# Service difficulty reports: N17244

A list on [N17244](https://openairdocs.org/aircraft/N17244.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 118 reports

- [SDR CALA2026062617359](https://openairdocs.org/sdr/CALA2026062617359.md): Outflow Valve · faulted · Jun 24, 2026 · N17244 · Boeing 737824 · Pressure Regulator/Outflow Valve
  > IN DESCENT THROTTLES IDLE NOTICABLE PRESS BUMP. NEEDLE SHOWS 300 0 DN THEN RECOVERS PILOT CLARIFIED NEEDLE DN FLUCTUATED TO 3000 AND BEHAVED ERRATICALLY. CONTROLLER FAULT 19 OFV. REMOVED AND REPLACED AFT OUTFLOW VALVE ASSY. OPS CHECKS & GROUND CHKD SYS OKAY
- [SDR CALA2026052716567](https://openairdocs.org/sdr/CALA2026052716567.md): Filter · odor · May 27, 2026 · N17244 · Boeing 737824 · Air Distribution System
  > DIRTY SOCK SMALL ON CLIMB AND ARRIVAL BLEEDS AND PACKS WERE ON. REMOVED AND REPLACED BOTH LEFT AND RIGHT RECIRCULATION FILTERS REF AMM 21-25-01 RAN BOTH ENGINES WITH BLEEDS ON NO SMELL NOTED WHILE RUNNING ENGINES OR APU BLEEDS.
- [SDR CALA2025100909824](https://openairdocs.org/sdr/CALA2025100909824.md): Slide · no discrepancy · Oct 8, 2025 · N17244 · Boeing 737824 · Escape Slide
  > R2 DOOR SLIDE REMOVED FOR TS OF DOOR HANDLE, REINSTALLED R2 DOOR SLIDE MM 25-66-01-400-803. RENDERED SAFETY CHECKLIST COMPLETED. VERIFIED RII REQUIREMENTS REF MM 25-66-01-400-803
- [SDR CALA2025100209527](https://openairdocs.org/sdr/CALA2025100209527.md): Bulb · inoperative · Oct 2, 2025 · N17244 · Boeing 737824 · Emergency Lighting
  > RIGHT FORWARD OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-51-04-960-801, OPS CHECKED OK.
- [SDR CALA2025091108755](https://openairdocs.org/sdr/CALA2025091108755.md): Slide · loose · Sep 11, 2025 · N17244 · Boeing 737824 · Escape Slide
  > R2 DOOR SLIDE LOWER Z FOLD HITTING DOOR THRESHOLD. REMOVED AND REPLACED R2 DOOR SLIDE REF AMM 25-66-01-000-803 AND REF AMM 25-66-01-400-803.
- [SDR CALA2025091208836](https://openairdocs.org/sdr/CALA2025091208836.md): Frame · cracked · Aug 28, 2025 · N17244 · Boeing 737824 · Fuselage Main, Frame
  > AFT CARGO COMP CRACKED AT FRAME AROUND FASTENER HEAD STA 947.5 RBL 9. ACCOMPLISHED REPAIR OF STA 947 FRAME AT RBL 15 TO BL 0 IAW ESR WI#53-12688 AND SRM 51-40-02-0G-0.
- [SDR CALA2025082808231](https://openairdocs.org/sdr/CALA2025082808231.md): Support · corroded · Aug 26, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT CORROSION OUT OF LIMITS, SIDEWALL SUPPORT BETWEEN STR 23L-25 BS 500D.
- [SDR CALA2025082608120](https://openairdocs.org/sdr/CALA2025082608120.md): Bracket · damaged · Aug 22, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN E&E COMP BRACKET BETWEEN BS 294.5 - 312, S22L FASTENER HOLES ELONGATED. LOCATED, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED NEW BRACKET AT MAIN E&E COMP BRACKET BETWEEN BS 294.5-312, S22L IAW SRM 51-40-05-0G-0, AMM 51-21-72-370-804, AMM 51-21-
- [SDR CALA2025091208835](https://openairdocs.org/sdr/CALA2025091208835.md): Door Sill · corroded · Aug 21, 2025 · N17244 · Boeing 737824 · Fuselage Main, Structure
  > DAMAGE FOUND ON FORWARD ENTRY DOORWAY, LEFT, LOWER AUXILIARY SILL OUTER CHORD BETWEEN STA.299 AND STA.348 AT STR 23L. ACCOMPLISHED REPAIR PER ECRA 5310-08680 DIP REQUIRED PER ECRA5310-08680
- [SDR CALA2025082208050](https://openairdocs.org/sdr/CALA2025082208050.md): Strap · corroded · Aug 21, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN E&E COMP LEFT, CORROSION AT STRAP BETWEEN BS 294.5 - 312, S22L.
- [SDR CALA2025082908257](https://openairdocs.org/sdr/CALA2025082908257.md): Bracket · cracked · Aug 20, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE ACCESS 192BL STA 663.75 LBL 54" SMALL BRACKET CRACKED. INSTALL CLIP AT LOWER FUSELAGE ACCESS 192BL STA 663.75 LBL 54" IAW SRM 51-40-02-0G-0 AND DWG 149A3501.
- [SDR CALA2025082508077](https://openairdocs.org/sdr/CALA2025082508077.md): Web · corroded · Aug 20, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN E&E COMP LH CORROSION AT INTERCOSTAL BETWEEN STA 328-312 STR 22L. PARTIALLY INSTALLATION NEW WEB AT E&E COMP BETWEEN STA 312 AND STA 325 REF SRM 51-40-02-0G-0SECTION SUBSTANTIATING THAT COMPLIANCE WITH THE REQUIREMENTS OF ESR-WI 40-12610/41-12611) AND EC
- [SDR CALA2025082208044](https://openairdocs.org/sdr/CALA2025082208044.md): Channel · corroded · Aug 17, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY LH 'Z' CHANNEL HAS MULTIPLE SPOTS OF CORROSION FROM BS 727H - 787. R & R LT ZEE CHANNEL AT AFT CARGO BAY IAW SRM 51-40-02-0G-0. REMOVED CORROSION ON CHANNEL IAW SRM 51-10-02-0G-0. EVALUATED REWORKED AREA ORIGINAL MAT: 0.040" MAT LOSS" 0.001" R
- [SDR CALA2025081907927](https://openairdocs.org/sdr/CALA2025081907927.md): Channel · corroded · Aug 17, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO COMP CORROSION AT ZEE CHANNEL BETWEEN STA 500A-500D LBL 21" REF AAR N/R 97524861 INSTALLED FWD CARGO COMP ZEE CHANNEL BETWEEN STA 500A-500D LBL 21" PER SRM 51-40-02-0G-0 AND DWG# 143A7500. INSTALLED FWD CARGO COMP ZEE CHANNEL BETWEEN STA 500A-500D
- [SDR CALA2025082508074](https://openairdocs.org/sdr/CALA2025082508074.md): Strap · corroded · Aug 16, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUTOUT CORROSION AT FLOOR SUPPORT STRAP FASTENER HOLES BETWEEN STA 787-827 RBL 19". REMOVED AND REPLACED AFT CARGO DOOR CUTOUT FLOOR SUPPORT STRAP FROM STA 787 TO 827 RBL 19" PER REF SRM 51-40-02-0G-0 AND DWG 146A8120.
- [SDR CALA2025081907925](https://openairdocs.org/sdr/CALA2025081907925.md): Channel · corroded · Aug 16, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO COMP CORROSION AT ZEE CHANNEL BETWEEN STA 500A-500D RBL 21" REF AAR N/R 97524859 INSTALLED FWD CARGO COMP ZEE CHANNEL BETWEEN STA 500A-500D RBL 21" PER SRM 51-40-02-0G-0 AND DWG# 143A7500.. REMOVED AND INSTALLED NEW FWD CARGO COMP ZEE CHANNEL BETWEE
- [SDR CALA2025081807909](https://openairdocs.org/sdr/CALA2025081807909.md): Rib · cracked · Aug 15, 2025 · N17244 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > R / HAND HORIZONTAL STAB. LEADING EDGE PANEL, RIB #3 FROM I/B SIDE HAS A CRACK. REMOVED AND REPLACED R/H HORIZONTAL STAB LEADING EDGE PANEL RIB # 3 REF 51-40-02-0G-0 AND DWG 186A1001.
- [SDR CALA2025081507816](https://openairdocs.org/sdr/CALA2025081507816.md): Rib · cracked · Aug 15, 2025 · N17244 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STAB. LEADING EDGE PANEL, RIB 4 FROM I/B SIDE HAS A CRACK. REMOVED AND REPLACED RT HORIZONTAL STAB LEADING EDGE RIB 4 IAW 51-40-02-0G-0 AND DWG 186A1001.
- [SDR CALA2025081807905](https://openairdocs.org/sdr/CALA2025081807905.md): Scuff Plate · corroded · Aug 14, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR LOWER SCUFF PLATE AREA IS CORRODED. REF AAR N/R 97524634. REMOVED AND REPLACED FWD CARGO THESHOLD WEB PER SRM 51-40-02-0G-0 AND DWG#143A8120,
- [SDR CALA2025081507843](https://openairdocs.org/sdr/CALA2025081507843.md): Rib · cracked · Aug 14, 2025 · N17244 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > CRACK FOUND ON LT HORIZ STAB LEADING EDGE AT RIB OF HSS 309. REMOVED AND REPLACED LT HORIZ STAB LEADING EDGE PANEL RIB AT HSS 309 IAW SRM 51-40-02-0G-0 AND DWG 186A1001.
- [SDR CALA2025082208043](https://openairdocs.org/sdr/CALA2025082208043.md): Frame · corroded · Aug 12, 2025 · N17244 · Boeing 737824 · Fuselage Main, Frame
  > MAIN E & E COMP LT, CORROSION AT FRAME BETWEEN STR20L-22L BS 328-6 IAW AAR N/R 97525286. INSTALLED FRAME AT MAIN E & E COMP LT BETWEEN S20L, BS 328-6". IAW SRM 51-40-02-0G-0. DWG 142A1150. SECTION SUBSTANTIATING THAT COMPLIANCE WITH THE REQUIREMENTS OF ESR-WI
- [SDR CALA2025081807901](https://openairdocs.org/sdr/CALA2025081807901.md): Frame · corroded · Aug 12, 2025 · N17244 · Boeing 737824 · Fuselage Main, Frame
  > MAIN E&E COMP LEFT, CORROSION AT FRAME STR 22L STA 328+7". INSTALLED NEW WEB/FRAME IAW SRM 51-40-02-OG-0 AND DWG 142A1150 WORK
- [SDR CALA2025081807899](https://openairdocs.org/sdr/CALA2025081807899.md): Housing · corroded · Aug 12, 2025 · N17244 · Boeing 737824 · Cargo/Baggage Doors
  > FWD CARGO DOOR EXTERIOR HANDLE HOUSING GOUGED. REMOVED AND REPLACED FWD CARGO DOOR EXTERIOR HANDLE HOUSING PER SRM 51-40-02-0G-0 AND DWG 146A6110.
- [SDR CALA2025082608119](https://openairdocs.org/sdr/CALA2025082608119.md): Intercostal · corroded · Aug 11, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN E&E COMP LT CORROSION AT INTERCOSTAL BETWEEN BS 294.5-312 STR 23L. COMPLETED INSTALLATION NEW WEB BETWEEN BS 294.5 & 312 S23L IAW SRM 51-40-02-G-0 AND DWG# 141A8131.
- [SDR CALA2025082608118](https://openairdocs.org/sdr/CALA2025082608118.md): Intercostal · corroded · Aug 11, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN E&E COMP LT CORROSION AT INTERCOSTAL BETWEEN BS 344-3" S23L. INSTALLED NEW WEB AT E&E COMP LT BETWEEN BS 330 & 344, S23L IAW SRM 51-40-02-0G-0 AND DWG# 141A8131.
- [SDR CALA2025082708187](https://openairdocs.org/sdr/CALA2025082708187.md): Frame Angle · corroded · Aug 10, 2025 · N17244 · Boeing 737824 · Fuselage Main, Structure
  > MAIN E & E COMP LT CORROSION AT FRAME LOWER ANGLE STR 22L STA 328+7" REF AAR N/R 97525318 INSTALLED NEW CHORD P/N: 141A8240U16 AT STA 328+7 STR 22L REF SRM 51-40-02-0G-0 AND DWG # 141A8240 INSTALLED NEW CHORD P/N: 141A8240-16 AT STA 328+7 STR 22L -23L REF S
- [SDR CALA2025091208834](https://openairdocs.org/sdr/CALA2025091208834.md): Skin · damaged · Aug 9, 2025 · N17244 · Boeing 737824 · Fuselage Main, Plate/Skin
  > SCRATCH & DENT ON RIGHT SIDE OF AC 15 INCHES AFT OF FS 500E AND 4 INCHES BELOW S24R. REPAIR ACCOMPLISHE D ON THE RIGHT SIDE OF FUSELAGE 15 INCHES AFT OF STA.500E 4 INCH ES BELOW S24R IN ACCORDANCE WITH SRM 53-00-01-2R-3 REPAIR 3.
- [SDR CALA2025081207631](https://openairdocs.org/sdr/CALA2025081207631.md): Housing · gouged · Aug 4, 2025 · N17244 · Boeing 737824 · Cargo/Baggage Doors
  > AFT CARGO DOOR EXTERIOR HANDLE HOUSING GOUGED. REMOVED AND REPLACED AFT CARGO DOOR EXTERIOR HANDLE HOUSING PER SRM 51-40-02-0G-0 AND DWG 146A6110.
- [SDR CALA2025081207630](https://openairdocs.org/sdr/CALA2025081207630.md): Structure · cracked · Aug 4, 2025 · N17244 · Boeing 737824 · Horizontal Stabilizer Structure
  > CRACK FOUND ON LT HORIZ STAB LEADING EDGE, AT RIB OF LE HSS 95.96. REF AAR N/R 97525091. REMOVED AND REPLACED L/H HORIZONTAL STAB LEADING EDGE RIB AT L/E STA 95.96 REF 51-40-02-0G-0 AND DWG 186A1001.
- [SDR CALA2025081207629](https://openairdocs.org/sdr/CALA2025081207629.md): Skate Angle · worn · Aug 4, 2025 · N17244 · Boeing 737824 · Vertical Stabilizer
  > LEFT BODY-TO-VERTICAL FIN FAIRINGS FLANGE HAS CHAFING WORN DAMAGE FOR REF AAR N/R 97525018. REMOVED AND REPLACED SKATE ANGLE AT LT BODY TO VERTICAL FIN AFT SECTION REF SRM 51-40-02-0G-0 AND DWG 148A8300.
- [SDR CALA2025080707430](https://openairdocs.org/sdr/CALA2025080707430.md): Angle · gouged · Aug 4, 2025 · N17244 · Boeing 737824 · Auxiliary Power Unit (APU) Doors
  > APU DOOR AFT RIGHT SIDE DEEP GOUGE. REMOVED AND REPLACED APU DOOR Z EDGE ANGLE REF SRM 51-40-02-0G-0 AND DWG 148A6350.
- [SDR CALA2025080707429](https://openairdocs.org/sdr/CALA2025080707429.md): Skate Angle · worn · Aug 4, 2025 · N17244 · Boeing 737824 · Vertical Stabilizer
  > {B737-06-3-0068} RH BODY-TO-VERTICAL FIN FAIRINGS FLANGE HAS CHAFFING WORN DAMAGE. REMOVED AND REPLACED AFT RIGHT BODY TO VERTICAL FIN ANGLE (SKATE ANGLE) REF SRM 51-40-02-0G-0 AND DWG 148A8300. REMOVED AND REPLACED AFT RIGHT BODY TO VERTICAL FIN ANGLE (SK
- [SDR CALA2025080607391](https://openairdocs.org/sdr/CALA2025080607391.md): Angle · cracked · Aug 2, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE RT A/C BAY AFT REAR SPAR BULKHEAD VAPOR BARRIER LOWER ANGLE CRACKED AT I/B END RBL 7 BS 663.75. REMOVED AND COMPLETELY INSTALLED NEW STIFFENER AT FWD SIDE OF VAPOR BARRIER FROME RBL 6 TO RBL 31 IAW SRM 51-40-02-0G-0 AND DWG 111A1001.
- [SDR CALA2025080507325](https://openairdocs.org/sdr/CALA2025080507325.md): Flange · worn · Aug 2, 2025 · N17244 · Boeing 737824 · Vertical Stabilizer Miscellaneous Structure
  > LH BODY-TO-VERTICAL FIN FAIRINGS FLANGE BROKEN. REMOVED AND REPLACED LH BODY TO VERTICAL FIN FAIRINGS FLANGE IAW SRM 51-40-02-0G-0 AND DWG 147A0030.
- [SDR CALA2025080507324](https://openairdocs.org/sdr/CALA2025080507324.md): Skate Angle · worn · Aug 2, 2025 · N17244 · Boeing 737824 · Rudder, Plate/Skin
  > CRACK FOUND ON FWD RT BODY-TO-VERTICAL FIN FAIRINGS FLANGE.. REMOVED AND REPLACED SKATE ANGLE AT FWD RT BODY TO VERTICAL FIN FAIRING REF SRM 51-40-02-0G-0 AND DWG 147A0030.
- [SDR CALA2025081107557](https://openairdocs.org/sdr/CALA2025081107557.md): Seat Track · corroded · Aug 1, 2025 · N17244 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN GOUGE AT SEAT TRACK CROWN TOP STA 520 RBL 24.75. INSTALLED SEAT TRACK SECTION AND CHANNEL AT STA 520 TO 500I+12 RBL24.75 IAW B737 SRM 51-40-02 AND 53-00-52-2R4. ACCOMPLISHED REPAIR OF SEAT TRACK SECTION AND CHANNEL AT STA 520 TO 500I+12 RBL 24.75
- [SDR CALA2025081107556](https://openairdocs.org/sdr/CALA2025081107556.md): Seat Track · corroded · Aug 1, 2025 · N17244 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN GOUGE AT SEAT TRACK CROWN TOP STA 520 LBL 24.75 INSTALLED SEAT TRACK SECTION AND CHANNEL AT STA 520 TO 500I+12 LBL24.75 IAW B737 SRM 51-40-02 AND 53-00-52-2R4
- [SDR CALA2025081107555](https://openairdocs.org/sdr/CALA2025081107555.md): Seat Track · corroded · Aug 1, 2025 · N17244 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN GOUGE AT SEAT TRACK CROWN TOP BS 520 LBL 45.50. COMPLETED INSTALLATION OF SEAT TRACK SECTION AND CHANNEL AT STA 520 LBL 45.50" PER SRM 51-40-02-0G-0 AND SRM-53-00-52-2R-4 DWG 143A5400. ACCOMPLISHED REPAIR OF SEAT TRACK SECTION AND CHANNEL AT BS 5
- [SDR CALA2025080407242](https://openairdocs.org/sdr/CALA2025080407242.md): Rib · gouged · Aug 1, 2025 · N17244 · Boeing 737824 · Vertical Stabilizer, Spar/Rib
  > MULTIPLE GOUGES FOUND ON VERTICAL FIN L/E FIXED RIB LE HSS 1007.65). REMOVED AND REPLACED VERTICAL FIN L/E FIXED RIB IAW SRM 51-40-02-0G-0 AND DWG 176A3002.
- [SDR CALA2025080407240](https://openairdocs.org/sdr/CALA2025080407240.md): Seat Track · corroded · Aug 1, 2025 · N17244 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN, GOUGE AT SEAT TRACK CROWN TOP BS 520, RBL 45.50. COMPLETED INSTALLATION OF SEAT TRACK AND CHANNEL BS 520, RBL 45.50 IAW SRM 51-40-02-0G-0 SRM-53-00-52-2R-4 DWG 143A5400.
- [SDR CALA2025080407231](https://openairdocs.org/sdr/CALA2025080407231.md): Floorbeam · corroded · Jul 28, 2025 · N17244 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN FWD WET AREA CORROSION AT FLOOR BEAM FASTENER HOLES STA 328 BETWEEN RBL 21"-50". INSTALLED STRAP ON FWD MAIN CABIN WET AREA STA 328 FLOOR BEAM WITH BMS 5-95 SEALEANT, SEALANT WAS MIXED AT 11: 30 A.M, SQUEEZE OUT TIME WAS AT 11:33 A.M, CURE TIME I
- [SDR CALA2025072907046](https://openairdocs.org/sdr/CALA2025072907046.md): Floorbeam · corroded · Jul 28, 2025 · N17244 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN FWD WET AREA CORROSION AT FLOOR BEAM PREVIOUS REPAIR STA 328 RBL 12" REF AAR N/R 97524617 ACCOMPLISHED INSTALLATION OF NEW REPAIR STRAP AT FLOOR BEAM REPAIR STA 328 RBL 12" AS PER EC/RA#: 5321-01454 AND SRM-51-40-02-0G-0.
- [SDR CALA2025072907045](https://openairdocs.org/sdr/CALA2025072907045.md): Web · corroded · Jul 28, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA CORROSION AT FLOOR WEB STA 986.5+2" RBL 35. REMOVED AND INSTALLED WEB AT FLOOR STA986.5+2, RBL 35" IAW 51-40-02.
- [SDR CALA2025091208833](https://openairdocs.org/sdr/CALA2025091208833.md): Skin · cracked · Jul 27, 2025 · N17244 · Boeing 737824 · Fuselage Main, Plate/Skin
  > TYPICAL CRACK FOUND AT R1 DOOR BEAR STRAP AT FASTENER ADJACENT TO FITTING LATCH. CRACK AT 10 O'CLOCK POSITION WITH CRACK LENGTH: 0.156". ACCOMPLISHED REPAIR AT R1 DOOR BEAR STRAP REFERENCE B737-800 SRM 53-10-01-2R-6 FIGURE 202
- [SDR CALA2025080507318](https://openairdocs.org/sdr/CALA2025080507318.md): Doubler · cracked · Jul 27, 2025 · N17244 · Boeing 737824 · Fuselage Main, Plate/Skin
  > EXTERNAL POWER RECEPTACLE DOOR CUTOUT INNER DOUBLER FWD CENTER AREA CRACKED. APPLIED TOP COAT EXTERNAL POWER RECEPTACLE DOOR CUTOUT IAW AMM 51-21-73-370-803. REMOVED AND REPLACED EGPR INNER DOUBLER AS REQUIRED IAW SRM 51-40-02-0G-0, DWG 141A3702 AND DWG 141
- [SDR CALA2025072907040](https://openairdocs.org/sdr/CALA2025072907040.md): Web · corroded · Jul 27, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA CORROSION/GOUGE AT FLOOR WEB STA 986.5 LBL 39". REMOVED AND INSTALLED WEB BS 986.5 LBL 39 IAW SRM 51-40-02. REMOVED AND INSTALLED WEB STA 986.5 LBL 39" IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0 AND DWG 147A5700.
- [SDR CALA2025072907039](https://openairdocs.org/sdr/CALA2025072907039.md): Angle · cracked · Jul 27, 2025 · N17244 · Boeing 737824 · Fuselage Main, Bulkhead
  > WHEEL WELL VAPOR BARRIER UPPER ANGLE CRACK AT RBL 5. ACCOMPLISHED REPAIR OF RT VAPOR BARRIER UPPER ANGLE BS 663 RBL 3 TO RBL 20 IAW SRM 57-10-10-2R-5, APPLIED FILLET SEAL AS REQUIRED AT REPAIR AREA IAW AMM 51-31-00-390-802 AND APPLIED CIC AS REQUIRED IAW AMM
- [SDR CALA2025072907038](https://openairdocs.org/sdr/CALA2025072907038.md): Angle · cracked · Jul 27, 2025 · N17244 · Boeing 737824 · Fuselage Main, Bulkhead
  > LEFT WHEEL WELL VAPOR BARRIER UPPER ANGLE CRACKED AT LBL 5. ACCOMPLISHED REPAIR OF LT VAPOR BARRIER UPPER ANGLE BS 663 LBL 3 TO LBL 20 IAW SRM 57-10-10-2R-5. APPLIED FILLET SEAL AS REQUIRED AT REPAIR AREA IAW AMM 51-31-00-390-802 AND APPLIED CIC AS REQUIRED I
- [SDR CALA2025072806967](https://openairdocs.org/sdr/CALA2025072806967.md): Support · corroded · Jul 25, 2025 · N17244 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA CORROSION AT RT INNER CHORD BETWEEN STA 947.5-986.5. REMOVED AND INSTALLED RH INNER CHORD STA 947.5 TO 1006 IAW SRM 51-40-02 AND DWG 147A8501.
- [SDR CALA2025072806966](https://openairdocs.org/sdr/CALA2025072806966.md): Floorbeam · corroded · Jul 25, 2025 · N17244 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT WET AREA CORROSION AT FLOORBEAM PREVIOUS REPAIR STA 986.5 BETWEEN LBL 0"- 49" REF AAR N/R 97524598 ACCOMPLISHED FLOORBEAM REPAIR AT MAIN CABIN AFT WET AREA STA 986.5 FROM LBL 52" RBL 52" IAW B737 SRM 53-70-51-2R-4.

Next page: https://openairdocs.org/aircraft/N17244/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 n_number = 'N17244' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N17244/reports

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