPECTION TYPE:IN, CRACK FOUND IN LIGHTENING HOLE, AFT AIRSTAIRS AREA AT APPROX STATION 1283 AT WL 175, LT SIDE. STOPPED DRILLED CRACK PER SRM 51-10-1/11, ITEM 9A.Jan 30, 2001 · N213UP · Boeing 7272A1 · Fuselage Main, StructureSDR UPS01235023Stringer · corrodedINSPECTION TYPE:C CORROSION (C53-100-01.00-04) UNDER STRINGER 29L BETWEEN BS 1166- BS 1183 AND T-CLIP AT 1183. REMOVED CORROSION ON STRINGER 29L IN AN AREA OF 1.0 X.5 X.020 INCH FROM ORIG THICKNESS OF .090 INCH OUT OF LIMITS PER SRM 53-10-1, SRM 53-10-2 SRM 5Jan 10, 2001 · N214UP · Boeing 7272A1 · Fuselage Main, Longeron/StringerSDR UPS01235022Shear Tie · corrodedINSPECTION TYPE:C CORROSION (C53-113-01.00-01) ON FRAME SHEAR TIE, BS 600 BETWEEN STR 28R AND STR 28L. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-4, 51-10-2, 51-30-2 AND MM 51-20-151.Jan 7, 2001 · N214UP · Boeing 7272A1 · Fuselage Main, StructureSDR C8GA200000013Switch · inoperativeFLT 033 FROM ELP TO DAY. AFTER TAKEOFF, WHEN RETRACTING FLAPS, THE TRANSIT LIGHT FOR THE LEADING EDGE FLAPS REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO ELP AND LANDED WITHOUT FURTHER INCIDENT. FOUND THE NR 6 LEADING EDGE FLAP SWITCH INOPERATIVE. REPLACEOct 20, 2000 · N287 · Boeing 7272A1 · Leading Edge Slat Position Indicating SystemSDR C8GA200000005Accessory Unit · inoperativeFLIGHT 716 FROM TOL TO ATL. AFTER TAKE OFF AND ON CLIMB OUT, WHEN GEAR HANDLE PLACED IN THE UP POSITION, THE GEAR WARNING HORN SOUNDED. WITH GEAR RETRACTED, GEAR RED LIGHTS REMAINED ILLUMINATED. CYCLED GEAR NO EFFECT. SELECTED GEAR DOWN AND RETURNED TO TOLJul 7, 2000 · N286 · Boeing 7272A1 · Landing Gear Position and WarningSDR C8GA200000001Adi · inoperativeFLT 579 FROM KMCO TO KPIA, NR 1 GYRO FAILURE ON CLIMBOUT AND NR 2 COMPASS LAGS 20 DEGREES IN TURNS. RETURNED TO KMCO WITHOUT FURTHER INCIDENT. TROUBLESHOT TO A DEFECTIVE ATTITUDE DIRECTION INDICATOR (ADI) ON THE CAPTAINS POSITION. REMOVED AND REPLACED THE CApr 25, 2000 · N287SC · Boeing 7272A1 · Directional Gyro and Indicating SystemSDR UPS99231000Light · inopCOCKPIT EMERGENCY LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AND TESTED PER MM 33-50-101. OPS CHECK GOOD.Oct 28, 1999 · N213UP · Boeing 7272A1 · Emergency LightingSDR UPS99230991Battery Pack · dischargedINSPECTION TYPE:N/A, ENTRY DOOR EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.Oct 26, 1999 · N214UP · Boeing 7272A1 · Emergency LightingSDR UPS99230990Battery Pack · dischargedINSPECTION TYPE:N/A, COCKPIT EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.Oct 26, 1999 · N214UP · Boeing 7272A1 · Emergency LightingSDR SCNA99605Battery Pack · dischargedDURING A HEAVY MAINTENANCE CHECK, THE R1 SLIDE LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE BATTERY PACK IAW MM 335022, OPERATIONALLY CHECKS GOOD.Oct 12, 1999 · N286SC · Boeing 7272A1 · Emergency LightingSDR SCNA99602Beam · crackedDURING A HEAVY MAINTENANCE CHECK, A CRACKED DOUBLER WAS FOUND AT BS 1183 PRESSURE WEB AT THE 6 O'CLOCK POSITION ON THE LEFT VERTICAL I BEAM ON THE BOTTOM. REMOVED AND REPLACED THE VERTICAL STIFFENER.Oct 12, 1999 · N286SC · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR SCNA99601Beam · crackedDURING A HEAVY MAINTENANCE CHECK, THE I BEAM IN THE AFT PIT AT BL 0 OF 1183 BULKHEAD WAS FOUND TO EXHIBIT CORROSION ON THE LOWER LEFT SIDE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. I BEAM TO BE REPLACED.Sep 21, 1999 · N286SC · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR SCNA99603Beam · crackedDURING A HEAVY MAINTENANCE CHECK, A CREASE BEAM WAS FOUND CRACKED AT LEFT FS 740 SIDE. FABRICATED A NEW ATTACH Z-ANGLE OUT OF 7075 T6 .040 PER B727 SRM 51-20-1. FABRICATED REPAIR ANGLES OUT OF 7075 T6 .063 IAW BAC 727 SRM 51-40-4. INSTALLED REPAIR ANGLES ANSep 18, 1999 · N286SC · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230642Beam · corrodedINSPECTION TYPE:SI, LT MLG BEAM IS CORRODED AT NR 4 FLAP TRACK MOUNT BOLT HOLES. REMOVED CORROSION AND REPAIRED LG BEAM PER ER NR 99-6038.Sep 15, 1999 · N213UP · Boeing 7272A1 · Wing Miscellaneous StructureSDR UPS99230641Chord · corrodedINSPECTION TYPE:SI WHILE WORKING CARD NR919297 DISCOVERED GOUGES AND CORROSION ON BS 345-350 RBL 20 WL 148 (DAMAGED RT NOSE GEAR DRAG BRACE SIDE CHORD). REMOVED AND REPLACED PER SRM 51-30-2.Sep 10, 1999 · N213UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230640Flap Track · corrodedINSPECTION TYPE:SI, NR 5 FLAP TRACK IS CORRODED AT FWD ATTACH LUG AND AT SPOILER BEAM ATTACH POINT. REPLACED NR 5 FLAP TRACK. REMOVAL AND INSTALLATION ACCOMPLISHED ON TC NR C57-581-04-4A.Sep 6, 1999 · N213UP · Boeing 7272A1 · Trailing Edge FlapsSDR UPS99230599Flap Track · corrodedINSPECTION TYPE:SI NR 6 FLAP TRACK IS CORRODED AT FWD ATTACH LUG AND AT SPOILER BEAM ATTACH POINT. REPLACED NR 6 FLAP TRACK. INSTALLATION OF NEW NR 6 FLAP TRACK WILL BE ACCOMPLISHED ON TC NR C57-581-04-4D.Sep 6, 1999 · N213UP · Boeing 7272A1 · Trailing Edge FlapsSDR UPS99230598Wing · corrodedINSPECTION TYPE:SI NR 4 FLAP TRACK CORRODED AT SPOILER BEAM MOUNT BOLT HOLES AREA AND FWD FITTING MOUNT BOLT HOLE. REPLACED NR 4 FLAP TRACK. INSTALLATION OF NEW NR 4 TRACK WILL ACCOMPLISHED ON TC NR C57-581-04-3D.Sep 6, 1999 · N213UP · Boeing 7272A1 · Trailing Edge FlapsSDR SCNA99600Floorbeam · crackedDURING A HEAVY MAINTENANCE CHECK, A FLOORBEAM WAS FOUND CRACKED AT RBL 55 FS 760.95. FABRICATED, TREATED AND INSTALLED A REPAIR DOUBLER IAW B727 SRM 51402 AND 51201, 51302.Sep 2, 1999 · N286SC · Boeing 7272A1 · Fuselage Main, Floor BeamSDR SCNA99604Frame · crackedDURING A HEAVY MAINTENANCE CHECK IN THE AFT CARGO COMPARTMENT AT FS 950F WL 203 RBL 55. THE FUSELAGE SKIN FRAME WAS FOUND CRACKED FWD OF THE DOOR WARNING SWITCH ON THE SECONDARY LIP FLANGE. FOUND SEAL DEPRESSOR DAMAGED BEYOND REPAIR. FABRICATED A NEW SEAL DAug 31, 1999 · N286SC · Boeing 7272A1 · Fuselage Main, FrameSDR UPS99230533Frame · crackedINSPECTION TYPE:SI, FRAME IS CRACKED AROUND FASTENER HOLE AT BS 360 LBL 68, WL 303 JUST ABOVE STR 8. DAMAGE WAS OUT OF LIMITS. CUT OUT DAMAGE AREA 2.0' X 2.4 X .050, FABRICATED REPAIR DOUBLER OUT OF 7075.0. 50. SENT TO HEAT TREAT TO-T6 CONDITION AND INSTALLAug 30, 1999 · N213UP · Boeing 7272A1 · Fuselage Main, FrameSDR UPS99230514Seat Track · corrodedINSPECTION TYPE:SI, SEAT TRACK CORRODED AT BS 700 LBL 25 WL 208. REPLACED SEAT TRACK EXTRUSION FROM BS 690 TO BS 720D+10 PER 727 SRM 53-10-5.Aug 30, 1999 · N213UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS99230510Frame · corrodedINSPECTION TYPE:SI, CORROSION ON FRAME HAT SECTION AT BS 720E FRAME ABOVE STR 5R TO STR 15R. CORROSION OUT OF LIMITS, FABRICATED NEW FRAME, REPLACEMENT PER SRM 53-10-4.Aug 28, 1999 · N213UP · Boeing 7272A1 · Fuselage Main, FrameSDR UPS99230536Seat Track · corrodedINSPECTION TYPE:SI, CORROSION ON SEAT TRACK B STA 372 TO 377, LBL 45, WL 208. CORROSION CLEAN-UP BEYOND ACCEPTABLE LIMITS. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM 51-30-5 AND 51-30-8.Aug 26, 1999 · N213UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS99230532Frame · crackedINSPECTION TYPE:SI, BS 360 FRAME IS CRACKED AT NUT PLATE HOLE, BS 360 WL 218, LBL 68. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3 PG 1-6.Aug 25, 1999 · N213UP · Boeing 7272A1 · Fuselage Main, FrameSDR UPS99230512Seat Track · corrodedINSPECTION TYPE:SI, SEAT TRACK CORRODED BETWEEN 580 - 600 RBL 45 WL 208. REPLACED SEAT TRACK RBL 45 BS 540 TO 610 PER SRM 53-10-5.Aug 25, 1999 · N213UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS99230511Seat Track · corrdedINSPECTION TYPE:SI, SEAT TRACK CORRODED AT BS 950F - 1010 LBL 45 AT NUT PLATE HOLES. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 3. REMOVED AND REPLACED SEAT TRACK FROM BS 950E BS 1020 LBL 45 PER 53-10-5.Aug 23, 1999 · N213UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS99230530Seat Track · corrodedINSPECTION TYPE:SI, SEAT TRACK CORRODED AT BS 950B-950C LBL 25 WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED SEAT TACK FROM BS 950+10 TO BS 950F+10 LBL 25 PER SRM 53-10-5.Aug 21, 1999 · N213UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS99230645Stringer · corrodedINSPECTION TYPE:SI, CORROSION (C57-571-01.02-02) RW FUEL CELL INTERIOR AROUND FASTENERS ON STR 4 BETWEEN WS 224.5 AND WS 251.0. REPAIRED PER ER 99-6010 FILE NR 727-57-2110.Aug 20, 1999 · N213UP · Boeing 7272A1 · Wing, Longeron/StringerSDR UPS99230644Stringer · corrodedINSPECTION TYPE:SI, CORROSION IN 3 AREAS R/W FUEL CELL INTERIOR, UPPER SURFACE OF LOWER SKIN BETWEEN WS 304 AND WS 277.5 STR 10-11. REMOVED CORROSION PER SRM 51-10-6, REPAIRED STRINGER 10 PER SRM 57-10-4 AND ER 99-6058.Aug 20, 1999 · N213UP · Boeing 7272A1 · Wing, Longeron/StringerSDR UPS99230643Stringer · corrodedINSPECTION TYPE:SI, CORROSION (C57-571-01.02-02) RW FUEL CELL INTERIOR ON STR 4 AROUND SEVERAL FASTENERS BETWEEN WS 251.0 AND WS 277.5. REPAIR WORK DONE PER ER 99-6010 FILE NR 727-57-2110.Aug 20, 1999 · N213UP · Boeing 7272A1 · Wing, Longeron/StringerSDR UPS99230531Floorbeam · corrodedINSPECTION TYPE: SI, CORROSION ON FLOORBEAM UPPER TEE BS 620 RBL 26 TO 43. CORROSION FOUND TO BE OUT OF LIMITS ON CHORD AT RBL 31-36.5. PERFORMED FLOORBEAM REPAIR PER SRM 53-10-8.Aug 20, 1999 · N213UP · Boeing 7272A1 · Fuselage Main, Floor BeamSDR UPS99230513Seat Track · corrodedINSPECTION TYPE:SI, SEAT TRACK CORRODED BETWEEN BS 480 - 520 BL 0, WL 208. CORROSION CLEAN-UP BEYOND ACCEPTABLE LIMITS. FABRICATED AND INSTALLED REPLACEMENT TRACK PER SRM 51-10-8 AND 53-10-5.Aug 20, 1999 · N213UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS99230600Seat Track · corrodedINSPECTION TYPE:SI SEAT TRACK CORRODED AT BS 680-740 LBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 660-740 PER SRM 51-30-2 AND 53-10-5 FIG 1.Aug 16, 1999 · N213UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS99230534Beam · corrodedINSPECTION TYPE:SI, SPOILER BEAM MOUNT PAD FOR NR 6 FLAP TRACK IS CORRODED (ON WING SIDE). REMOVED AND REPLACED SPOILER BEAM MOUNT PAD PER SRM 51-20-151, 51-30-2.Aug 14, 1999 · N213UP · Boeing 7272A1 · Wing Miscellaneous StructureSDR UPS99230241Skin · corrodedINSPECTION TYPE:C WHILE WORKING CARD 973519, FOUND CORROSION ON INNER SKIN AT BS 1005, RBL 7, WL 148. REMOVED CORRODED SECTION OF SKIN AT BS 1005, RBL 7, WL 148 AND REPAIRED IAW ER NR 99-5802 AND SRM 53-30-03 FIG 3A.Jul 28, 1999 · N214UP · Boeing 7272A1 · Fuselage Main, Plate/SkinSDR UPS99230239Keel Beam · corrodedINSPECTION TYPE:C CORROSION (C53-113-01.06-02) BS 982 RT KEEL BEAM. REMOVED CORRODED KEEL BEAM SEGMENT AND REPLACED WITH NEW SEGMENT IAW ER 99-5790.Jul 28, 1999 · N214UP · Boeing 7272A1 · Fuselage Main, KeelSDR UPS99230240Stringer · corrodedINSPECTION TYPE:C WHILE WORKING CUST CARD NR 973522 FOUND CORROSION ON STR 20R STA 1153. REMOVED CORRODED STRINGER BS 1153 AND REPLACED WITH NEW STRINGER IAW SRM 51-40-03, 51-10-1, 51-30-02, DRW NR 65-16349.Jul 27, 1999 · N214UP · Boeing 7272A1 · Fuselage Main, Longeron/StringerSDR UPS99230238Clip · corrodedINSPECTION TYPE:C CORROSION ON SHEAR TIE T-CLIP AT BS 990, RBL 8, WL 148 BETWEEN STR 29-29 R (WHILE WORKING CARD 973519). REMOVED CORRODED T-CLIP AND REPLACED WITH NEW T-CLIP IAW 51-10-1 AND 51-30-02.Jul 26, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230172Shear Tie · corrodedINSPECTION TYPE:C WHILE WORKING 973519, FOUND CORROSION ON SHEAR TIE AT BS 970 RBL 8, WL 148 BETWEEN STRINGER 28, 29R. REPAIRED SHEAR TIE AT BS 970 RBL 8 WL 148 PER SRM 53-10-1, 51-30-2, 53-10-4, 51-10-2.Jul 25, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230171Shear Tie · corrodedINSPECTION TYPE:C CORROSION ON FRAME SHEAR TIE BS 990, RBL 4, WL 148 BETWEEN STR 29-30R. REMOVED DAMAGE SHEAR TIE AND REPAIRED IAW SRM 53-10-04 FIG 15.Jul 23, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230170Seat Track · corrodedINSPECTION TYPE:C CORROSION ON SEAT TRACK UPPER SURFACE O/B SIDE BS 950, LBL 45. REMOVED AND REPLACED SEAT TRACK FROM BS 870 TO BS 960.Jul 23, 1999 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS99230156Crease Beam · crackedINSPECTION TYPE:C, LEFT I/B CREASE BEAM IS CUT AT BS 116, WL 209, LBL 64. FOUND CREASE BEAM TO BE CRACKED AT BS 1166, WL 209, LBL 64 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF CREASE BEAM FROM BS 1157 TO BS 1177, FABRICATED NEW CREASE BEAM, REPAIJul 23, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230157Splice · corrodedINSPECTION TYPE:C, WHILE WORKING CARD 973519, FOUND CORROSION AND GOUGE ON STRINGER SPLICE BS 1000, STR 29R, RBL 6, WL 148. REMOVED AND REPLACED STR SPLICE BS 1000 STR 29R, RBL 6, WL148, WITH NEW STR SPLICE.Jul 22, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR SCNA99096Switch · inopUPON GEAR RETRACTION, GEAR WARNING HORN SOUNDED. PULLED AURAL WARNING CIRCUIT BREAKER TO SILENCE HORN. RESET CIRCUIT BREAKER BEFORE GEAR EXTENSION, GEAR WARNING HORN CAME ON AND THEN WENT OUT WHEN ALL GEAR SHOWED DOWN AND LOCKED. REMOVED AND REPLACED FLAP SJul 22, 1999 · N286SC · Boeing 7272A1 · Landing Gear Position and WarningSDR UPS99230178Crease Beam · corrodedINSPECTION TYPE:C CORROSION ON CREASE BEAM I/B BS 1166, WL 209 RBL 64. CORROSION OUT OF LIMITS REPAIR WILL BE ACCOMPLISHED ON NRC 973389 DO TO OTHER DEFECTS REPAIR WILL COVER FROM 1138-1176.*Jul 12, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230177Crease Beam · corrodedINSPECTION TYPE:C CORROSION ON I/B CREASE BEAM BS 1170 WL 208 LBL 64. CORROSION OUT OF LIMITS REPAIRS WILL BE ACCOMPLISHED ON NRC 973397, WHICH ENCOMPASS THIS AREA. REPAIR GOES FROM BS 1159-1176.Jul 12, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230112Frame · crackedINSPECTION TYPE:C, CRACKS NOTED IN BS 1183, LBL 18 DOOR FRAME. ONE CRACK AT NR 7L DOOR STOP CUTOUT AND THE OTHER CRACK AT 2 FWD OF NR 7L DOOR STOP CUTOUT. ACCESSED AREA AT 1183 FRAME AND REPAIRED FRAME IAW SB B727-53-0210.Jul 6, 1999 · N214UP · Boeing 7272A1 · Fuselage Main, FrameSDR UPS99229972Window · shatteredINSPECTION TYPE:N/A, AIRCRAFT DIVERTED INTO TUL DUE TO L-2 WINDOW SHATTERED IN FLIGHT. *S/D* REMOVED AND REPLACED L-2 WINDOW WITH NEW PER MM 56-12-11 (P/N 5-71762-39) (S/N 1429) OFF. (P/N 5-71762-39) (S/N 84-H -3-5-116) ON. HEAT CONTROL (P/N 1231-2) (S/N 9Jun 25, 1999 · N214UP · Boeing 7272A1 · Flight Compartment WindowsSDR SCNA99087Power Supply · inoperativeDURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE AFT AIRSTAIR POWER SUPPLY, OPERATIONALLY CHECKS GOOD.Jun 23, 1999 · N287SC · Boeing 7272A1 · Emergency Lighting
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