Boeing 747-122
Service difficulty reports · 2,143
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 = '747122' 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 = '747122' 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 P5CA0200684Actuator · failed#1 CROSSFEED VALVE FAILED CLOSED DURING FLIGHT. RETURNED TO JFK PER MOD LGB. FUEL DUMP ACCOMPLISHED DUE TO AIR TURN-BACK. MX CTL NOTIFIED. REMOVED & REPLACED #1 CROSSFEED VALVE ACTUATOR IAW MM 28-22-02. OPS CHECKED NORMAL.SDR P5CA0200670Inverter · failedWHEN MICROWAVE WAS TURNED ON, GALLEY INVERTER FAILED & SMELLED ELECTRICAL FUMES. REMOVED CANNON PLUG FROM GALLEY STATIC INVERTER. NO POWER TO GALLEY. TRANSFERED TO O.I.L. #61919 PER MX CTRL DAVID.SDR P5CA0200667Panel · delaminatedDELAMINATION FOUND ON RH MLG WING DOOR INBRD PANEL #723. DELAMINATED DOUBLER REPLACED REF SRM 51-40-05SDR P5CA00200666Skin · crackedCRACK FOUND IN BODY TAIL LOWER SKIN AT STATION 2280. CRACK CUT OUT, PACKER FITTED & NEW REPAIR DONE ON OUTER SKIN AS PER SRM 53-30-03.SDR P5CA0200665Firewall · crackedCRACK ON CLOSURE BULKHEAD FIREWALL, NR 3 PYLON UNDER SLOT SEAL AREA. CRACK RUNS VERTICALLY APPROX 5 INCHES THEN SPLITS TO INBOARD SIDE. REPAIR CARRIED OUT REF SRM 54-10-03. CRACK STOP DRILLED PER SRM 51-10-01.SDR P5CA0200664Bolt · shearedONE BOLT HEAD SHEARED OFF ON RT SIDE OF NR 1 ENGINE AFT MOUNT TO PYLON FITTING. REMOVED AND REPLACED TWO BOLTS ON RT SIDE FOR AFT MOUNT TO FITTING PER MM 54-41-02.SDR P5CA0200663Valve · bindingDURING REFUELING, NR 1 RESERVE VALVE FAILED TO OPEN AND UNABLE TO PUT FUEL INTO NR 1 RESERVE TANK. FOUND EXCESSIVE SHAFT BINDING THAT WOULD ONLY ALLOW PARTIAL OPENING OF THE VALVE. FUELED TANK, MANUALLY CLOSED VALVE. AFTER REFUELING, NR 2 MAIN TANK READ 38.SDR P5CA0200661Computer · faultyINS SELECTED IN DUAL, CAPT'S FLT DIRECTOR HEAD FOLLOWS HEADING BUG. F/O'S SIDE OPS NORMAL. SWAP ROLL COMPUTERS A & B. GROUND OPS CHECK OK.SDR P5CA0200660Computer · faultyWITH AUTO PILOT "A" OR "B" ENGAGED, ALTITUDE ALERT HORN & LIGHT CONTINUALLY CHIME IN LEVEL FLIGHT AFTER CLIMB TO FL 34.0 (WAS O.K. AT FL 32.0 & FL 33.0) REMOVED & REPLACED ALT ALERT WARNING COMPUTER IAW MM 31-16-00. OPS CHK GOOD.SDR P5CA0200656Wire · brokenON T/O ROLL, AS SOON AS POWER WAS ADVANCE, TAKE-OFF WARNING CAME ON. (ALL PARAMETERS NRML FOR T/O). RETURNED TO BLOCKS. FOUND BROKEN WIRE FOR SWITCH #334 POWER. REPAIRED WIRING BTWN LWR FIRE DISCONNECT & SWITCH S334 PER BMM CH 20. PERFORMED OPS TEST. CHKD GOODSDR P5CA0200657Warning System · malfunctionedWHEN READY FOR T/O, TAKEOFF WARNING HORN SOUNDED. ALL T/O CONDITIONS SATISFACTORY. CYCLED ALL CONTROL SURFACES SEVERAL TIMES, CYCLED FLAPS FULL TRAVEL, EXERCISED HORIZONTAL STAB LIMIT SWITCHES, PERFORMED OPS CHECK. ALL OPS CHECKS NORMAL ON GROUND.SDR P5CA0200652Switch · faultyREF DMI 28874 / MEL 27-9 : AUTOSPOILER BRAKE DID NOT DEPLOY ON LANDING. TROUBLESHOT & FOUND THROTTLE SWITCH S860 AT FAULT. REPLACED SAME & OPS CHKD OK PER MM 27-62-00. THIS CLEARS DMI 28874 / MEL 27-9. PLACARDS REMOVED.SDR P5CA0200638Compressor · failedWHILE CLIMBING, NR 3 FAILED WITH LOUD BANG AND VIBRATION. EPR DECREASED RAPIDLY AND EGT INCREASED TO APPROX 910. PERFORMED ENG FIRE/SEVERE DAMAGE CHECKLIST. SECURED ENGINE WITH ENGINE SHUTDOWN CHECKLIST. EMERGENCY DECLARED; DIVERTED TO SIN - CHANGI AIRPORTSDR P5CA0200630Actuator · failedRUDDER PEDAL STEERING INOPERATIVE ON TAKEOFF ROLL. TILLER OK. TURNED BACK TO BLOCKS FOR MAINTENANCE. REMOVED AND REPLACED RUDDER PEDAL STEERING ACTUATOR PER MM 32-51-07 PG 401 THROUGH 403. OPS NOW OK.SDR P5CA0100617Web · crackedNOSE WHEEL WELL VERTICAL BEAM INSPECTION IAW MA A5310-33:01 REVEALED A CRACK 1-3/8" LONG AT WEB TO CHORD FASTENER LOCATION AT VERTICAL BEAM STN 320 R/H SIDE, WEB 2. REPAIRED IAW SRM 51-40-02, PAGE 5, DETAIL 111.SDR P5CA0100616Web · crackedNOSE WHEEL WELL VERTICAL BEAM INSPECTION IAW MA A5310-33:01 REVEALED A CRACK AT STANDOFF HOLE 2-3/8" LONG AT VERTICAL BEAM STN 320 R/H SIDE, WEB 2. CRACK REPAIRED IAW SRM 51-40-02, PAGE5, DETAIL 111.SDR P5CA0100614Aileron · delaminatedR/H OUTBD AILERON TOP CENTER HONEYCOMB PANEL TOP SKIN DELAMINATED 5' FROM I/B END, APPROX. 15" DIA. REMOVED & REPLACED R/H OUTBD AILERON PER MM 27-11-02SDR P5CA0100602Wire · chafedFWD LOWER CARGO DOOR ANNUNCIATOR LIGHT ILLUMINATED WHEN LEVELING FL350. FWD ANNUNCIATOR CARGO DOOR LIGHT ON GLARESHIELD WAS ILLUMINATED. LIGHT EXTINGUISHED WHEN DESCENDING THROUGH FL270 AT 6.0 PSI DIFFERENTIAL CABIN. FOUND CHAFED WIRE AT FWD CARGO DOOR JUNCSDR P5CA0100590Engine · malfunctionedDURING CLIMBOUT NR 3 ENGINE FIRE LIGHT CAME ON WITH FIRE LOOPS BOTH AT 9 ALSO STARTER VALVE OPEN LIGHT. ZERO OIL QTY CSD OIL AND RISE IN TEMP READING. ZERO N2 RPM AND N1 14 PERCENT. RAN ENG FIRE CHECK LIST BOTH LIGHTS STAYED ON. ENGINE REMOVED AND REPLACEDSDR 0100570Panel · delaminatedLT WING PANEL AT L/E 4TH PANEL FROM FUSELAGE DELAMINATED. REMOVED AND REPLACED LT WING PANEL L/E 4TH FORM FUSELAGE AS PER SRM 51-30-02.SDR P5CA0100568Control Unit · failedWHEN COMPLYING WITH FCD 35-10, O2 DOOR AND MASK FAILED TO DEPLOY. REMOVED AND REPLACED FLOW CONTROL UNIT SYSTEM OPS CHECK NORMAL P/N ON 800802-01 ON 0444, P/N OFF 800802-01 S/N OFF 761.SDR P5CA0100529Panel · delaminatedRT WING PANEL BEHIND NR 2 INBOARD SPOILER FIBERGLASS COMING LOOSE. FIBERGLASS PANEL REPAIRED PER SRM 51-40-08.SDR P5CA0100528Panel · delaminatedRT WING PANEL BEHIND NR 1 INBOARD SPOILER WBL 264 FIBERGLASS COWLING LOOSE. FIBERGLASS PANEL REPAIRED AS PER SRM 51-40-08.SDR P5CA0100527Fairing · damagedDAMAGE FOUND ON NR 6 CANOE FIXED FAIRING WBL 353. FAIRING REPAIRED PER SRM 51-40-08.SDR P5CA0100526Fairing · damagedDAMAGE FOUND ON FIX FAIRING IN FRONT OF NR 6 CANOE. FAIRING REPAIRED PER SRM 51-40-08.SDR P5CA0100525Skin · delaminatedDELAMINATION FOUND ON RT WING INBOARD LOWER FLAP WBL 163. REPAIRED PER SRM 51-40-08.SDR P5CA0100524Panel · delaminatedLT WING PANEL WBL 461 OF INBOARD AILERON HAS LOOSE FIBERGLASS. REPAIR CARRIED OUT IAW SRM 51-40-08.SDR P5CA0100532Panel · delaminatedLT WING PANEL THAT IS BEHIND FLYING PANEL HAS FIBERGLASS COMING LOOSE STA 197. REPAIRED CARREID OUT IAW SRM 51-40-08.SDR P5CA0100531Panel · delaminatedLT PANEL DIRECTLY BEHIND FLYING PANEL LT WING WBL 197 HAS LOOSE FIBERGLASS. REPARIED CARRIED OUT IAW SRM 51-40-08.SDR P5CA0100530Panel · delaminatedLT WING PANEL ON L/EDGE OF FUSELAGE WBL 150 HAS LOOSE FIBERGLASS. REPAIRED CARRIED OUT PER SRM 51-40-08.SDR P5CA0100482Bearing · damagedDAMAGE FOUND ON NR 2 ENG LT TANGENTIAL BEARING. REPLACED TANGENTIAL LINK AND BEARING PER MM 71-21-04 ITEM 13.SDR P5CA0100467Skin · delaminatedDELAMINATION FOUND ON LEFT O/B MID FLAP. REPAIRED PER PAO-LGB01-00045F.SDR P5CA0200631Light · defectiveEMERGENCY LIGHT IN CEILING AFT OF P6 PANEL ILLUMINATES ONLY MOMENTARILY. REPLACED EMERGENCY LIGHT AFT OF P6. OPS CHECK OK.SDR P5CA0000324Skin · corrodedLEVEL 1 CORROSION FOUND ON NR 7 SPOILER. BOND REPAIR PER SRM 51-40-06.SDR P5CA0000323Skin · delaminatedDELAMINATION FOUND ON NR 1 SPOILER. REPAIRED PER SRM 51-40-06.SDR P5CA0000322Structure · crackedCRACK FOUND ON RBJ - I/B W/W DOOR INBOARD EDGE. REPAIRED PER SRM 51-10-01 & 51-30-02.SDR P5CA0000321Skin · delaminatedDELAMINATION FOUND ON L/WING INBOARD T/E FLAP AFT FLAP UPPER SURFACE WBL-236. REPAIRED PER SRM 51-40-26.SDR P5CA0000216Fastener · missingNR 3 ENG STRUT TO DIAGONAL BRACE ATTACH FITTING ON FORWARD SIDE, ONE FASTENER MISSING AND SOME FOUND LOOSE. DETAILED VISUAL INSPECTION CARRIED OUT AND MISSING AND LOOSE FASTENERS REPLACED. NDT PERFORMED AND CONFIRMED NO CRACKS PER BOEING SB 747-54-2186.SDR P5CA0000207Bolt · shearedON PYLONS NR 1, 3 AND 4, SHEARED .375 BOLTS ON HORIZONTAL FIRE WALL ADJACENT TO THE AFT MOUNT LUGS. BOLTS ARE VERTICAL THROUGH AFT MOUNT FITTING AND LOWER PYLON SKIRT CHORDS. REMOVED AND REPLACED ALL 8 BOLTS PER PYLON. REPLACED WITH OVERSIZED TO .4375 PER BSDR P5CA0000215Wire · brokenRIGHT UPPER DECK EMERGENCY LIGHT ADJACENT TO CREW EXIT LIGHT INOP. REPAIRED BROKEN WIRE. OPS CHECK GOOD IAW 20-10-13.SDR P5CA0000199Skin · puncturedA/C DAMAGED BY GROUND HANDLER AT STA 1780, LT SIDE WL 130 BS 1788 STRINGER 35 LEFT TO STRINGER 36 LEFT EXTERIOR SKIN PUNCTURED. REMOVED AFT CARGO LINER AT BS 1780, REMOVED DAMAGED SKIN, INSTALLED DOUBLER PER SRM 53-30-03 FIG 1, INSTALLED AFT CARGO LINER.SDR P5CA0000196Fitting · crackedON TAKEOFF AT CTS, ACFT HAD STRONG VIBRATION IN AIRFRAME UNTIL FLAPS REACHED FLAPS ONE POSITION. PERFORMED COMPLETE INSPECTION OF AIR WINGS TAIL AND FUSELAGE. FOUND CRACKED FITTING LT FORE FLAP ATTACH 11B. ALSO, FOUND LT FORE AND MID FLAP SEAL DAMAGED. REPSDR P5CA0000195Torque Tube · damagedLEFT ENTRY DOOR LIGHT DR1 CAME ON DURING DESCENT AND REMAINED ON. DR1 LIGHT CAME ON AT APPROX 2.4 PSI DIF PRESS. REMOVED AND REPLACED LOWER TORQUE TUBE ASSY, PER MM 52-11-00, ADJUSTED DOOR WARNING LIGHT PER MM 52-17-00. OPS CHECK OK ON GROUND.SDR 20000530SH001Light · will not testON GROUND, N1 LIGHT IN FORWARD P-2 PANEL WILL NOT TEST. TROUBLESHOOTING CARRIED OUT PER PAC WDM 77-12-11 AND WDM 33-11-01. COMPONENTS CHECKED AND REFITTED. DEFECT SELF-RECTIFIED. OPS CHECK SATISFACTORY. (X)SDR P5CA0000183Actuator · failedLT WING GEAR ALT ROTARY ACTUATOR (MOTOR) FAILED FUNCTIONAL CHECK. LT WING ROTARY ACTUATOR (ALT) REPLACED PER MM 32-35-01.SDR P5CA0000182Skin · damagedLEFT WING FIXED T/E UPPER PANEL REMOVED DUE TO WATER CONTAMINATION. REPAIRED AND REPLACED PER SRM 51-40-12, 51-40-09 & 57-22-01.SDR P5CA0000181Frame · crackedSTA 940 FRAME CRACKED AROUND STRINGER 34R AND VERTICAL POST. FRAME REPAIRED PER SRM 53-10-04 FIG 52.SDR P5CA0000104Skin · dentedLEFT HORIZ STAB L/E SKIN DENT 4 LOCATIONS STAB STA L/E 165, 235, 3335 AND 385. SMOOTH OUT DENTS AND NDT CKD OK PER NDT DT-6, MM 51-00-00 SRM 51-10-01.SDR P5CA0000103Keel Beam · corrodedAT BS 987 BOTTOM CENTER KEEL BEAM PANEL FOUND SURFACE CORROSION (PANEL 191GG). LEVEL 1 CORROSION REMOVED PER SRM 51-10-02.SDR P5CA0000102Flange · crackedENG NR 3 R AND S FLANGES RADIAL CRACKS. CRACK WELDED AND CK W FLOURESCENT LIGHT OK. REPAIRED PER MM 42-53-01..
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