Boeing 747-132
Service difficulty reports · 1,451
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 = '747132' 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 = '747132' 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 EIAA2000090Fitting · damagedEAC-MZJ - C6/D-CHECK - DSB AND BACKUP FITTING HOLE LOCATIONS - NR 4 WING POSITION. REPAIRED PER ECRA 479-57-130-2. NR 1 HOLE - REAMED USING EXISTING HOLE LOCATION, NR 2 HOLE - PULLED OUTBOARD 0.063 INCH, NR 3 HOLE - PULLED 0.063 INCH, NR 4 HOLE - PULLED FORWSDR EIAA2000089Fitting · damagedEAC-MZJ - C6/D-CHECK - DSB AND BACKUP FITTING HOLE LOCATIONS - NR 2 WING POSITION. REPAIRED PER ECRA 479-57-129-2, NR 1 HOLE - REAMED AND PULLED DIRECTLY INBOARD 0.130 INCH, NR 2 HOLE - PULLED DIRECTLY OUTBOARD 0.100 INCH, NR 3 HOLE AND NR 4 HOLE - USED EXISTSDR EIAA2000088Fitting · damagedEAC-MZJ - C6/D-CHECK - DSB AND BACKUP FITTING HOLE LOCATIONS - NR 1 WING POSITION. REPAIRED PER ECRA 479-57-128-2, NR 2 HOLE - REAMED UP AND PULLED OUTBOARD 0.063 INCH. NR 3 HOLE - REAMED AND PULLED AFT 0.063 INCH, NR 4 HOLE - REAMED AND PULLED FORWARD 0.044SDR EIAA2000087Skin · corrodedEAC-MZJ - C6/D-CHECK - CENTER WING LOWER EXTERIOR SKIN AT APPROXIMATE STA 1030 ON RIGHT SIDE OF KEEL BEAM HAD AN AREA 1 INCH BY 2 INCH WITH SEVERE CORROSION. REPAIRED PER ECRA 479-57-127-2 REV B. BLENDED CORROSION, FLAP PEENED, AND INSTALLED FILLER. (X)SDR EIAA2000086Structure · damagedEAC-MZJ - C6/D-CHECK - DSB AND BACKUP FITTING HOLE LOCATIONS - NR 3 WING POSITION. REPAIRED PER ECRA 479-57-121-2, NR 1 HOLE. INSTALLED FREEZE PLUG, NR 2 HOLE - REAMED UP AND PULLED OUTBOARD 100 PERCENT (-0.14 INCH), NR 3 HOLE - INSTALLED 0.56 INCH DIA BOLT SDR EIAA2000085Structure · crackedEAC-MZJ - C6/D-CHECK - LEADING EDGE WING CRACKED IN SEVERAL PLACES, CONTINUES PAST FIELD REPAIR AND INTO WEB STRUCTURE AT WING AT APPROXIMATELY STA 557. REPAIRED BY PART 1 OF ECRA 479-57-116-2. INSTALLED REPAIR DOUBLER AND FILLER. (X)SDR EIAA2000084Structure · corrodedEAC-MZJ - RIGHT HORIZONTAL STABILIZER UPPER SURFACE FROM FRONT SPAR TO REAR SPAR STA 143.6 TO TIP HAD AREAS OF CORROSION. REPAIRED PER ECRA 479-55-133-2. BLENDED CORROSION, REMOVED AND REPLACED FASTENERS, ROTO-PEENED REWORKED AREAS. ACCOMPLISHED REPAIR AT SSDR EIAA2000083Skin · corrodedEAC-MZJ - C6/D-CHECK - LEFT HORIZONTAL UPPER SURFACE, INBOARD SIDE HAD CORROSION REMOVAL BLEND-OUTS WHICH WERE OUT OF LIMITS. REPAIRED PER ECRA 479-55-132-2. FLAP PEENED, INSTALLED NEW FASTENERS, AND TREATED ALL BLEND-OUT AREAS. (X)SDR EIAA2000082Keelbeam · damagedEAC-MZJ - LOWER FLANGE CUT AWAY AT RT KEEL BEAM BE 1480. REPAIRED PER ECRA 479-53-125-2. PERFORMED EDDY CURRENT OF UPPER/LOWER SURFACES AND RADIUSES; FLAP PEENED AND TREATED CUT AWAY AREA. (X)SDR EIAA2000081Stringer · corrodedEAC-MZJ - STA 1741 STR 46R CORROSION REPAIR CANNOT BE ACCOMPLISHED PER SRM 53-10-03 FIG 8 DUE TO LOCATION OF LAP SEAM. ACCOMPLISHED REPAIR PER ECRA 479-53-124-2. CUT OUT CORRODED STRINGER, SPLICED IN STRINGER SECTION WITH REPAIR ANGLES AND STRINGER SPLICE. SDR EIAA2000080Frame · corrodedEAC-MZJ - STA 480 BETWEEN STR'S 8L-9L FORWARD SIDE OF FRAME NEAR FRAME SPLICE HAD SMALL AREA OF EXFOLIATION CORROSION. REPAIRED PER ECRA 479-53-120-2. BLENDED CORROSION, FLAP PEENED, AND INSTALLED REPAIR SPLICE. (X)SDR EIAA2000079Frame · crackedEAC-MZJ - R-5 CLOSEOUT FRAME, FORWARD OF R-5 DOOR HAD CRACK 1.50 INCHES LONG AT TOP DOOR FITTING LOCATION STA 2235R. REPAIRED PER ECRA 479-53-115-2. TRIMMED OUT CRACK, INSTALLED FILLER AND EXTERNAL DOUBLER. (X)SDR EIAA2000078Skin · damagedEAC-MZJ - STA 2598 STR 29R, TAIL JACK PAD AREA HAD SKIN PUNCTURE, INTERNAL DAMAGE. REPAIRED PER ECRA 479-53-114-2. TRIMMED OUT DAMAGE, INSTALLED A FILLER AND EXTERNAL DOUBLER, SHIMMED EXTERNAL JACK FITTING TO COMPENSATE FOR THE REPAIR AFT OF STA 2598. (X)SDR EIAA2000092Skin · damagedEAC - MZJ - C6/D CHECK - RIGHT WING NR 3 PYLON POS, LOWER WING SKIN HAD 2 EXISTING DISCREPANT HOLES COMMON TO OUTBOARD MID-SPAR. REPAIRED PER ECRA 479-57-135-2. REAMED FORWARD HOLE TO 0.4990 INCH/0.5010 INCH DIAMETER AND INSTALLED TENSION HEAD HI-LOK. REAMESDR EIA2000001Unknown · smokePANC - ON THE GROUND, WITH APU RUNNING AND NR 1 AIR CONDITIONING PACK OPERATING, AIRCRAFT FILLED UP WITH SMOKE. APU OIL ATY DROPPED. APU AUTO SHUTDOWN. DEFERRED APU AND SECURED BLEED VALVE PER DDPT 36-12. REPLACED APU, LP F53497. (M)SDR K4HA99101Pump · failedSEA - FLT 14235 - NR 1 ENGINE COMPRESSOR STALLED AT 26K, ATTEMPTED 2 RESTARTS, OIL PRESSURE 16 PSI. FOUND NR 1 ENGINE FUEL PUMP FAILED. REPLACED NR 1 FCU AND EDF PUMP. ADJUSTED AND TESTED GOOD IAW 747 MM 32-53-04. (M)SDR K4HA99087Panel · separatedFLAP PANEL ON RT WING FOUND MISSING ON POST FLIGHT (FLAP PANEL NR 7). INSPECTED L/E FLAP AREA FOUND DAMAGE TO L/E FLAP PANEL NR 19 AND I/B LEFT AND RIGHT ROTORY ACTUATORS. REPLACED NR 19 L/E FLAP PANEL ASSY PER MM 27-81-02. REMOVED AND REPLACED LEFT AND RIGSDR EIA990189Filter · contaminatedVHHH - ON DESCENT, THROUGH FL310, CREW NOTED THE SUDDEN ROLL BACK OF THE NR 3 ENGINE. ENGINE WAS RESTARTED AND FLIGHT CONTINUED. MAINTENANCE FOUND A CONTAMINATED MAIN FUEL FILTER. FILTER WAS REPLACED AND TANK SUMPED. (M)SDR P5CA9900668Skin · delaminatedRIGHT WING LEADING EDGE FIXED PANEL DELAMINATED. REPAIRED PER SRM 51-40-09.SDR P5CA9900667Skin · delaminatedLEFT HORIZONTAL STABILIZER LOWER SURFACE OF TRAILING EDGE NEAR OUTBOARD ELEVATOR FOUND DELAMINATION. REPAIRED PER SRM 51-40-09.SDR P5CA9900666Skin · delaminatedLEFT INBOARD ELEVATOR TRAILING EDGE DELAMINATED. REPAIRED PER SRM 51-40-09.SDR P5CA9900665Skin · delaminatedOUTBOARD FWD FLAP TRAILING EDGE DELAMINATED. REPAIRED PER SRM 51-40-09.SDR P5CA9900664Skin · delaminationOUTBOARD AFT FLAP LOWER SURFACE FOUND DELAMINATED. REPAIRED PER SRM 51-40-09.SDR P5CA9900663Skin · delaminatedRIGHT INBOARD MID FLAP LEADING EDGE HAS DELAMINATION. REPAIRED PER SRM 51-40-09.SDR P5CA9900662Skin · delaminatedRIGHT INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED PER SRM 51-40-09.SDR P5CA9900660Skin · delaminatedRIGHT HORIZONTAL STABILIZER NR 5 ACCESS PANEL HAS SEVERE AREAS OF DELAMINATION. REBONDED SKIN TO THE HONEYCOMB PER SRM 51-40-06.SDR P5CA9900659Skin · delaminatedLEFT HORIZONTAL STABILIZER NR 3 ACCESS PANEL 334JB DELAMINATED ON INNER SKIN. REBONDED SKIN TO HONEYCOMB PER SRM 51-10-06.SDR P5CA9900658Skin · corrodedLEVEL 1 CORROSION ON PANEL SKIN BEHIND REAR SPAR WBL 235 LEFT WING. REMOVED RIVETS AND REPAIRED CORROSION PER SRM 57-10-01.SDR P5CA9900657Skin · corrodedLEVEL 1 CORROSION ON SKIN BETWEEN STA 250-260 STR 27 AND 28 LEFT. REMOVED CORROSION PER SRM 51-10-02 AND 53-30-01.SDR P5CA9900656Skin · corrodedLEVEL 1 CORROSION FOUND ON SKIN BETWEEN STA 180-200 STR 44 RIGHT SIDE. CORROSION REMOVED PER SRM 51-10-02 AND 53-30-01.SDR P5CA9900655Skin · corrodedLEVEL 1 CORROSION FOUND ON SKIN AT STR 14 BETWEEN STA 2780 AND 2200 AND STA 2240 AND 2280 ON RIGHT SIDE. REMOVED CORROSION PER SRM 51-00-02 AND 53-30-01.SDR P5CA9900653Skin · corrodedLEVEL 1 CORROSION FOUND ON SKIN BETWEEN STA 740 AND 760 RIGHT SIDE. CLEANED AND REPAIRED PER SRM 51-10-02 AND 53-30-07.SDR EIA990250Structure · damagedHKG - DURING C/D CHECK, NR 1 PYLON HAS EVIDENCE OF OVERHEAT DAMAGE, PARTIALLY REPAIRED PREVIOUSLY. NR 1 PYLON SIDE FRAMES REPLACED AT NAC STATION 183 L/R, 210 L/R, 236 L/R, 253 L/R. STIFFENERS REPLACED NR 1 NAC STATION 221-265 LEFT, NR 2 STATION 193-221 L/R,SDR EIAA990244Spar · crackedHKG - DURIGN C/D CHECK, BS 1241 BULKHEAD FITTING AT RIGHT SIDE, CRACK FOUND OF SPAR WEB AT INBOARD FITTING LEG LOWEST BOLT HOLE. REPAIRED SPAR WEB AND FITTING PER RS-R-53-43-34090 REV B, 8110-3. (M)SDR EIA990249Frame · crackedHKG - DURING C/D CHECK, M/D L1 MED CUTOUT AFT FRAME CRACKED AT WEB AND DOUBLER AT NR 1 STOP FITTING. REPAIRED DOOR FRAME AT BS 488 PER SRM 53-10-04 FIG 92. (M)SDR EIA990248Pan · wornHKG - DURING C/D CHECK, NR 3 PYLON FORWARD STRUT CLOSURE PAN, RT REAR CORNER SKIN WORN. CLOSURE PAN TRIMMED AND REPAIRED PER RS-R-71-90-34115. (M)SDR EIA990247Spar · crackedHKG - DURING C/D CHECK, LEFT WING FOWARD SPAR, WS 670 LOWER CHORD FITTING VERTICAL LEG 2 FASTENER HOLES CRACKED. FASTENER HOLES REPAIRED PER RS-R-57-24-34095, 8110-3. (M)SDR EIA990246Frame · crackedHKG - DURING C/D CHECK, BS 1265 LEFT FRAME FOUND CRACKED AT WEB AND CHORD, AT WL 200. REPAIRED PER BOEING DRAWING 144U0053 AND RS-R-53-42-34098, 8110-3. (M)SDR EIA990245Bulkhead Ftg · crackedHKG - DURING C/D CHECK, BS 1241 BULKHEAD FITTING AT RIGHT SIDE, CRACK FOUND OF OUTBOARD FITTING LEG UPPER MOST BOLT HOLE. REPAIRED FITTING PER RS-R-53-43-34090 REV B, 8110-3. (M)SDR EIA990243Spar · crackedHKG - DURING C/D CHECK, NR 1 PYLON LOWER SPAR WEB CRACKED AT NAC 221.5 BL 0, DURING EO ACCOMPLISHMENT. REPAIRED PER SRM 54-10-03 FIG 2. (M)SDR EIA990242Stringer · crackedHKG - DURING C/D CHECK, M/D BS 1348 STRINGER 11R STRINGER END FOUND CRACKED. REPAIRED STRINGER END PER RS-R-R-53-41-34083, 8110-3. (M)SDR EIA990241Panel · disbondedHKG - DURING C/D CHECK, VERTICAL STABILIZER T/E CAVITY ACCESS PANEL 324FL FOUND DISBONDED. ACCOMPLISHED A TIME LIMITED REPAIR PER RS-R-55-10-34113. (M)SDR EIA990240Tie · crackedHKG - DURING C/D CHECK, M/D BS 940 LEFT TENSION TIE AFT CHANNEL CRACKED. CHANNEL REPAIRED PER SB 747-53-2371 FIG 3 AND TELEX EVR-HKG-99-0101ER/0092TE, 8110-3. (M)SDR EIA990239Skin · crackedHKG - DURING C/D CHECK, UPPER FUSELAGE AT BS 340, RT WINDSHIELD CUTOUT HAS A CRACK AT THE LOWER AFT CORNER. SKIN REPAIRED PER SRM 53-30-03 FIG 49. (M)SDR EIA990238Skin · crackedHKG - DURING C/D CHECK, UPPER FUSELAGE AT BS 340, LEFT WINDSHIELD CUTOUT HAS A CRACK AT THE LOWER AFT CORNER. SKIN REPAIRED PER SRM 53-30-03 FIG 49. (M)SDR EIA990237Frame · crackedHKG - DURING C/D CHECK, R1 MED CUTOUT AFT FRAME CRACKED AT FRAME WEB AND WEB DOUBLER AT NR 1 STOP FITTING. REPAIRED DOOR FRAME AT BS 488 PER SRM 53-10-04 FIG 92. (M)SDR EIA990236Frame · crackedDURING C/D CHECK, R2 MED AFT FRAME UPPER CORNER CRACKED. REPAIRED DOOR FRAME PER SRM 52-10-02 FIG 10. (M)SDR EIA990235Fitting · nickedHKG - DURING C/D CHECK, NR 4 PYLON UPPER FRONT SPAR FITTING AT STATION 225 HAS SEVERAL BAD NICKS. REPAIRED PER RS-R-54-54-34111 AND SRM 54-40-01 FIG 1, 8110-3. (M)SDR EIA990234Fitting · corrodedHKG - DURING C/D CHECK, NR 4 PYLON UPPER FRONT SPAR FITTING AT STATION 225, CORROSION FOUND IN BUSHING BORE. REPAIRED BUSHING BORE IAW SB 747-54-2164 FIG 2, INSURANCE CUT TO FINAL SIZE 2.360 INCH AND RS-R-54-34085, 8110-3. (M)SDR EIA990233Frame · crackedHKG - DURING C/D CHECK, MAIN DECK, RT BS 1265 FRAME CRACKED AT WEB AD CHORD AT WL 200. REPAIRED FRAME CHORD AND WEB PER BOEING DRAWING 144U0053 AND RS-R-53-42-34098, 8110-3. (M)
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