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 UPS02238725Bracket · crackedINSPECTION TYPE:C+SI DUCT WEB BRACKET CRACKED BS 1090 LBL 45.5. DUCT WEB BRACKET REPLACED IAW SRM 51-20-1, 51-10-02 AND 51-30-02.Jun 18, 2002 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS02238838Spar · crackedINSPECTION TYPE:C+SI HORIZONTAL STAB RT SIDE FRONT SPAR LOWER CHORD IS CRACKED AT STAB STA 60.28. FRONT SPAR WEB SECTION CUT FROM ST 82.16 AND 44.6 IAW SRM 51-10-0, DAMAGED SECTION OF CHORD REMOVED IAW SRM 51-10-01, REPAIR PARTS FABRICATED IAW BOEING TELEX SRJun 17, 2002 · N942UP · Boeing 72722C · Horizontal Stabilizer, Spar/RibSDR UPS02238763Tie · crackedINSPECTION TYPE:C+SI STRINGER TIE CRACKED BS 950 STR 6L. STRINGER TIE REPLACED IAW SRM 51-30-02.Jun 17, 2002 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS02238839Floor Support · corrodedINSPECTION TYPE:C+SI CORROSION FOUND ON FLOOR SUPPORT STRUCTURE AT BS 343 RBL 15. TOILET PARTITION REMOVED FOR ACCESS IAW MM25-40-00, CORROSION REMOVE D IAW SRM 51-10-6 , FOUND OUTSIDE LIMITS IAW SRM 53-10-1, PARTS FABV RICATED IAW DWG 65-26173. INSTALLED Jun 15, 2002 · N942UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS02238832Sill · corrodedINSPECTION TYPE:C+SI LT SLIDING WINDOW SILL CHORD CORRODED BETWEEN BS236 AND 244L. REMOVED SLIDING WINDOW IAW 56-12-11, REMOVED CHORD IAW DWG 5-71775 A ND SRM 51-30-02, NEW CHORD FABRICATED IAW SRM 51-20-1 FIG 7, CHORD INSTALLED IAW DWG 5-71775 AND SRM 51-30-Jun 15, 2002 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS02238811Bracket · crackedINSPECTION TYPE:C+SI AFT CARGO DOOR HAS SUSPECT CRACKS AT FWD END AFT HINGE ATTACH POINTS FRAME ANGLES. CRACKED BRACKETS REMOVED IAW SRM 51-30-2, TWO NEW BRACKETS FABRICATED IAW SRM 51-20-1 F7. TWO NEW BRACKETS INSTALLED IAW DWG NR 65-18625 AND SRM 51-30-2.Jun 15, 2002 · N942UP · Boeing 72722C · Cargo/Baggage DoorsSDR UPS02238745Hinge Fitting · crackedINSPECTION TYPE:C+SI SUSPECT CRACKS ON FWD.(FRAME)LWR. HINGE CUTOUT FITTING(MID GALLEY DO OR) REMOVED FITTING IAW SRM 51-30-2. INSTALLED NEW FITTING IAW DRG.65-16722.Jun 15, 2002 · N942UP · Boeing 72722C · Fixed Inner DoorsSDR UPS02238729Bracket · crackedINSPECTION TYPE:C+SI BRACKET CRACKED AT RIVET HOLE(UPP FASTENER) AT I/B LEG OF FRAME BS72 0" STR 17R 4" ABOVE FLOOR LEVEL. BRACKET REPAIRED IAW SRM 51-40-3 FIG 1.Jun 15, 2002 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS02238723Stringer · corrodedINSPECTION TYPE:C+SI INTERGRANULAR CORROSION S19L BS 460-440, CORROSION FOUND TO BE OUTSIDE LIMITS OF SRM 51-10-1. STRINGER REPAIR ED IAW SRM 53-10-3.Jun 15, 2002 · N942UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02238719Stringer · corrodedINSPECTION TYPE:C+SI SURFACE CORROSION STRINGER 21R BS 448 APPROX SURFACE CORROSION FOUND TO BE OUTSIDE LIMITS I.A.W SRM 53-10-1. STRINGER 21 R REPAIRED I.A.W SRM 53-10-3 FIG1.Jun 15, 2002 · N942UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02238842Casting · crackedINSPECTION TYPE:C+SI NR 12 SPOILER SUPPORT CASTING O/B ATTACH ANGLE LWR HOLE HAS CRACK INDICATION. SUPPORT CASTING REPLACED IAW SRM 51-30-02Jun 14, 2002 · N942UP · Boeing 72722C · SpoilersSDR UPS02238809Support Fitting · corrodedINSPECTION TYPE:C+SI R/H MLG WING DOOR ACTUATOR SUPPORT FITTING CRACKED. FITTING REPLACED IAW EO B727-3210-2583 APP D,E,F,G.Jun 14, 2002 · N942UP · Boeing 72722C · Main Landing GearSDR UPS02238808Support Fitting · corrodedINSPECTION TYPE:C+SI LT WING LANDING GEAR DOOR ACTUATOR SUPPORT FITTING HAS EVIDENCE OF CORROSION. CORROSION FOUND TO BE OUT OF LIMITS, OLD FITTING WAS REMOVED AND NEW FITTING INSTALLED IAW UPS EO B727-3210-2583 APP D,E,F,G.Jun 14, 2002 · N942UP · Boeing 72722C · Landing Gear Door ActuatorSDR UPS02238800Floorbeam · corrodedINSPECTION TYPE:C+SI CORROSION ON FLOORBEAM AT BS 480 AT RBL 27.39. CORRODED FLANGES CUTOUT AT STA 480 RBL 27-31 AS CORROSION NOT ALLOWED AND AT RBL 35-39 IAW SRM 53-10-8. FLOORBEAM REPAIR IAW SRM 53-10-8 FIGURE 5.Jun 14, 2002 · N942UP · Boeing 72722C · Fuselage Main, Floor BeamSDR UPS02238799Skin · corrodedINSPECTION TYPE:C+SI SUSPECT CORROSION BETWEEN SKIN AND DOUBLER AT BS 1080 TO BS 1110 STR 11RT TO STR 13 RT. AREA OPENED UP IAW SRM 51-10-1, FOUND CORROSION BS1080-1100 AND AROUND SKIN CUTOUT TOP AFT CORNER WINDOW AT BS 1090 BETWEEN STRINGERS 11 AND 13 RT. FJun 14, 2002 · N942UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS02238765Angle · corrodedINSPECTION TYPE:C+SI CORROSION ON FAIRING SUPPORT ANGLE BS 760 AIR CONDITIONING BAY AT LBL 10 AND RBL 10. ANGLE SECTION REPLACED IAW SRM 51-30-02.Jun 14, 2002 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS02238744Angle · corrodedINSPECTION TYPE:C+SI INTERGRANULAR CORROSION ON FRAME ANGLE BS 328 AT ATTACH POINT TO S22R. FRAME ANGLE REPLACED IAW SRM 51-40-3 FIG 1 FROM BELOW S21R TO BETWEEN S22R AND S23R.Jun 14, 2002 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS02238742Door Frame · crackedINSPECTION TYPE:C+SI CRACK ON FRAME BS 540 AT CARGO DOOR FITTING. CRACKED LUG OF BS 540 FRAME AT MCD LATCH SUPPORT FITTING CUT AWAY IAW SRM 51-40-3. REPAIR PARTS FABRICATED IAW SRM 51-40-3. PARTS INSTALLED IAW SRM 51-30-02 AND SRM 51-40-3.Jun 14, 2002 · N942UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02238740Rib · crackedINSPECTION TYPE:C+SI INSPECT REMOVED STAB.RIBS. FOR CRACKS AND FORWARD FINDING TO ENGINEE RING(RETAIN CRACKED RIBS) DVI INSPECTION PERFORMED IAW CUSTOMER REQUEST :CRACKS NOTED @ L/H RI BS 17:20 AND 136:50 AND R/H RIBS 17:20 AND 66:50 AND 99:79.Jun 14, 2002 · N942UP · Boeing 72722C · Horizontal Stabilizer StructureSDR UPS02238721Stringer · crackedINSPECTION TYPE:C+SI CRACK ON STRINGER FLANGE S21R BS 580-BS600. UPON FURTHER INVESTIGATION STRINGER CRACKED DUE TO CORROSION. CORRODED SECTION CUT AWAY AND STRINGER REPAIRED IAW SRM 53-10-3 FIG 1Jun 14, 2002 · N942UP · Boeing 72722C · Fuselage Main, Longeron/StringerSDR UPS02238805Door Frame · crackedINSPECTION TYPE:C+SI 1 INCH CRACK FOUND ON FWD DOOR AFT FRAME AT LOWER LATCH ROLLER TORQUE SHAFT CUTOUT. CRACKING STOP DRILLED PREVIOUSLY. DOOR FRAME REPAIRED IAW BOEING INSTRUCTION SRV-SNN-02-00135H 00100H.Jun 13, 2002 · N942UP · Boeing 72722C · Passenger/Crew DoorsSDR UPS02238766Flap Track · corrodedINSPECTION TYPE:C+SI PITTING CORROSION IN BORE OF HOLES F+G ON NO3 FLAP TRACK TRACK REPLACED REF NRC 541795 FOR REPLACMENT DETAILS.Jun 13, 2002 · N942UP · Boeing 72722C · Wing, Control SurfacesSDR UPS02238764Casting · corrodedINSPECTION TYPE:C+SI #6 SPOILER CENTRE HINGE SUPPORT CASTING O/B FACE OF I/B HINGE LUG HA S EVIDENCE OF CORROSION. CORROSION REMOVED IAW SRM 51-10-06 AND FOUND OUT OF LIMITS IAW SRM 5 1-10-01. HINGE CASTING REPLACED IAW DWG 65-16216Jun 13, 2002 · N942UP · Boeing 72722C · Wing Miscellaneous StructureSDR UPS02238760Web · crackedINSPECTION TYPE:C+SI CRACK TO WEB AT BS 1182 LBL54 APPROX AT ACCESS HOLE FOR PIPE WORK WEB REPLACED IAW SRM 51-20-1 FIG7 AND SRM 51-30-2Jun 13, 2002 · N942UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02238728Angle · crackedINSPECTION TYPE:C+SI ANGLE CRACKED AT BS1180 RBL 30 APPROX IN LWR AFT CARGO BAY. CRACKED ANGLE REMOVED IAW SRM 51-30-2 NEW ANGLE FAB. IAW SRM 51-20-1 FIG7 AND SRM 53-10-2 FIG 5 NEW ANGLE INSTALLED IAW SRM 51-30-2.Jun 13, 2002 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS02238722Mount · corrodedINSPECTION TYPE:C+SI NR 3 ENG, FWD MOUNT FITTING HAS PITTING CORROSION IN BOLT HOLES. REPAIR CARRIED OUT IAW EOB727-5440-11592 APPENDIX B.Jun 13, 2002 · N942UP · Boeing 72722C · Engine Cowling SystemSDR UPS02238841Pin · corrodedINSPECTION TYPE:C+SI CORROSION ON RT WING FRONT SPAR BOTTLE PIN HEAD AFT FLANGE. BOTTLE PIN REPLACED IAW MM57-41-01.Jun 12, 2002 · N942UP · Boeing 72722C · Wing, Attach FittingsSDR UPS02238825Keelbeam · crackedINSPECTION TYPE:C+SI CRACK FOUND ON KEELBEAM WEB FWD OF APU CUTOUT IN RIGHT HAND WHEEL WELL. KEEL BEAM REPAIRED IAW SRM ADDENDUM EO B727-5330-1995.Jun 12, 2002 · N942UP · Boeing 72722C · Fuselage Main, KeelSDR UPS02238801Cap · corrodedINSPECTION TYPE:C+SI NOSE LANDING GEAR LT TRUNNION CAPS CORRODED. TRUNNION CAPS REWORKED IAW SRM 53-40-01. FLUORESCENT PENETRANT INSPECTION COMPLIED WITH NDF. NEW BEARINGS FABRICATED IAW SOPM AND OHM.Jun 12, 2002 · N942UP · Boeing 72722C · Nose/Tail Landing GearSDR UPS02238787Frame · corrodedINSPECTION TYPE:C+SI INTERGRANULAR CORROSION ON FRAME WEB BS 218 LBL24 FASTENERS REMOVED, CORRODED SECTION OF FRAME WEB CUT OUT IAW 51-40-2 FIG1. PARTS FABRICATE, FRAME REPAIRED IAW SRM 51-40-2 FIGURE 1.Jun 12, 2002 · N942UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02238761Bracket · crackedINSPECTION TYPE:C+SI CRACK ON SUPPORT ANGLE AT BS 178 BULKHEAD RBL24 SUPPORT BRAKET REPLACED IAW SRM 53-10-2 FIG1 ABD SRM 51-20-1 FIG 7 A ND SRM 51-30-2.Jun 12, 2002 · N942UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02238759Carriage · corrodedINSPECTION TYPE:C+SI FLAP CARRIAGE NR 7 HAS SUSPECT CORROSION INSIDE SPINDLE BORE. FLAP CARRIAGE REPLACED AS CORROSION OUTSIDE LIMITS.Jun 12, 2002 · N942UP · Boeing 72722C · Trailing Edge FlapsSDR UPS02238741Carriage · corrodedINSPECTION TYPE:C+SI FLAP CARRIAGE NR 2 HAS SUSPECT CORROSION INSIDE SPINDLE BORE. CORROSION FOUND TO BE OUTSIDE LIMITS IAW OHM 57-58-01. REPLACED FLAP CARRIAGE IAW MM 27-51-13.Jun 12, 2002 · N942UP · Boeing 72722C · Trailing Edge FlapsSDR UPS02238738Carriage · corrodedINSPECTION TYPE:C+SI FLAP CARRIAGE NR 8 HAS SUSPECT CORROSION INSIDE SPINDLE BORE HOLE. CORROSION FOUND TO BE OUTSIDE LIMITS IAW OHM 57-58-01. REPLACED FLAP CARRIAGE IAW MM 27-51-13.Jun 12, 2002 · N942UP · Boeing 72722C · Trailing Edge FlapsSDR UPS02238727Hinge · corrodedINSPECTION TYPE:C+SI FOUND ON #5 BALANCE PANEL(LH ELEV) 1.LIGHT SURFACE CORROSION ON AFT HINGE ASSY. 2.LIGHT SURFACE CORROSION WHERE AFT HINGE MATES WITH BAL ANCE PANEL. UPON INVESTIGATION FOUND HALF OF AFT HINGE ASSY CORRODED BEYOND LIMI TS IAW SRM 51-80-Jun 12, 2002 · N942UP · Boeing 72722C · Elevator Control SystemSDR UPS02238718Intercostal · corrodedINSPECTION TYPE:C+SI SURFACE CORROSION ON INTERCOSTAL BETWEEN BS219+BS211 LBL 24 L/H. INTERCOSTAL FABRICATED IAW SRM 51-20-1 INTERCOSTAL INSTALLED IAW SRM 53-30-2Jun 12, 2002 · N942UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02238845Clevis · crackedINSPECTION TYPE:C+SI CORROSION AT RT BS 870 FRAME SPLICE ON WW WALL WBL 60 APPROX. CORROSION LOCATED ON HORIZONTAL CLEVIS FLANGES, CRACKS ALSO LOCATED. CORROSION AND CRACKS BEYOND LIMITS. 870 RT CLEVIS REPAIRED IAW SB 727-53-0077 R2 AND BOEING INSTRUCTIONS SJun 11, 2002 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS02238810Butt Joint · corrodedINSPECTION TYPE:C+SI LFEC INSPECTION INDICATES MATERIAL LOSS AT BS 1080 BETWEEN S4L AND 6 L AREA REPAIRED IAW UPS ENGINEERING ORDER B727-5330-1177 APPEDIX 7.BET WEEN STRINGER 5L AND 6L AT BS 1080. BUTT JOINT RESEALED AND FASTENED IAW SRM 51-30-02.Jun 11, 2002 · N942UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02238846Frame · corrodedINSPECTION TYPE:C+SI NOSE LANDING GEAR BAY, EVIDENCE OF CORROSION IN TORQUE BOX AREA. ARE A JUST AFT OF LT FWD NLG DOOR AT BS 288 LT. CORROSION REMOVED AND FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-1. OLD CHORD REMOVED IAW SRM 51-30-2 AND NEW CHORD DRILLED OFJun 10, 2002 · N942UP · Boeing 72722C · Fuselage Main, FrameSDR UPS02238814Skin · corrodedINSPECTION TYPE:C+SI SUSPECT MATERIAL LOSS ON CROWN SKIN AT BS 500 TO 519 BETWEEN STRINGE R 1 L TO STRINGER 3L SKIN DERIVETED BETWEEN BS441 AND 521 S2L TO 10L IAW SRM 51-10-2, COR ROSION FOUND OUT OF LIMITS, SKIN CUT BETWEEN BS441 BS521 BETWEEN S1L AND S2Jun 10, 2002 · N942UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS02238803Lap Joint · corrodedINSPECTION TYPE:C+SI SUSPECT CORROSION AT LAP JOINT BS 490 TO 470 AT S19R/H LFEC INDICATES MATERIAL LOSS 15-20% BS 498-465 AT STR 19R.CORROSION REMOVED FROM LAP JOINT AT BS470-480, FOUND WITHIN LIMITS AND LAP CLO SED IAW SRM 51-40-5 AND 51-30-2. AREA BETWEJun 10, 2002 · N942UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS02238802Casting · corrodedINSPECTION TYPE:C+SI NLG FWD WHEEL WELL BS 227, BULKHEAD FITTING FOR NLG DOOR OPERATION CORRODED AT OUTBOARD UPPER SURFACE, ATTACHES TO RADIUS ROD. CASTING REMOVED IAW SRM 51-30-02, NEW CASTING INSTALLED IAW DWG 65-1 6306 AND SRM 51-30-02.Jun 10, 2002 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS02238779Skin · crackedINSPECTION TYPE:C+SI SUSPECT CRACK IN FUSELAGE SKIN FROM FASTENER HOLE AT FWD UPPER CORNER OF FWD ENTRY DOOR CUT OUT. HEFC INSP CARRIED OUT IAW NDT MANUAL PT 6 51-00-00 FIG 4, CRACK CONFIRMED AND MEASURED AS 5MM IN LENGTH. REPAIR CARRIED OUT IAW UPS EO B727-Jun 10, 2002 · N942UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS02238720Torque Box · crackedINSPECTION TYPE:C+SI CRACK IN TORQUE BOX OF FWD ENTRY DOOR WHERE LATCH ROD GOES THROUGH T-BOX. REPAIRED IAW SMRO EO2002-035-001 UPS ENG FILE NR 727-52-20010.Jun 10, 2002 · N942UP · Boeing 72722C · Passenger/Crew DoorsSDR UPS02238807Gate · crackedINSPECTION TYPE:C+SI FWD ENTRY DOOR GATE STOP LUG CRACKED ON UPPER GATE. GATE REMOVED IAW MM 52-11-01, GATE REPLACED IAW MM52-11-01 AND SRM 51-30-2.Jun 7, 2002 · N942UP · Boeing 72722C · Passenger/Crew DoorsSDR UPS02238726Web · crackedINSPECTION TYPE:C+SI FWD CARGO DOOR AFT LWR.STOP ON FUSELAGE HAS A CRACKED SUPPORT WEB. WEB REMOVED IAW SRM 51-30-02. NEW WEB FABRICATED IAW SRM 53-10-2 FIG.3 AND SRM 51-20-1 FIG 7. WEB INSTALLED IAW SRM 51-30-02.Jun 7, 2002 · N942UP · Boeing 72722C · Cargo/Baggage DoorsSDR UPS02238317Intercostal · corrodedINSPECTION TYPE:C CORROAION ON INTERCOSTAL FROM BS 294.5 - BS 312 AT LBBL 40 APPROX INTERCOSTAL REPAIRED IAW SRM 51-40-3May 10, 2002 · N943UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02238306Flap Track · crackedINSPECTION TYPE:C RH WING #8 FLAP TRACK SAILBOAT FAIRING, O/B ROLLER GUIDE TRACK IS CR ACKED #8 FLAP TRACK FAIRING TRACK GUIDE REPLACED IAW SRM 51-30-02May 9, 2002 · N943UP · Boeing 72722C · Trailing Edge Flap Control SystemSDR UPS02238319Skin · crackedINSPECTION TYPE:C SUSPECT CRACK ON RH WING LE SKIN AT CUT OUT FOR NO 6 LE SLAT O/B SLA T HOOK REPAIR CARRIED OUT IAW 57-30-4 SRMMay 8, 2002 · N943UP · Boeing 72722C · Wing StructureSDR UPS02238314Bracket · crackedINSPECTION TYPE:C, SUSPECT CRACKS ON NR 6 L/E FLAP ACTUATOR I/B & O/B ATTACH BRACKETS LWR FWD CORNERS. ATTACH BRACKETS FABRICATED IAW SRM 51-20-1 FIG 7, HEAT TREATMENT REF HT 02-27-03. BRACKETS INSTALLED IAW SRM 51-30-2 & DRAWING 65-16275.May 8, 2002 · N943UP · Boeing 72722C · Leading Edge Slat Actuator
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