Boeing 727-224
Service difficulty reports · 2,252
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 = '727224' 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.
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 = '727224' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR MZZA99181Control Cable · rustedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A RUSTED AILERON CABLE WAS FOUND ON LEFT WING TE CAVITY, FORWARD OF APU OF FIRE EXTINGUISHER BOTTLE. THE DAMAGED CABLE WAS REMOVED AND REPLACED PER B727 MM CHAPTER 27-10-71, 27-10-00 AND OPERATIONALLY CSDR CALA9901130Casting · crackedINSPECTION FOUND A 1 INCH CRACK IN RT FORWARD OVERWING DOOR INNER UPPER CASTING. THE CASTING WAS REMOVED AND A NEW CASTING WAS INSTALLED IAW SRM 51-30-2, FIGURE 1.SDR MZZA99179Skin · crackedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A .25 INCH LONG CRACK WAS FOUND ON BS 1218 FUSELAGE SKIN. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 53-30-03 FIG 1. (M)SDR CALA9901103Battery Pack · dischargedINSPECTION FOUND FORWARD OVERHEAD EMERGENCY LIGHT AT ROW NR 2 INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK AT FAULT. THE BATTERY PACK WAS RECHARGED AND REINSTALLED. OPERATION CHECKED GOOD IAW MM 33-50-81, PAGE 403.SDR CALA9901102Fitting · corrodedINSPECTION FOUND FORWARD END OF LT WING NR 4 FLAP TRACK FITTING CORRODED. THE FITTING WAS REMOVED AND REPLACED. THE FLAP TRACK WAS REINSTALLED IAW MM 27-51-72, PAGE 401.SDR CALA9901099Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1130, RBL 0 TO WALL. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW ECRA 5310-03893.SDR MZZA99164Gussett · corrodedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON GUSSET WHICH IS ATTACHED TO BS 950 BULKHEAD LOWER T-CHORD AND S29R. THE CORRODED GUSSET WAS REMOVED AND REPLACED PER SRM 51-30-2 FIG 1-4. (M)SDR MZZA99163Bulkhead Tee · corrodedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER T-CHORD BETWEEN S30 AND S29R. THE CORRODED LOWER T-CHORD WAS REMOVED AND REPLACED PER B727 CHAPTER 51-30-02 FIG 1-4. (M)SDR MZZA99167Skin · corrodedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH BY 5 INCH IG CORROSION WAS FOUND ON FUSELAGE SKIN AT STRINGER 29R BETWEEN BS 950 PLUS 11 AND BS 950A. THE CORRODED SKIN WAS TRIMMED OUT AND REPAIRED PER ECRA 5330-02865. (M)SDR MZZA99162Angle · corrodedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON L-ANGLE WHICH ATTACH WITH S29R (KEEL BEAM) SPLICE AND BS 950 BULKHEAD WEB IN RIGHT MLG WW. THE CORRODED L ANGLE WAS REMOVED AND REPLACED EPR SRM 51-30-02 FIG 1-4. (M)SDR MZZA99161Bulkhead Web · corrodedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON T-STIFFENER JUST ATTACHED TO BS 950 PRESSURE BULKHEAD WEB FORWARD SIDE IN RT MLG WW/ THE CORRODED T-STIFFENER WAS REMOVED AND REPLACED PER SRM 51-30-2 FIGURE 1-4. (M)SDR MZZA99160Keel Beam · corrodedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3.5 INCH BY .5 INCH WIDTH BY .122 INCH DEPTH CORROSION WAS FOUND ON RT FUSELAGE KEEL BEAM RADIUS AT BS 950 PLUS 11. THE CORRODED KEEL BEAM WAS BLENDED OUT AND REPAIRED PER ECRA 5310-03908. (M)SDR MZZA99157Bulkhead Tee · corrodedDURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 SQUARE INCH AREA CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER T-CHORD FORWARD SURFACE AT STRINGER 29R. THE CORRODED AREA WAS BLENDED OUT AND REPAIRED PER ECRA 5310-03910. (M)SDR CALA9901070Wire · brokenINSPECTION FOUND THE L-1 DOOR EXIT LIGHT INOPERATIVE. REPAIRED BROKEN WIRE AT THE L-1 DOOR EXIT IDENTIFIER. OPERATION CHECKED GOOD IAW MM 33-51-0.SDR CALA9901069Wire · brokenINSPECTION FOUND THE R-1 DOOR EXIT LIGHT INOPERATIVE. REPAIRED BROKEN WIRE TO CHARGER AND R-1 DOOR EXIT IDENTIFIER, AND RELAMPED. OPERATION CHECKED GOOD IAW SRM 33-51-0.SDR CALA9901068Battery Pack · dischargedINSPECTION FOUND A SECTION OF CABIN EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-01.SDR MZZA99174Cables · rustedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, THREE SPOILER CONTROL CABLES WERE FOUND RUSTED IN LEFT WING TE CAVITY. THE DAMAGED CABLES WERE REMOVED AND REPLACED WITH NEW ONES PER B727 MM CHAPTER 27-61-00 AND OPERATIONAL CHECK NORMALLY. (M)SDR MZZA99173Cables · rustedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO INBOARD AILERON TAB CONTROL CABLES WERE FOUND RUSTED IN LEFT MLG WW. THE DAMAGED CABLES WERE REMOVED AND REPALCED WITH NWE ONES PER B727 MM CHAPTER 27-10-00 AND OPERATIONAL CHECK NORMALLY. (M)SDR MZZA99170Front Spar · corrosionTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 6 INCH BY 1.5 INCH AREA CORROSION WAS FOUND ON LEFT WING FRONT SPAR LOWER CHORD PLATE UPPER SURFACE BETWEEN FSS 551 AND FSS 557. THE CORRODED SECTION WAS TRIMMED OUT AND REPAIRED PER ECRA NR 5710-0196SDR MZZA99168Chord Plate · corrodedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INCH BY 1.28 INCH AREA CORROSION WAS FOUND ON LEFT WING FRONT SPAR LOWER CHORD PLATE UPPER SURFACE BETWEEN FSS 513 AND FSS 516. THE CORODED SECTION WAS TRIMMED OUT AND REPAIRED PER ECRA NR 5710-0196SDR MZZA99166Fire Detector · damagedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, APU FIRE DETECTOR SENSOR EXTERIOR INSULATOR WAS FOUND STRIPPED. THE DAMAGED APU FIRE DETECTOR SENSOR WAS REMOVED AND REPLACED WITH A NEW ONE PER B727 MM 26-10-0 AND OPERATIONAL CHECK NORMALLY. (M)SDR 99ZZZM758Cables · rustedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO INBOARD AILERON TAB CONTROL CABLES WERE FOUND RUSTED IN LEFT MLG WW. THE DAMAGED CABLES WERE REMOVED AND REPALCED WITH NWE ONES PER B727 MM CHAPTER 27-10-00 AND OPERATIONAL CHECK NORMALLY. (M)SDR 99ZZZM757Cables · rustedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, THREE SPOILER CONTROL CABLES WERE FOUND RUSTED IN LEFT WING TE CAVITY. THE DAMAGED CABLES WERE REMOVED AND REPLACED WITH NEW ONES PER B727 MM CHAPTER 27-61-00 AND OPERATIONAL CHECK NORMALLY. (M)SDR 99ZZZM756Cables · rustedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, THREE SPOILER CONTROL CABLES WERE FOUND RUSTED IN LEFT WING TE CAVITY. THE DAMAGED CABLES WERE REMOVED AND REPLACED WITH NEW ONES PER B727 MM CHAPTER 27-61-00 AND OPERATIONAL CHECK NORMALLY. (M)SDR MZZA99172Control Cable · frayedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A FRAYED NR 2 ENGINE CONTROL CABLE (ESS2A) WAS FOUND AT BS 1204. THE DAMAGED CABLE WAS REMOVED AND REPLACED WITH A NEW ONE PER B727 MM CHAPTER 76-11-11 AND OPERATIONAL CHECK NORMALLY. (M)SDR MZZA99169Control Cable · frayedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A FRAYED NR 1 ENGINE CABLE (ESS1A) WAS FOUND AT BS 1186. THE DAMAGED CABLE WAS REMOVED AND REPLACED WITH A NEW ONE PER B727 MM CHAPTER 76-11-11 AND OPERATIONAL CHECK NORMALLY. (M)SDR MZZA99165Angle · crackedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AIR ASIA, A .25 INCH LONG CRACK WAS FOUND ON ANGLE WHICH IS ATTACHED TO RIGHT LOWER TORQUE BOX VERTICAL WEB AT BS 1340. THE DAMAGED ANGLE WAS REMOVED AND REPLACED PER B727 SRM CHAPTER 51-30-02 FIG 1-4. (M)SDR MZZA99156Channel · crackedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH LONG CRACK WAS FOUND ON U-CHANNEL WHICH IS ATTACHED TO RIGHT LOWER TORQUE BOX HORIZONTAL WEB AT BS 1273. THE DAMAGED U-CHANNEL WAS REMOVED AND REPLACED PER B727 SRM CHAPTER 51-40-03 FIG 1. (M)SDR MZZA99155Angle · crackedDURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH LONG CRACK WAS FOUND ON RIGHT LOWER TORQUE BOX ANGLE AT BS 1263. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 51-40-04 FIG 1. (M)SDR MZZA99159Stringer · crackedTNN - DUIRNG S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO 3.1 AND 1.68 INCH LONG CRACKS WERE FOUND ON RT FUSELAGE S-18A VERTICAL FLANGE AT BS 943. THE DAMAGED SECTION WAS TRIMMED OUT AND REPAIRED PER ECRA NR 5310-03914. (M)SDR MZZA99158Skin · crackedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A .25 INCH LONG CRACK WAS FOUND ON FUSELAGE SKIN AT BS 1218. THE CRACKED SKIN WAS STOP DRILLED AND REPAIRED PER B727 SRM 53-30-03 FIG 1. (M)SDR 2000ZZZM204B-Nut · looseON FAE - FLT 945 - KMEM TO NBJ, DURING CLIMB, THROUGH FL260 NR 3 ENGINE STARTED FLUCTUATING INTERMITTENT AT FIRST THEN STEADY. AFTER LEVEL OFF AT FL290, NR 3 ENGINE CONTINUED TO FLUCTUATE. AIRCRAFT RETURNED TO KMEM. ON GROUND MAINTENANCE INSPECTED NR 3 ENGISDR CALA9901058Web · crackedINSPECTION FOUND A 1.5 INCH CRACK AND A BEND IN INTERCOSTAL WEB BETWEEN BS 1110-1130, BL 0. THE INTERCOSTAL WEB WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 2 AND 4.SDR CALA9901055Floorbeam · corrodedINSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 320, BL 0 TO LBL 42. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-10-8, PAGE 51-52.SDR CALA9901054Angle · crackedINSPECTION FOUND FOUR CRACKS IN RT WING FIXED LEADING EDGE RIB TO SKIN INBOARD SIDE CURVED ATTACH ANGLE AT WBL 92, ACCESS CUTOUT 6401. THE CRACKS MEASURED FROM .5 TO FIVE INCHES IN LENGTH. THE CRACKS WERE STOP DRILLED, A REPAIR DOUBLER, ANGLE AND STIFFENER WSDR CALA9901053Structure · gougedINSPECTION FOUND FORWARD CARGO COMPARTMENT DOOR LOWER FORWARD AND AFT CORNERS GOUGED. THE FORWARD AND AFT CORNERS OF DOOR WERE REMOVED IAW SRM 51-10-1, PAGE 4. REPAIRED IAW SRM 51-10-2, PAGE 4, 51-10-1, PAGE 4, AND OVERHAUL MANUAL 52-30-23, PAGE 403.SDR CALA9901004Angle · crackedINSPECTION FOUND TWO .5 INCH CRACKS THROUGH BOLT HOLES AT O/B LOWER ANGLE INSIDE RT WING FIXED LEADING EDGE RIB, WBL 92.0 (AFT OF NR 4 L/E FLAP I/B END). THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, PAGE 2, 51-40-3, PAGE 1, AND 51-20-2SDR CALA9901003Web · corrodedINSPECTION FOUND TOP OF WEB CORRODED AT STA 1183, LBL 14. THE CORRODED AREA WAS CUT OUT AND A NEW WEB WAS INSTALLED IAW SRM 51-40-2, PAGE 6, FIGURE 1.SDR CALA9901002Angle · crackedINSPECTION FOUND A 4.5INCH CRACK IN UPPER T-ANGLE ABOVE WHERE RT O/B AILERON I/B HINGE BRACKET ATTACHES AT RT WING T/E RIB. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-01, PAGE 401 AND 51-30-2.SDR CALA9901001Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1138, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-1, PAGE 4 AND 51-30-2, PAGE 2.SDR CALA9901000Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 44. THE CORRODED AREA WAS CUT OUT. A REPAIR DOUBLER AND FILLER WAS INSTALLED IAW SRM 53-10-8, 51-30-2, AND 51-10-6.SDR CALA9900997Shear Web · corrodedINSPECTION FOUND AFT CABIN SHEAR WEB CORRODED JUST FORWARD OF BS 1183, LBL 17 TO RBL 17. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-1, PAGE 4 AND 51-10-7, PAGE 4.SDR CALA9900936Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN RT WING NR 7 SLAT LOWER CHORD. THE LOWER CHORD ANGLE WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-40-4, 51-30-2, 51-10-2.SDR CALA9900886Stringer · crackedINSPECTION FOUND A ,25 INCH CRACK AT LEFT WING TANK UPPER STRINGER, FIRST FORWARD FROM REAR SPAR, WS 656.5 AT TANK CUT OUT. A REPAIR WAS INSTALLED IAW ECRA 5762-01050.SDR CALA9900877Light · inopINSPECTION FOUND THE SEAT MOUNTED EMERGENCY EXIT PATH LIGHT AT ROW 30 INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED.SDR CALA9900869Floorbeam · corrodedINSPECTION FOUND CABIN FLOORBEAM CORRODED AT FS 400 BL 0 TO RBL 24. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS ACCOMPLISHED IAW SRM 53-10-8, PAGE 47.SDR CALA9900868Skin · chafedINSPECTION FOUND THE LEFT O/B FOREFLAP CHAFED IN TWO AREAS AT INBOARD END. THE CHAFED AREAS WERE CUT OUT IAW SRM 57-50-4, PAGE 17. REPAIR PARTS WERE INSTALLED IAW SRM 57-50-4, PAGE 17 AND 51-30-2.SDR CALA9900867Press Panel · crackedINSPECTION FOUND A .5 INCH CRACK IN FORWARD RT OVERWING EXIT LOWER PRESSURE PANEL. THE CRACKED AREA WAS CUT OUT IAW SRM 51-10-1, PAGE 5. A DOUBLER WAS INSTALLED IAW SRM 51-40-3, PAGE 1, 51-10-2, PAGE 1, AND 51-30-2, PAGE 1.SDR CALA9900864Stiffener · crackedINSPECTION FOUND A 1 INCH CRACK IN STIFFENER ON I/B SIDE OF FIXED L/E RIB O/B OF RT WING FORWARD BOTTLE PIN (AFT OF ANTI-ICE DUCT, ACCESS CUTOUT 6402). THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 2. A FORMER ANGLE WAS INSTALLED IAW SRM 51-40-3, FIGURE 1SDR CALA9900851Power Supply · inopINSPECTION FOUND THE FORWARD ENTRY AND FORWARD GALLEY ESCAPE SLIDE EMERGENCY LIGHTS INOPERATIVE. THE BATTERY AND POWER SUPPLY IN E&E COMPARTMENT WAS REMOVED AND REPLACED.
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