Boeing 747 212B

Service difficulty reports · 2,202

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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 = '747212B'
  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.

SDR UIEA01024Skin · wornDURING ROUTINE INSPECTION, FOUND NR 3 PYLON SKIN WORN AT NAC STATION 290 WL 145 R/S ACCESS PANEL. TRIMMED OUT WORN AREA. FABRICATED FILLER FROM CRES STEEL 301.5 HARD AND ALUMINUM DOUBLER. INSTALLED PER STANDARD PRACTICES. (M)Mar 9, 2000 · N808MC · Boeing 747212B · Nacelle/Pylon, Plate/SkinSDR UIEA01023Flap Track · corrodedDURING ROUTINE INSPECTION, FOUND NR 6 INBOARD FLAP TRACK REAR SPAR FORWARD AFT ATTACH HOLES CORRODED. CORROSION REMOVED BY MILLING FLANGE THICKNESS TO .8799 AT THE FORWARD HOLES; .8630 AT THE AFT HOLES. FABRICATED NEW BEARING PLATES. REWORK AREA TREATED, PAMar 9, 2000 · N808MC · Boeing 747212B · Trailing Edge FlapsSDR UIEA01022Frame · dentedDURING ROUTINE INSPECTION, FOUND FRAME DENTED AT STATION 1860 STRINGER 12 AND 13R. TRIMMED AWAY DAMAGE. FABRICATED REPAIR DOUBLER, FILLERS AND SHEAR TIE. INSTALLED PER STANDARD PRACTICES. (M)Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, FrameSDR UIEA01021Frame · dentedDURING ROUTINE INSPECTION, FOUND FRAME DENTED AT STATION 1840 STRINGER 12 AND 13R. TRIMMED AWAY DAMAGE. FABRICATED REPAIR DOUBLERS, FILLERS AND SHEAR TIE. INSTALLED PER STANDARD PRACTICES. (M)Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, FrameSDR UIEA01020Frame · dentedDURING ROUTINE INSPECTION, FOUND FRAME DENTED AT STATION 1820 STRINGER 12R. TRIMMED AWAY DAMAGE. FABRICATED REPAIR DOUBLERS, FILLERS AND SHEAR TIE. INSTALLED PER STANDARD PRACTICES. (M)Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, FrameSDR UIEA01019Frame · dentedDURING ROUTINE INSPECTION, FOUND FRAME DENTED AT STATION 1760 STRINGER 13R. TRIMMED AWAY DAMAGE. FABRICATED REPAIR DOUBLERS, FILLERS AND SHEAR TIE. INSTALLED PER STANDARD PRACTICES. (M)Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, FrameSDR UIEA01018Frame · dentedDURING ROUTINE INSPECTION, FOUND OUTER CHORD DAMAGED/DENTED AT BS 1680 STRINGER 15R. TRIMMED AWAY DAMAGE. MANUFACTURED FILLER, REPAIR DOUBLER AND STRAPS. INSTALLED IAW SRM 53-10-04. (M)Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, FrameSDR UIEA01017Seat Track · scratchedDURING ROUTINE INSPECTION, FOUND SEAT TRACK GOUGED/SCRATCHED AT LBL 75.92 BETWEEN STATION 1320 AND 1460. ALL AREAS BLENDED PER SRM 51-10-01. HFEC INSPECTION PERFORMED. ALL WITHIN LIMITS PER SRM 53-10-01. AT STATION 1450 SEAT TRACK LUGS AFTER BLENDING WERE Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage, Seat/Cargo Attach FittingsSDR UIEA01016Seat Track · scratchedDURING ROUTINE INSPECTION, FOUND SEAT TRACK GOUGED/SCRATCHED AT LBL 98.58 BETWEEN STATION 1030 AND 1135. ALL AREAS BLENDED PER SRM 51-10-01. HFEC INSPECTION PERFORMED. ALL FOUND WITHIN LIMITS PER SRM 53-10-01. FOUND SEAT TRACK LBL 75.92 GOUGED/SCRATCHED ATMar 9, 2000 · N808MC · Boeing 747212B · Fuselage, Seat/Cargo Attach FittingsSDR UIEA01015Skin · corrodedDURING ROUTINE INSPECTION, FOUND UPPER WING SKIN CORRODED AT BS 1140, FROM RBL 57 TO RBL 98. REMOVED CORROSION PER SRM 51-10-01, FOUND AREAS FROM RBL 57-87 WITHIN LIMITS PER 57-30-01. AREA FROM RBL 88 TO 98 WAS BLENDED PER REPAIR INSTRUCTIONS, FASTENERS REMOMar 9, 2000 · N808MC · Boeing 747212B · Wing, Plate/SkinSDR UIEA01014Frame · crackedDURING ROUTINE INSPECTION, FOUND FRAME WEB CRACKED AT STATION 360 R/S STRINGER 23R CUT OUT. ROUTED CRACKED AREA OF WEB. MANUFACTURED REPAIR DOUBLER AND FILLERS. INSTALLED IAW 747-53A2265 WITH OVERSIZED RIVETS BACR15BB6D. (M)Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, FrameSDR UIEA01013Frame · crackedDURING ROUTINE INSPECTION, FOUND FRAME WEB CRACKED AT STATION 360 R/S STRINGER 15 AND 16R. TRIMMED DAMAGE AREA OF WEB. MANUFACTURED REPAIR ANGLES, FILLERS, STRAPS. INSTALLED PER STANDARD PRACTICES USING BACB30MY6K FASTENERS AND BACC30M COLLARS. (M)Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, FrameSDR UIEA01012Shear Tie · crackedDURING ROUTINE INSPECTION, FOUN FRAME SHEAR TIE CRACKED IN RADIUS BETWEEN STATION 340-360 R/S AT MAIN DECK LEVEL (WBL200). TRIMMED DAMAGE AREA. MANUFACTURED REPAIR ANGLES AND FILLER. INSTALLED PER STANDARD PRACTICES WITH RIVETS BACR15BB5AD. (M)Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, StructureSDR UPS00432187Frame · crackedINSPECTION TYPE: C, CRACK FOUND REPAIRED I.A.W QUERY NOTE N522UP/11/2000.NOTE THIS REPAIR IS SUBJECT TO A REPEAT INSPECTION.Mar 8, 2000 · N522UP · Boeing 747212B · Fuselage Main, FrameSDR UPS00432191Spar · corrodedINSPECTION TYPE: C, RT WING FRONT SPAR. CORROSION ON FRONT SPAR AT ILES 427. REPAIRED ACCOMPLISHED I.A.W QUERY NOTE N522UP/15/2000,AND APPROVED 8 110-3.Mar 7, 2000 · N522UP · Boeing 747212B · Wing SparSDR UPS00431930Spar · corrodedINSPECTION TYPE: C, RT WING LEADING EDGE. CORROSION ON FRONT SPAR OF LT WING AT ILES 621. REPAIRED IAW QUERY NOTE N522UP/08/2000, AND APPROVED 8110-3Mar 4, 2000 · N522UP · Boeing 747212B · Wing SparSDR UPS00432193Rib · corrodedINSPECTION TYPE: C, RT WING LEADING EDGE, CORROSION ON LE RIB AT OLES 1543 RT O/B SIDE. NEW RIB FABRICATED AND INSTALLED I.A.W SRM 51-30-02.REF WORK SHOP OR DER E0098342.Mar 4, 2000 · N522UP · Boeing 747212B · Wing, Rib/BulkheadSDR UPS00432186Spar · corrodedINSPECTION TYPE: C, LT WING LEADING EDGE. CORROSION ON FRONT SPAR OF LT WING WEB BETWEEN OLES 1543 AND OLES 1562.Mar 4, 2000 · N522UP · Boeing 747212B · Wing SparSDR UPS00432194Spar · corrodedINSPECTION TYPE: C, RT WING LEADING EDGE. CORROSION ON RT FRONT SPAR WEB AT OLES 1418-1446. REPAIRED I.A.W QUERY NOTE N522UP/10/2000,AND APPROVED 8110-3.Mar 1, 2000 · N522UP · Boeing 747212B · Wing SparSDR UPS00432192Spar · corrodedINSPECTION TYPE: C, RT WING FRONT SPAR. CORROSION ON RT UPPER SPAR SKIN EXTENSION, AT OLES 1395. CORROSION REMOVED I.A.W SRM 51-10-01 AND REPROTECTED I.A.W SRM51-10- 02.REF NRC 44255054 FOR NDT INSPECTION.Mar 1, 2000 · N522UP · Boeing 747212B · Wing SparSDR UPS00432183Shear Tie · corrodedINSPECTION TYPE: C, REAR CARGO HOLD. LIGHT CORROSION AT BS 2160 BETWEEN STRINGERS 43 AND 51 RT. (1) REMOVE CORROSION (2) EVALUATE (3) REPROTECT SHEAR TIE SECTION FROM STRS 43 LT TO 51 RT REPLACED I.A.W 51-30-02 AND 53-10-04.Mar 1, 2000 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS00432181Shear Tie · corrodedINSPECTION TYPE: C, IN REAR CARGO HOLD CORRODED AND SHEARED FASTENER ON SHEAR TIE AT BS .2160 BETWEEN STRINGERS 47 - 48 RT. CARRY OUT REPAIR. SHERE TIES FABRICATED I.A.W WORK ORDERS E0097634 & E0097646 INSTALLED I.A.W SRM 53-10-04.Mar 1, 2000 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS00432180Skin · corrodedINSPECTION TYPE: C, AFT UNDER FLOOR LIGHT CORRODED ON FUSELAGE INNER SKIN AT BS.2180 - 2200 BETWEEN STRINGERS 48 -49 LT AND 49-50 LT. (1) REMOVE CORROSION (2) EVALUATE (3)REPROTECT REF.NON ROUTINE CARD 44256 585 FOR ACCESS UNDER TANK.REPAIRED I.A.W Q UERMar 1, 2000 · N522UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS00432145Floor Support · corrodedINSPECTION TYPE: C 44. AFT CARGO HOLD.EXTENSIVE SURFACE CORROSION ON BULK CARGO HOLD FLOOR SUPPORTS AT HOLES AND AT ATTACHMENT TO INNER CHORD OF FLOORBEAMS. (1) REMOVE CORROSION (2) EVALUATE (3) REPROTECT. CORROSION REMOVED AND REPROTECTED I.A.W SRM 51-10-Mar 1, 2000 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS00432182Shear Tie · corrodedINSPECTION TYPE:C 44. AFT CARGO HOLD SHEAR TIE IS BADLY CORRODED AT BS 2160 BETWEEN STR.45-46 LT. CARRY OUT REPAIR. SHEAR TIE FABRICATED AND REPLACED IAW SRM 53-10-04. REF WORK ORDER E0097646.Feb 29, 2000 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS00432141Cargo Track · damagedINSPECTION TYPE:C 44 AFT CARGO HOLD BULK CARGO HOLD SUPPORT IS DAMAGED AT BS 1980 RBL 9. CARRY OUT REPAIR. SUPPORT REPLACED IAW SRM 51-40-03, CORROSION REMOVED IAW 51-10-0 2, REPROTECTED IAW SRM 51-10-01.Feb 29, 2000 · N522UP · Boeing 747212B · Fuselage, Seat/Cargo Attach FittingsSDR UPS00432105Floor Support · crackedINSPECTION TYPE:C 44 AFT CARGO HOLD BULK CARGO HOLD FLOOR SUPPORT IS CRACKED AT BS 202 0 RBL 39. CARRY OUT REPAIR. SUPPORT REPLACED IAW SRM 51-40-03. CORROSION REMOVED AND REPROTECTED IAW 51-10-01, 51-10-02.Feb 29, 2000 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS00432103Floor Support · crackedINSPECTION TYPE:C, AFT CARGO HOLD BULK CARGO HOLD FLOOR SUPPORT IS CRACKED AT BS 1975, 2060 AND 2080 RBL 9. CARRY OUT REPAIR. SUPPORT REPLACED IAW SRM 51-30-02 AND 51-40-03. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-10-01. FASTENERS REMOVEDFeb 29, 2000 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS00432102Floor Support · crackedINSPECTION TYPE:C 44. AFT CARGO HOLD BULK CARGO HOLD FLOOR SUPPORT IS CRACKED AT BS 202 0, 2024 AND 2026 RBL 9. CARRY OUT REPAIR/REPLACEMENT. SUPPORT REPLACED IAW SRM 51-40-03. CORROSION REMOVED IAW SRM 51-10-02, REPROTECTED TREATED IAW SRM 51-30-01. FASTEFeb 29, 2000 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS00432041Stringer · damagedINSPECTION TYPE:C 44. LOWER SECTION 41 STR 39 RIGHT HAND IS DAMAGED AT BS 280, CARRY OUT REPAIR. STRINGER REPLACED IAW SRM 51-30-02.Feb 29, 2000 · N522UP · Boeing 747212B · Fuselage Main, Longeron/StringerSDR UPS00432146Skin · damagedINSPECTION TYPE:C 44. DAMAGE TO L/E OF UPPER RUDDER JUST BELOW PCU (LHS), PLEASE INVESTIGATE. NEW SKIN PANEL FABRICATED IAW E0097709 AND INSTALLED IAW SRM 51-30-02.Feb 26, 2000 · N522UP · Boeing 747212B · Rudder, Plate/SkinSDR UPS00432185Web · corrodedINSPECTION TYPE:C 44. RT WING L/E CORROSION ON FRONT SPAR WEB AT SEVERAL LOCATIONS BETWEEN OLES 1200 AND OLES 1300 RT. PLEASE INVESTIGATE / RECTIFY. REPAIRED IAW QUERY NOTE N522UP/9/2000 AND APPROVED 8110-3.Feb 24, 2000 · N522UP · Boeing 747212B · Wing Miscellaneous StructureSDR UPS00432179Skin · corrodedINSPECTION TYPE:C 44. LEFT HAND WING LEADING EDGE CORROSION ON LT LWR INSPAR SKIN EXTENSION AT OLES 1328. REMOVED CORROSION AND REPROTECT AREA. REPAIRED IAW QUERY NOTE N522UP/7/2000 AND APPROVED 8110-3 DATED 29TH OF MARCH 2000.Feb 23, 2000 · N522UP · Boeing 747212B · Wing, Plate/SkinSDR TWRA0019Structure · damagedFORWARD CARGO DOOR CLOSED SIDEWAYS, APPARENTLY NOT CONTACTING THE AFT LATCHES, CAUSING HOLE PUNCTURE IN FORWARD CARGO DOOR. REPLACED HOOK ACTUATOR, RODS ADN BELL CRANK BEARINGS PER MM 52-34-07, REPAIRED FORWARD CARGO DOOR DAMAGED RIB T CHORD AND PLACED DOUBLEFeb 22, 2000 · N620FF · Boeing 747212B · Cargo/Baggage DoorsSDR TWRA0017A/C Pack · malfunctionedNR 1 PACK BEGAN TO RUMBLE AND PRODUCE SMOKE IN THE CABIN. A/C SMOKE EMERGENCY CHECKLIST AND SHUTDOWN NR 1 PACK. ACCOMPLISH ONE PACK CHECKLIST, MAINTAIN NORMAL PRESSURE. (M)Feb 20, 2000 · N616FF · Boeing 747212B · Cabin Cooling SystemSDR 20000330SH016Brake · overheatedON ARRIVAL, LT WING AND BODY GEAR WHEEL BRAKES OVERHEATED. NR 4 WHEEL ASSY IGNITED, BUT WAS IMMEDIATELY EXTINGUISHED. NR 6 AND NR 7 WHEEL ASSY THERMAL FUSE PLUGS RELIEVED AND WHEELS DEFLATED. INSP OF GEAR AREAS CARRIED OUT OK AND MAIN WHEELS REPLACED (4, 6,Feb 4, 2000 · N482EV · Boeing 747212B · BrakeSDR TWRA0014Wire · disconnectedDURING C-CHECK, FOUND T-LAVATORY SMOKE DETECTOR WIRING DISCONNECTED FROM SPLICE. RE-CONNECTED WIRING. OPERATIONAL CHECK OK. (X)Feb 4, 2000 · N624FF · Boeing 747212B · Smoke DetectionSDR TWRA0013Wire · failedDURING C-CHECK, FOUND GENERATOR FEEDER CABLE BURNED AT STA'S 970, 980, AND 985. REPLACED FEEDER CABLES. (X)Feb 4, 2000 · N624FF · Boeing 747212B · Electrical Power System WiringSDR EIA2000072Stringer · crackedFOUND BS 742 STRINGER 2A LT END CRACKED. DEFECTIVE STRINGER END REPAIRED PER SRM 53-10-03 FIG 10. (M)Feb 2, 2000 · N485EV · Boeing 747212B · Fuselage Main, Longeron/StringerSDR EIA2000071Stringer · crackedFOUND BS 742 STRINGER 2A RT END CRACKED. DEFECTIVE STRINGER END REPAIRED PER SRM 53-10-03 FIG 10. (M)Feb 2, 2000 · N485EV · Boeing 747212B · Fuselage Main, Longeron/StringerSDR EIA2000070Stringer · crackedFOUND BS 742 STRINGER 1R END CRACKED. DEFECTIVE STRINGER END REPAIRED PER SRM 53-10-03 FIG 10. (M)Feb 2, 2000 · N485EV · Boeing 747212B · Fuselage Main, Longeron/StringerSDR EIA2000069Skin · damagedFX BS 980 STRINGER 39R SKIN FOUND CHAFING MARK BY THE RAM AIR INLET DUCT. CARRIED OUT SKIN REPAIR AT BS 980 STRINGER 39R AS PER SRM 53-30-03. (M)Feb 2, 2000 · N485EV · Boeing 747212B · Fuselage Main, Plate/SkinSDR EIA2000068Stringer · crackedFOUND FORWARD CARGO BS 478 STRINGER 38L CRACKED. BS 470-490 STRINGER 38L REPAIRED PER SRM 53-10-03 FIG 3. (M)Feb 2, 2000 · N485EV · Boeing 747212B · Fuselage Main, Longeron/StringerSDR EIA2000067Spindle · damagedLT WING INBOARD T/E AFT FLAP SPINDLE ATTACH BOLT HOLES ELONGATED. ELONGATED BOLT HOLES OVERSIZED, NDT INSPECTED, AND OVERSIZED FASTENER INSTALLED PER BOEING MESAGES EVR-HKG-00-00011H/-00009F AND HAECO REPAIR SCHEME R-57-55-34270. (M)Feb 2, 2000 · N485EV · Boeing 747212B · Trailing Edge FlapsSDR EIAA2000077Floorbeam · crackedHAECO-HKG - M/D BS 1220 RBL 115 FLOORBEAM WEB CRACKED. FLOORBEAM WEB REPAIRED PER SRM 51-40-02 FIG 1. (X)Feb 2, 2000 · N485EV · Boeing 747212B · Fuselage Main, Floor BeamSDR EIAA2000076Floorbeam · crackedHAECO-HKG - C1 CHECK - M/D BS 1220 LBL 115 BELOW FLOORBEAM WEB CRACKED. FLOORBEAM REPAIRED PER SRM 51-40-02 FIG 1. (X)Feb 2, 2000 · N485EV · Boeing 747212B · Fuselage Main, Floor BeamSDR EIAA2000075Frame · crackedHAECO-HKG - C1 CHECK - M/D BS 960 STR 9R FRAME CRACKED. FRAME REPAIRED PER SRM 53-10-04 FIG 54. (X)Feb 2, 2000 · N485EV · Boeing 747212B · Fuselage Main, FrameSDR EIAA2000074Stringer · crackedHAECO-HKG - C1 CHECK - M/D BS 760 STR 23L STRINGER END FOUND CRACKED. REPAIRED PER SRM 53-10-03 FIG 4. (X)Feb 2, 2000 · N485EV · Boeing 747212B · Fuselage Main, Longeron/StringerSDR EIAA2000073Floorbeam · crackedHAECO-HKG - C1 CHECK, M/D BS 460 STR 13R FLOORBEAM WEB CRACKED. REPAIRED FROM RBL 76 TO RBL 115 PER SRM 53-10-07. (X)Feb 2, 2000 · N485EV · Boeing 747212B · Fuselage Main, Floor BeamSDR EIA2000066Bulkhead · crackedFOUND AFT CARGO COMPT BS 1480 LEFT BULKHEAD WEB CRACKED AT APU BLEED DUCT CUTOUT 1 O-CLOCK POSITION. BS 1480 LEFT BULKHEAD WEB REPAIRED AT APU BLEED DUCT CUTOUT AREA PER BOEING DWG 144U2602 AND SB 747-53-2309. (M)Feb 1, 2000 · N485EV · Boeing 747212B · Fuselage Main, Bulkhead
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