Boeing 727-200

Service difficulty reports · 2,835

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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 = '727200'
  ORDER BY difficulty_date DESC"

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SDR DHL2003741513Frame · dentedDURING C-CHECK FOUND BS 460 RT CIRCUMFERENTIAL DENTED 4 INCHES ABOVE FLOOR. CUT OUT DAMAGED AREA AS PER B-727 SRM 53-10-2. FABRICATED DOUBLER REPAIR IAW B-727 SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2. INSTALLED DOUBLER AS PER B-727 SRM 51-30-2.Mar 23, 2003 · N741DH · Boeing 727200 · Fuselage Main, FrameSDR DHL2003741508Frame · dentedDURING C-CHECK DISCREPANCY AS FOLLOWS, BS 680 CIRCUMFERENTIAL DENTED WITH UNFILLED DRILL HOLE BETWEEN STRINGERS 16 LT AND 17 LT. REMOVED FASTENERS IAW B-727 SRM 51-30-2. CUT OUT DAMAGE IAW SRM 53-10-2. FABRICATED DOUBLER REPAIR IAW B-727 SRM 53-10-2 AND 53-Mar 23, 2003 · N741DH · Boeing 727200 · Fuselage Main, FrameSDR DHL2003741504Door Frame · crackedDURING C CHECK, FUSELAGE INTERIOR BS 480 AND LWR SILL BEAM. ( CARGO DOOR) FRAME ATTACH TO FUSELAGE CRACKED FWD. AND AFT. ALSO MISSING (8 EACH).Mar 23, 2003 · N741DH · Boeing 727200 · Fuselage Main, StructureSDR DHL2003741503Frame · dentedDURING C CHECK, BS 500 RT CIRCUM. DENTED 4 INCH ABOVE FLOOR. CUT-OUT DAMAGED AREA DIM 1 1/2 INCH AS PER B-727 SRM 53-10-4 FIG. 2.Mar 23, 2003 · N741DH · Boeing 727200 · Fuselage Main, FrameSDR DHL2003741502Frame · crackedDISCREPANCY AS FOLLOWS DURING C CHECK, B.S. 1030 CIRCUM. IS CRACK LT SIDE 3" ABOVE FLOOR. REMOVED FASTENER AT BS 1030 CIRCUM LT SIDE 3 INCH ABOVE FLOOR IAW B-727 SRM 51-30-2.Mar 23, 2003 · N741DH · Boeing 727200 · Fuselage Main, FrameSDR DHL2003741506Structure · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, LEFT MLG W/W FWD STA 870 O/B STRUCTURE CRACKED OUT FASTENER. REMOVED WEB AT LEFT MLG WHEEL WELL BS 870 FWD O/B STRUCTURE IAW B-727 SRM 51-30-2. PART MADE IAW B-727 SRM 51-20-1 AND 53-10-2 FIG 5. INSTALLED WEB AT LEFT MMar 22, 2003 · N741DH · Boeing 727200 · Fuselage Miscellaneous StructureSDR DHL2003749003Battery Pack1) COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE.2) REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. OPS CHECKED GOOD. DONE IAW B-727 M/M 33-50-111.Mar 22, 2003 · N749DH · Boeing 727200 · Emergency LightingSDR 2003F00330Engine · stalledNR 2 ENGINE WENT INTO A CONTINUOUS COMPRESSOR STALL SHORTLY AFTER LANDING GEAR RETRACTION ON TAKEOFF AT MSP. EGT CLIMBED INTO AND STABILIZED IN THE RED ARC FOR 1 MINUTE, RETARDED ENGINE THROTTLE TO IDLE POSITION AND ENGINE STABILIZED, ALL OTHER SYSTEMS NORMALMar 21, 2003 · N919PG · Boeing 727200 · Engine (Turbine/Turboprop)SDR 2003F00264Dome · damagedNR 2 ENGINE WENT INTO A CONTINUOUS COMPRESSOR STALL SHORTLY AFTER LANDING GEAR RETRACTIONON TAKEOFF AT MSP. EGT CLIMBED INTO AND STABILIZED IN THE RED ARC FOR 1 MINUTE, RETARDED ENGINE THROTTLE TO IDEL POSITION AND ENGINE STABILIZED, ALL OTHER SYSTEMS NORMAL.Mar 21, 2003 · N919PG · Boeing 727200 · Turbine Engine Compressor SectionSDR 03FDEA00342Connector · failedON SHORT FINAL APPROACH TO MEM. NR2 ENGINE FIRE WARNING LIGHT ILLUMINATED AND FIRE BELL SOUNDED. NO INDICATION IN COCKPIT OTHER THAN LIGHT AND BELL. FOUND PIN A AND PIN E OF PLUG D352J SHORTING TOGETHER INTERMITTENTLY. REPLACED D352J IAW MFG STANDARD MAINTENMar 21, 2003 · N210FE · Boeing 727200 · Fire DetectionSDR DHL2003741550Skin · dentedDURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS 2 EACH DENTS AFT BS 400 BELOW STR 18L. CUT OUT DAMAGE AREA (2 EACH DENTS) 1 INCH DIA BS 400 BELOW STR 18L IAW B-727 SRM 53-30-3 FIG 13. FABRICATED REPAIR DOUBLER 3.80 DIA 2024 T-3 .050 PO 9912380 IAW BMar 20, 2003 · N741DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2003741547Skin · dentedDURING C-CHECK DISCREPANCY AS FOLLOWS, C1 DOOR SKIN HAS MANY DENTS ALL ARE MARKED. AREA FOUND TO BE OUT OF LIMITS IAW B-727 SRM 52-00-2. CUT OUT DAMAGED AREA OF SKIN DIM 59 X 14.75 INCHES AND FABBED NEW SKIN FROM 2024-T3 .071 PO 9912398 (59 X 14.75 INCHES) AMar 20, 2003 · N741DH · Boeing 727200 · Cargo/Baggage DoorsSDR DHL2003741545Skin · dentedDURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS 3 DENTS BETWEEN BS 1133 AND 1148 BELOW STR 19R. REMOVED PAINT IAW B-727 MM 51-20-01. DAMAGED AREAS FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA (2 DENTS IN 1 CUTOUT) DIMMar 20, 2003 · N741DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2003741544Skin · dentedDURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS 3 DENTS FWD BS 1110 ABOVE AND BELOW STR 19 R. DAMAGED FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT 2 EACH DAMAGED AREA (2 DENTS IN 1 CUT OUT) DIM 2 X 1 INCH AND FABBED REPAIR DOUBLER Mar 20, 2003 · N741DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2003741541Skin · dentedDURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS A DENT FWD BS 1133 BELOW STR 19 R. DAMAGED FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 1 X 1 INCH AND FABBED REPAIR DOUBLER THAT INCORPORATES NR 43432, 43433, 43435,Mar 20, 2003 · N741DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2003741539Skin · dentedDURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN PREVIOUS REPAIR AT BS 1050 TO 1070 HAS DENTS AT EACH END ALONG STR 28R. REMOVED PREVIOUS REPAIR BS 1050 TO 1070 TO INCORPORATE NEW REPAIR IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA DIMENSIONS 40 X 17.5 INMar 20, 2003 · N741DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2003741537Skin · dentedDURING C-CHECK. FUSELAGE SKIN BS 472 BELOW STR 17L HAS A DENT OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGE AREA DIAMETER .875 INCH IAW B-727 SRM 53-30-3 FIG 1. FAB DOUBLER REPAIR DIAMETER 3.80 INCH FROM MAT 2024-T-3 .050 PO 9912140 AND FILLER DIMar 20, 2003 · N741DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2003741532Skin · dentedDURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS A SHARP DENT AT BS 420 BELOW STR 18L. CUT OUT DAMAGE AREA 1.90 X 1.60 INCH AT BS 420 BELOW STR 18L IAW B-727 SRM 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER 10 X 7.375 INCH 2024 T-3 -.071 PO 9912598 IAW BMar 20, 2003 · N741DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2003741531Skin · corrodedDURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS PILLOWING FWD BS 1070 AT STR 22R. REMOVED FASTENERS AT FWD BS 1070 AT STR 22R IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER REPAIR IAW B-727 SRM 53-30-0 FIG 2 FROM 2024-T3 .071 PO Mar 20, 2003 · N741DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2003741529Skin · dentedDURING C-CHECK, FUSELAGE SKIN HAS A DENT BS 345 AT STR 21 L. FUSELAGE SKIN BS 345 STR 21L HAS A DENT OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 1 X 1.75 INCH IAW B-727 SRM 53-30-3 FIG 1. FABRICATED DOUBLER EXTERNAL REPAIR FROM MAT 2Mar 20, 2003 · N741DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2003741527Skin · dentedDURING C-CHECK, FUSELAGE SKIN HAS A DENT AFT BS 1070 BELOW STR 20L. REMOVED FASTENERS FOR ACCESS BS 1070 STR 20 L IAW B-727 SRM 51-30-2. REMOVED AFT LT SIDE WALL AIR DUCT FOR ACCESS IAW B-727 SRM 36-00-01. CUT OUT DAMAGED AREA IAW B-727 SRM 53-30-3 FIG 2 DIMar 20, 2003 · N741DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2003741525Skin · dentedDURING C-CHECK, FUSELAGE SKIN HAS 2 DENTS FWD AND AFT BS 1148 ABOVE STR 19L. BLENDED AREA (PREVIOUS) 2 EACH FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGE AREA DIM 2.4 X 1.4 AND FAB REPAIR DOUBLER FROM MAT ID 2024-T3 .063 PO 9912380 DIMar 20, 2003 · N741DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2003741524Skin · corrodedDURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS PILLOWING FWD BS 420 AT STR 20R. STRIPPED PAINT ON AFFECTED AREA IAW B-727 MM 51-20-01. REMOVED FASTENERS PREVIOUS REPAIR IAW B-727 SRM 51-30-2 AND FOUND CORROSION ON REPAIR OUT OF LIMITS IAW B-727 SRMMar 20, 2003 · N741DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2003741520Skin · dentedDURING C-CHECK, FUSELAGE SKIN HAS 2 DENTS FWD BS 520 ABOVE STR 26R AND 1 DENT BELOW STR 26R. CUT OUT 2 EACH DAMAGED AREAS (2 X 1 INCH) AND (1.5 X 1.5 INCH). FABRICATED DOUBLER 2024-T3, .071, PO 9912441 (21" X 13.25 INCH) AND STRUCTURAL FILLER, 2024-T3, .06Mar 20, 2003 · N741DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2003741507Skin · canningDURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS OIL CANNING FWD BS 1050 AT STR'S 23, 24, AND 25R. CUT OUT DAMAGE AREA DIM 2.90 X 2.60 INCH 2024 T-3 IAW B-727 SRM 53-30-3 FIG 4. FAB FILLER DIM AREA 2.90 X 2.60 INCH .063 PO 9912350 AND FAB DOUBLER, SHMar 20, 2003 · N741DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00336Switch · failedMAIN CARGO DOOR LIGHT CAME ON INFLT . BOTH PACKS TURNED OFF . ALT 6000 FT PSI DIFF. 2.8 . LIGHT WENT OUT ONCE DEPRESS. COMPLIED WITH CHECKLIST RETURN TO MCO . OPERATED MCD OPEN/CLOSED SEVERAL TIMES. CLOSED DOOR AND PRESSURIZED A/C. WAS ABLE TO GET DOOR WARNMar 19, 2003 · N480FE · Boeing 727200 · Door Warning SystemSDR 2003F00263Light · brokenEMERGENCY LIGHTING BY FORWARD GALLEY AFT SIDE BROKEN. RE-INSTALLED FORWARD GALLEY EMERGENCY STRIP IAW 25-30-344. (M)Mar 18, 2003 · N910PG · Boeing 727200 · Emergency LightingSDR 03FDEA00332Frame · crackedFRAME IS CRACKED AT WL 208, BS 1176, LBL 16. BS 1176 FRAME CRACKED AT LBL 16, WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1, REMOVED BS 1176 FRAME RBL 65 - LBL 65 WL 208, LOCATED AND BACKDRILLED REPLACEMENT FRAME PER SRM 51-30-5 AND 51-30-8Mar 18, 2003 · N265FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00330Stringer · gougedGOUGE IN STRINGER 3 RT OB FLANGESTA 540. REMOVED & REPALCED STRINGER 3 RT BS 530 TO BS 550 I.A.W. FED EX EA 7-5310-69439.Mar 18, 2003 · N265FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA00329Stringer · gougedGOUGE IN STRINGER 3 RT OB FLANGE STA 520. REMOVED & REPLACED STR 3 RT BS 510 TO BS 530 IAW FED EX EA 7-5310-69439.Mar 18, 2003 · N265FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA00331Web · corrodedCORROSION ON UPPER SURFACE OF HORIZONTAL WEB INBOARD OF STRINGER 18A, BS 908 RBL 66 WL 189.Mar 18, 2003 · N265FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA00327Stringer · crackedSTRINGER END CRACKED AT FASTENER BS 720B PLUS 4 STR 15L. REPAIRED STR 15L BY SPLICING IN NEW REPAIR SECTION STRINGER FROM BS 720A+13, AFT TO LIGHT. REPAIR DONE PER 727 SRM 53-10-3 FIG 1 DETAIL 2.Mar 17, 2003 · N265FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA00316Bracket · brokenNR 1 FIRE WARNING LITE AND BELL COMES ON INTERMITTANTLY ABOUT 30 SEC INTERVALS, OCCURRED ON FINAL WITH THRUST LEVER AT IDLE. ENGINE SHUT DOWN ON LANDING. OPENED ENGINE NACELLE TO FACILITATE MAINTENANCE. DISCOVERED ENGINE FIRE DETECTION LOOP BRACKET ASSY TOMar 14, 2003 · N208FE · Boeing 727200 · Fire DetectionSDR 03FDEA00297Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 500 STR 25L.Mar 12, 2003 · N265FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00298Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 500, BETWEEN STR 23R AND 24R.Mar 12, 2003 · N265FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00299Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 520 STR 24R.Mar 12, 2003 · N265FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00300Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 580 BETWEEN STR 24L AND 25L.Mar 12, 2003 · N265FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00301Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 600, BETWEN STR 24L AND 25L.Mar 12, 2003 · N265FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00302Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 560, BETWEEN STR 24L AND 25L.Mar 12, 2003 · N265FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00303Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 660, BETWEEN STR 24L AND 25L.Mar 12, 2003 · N265FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00304Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 660 STR 24R.Mar 12, 2003 · N265FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00307Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 520, BETWEEN STR 24L AND 25L.Mar 12, 2003 · N265FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00308Frame · corrodedCORROSION ON FRAME AT WL 208 BS 1166 RBL 65.Mar 12, 2003 · N265FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00309Clamp · loose1 HR INTO FLIGHT SELECTED ENGINE THEN WING A/I (FL310 .82M) ALMOST INMEDIATELY ENG 3 STRUT OVERHEAT LIGHT ILLUMINATED. NO CHANGE AFTER QRH PROCEDURES ACCOMPLISHED. NR 3 ENGINE SHUTDOWN AS PER QRH . LIGHT REMAINED ILLUMINATED FOR 5 MORE MINUTES, THEN EXTINGUIMar 12, 2003 · N220FE · Boeing 727200 · Overheat DetectionSDR 03FDEA00310Skin · crackedNR 3 AFT LOWER CARGO DOOR INTERNAL SKIN CRACKED BETWEEN 2 LIGHTNING HOLES 8 INCHES FROM FWD EDGE, 5 INCHES FROM LOWER EDGE.Mar 12, 2003 · N265FE · Boeing 727200 · Cargo/Baggage DoorsSDR 03FDEA00295Structure · corrodedWHILE WORKING MAIN CARGO CLOSE CARD, FOUND CORROSION EMANATING FROM UNDERNEATH PLASTIC STRIP BS 825, RBL 15, WL 196Mar 11, 2003 · N464FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA00293Skin · damagedMECHANICAL DAMAGE ON SKIN BS 1066, STR 27R AT EDGE OF FASTENER HOLE. DAMAGE ON SKIN REPAIRED PER SRM 53-03-03 FIG 3.Mar 10, 2003 · N265FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00288Floor Support · corrodedCORROSION ON FLOOR SUPPORT UNDER NUTPLATE BS 1165-1166, LBL 7, WL 155. REMOVED CORROSION ON FLOOR SUPPORT UNDER NUT PLATE BS 1165-1166, LBL 7, WL 155. AN AREA OF 1 X 2 INCHES. ORIGINAL THICKNESS .063 INCH. REMAINING .050 INCH OUT OF LIMITS PER SRM 53- Mar 7, 2003 · N464FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA00287Floorbeam · corrodedCORROSION ON 950 FLOORBEAM UPPER AND LOWER SURFACE OF UPPER FLANGE AT NUT PLATE HOLE LBL 23 WL 208. REMOVED CORROSION ON BS 950 FLOORBEAM AT LBL 23 WL 208 OUT OF LIMITS IAW SRM 53- 10-1 FIG 5 REMOVED DAMAGED PORTION OF FLOORBEAM, FABRICATED AND INSTALMar 7, 2003 · N464FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA00286Frame · dentedDENTED FRAME BS 1030 LBL 28 WL 150. REPAIRED DENTED FRAME IAW EA 7-5310-69419.Mar 7, 2003 · N464FE · Boeing 727200 · Fuselage Main, Frame
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