Boeing 727-191

Service difficulty reports · 85

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 = '727191'
  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 B4MR98048Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND BS 680 S-16 RT END FITTING CRACKED. REMOVED FITTING IAW SRM 51-30-2. INSTALLED FITTING IAW B727 SRM 51-30-2. C-CHECK CARD NUMBER 5C-12. NON-ROUTINE TASK CARD NUMBER 113990. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR5Jun 18, 1998 · N504MG · Boeing 727191 · Fuselage Miscellaneous StructureSDR B4MR98047Stringer · damagedDURING ROUTINE C-CHECK INSPECTION, FOUND BS 380 S-4 RT STRINGER DAMAGED. REPAIRED STRINGER 4 RT AS PER B727 SRM 53-10-3 FIG 2. CROWN STRINGER REPAIR PER SRM. C-CHECK CARD NUMBER 5C-12. NON-ROUTINE TASK CARD NUMBER 113980. AMERICAN INTERNATIONAL AIRWAYS INJun 18, 1998 · N504MG · Boeing 727191 · Fuselage Main, Longeron/StringerSDR B4MR98046Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND CORROSION ON SEAT TRACK RBL-25 STA 760 TO 784. REMOVED AND REPLACED SEAT TRACK IAW 727 SRM 51-10-1 AND 53-10-5. PORTION OF SEAT TRACK REPLACED BETWEEN BS 760 AND BS 784 RBL 25. SEAT TRACK SPLICE GAP IS MORE THAN 0.19, NJun 18, 1998 · N504MG · Boeing 727191 · Fuselage, Seat/Cargo Attach FittingsSDR B4MR98045Frame · crackedDURING ROUTINE CPCP INSPECTION, FOUND 2 CRACKS IN LT FUSELAGE FRAME AT STA930 S-14L. REPAIRED 2 CRACKS IN FUSELAGE FRAME STA 930 S-14L IAW 727 SRM 53-10-4. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 113956. AMERICAN INTERNATIONAL AJun 18, 1998 · N504MG · Boeing 727191 · Fuselage Main, FrameSDR B4MR98044Frame · crackedDURING ROUTINE CPCP INSPECTION, FOUND 2 CRACKS IN RT FUSELAGE FRAME AT STA 930 S-14R. REPAIRED 2 CRACKS IN RT FUSELAGE FRAME STA 930 S14R IAW 727 SRM 53-10-4. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 113955. AMERICAN INTERNATIONAJun 18, 1998 · N504MG · Boeing 727191 · Fuselage Main, FrameSDR B4MR98043Forging · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND TAIL SKID COMPT ACTUATOR ATTACH FORGING CRACKED. REMOVED AND REPLACED TAIL SKID ACTUATOR ATTACH FORGING IAW B727 MM 32-71-41. OPS CHECKED TAIL SKID ACTUATOR, FOUND TO CHECK OUT GOOD IAW 727-100 MM REF 32-71-00. C-CHEJun 18, 1998 · N504MG · Boeing 727191 · Auxiliary Gear (Tail Skid)SDR B4MR98042Skin · corrodedDURING ROUTINE CPCP INSPECTION, FOUND CORROSION ON CENTER WING UPPER SKIN APPROX STA 760 RBL 44 TO BE OUT OF LIMITS IAW B727 SRM 57-30-1 FIG 4 NOTE A. PERFORM HFEC INSPECTION ON EFFECT HOLES NO DEFECT NOTED. INSTALLED REPAIR PARTS IAW AIA ENGINEERING DRAWINGJun 18, 1998 · N504MG · Boeing 727191 · Wing, Plate/SkinSDR B4MR98041Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND SEAT TRACK CORRODED BETWEEN BS 1110 AND 1130 RBL 45. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 113940. AMERICAN INTERNATIONAL Jun 18, 1998 · N504MG · Boeing 727191 · Fuselage, Seat/Cargo Attach FittingsSDR B4MR98040Fitting · crackedDURING ROUTINE CPCP INSPECTION, FOUND NR 13 SPOILER ACTUATOR / FLAP TRANS ATTACH FITTING CRACKED APPROXIMATELY WS 546. REMOVED AND REPLACED BRACKET IAW AIA EDR NR B205594 AND B727 SRM 51-30-2 AND 51-10-1. CORROSION TASK CARD NUMBER C57-581-03. NON-ROUTINE TAJun 18, 1998 · N504MG · Boeing 727191 · Wing, Control Surface Attach FittingsSDR B4MR98039Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND SEAT TRACK CORRODED STA 760 TO 785 RBL 42.5. REMOVED AND REPLACED SEAT TRACK BS 760 TO BS 850 IAW B727 SRM 51-10-1 AND 51-30-2 TREATED AREA FOR CORROSION CONTROL IAW B727 SRM 51-10-2. CORROSION TASK CARD NUMBER C53-224-0Jun 18, 1998 · N504MG · Boeing 727191 · Fuselage, Seat/Cargo Attach FittingsSDR B4MR98038Stringer · crackedDURING ROUTINE CPCP INSPECTION, FOUND MAIN BOX INTERIOR HAS CRACKED STRINGER AT RIB WS 601. REPAIRED IAW SB 727 57A159 FIG 4. CORROSION TASK CARD NUMBER C57-571-01. NON-ROUTINE TASK CARD NUMBER 113875. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLIJun 18, 1998 · N504MG · Boeing 727191 · Wing, Longeron/StringerSDR B4MR98037Skin · corrodedDURING ACCOMPLISHMENT OF AD 90-21-10 / SB 727-53-0109, FOUND WHILE ACCOMPLISHING LFEC INSPECTION OF BS 1080 S/B 727-53-0109 NOTED MATERIAL LOSS GREATER THAN 10 PERCENT AT LT S3 APPROX 1 TO .5 AREA. REPAIRED SKIN IAW B727 DRAWING NR 69-62161 FIG 13 (SB 727-53-Jun 18, 1998 · N504MG · Boeing 727191 · Fuselage Main, Plate/SkinSDR B4MR98036Skin · corrodedDURING ACCOMPLISHMENT OF AD 90-21-10 / SB 727-53-0109, FOUND WHILE ACCOMPLISHING LFEC INSPECTION OF BS 1080 SB 727-53-0109 NOTED MATERIAL LOSS OF GREATER THAN 10 PERCENT AT RT S10 APPROX 3 AREA. REPAIRED SKIN IAW B727 DRAWING NR 69-62161 FIG 12 (SB 727-53-010Jun 18, 1998 · N504MG · Boeing 727191 · Fuselage Main, Plate/SkinSDR B4MR98035Bushing · damagedDURING ROUTINE CPCP INSPECTION, FOUND LEFT FRONT SPAR WING TO BODY FITTING BOTTLE PIN BUSHING HAS SECTION OF LINING MISSING. REMOVED AND REPLACED LEFT FRONT SPAR WING TO BODY FITTING BOTTLE PIN BUSHINGS IAW B727 MM 57-41-11. CORROSION TASK CARD NUMBER C53-13Jun 18, 1998 · N504MG · Boeing 727191 · Wing, Fuselage Attach FittingsSDR B4MR98034Bushing · damagedDURING ROUTINE CPCP INSPECTION, FOUND RIGHT FRONT SPAR WING TO BODY FITTING BOTTLE PIN BUSHING HAS SECTION OF LINING MISSING. REMOVED AND REPLACED RIGHT FRONT SPAR WING TO BODY FITTING BOTTLE PIN BUSHINGS IAW 727 MM 57-41-11. CORROSION TASK CARD NUMBER C53-1Jun 18, 1998 · N504MG · Boeing 727191 · Wing, Fuselage Attach FittingsSDR B4MR98033Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND 2ND FROM O/B TIP OF LEFT HAND ELEVATOR STATIC WICK BASE CORRODED BETWEEN SKIN. REPAIRED IAW B727 SRM CH 55-20-3 FIG 2 SHT 1. C-CHECK CARD NUMBER 1C-52. NON-ROUTINE TASK CARD NUMBER 113726. AMERICAN INTERNATIONAL AIRJun 18, 1998 · N504MG · Boeing 727191 · Elevator, Plate/SkinSDR B4MR98032Skin · damagedDURING ROUTINE C-CHECK INSPECTION, FOUND SKIN DAMAGED AT BS 1000 S4 RT. REPAIRED SKIN IAW B727 SRM 53-30-3 FIG 5. C-CHECK CARD NUMBER 1C-133. NON-ROUTINE TASK CARD NUMBER 113705. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEAJun 18, 1998 · N504MG · Boeing 727191 · Fuselage Main, Plate/SkinSDR B4MR98031Fitting · crackedDURING ROUTINE CPCP INSPECTION, FOUND NR 3 SPOILER ACTUATOR/FLAP TRANS ATTACH FITTING CRACKED APPROXIMATELY WS 515. REMOVED AND REPLACED BRACKET IAW AIA EDR NR B2-05594 AND IAW B727 SRM 51-30-2 AND 51-10-1. CORROSION TASK CARD NUMBER C57-581-03. NON-ROUTINEJun 18, 1998 · N504MG · Boeing 727191 · Wing, Control Surface Attach FittingsSDR B4MR98030Gate · corrodedDURING ROUTINE CPCP INSPECTION, FOUND L-1 DOOR UPPER AND LOWER GATES HAVE CORROSION. LOWER GATE CORROSION WITHIN LIMITS IAW B727 SRM CH 52-00-2 FIG 2. REMOVED AND REPLACED UPPER GATE IAW B727 MM CH 52-11-00 AND SRM CH 51-30-2. CORROSION TASK CARD NUMBER C53Jun 18, 1998 · N504MG · Boeing 727191 · Passenger/Crew DoorsSDR B4MR98029Skin · damagedDURING ROUTINE C-CHECK INSPECTION, FOUND BS 480 S4 RT SKIN DAMAGED. REMOVED DAMAGE AND INSTALLED REPAIR IAW B727 SRM 53-30-3 FIG 14. C-CHECK CARD NUMBER 1C-133. NON-ROUTINE TASK CARD NUMBER 112383. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHINJun 18, 1998 · N504MG · Boeing 727191 · Fuselage Main, Plate/SkinSDR B4MR98028Stringer · corrodedDURING ROUTINE CPCP INSPECTION, FOUND BS 600 S19 RT BULGE IN LAP. REMOVED CORRODED STRINGER AND REPAIRED IAW BOEING 727 SRM 53-10-04 FIG 1. CORROSION TASK CARD NUMBER C53-100-01. NON-ROUTINE TASK CARD NUMBER 110055. AMERICAN INTERNATIONAL AIRWAYS INC (B4MRJun 18, 1998 · N504MG · Boeing 727191 · Fuselage Main, Longeron/StringerSDR B4MR96001Skin · crackedDURING C1 CHECK, INSPECTION FOUND AD94-07-08 AGING AIRCRAFT REFERENCE SB 727-53-0183: HFEC INSPECTION REVEALED FIVE CRACK INDICATIONS AT FASTENERS MARKED ON RIGHT HAND SECTION 41 FUSELAGE SKIN BS 219.8 TO BS 251.6 BETWEEN S15R TO S17R. REPAIRED CRACK RIGHT HAAug 12, 1996 · N503MG · Boeing 727191 · Fuselage Main, Plate/SkinSDR 96ZZZM868Skin · corrodedFOUND BS 360 AFT OF SPLIT SKIN THICKNESS LOSS STRINGER R3 TO R3 PLUS 8 INCHES 10 PERCENT, R3 PLUS 8 INCHES TO R4 20 PERCENT, STRINGER R2 TO L2 PLUS 10 PERCENT, L2 TO L3 10 PERCENT, L3 PLUS 10 INCHES TO L4 20 PERCENT AS MARKED AND STRINGER R2 TO R3 10 PERCENT. Mar 11, 1996 · N503MG · Boeing 727191 · Fuselage Main, Plate/SkinSDR 96ZZZM867Skin · corrodedFOUND BS 481 AFT OF SPLIT SKIN, THICKNESS LOSS STRINGER 1 PLUS 2 INCHES L TO 1 PLUS 3 INCHES R PLUS 10 PERCENT, STRINGER 1 PLUS 3L TO R2 PLUS 10 PERCENT, STRINGER R-2 TO R-2 PLUS 3 INCHES 10 PERCENT, R2 PLUS 3 INCHES TO R3 PLUS 8 INCHES PLUS 10 PERCENT, R3 PLUMar 11, 1996 · N503MG · Boeing 727191 · Fuselage Main, Longeron/StringerSDR 96ZZZM866Skin · corrodedFOUND BS 481 AFT OF SPLIT SKIN. THICKNESS LOSS STRINGER R-4 TO R4 PLUS 8 INCHES PLUS 20 PERCENT, R4 PLUS 8 INCH TO R-5 20 PERCENT, STRINGER R-5 TO R5 PLUS 6 INCHES PLUS 10 PERCENT, R6 PLUS 6 INCH TO R6 PLUS 8 INCHES 10 PERCENT, STRINGER 6 PLUS 8 INCHES TO R7 Mar 11, 1996 · N503MG · Boeing 727191 · Fuselage Main, Plate/SkinSDR 96ZZZM865Skin · corrodedFOUND BS 360 SKIN THICKNESS LOSS 10 PERCENT AT DIFFERENT STRINGER STATIONS IN BETWEEN STRINGER 10L AND STRINGER 10R, CROWN AREA INSPECTED PER AD 90-26-09. REMOVED AND REPLACED FASTENERS WITH OVERSIZE FASTENERS FROM STRINGER 5R TO 10R AND FROM STRINGER 5L TO 1Mar 11, 1996 · N503MG · Boeing 727191 · Fuselage Main, Plate/SkinSDR 96ZZZM864Skin · corrodedFOUND BS 481 SKIN THICKNESS LOSS 10 PERCENT AT MANY STRINGER STATIONS IN BETWEEN STRINGER 10L AND STRINGER 10R, CROWN AREA INSPECTED PER AD 90-26-09. REMOVED AND REPLACED FASTENERS WITH OVERSIZE FASTENERS FROM STRINGER 2L TO 10L AND FROM STRINGER 7R TO 10R PEMar 11, 1996 · N503MG · Boeing 727191 · Fuselage Main, Plate/SkinSDR 96ZZZM863Doubler · corrodedFUSELAGE EXTERIOR HAS LEVEL 1 CORROSION AROUND FASTENER AT STATION 1070 STRINGER 10R AT DOUBLE REPAIR. CORROSION REMOVED AROUND FASTENER, TREATED AREA PER SRM 51-10-6 AND 51-10-2 MATERIAL LOSS WITHIN LIMITS PER SRM 53-10-1.Feb 29, 1996 · N503MG · Boeing 727191 · Fuselage Miscellaneous StructureSDR C1HA960007Connector · dirtyNR 2 ENGINE FIRE WARNING CAME ON BRIEFLY ON TAKEOFF AND DURING T/R ON LANDING. ACCOMPLISHED VISUAL AND SHAKE CHECK OF WIRING. CLEANED OIL OUT OF CANNON PLUG. SYSTEM OPS CHECK NORMAL. NO DEFECTS NOTED. PRIOR TO T/S GROUND CHECK ACCOMPLISHMENT OF SYSTEM ANDJan 28, 1996 · N502MG · Boeing 727191 · Fire DetectionSDR CIHA9502311Fire Wire · shortedPHX - AFTER DEPARTING & DURING CLIMB AT 8,500 FEET, NR 2 ENGINE FIRE BELL & LIGHT CAME ON. ACCOMPLISHED ENG FIRE CHECK LIST. AFTER BOTH FREON BOTTLES DISCHARGED, LIGHT DID NOT GO OUT. DECLARED EMERG & RETURNED PHX PRIOR TO SHUT DOWN. ALL NR 2 ENGINE PARAMNov 30, 1995 · N504MG · Boeing 727191 · Fire DetectionSDR MGMA950187Eel Batt Pack · dischargedLEFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND OPS RESTORED TO NORMAL.May 4, 1995 · N504MG · Boeing 727191 · Emergency LightingSDR MGMA950177Switch · defectiveAFTER LANDING, TAKEOFF WARNING HORN SOUNDED WITH SPEED BRAKE HANDLE FULLY UP AND FLAPS 25 DEGREES. REMOVED AND REPLACED LEFT GEAR SAFETY SWITCH. OPS CHECK PER MM 32-07-211 OK. (M)Apr 13, 1995 · N503MG · Boeing 727191 · Landing Gear Position and WarningSDR MGMA950167Linkage · bindingWHEN SELECTING FLAPS 5 DEGREES, OUTBOARD FLAPS STUCK AT 2 DEGREES. FOLLOWED GRAND AIR ABNORMAL CHECKLIST. LANDED NORMAL FLAPS AND SLATS. AFTER LANDING, CYCLED FLAP, OPERATED NORMAL. FOUND OUTBOARD FLAP SELECTOR VALVE LINKAGE BINDING, LUBRICATED SAME, CYCLEMar 19, 1995 · N503MG · Boeing 727191 · Trailing Edge Flap Control SystemSDR MGMA950127Switch · out of adjustAFTER GEAR RETRACTION, RED DOOR LIGHT IN FORWARD PANEL AND AMBER LIGHT ON F/E PANEL ILLUMINATED AS SOON AS GEAR HANDLE SELECTED FROM UP TO OFF. PUT THE GEAR HANDLE TO THE UP POSITION, BOTH LIGHTS WENT OFF. WAITED A FEW MINUTES, THEN PUT HANDLE IN OFF POSITIOFeb 18, 1995 · N504MG · Boeing 727191 · Landing Gear Position and WarningSDR MGMA950037Eel Battery Pack · dischargedCENTER OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPS CHECKED NORMAL. TOTAL CYCLES 42,010. (Z)Jan 7, 1995 · N504MG · Boeing 727191 · Emergency Lighting
Back to Boeing 727-191