Boeing 727-2Q9
Service difficulty reports · 830
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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 = '7272Q9' 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 = '7272Q9' 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 DHL2005740504Channel · corrodedHORIZ CHANNEL AND ANGLE CORRODED WL 172 RBL 20 STA 1183 AFT CARGO COMPARTMENT. REMOVED ANGLE IAW B727 SRM 51-30-2 FABRICATED NEW ANGLE AT WL 172 RBL 20 STA 1183 AT AFT CARGO MAT USED 2024 T3 .050 PO NR 90020093 DIMENSION 6" BY 3" IAW B727 SRM 51-20-1 AND 53-1SDR DHL2005741545Panel · dentedRUDDER STA 0.00 RT TRAPEZOIDAL PANEL HAS 10 DENTS. MEASURED 10 EA DENTS ON RT TRAPEZOIDAL PANEL. A/Y RATIO OF 9 DENTS WITH-IN LIMITS. A/Y RATIO OF 1 DENT OUT-OF-LIMITS. CLEANED, PREPPED, APPLIED POTTING COMPOUND TO DENT, CURED AND SANDED SMOOTH. FABRICATESDR DHL2005740501Rib · crackedNR 5 SLAT INTERIOR AT ACTUATOR ATTACHMENT INBD AND OUTBD RIBS CRACKED NDT CONFIRMED. REMOVED AND REINSTALLED NR 5 SLAT PER 727 MM 27-81-11. OPS CHECKED OK IAW B727 MM 27-81-00. FAB Z NEW RIBS FROM 2024T3 .0140 PO NR 9002012 SIZE 15 1/8" BY 5 1/8" IAW B727 SSDR DHL2005740502Shear Tie · crackedAFT CARGO COMPT BS 1166 BETWEEN STR 22 RIGHT TO STR 23 RIGHT IS CRACKED AT SHEAR TIE NDT CONFIRMED. CUT OUT FRAME SECTION STR 23R TO STR 24R DIM 22" BY 6 1/2" IAW 727 SRM 53-10-4 FIG 1. FABRICATED FRAME SECTION FROM 7075 T6 .063 DIM 22" BY 6 1/2" FRAME SPLICSDR DHL2005740535Keelbeam · crackedREMOVED FASTENERS AS REQ AND PRIMED THE UPPER FLANGE OF THE KEELBEAM CHORD PER S/B 727-53-208 REV 1 FIG 3 DETAIL 2 AT LEFT SIDE BS 870. FABBED REPAIR DOUBLER FROM 15-5 PH .071 HEAT TREATED TO 170 TO 190 KSI PO NR 315722 DIM 8.625 BY 3.875 INCHES HFEC INSPECTSDR DHL2005740508Skin · damagedACCOMPLISHED IDENTIFICATION OF EXISTING REPAIR ON FUSELAGE SKIN AT STA 1148 AND STRINGER 29L PER ASTAR J/C FCD 500001-001B. REMOVED EXISTING REPAIR AT STA 1148 AND STR 29L IAW B727 SRM 51-30-2, DRAIN MAST REMOVED IN EA 38100001-001B. CUT OUT DAMAGE AT SKIN DSDR DHL2005740543Skin · corrodedREMOVED INBD FLOW CONTROL VALVE TO FOM S/M IAW B727 MM 21-58-21. REMOVED OUTBD FLOW CTL VLV TO FOM S/M REPAIR IAW B727 MM 21-58-31. REMOVED FASTENERS AT FUSE EXT SKIN BS 1223 BELOW STR 20L IAW B727 SRM 51-30-2, CUTOUT 4 EA DAMAGED AREAS DIM 3 3/8" BY 1 1/4"SDR DHL2005740533Skin · dentedREMOVED EXTERNAL SKIN DOUBLER AT STA 1157-1183, STR 19L-22L DUE TO PILLOWING AT UPPER END IAW B727 SRM 51-30-2, CLEANED UP INTERNAL STRUCTURE AND FUSELAGE SKIN AREA FOR RE-EVALUATION IAW B727 MM 12-40-0 WITH NO CORROSION NOTED, CUT OUT 1 BY 1 1/2 IN SECTION OFSDR DHL2005740558Seat Track · damagedMAIN CABIN SEAT TRACK BS 480 TO 690 LBL 45.5 DAMAGED. REMOVED SEAT TRACK FROM BS 480- 740 LBL 45.5 IAW B727 SRM 51-30-2. FAB NEW SEAT TRACK FROM PN BAC 1520-792 PO NR 9001707 DIM 29' IAW B727 SRM 53-10-5 (1) AN DWN NR 2902 VENTURA AEROSPACE. FAB NEW ANGLES SDR DHL2005740517Seat Track · damagedMAIN CABIN SEAT TRACK BS 480 T0 BS 560 LBL 24.75 DAMAGED. REMOVED AND REPLACED SEAT TRACK AT BS 480 TO BS 690 LBL 24 .75 AND FABRICATED SEAT TRACK FROM BAC 1520-792, PO NR 900146 AND 900146 DIM 18 FT. FABRICATED SPLICE FROM P/N BAC 1503-100122 PO NR 900943,DSDR DHL2005740526Skin · damagedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; SKIN REPAIR DOUBLER STA 318-339 AND STR 1-4L AT LOCATION OF VENTURA AEROSPACE 9G BULKHEAD INST OF EXTERNAL SUPPORT PLATE,( STC;ST00848LA). REMOVED EXISTING FUSELAGE SKIN REPAIR DOUBLER/FILLER AT STA 31SDR DHL2005740559Skin · dentedDENT LT FUSELAGE SKIN AT STA 1355 NR 2 ENGINE SUPPORT STRUCTURE. REMOVED FASTENERS AT L/SIDE FUSELAGE SKIN AT STA 1355 NR 2 ENG SUPPORT IAW B727 SRM 51-30-2. CUT-OUT DAMAGE AREA DIMENSION 1" BY 1 1/4" IAW B727 SRM 51-40-2 FIG 1. FABRICATED DOUBLER MAT USEDSDR DHL2005740557Structure · dentedDENT LT SIDE FUSELAGE STA 1374, NR 2 ENGINE SUPPORT STRUCTURE. REMOVED FASTENERS AT LT SIDE FUSELAGE SKIN STA 1374 NR 2 ENGINE SUPPORT STRUCTURE IAW B727 SRM 51-40-2 FIG 1. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .050 PO NR 9002093 SIZE 5 1/4" BY 5 1/4" IASDR DHL2005740555Web · crackedCRACK AT INBD WEB R/LOWER TORQUE BOX LWR LIGHTENING HOLES STA 1248. STOP DRILLED CRACK .250 TERMINATED AT END OF CRACK AT INBD R/LOWER TORQUE BOX LWR LIGHTENING HOLE STA 1248 IAW B727 SRM 51-10-1 NDT INSPECTED USING HFEC IAW B727 NDT MAN PART 651-00-00 FIG 23SDR DHL2005740554Torque Box · crackedCRACK AT INBD WED RT LOWER TORQUE BOX, LOWER LIGHTENING HOLE STA 1240. STOP DRILLED CRACK .250 TERMINATED AT END OF CRACK ON RT LOWER TORQUE BOX WEB STA 1240 IAW B727 SRM 51-10-1 NDT INSP AREA USING HFEC IAW B727 NDTM PAR 6 51-00-00 FIG 23. CRACK TERMINATED SDR DHL2005740556Strap · damagedREPAIRED STRAP AT FWD E/E BS STA 328-344 LBL 24 IAW B727 SRM 53-10-8 FIG 6. TREATED AND PRIMED STRAP IAW B727 SRM 51-10-2, DIM 24"X2 5/8" PO 900505.SDR DHL2005740515Torque Box · crackedCRACK ON TORQUE BOX UPPER WEB STA 1231. REMOVED FASTENERS FOR ACCESS CUT OUT DAMAGED AREA DIM 5 X 1.75 INCH AT WEB LOWER TORQUE BOX BS 1231 IAW B727 SRM 51-30-2 AND 51-40-2 FIG 1. HFEC INSP CUTOUT WITH NO CRACKS NOTED IAW B727 NDT MAN PT6 51-00-00 FIG 23. FSDR DHL2005740511Skin · dentedC1 CARGO DOOR HAS NUMEROUS DENTS ON SKIN BETWEEN STA 560 TO 620. REMOVED FASTENERS AT C1 DOOR STA 560 TO 620 IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA 59 X 14.5 INCHES IAW B727 SRM 52-00-03 FIG 3. FAB NEW SKIN WITH 2024T3 .080 PO 9002012 SIZE 59 X 14.5 INCSDR DHL2005740518Web · crackedREMOVED FASTENERS AT FWD CORNER ENTRY DOOR WEB (INTERIOR) IAW B727 SRM 51-30-2,STOP DRILLED CRACK IAW B727 SRM 51-30-2. .250 TERMINATED OF END OF CRACK,NDT HFEC INSP PER 727 NDT PT6 51-00-00 FIG 23 CRACK END IN STOP HOLE, FABRICATED DOUBLER REPAIR MATL USED 70SDR DHL2005740560Frame · dentedFRAME BS540 SHOW DENT BTW STR16R AND 17R PREVIOUS FRAME REPAIR. REMOVED PREVIOUS REPAIR AT FS FRAME BS 540 BTW 16R AND 17R IAW B727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MAT USED 7075 T6 .071 PO NR 9001737 DIMENSION 6" BY 5" IAW B727 SRM 53-10-2 FIG 3 ANDSDR DHL2005740551Frame · damagedREMOVED PREVIOUS REPAIR AT FUSELAGE FRAME BS 600 BTW 16R AND 17R IAW B727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MAT USED 7075T6 .071 PO 9001737 DIM 6" BY 5" IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-10SDR DHL2005740550Seat Track · damagedMAIN CABIN SEAT TRACK 0 BS 344 TO BS 580 RBL .5. REMOVED AND REPLACED 0 SEAT TRACK BS 344 TO BS 580 RBL .5 IAW DWG NR AE 727-2-063 REVP. FABRICATED NEW SEAT TRACK P/N S139966 PO NR 438032 DIA 12FT P/N S139966 PO NR 991600 DIM 8FT IAW B727 SRM 51-30-5 AND DWGSDR DHL2005740552Splice · corrodedREMOVED STRINGER SPLICE FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-30-2 AT STR 28 LT BS 480, FABRICATED NEW STRINGER SPLICE MAT USED 7075T6 .040 PO 9001068 DIM 13" BY 4" IAW B727 SRM 51-20-1 AND 53-10-2 FIG 9. ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-SDR DHL2005740553Splice · corrodedSTR 27L AT BS 680 IS CORRODED. STR 27L AT FRAME 680 STRINGER SPLICE FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. REMOVED AND FABBED FROM P/N BAC1498-97 PO NR 3160113 1 FT LONG IAW B727 SRM 53-10-2 FIG 9 AND INSTALLED STRINGER SPLICE IAW B727 SRM 53-SDR DHL2005740549Stringer · corrodedSTR 26L AT BS 480 IS CORRODED. REMOVED STRINGER SLICE FOUND TO BE OUT IF LIMITS AT STR 26L AT BS 480 IAW B727 SRM 51-30-2. FABRICATED NEW STRINGER REPAIR MAT USED 7075T6 .040 PO NR 9001068 DIM. 13" BY 4" IAW B727 SRM 51-20-1 AND 53-10-2 FIG 9. ALODINED AND SDR DHL2005740545Frame · dentedFUSELAGE FRAME AT STA 520 SHOW DENT BTW STR 16R AND 17R PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR AT BS 520 BTW STR16R AND 17R IAW B727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MAT USED 7075T6 .071 PO NR 9001737 DIMENSION 8" BY 5" IAW B727 SRM 53- SRM 10-2 FISDR DHL2005740547Frame · damagedFRAME BS 640 SHOW DENT BETWEEN STR 16R AND 17R PREVIOUS FRAME REPAIR. REMOVED PREVIOUS REPAIR AT FUSELAGE FRAME BS 640 BETWEEN STR 16R AND 17R IAW B727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MAT. USED 7075T6 .071 PO NR 9001737 DIM 7" BY 5" IAW B727 SRM 53-SDR DHL2005740546Frame · damagedREMOVED PREVIOUS REPAIR AT FS AT 560 BTW 16R AND 17R IAW B 727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MAT USED 7075T6 .071 PO 9001737 DIM 6" BY 5" IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-10-3. INSTALSDR DHL2005740544Seat Track · damagedMAIN CABIN SEAT TRACK BS 760 - BS 870 LBL 24.75 DAMAGED. REMOVED SEAT TRACK BS 760 - BS 870 LBL 24.75 IAW B727 SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM P/N BAC1520-841 PO NR 9001474 DIM 4 FT AND P/N BAC1520-841 PO NR 9001690 DIM 4 FT IAW B727 SRM 53-10-2 SDR DHL2005740540Frame · damagedCABIN INTERIOR FRAME AT BS348 IS BENT AND ELONGATED HOLES BETWEEN STR 4L - 6L. PREVIOUS FRAME REPAIR. REMOVED ANGLE SUPPORT IAW B727 SRM 51-30-2, DUE TO ELONGATED HOLES, CUT OUT DAMAGED AREA DIM .50 INCH EDGE UPPER AND LOWER FRAME IAW B727 SRM 51-10-1 AND DWSDR DHL2005740525Stringer · corrodedDURING A "C" CHECK, 2 EACH RIVET HEADS POPPED RT FUSELAGE SKIN STA 1177 STR 22R. REMOVED RIVETS RT FUSELAGE SKIN AT BS 1177 ON STR 22R EVALUATED STRINGER OUT OF LIMITS IAW B727 SRM 51-30-2 AND 53-10-1 FIG 1. CUT OUT STRINGER AND REMOVED SPLICE AND COVER, 3 ESDR DHL2005740519Frame · corrodedFRAME BS 720C STR 28 LT AND STR 28 RT FOUND AFTER REMOVING SEALANT (CORROSION) TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. REMOVED LOWER SECTION OF FRAME BS 720C BETWEEN STR 28L TO 28R IAW B727 SRM 51-40-3 FIG 1. EVALUATED LOWER SKIN SECTION OK, NO DAMAGSDR DHL2005740509Frame · dentedCABIN INTERIOR FRAME AT BS 360 IS DENTED BETWEEN ST4R AND 5R PREVIOUS FRAME REPAIR. REMOVED ANGLE SUPPORT DUE TO DENT IAW B727 SRM 51-30-2. LOCATED AND DRIILED NEW ANGLE P/N AE 727-2-360-11 PO507998 AND DOUBLER AE 727-2-360-12 PO5080133. TREATED AND PRIMED SDR DHL2005740507Stringer · crackedVERT STAB FIN STA 180 STRINGER S-8 LT IS CRACKED AT FRAME ATTACH SCREW. REMOVED FASTENERS FOR ACCESS AT VERT STAB FIN STA 180 S-8 LT AND TRIMMED OUT DAMAGED AREA SIZE 3 1/2 INCH BY 3 INCH IAW B727 SRM 55-30-4 FIG1. FABRICATED REPAIR PARTS P/N BAC 1517-1367 7SDR DHL2005740506Stringer · crackedVERT STAB FIN STA 180 STR IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS AT VERT STAB FIN STA 180 S-8 RT AND TRIMMED OUT DAMAGED AREA SIZE 4 1/2 INCH BY 3 INCH IAW B727 SRM 55-30-4 FIG 1 AND 51-30-2. FABRICATED REPAIR FILLER P/N BAC 1517-1367 SDR DHL2005740539Torque Box · crackedREF. FLIGHTSTAR NR 104834 DISCREPANCY - RT LOWER TORQUE BOX CRACKED AT ST 1230. CORRECTIVE ACTION - STAP DRILLED CRACK .250 TERMINATED AT END OF CRACK ON RH LOWER TORQUE BOX BS1230 IAW B727 SRM 51-10-1. HFEC INSP. PER 727 NDT PT.6 51-00-00 FIG.23 NO CRACKS NOTSDR DHL2005740536Torque Box · crackedRT LOWER TORQUE BOX CRACKED AT STA 1223. STOP DRILLED CRACK .250 TERMINATED AT END OF CRACK ON RT LOWER TORQUE BOX STA 1223 IAW B727 SRM 51-10-1, HFEC INSP PER NDT PT.6 51-00-00 FIG 23. CRACK ENDS IN STOP HOLE. FABRICATED DOUBLER REPAIR IAW B727 SRM 53-10-2SDR DHL2005740534Seat Track · damagedMAIN CABIN SEAT TRACK BS 760 - 870 RBL 45.5 DAMAGED. REMOVED AND REPLACED SEAT TRACK BS760 - 870 RBL 45.5 IAW SRM 53-10-5 FIG 2. FABRICATED FROM P/N BAC1520-841 PO NR 9001690 DIM 8 FT IAW B727 SRM 53-10-2 FIG 1 AND 53-10-5 FIG 2. TREATED AND PRIMED SEAT TRSDR DHL2005740563Skin · dentedVERT STAB ABOVE RT FIN STA 133 LOWER RUDDER SURF IS DENTED NEAR T/E. EVAULATED DENTED AREA AT VERT STAB ABOVE RT FIN STA 133 LOWER RUDDER SURF. TRIM OUT DAMAGED SKIN SIZE 1/2" BY 3/4" IAW B727 SRM 55-30-3 AND 51-10-1. FABRICATED DOUBLER REPAIR SIZE 2" BY 2.SDR DHL2005740561Skin · dentedVERT STAB BELOW FIN STA 133 RT LOWER RUDDER SURF IS DENTED NEAR T/E CORRECTIVE ACTION: EVALUATED DENTED AREA AT VERT STAB FIN STA 133 RT LOWER RUDDER SURF IAW B727 SRM 55-40-1 FOUND OUT OF LIMITS TRIM OUT DAMAGED AREA. SIZE 1/2" BY 3/4" IAW B727 SRM 55-30-3- ASDR DHL2005740532Seat Track · corrodedMAIN CABIN SEAT TRACK BS 760 - BS 870 LBL 45.5 CORROSION AND DAMAGED. REMOVED AND REPLACED SEAT TRACK FROM P/N BAC1520-841 PO NR 9001650 DIM 8 FT IAW B727 SRM 53-10-2 FIG 1 AND 53-10-5 FIG 2. TREATED AND PRIMED SEAT TRACK IAW B727 SRM 51-10-2.SDR DHL2005740531Spar · crackedRT WING TRAILING EDGE FALSE SPAR HAS A TWO INCH CRACK JUST INBD OF NR 6 FLAP TRACK WBL 202 WING STA 330.5. REMOVED AND DISPLACED R/WING LOWER T/EDGE PANELS AS REQUIRED FOR ACCESS IAW B727 SRM 51-30-2. CUT OUT AND REMOVED 52" SECTION OF CRACKED AUX SPAR LWR CSDR DHL2005740530Skin · lightning strike2 RIVETS SHOWING SIGNS OF LIGHTNING STRIKE AFT OF STA 950B UNDERNEATH FUSELAGE SKIN STR 29R. CUT-OUT 6.750 X 3.125 INCHES SECTION OF LOWER FUSELAGE SKIN AT BS 950B+15 AT STR 29R DUE TO LIGHTNING STRIKE DAMAGED BEYOND ALLOWABLE LIMITS PER B727 SRM 53-30-1 FIG SDR DHL2005740529Skin · dentedDENT RT FUSELAGE SKIN 4 INCHES AFT OF STA 1342.4 STRINGER 22R. REMOVED FASTENERS FOR ACCESS IAW B727 SRM 51-30-2 CUTOUT DAMAGED AREA ON RT FUSELAGE STA 1342 STR 22R AND 23R SIZE 3 X .750 INCHES AND 1 X .500 INCHES IAW B727 SRM 54-30-3 FIG 7. FABRICATED DOUBLSDR DHL2005740528Skin · dentedDENT R/SIDE FUSELAGE SKIN 3 INCHES FWD OF STA 1342.4 STRINGER 23R. REMOVED FASTENERS FOR ACCESS IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA 3 BY 1.5 INCHES IAW B727 SRM 53-30-3 FIG 1. FABRICATED FILLER SIZE 3 BY 1.5 INCHES FROM 2024T3 .050 PO NR 9002093 AND SDR DHL2005740527Skin · dentedPREVIOUS FLUSH REPAIR RT FUSELAGE SKIN IS DENTED FWD OF STA 1243 ABOVE STR 22R. REMOVED PREVIOUS REPAIR TO BE OUT OF LIMITS AT R/SIDE FUSELAGE SKIN STA 1243 STR 22R IAW B727 SRM 51-30-2. CUTOUT DAMAGED AREA DIM 4.5 BY 4 INCHES IAW B727 SRM 53-30-3 FIG 24. FSDR DHL2005740514Skin · delaminatedCUT OUT DAMAGED AREA LWR SKIN APPROX 5 X 1.5 INCH IAW B727 SRM 51-40-20 FIG 31. FABRICATED ONE FILLER APPROX 5 X 1.5 INCH AND ONE DOUBLER APPROX 8 X 3 INCHES USING .016 2024-T3 PO 9001660 IAW B727 SRM 57-50-2 FIG 4. CLEANED, PREPPED, APPLIED ADHESIVE PRIMERSDR DHL2005740513Skin · debondedRT WING TE OB AFT FLAP LOWER SKIN DISBONDED AT TE CENTER. CUT OUT DAMAGED AREA LWR SKIN APPROX 5 INCHES BY 1 1/2 INCHES IAW B727 SRM 54-40-20 FIG 31. FABRICATED ONE FILLER APPROX 5 INCHES BY 1 1/2 INCHES AND ONE DOUBLER APPROX 8 INCHES BY 3 INCHES USING .01SDR DHL2005740505Skin · delaminatedRT WING OUTBD AFT-FLAP TRAILING EDGE INBD CORNER IS DELAMINATED LOWER SURFACE. CUTOUT DAMAGED LWR SURFACE APPROX 3 INCH BY 5 INCH BAGGED FOR MOISTURE REMOVAL IAW B727 SRM 51-40-20 FIG 32. REMOVAL AND REPLACED HONEYCOMB CORE APPROX 3 INCH BY 4 INCH USING DUR-SDR DHL2005740019Seat Track · damagedMAIN CABIN SEAT TRACK BS 344 TO 480 LBL 45.5 DAMAGED. REMOVED AND REPLACED NEW SEAT TRACK AT BS 344 TO BS 480 LBL 45.5 AND FABRICATED SEAT TRACK P/N BAC1520-792 PO NR 9001329 DIM. 12 FT IAW B727 SRM 53-10-2 FIG 1 AND 51-30-5 AND DWG NR 2902 VENTURA AEROSPACE.
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