# Service difficulty reports: N8512U

A list on [N8512U](https://openairdocs.org/aircraft/N8512U.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 · 96 reports

- [SDR SWAA2026072435880](https://openairdocs.org/sdr/SWAA2026072435880.md): Megaphone · inoperative · Jul 20, 2026 · N8512U · Boeing 7378H4 · Emergency Equipment
  > FWD GALLEY MEGAPHONE INOPERATIVE. REPLACED THE BATTERIES, NO HELP. R & R MEGAPHONE WITH NEW BATTERIES NEW DUE DATE JUL 27 REF AMM 25-64-00.
- [SDR SWAA2026070718816](https://openairdocs.org/sdr/SWAA2026070718816.md): Bulb · inoperative · Jul 6, 2026 · N8512U · Boeing 7378H4 · Emergency Lighting
  > FWD ENTRY OVERDOOR EXIT SIGN HAS INOP BULBS. REPLACED THE BULBS AND PERFORMED GOOD TEST OF FWD ENTRY OVERDOOR EXIT SIGN IAW AMM 33-51-01-960-801.
- [SDR SWAA2026070718817](https://openairdocs.org/sdr/SWAA2026070718817.md): Bulb · inoperative · Jul 6, 2026 · N8512U · Boeing 7378H4 · Emergency Lighting
  > LEFT FWD OWE OVERDOOR SIGN HAS INOPERATIVE BULBS. REPLACED THE BULBS AND PERFORMED A GOOD FUNCTIONAL TESTED NEW BULBS IAW AMM 33-51-01-960-801.
- [SDR SWAA2026070718384](https://openairdocs.org/sdr/SWAA2026070718384.md): Battery Pack · inoperative · Jul 3, 2026 · N8512U · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1672 ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK M1672 AND PERFORMED SATISFACTORY INSTALLATION TEST PER AMM 33-51-06-960-805.
- [SDR SWAA2026061009589](https://openairdocs.org/sdr/SWAA2026061009589.md): Gusset · cracked · Jun 6, 2026 · N8512U · Boeing 7378H4 · Landing Gear Doors
  > LEFT MLG INNER DOOR GUSSET HAS POSSIBLE CRACK FWD OF AFT INNER-DOOR, MID-DOOR HINGE. VERIFIED 0.3IN CRACK NOT FULLY THRU REF NDT PART 6 51-00-00 PROC 23. MATCH DRILLED LT INNER DOOR HINGES IAW DWG 113A8000. REMOVED AND REPLACED LT MLG INNER DOOR IAW AMM 32-
- [SDR SWAA2026061009588](https://openairdocs.org/sdr/SWAA2026061009588.md): Door · cracked · Jun 6, 2026 · N8512U · Boeing 7378H4 · Landing Gear Doors
  > RIGHT MLG INNER DOOR GUSSET HAS POSSIBLE CRACK FWD OF AFT INNER-DOOR, MID-DOOR HINGE. VERIFIED 0.3IN CRACK NOT FULLY THRU REF NDT PART 6 51-00-00 PROC 23. MACHINED WEB TO REMOVE CRACK IN RT MLG INNER DOOR IAW SRM 52-80-02-1A-2. COMPLETED HIGH FREQ. REF. N
- [SDR SWAA2026021770845](https://openairdocs.org/sdr/SWAA2026021770845.md): Flashlight · inoperative · Feb 14, 2026 · N8512U · Boeing 7378H4 · Emergency Equipment
  > AFT FA FLASHLIGHT INOPERATIVE. ( FO SIDE) RESEATED AFT FA FLASHLIGHT IAW AMM 25-64-00. OPS CHECKED GOOD.
- [SDR SWAA2025121643476](https://openairdocs.org/sdr/SWAA2025121643476.md): Panel · delaminated · Dec 7, 2025 · N8512U · Boeing 7378H4 · Fuselage Main, Structure
  > PANEL 193B DELAMINATED AT TRAILING EDGE UNDER THE LOWER ANTI-COLLISION LIGHT. REPAIRED THE PANEL 193B IAW SRM 53-40-70-2R-1, AND SRM 51-70-04-2R-1.
- [SDR SWAA2025121641802](https://openairdocs.org/sdr/SWAA2025121641802.md): Floorbeam · cracked · Dec 2, 2025 · N8512U · Boeing 7378H4 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBBEAM, BS 540, BETWEEN LBL 0 - LBL 25 INBD END WAS CRACKED AROUND THE FASTENER. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0-B00069. LOCATED AND DRILLED IAW SRM 51-40-05-0G-0. APPLIED CIC IAW AMM 51-21-91-620-802.
- [SDR SWAA2025121641447](https://openairdocs.org/sdr/SWAA2025121641447.md): Plate · cracked · Dec 2, 2025 · N8512U · Boeing 7378H4 · Wing Main, Frame Structure
  > LEFT WING REAR SPAR, IRSS 215 WIGGLE PLATE IS CRACKED, AND NOT SECURE. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0-B00069,
- [SDR SWAA2025121641893](https://openairdocs.org/sdr/SWAA2025121641893.md): Hook · corroded · Dec 2, 2025 · N8512U · Boeing 7378H4 · Emergency Equipment
  > RIGHT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK HAS LIGHT SURFACE CORROSION. REMOVED EMERGENCY EXIT DOOR UPPER LINING IAW AMM 25-21-20-000-801, & REINSTALLED EMERGENCY EXIT DOOR UPPER LINER IAW AMM 25-21-20-400-801 3.D. (2) AND (4). AND REMOVED AND REPLACED EME
- [SDR SWAA2025121641892](https://openairdocs.org/sdr/SWAA2025121641892.md): Life Line · corroded · Dec 2, 2025 · N8512U · Boeing 7378H4 · Emergency Equipment
  > LEFT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK HAS LIGHT SURFACE CORROSION. REMOVED EMERGENCY EXIT DOOR LINING ASSEMBLY IAW AMM 25-21-20-000-801, & REINSTALLED EMERGENCY EXIT UPPER DOOR LINING ASSEMBLY IAW AMM 25-21-20-400-801, STEP 3. D. (2) AND (4), REMOVED A
- [SDR SWAA2025121640842](https://openairdocs.org/sdr/SWAA2025121640842.md): Handle · loose · Nov 30, 2025 · N8512U · Boeing 7378H4 · Passenger/Crew Doors
  > BOTH R2 AND L2 DOOR ASSIST HANDLES (NOT THE LINER) ARE LOOSE. SECURED BOTH R2 & L2 DOOR ASSIST HANDLES IAW AMM 25-21-25-420-801, STEP 3.B.(5).
- [SDR SWAA2025121640061](https://openairdocs.org/sdr/SWAA2025121640061.md): Support Angle · cracked · Nov 26, 2025 · N8512U · Boeing 7378H4 · Wing Miscellaneous Structure
  > LEFT WING AFT SPAR AREA, 21 INCHES INBD OF DEFLECTION CONTROL RIB SUPPORT ANGLE FOR FIXED WING UPPER PANEL JUST OTBD OF NR 6 SPOILER, CRACKED. REMOVED THE SUPPORT ANGLE IAW SRM 51-40-02, & AIPC 27-62-12-05, ITEM 55. LOCATED & DRILLED IAW SRM 51-40-05-0G-0.
- [SDR SWAA2025121640062](https://openairdocs.org/sdr/SWAA2025121640062.md): Support Angle · cracked · Nov 26, 2025 · N8512U · Boeing 7378H4 · Wing Miscellaneous Structure
  > RIGHT WING AFT SPAR AREA, 21 INCHES INBD OF DEFLECTION CONTROL RIB SUPPORT ANGLE FOR FIXED WING UPPER PANEL JUST OTBD OF NR 7 SPOILER, CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE FOR FIXED WING UPPER PANEL IAW SRM 51-40-02-0G-0, DWG 115A2512, REV -, AND
- [SDR SWAA2025121640063](https://openairdocs.org/sdr/SWAA2025121640063.md): Support Angle · cracked · Nov 26, 2025 · N8512U · Boeing 7378H4 · Wing Miscellaneous Structure
  > RIGHT WING AFT SPAR AREA UPPER WING FIXED PANEL SUPPORT ANGLE JUST INBD AND COMMON TO THE DEFLECTION CONTROL RIB CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 115A6200, REV A.
- [SDR SWAA2025082908309](https://openairdocs.org/sdr/SWAA2025082908309.md): Handle · loose · Aug 26, 2025 · N8512U · Boeing 7378H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR MOUNTED ASSIST HANDLE NEEDS TIGHTENING. TIGHTENED LOOSE FWD ENTRY DOOR MOUNTED ASSIST HANDLES IAW AMM 52-11-31-400-802 STEP 2(D).
- [SDR SWAA2025082908310](https://openairdocs.org/sdr/SWAA2025082908310.md): Handle · loose · Aug 26, 2025 · N8512U · Boeing 7378H4 · Service Doors
  > FWD SERVICE DOOR MOUNTED ASSIST HANDLE NEEDS TIGHTENED. TIGHTENED LOOSE FWD SERVICE DOOR MOUNTED ASSIST HANDLES IAW STEP 2(D).
- [SDR SWAA2025081199243](https://openairdocs.org/sdr/SWAA2025081199243.md): Flashlight · inoperative · Aug 7, 2025 · N8512U · Boeing 7378H4 · Emergency Equipment
  > EMERGENCY FLASHLIGHT AFT GALLEY F/O'S SIDEWALL NOT TEST<[01] PREFORMED OPS CHECK OF TEST FUNCTIONS OF ALL AFT GALLEY FLASHLIGHTS OPS CHECK GOOD AND RESEALED AMM 25-64-00
- [SDR SWAA2025080197070](https://openairdocs.org/sdr/SWAA2025080197070.md): Battery · no test · Jul 31, 2025 · N8512U · Boeing 7378H4 · Emergency Equipment
  > AFT GALLEY LOWER F/O SIDE GREY FLASHLIGHT TEST RED. R & R AFT RT OTBD EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00.
- [SDR SWAA2025062483920](https://openairdocs.org/sdr/SWAA2025062483920.md): Flashlight · inoperative · Jun 21, 2025 · N8512U · Boeing 7378H4 · Emergency Equipment
  > AFT JUMP SEAT FLASHLIGHT INOP<[01] SECURED FLASH LIGHT IN HOLDER OPS CHECK GOOD PER. AMM 25-64-00
- [SDR SWAA2025022599062](https://openairdocs.org/sdr/SWAA2025022599062.md): Slide · low pressure · Feb 23, 2025 · N8512U · Boeing 7378H4 · Escape Slide
  > CREW REPORTS L1 SLIDE PRESSURE IN RED <[01]. R+R L1 SLIDE PER MT 725-61-06.
- [SDR SWAA2025010281359](https://openairdocs.org/sdr/SWAA2025010281359.md): Flashlight · inoperative · Dec 29, 2024 · N8512U · Boeing 7378H4 · Emergency Equipment
  > FWD CABIN FLASHLIGHT INOP. FWD EMERGENCY FLASHLIGHT. OPS CK GOOD PER MM 25-64-00-SWA-802
- [SDR SWAA2024122780912](https://openairdocs.org/sdr/SWAA2024122780912.md): Battery Pack · inoperative · Dec 26, 2024 · N8512U · Boeing 7378H4 · Emergency Lighting
  > L/H OVERWING EXIT SIGN LIGHTS INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]. OPS CHECK GOOD.;[02] INSPECTION C/W
- [SDR SWAA2024122780113](https://openairdocs.org/sdr/SWAA2024122780113.md): Stringer · cracked · Dec 22, 2024 · N8512U · Boeing 7378H4 · Fuselage Main, Longeron/Stringer
  > FWD CARGO FLOOR STRUCTURE STRINGER CLIP CRACKED AT STATION 500I STRINGER 26R. HFEC VERIFIED.<[01] REMOVED STRINGER CLIP AT 500I STRINGER 26R PER SRM 51-40-02.;[02] REMOVED AND REPLACED CLIP PER SRM 51-40-02;[03] INSPECTED REPLACEMENT OF STRINGER CLIP REF: SRM
- [SDR SWAA2024122779024](https://openairdocs.org/sdr/SWAA2024122779024.md): Scuff Plate · cracked · Dec 19, 2024 · N8512U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO FORWARD CORNER THRESHOLD SCUFF PLATE IS CRACKED<[01] PARTS DATA UPDATE ONLY;[02] REMOVED AND REPLACED FWD CORNER SCUFF PLATE PER AMM 53-11-02.
- [SDR SWAA2024122775356](https://openairdocs.org/sdr/SWAA2024122775356.md): Angle · corroded · Dec 9, 2024 · N8512U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO PIT RH TRANSITION ANGLE BETWEEN 500A THRU 500I REQUIRES REPLACEMENT. REMOVED RT TRANSITION ANGLE. IAW SRM 51-40-02, LOCATED AND DRILLED NEW FASTENER HOLES ON FWD CARGO RT TRANSITION ANGLE, ALODINED AND PAINTED AS REQUIRED. IAW SRM 51-40-02, REMOVED
- [SDR SWAA2024122773388](https://openairdocs.org/sdr/SWAA2024122773388.md): Angle · corroded · Nov 27, 2024 · N8512U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT: LEFT TRANSITION ANGLE IS MISSING MULTIPLE CHEMICALLY BONDED NUT PLATES STARTING AT STA 727A TO STA 807.<[01] DUE TO CORROSION AROUND FASTENER HOLES L/H TRANSITION ANGLE WAS R/R ON TTG8Q00XAH7P;[02] INSPECTED WORK IN C/A #1
- [SDR SWAA2024122772052](https://openairdocs.org/sdr/SWAA2024122772052.md): Seal · cracked · Nov 27, 2024 · N8512U · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > LH HORIZONTAL STAB FORWARD SPAR UPPER SLIDING SEAL IS CRACKED<[01] REMOVED AND REPLACED LEFT UPPER; FORWARD HORIZONTAL SLIDING SEAL; OPS CHECK GOOD; WORK PERFORMED I.A.W. M.M. 53-31-31.;[02] 02 - INSPECTED PER [AMM 53-31-31-400-801-NG (STABILIZER-TO-BODY FRONT
- [SDR SWAA2024121872053](https://openairdocs.org/sdr/SWAA2024121872053.md): Angle · corroded · Nov 27, 2024 · N8512U · Boeing 7378H4 · Cargo Compartments
  > AFT CARGO L/H SIDEPLATE (TRANSITION ANGLE) HAS CORROSION AROUND NUTPLATE HOLES STA. 767 TO STA.787.<[01] TRANSITION ANGLE IS BEING REPLACED COMPLETELY; THE WORK AND SIGN OFF WILL BE COMPLETED ON THIS CARD TTG8Q00XAH7P;[02] REMOVED L/H TRANSITION ANGLE PER SRM
- [SDR SWAA2024121872054](https://openairdocs.org/sdr/SWAA2024121872054.md): Angle · corroded · Nov 27, 2024 · N8512U · Boeing 7378H4 · Cargo Compartments
  > AFT CARGO L/H SIDEPLATE (TRANSITION ANGLE) HAS CORROSION AROUND NUTPLATE HOLES STA. 787 TO STA.807.<[01] TRANSITION ANGLE IS BEING REPLACED COMPLETELY; THE WORK AND SIGN OFF WILL BE COMPLETED CARD TTG8Q00XAH7P.;[02] VERIFIED WORK IN C/A #1
- [SDR SWAA2024121872055](https://openairdocs.org/sdr/SWAA2024121872055.md): Angle · corroded · Nov 27, 2024 · N8512U · Boeing 7378H4 · Cargo Compartments
  > AFT CARGO COMPARTMENT: LEFT TRANSITION ANGLE HAS CORROSION AROUND MULTIPLE FASTENERS HOLES STARTING AT STA 727B +9 TO STA 727F + 19 LBL 22.<[01] TRANSITION ANGLE IS BEING REPLACED COMPLETELY; THE WORK AND SIGN OFF WILL BE COMPLETED ON TTG8Q00XAH7P;[02] INSPECT
- [SDR SWAA2024121872056](https://openairdocs.org/sdr/SWAA2024121872056.md): Angle · corroded · Nov 27, 2024 · N8512U · Boeing 7378H4 · Cargo Compartments
  > AFT CARGO COMPARTMENT: LEFT TRANSITION ANGLE HAS CORROSION AROUND MULTIPLE FASTENERS HOLES STARTING AT STA 727G +9 TO STA 767 +14 LBL 22.<[01] TRANSITION ANGLE IS BEING REPLACED COMPLETELY; THE WORK AND SIGN OFF WILL BE COMPLETED ON TTG8Q00XAH7P;[02] VERIFIED
- [SDR SWAA2024121872057](https://openairdocs.org/sdr/SWAA2024121872057.md): Angle · corroded · Nov 27, 2024 · N8512U · Boeing 7378H4 · Cargo Compartments
  > AFT CARGO COMPARTMENT: RIGHT TRANSITION ANGLE HAS CORROSION AROUND MULTIPLE FASTENERS HOLES STARTING AT STA 727F TO 727J + 10.<[01] TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2 TRANSITION ANGLE IS BEING REPLACED COMPLETELY; THE WORK AND SIGN OFF WIL
- [SDR SWAA2024122772047](https://openairdocs.org/sdr/SWAA2024122772047.md): Bracket · cracked · Nov 26, 2024 · N8512U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE INTERCOSTAL WEB; FWD CLIP/BRACKET CRACKED @ STA 400. (MARKED)<[01] REMOVED AND REPLACED PER SRM 51-40-02.
- [SDR SWAA2024122771918](https://openairdocs.org/sdr/SWAA2024122771918.md): Angle · corroded · Nov 26, 2024 · N8512U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD ENTRY DOOR THRESHOLD L-ANGLE VERTICAL LEG AT STA 312 LBL 52 HAS CORROSION.(MARKED)<[01] BLENDED AREA OF CORROSION ON FWD ENTRY DOOR THRESHOLD L-ANGLE VERTICAL LEG AT STA 312 LBL 52; BLEND FOUND TO BE OUT OF LIMITS ALL IAW SRM 53-10-15-1A-1.;[02] REMOVED; L
- [SDR SWAA2024122771915](https://openairdocs.org/sdr/SWAA2024122771915.md): Angle · corroded · Nov 26, 2024 · N8512U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD ENTRY DOOR THRESHOLD L-ANGLE HORIZONTAL LEG AT STA 328+12 LBL 56 HAS CORROSION.(MARKED)<[01] BLENDED AREA ON FWD ENTRY DOOR THRESHOLD L-ANGLE HORIZONTAL LEG AT STA 328+12 LBL 56; BLENDS FOUND TO BE OUT OF LIMITS ALL IAW SRM 53-10-15-1A-1.;[02] REMOVED AND
- [SDR SWAA2024122772048](https://openairdocs.org/sdr/SWAA2024122772048.md): Web · corroded · Nov 26, 2024 · N8512U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT; SCUFF PLATE WEB HAS SURFACE CORROSION AROUND FASTENERS HOLES.<[01] LOCATED AND DRILLED HOLES FOR NUT PLATES. ALODINE AND PRIMED HOLES. INSTALLED NEW NUT PLATES IAW SRM 51-40-02;[02] REMOVED OLD WEB AND ALLOCATED HOLES ON NEW SERVICEABLE
- [SDR SWAA2024121872029](https://openairdocs.org/sdr/SWAA2024121872029.md): Plate · corroded · Nov 26, 2024 · N8512U · Boeing 7378H4 · Cargo Compartments
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 500A-500B AROUND FASTENER HOLES.<[01] THE CORROSION IS OUT OF LIMIT PER SRM 53-00-53-1A-2.;[02] REMOVED FWD CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE STA.500A TO 5
- [SDR SWAA2024121872040](https://openairdocs.org/sdr/SWAA2024121872040.md): Plate · corroded · Nov 26, 2024 · N8512U · Boeing 7378H4 · Cargo Compartments
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 500B-500C AROUND FASTENER HOLES.<[01] TOOL UPDATE.;[02] THE CORROSION IS OUT OUT OF LIMIT PER SRM 53-00-53-1A-2.;[03] REMOVED AND REPLACED FWD CARGO RH TRANSITION ANGLE BETW
- [SDR SWAA2024121872031](https://openairdocs.org/sdr/SWAA2024121872031.md): Plate · corroded · Nov 26, 2024 · N8512U · Boeing 7378H4 · Cargo Compartments
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 500C TO 500D AROUND FASTENER HOLES.<[01] TOOL UPDATE.;[02] THE CORROSION IS OUT OF LIMIT PER SRM 53-00-53-1A-2.;[03] REMOVED AND REPLACED FWD CARGO RH TRANSITION ANGLE BETWE
- [SDR SWAA2024121872032](https://openairdocs.org/sdr/SWAA2024121872032.md): Plate · corroded · Nov 26, 2024 · N8512U · Boeing 7378H4 · Cargo Compartments
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 500D TO 500E AROUND FASTENER HOLES.<[01] TOOL UPDATE.;[02] THE CORROSION IS OUT OF LIMIT PER SRM 53-00-53-1A-2.;[03] REMOVED AND REPLACED FWD CARGO RH TRANSITION ANGLE BETWE
- [SDR SWAA2024121872033](https://openairdocs.org/sdr/SWAA2024121872033.md): Plate · corroded · Nov 26, 2024 · N8512U · Boeing 7378H4 · Cargo Compartments
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 500E TO 500F AROUND FASTENER HOLES.<[01] TOOL UPDATE.;[02] THE CORROSION IS OUT OF LIMIT PER SRM 53-00-53-1A-2.;[03] REMOVED AND REPLACED FWD CARGO RH TRANSITION ANGLE BETWE
- [SDR SWAA2024121872045](https://openairdocs.org/sdr/SWAA2024121872045.md): Angle · corroded · Nov 26, 2024 · N8512U · Boeing 7378H4 · Cargo Compartments
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 500F TO 500G AROUND FASTENER HOLES.<[01] TOOL UPDATE.;[02] THE CORROSION IS OUT OF LIMIT PER SRM 53-00-53-1A-2.;[03] REMOVED AND REPLACED FWD CARGO RH TRANSITION ANGLE BETWE
- [SDR SWAA2024121872034](https://openairdocs.org/sdr/SWAA2024121872034.md): Angle · corroded · Nov 26, 2024 · N8512U · Boeing 7378H4 · Cargo Compartments
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 500H TO 500I AROUND FASTENER HOLES.<[01] TOOL UPDATE.;[02] THE CORROSION IS OUT OF LIMIT PER SRM 53-00-53-1A-2.;[03] REMOVED AND REPLACED FWD CARGO RH TRANSITION ANGLE BETWE
- [SDR SWAA2024121872035](https://openairdocs.org/sdr/SWAA2024121872035.md): Intercostal · cracked · Nov 26, 2024 · N8512U · Boeing 7378H4 · Cargo Compartments
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE INTERCOSTAL WEB HAS CRACK @ STA 400. (MARKED)<[01] FABRICATED INTERCOSTAL WEB/BAFFLE P/N 143A7510-39 PER GRANTED SMAL AND BOEING DWG 143A7510.;[02] VERIFIED WORK COMPLETED IN CORRECTIVE ACTION #1 PER GRANT
- [SDR SWAA2024121872038](https://openairdocs.org/sdr/SWAA2024121872038.md): Angle · corroded · Nov 26, 2024 · N8512U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 480-500 AROUND FASTENER HOLES.<[01] BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMIT SRM 53-00-53-1A-2.;[02] REMOVED FWD CARGO COMPARTMENT L/H TRANSITION ANGLE FROM STA 400
- [SDR SWAA2024121872039](https://openairdocs.org/sdr/SWAA2024121872039.md): Angle · corroded · Nov 26, 2024 · N8512U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 500-500A AROUND FASTENER HOLES. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2. L/H TRANSITION ANGLE BEING REPLACED FROM BS 400 - 500I ON TTG8Q00
- [SDR SWAA2024121872027](https://openairdocs.org/sdr/SWAA2024121872027.md): Plate · corroded · Nov 26, 2024 · N8512U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 500A-500B AROUND FASTENER HOLES. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2. TRANSITION ANGLE REPLACED FROM BS 400 - 500I ON TTG8Q00XLZZH. PER
- [SDR SWAA2024121872028](https://openairdocs.org/sdr/SWAA2024121872028.md): Plate · corroded · Nov 26, 2024 · N8512U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 500B-500C AROUND FASTENER HOLES. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2. LT TRANSITION ANGLE REPLACED FROM BS 400 - 500I ON TTG8Q00XLZZH.

Next page: https://openairdocs.org/aircraft/N8512U/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 = 'N8512U' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8512U/reports

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