Boeing 727-227
Service difficulty reports · 5,082
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 = '727227' 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 = '727227' 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 98FDEA00111Bellframe · dentedBS 660L, STR 23L, 22L, 24L AND 25L IS DENTED (BELLFRAME) AND HOLES DRILLED IN RADIUS. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-40-3.SDR 98FDEA00114Skin · corrodedLWR FUSE SKIN BULGE BETWEEN STR 26R AND STR 25R, BS 1148R. REMOVED ALL CORROSION AND INSTALLED FRAME SHEAR TIE REPAIR AT SKIN ATTACHMENT PER SRM 53-10-4 FIG 11.SDR 98FDEA00113Frame · crackedINSPECTED FRAME AT BS 930, STR 14R, CRACK FOUND. INSTALLED DOUBLER AS PER EO 7-5310-7-4330.SDR CALA9800716Light · inoperativeINSPECTION FOUND CENTER AISLE EMERGENCY EXIT LIGHT BETWEEN L-2 AND R-2 DOORS INOPERATIVE. THE BATTERY PACK FOR EMERGENCY EXIT LIGHT WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-11.SDR CALA9800265Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 380, RBL 0 TO 65. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-08, FIGURE 3, 51-10-2, AND 51-30-2.SDR CALA9800264Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 400, RBL 0 TO 25. A FLOORBEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-08, FIGURE 3.SDR TAOA029805Battery Pack · dischargedFLT 6141, L/S OVERNIGHT, EMERGENCY EXIT LAMP AT 3 ABC OVERHEAD INOPERATIVE. REPLACED BASE ASSEMBLY AND BATTERY PACK, OPERATIONAL CHECK NORMAL PER MM 33-50-00. (M)SDR CALA9800211Fuel Nozzle · streakingTHE NR 1 ENGINE POPPED AND EGT WENT TO 600 DEGREES WHILE CLIMBING THROUGH 18000 FEET AFTER TAKEOFF FROM IAH. THE ENGINE VIBRATED AND WAS SHUTDOWN. THE N2 DROPPED TO 70 PERCENT BEFORE THROTTLE WAS PULLED TO IDLE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANSDR 98FDEA00101Beam · corrodedNR 0794 7-5750-7-231, LEFT MLG BEAM CORRODED ON UNDERSIDE WHERE NR 4 FLAP TRACK CONTACTS IT. REMOVED CORROSION BLENDED AREA PER EA 7-5730-29358 EA - DATE 2/10/98.SDR 98FDEA00100Stringer · crackedNR 0502 72C235-02, UPPER LOBE BS 720B - 720C, STR 15L CRACKED AT AFT FASTENER FWD OF ICE LIGHT HOUSING. REPAIRED CRACKED STRINGER PER SRM 53-10-3 FIG 5.SDR 98FDEA00099Bellframe · dentedNR 0172 71C209-02, BELLFRAME DENTED BS 560L BETWEEN STRINGERS 22-25L. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-40-3 FIG 1.SDR AALA980278Retract Mech · req'd serviceMCI - FLT 1675 - AFTER TAKEOFF MCI, FLAPS WERE RETRACTED AND NR 7 FLAP DID NOT RETRACT. AIRCRAFT RETURNED TO MCI AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED SYSTEM AND CYCLED FLAPS SEVERAL TIMES WITH NORMAL OPERATION. SYSTEM GROUND CHECKED NORMAL OPERSDR 98ZZZM410Battery Pack · dischargedDURING P/F FOUND THE EMERGENCY EXIT LIGHT ON AFT CARGO DOOR INOP. REPLACED BATTERY PACK FOR EMERGENCY LIGHT ON AFT CARGO DOOR. (M)SDR 98ZZZM409Light · missingDURING P/F FOUND THE FORWARD EMERGENCY CEILING AREA LIGHT MISSING (NEAR ROW 11). REPLACED MISSING AREA LIGHT AS REQUIRED, OPS CHECKED NORMAL. (M)SDR TAOA019816Battery Pack · dischargedFLT 6151 - OVERNIGHT L/S LGA, EMERGENCY EXIT SIGN AT ROW 3 IS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL PER MM CHAPTER 33-50. (M)SDR TAOA019815Battery Pack · dischargedFLT 6151 - DURING OVERNIGHT L/S LGA, FORWARD ENTRY AISLE EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL PER MM CHAPTER 33-50. (M)SDR AALA980241Light · inoperativeTUL - FLOOR TRACK LIGHTING INOPERABLE. INSTALLED NEW EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROW 5 AND ROW 6. INSTALLED NEW CONNECTOR ON EMERGENCY FLOOR TRACK POWER WIRES AT ROW 30. OPS CHECKED OK. TST: 70,613 HOURS. CYCLES: 47,995. (X)SDR CALA9800138Bulkhead · crackedINSPECTION FOUND, A 1 CRACK IN FORWARD FACE OF STA 1183 BULKHEAD ON RT SIDE ABOVE OUTFLOW VALVE. A WEB REPAIR WAS INSTALLED IAW BOEING DRAWING NR 65C31446, SRM 51-30-0, AND ECRA 553A0022.SDR 98FDEA00059Annunciator · inoperativePASSING 1000 FT ON T/O, THE MAIN CARGO DOOR WARNING LIGHT CAME ON. AIRCRAFT RELEASED FOR SERVICE PER MEL/CDL: 52-4A CATEGORY: A EXPIRATION: 29-JAN-98. MAIN CARGO DOOR ANNUNCIATOR LIGHT INOP. MAIN CARGO DOOR IS CLOSED AND LOCKED PRIOR TO EACH BLOCK OUT OK TOSDR 98FDEA00058Shear Web · corrodedCORROSION (C53-224-04) ON TOP AND BOTTOM OF SHEAR WEB AT BS 1175, RBL 1 TO 15, WL 208. *S/D* REMOVED AND REPLACED DAMAGED SHEAR WEB, BS 1140 TO 1176, RBL 20 TO LBL 20, WL 208 IAW FED-EX SRM 51-30-2, 51-20-1.SDR 98FDEA00057Chord · corrodedCORROSION (C53-224-08) ON 1176 REINFORCEMENT CHORD AT BS 1176, RBL 7, WL 208. *S/D* REMOVED AND REPLACED REINFORCEMENT CHORD AT BS 1176, RBL 65 TO LBL 65, WL 208 PER FED-EX SRM 51-30-2 AND BOEING DRAWING NR 65-19606.SDR 98FDEA00056Shear Web · corrodedUPON REMOVAL OF 1176 REINFORCEMENT CHORD ON NR 0094, DISCOVERED CORROSION ON SHEAR WEB AT BS 1176, RBL 32, WL 208. *S/D* REMOVED AND REPLACED SHEAR WEB FROM BS 1171 TO 1177, RBL 16 TO RBL 44 PER FED-EX SRM 51-40-2.SDR CALA9800129Battery Pack · dischargedINSPECTION FOUND, THE AFT ENTRY EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED.SDR CALA9800128Rib · crackedINSPECTION FOUND A 2 INCH CRACK AT FASTENER OF RT WING LEADING EDGE RIB, INBOARD OF NR 4 LEADING EDGE FLAP, AT L/E STA 130. THE CRACKED AREA WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR CALA9800127Skin · crackedINSPECTION FOUND A .5, 1, AND 2 CRACK IN RT SIDE OF VERTICAL STABILIZER SKIN LOWER SECTION AT STA 1343. THE AREA WAS REPAIRED IAW ECRA 5530-01190.SDR CALA9800126Stop · crackedINSPECTION FOUND A 1 CRACK IN L-1 AFT UPPER DOOR STOP AT FITTING. THE L-1 AFT UPPER DOOR STOP WAS REMOVED AND REPLACED IAW SRM 52-40-1.SDR TAOA019813Battery Pack · dischargedFLT 6131 - BOS-LGA - L-2 EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL PER CHAPTER 33-50. (M)SDR CALA9800105Rib · crackedINSPECTION FOUND A 2 INCH CRACK AT FASTENER IN RT WING RIB INBOARD OF NR 4 LEADING EDGE FLAP AT L/E STA 130. THE CRACKED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR 98FDEA00065Floorbeam · corrodedNR 0682 72 C 237-02 BS 1070, RBL 60 TO LBL 24 LOWER FORWARD FLANGE CORRODED. REMOVED CORRODED AREA OF FLOORBEAM FLANGE AND REPAIRED WITH FLOORBEAM REPAIR PER SRM 53-10-8.SDR CALA9800078Bracket · crackedINSPECTION FOUND A .2812 INCH CRACK OUTBOARD OF NR 8 SPOILER ACTUATOR IN RT WING INBOARD TRAILING EDGE PANEL SUPPORT BRACKET AT WS 232. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND ECRA 5750-0287SDR CALA9800077Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN RT WING LEADING EDGE LOWER SKIN ABOVE NR 5 LEADING EDGE FLAP ACTUATOR, WS 224. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9800076Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN FRAME TO FUSELAGE ATTACH ANGLE IN AFT STAIR COMPARTMENT, RT SIDE, STA 1283. THE ANGLE WAS REMOVED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR AALA980088Web · crackedTUL - APPROX .75 INCH CRACK IN WEB RADIUS AT UPPER CORNER ATTACH TO VERTICLE FIN RT SIDE STATION 1363. STOP DRILLED CRACK, INSTALLED WEB ANGLE DOUBLER REPAIR PER SRM 51-40-2 FIG 1. (M)SDR TAOA019809Battery Pack · dischargedFLT 6141 - BOS-LGA - FOUND ON L/S CHECK, OVERHEAD EMERGENCY EXI LIGHT AT ROW 3 ABC INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL PER MM CHAPTER 33-50. (M)SDR CALA9800075Light · inoperativeINSPECTION FOUND EMERGENCY FLOOD LIGHT AT LEFT SIDE OVER AFT AIRSTAIRS INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED.SDR CALA9800073Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF NR 6 LEADING EDGE SLAT STA 234. AN ANGLE DOUBLER WAS INSTALLED IAW SRM 51-40-3.SDR CALA9800072Rib · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF BOTTLE PIN ABOVE PNEUMATIC DUCT FORWARD SUPPORT BRACKET AT FSS 106.8. A REPAIR WAS INSTALLED IAW SRM 51-40-3.SDR CALA9800071Skin · crackedINSPECTION FOUND A .25 INCH CRACK IN RT WING LEADING EDGE SKIN AT NR 6 SLAT OUTBOARD HOOK. THE CRACK WAS STOP DRILLED PER SRM 51-10-1, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4.SDR CALA9800070Skin · bentINSPECTION FOUND LT WING OUTBOARD AILERON TAB LOWER LEADING EDGE SKIN BENT AND DEBONDED. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41.SDR CALA9800067Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN RT SIDE OF VERTICAL STABILIZER STRINGER NR 9 BETWEEN RIB NR 7 AND NR 8. THE CRACK WAS LOCATED AT ATTACH BOLT. THE FASTENERS WERE REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-2.SDR CALA9800066Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER STRINGER NR 8 BETWEEN RIB NR 8 AND NR 9. THE FASTENERS WERE REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-2.SDR MZZA98055Skin · delaminatedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD FORE FLAP UPPER SKIN AT WBL 164. THE DAMAGED SKIN 4 INCH BY 3 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)SDR CALA9800064Stringer · crackedINSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE IN LT WING SECOND UPPER STRINGER FROM REAR SPAR ABOVE RIB AT WS 629. THE FASTENERS AND CLAMPS WERE REMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW EA 5762-01SDR CALA9800063Stringer · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING STRINGER AT WS 656.5, TOP OF RIB ATTACH POINT ACCESS THROUGH PANEL 7617. THE CRACK WAS STOP DRILLED AND THE AREA WAS REPAIRED IAW EA 5762-01050.SDR CALA9800062Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF BOTTLE PIN LOWER EDGE AT FSS 106.8. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3.SDR CALA9800061Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE RIB INBOARD OF NR 4 LEADING EDGE FLAP AT LEADING EGDE STA 130. THE CRACK WAS STOP DRILLED AND AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-1, AND 51-30-2.SDR CALA9800060Skin · crackedINSPECTION FOUND FOUR .5 INCH CRACKS AROUND FASTENERS OUTBOARD OF LAMP LIGHT IN WING LEADING EDGE INTERNAL SKIN AT FSS 106. THE CRACKED AREAS WERE CUT OUT. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-10-6.SDR CALA9800059Rib · crackedINSPECTION FOUND A .5 INCH CRACK INSIDE LT WING LEADING EDGE AT RIB LEADING EDGE STA 130 ABOVE HOT AIR DUCT PLENUM. ALSO, A .5 INCH CRACK WAS FOUND INSIDE LT WING LEADING EDGE AT RIB LEADING EDGE STATION 130 BELOW LIGHTENING HOLE AREA. DOUBLER REPAIRS WERE FSDR CALA9800058Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN LEADING EDGE SKIN AT DOUBLER STRAP INSIDE LT WING DIRECTLY ABOVE NR 2 LEADING EDGE FLAP ACTUATOR AT WS 224. THE CRACKED DOUBLER WAS REMOVED, A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9800057Stringer · crackedINSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE IN LT WING FIRST UPPER STRINGER FROM REAR SPAR, ABOVE RIB AT WS 656.50. THE FASTENERS AND CLAMPS WERE REMOVED. THE CRACK WAS STOP DRILLED AND THE AREA WAS REPAIRED IAW EA 5762-01050.
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