# Service difficulty reports: N5237A

A list on [N5237A](https://openairdocs.org/aircraft/N5237A.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 2 · 67 reports

- [SDR SCNA20261014423](https://openairdocs.org/sdr/SCNA20261014423.md): Lamp · inoperative · Oct 14, 2026 · N5237A · Boeing 737800* · Emergency Lighting
  > RH EMERGENCY LIGHT INOP. REPLACED RH EMERGENCY LIGHT LAMP PER AMM 33-51-04/201. OPS CHECK GOOD
- [SDR SCNA20260917402S](https://openairdocs.org/sdr/SCNA20260917402S.md): Speed Brake · no discrepancy · Sep 13, 2026 · N5237A · Boeing 737800* · Drag Control System
  > AFTER LANDING THRUST WAS ADVANCED FOR TAXI AUTO RETRACTION OF SPEED BRAKES DID NOT OCCUR. FIM 27-61 TASK 805, NO DEFECTS FOUND, PERFORMED SEVERAL CYCLES ON SPEED BRAKE AND IT OPERATED NORMALLY. FAULT COULD NOT BE DUPLICATED. THS CLEARS MEL 27-7-1.
- [SDR SCNA20260917402](https://openairdocs.org/sdr/SCNA20260917402.md): Speed Brake · faulted · Sep 13, 2026 · N5237A · Boeing 737800* · Drag Control System
  > AFTER LANDING THRUST WAS ADVANCED FOR TAXI AUTO RETRACTION OF SPEED BRAKES DID NOT OCCUR. OPEN.
- [SDR SCNA20260917401](https://openairdocs.org/sdr/SCNA20260917401.md): Elec Connector · loose · Sep 13, 2026 · N5237A · Boeing 737800* · Flight Control System Wiring
  > DURING LANDING CHECKLIST NOTICED THAT THE SPEED BRAKE ARM LIGHT DID NOT ILLUMINATE AFTER ARMING THE SPEED BRAKE. MOVED LEVER BACK DOWN AND BACK TO ARM, ALSO DID A LAMP CHECK AND ARM LIGHT AND DO NOT ARM WOULDN'T ILLUMINATE. AFTER LANDING NOTICED AUTO SPEED BRA
- [SDR SCNA20260916398](https://openairdocs.org/sdr/SCNA20260916398.md): Door · open · Aug 28, 2026 · N5237A · Boeing 737800* · Accessory Compartment Doors
  > ON CLIMB OUT ABOVE 16,000 NOTICED A VIBRATION THAT SEEMED STRONGEST ON THE FO NEAR OUTBOARD CUP HOLDER VIBRATION WENT AWAY AFTER DESCENDING BELOW 16000 ON WALK AROUND FOUND THE GPU DOOR OPEN. PERFORMED WALK AROUND IAW AMM 05-41-01-210-801 CONFIRMED WITH GROUN
- [SDR SCNA20260827373](https://openairdocs.org/sdr/SCNA20260827373.md): Smoke Goggles · missing · Aug 25, 2026 · N5237A · Boeing 737800* · Emergency Equipment
  > FIRST OFFICER EMERGENCY EQUIPMENT MISSING GOGGLES. REPLACED FIRST OFFICER GOGGLES IAW AMM 25-11-00.
- [SDR SCNA20260916397](https://openairdocs.org/sdr/SCNA20260916397.md): Actuator · out of rig · Aug 15, 2026 · N5237A · Boeing 737800* · Drag Control System
  > SPEED BRAKE NOT ENGAGING ON LANDING. FOUND AUTO SPEED BRAKE ACTUATOR TO BE OUT OF RIG. RIGGED AUTO SPEED BRAKE ACTUATOR AND PERFORMED OPS CHECK REF AMM 27-26-31 THIS CLEARS MEL 27-7-1.
- [SDR SCNA20260916396](https://openairdocs.org/sdr/SCNA20260916396.md): Speed Brake · faulted · Aug 14, 2026 · N5237A · Boeing 737800* · Drag Control System
  > SPEED BRAKE NOT ENGAGING ON LANDING. PERFORMED BITE TEST OF AACU PER B737 FIM TASK 32-42 TASK 801. FAULT CLEARED. RETESTED NO FAULTS. A/C OK FOR SVC AT THIS TIME.
- [SDR SCNA20260916395](https://openairdocs.org/sdr/SCNA20260916395.md): Lever · lack of lube · Aug 8, 2026 · N5237A · Boeing 737800* · Drag Control System
  > ON DESCENT INTO AFW SPEED BRAKE LEVER WOULD NOT ARM GREEN SPEED BRAKE ARMED LIGHT. FOUND FORCE FROM DOWN TO FLIGHT DETENT AT 26 LBS LUBRICATED SPEED BRAKE LEVER FORCE NEEDED AFTER IS 18 LBS. SPEED BRAKE LEVER FRICTION TEST REF AMM 22-62-00-800-803. AUTO SPE
- [SDR SCNA20260714297](https://openairdocs.org/sdr/SCNA20260714297.md): Housing · damaged · Jul 13, 2026 · N5237A · Boeing 737800* · Cargo/Baggage Doors
  > AFT CARGO COMPARTMENT DOOR HANDLE HOUSING WITH SHARP EDGES AND OUTER SKIN PANEL WITH DETERIORATED PAINT. REWORKED AFT CARGO COMPARTMENT DOOR HANDLE HOUSING IAW BAC 5300-1 SECT 11.2.2 AND APPLIED PROTECTIVE TREATMENT IAW B737-800 SRM 51-20-01-0G-0 PARAG 5D S
- [SDR SCNA20260730333](https://openairdocs.org/sdr/SCNA20260730333.md): Beam · cracked · Jul 9, 2026 · N5237A · Boeing 737800* · Leading Edge Devices
  > DURING THE HFEC FASTENER HOLE PERFORMED AT RT WING SLAT NR 7 PER NRI 6-6, FOUND CRACK IN THE NOSE BEAM AT OPEN HOLE ADJACENT TO THE ACTUACTOR RIB. PERFORMED REPAIR RT WING SLAT NR 7 NOSE BEAM SECTION FROM SS290.250" TO SS343.750" DUE TO CRACK IAW BCF SRM 57-
- [SDR SCNA20260709289](https://openairdocs.org/sdr/SCNA20260709289.md): Door Frame · damaged · Jul 8, 2026 · N5237A · Boeing 737800* · Fuselage Main, Structure
  > FORWARD CARGO DOOR FORWARD FRAME WITH SHARP EDGES BETWEEN FITTING STOPS N°4 AND N°5. REWORKED CUT OUT EDGE IAW BAC5300-1 SEAT 11.2.2 REV K DATED 05-11-2018 TREATED REWORKED AREA IAW B737-800 BCF SRM 51-20-01-0G-0 PARAG 5D REV 26 DATED 03-10-2026 AND SOPM 20-4
- [SDR SCNA20260707283](https://openairdocs.org/sdr/SCNA20260707283.md): Retainer · out of limits · Jul 2, 2026 · N5237A · Boeing 737800* · Emergency Equipment
  > FWD GALLEY EMERGENCY ESCAPE SLIDE COVER,GIRT BAR RETAINER CLIPS WITHOUT LIMITS (2EA). REPLACED RETAINER CLIPS (2EA) P/N:65C16820-10 IAW B737-800 AIPC 25-66-00-14 SHEET 002 ITEMS 95 REV 129 DATED 04-15-2026 AND INSTALLED SOLID IVETS IAW B737-800 SRM 51-40-02-0
- [SDR SCNA20260427171](https://openairdocs.org/sdr/SCNA20260427171.md): Hook · damaged · Apr 26, 2026 · N5237A · Boeing 737800* · Emergency Equipment
  > DUE TO TEMPORARY REPAIR OF L1 DOOR SLIDE GRIT BAR J HOOK REF EA 25-0138, PERMANENT REPAIR TO BE COMPLETED AT NEXT CONVENIENT OPPORTUNITY. ACOMPLISHED REPAIR OF THE DOOR 1L GIRT BAR HOOK IAW SCA EA 25-0138 THIS CLEARS MEL 52-16-1.
- [SDR SCNA20260318128](https://openairdocs.org/sdr/SCNA20260318128.md): Holder · loose · Mar 18, 2026 · N5237A · Boeing 737800* · Emergency Equipment
  > GIRT BAR HOLDER ON L1 DOOR LOOSE. ACOMPLISHED REPAIR OF THE DOOR 1L GRIT BAR HOOK PER SCA EA 25-0138 THIS CLEARS MEL 52-16-1.
- [SDR SCNA20260105006](https://openairdocs.org/sdr/SCNA20260105006.md): Proximity Sensor · malfunctioned · Jan 3, 2026 · N5237A · Boeing 737800* · Leading Edge Slat Position Indicating System
  > RED TAKEOFF CONFIG LIGHT AND TAKE OFF WARNING DURING TLCC WITH FLAPS 5 AND CONFIGURED FOR TAKEOFF NR 1 LEADING EDGE FLAP TRANSIT LIGHT DURING EXTENSION OR RETRACTION. R & R NR 1 KRUGER FLAP NR 1 PROX SENSOR IAW AMM 27-88-11-400-802. OPS CHECKED, LIGHTS OPERA
- [SDR SCNA20250627234](https://openairdocs.org/sdr/SCNA20250627234.md): Lamp · inoperative · Jun 27, 2025 · N5237A · Boeing 7378 · Emergency Lighting
  > DURING LO CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT REF AMM 33-51-04.
- [SDR UIEA2024122301182](https://openairdocs.org/sdr/UIEA2024122301182.md): Window · arced · Dec 24, 2024 · N5237A · Boeing 7378 · Flight Compartment Windows
  > F/O FWD WINDOW ARC'D THEN WINDOW CRACKED AT 22,000'. PRESSURE NORMAL(<P>REPLACED R1 WINDOW AND WINDOW HEAT CONTROLLER IAW AMM 56-11-11, OPS CHECK GOOD.</P>)
- [SDR UIEA2024072900760](https://openairdocs.org/sdr/UIEA2024072900760.md): Fire Handle · no test · Jul 29, 2024 · N5237A · Boeing 7378 · Detection System
  > #1 ENGINE FIRE HANDLE WILL NOT TEST(<P>RERACKED APU FIRE MODULE IAW AMM 26-10-01. OPS TEST PERFORMED IAW AMM 26-11-00, NO DEFECTS NOTED</P>)
- [SDR UIEA2024062600569](https://openairdocs.org/sdr/UIEA2024062600569.md): Support Plate · cracked · Jun 28, 2024 · N5237A · Boeing 7378 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT BETWEEN STA 727H AND 727I RBL 21" SIDE PLATE SUPPORT ZEE WITH CRACKS. NOTE: WAS FOUND WHEN PERFORMING JOB (REMOVAL METALIC FLOOR PANEL) WITH NRI 1-21.(<P>REPLACED FLOOR ZEE CHANNEL SIDE PLATE P/N: BAC1496-377 FROM STA 727G+11.5" TO STA 767 RBL2
- [SDR UIEA2022092301043](https://openairdocs.org/sdr/UIEA2022092301043.md): Actuator · leaking · Oct 20, 2022 · N5237A · Boeing 7378 · Engine Thrust Reverser
  > #2 ENGINE O/B TR EVIDENCE OF OIL LEAK AT MID AND LWR ACTUATOR (ENG #2 O/B T/R OIL LEAK MID AND LWR ACTUATOR CLEANED IAW SOPM 20-30-03 PAGE 5 STEP 4. PERFORMED OPERATION CHECK AND FOUND ACTUATOR LEAK IS IN LIMITS IAW AMM 78-31-00-700-801-F00)
- [SDR UIEA2022092301044](https://openairdocs.org/sdr/UIEA2022092301044.md): Channel · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Miscellaneous Structure
  > R/H AFT MOP STILL AT FS950 HAS CORROSION (REMOVED CORROSION IAW 53-70-15-1A-1 AND FOUND TO BE IN LIMITS.)
- [SDR UIEA2022092301045](https://openairdocs.org/sdr/UIEA2022092301045.md): Frame Splice · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Main, Frame
  > CORROSION FWD CARGO RH FRAME SPLICE HAS CORROSION, STA500H, RBL25, WL157. (MARKED) (REMOVED AND REPLACED FWD. CARGO R/H FRAME SPLICE STA. 500H, RBL 25, WL 157 WITH NEW PO #881742 PER SRM 51-40-02-0G-0 AND DWG #143A1215)
- [SDR UIEA2022093001063](https://openairdocs.org/sdr/UIEA2022093001063.md): Frame · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Main, Frame
  > WHILE GIVING OK TO INSTALL AFT PIT BULKHEAD SUPPORTS, FOUND CORROSION ON BEAM AT STA 947.5, BETWEEN STR 24-26, WL 170 (LOWER FRAME) (REMOVED CORROSION ON INNER CHORD LOWER FRAME @STA. 947.5, STR. 24R-26R IN AREA OF 5.5"L X.8"W X.007"D. FOUND IN LIMITS PER S
- [SDR UIEA2022093001064](https://openairdocs.org/sdr/UIEA2022093001064.md): Floorbeam · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Main, Floor Beam
  > ***CORROSION*** FLOO BEAM TOP SURFACE, STA986, RBL35 - RBL45, WL208. (MARKED) (CORROSION REMOVED FROM UPPER CHORD OF STA. 986.5 FLOOR BEAM IN AREA OF 2.0"L X.9"W X.051"D WAS FOUND OUT OF LIMITS AND REMOVED PER SRM 51-10-02-OG-0. UPPER CHORD OF FLOORBEAM REP
- [SDR UIEA2022100101067](https://openairdocs.org/sdr/UIEA2022100101067.md): Stub Frame · no indication · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Main, Floor Beam
  > CORROSION ON STUB BS 396 STUB FRAME APPROX. RBL6 TO RBL 18 WL 156(REMOVED CORROSION ON STA 396 FRAME RBL6-18 WL 156 BY BURNISHING IAW SRM 51-10-02-0G-0, DAMAGE FOUND TO BE IN FINISH ONLY NO MATERIAL LOSS NOTED. TREATED AND PRIMED REWORKED ARE IAW AMM51-21-41-3
- [SDR UIEA2022100201069](https://openairdocs.org/sdr/UIEA2022100201069.md): Frame · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Main, Frame
  > CORROSION ON AFT CARGO COMP ON FLOOR FRAME 787, RBL 16-RBL21, WL156(REMOVED CORROSION ON 787 FRAME RBL16-RBL 21 WL156 IAW SRM 51-10-02-0G-0, BLEND AREA MEASURES 2"X.5"X.001" FOUND TO BE IN LIMITS IAW SRM 53-00-07-1A-1)
- [SDR UIEA2022100301071](https://openairdocs.org/sdr/UIEA2022100301071.md): Support Bracket · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Main, Frame
  > FWD CARGO LH SIDEWALL LINER SUPPORT BRACKET HAS CORROSION,STA 500B, BETWEEN S23L & 24L (FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. REMOVED DAMAGED BRACKET STA 5400B STR23L TO 24L INSTALLED NEW BRACKET STA 500B STR 23L TO 24L PE
- [SDR UIEA2022100301073](https://openairdocs.org/sdr/UIEA2022100301073.md): Web · no indication · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Main, Floor Beam
  > FLOOR WEB TO SURFACE STA 986+9 WL208 HAS CORROSION (REMOVED PAINT ON WEB TOP SURFACE AT STA 986+9 RBL 35 TO RBL 45 WL 208. NO CORROSION NOTED. RESTORED FINISH IAW B737-800 AMM 51-21-41-370-802, 51-21-72-370-804 AND 51-21-91-620-802)
- [SDR UIEA2022100401084](https://openairdocs.org/sdr/UIEA2022100401084.md): Channel · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Miscellaneous Structure
  > ***CORROSION*** AFT CARGO COMP, CORROSION ON RH ZEE CHANNEL STA727 - STA767, RBL21, WL155 (REMOVED AND REPLACED WITH NEW ZEE CHANNEL IAW 146A7500)
- [SDR UIEA2022100401085](https://openairdocs.org/sdr/UIEA2022100401085.md): Shield · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Miscellaneous Structure
  > ***CORROSION*** AFT CARGO COMP, CORROSION ON RH SHIELD STA767-787, RBL23, WL156 (REMOVED AND REPLACED SHIELD PER RCM 51-40-02 AND BOEING DRAWING 146A0081)
- [SDR UIEA2022100401086](https://openairdocs.org/sdr/UIEA2022100401086.md): Channel · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Miscellaneous Structure
  > ***CORROSION*** AFT CARGO COMP, CORROSION ON LH ZEE CHANNEL STA727+12 - STA807+7, LBL21, WL155(<P>REMOVED AND REPLACED PER SRM 53-00-53-2R-5</P>)
- [SDR UIEA2022100501087](https://openairdocs.org/sdr/UIEA2022100501087.md): Channel · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Miscellaneous Structure
  > ***CORROSION*** FWD CARGO COMP, CORROSION ON RH Z CHANNEL, STA500A-500G, RBL23, WL157. (CORROSION FOUND AROUND MULTIPLE NUTPLATES @STA. 500A-500G, RBL 23, WL 157 IN AREAS OF 1.0" X 1.0". FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2. FABRICATED REPLACEMENT PART P
- [SDR UIEA2022100501088](https://openairdocs.org/sdr/UIEA2022100501088.md): Support · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Miscellaneous Structure
  > ***CORROSION*** AFT CARGO COMP, CORROSION FWD CARGO DOOR REVEAL SUPPORT STA787+12, RBL24, WL157 (REMOVED AND REPLACED AFT CARGO FWD OF DOOR REVEAL SUPPORT CLIP PER SRM 51-40-02 AND BOEING DRAWING 146A8320)
- [SDR UIEA2022100501089](https://openairdocs.org/sdr/UIEA2022100501089.md): Support Angle · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Miscellaneous Structure
  > ***CORROSION*** STA 947 BULKHEAD SUPPORT ANGLE STR21-25R (REMOVED AND REPLACED AFT BULKHEAD SUPPORT ANGLE @STA 947, STR. 21R-25R PER DWG# 149A8117 AND SRM 51-40-02-0G-0)
- [SDR UIEA2022100501090](https://openairdocs.org/sdr/UIEA2022100501090.md): Support Bracket · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Miscellaneous Structure
  > ***CORROSION*** FWD CARGO LH SIDEWALL LINER SUPPORT BRACKET HAS CORROSION, STA500E, BETWEEN S23L & S24L (REMOVED AND REPLACED BRACKET PER SRM 51-40-02 AND BOEING DRAWING 417A2150)
- [SDR UIEA2022100501091](https://openairdocs.org/sdr/UIEA2022100501091.md): Support Bracket · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Structure (General)
  > ***CORROSION*** FWD CARGO LH SIDEWALL LINER SUPPORT BRACKET HAS CORROSION, STA500A, BETWEEN S23L & S24L (REMOVED AND REPLACED BRACKET PER SRM 51-40-02 AND BOEING DRAWING 417A2150)
- [SDR UIEA2022100501092](https://openairdocs.org/sdr/UIEA2022100501092.md): Support Bracket · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Structure (General)
  > ***CORROSION*** FWD CARGO LH SIDEWALL LINER SUPPORT BRACKET HAS CORROSION, STA500H, BETWEEN S23L & S24L (REMOVED AND REPLACED BRACKET PER SRM 51-40-02 AND BOEING DRAWING 417A2150)
- [SDR UIEA2022100501093](https://openairdocs.org/sdr/UIEA2022100501093.md): Support Bracket · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Structure (General)
  > ***CORROSION*** FWD CARGO LH SIDEWALL LINER SUPPORT BRACKET HAS CORROSION, STA500G, BETWEEN S23L & S24L (REMOVED AND REPLACED BRACKET PER SRM 51-40-02 AND BOEING DRAWING 417A2150)
- [SDR UIEA2022100701096](https://openairdocs.org/sdr/UIEA2022100701096.md): Support Bracket · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Miscellaneous Structure
  > ***CORROSION***FWD CARGO LH SIDEWALL LINER SUPPORT BRACKET HAS CORROSION, STA 500F, BETWEEN S23L S24L (FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMIT IN THE SRM. REMOVED DAMAGE BRACKET @STA 500F S23L TO S24L. INSTALLED REPLACEMENT BRAKET @STA 500
- [SDR UIEA2022100701097](https://openairdocs.org/sdr/UIEA2022100701097.md): Flange · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Main, Floor Beam
  > ***CORROSION*** STA 986 FLOORBEAM UPPER CHORD FWD FLANGE LBL43 WL207 (ACCOMPLISHED REPAIR AT FLOOR BEAM UPPER CHORD FWD. FLANGE @STA 986, LBL43, WL 207 PER ER #22-02313 REV. IR AND SRM 53-70-51-2R-6)
- [SDR UIEA2022100701098](https://openairdocs.org/sdr/UIEA2022100701098.md): Support Angle · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Main, Bulkhead
  > ***CORROSION***STA 947 LWR CTR BULKHEAD SUPPORT ANGLE (REMOVED AND REPLACED AFT LWR CTR BULKHEAD SUPPORT ANGLE @STA 947 PER DWG# 149A8117 AND SRM 51-40-02-0G-0)
- [SDR UIEA2022100701099](https://openairdocs.org/sdr/UIEA2022100701099.md): Threshold Web · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Structure (General)
  > ***CORROSION*** AFT CARGO COMP CARGO DOOR CUTOUT WEB HAS CORROSION STA787+9 - 827+5, RBL26, WL156. (REMOVED DAMAGED THRESHOLD WEB. INSTALLED REPLACEMENT THRESHOLD WEB PN# 146A8123-25 PER DWG# 146A8340 AND SRM 51-40-02-0G-0)
- [SDR UIEA2022100801101](https://openairdocs.org/sdr/UIEA2022100801101.md): Threshold Web · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Main, Plate/Skin
  > ***CORROSION***FWD CARGO DOOR THRESHOLD WEB, CORROSION STA. 460+3-460+10, RBL 28, WL 157 (REMOVED DAMAGED THRESHOLD WEB AND INSTALLED REPLACEMENT THRESHOLD WEB PN# 654A0003-58 @STA 440 TO 492 FWD CARGO DOOR THRESHOLD PER DWG# 143A8330 AND SRM 51-40-02-0G-0)
- [SDR UIEA2022100801102](https://openairdocs.org/sdr/UIEA2022100801102.md): Tie Down · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** AFT CARGO COMP, CORROSION R/H CARGO TIE DOWN TRACK @STA 787+8, RBL 14, WL 156 (CORROSION REMOVAL @STA 795, RBL 14 3.4"L X.9"W X.019"D FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG 103 DET. G. REMOVED AND REPLACED CARGO TIE DOWN TRACK P
- [SDR UIEA2022100801103](https://openairdocs.org/sdr/UIEA2022100801103.md): Intercostal · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Main, Structure
  > ***CORROSION*** AFT CARGO COMP, CORROSION ON FWD SIDE OF INTERCOSTAL STA 727+8, LBL5-RBL5, WL150. (CORROSION FOUND ON FWD SIDE OF INTERCOSTAL @STA 727+8, LBL 5 TO RBL 5, WL 150 TO BE 100% MATERIAL LOSS AND FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND
- [SDR UIEA2022100801104](https://openairdocs.org/sdr/UIEA2022100801104.md): Panel Support · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Main, Bulkhead
  > ***CORROSION*** FWD CARGO COMP, R/H AFT BULKHEAD PANEL SUPPORT, STA 500G, RBL 25, WL 157 (REMOVED AND REPLACED R/H AFT BULKHEAD PANEL SUPPORT @STA 500G, RBL 25, WL 157 PER DWG# 143A7902 AND SRM 51-40-02-0G-0)
- [SDR UIEA2022101001112](https://openairdocs.org/sdr/UIEA2022101001112.md): Bracket · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Miscellaneous Structure
  > ***CORROSION*** FWD CARGO L/H SIDEWALL LINER SUPPORT BRACKET HAS CORROSION, STA500E, BETWEEN S23L & S24L (FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS FOUND IN THE SRM. REMOVED DAMAGE BRACKET @STA 500E, S23L TO S24L. INSTALLED REPLACEMENT BRAC
- [SDR UIEA2022101001113](https://openairdocs.org/sdr/UIEA2022101001113.md): Skin · out of limits · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Main, Plate/Skin
  > FWD CARGO DOOR CUTOUT INTERIOR SKIN, MATERIAL LOSS AT EDGE OF SKIN, 4.0" UP FROM FWD LOWER CORNER (DAMAGE ON EDGE OF FWD CARGO DOOR, LOWER FWD ORNER IN AREA OF.9"L X.150"W X.110"D FOUND OUT OF LIMITS DUE TO BEING WITHIN 3.0" OF DOOR CUTOUT PER SRM 53-00-01-
- [SDR UIEA2022101101115](https://openairdocs.org/sdr/UIEA2022101101115.md): Frame · corroded · Oct 20, 2022 · N5237A · Boeing 7378 · Fuselage Main, Frame
  > ***CORROSION***AREA AFT OF AFT CARGO COMPARTMENT, CORROSION ON FRAME, STA. 947, BETWEEN STRINGERS S19R - S21R (CORROSION FOUND IN AREAS 4.0"L X 2.0"WV@STR 19R-20R. 2.6"L X 2.3"W @STR. 20R-21R AND 8.0"L X.8"W ON INNER CHORD STR 20R-21R @STA. 947. CORROSION REW

Next page: https://openairdocs.org/aircraft/N5237A/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 = 'N5237A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N5237A/reports

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