Boeing 727-232
Service difficulty reports · 6,539
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 = '727232' 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 = '727232' 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 DL72S992186Web · crackedFOUND ON F1 LETTER CK, .25 INCH CRACKS AT LIGHTENING HOLES LT LOWER TORQUE BOX WEB AT STA 1223 AND 1235. REPAIRED PER MM 53-11-0.SDR DL72S992175Sensor · failedNR 2 ENG LOW OIL PRESS LIGHT ILLUMINATED ON T/O ROLL. ABORTED T/O. RETURNED TO GATE. REPLACED PRESSURE SENDING UNIT.SDR DL72L992180Batteries · dischargedBATTERIES WEAK IN FWD COACH CLASS CABIN OVERHEAD EMERGENCY LIGHT. REPLACED BATTERIES.SDR MZZA99204Frame · crackedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG CRACK WAS FOUND ON FUSELAGE FRAME BETWEEN STRINGER 16R AND 17R AT BS 783.9. THE DAMAGED SECTION WAS TRIMMED AND REPAIRED PER BOEING DRAWING NR 65C36280 USING REPAIR KIT NR 65C36280-24. (MSDR MZZA99191Skin · damagedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.5 INCH BY 1 INCH AREA DAMAGE WAS FOUND ON L2 CABIN DOOR SKIN FORWARD LOWER CORNER. THE DAMAGED AREA WAS TRIMMED AND REPAIRED PER B727 SRM CHAP 52-40-02. (M)SDR MZZA99222Web · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO CRACKS WERE FOUND ON LEFT LOWER TORQUE BOX VERTICAL WEB LIGHTENING HOLES AT BS 1223. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAPTER 51-40-02. (M)SDR MZZA99221Gusset · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON GUSSET ATTACHED TO BS 950 LOWER TEE CHORD AND STRINGER 29L IN FLANGE. THE CORRODED GUSSET WAS REMOVED AND REPAIRED PER B727 SRM CHAPTER 51-10-01 AND 51-30-02. (M)SDR MZZA99219Fitting · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACK WAS FOUND ON LEFT WING BOTTLE PIN. THE CORRODED FITTING WAS REMOVED AND REPLACED WITH A NEW ONE POWER SRM 53-30-02. (M)SDR MZZA99218Gusset · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, AN IG CORROSION WAS FOUND ON GUSSET ATTACHED TO BS 950 BULKHEAD LOWER TEE CHORD AND STRINGER 29R INBOARD FLANGE. THE CORRODED GUSSET WAS REMOVED AND REPLACED WITH A NEW ONE PER B727 SRM CHAPTER 51-10-01SDR MZZA99216Stringer · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON RIGHT WING UPPER STRINGER S-13 ATTACHED TO WS 629 RIB. THE CRACK WAS STOP DRILLED AND REPAIRED PER CMI EA NR 5762-01050. (M)SDR MZZA99215Rib · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON RIGHT WING INSPAR WS 738.5 RIB UPPER FLANGE ATTACHED TO UPPER STRINGER 12. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 57-10-05 FIG 5. (M)SDR MZZA99214Stringer · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON RIGHT WING UPPER STRINGER S-9 ATTACHED TO WS 629 RIB. THE CRACK WAS STOP DRILLED AND REPAIRED PER CMI EA NR 5762-01050. (M)SDR MZZA99211Web · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUR CRACKS WERE FOUND ON RIGHT LOWER TORQUE BOX VERTICAL WEB LIGHTENING HOLES BETWEEN BS 1223 AND BS 1243. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAPTER 51-40-02. (M)SDR MZZA99189Fitting · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON TAIL SKID ACTUATOR RIGHT HINGE ARM INBOARD SUPPORT BRACKET IN TAIL SKID BAY. THE CRACKED FITTING WAS REMOVED AND REPLACED WITH A NEW (P/N 65-57934-8) PER B727 SRM CHAPTER 51-10-01, SDR DL72S992133Compressor · stalledAS POWER WAS INCREASING TO TAKEOFF SETTING NR 2 ENGINE HAD A HARD COMPRESSOR STALL. A HEAVY VIBRATION AND RUMBLING NOISE WAS HEARD/FELT FROM NR 2 ENGINE. MAXIMUM CROSSWIND WAS LESS THAN 3 KTS. REPLACED NR 2 ENGINE.SDR DL72S992132Light · contaminatedDURING GROUND TRANSFER OF FUEL, THE NR 1 VALVE INDICATOR LIGHT SPARKED AND CAUGHT ON FIRE. DE-POWERED SWITCH AND FIRE EXTINGUISHED. MAINTENANCE FOUND LIGHT ASSY FULL OF FUEL. CHECKED FOR FUEL LEAKS, NONE FOUND. REPLACED LIGHT ASSY, OPN NOW NORMAL.SDR MZZA99205Skin · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH LONG CRACK WAS FOUND ON FUSELAGE SKIN AT STRINGER 17R BETWEEN BS 730 AND BS 734. THE DAMAGED SECTION WAS TRIMMED AND REPAIRED PER CML ECRA NR 5330-2891. (M)SDR MZZA99200Keel Beam · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY .5 INCH AREA IG CORROSION WAS FOUND ON STRINGER29R KEEL BEAM OUTBOARD FLANGE AT BS 950 PLUS 14. THE CORRODED T-CHORD SECTION WAS TRIMMED AND REPAIRED PER B727 SB 53-0179. (M)SDR MZZA99198Keel Beam · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INCH BY .5 INCH AREA CORROSION WAS FOUND S-29L KEEL BEAM OUTBOARD FLANGE AT BS 950 PLUS 14. THE CORRODED KEEL BEAM OUTBOARD FLANGE WAS TRIMMED AND REPAIRED PER B727 SB 53-0179. (M)SDR MZZA99197Tee · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY 1 INCH AREA CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER T-CHORD AT RIGHT SIDE OF STRINGER 29R. THE CORRODED T-CHORD WAS TRIMMED AND REPAIRED PER CMI EC/RA NR 5310-3928. (M)SDR MZZA99196Tee · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG IG CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER TEE CHORD BETWEEN STRINGER 29R AND S29L. THE CORRODED SECTION WAS TRIMMED AND REPAIRED PER B727 SRM CHAPTER 51-10-01 AND 51-30-02. (M)SDR MZZA99193Fitting · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AIR ASIA, CRACK WAS FOUND ON C3 DOOR FORWARD LOWER CORNER STOP FITTING. THE DAMAGED STOP FITTING WAS REMOVED AND REPLACED WITH A NEW ONE (P/N 65-57768-6) PER CMI EA NR 5230-0185. (M)SDR MZZA99192Skin · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.5 INCH LONG IG CORROSION WAS FOUND ON NR 3 CARGO DOOR FORWARD EDGE BETWEEN NR 3 AND NR 4 STOP FITTING. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 51-40-03 FIG 1. (M)SDR DL72S992130Battery · dischargedAFT AIRSTAIR EMERGENCY EXIT LIGHT INOP ON L/O CHECK. REPLACED BATTERYS (P/N 334101877), OPER NOW NORMAL.SDR CALA9901283Stringer · crackedINSPECTION FOUND A 5 INCH CRACK AT ATTACH POINT IN LT WING UPPER FORWARD STRINGER AT WING STA 629.0. THE CRACKED AREA WAS CUT OUT, REPAIR PARTS WERE INSTALLED IAW EA 5762-01050.SDR MZZA99225Control Cable · frayedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AIR ASIA, NR 1 ENGINE START CONTROL CABLE (ESS1A) WAS FOUND FRAYED AT BS 1186. THE FRAYED CABLE WAS REMOVED AND REPLACED PER B727 MM CHAPTER 76-12-01 AND OPERATIONAL CHECK FOUND NORMAL. (M)SDR MZZA99217Spar · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION OWAS FOUND ON LEFT WING FRONT SPAR WEB ABOVE FUEL BYPASS VALVE ACTUATOR. THE DAMAGED AREA WAS BLENDED OUT AND REPAIRED PER CMI EC/RA NR 5710-01978. (M)SDR MZZA99213Spar · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON LEFT WING FRONT SPAR LOWER CHORD VERTICAL LEG AT FSS 401. THE CORRODED SECTION WAS CLEANED UP AND REPAIRED PER CMI EC/RA NR 5710-01975. (M)SDR MZZA99212Skin · bulgedTNN - DURING D-CHECK INSPECTIN ON AIRCRAFT AT AIR ASIA, A 7 INCH BY 3 INCH AREA BULGE WAS FOUND ON UPPER RUDDER SKIN AT FIN STATION 270. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-40-02, 55-20-03. (M)SDR MZZA99210Skin · bulgedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY 4 INCH AREA BULGE WAS FOUND ON UPPER RUDDER SKIN AT FIN STATION 213. THE BULGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-40-02 FIG 1 AND 55-20-03 FIG 1. (M)SDR MZZA99209Beam · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG IG CORROSION WAS FOUND ON LEFT STABILIZER UPPER T/E BEAM AT ELEV STAB 146. THE CORRODED AREA WAS REMOVED AND REPAIRED PER B727 SRM CHAP 55-10-06. (M)SDR DL72S992134Frame · crackedTHE WEB OF THE C1 DOOR CUTOUT AFT JAMB WAS FOUND WITH A SMALL CRACK EMANATING FROM A FASTENER HOLE JUST BELOW THE NR 6 DOOR STOP FITTING. THE CRACK WAS REPAIRED WITH A DOUBLER PER ER/A 368332-14.SDR DL72S992125Stiffener · crackedI/B SPAR STIFFENER CRACKED NR 7 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21 P 813.SDR DL72S992119Skin · crackedTPA LTR CHK D-2 09/21/99, .625 INCH CRACK AT FUSE SKIN STA 1250 AND STR 21R. REPAIRED PER SRM 53-30-03 FIG 25 AND ERA 368334-14.SDR DL72S992117Web · crackedONE CRACK ON VERT WEB ABOVE S-DUCT AT STA 1303 ON LT SIDE AT STR CUTOUT. REPAIRED PER SRM 53-10-4.SDR DL72S992116Skin · crackedTPA LTR CHK D-2 9/21/99, 1 CRACK ON S-DUCT HOUSING RT SIDE AT UPPER END OF PANEL 9524. REPAIRED PER MM 54-30-0.SDR DL72S992115Casting · crackedVERT STAB LT TENSION TIE BOLT CASTING CRACKED I/B SIDE. REPLACED FITTING PER BAC DWG 65-17509 REV M. TPA LTR CHK D-2 09/21/99.SDR MZZA99202Fitting · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON AFT AIRSTAIR RIGHT LOWER STRUT END TO AIRSTAIR FITTING. THE CRACKED FITTING WAS REMOVED AND REPLACED WITH A NEW ONE (P/N 65-26651-18) PER B727 SRM CHAPTER 51-10-01. (M)SDR MZZA99201Fitting · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON AFT AIRSTAIR LEFT LOWER STRUT END TO AIRSTAIR FITTING. THE CRACKED FITTING WAS REMOVED AND REPLACED WITH A NEW ONE (P/N 65-26651-17) PER B727 SRM CHAPTER 51-10-01. (M)SDR DL72L992357Insulation · damagedON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION ON ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN RT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SLSDR DL72L992356Insulation · damagedON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION ON ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FOR SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SLSDR CALA9901273Skin · delaminatedINSPECTION FOUND O/B END UPPER SURFACE OF LT WING NR 7 SPOILER DELAMINATED. THE NR 7 SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1.SDR CALA9901272Seat Track · corrodedINSPECTION FOUND G-1 GALLEY SEAT TRACK CORRODED AT STA 344-380. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-1, 51-10-06, 53-10-5, AND ECRA 5100-01844.SDR CALA9901271Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT CENTERLINE FLOORBEAM, STA 1035. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR CALA9901251Wire · disconnectedTHE EMERGENCY EXIT LIGHT WIRING WAS FOUND PULLED OUT OF CONDUIT AND DISCONNECTED AT ROW 11. THE WIRING WAS RECONNECTED AND PLACED BACK INTO CONDUIT IAW MM 20-00-00.SDR CALA9901250Intercostal · crackedINSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 990, STRINGER 23L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51-10-1.SDR DL72S992082Batteries · dischargedON L/O, FOUND MID CABIN OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPERATION NOW NML.SDR DL72S992081Stiffener · cracked2 INCH CRACK IN VERTICAL SPAR STIFFENER NR 7 SLAT O/B TRACK I/B SIDE. REPLACED SPAR STIFFENER PER MM 57-20-21.SDR DL72S992080Antenna · failedWEATHER RADAR INOP, RESET CB, LEFT IN STANDBY FOR 5 MIN. WORKED 10 MIN, THEN INOP AGAIN, REPEAT WRITE-UP. REPLACED RADAR ANTENNA AND CONTROL PANEL. TRANSMITTED RADAR FOR 20 MIN. RADAR CKS OK.SDR DL72S992079Skin · cracked5 INCH CRACK NR 2 ENG INLET OUTER SKIN BELOW DOUBLER AT 3:00 POSITION. REPAIRED PER MM 54-30-0 P 801.
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