Boeing 727-22

Service difficulty reports · 1,282

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 = '72722'
  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 98FDEA00610Skin · corrodedCORROSION ON FUSELAGE SKIN 25 PERCENT LOBE OF MATERIAL BETWEEN STR 25R-26R, BS 360. CUT OUT CORROSION, INSTALLED DOUBLER AND FILLER ON OUTSIDE OF SKIN EXTENDING 3 ROWS BELOW SKIN LAP PER EA 7-5330-29666. DATED 9/18/98 AND SRM 53-30-3.Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 98FDEA00609Floorbeam · damagedUPPER LOBE FLOORBEAM HAS DOUBLER DRILL HOLE BS 990. CUT OUT DAMAGE, INSTALLED DOUBLER PER AARD 53-10-07-02 AND EA 7-5310-29648.Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00608Floorbeam · damagedCABIN FLOORBEAM HAS ONE DOUBLE DRILL HOLE BS 1010, RBL 63. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-07-02 FIG 3 AND EA 7-5310-29648.Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00607Floorbeam · damageFLOORBEAM CUT ACROSS TOP FLANGE BS 1130, RBL 63. BLENDED OUT DAMAGE AND INSTALLED .080 STRAP OF 7075-T6 ALUM PER AARD 53-10-07-01 AND 7-5310-29698.Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00606Floorbeam · damagedCABIN FLOORBEAM CUT ACROSS TOP FLANGE BS 1050, RBL 63. CUT OUT DAMAGE, INSTALLED DOUBLER PER AARD 53-10-07-02 AND EA 7-5310-29648.Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00605Floorbeam · damagedCABIN FLOORBEAM CUT ACROSS TOP FLANGE AT STR 970, RBL 63. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-07-02 AND EA 7-5310-29648.Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00603Floorbeam · corrodedUPPER LOBE, BS 1050 HEAVY CORROSION ON LWR FWD LEG OF FLOORBEAM AT LBL 29. BLENDED OUT CORROSION IN AREA NOTED PER SRM 51-10-6. BLENDED AREA OUT OF LIMITS. CUT OUT DAMAGE AND INSTALLED DOUBLER ON FLOORBEAM PER AARD 53-10-07-2.Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00594Wire · brokenON CLIMBOUT AFTER T/O, OBSERVED NR1 OIL TEMP PEG OUT. IT DID COME TO YELLOW BAND. CYCLED CB WHEN RESET GAUGE PEG AGAIN. ALL OTHER IND NORM. EXECUTED PRECAUTION SHUTDOWN PER RED TAB LAND AND TAXI NORM. FOUND BROKEN WIRE AT CONNECTOR ON TEMP BULB. REPAIREDSep 25, 1998 · N191FE · Boeing 72722 · Engine Oil System WiringSDR 98FDEA00592Compressor · bird strike98-235 - ON T/O, SUSPECT BIRD STRIKE AT NOSE WHEEL WELL AREA, FOLLOW BY SEVERE VIBRATION IN NR 3 ENG. ENG SHUTDOWN IAW FOM AND EMERG LAND MADE (MEM RETURN). REMOVED AND REPLACED NR 3 ENG COMPRESSOR BLADES DAMAGED IAW WORK CARD 70T0503 AND 70T0301. OPS CHECKSep 24, 1998 · N105FE · Boeing 72722 · Turbine Engine Compressor SectionSDR 98FDEA00578Bulb · failedSHORT FINAL RUNWAY 36R MEM, NORM GEAR EXT CREW OBSERVED NO DOWN GROUND IND ON LEFT MAIN GEAR. NOSE AND R/M IND DOWN NORM. CAPT PERFORMED GO-AROUND AFTER RECYCLING GEAR TO NO AVAIL. DID MAN GEAR EXT CKLIST AND GOT VISUAL CONFIRMATION FROM TOWER. LANDED, PINSep 17, 1998 · N166FE · Boeing 72722 · Landing Gear Position and WarningSDR 98FDEA00613Floorbeam · corrodedAFT CARGO FLOORBEAM BS 1050, LWR CHORD HAS CORROSION FROM RBL 24- RBL 43. INSTALLED FLOORBEAM REPAIR LWR CHORD PER SRM 53-10-8 PG 11-17.Sep 16, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00602Floorbeam · corrodedUPPER LOBE HEAVY CORROSION ON UPPER SURFACE OF LWR FLANGE OF FLOORBEAM BS 1050, RBL 39. INSTALLED FLOORBEAM LWR CHORD REPAIR PER SRM 53-10 8 PG 11-17.Sep 16, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00601Floorbeam · misdrilledUPPER LOBE FLOORBEAM BS 1070, RBL 625 HAS DOUBLE DRILL HOLE IN FLOORBEAM. CUT OUT AREA OF DAMAGE AND REPAIR PER AARD 53-10-07.Sep 14, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00559Floorbeam · corrodedNR 0936 - UPPER LOBE, FLOORBEAM BS 680 CORROSION ON UPPER FLANGE LBL 10- RBL 6. CORROSION REMOVAL OUT OF LIMITS AT LBL 5 FWD SIDE OF FLANGE. INSTALLED ANGLE DOUBLER PER AARD 53-10-07-2.Sep 9, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00557Skin · damagedNR 0698 - LFEC IND 10 PERCENT MATERIAL LOSS JUST ABOVE STR 23 LT, 2 AFT OF BS 360 FRAME. DAMAGED AREA, REMOVED AND REPLACED DOUBLER INSTALLED PER SRM 53-30-3 PG 14B-14D.Sep 9, 1998 · N169FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 98FDEA00556Skin · corrodedNR 0342 - UPPER LOBE BS 886 HEAVY CORROSION AT WINDOW BELT AND ON SKIN 8 ABOVE STR 14L. REMOVED CORROSION FRAME WAS TAKEN OUT OF LIMITS. WINDOW FRAME REPLACED FOR EA 7-5330-29636 AND SRM 51-30-2 DOUBLER INSTALL PER EA 7-5330-29636.Sep 9, 1998 · N169FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 98FDEA00549Skin · damagedLOW FREQ EDDY CURRENT IND 15 PERCENT MATERIAL LOSS BS 360 AFT FASTENER ROW STR 4 RT BOTTOM OF SKIN LAP TO ONE INCH BELOW. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 5.Aug 26, 1998 · N169FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 98FDEA00550Floorbeam · corrodedUPPER LOBE BS 380 HEAVY CORROSION ON FLOORBEAM AT LBL 34. REMOVED CORROSION PER SRM 51-10-6. CORROSION REMOVAL OUT OF LIMITS. INSTALLED REPAIR PER AARD 53-10-07-2 PG 1 AND 2 FIG 3.Aug 18, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00498Clamp · loose98-0199 - DURING CLIMB-OUT PASSING 10K FT, ENG 3 STRUT LGT ILLUM. RT PACK WAS TURNED OFF AND ENG 3 BLEED CLOSED. WHILE REFERENCING RED TABS, LGT EXT LGT TESTED OK. RED TABS COMPLETE. FOUND NR 3 ENG BLEED VLV IN 3 STRUT WITH LOOSE CLAMPS. AIR LEAK. RESECUAug 11, 1998 · N195FE · Boeing 72722 · Pneumatic Distribution SystemSDR 98FDEA00497Computer · malfunctionedSTICK SHAKER AFTER TAKEOFF DURING FIRST FLAP RETRACTION 165 KIAS. OCCURRED INTERMITTENTLY AT ALL ALTITUDES AND AIRSPEEDS UNTIL LANDING, PITCH APPROX 8 DEG UP. *S/D* REMOVED AND REPLACED STALL WARN COMP AND ANGLE ATTACK SENSOR RIGHT, TEST OK.Aug 11, 1998 · N190FE · Boeing 72722 · Stall Warning SystemSDR 98FDEA00481Connector · contaminated98-0188 STA-MEM - SHORTLY AFTER GEAR SELECTED DOWN HAD FIRE WARN BELL WITH NO ASSOCIATED LIGHTS. LANDED AND MEMPHIS FIRE CREW INSP A/C, FOUND NO EVIDENCE OF FIRE. APPROXIMATELY 30 SECONDS AFTER GEAR EXTENSION. FOUND CONDENSATION ON CONNECTOR. DISCONNECTEDJul 31, 1998 · N149FE · Boeing 72722 · Fire DetectionSDR DHL98707003Actuator · leakingAFTER TAKEOFF WITH GEAR AND FLAPS UP, THE A- SYSTEM QUANTITY DECREASED TO ZERO. CRANKED GEAR DOWN, EXTENDED FLAPS AND LED WITH ALTERNATE SYSTEM. A-SYSTEM SHUT OFF 7 MINUTES. ABNORMAL PROCEDURES COMPLIED WITH. FOUND NR 1 LEADING EDGE FLAP ACTUATOR LEAKING.Jul 28, 1998 · N707DH · Boeing 72722 · Leading Edge Slat ActuatorSDR 98FDEA00459Splice · crackedCRACKED STRINGER SPLICE AT BS 440, STR 20 RT. *S/D* REPLACED STRINGER SPLICE, BS 440, STR 20 RT IAW FED-EX SRM 53-10-3.Jul 17, 1998 · N193FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR DHL98707002Oil Syst · reqd serviceLOST OIL QUANTITY ON CLIMBOUT FROM NR 2 ENGINE FROM 3.8 GAL TO 2.2 GAL. OIL TEMP WAS 119 DEGREES AND DROPPED TO 105 DEGREES. SERVICED NR 2 ENGINE WITH 7 QTS OF OIL PER MM 12-13-1, RESECURED CAP.Jul 14, 1998 · N707DH · Boeing 72722 · Turbine Engine Oil SystemSDR 98FDEA00451Switch · malfunctioned98-0176 STA-MEM: AFTER TAKEOFF WHEN GEAR WAS RAISED, THE GREEN NLG LIGHT AND RED GEAR DOOR LIGHT FOR NOSE GEAR REMAINED ON. AFM PROCEDURES WERE FOLLOWED BUT NO LUCK. REMOVED AND REPLACED LANDING GEAR ACCESSORY BOX AND NLG LOCK SWITCH PER M/M 32-61-21. REJul 11, 1998 · N184FE · Boeing 72722 · Landing Gear Position and WarningSDR 98FDEA00448Switch · inopSTA-MEM: NOSE GEAR UNSAFE. RECYCLED 4 TIMES, FOURTH TIME AFTER 3 MINUTES DELAY GOT GREEN LIGHT. NOSE ALIGNMENT STRIPE SAFE. REPEAT. INSTALLED (3) GEAR LOCK PINS. REMOVED AND REPLACED NOSE GEAR POSITION SWITCH PER 32-61-20. OPERATIONAL CHECK PER MAINTENAJul 9, 1998 · N184FE · Boeing 72722 · Landing Gear Position and WarningSDR 98FDEA00435Frame · crackedNR 866 001 - STA-PAE, CRACK IN RADIUS OF BS 480 FRAME B4 STR 27 RT. REPAIRED CRACK IN RADIUS OF BS 480 BY STR 27 RT PER FED-EX EA NR 7-5310-39851.Jul 6, 1998 · N193FE · Boeing 72722 · Fuselage Main, FrameSDR 98FDEA00454Chord · corrodedSTA-PAE - LOWER CHORD AT BS 740 IS CORRODED AT RBL 13 TO RBL 20. COMPLIED WITH EA 7-5710-39850 ACCESS BLENDED AND TREATED CORROSION ON LOWER CHORD 740, RBL 13 - RBL 20. RESTORED AREA IAW ER 98-2645.Jul 2, 1998 · N193FE · Boeing 72722 · Wing Miscellaneous StructureSDR 98FDEA00427Bleed Line · loose98-0165 STA-FLL: LWR AFT BODY OVERHEAT LIGHT ILLUM PASSING FLT LEVEL 20. THE LIGHT EXTINGUISHED 3 MIN AFTER CLOSING NR 1 ENG BLEED AND THE LEFT PACK AS DIRECTED IN CHECKLIST. THE INITIAL CONFIGURATION WHEN THE LIGHT ILLUM WAS BOTH PACKS ON NR 1 AND RIGHT NRJul 2, 1998 · N181FE · Boeing 72722 · Pneumatic Distribution SystemSDR 98FDEA00426Valve · overheat98-0164 - STA-AFW - IN CRUISE FLIGHT LEVEL 250 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. AFTER OPENING NR 1 BLEED VALVE AND CLOSING THE LEFT NR 2 BLEED VALVE LIGHT EXTINGUISHED AFTER ABOUT 1 MINUTE. NO ANTI-ICE WAS USED. REMOVED AND REPLACED LEFT PACK VALJul 2, 1998 · N181FE · Boeing 72722 · Cabin Cooling SystemSDR 98FDEA00422Pack Valve · leakingCLIMBING THRU 17,000 LOWER AFT BODY HEAT LIGHT CAME ON. COMPLIED WITH PROCEDURES. LIGHT WENT OUT AFTER SECURING NR 1 BLEED. LEAK BETWEEN PACK AND BLEED VALVE ON NUMBER 1 ACCORDING TO PROCEDURE. RAN ENGINE DUPLICATING BLEED CONFIGURATION. CHECKED DUCTING CJun 30, 1998 · N181FE · Boeing 72722 · Pneumatic Distribution SystemSDR 98FDEA00350Retract Mech · lack of lubeON FINAL, NOSE GEAR DID NOT INDICATE DOWN (NO GREEN LIGHT) WHEN GEAR DOWN WAS INITIALLY SELECTED. GEAR HANDLE RECYCLED AND ALL GEAR INDICATED NORMAL DOWN AND LOCKED. LUBED NOSE GEAR, CYCLED GEAR SEVERAL TIMES, OPS CK NORMAL, INDICATED THREE GREEN LIGHTS, PERMay 15, 1998 · N184FE · Boeing 72722 · Landing Gear Retraction/Extension SystemSDR 98FDEA00335Coalescer Bag · dirty98-0118 - ON T/O WITH T/O PWR SET. COCKPIT FILL WITH BURN ODOR. NR 1 BLD WAS OPEN AND LEFT PACK ON. SWITCH BLD AIR SOURCE TO NR 2 ENG. STILL HAD FUMES SWITCH TO RIGHT PACK OPER AND WAS OK. AFTER T/O TURNED LEFT PACK ON WITH CLIMB POWER AND SMELL CAME BACKMay 7, 1998 · N167FE · Boeing 72722 · Humidity Control SystemSDR 98FDEA00333Condenser · malfunctionedAT TAKEOFF POWER COCKPIT FILLS WITH STRONG BURNING ODOR. SUSPECT LEFT PACK OR ENGINE NR 1 BLEED SYSTEM IS CONTRIBUTING TO PROBLEM. WHEN LEFT PACK IS TURNED OFF IN FLIGHT ODOR IS REDUCED. DO NOT APPEAR TO GET ODOR EXCEPT IN HIGH ENGINE POWER SITUATION. RAN May 7, 1998 · N167FE · Boeing 72722 · Cabin Cooling SystemSDR 98FDEA00332Condenser · malfunctionedDURING FLIGHT, LEFT PACK EMITS STRONG ODOR. SMELLS LIKE PAINT, HOT ODOR. REMOVED AND REPLACED LEFT PACK CONDENSER, WATER SEPARATOR. OPERATIONAL LEFT PACK NO ODOR NOTICED AFTER 20 MINUTES. LEFT PACK OK FOR SERVICE.May 5, 1998 · N167FE · Boeing 72722 · Cabin Cooling SystemSDR DHL9870738CBulkhead · crackedAT C-CHECK, AFT BAGGAGE 950 BULKHEAD CRACKED AT LBL 12 WL 185. STOP DRILLED END OF CRACK, HFEC. INSTALLED DOUBLER REPAIR 5 BY 12 PER SRM 53-10-9. N/R 3724.Apr 30, 1998 · N707DH · Boeing 72722 · Wing, Rib/BulkheadSDR DHL9870712CFitting · crackedAT C-CHECK, CRACK INDICATION AT R/W INBD T/E FLAP CAVITY NR 10 SPOILER INBD HINGE SUPPORT FITTING. REMOVED AND REPLACED SUPPORT FITTING PER SRM 51-30-2. N/R 2777Apr 30, 1998 · N707DH · Boeing 72722 · SpoilersSDR DHL9870739CBulkhead · crackedAT C-CHECK, AFT 950 BULKHEAD CRACKED AT APPROX RBL 41 WL 185. STOP DRILLED ENDS OF CRACK, HFEC. INSTALLED DOUBLER REPAIR PER SRM 53-10-9, 11.5 BY 5. N/R 3712.Apr 28, 1998 · N707DH · Boeing 72722 · Wing, Rib/BulkheadSDR DHL9870717CBulkhead · crackedAT C-CHECK, AFT BAGGAGE 950 BULKHEAD CRACKED AT APPROX RBL 22 WL 185. STOP DRILLED ENDS OF CRACK, HFEC, INSTALLED DOUBLER REPAIR 12 X 5. N/R 3713Apr 28, 1998 · N707DH · Boeing 72722 · Fuselage Main, BulkheadSDR DHL9870716CBulkhead · crackedAT C-CHECK, AFT BAGGAGE 950 BULKHEAD CRACKED AT APPROX RBL 12 WL 185. STOP DRILLED END OF CRACK, HFEC, INSTALLED DOUBLER REPAIR PER SRM 53-10-9, 12 X 5. N/R 3711Apr 28, 1998 · N707DH · Boeing 72722 · Fuselage Main, BulkheadSDR DHL9870728CFitting · crackedAT C-CHECK, RIGHT SIDE STA 1183 DOOR FRAME 7 DOOR STOP FITTING CRACKED. REMOVED NR 7 STOP FITTING AND REPLACED PER SRM 51-10-1, N/R 5599.Apr 27, 1998 · N707DH · Boeing 72722 · Passenger/Crew DoorsSDR DHL9870727CFitting · crackedAT C-CHECK, LEFT SIDE 1183 DOOR FRAME STOP FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-30-2. DOOR ADJUSTED ON N/R 5546 N/R 5600.Apr 27, 1998 · N707DH · Boeing 72722 · Passenger/Crew DoorsSDR DHL9870735CFloor Beam · crackedAT C-CHECK, LEFT MLG BEAM SUPPORT AT BS 940 CRACKED AT FWD LOWER FLOORBEAM FLANGE. HFEC OF CRACK, STOP DRILLED, HFEC. INSTALLED REPAIR KIT PER S/B 53-190. N/R 3683.Apr 24, 1998 · N707DH · Boeing 72722 · Fuselage Main, Floor BeamSDR DHL9870737CInlet · crackedAT C-CHECK, CENTER INLET OUTER HOUSING DELAMINATED AND CRACKED FROM BS 1116 TO BS 1151 12 O'CLOCK TO 3 O'CLOCK POSITION. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8, 75 BY 38, 20 BY 38. N/R 4891.Apr 23, 1998 · N707DH · Boeing 72722 · Nacelle/Pylon StructureSDR DHL9870736CFitting · crackedAT C-CHECK, CENTER ENGINE INLET DUCT HOUSING ATTACH FITTING CRACKED AT STA 1130 RT SIDE I/B SIDE. REMOVED AND REPLACED ATTACH FITTING PER S/B 54-011, N/R 4829.Apr 23, 1998 · N707DH · Boeing 72722 · Nacelle/Pylon StructureSDR DHL9870726CAngle · crackedAT C-CHECK, CRACK AT BS 1263 RT SIDE BELOW UPPER SKIN TORQUE BOX FWD SIDE OF FS 1263 UNDER FILLER. REMOVED AND INSTALLED ANGLE PER SRM 51-30-2. 30 BY 1.5 BY 1.5. INSTALLED WEB REPAIR ON TORQUE BOX PER SRM 51-40-2, 31. BY 15. N/R 4850.Apr 23, 1998 · N707DH · Boeing 72722 · Fuselage Miscellaneous StructureSDR DHL9870723CTab · damagedAT C-CHECK, LOWER RUDDER TAB SEPARATING AT LOWER RT AFT EDGE. INSTALLED REPAIR PER SRM 51-40-8, 15 X 15. N/R 4840Apr 23, 1998 · N707DH · Boeing 72722 · Rudder, Tab StructureSDR DHL9870722CSkin · dentedAT C-CHECK, 3 DENTS IN EMPENNAGE SKIN JUST ABOVE STR 8R, ONE AT BS 1275 AND TWO AT BS 1285. CUT OUT DAMAGED AREAS AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 27 X 17. N/R 4845Apr 23, 1998 · N707DH · Boeing 72722 · Fuselage Main, Plate/SkinSDR DHL9870745CAngle · crackedAT C-CHECK, 36 SLAT ACTUATOR ACCESS PANEL ATTACH ANGLES ARE CRACKED. REPLACED ANGLES PER SRM 51-40-4, N/R 2814.Apr 22, 1998 · N707DH · Boeing 72722 · Leading Edge DevicesSDR DHL9870742CBulkhead · crackedAT C-CHECK, AFT BAGGAGE 950 BULKHEAD HAS 3 INCH CRACK AT RBL 57 WL 191. STOP DRILLED CRACK, HFEC. INSTALLED DOUBLER REPAIR PER SRM 53-10-9, 5.75 BY 2.75, N/R 3695.Apr 22, 1998 · N707DH · Boeing 72722 · Fuselage Main, Bulkhead
Back to Boeing 727-22