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 EIA2003019StrapLap repairs from STA 1770-1960 at Stringer 12R reguires an additional strap. CORRECTIVE ACTION: Installed external strap per ECRA 481-53-169-2 Rev ASDR EIA2003018StrapLap repairs from STA 1460-2180 at Stringer 19R requires an additional strap. CORRECTIVE ACTION: Install external strap per ECRA 481-53-169-2 Rev ASDR EIA2003017BeltframeCracked frame at STA 1740. Stringer 4 left. CORRECTIVE ACION: Repaired cracked frame at STA 1740 stringer 4 left per ECRA 481-53-173-2SDR EIA2003036SpliceMAIN CABIN L/H INTERIOR CORROSION ALONG SKIN LONGITUDINAL SPLICE AT STRINGER 19L, BS 1960 to 2180. CORRECTIVE ACTION: REMOVED DAMAGE, NDT & VISUAL INSPECTION, FAB'D AND INSTALLED REPAIR PER ECRA 481-53-169-2 Rev ASDR EIA2003035SpliceFUSELAGE RIGHT SIDE INTERIOR CORROSION ALONG SKIN LONGITUDINAL SPLICE AT STRINGER 19R, FROM STA 1760-2180 CORRECTIVE ACTION: REMOVED DAMAGE, NDT AREA & VISUALLY IINSPECT, FAB'D AND INSTALLED REPAIR PER ECRA 481-53-169-2 Rev ASDR EIA2003021Skin PanelImpact damage on R/H bottom of Horizontal Stab at STA 240, 30" from L/E. CORRECTIVE ACTION: Repaired damaged skin and Rib lower chord per B747 SRM 55-10-02, 55-10-03, 51-1002, 51-4--04, & ECRA 481-53-180-2SDR EIA2003020BeltframeR/H STA 1740 between Stringer 12R & 13R frame bent and gouged. CORRECTIVE ACTION: Repaired R/H STA 1740 Frame @ Sringer 12R- 13R per ECRA 481-53-176-2SDR EIA2003015Skin PanelR/H Lower fuselage at STA 400, lower lap skin has evidence of damage and corrosionCORRECTIVE ACTION: Repaired area per ECRA 481-53-182-2SDR EIA2003013Support FittingL/H Main Gear Wheel @ STA 1241 BL) to 43" WL 175" (approx) longitudinal support fitting has two double drilled holes (1 ea) in the flanges. CORRECTIVE ACTION: Complied with ECRA # 481-53-190-2 (Removed & Replaced Support Fitting)SDR EIA2003012Skin PanelImproper Fastener on lap Seam at STA. 615 and S-47R on Fuselage below FWD. Lower Cargo Compt. CORRECTIVE ACTION: Removed fastener and existing doubler, cut overlapping skin, requested NDT, fabricated, alondined, primed and installed -1 repair doubler and -2 fSDR EIA2003011Skin PanelExternal Skin Repair, at Station 1580 Stringer 35L to 36L is not per S.R.M. CORRECTIVE ACTION: Removed external skin repair, fabricated new fillers,(2 ea.) and doubler. Alodined, primed and installed per Boeing SRM 51-30-03, Page 2A-2F, and SOPM Ch. 20-41-0SDR EIA2003010StiffenerSTIFFENER CRACKED AT STA 291, LBL 10 ON TOP OF NOSE WHEEL WELL BO. CORRECTIVE ACION: INSTALLED KIT # 65B28266-5 AND SUB KIT 65B28266-6 PER E.O. 53-747-1138-91 REV C, PER S.B. B747SRM 51-30-02 PGS 1-15SDR EIA2003009Intercostal · crackedINTERCOSTAL CRACKED AT STA 291 LBL 20 ON TOP TOP OF NOSE WHEEL WELL BOX. C/A: K/H SIDE INSTALLED KIT NR 65B28266-5 AND SUB KIT NR 65B28266-6 EO 53-747-1138-91 REV C, IAW SB NR 747-53A-2293 REV 8 AND DRWG 3 62460005.SDR EIA200311Skin · damagedEXTERNAL SKIN REPAIR, AT STATION 1580 STRINGER 35L TO 36L IS NOT IAW SRM. REMOVED EXTERNAL SKIN REPAIR, FABRICATED NEW FILLERS, AND DOUBLER. ALODINED, PRIMED AND INSTALLED IAW SRM 51-30-03, PAGE 2A-2F, AND SOPM CH. 20-41-02, PAGE 17-19. CATEGORY (B) REPAIRSDR EIA200310Stiffener · crackedSTIFFENER CRACKED AT STA 291, LBL 10 ON TOP OF NOSE WHEEL WELL BOX. INSTALLED KIT NR 65B282665 AND SUB KIT 65B282666 IAW EO 53-747-1138-91 REV C, IAW SB B747, SRM 51-30-02 PGS 1-15SDR EIA2003034Door FrameBULK PIT DOOR CUT OUT HAS BENT AND GOUGED EDGE APPROXIMATELY 14 IN. UP FROM FORWARD LOWER CORNER. CORRECTIVE ACTION: REMOVED DAMAGE, NDT & VISUAL INSPECTION OF AREA, FAB'D AND INSTALLED REPAIR PER ECRA 481-53-157-2 Rev ASDR EIA2003007Skin · corrodedFS 1350 RBL4 TO LBL4 TOP SURFACE OF WING BOX PILLOWING (CORROSION). REMOVED DAMAGE, NDT AREA, FAB'D & INSTALLED REPAIR PARTS PER ECRA 481-53-165-2.SDR EIA2003014BeltframeFrame Cracked STA 340 1" below Sringer 16 left. CORRECTIVE ACTION: Repaired per ECR # 481-53-175-2SDR EIA2003008Frame · crackedFRAME CRACKED STA 340, 1 INCH BELOW STRINGER 16 LEFT. REMOVED DAMAGE, FABRICATED DOUBLER -2 DOUBLER, FILLER-4 DOUBLER, PER ECRA 481-53-1752 & 51-10-02 PG 7, SOPM PER 20-41-02 PG 10SDR EIA2003006Smoke Detector · defectiveFWD LOWER CARGO FIRE WARNING LIGHT ILLUMINATED. NR1 BOTTLE FIRED. REMAINED ILLUMINATED, VISUAL SCAN INDICATED NO FIRE. NR 1 BOTTLE DISCHARGED LIGHT DID NOT ILLUMINATE. HOWEVER SQUIB TEST INDICATED BOTTLE NR 1 (FWD) DID DISCHARGE, CARGO FIRE LIGHT WENT OUT AT 4SDR EIA2004010Module · malfunctionedEMERGENCY EXIT LIGHT DOES NOT ILLUMINATE WITH SW ON OR OFF. R&R LITE MODULE PER MM 33-51-04SDR EIA2003004Frame · crackedFUSELAGE INTERIOR RIGHT SIDE F.S. 1760 CRACK IN FRAME AT STRINGER 13 UPPER FLANGE OF FRAMECUT OUT DAMAGED SECTION FABRICATED FRAME SECTION AND REPAIR SPLICES(2EA) PER B747 SRM 51-40-06 PG. 2 SHEET 1-4, ALODINED, PRIMED AND INSTALLED REPAIR PER B747 SRM 51-30-0SDR EIA2003003Frame · crackedFRAME WEB CRACKED FS 1580 ABOVE STR. 43R. REMOVED DAMAGE, NDT AREA, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PER B747 SRM 53-10-01 FIG. 70SDR EIA2002100Relay · failedKJFK - GROUND SAFE RELAY ON LIGHT STAYED ILLUMINATED AFTER TAKEOFF, INBOARD FLAPS WOULD NOT RETRACT NORMALLY AFTER LANDING. REPLACED RELAYS, R952 AND R226 IN P14 EPR MM 32-09-02. (M)SDR EIA2002098Engine · flamed outKJFK - FOUND ENGINE NR 4 FLAMED OUT DURING DESCENT. (M)SDR EIA2002088Fuel Control · malfunctionedWHILE CRUISING AT FL 35.0, NR 1 ENGINE COMPRESSOR STALLED, N1 RPM DECREASED AND EGT INCREASED RETARDED THROTTLE. NO RESPONSE, SHUTDOWN NR 1 ENGINE. DURING WINDMILLING ATTEMPTED RESTART. EGT OUT OF LIMITS, RETURN TO ANC. REMOVED AND REPLACED NR 1 ENGINE MAISDR EIAA2002088Engine · stalledFLT 481 - PANC - WHILE CRUISING AT FL35.0, NR 1 ENGINE COMPRESSOR STALLED, N1 RPM DECREASED AND EGT INCREASED RETARDED THROTTLE NO RESPONSE, SHUTDOWN NR 1 ENGINE. DURING WINDMILLING ATTEMPTED RESTART, EGT OUT OF LIMITS, RETURN TO ANC. (M)SDR EIAA2002084Light · inoperativeJFK - R5 EMERGENCY DOOR FLOOD LIGHT INOPERATIVE. FOUND BAD LIGHT ASSEMBLY, REPLACED LIGHT ASSEMBLY IAW MM 33-52-00. (M)SDR EIA2002062Fan · malfunctionedNR 2 RECIRCULATION FANS MAKE WHINING NOISE AND SMELLS OF HOT ELECTRIC FUMES. REMOVED AND REPLACED NR 2 RECIRCULATION FAN AS PER MM.SDR 200200243Support Fitting · crackedLEFT WING WBL 235, UPPER TRAILING EDGE PANEL SUPPORT TEE CRACKED ABOVE NR 4 FLAP TRACK. REMOVED CRACKED SUPPORT FITTING AND INSTALLED NEW FITTING PER B747 SRM 51-30-02, 51-30-05, 51-30-04 AND SOPM 20-41-02.SDR 200200242Shear Tie · corrodedCORROSION FOUND ON SHEAR TIE AT BOTTOM OF FRAME AT STA 2200 AT LEFT OUTFLOW VALVE. REMOVED OLD SHEAR TIE FABRICATED NEW AND INSTALLED AS PER B747 SRM 51-30-02, SRM 51-20-01 AND SRM 51-30-05.SDR 200200241Skin · corrodedLAP SEAM AT STA 930 TO 950 STR 8 LEFT HAS SURFACE CORROSION AND SKIN EXFOLIATED. OPENED LAP, REMOVED CORROSION, REPAIRED AREA AND CLOSED LAP PER B747 SRM.SDR 200200234Bulkhead · crackedBS1480 BULKHEAD AND SPLICE COMPONENT INSPECTION/ REPAIR/ MODIFICATION. THIS EO PERFORMS THE (PLAN B) INSPECTION AND MODIFICATION AS OUTLINED IN SB, INCLUDED ARE INSTRUCTIONS FOR INSPECTION, REPAIR AND MODIFICATION WORK ON THE SKIN, BULKHEAD AND COMPONENTS THATSDR 200200233Balance Weight · chippedLEFT HAND HORIZONTAL STABILIZER ELEVATOR BALANCE WEIGHTS FROM STA. 206.8 - 331.8 HAS CHIPPED PAINT UPPER AND LOWER SURFACES. REMOVED LOOSE AND FLAKING PAINT ON LEFT HORIZONAL STABILIZER BALANCE WEIGHTS AND PRIMED.SDR 200200232Angle · crackedLT HORIZONTAL STAB INBOARD LEADING EDGE FAIRING HAS AN (L) ANGLE CRACKED 3RD RIB FROM INBOARD END. REMOVED (L) ANGLE CRACKED, ORIGINAL MATERIAL 7075 PER CHEMICAL TEST 747 SRM 51-10-01 AND .030 PER CALIPER NR 99-0043 DUE DATE 04-02. FABRICATED (C) ANGLE FROM 70SDR 200200231Bracket · brokenNR 6 FLAP TRACK TRANSMITTER POSITION CABLE PULLEY SUPPORT BRACKET LUG BROKEN OUTBOARD SIDE. REMOVED AND REPLACED SUPPORT BRACKET ON NR 6 FLAP TRACK TRANSMITTER POSITION CABLE PULLEY BRACKET REF. B747 MM.SDR 200200230Mount · corrodedNR 8 FLAP TRACK I/B MOUNT HAS PITTING CORROSION ON FACE OF MOUNT AND BOLT HOLE. REPLACED NR 8 FLAP TRACK I/B SIDE LOAD FITTING PER B747 MM 27-51-27.SDR 200200229Pin · corrodedNR 5, 6, 7, 8 FLAP TRACK FWD FUSE PINS HAVE PITTING CORROSION ON INTERIOR OF PINS. REPLACED NR 5, 6, 7, 8 FLAP TRACK FWD FUSE PINS PER 747 MM CHAP 27-51-27, 25, 22.SDR 200200228Pin · corrodedNR 1, 2, 3, 4, FLAP TRACK FWD FUSE PINS HAVE PITTING CORROSION ON INTERIOR OF PINS. REPLACED 1, 2, 3, 4 FLAP TRACK FWD FUSE PINS PER B747 MM CHAP 27-51-22, 25, 27.SDR 200200227Fitting · crackedSTA 2484 LEFT LOWER BULKHEAD SPLICE FITTING AT S-23 CRACKED FROM LWR INBOARD FASTENER. REMOVED AND REPLACED FITTING PER SERVICE BULLETIN 53-2162 AND 05-0323 STEPS 5 & 6.SDR 200200226Spacer · corrodedCORROSION ON SPACER TO FITTING AT NR 5 FLAP TRACK ON WALKING BEAM AFT ATTACH FITTING. REMOVED AND REINSTALLED FITTING AT NR 5 FLAP TRACK WITH NEW SHIM AND HARDWARE PER 747 20-51-01.SDR 200200225Balance Weight · corrodedLEFT HAND HORIZONTAL STAB ELEVATOR WEIGHT APPROX STA 281.3 - 306.8 HAS CORROSION. REMOVED AND REPLACED LEFT HAND HORIZ STAB ELEVATOR WEIGHT AT STA 260-268 PER B747 OHM 55-20-21.SDR 200200224Attach Fitting · corrodedPITTING CORROSION ON ATTACH FITTING BELOW BRONZE SHIM/SPACER ON NR 6 FLAP TRACK INBOARD ATTACH FITTING. REMOVED AND REPLACED ATTACH FITTING WITH SHIM PER 747 MM 27-51-25.SDR 200200223Attach Fitting · corrodedPITTING CORROSION ON ATTACH FITTING BELOW BRONZE SHIM/SPACER ON NR 6 FLAP TRACK OUTBOARD ATTACH FITTING. REPLACED ATTACH FITTING PER 747 MM 27-51-27.SDR 200200222Attach Fitting · corrodedPITTING CORROSION ON NR 1 FLAP TRACK OUTBOARD ATTACH FITTING. REPLACED NR 1 TRACK OUTBOARD ATTACH (SIDELOAD) FITTING PER 747 MM 27-51-27.SDR 200200221Attach Fitting · corrodedPITTING CORROSION ON NR 1 FLAP TRACK INBOARD ATTACH FITTING. REPLACED NR 1 TRACK INBOARD SIDE LOAD FITTING PER 747 MM 27-51-27.SDR 200200220Attach Fitting · corrodedNR 3 FLAP TRACK ATTACHMENT FITTINGS BOTH INBOARD AND OUTBOARD CORRODED (PITTED). REMOVED AND REPLACED NR 3 TRACK ATTACH FITTINGS PER 747 MM 27-51-25.SDR 200200219Seat Track · corrodedMAIN DECK AT STA 1000 RBL 33 HAS A CORRODED SEAT TRACK FLANGE I/B SIDE. REPAIRED PER SRM 53-10-5 FIG 1A.SDR 200200218Tie Clip · crackedSTRINGER TIE-CLIP DAMAGED -TWO SMALL CRACKS AT STA 1660 AND S-12 RIGHT. INSTALLED TIE-CLIP B747 SRM 51-30-02.SDR 200200217Angle · crackedMAIN DECK AT STA 340, STR 26R FLOORBOARD SUPPORT ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED REPAIR PARTS PER B747 SRM 51-40-04, 51-10-01, 51-30-05, 51-10-02 AND B747 SOPM 20-41-02.
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