Boeing 727-22C

Service difficulty reports · 2,328

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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 = '72722C'
  ORDER BY difficulty_date DESC"

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SDR UPS96220423Mop Sill · crackedINSPECTION TYPE SI, MOP SILL IS CRACKED STA 294 TO 300 LBL 53 WL 208. REMOVED CRACKED MOP SILL AND REPLACED WITH NEW IAW SRM 51-30-02 SRM 51-30-05, SRM 51-10-01, SRM 51-20-04.May 31, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS96220422Balance Panel · corrodedINSPECTION TYPE SI, CORROSION RT NR 5 BALANCE PANEL AT MATING SURFACES OF BALANCE PANEL HINGE AND WEIGHT ASSM. REMOVED PANEL NR 5 BALANCE BAY, DRILLED OUT FASTENERS, REMOVED CORROSION FROM DOUBLER AND FOUND DOUBLER TO BE OUT OF LIMITS. FABRICATED NEW DOUBLERMay 31, 1996 · N929UP · Boeing 72722C · Elevator, Plate/SkinSDR UPS96220421Seat Pedestal · corrodedINSPECTION TYPE SI, CORROSION ON CAPTAINS SEAT PEDESTAL STA 226, LBL 13 TO 31, WL 208. REMOVED CORROSION WAS OUT OF LIMITS, REMOVED BAD CHANNEL RECEIVED NEW CHANNEL AND INSTALLED IAW SRM 51-30-2.May 31, 1996 · N929UP · Boeing 72722C · Flight Compartment EquipmentSDR UPS96220523Hat Channel · corrodedINSPECTION TYPE SI, CORROSION ON HAT CHANNEL AT BS 342 RBL 16 TO RBL 61, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED HAT CHANNEL, FABRICATED NEW HAT CHANNEL PER BOEING DWG 65-26173-3. INSTALLED NEW HAT CHANNEL, WORK DONE IAW SRM 51-30-2 SRMMay 30, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS96220521Angle · corrodedINSPECTION TYPE SI, CORROSION IN RADIUS OF L-ANGLE AT BS 300, RBL 14 TO RBL 58 WL 208. ALSO, FOUND L-ANGLE TO BE CRACKED ALONG RADIUS. REMOVED AND REPLACED L-ANGLE WITH NEW IAW SRM 51-30-2.May 30, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS96220437Centering Crank · crackedINSPECTION TYPE SI, RUDDER AFT CONTROL CENTERING CRANK ASSM HOUSING IS CRACKED AT LEFT SPRING MOUNT FLANGE. REMOVED AND REPLACED RUDDER CENTERING MECHANISM IAW MM 27-20-91.May 30, 1996 · N929UP · Boeing 72722C · Rudder Control SystemSDR UPS96220420Web Finger · crackedINSPECTION TYPE SI, CRACKED WEB FINGER STA 500, LBL 7 WL 302. REMOVED DAMAGED SECTION OF WEB, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-30-02.May 30, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS96220419Stringer Tie · corrodedINSPECTION TYPE SI, CORROSION ON STRINGER TIE STA 950 STR 1 WL 302. REMOVED CORROSION FROM STR TIE STA 950 STR 1 WL 302, REMOVED .035 FROM ORIGINAL .163 OUT OF LIMITS. REMOVED OLD STRINGER TIE AND INSTALLED NEW TIE IAW SRM 51-30-2.May 30, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS96220418Stringer · corrodedINSPECTION TYPE SI, CORROSION ON RT STRINGER NR 7 STA 405. REMOVED CORROSION, 1 BY .025 BY .025 OF ORIGINAL .032 OUT OF LIMITS, FABRICATED REPAIR PARTS AND INSTALLED ON A/C AFTER TREATING AFFECTED AREA IAW SRM 51-10-6, 53-10-2 AND SRM 53-10-3.May 30, 1996 · N929UP · Boeing 72722C · Fuselage Main, Longeron/StringerSDR UPS96220417Rib · crackedINSPECTION TYPE SI, 2ND AND 3RD RIB CRACKED ON NR 4 SLAT. REMOVED BOTH 2ND AND 3RD RIB FROM SLAT DRILLED UP NEW RIBS AND INSTALLED IN SLAT PER SRM 51-30-2.May 30, 1996 · N929UP · Boeing 72722C · Leading Edge DevicesSDR UPS96220416Act Support Web · crackedINSPECTION TYPE SI, NR 5 K-FLAP ACTUATOR O/B TRUNNION SUPPORT WEB IS CRACKED. REMOVED CRACKED SUPPORT WEB, FABRICATED NEW SUPPORT WEB AND INSTALLED ON A/C IAW SRM 51-30-2, SRM 51-10-2.May 30, 1996 · N929UP · Boeing 72722C · Leading Edge Slat ActuatorSDR UPS96220415Intercostal · corrodedINSPECTION TYPE SI, CORROSION ON FLOORBOARD SUPPORT INTERCOSTAL STA 313 TO 327, WL 208, LBL 30 AREAS MARKED. CLEANED AND EVALUATED AREA 2.3 BY 14, OUT OF LIMITS WITH .040 REMOVED ON ORIG THICKNESS OF .078, ORDERED NEW PART RECEIVED AND INSTALLED IAW SRM 51-10May 30, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS96220550Spoiler Mixer · corrodedINSPECTION TYPE SI, CORROSION ON THE SPOILER MIXER INPUT QUADRANT. FOUND CORROSION TO BE OUT OF LIMITS SRM 57-40. REMOVED CORRODED SPOILER MIXER AND REPLACED WITH SERVICABLE UNIT MM 27-62-00, MM 27-61-31.May 29, 1996 · N929UP · Boeing 72722C · Drag Control SystemSDR UPS96220549Pulley Fittings · corrodedINSPECTION TYPE SI, L/W I/B AILERON TURN AROUND PULLEY FITTING IS CORRODED ON LOWER SURFACE. REMOVED CORRODED FITTING WHICH WAS FOUND TO BE OUT OF LIMITS IAW SRM 57-40, INSTALLED NEW FITTING IAW SRM 51-30-2, MM 27-10-00 MM 27-61-00.May 29, 1996 · N929UP · Boeing 72722C · Aileron Control SystemSDR UPS96220537Mid Spar · corrodedINSPECTION TYPE SI, CORROSION VERTICAL FIN MID SPAR CHORD IS CHAFED AND FRETTING AT ACCESS PANEL 9601. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, FABRICATED REPAIR PARTS AND INSTALLED ON A/C IAW SRM 51-30-2 AND EWO 96-2334.May 29, 1996 · N929UP · Boeing 72722C · Vertical Stabilizer, Spar/RibSDR UPS96220536Mid Spar · corrodedINSPECTION TYPE SI, RT VERT FIN MID SPAR CHORD IS CHAFED AND FRETTING AT ACCESS PANEL 9602. REMOVED CORROSION FOUND OUT OF LIMITS, FABRICATED REPAIR PARTS AND INSTALLED ON A/C SRM 51-30-2 EWO 96-2333.May 29, 1996 · N929UP · Boeing 72722C · Vertical Stabilizer, Spar/RibSDR UPS96220522Floor Beam · corrodedINSPECTION TYPE SI, CORROSION AROUND NUTPLATE ON FLANGE OF FLOOR BEAM STA 768 TO 858 RBL 45 WL 28. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-10-1, FABRICATED NEW PART AND INSTALLED IAW SRM 51-30-2.May 29, 1996 · N929UP · Boeing 72722C · Fuselage Main, Floor BeamSDR UPS96220520Expansion Link · corrodedINSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 740 TO 760 RBL 45 WL 208. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED CORRODED EXPANSION LINK AND REPLACED WITH NEW PART IAW OHM 20-41-05, 20-50-01, 20-50-03, 20-50-02.May 29, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS96220414Tab Hinge Ftg · corrodedINSPECTION TYPE SI, R/W I/B AILERON SIDE TAB HINGE FITTINGS ARE CORRODED. REMOVED CORRODED HINGE FITTINGS, LOCATED NEW ONES AND INSTALLED IAW SRM 51-30-2.May 29, 1996 · N929UP · Boeing 72722C · Aileron TabsSDR UPS96220413Hinge Fitting · corrodedINSPECTION TYPE SI, RT I/B AILERON CENTER WING SIDE HINGE FITTING IS CORRODED. REMOVED CORRODED CENTER HINGE FITTING, FOUND BEARING BLOCK TO HAVE BLOWN DUST SEAL. REPLACED WITH NEW BEARING BLOCK AND REPLACED HINGE FITTING IAW OHM 57-50-01.May 29, 1996 · N929UP · Boeing 72722C · AileronsSDR UPS96220412Center Hinge · corrodedINSPECTION TYPE SI, BULLNOSE CENTER HINGE UPPER ATTACH POINT ON NR 3 K-FLAP B-CORRODED UNDER BOLT HEADS. REMOVED K-FLAP AND REPLACED WITH NEW K-FLAP.May 29, 1996 · N929UP · Boeing 72722C · Leading Edge DevicesSDR UPS96220411Panel · corrodedINSPECTION TYPE SI, NR 5 SPOILER PANEL IS DELAMINATED AT THE CENTER HINGE FITTING UPPER SURFACE. REMOVED CENTER HINGE FITTING, REPLACED DELAMINATED AREA, FOUND CENTER HINGE FITTING TO BE CRACKED AND WILL REPLACE ON OTHER NRC, WORK DONE IAW SRM 57-50-06.May 29, 1996 · N929UP · Boeing 72722C · SpoilersSDR UPS96220410Tab Hinge Ftg · corrodedINSPECTION TYPE SI, L/W I/B AILERON TAB HAS ALL THREE HINGE FITTINGS CORRODED, TAB SIDE. REMOVED L/W AILERON TAB I/B REMOVED FITTINGS AND INSTALLED NEW FITTINGS IAW SRM 51-30-2.May 29, 1996 · N929UP · Boeing 72722C · Aileron TabsSDR RAAAB196008Light · failedRIGHT FWD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER RED TRANSMITTER LIGHT STAYS ON. REPLACED LIGHT ASSY. (M)May 29, 1996 · N831RV · Boeing 72722C · Emergency LightingSDR UPS96220409Downstop Fitting · corrodedINSPECTION TYPE SI, NR 14 SPOILER O/B DOWNSTOP FITTING IS CORRODED. REMOVED AND REPLACED NR 14 SPOILER O/B DOWNSTOP FITTING IAW SRM 51-30-02.May 28, 1996 · N929UP · Boeing 72722C · SpoilersSDR UPS96220408Skin · delaminatedINSPECTION TYPE SI, NR 10 SPOILER IS DELAMAMINATED AT THE CENTER HINGE UPPER SURFACE. REMOVED DELAMAMINATED AREA, REMOVED CENTER HINGE TO ACCESS AREA, IMPREGNATED GLASS CLOTH, SEALED REPAIR, REINSTALLED CENTER HINGE AND WORK DONE IAW SRM 51-40-06, MM 20-50-01May 28, 1996 · N929UP · Boeing 72722C · SpoilersSDR 96FDEA01037Indicator · malfunctionedCYCLED THE GEAR 3 TIMES BEFORE NOSE GEAR IND DOWN. REMOVED AND REPLACED NLG POS PER MM 32-61-21, CYCLED GEAR PER 7-11-0 AND ALL IND NORMAL.May 28, 1996 · N107FE · Boeing 72722C · Landing Gear Position and WarningSDR UPS96220240Batteries · dischargedCREW LEFT EXIT LIGHTS ARMED, A/C SHUT DOWN BY OPERATIONS. REMOVED AND REPLACED BATTERIES.May 21, 1996 · N929UP · Boeing 72722C · Emergency LightingSDR 96ZZZM1024Actuator · malfunctioningTHE NR 2 LEADING EDGE SLAT FAILED TO RETRACT AFTER TAKEOFF FROM IND. AIRCRAFT MADE AIR TURN BACK TO IND AND LANDED WITHOUT INCIDENT. REPLACED THE NR 2 SLAT ACTUATOR PER MM 27-81-32. OPS CHECK GOOD. (M)May 19, 1996 · N429EX · Boeing 72722C · Leading Edge Slat ActuatorSDR RAAAB196009Line · crackedHYD A SYSTEM LOST ALL FLUID INFLIGHT CX1-HL LEG. REPLACED CRACKED NR 1 ENGINE HYD PUMP PRESS SUPPLY LINE AT A SYSTEM MODULE. (M)May 12, 1996 · N831RV · Boeing 72722C · Hydraulic System, MainSDR 96ZZZM931Hose · rupturedAFTER TAKEOFF, THE 'A' SYSTEM HYDRAULIC POWER WAS LOST. THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT MADE AIR TURN BACK TO IND. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND RIGHT MAIN LANDING GEAR RETRACT ACTUATOR HYDRAULIC FLEX LINE RUPTURED. REPLACED DAMAGEDMay 8, 1996 · N426EX · Boeing 72722C · Hydraulic System, MainSDR RAAAB296027Press Floor · crackedDURING SCHEDULED INSPECTION OF THE PRESS FLOOR IN THE LEFT WHEEL WELL PER AD 92-19-11, FOUND THE FOLLOWING 5 CRACKS AT STATION 940, BL 29-1 .375 INCH, BL 31 .625 INCH, BL 36 .375 INCH, BL 38 .75 INCH AND BL 55 1.125 INCH. REPAIRED PER SB 53-0149 RV AND DWG 65Apr 26, 1996 · N832RV · Boeing 72722C · Fuselage Floor PanelSDR 96FDEA00771Floor Beam · corrodedUPPER LOBE, CORROSION BEYOND LIMITS IN DEPTH ON TOP SURFACE OF FLOOR BEAM BS 480, RBL 26 TO 35. CUT OUT AREA OF CORROSION AND INSTALLED FLOOR BEAM REPAIR PER SRM 51-10-6, 51-10-8 FIG 6 AND 8, ESO 11782 DATE 3-20-96 AA AND EA 7-5310-28846 DATED 3-20-96 FEDEX.Apr 4, 1996 · N103FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA00770Stringer · crackedFUSE STR 25R CRACKED AROUND FASTENER STA 365. FABRICATED AND INSTALLED REPAIR SECTION OF STR 25R, STR 365 PER SRM 53-10-3 PAGE 4C AND E.Apr 2, 1996 · N103FE · Boeing 72722C · Fuselage Main, Longeron/StringerSDR 96ZZZX2969Accessory Unit · required rerackKLEX - FLT 73391 - DURING TAKEOFF, STEADY LANDING GEAR UNSAFE HORN SOUNDED IN ALL CONFIGURATIONS. RE-RACK LANDING GEAR ACCESS UNIT. OPS CHECK GOOD ON GROUND.Mar 30, 1996 · N727CK · Boeing 72722C · Landing Gear Position and WarningSDR 96FDEA00769Bulkhead · ripplesFUSE RIPPLES IN 1183 BULKHEAD AT BOTTOM INSIDE TAIL SKID COMP. REPAIRED RT 1183 BULKHEAD AT TAIL SKID AREA PER ESO 11782 DATED 03-18-96 AND EA NR 7-5310-28179 DATED 3-26-96.Mar 28, 1996 · N103FE · Boeing 72722C · Fuselage Main, BulkheadSDR RAAAB296026Battery Pack · dischargedMID CABIN DOOR EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (M)Mar 26, 1996 · N832RV · Boeing 72722C · Emergency LightingSDR 96FDEA00713Bellframe · dentUPPER LOBE BS 580 STR 6R DENT IN BELLFRAME. REMOVED DAMAGED SECTION OF BELLFRAME, FABRICATED SECTION OF BELLFRAME, INSTALLED BELLFRAME REPAIR PER SRM 53-10-4 FIG 1.Mar 26, 1996 · N103FE · Boeing 72722C · Fuselage Main, FrameSDR 96FDEA00712Bellframe · crackedAFT CARGO COMP FS 1090 BELLFRAME CRACKED IN FLANGE AND INTO WEB IN AREA BETWEEN STR 26 AND 27L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-40-3.Mar 25, 1996 · N103FE · Boeing 72722C · Fuselage Main, FrameSDR UPS96205756Batteries · dischargedMAINTENANCE REPORTED, EMERGENCY EXIT LIGHT OVER COCKPIT DOOR DIM. REPLACED BOTH BATTERIES. RELAMPED, TEST NORMAL PER MM 33-50-101.Mar 22, 1996 · N942UP · Boeing 72722C · Emergency LightingSDR 96FDEA00711Bulkhead · crackedAFT CARGO COMPARTMENT FS 1183 BULKHEAD IS CRACKED BL 30 RT, 10 ABOVE STR 26L COMING OUT BEHIND HORIZ STIFFENER. CRACKED AREA OF BULKHEAD REMOVED AND FILLER AND DOUBLER INSTALLED PER BOEING SB 727-53-0215.Mar 20, 1996 · N103FE · Boeing 72722C · Fuselage Main, BulkheadSDR 96FDEA00710Skin Lap · corrosionUPPER LOBE, CORROSION IN SKIN LAP FS 420 TO 440 BETWEEN STR 5 TO 6L. CORROSION REMOVED PER SRM 51-10-6, REPAIR INSTALLED PER SRM 51-40-2 PAGES 1 TO 6.Mar 19, 1996 · N130FE · Boeing 72722C · Fuselage Main, Plate/SkinSDR 96FDEA00709Floor Beam · corrosionUPPER LOBE SLAT BS 344 FLOOR BEAM HAS CORROSION FROM RBL 2 TO LBL 54. REMOVED CORRODED BEAM CAP OF FLOOR BEAM AND INSTALLED NEW REPAIR PER SRM 53-10-8.Mar 19, 1996 · N103FE · Boeing 72722C · Fuselage Main, Floor BeamSDR CKSA96023Hydraulic Line · crackedONT - TOTAL LOSS OF 'A' HYDRAULIC SYSTEM IN FLIGHT. REMOVED AND REPLACED LINE. OPS CHECK GOOD ON GROUND. BLED SYSTEM, LEAK CHECKED, OPS CHECKED GOOD. (M)Mar 14, 1996 · N727CK · Boeing 72722C · Hydraulic System, MainSDR 96ZZZM693Hyd Line · crackedTOTAL LOSS OF 'A' HYDRAULIC SYSTEM IN FLIGHT. REMOVED AND REPLACED LINE, TRANSFERRED TO CARRYOVER NR 032 IAW EA 94-192. SERVICED HYD SYSTEM IAW MM 29-00-06. OPS CHECK GOOD ON GROUND HARD LINE. REPLACED WITH FLEX LINE WHICH IS REASON FOR C/O 4032.Mar 14, 1996 · N727CK · Boeing 72722C · Hydraulic System, MainSDR DHL96706003Air Data Comp · malfunctionedBOTH TRANSPONDERS FAILED THROUGH 6,000 FEET. CYCLED TRANSPONDERS, PULLED AND RESET C/B. REMOVED AND REPLACED AIR DATA COMPUTER FOR NO ALT REPORTING. REMOVED AND REPLACED NR 2 ATC DUE TO WEAK REPLY AND LEAK CHECKED PER 34-11-0.Mar 10, 1996 · N706DH · Boeing 72722C · Air Data ComputerSDR RAAAB196007Bulkhead · crackedDURING SCHEDULED C-CHECK INSPECTION OF NLG WHEEL WELL, FOUND LEFT PRESSURE BULKHEAD CRACKED AT BS 259. REPAIRED PER SRM 51-4-2. (M)Mar 8, 1996 · N831RV · Boeing 72722C · Fuselage Main, BulkheadSDR RAAAB196006Skin · crackedDURING SCHEDULED C-CHECK INSPECTION OF FWD FUSELAGE, FOUND CRACK IN SKIN AT LEFT FORWARD NLG DOOR HINGE CUTOUT. REPAIRED PER SRM 53-30-3 FIG 3A, SHEET 1. (M)Mar 8, 1996 · N831RV · Boeing 72722C · Fuselage Main, Plate/SkinSDR RAAAB196005Shear Tie · crackedDURING SCHEDULED C-CHECK INSPECTION OF MCD LOWER SILL, FOUND FOLLOWING FRAME SHEAR TIES CRACKED, BS 580, BS 560, BS 540, BS 500. REPAIRED PER SRM 53-10-4, PG 54-57, FIG 14 SHEET 1. (M)Mar 8, 1996 · N831RV · Boeing 72722C · Fuselage Miscellaneous StructureSDR RAAAB196004Web · crackedDURING SCHEDULED C-CHECK INSPECTION OF MCD SILL, FOUND WEB CRACKED AND CORRODED AT THE FOLLOWING, BS 487, 499-506, 537-548, 552-562, 577-587, 597-607 AND 610-617. REPLACED WEB PER SRM 51-10-1. (M)Mar 8, 1996 · N831RV · Boeing 72722C · Fuselage Miscellaneous Structure
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