Boeing 727-22C

Service difficulty reports · 2,328

Newest first. General aviation reporting is voluntary.

Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS04242981Skin · delaminatedINSPECTION TYPE: C, UPPER RUDDER TAB HAS DELAMINATION AT LWR LT SIDE UPPER RUDDER REPLACED IAW MM 27-20-11.Jul 29, 2004 · N945UP · Boeing 72722C · Rudder, Tab StructureSDR UPS04242973Fairing · delaminatedINSPECTION TYPE:C, VERTICAL STAB TIP FAIRING (TAIL CONE) DELAMINATED AT BOTTOM NEAR WEDGE. REPAIR CARRIED OUT IAW SRM 51-40-9 & 51-30-2.Jul 29, 2004 · N945UP · Boeing 72722C · Aerodynamic FairingsSDR UPS04242968Angle · crackedINSPECTION TYPE: C, ON REMOVAL OF RIGHT CONTROL COLUMN, CRACK FOUND ON SUPPORT ANGLE AT I/B SIDE OF COLUMN CUTOUT IN FLOOR, COMING FROM ANCHOR NUT HOLE. REPAIR CARRIED OUT IAW SRM 51-40-4 & 51-30-2.Jul 26, 2004 · N945UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04242996Skin · crackedINSPECTION TYPE: C, 0.5 INCH CRACK IN LOWER WING SKIN AT LEFT WING TIP, APPROX 8 INCHES FROM TIP AND JUST FWD OF STRINGER FAIRING. CRACK STOP DRILLED IAW SRM 51-10-1. CRACK CONTAINED WITHIN DRILLED AREA. HOLE DRILLED IN RIB COMMON TO REPAIR SCHEME FOR NDT. Jul 9, 2004 · N945UP · Boeing 72722C · Wing, Plate/SkinSDR UPS04243015Window Frame · crackedINSPECTION TYPE: C, REPLACE LT WINDOW FRAME AT BS 1100 P/N:65-19850-149. FRAME REPLACED WITH NEW FRAME IAW SRM 51-30-2.Jul 7, 2004 · N945UP · Boeing 72722C · Fuselage Main, StructureSDR UPS04242321Support · crackedINSPECTION TYPE:C CRACK ON SUPPORT STRUCTURE IN NWW RT FWD AREA. SUPPORT STRUCTURE REMOVED REF NRC NR 748078, SUPPORT STRUCTURE FABRICATE D IAW SRM 51-20-1, SUPPORT STRUCTURE INSTALLED IAW SRM 51-30-02.Apr 27, 2004 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04242344Frame · crackedINSPECTION TYPE: C, VERT STAB JACKSCREW CUTOUT LT, FWD FRAME CRACKED AT FW STA 128 APPROX. CRACKED FRAME REMOVED IAW SRM 51-30-02. NEW FRAME INSTALLED IAW SRM 51-30-02Apr 26, 2004 · N930UP · Boeing 72722C · Vertical StabilizerSDR UPS04242316Pulley Bracket · crackedINSPECTION TYPE:C SUSPECT CRACKS ON RUDDER TRIM CABLE PULLEY BRACKET IN AIRSTAIRS AREA BS 1203 RT HFEC C/W, DERIVETED BRACKET, FAB BRACKET IAW SRM 51-20-01, BRACKET INSTALLED.Apr 26, 2004 · N930UP · Boeing 72722C · Rudder Control SystemSDR UPS04242343Skin · crackedINSPECTION TYPE: C, ENGINE NR 1 THRUST REV. UPPER DOOR INNER RAMP SKIN CRACKED. DYE PENETRANT INSP. CARRIED OUT ON THE ABOVE AREA IAW MIL-STD-6866. CRACKS FOUND AND ENDS MARKED. STOP DRILLED CRACKS IAW MM 78-30-01. DYE PENETRANT INSP. CARRIED OUT AROUND STOApr 24, 2004 · N930UP · Boeing 72722C · Engine Thrust ReverserSDR UPS04242341Skin · chafedINSPECTION TYPE:C CHAFING UNDER FAIRING AT BS1050 AND BS1070 JUST BELOW STR26L. AT BS1050 DAMAGE REMOVED AND FOUND TO BE WITHIN LIMITS IAW SRM 53-30-1. AREA REPROTECTED IAW SRM51-10-02. AT BS1070 DAMAGE OUT OF LIMITS IAW SRM 53-30-1. REPAIR CARRIED OUT IAWApr 16, 2004 · N930UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS04242358Rib · crackedINSPECTION TYPE: C, MID GALLEY DOOR UPPER GATE HINGE RIB CRACKED AT FWD CORNER. HINGE RIB REPLACED IAW DWG 65-16720 AND SRM 51-30-02Apr 15, 2004 · N930UP · Boeing 72722C · Service DoorsSDR UPS04242356Retainer · corrodedINSPECTION TYPE: C, SEAL RETAINER ON NWW CUTOUT FWD LHS CORRODED SEAL RETAINER REPLACED IAW SRM 51-20-01 AND AMM 20-80-01Apr 15, 2004 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04242342Cargo Track · corrodedINSPECTION TYPE: C, SECTION OF TIE DOWN RAIL IS CORRODED FROM BS530 TO BS480 IN LOWER FWD CARGO COMPARTMENT. CORRODED SECTION OF TIE DOWN RAIL REMOVED IAW SRM 51-30-2. TIE DOWN RAIL FABRICATED IAW DRG. NO.:66-01573 INSTALLED NEW TIE DOWN RAIL IAW SRM 51-30-2Apr 15, 2004 · N930UP · Boeing 72722C · Fuselage, Seat/Cargo Attach FittingsSDR UPS04242355Retainer · corrodedINSPECTION TYPE: C, FWD RT SEAT RETAINER ON NLG WW CUTOUT CORRODED SEAL RETAINER REMOVED, SEAL RETAINER FABRICATED IAW SRM 51-20-1, SEAL RETAINER INSTALLED MM 20-80-01Apr 14, 2004 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04242320Pressure Panel · crackedINSPECTION TYPE:C AIR LEAK FROM CRACK ON NWW WEB LHS BS 287. PAINT STRIPPED, HFEC INSPECTION C/O CRACKS CONFIRMED, CRACKED AREA CUT OUT, HFEC C/O AROUND CUT OUT AREA NDF, REMOVED SUPPORT STRUCTURE TO GAIN ACCESS, FABRICATED REPAIR PARTS, INSTALLED FABRICATED Apr 14, 2004 · N930UP · Boeing 72722C · Fuselage Main, BulkheadSDR UPS04242318Doubler · corrodedINSPECTION TYPE:C OLD REPAIR DOUBLER HAS SIGNS OF INTERGRANULAR CORROSION IN LOWER NOSE COMPT, DOUBLER LOCATED ON VERTICAL INTERNAL STRUCTURE OF NWW RBL 14.6 B STA 314. REMOVED OLD REPAIR. HFEC CW NDF. NEW DOUBLER INSTALLED IAW SRM 51-10-02 AND 51-30-02.Apr 14, 2004 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04242357Web · crackedINSPECTION TYPE: C, 5 FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB CRACKED. K FLAP ACTUATOR REMOVED, TRUNNION SUPPORT BOX I/B WEB REMOVED. WEB FABRICATED IAW DWG 65-16263. NEW K FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB FITTED IAW SRM 51-30-02Apr 13, 2004 · N930UP · Boeing 72722C · Leading Edge DevicesSDR CA040325002Actuator · leaking(CAN) ON APPROACH INTO CYVR SELECTED FLAPS 2, AMBER IN-TRANSIT LIGHT STAYED ON. NR 7 SLAT DID NOT EXTEND. HYDRAULIC SYSTEM (A) LOW PRESSURE LIGHTS ILLUMINATED AND HYDRAULIC (A) SYSTEM QUANTITY INDICATED ZERO QUANTITY. AIRCRAFT WAS VECTORED AND CREW PERFORMED HMar 25, 2004 · Boeing 72722C · Leading Edge Slat ActuatorSDR UPS04241972Bracket · crackedINSPECTION TYPE: C, BROKEN BRACKET AT BS 1223 LBL 36 AFT AIRSTAIRS EQUIP AREA. REMOVED BROKEN BRACKET IAW OHM 20-50-01. BRACKET FABRICATED IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-30-02.Feb 23, 2004 · N941UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04241974Yoke · corrodedINSPECTION TYPE: C, ON REMOVAL & BREAKDOWN OF LT SWING LINK, YOKE ASSY FOUND TO BE CORRODED. REPLACED SWING YOKE SUPPORT LT MLG SWING LINK IAW MM 57-15-01.Feb 17, 2004 · N941UP · Boeing 72722C · Main Landing GearSDR UPS04241973Flap Track · crackedINSPECTION TYPE: C, NR 7 FLAP TRACK FAIRING I/B TRACK CRACKED. REPLACED TRACK IAW DRW 65-21796 & SRM 51-30-02.Feb 13, 2004 · N941UP · Boeing 72722C · Trailing Edge FlapsSDR UPS04241991Skin · crackedINSPECTION TYPE: C, X-RAY INSPECTION OF RT ELEVATOR SHOWS 2 CRACK INDICATIONS ON BEADED SKIN, PREVIOUSLY STOP DRILLED ON PANEL ELEV STA 136.5 TO 173.21. HFEC CARRIED OUT. CRACKS CONTAINED WITHIN STOP DRILLED HOLES. REPAIR DOUBLERS FABRICATED IAW SRM 55-20-Feb 12, 2004 · N941UP · Boeing 72722C · Elevator StructureSDR UPS04241978Bracket · crackedINSPECTION TYPE: C, ENGINE NR 1 THRUST REV O/B FAIRING MID SUPPORT BRACKET IS CRACKED. ENGINE NR 1 TR O/B FAIRING MID SUPPORT BRACKET REPLACED IAW MM 78-30-00.Feb 12, 2004 · N941UP · Boeing 72722C · Engine Thrust ReverserSDR UPS04241976Seat Track · corrodedINSPECTION TYPE:C, CORROSION ON SEAT TRACK AT BEARSTRAP LOCK PIN LOCATION, BS 950 RBL 4 5.5. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5. REPAIR CARRIED OUT IAW SRM EO 2004-017-001 UPS ENGINEERING FILE 727-53-20136.Feb 12, 2004 · N941UP · Boeing 72722C · Fuselage, Seat/Cargo Attach FittingsSDR UPS04241971Skin · crackedINSPECTION TYPE: C, X-RAY INSPECTION OF RIGHT ELEVATOR SHOWS 2 CRACK INDICATIONS ON BEADED SKIN, PREVIOUSLY STOP DRILLED ON PANEL ELEVATOR STA 136.5 TO 173.21. REPAIR CARRIED OUT IAW SRM 51-30-02, 55-20-3, 51-40-5, 55-20-3, 51-30 -026, 51-10-02 & DRG 65-2563Feb 12, 2004 · N941UP · Boeing 72722C · Elevator, Plate/SkinSDR UPS04241969Web · crackedINSPECTION TYPE: C, NR 1 KRUEGER FLAP ACTUATOR TRUNNION CAP SUPPORT WEB I/B & O/B CRACKED. NR 1 K-FLAP ACTUATOR REMOVED PER MM 27-81-22. FABRICATED TRUNNION CAP SUPPORT WEB IAW SRM 51-20-1. INSTALLED 31 K-FLAP ACTUATOR TRUNNION SUPPORT CAP WEB PER BOEING DRFeb 12, 2004 · N941UP · Boeing 72722C · Leading Edge DevicesSDR UPS04241980Web · crackedINSPECTION TYPE: C, CRACKS ON NR 5 K-FLAP ACTUATOR I/B & O/B TRUNNION CAPS SUPPORT WEBS AT UPPER & LWR CORNERS. NR 5 K-FLAP ACTUATOR REMOVED PER MM 27-81-22. FABRICATED TRUNNION CAPS SUPPORT WEBS IAW SRM 51-20-1 & DRG 65-16269. INSTALLED TRUNNION CAPS SUPPOFeb 11, 2004 · N941UP · Boeing 72722C · Leading Edge DevicesSDR UPS04241979Fitting · crackedINSPECTION TYPE: C, LEFT UPPER TERMINAL FITTING IN TAIL SKID BAY CRACKED. LEFT UPPER TERMINAL FITTING IN TAIL SKID BAY REPLACED IAW DWG 65-2 5992.Feb 11, 2004 · N941UP · Boeing 72722C · Fuselage Main, Attach FittingsSDR UPS04241977Fitting · crackedINSPECTION TYPE:C, RIGHT LWR TERMINAL FITTING IN TAIL SKID BAY CRACKED. RIGHT LWR TERMINAL FITTING REPLACED IAW DWG 65-25992.Feb 11, 2004 · N941UP · Boeing 72722C · Fuselage Main, Attach FittingsSDR UPS04241968Skin · crackedINSPECTION TYPE: C, FUSELAGE SKIN CRACKED AT BS 1354 RT. REPAIRED IAW SRM 51-40-2 FIG 1.Feb 11, 2004 · N941UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS04241975Shock Absorber · crackedINSPECTION TYPE: C, TAIL SKID ABSORBER FOUND TO BE CRACKED. REPLACED TAIL SKIN ABSORBER IAW MM 32-71-41 & OHM 32-71-04.Feb 10, 2004 · N941UP · Boeing 72722C · Auxiliary Gear (Tail Skid)SDR UPS04241967Casting · corrodedINSPECTION TYPE: C, SURFACE CORROSION ON I/B RIGHT AILERON TAB HINGE BEARING SUPPORT CASTINGS (BOTH O/B AND MIDDLE CASTINGS). REMOVED I/B AILERON IAW MM 27-10-01. REPLACED CORRODED TAB HINGE SUPPORT CASTINGS IAW SRM 51-30-2. NO WEIGHT CHANGE OCCURRED TO AILFeb 10, 2004 · N941UP · Boeing 72722C · Aileron TabsSDR UPS04241985Fitting · crackedINSPECTION TYPE: C, SUSPECTED CRACK FOUND ON BS 940 FITTING LEFT ON FWD UPPER FLANGE. FITTING REPLACED IAW EO B727-5310-4501 AND DRW 65C15732.Feb 9, 2004 · N941UP · Boeing 72722C · Fuselage Main, Attach FittingsSDR UPS04241970Skin · crackedINSPECTION TYPE: C, SUSPECT CRACK INDICATION AT BS 243.7 WL 216.5. AREA PAINT STRIPPED IAW MM 51-20-01. HFEC INSPECTION CARRIED OUT AT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00. RESULT: CRACK CONFIRMED AND END MARKED. REPAIR CARRIED OUT IAW SRM 53-30-3 FFeb 9, 2004 · N941UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS04241937Skin · damagedINSPECTION TYPE:C PARTIAL REPLACEMENT OF SKIN LOCATED AT BS 360-390 S4L-4R. REPLACED IAW UPS AUTHORIZATION B727-5330-19967-A.Feb 6, 2004 · N942UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS04241932Rib · crackedINSPECTION TYPE:C ON REMOVAL OF PANEL 8855 FOUND NR 14 O/B SPOILER DOWN STOP RIB CRACKED AT WS 620.5. CRACKED RIB REPLACED IAW SRM 51-30-2 & SPOILER OPERATION WITH STOP TESTED SATISFACTORY IAW MM 27-61-00.Feb 4, 2004 · N942UP · Boeing 72722C · Wing, Rib/BulkheadSDR UPS04241875Bracket · crackedINSPECTION TYPE: C, BATTERY CHARGER FWD MOUNTING BRACKET CRACKED ON E3 RACK LOWER RT SIDE. REMOVED CRACKED BRACKET IAW SRM 51-30-02. FABRICATED NEW BRACKET IAW SRM 51-20-01. NEW BRACKET REPROTECTED IAW SRM 51-10-02, AND RE-INSTALLED IAW SRM 51-30-02.Feb 2, 2004 · N942UP · Boeing 72722C · Battery Box StructureSDR UPS04241872Bracket · damagedINSPECTION TYPE: C, LATCH FITTING ON W/BODY FAIRING BRACKET FOR AFT CARGO DOOR FAIRING LATCH IS DAMAGED. BRACKET REPLACED IAW SRM 51-20-01.Jan 30, 2004 · N942UP · Boeing 72722C · Aerodynamic FairingsSDR UPS04241876Bracket · corrodedINSPECTION TYPE: C, SUSPECT CORROSION WHERE 259.5 RT STIFFENER AND TOP LEFT HAND CORNER OF NWW TORQUE BOX MEET BRACKET. REMOVED IAW SRM 51-30-02. BRACKET FABRICATED IAW SRM 51-20-01. FASTENERS INSTALLED IAW SRM 51-30-2 & APPLIED SEALANT IAW SRM 51-20-04. BJan 25, 2004 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04241898Web · crackedINSPECTION TYPE: C, AFT STAIRWELL RT TORQUE BOX VERTICAL WEB HAS CRACKING BEYOND PREVIOUS REPAIR AT BS 1273. REPAIR CARRIED OUT IAW EO B727-5310-1239-E & MM 20-10-05.Jan 23, 2004 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04241873Hinge · crackedINSPECTION TYPE: C, LEFT WING GEAR DOOR AFT HINGE, INNER HINGE HALF CRACKED. REPLACED HINGE IAW SRM 51-30-02.Jan 23, 2004 · N942UP · Boeing 72722C · Landing Gear DoorsSDR UPS04241940Beam · corrodedINSPECTION TYPE:C PRESENCE OF INTERGRANULAR CORROSION FOUND ON VARIOUS HOLES AND THE LOWER I-BEAM AT BS 1110 RBL 31 AS MARKED. REPAIRED IAW UPS AUTHORIZATION B727-53-21034.Jan 22, 2004 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04241933Support Fitting · damagedINSPECTION TYPE:C REPAIR PLATES ON NR 3 SPOILER PCU SUPPORT FITTING, REAR SPAR ATTACH ANGLES DO NOT CONFORM TO REQUIREMENTS OF SRM REPAIR 51-40-4 FIG 1 OR S/B 57-84 R1 CRITERIA. REPAIR CARRIED OUT IAW DRAWING 65-16201 & MM 28-11-20 & 28-11-21.Jan 22, 2004 · N942UP · Boeing 72722C · SpoilersSDR UPS04241816Bracket · corrodedINSPECTION TYPE: C, INTERGRANULAR CORROSION FOUND ON CEILING PANEL BRACKET AT BS 1130 AFT CARGO COMPT, AS MARKED. HFEC INSPECTION CARRIED OUT AROUND CUTOUT AT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00 NDF. REPAIR CARRIED OUT IAW SRM 51-40-04.Jan 22, 2004 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04241939Fitting · crackedINSPECTION TYPE:C RIGHT MLG WHEEL WELL, EVIDENCE OF CORROSION ON BS 870 FITTING O/B FLANGE AREA ABOVE STR 18A. FITTING REPLACED IAW DWG65C23231 AND 2BOF65-72710 AND UPS EO B727-5310-3056G.Jan 21, 2004 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04241874Solenoid Valve · stickingINSPECTION TYPE: C, ENGINE NR 1 FIRE EXTINGUISHING SOLENOID STICKS DURING OPERATION. ENGINE NR 1 FIRE SOLENOID VALVE REPLACED IAW MM 26-21-21. TEST AND FOUND SATISFACTORY IAW MM 21-21-00.Jan 21, 2004 · N942UP · Boeing 72722C · Fire Bottle, FixedSDR UPS04241775Regulator · inoperativeINSPECTION TYPE: PFLT, OXYGEN REGULATOR AT S/O POSITION HAS FLOW IN ALL POSITIONS. REMOVED AND REPLACED S/O OXYGEN REGULATOR, OPS CHECK NORMAL.Jan 20, 2004 · N945UP · Boeing 72722C · Crew Oxygen SystemSDR CA040109004Fire Detector · malfunctioned(CAN) ON APPROACH, THE ENGINE FIRE WARNING BELL SOUNDED CONTINUOUSLY, THERE WERE NO ENGINE WARNING LIGHTS ON. ON THE GROUND MAINTENANCE INSPECTED ALL ENGINES NO FAULTS WERE FOUND. MAINTENANCE WAS UNABLE TO DUPLICATE PROBLEM AGAIN ON THE GROUND. THE FIRE DETECJan 9, 2004 · Boeing 72722C · Fire DetectionSDR UPS03241663Fire Detector · will not testLOWER CARGO FIRE MX LIGHT ON. CODES A7418A, A9051A 26-18-02 SYSTEM OK. TESTED AND RESET LOWER CARGO SMOKE DETECTOR SYSTEM IAW MM 26-18-02 SYSTEM OK.Dec 15, 2003 · N941UP · Boeing 72722C · Fire DetectionSDR CA031118011Rib · cracked(CAN) DURING ACCOMPLISHMENT OF AD 2002-12-13 AND ENGINEERING ORDER 7-5510-7-5001PT1 INSPECTION OF THE ELEVATOR HINGE SUPPORT RIBS FOR CRACKS IN THE FLANGES ON AIRCRAFT WITH KNOWN 7079-T6 MATERIALS. A CRACK WAS FOUND IN A NON-TYPICAL AREA NOT COVERED BY THE ADOct 20, 2003 · Boeing 72722C · Elevator Tab, Attach Fittings
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