# Service difficulty reports: N8522P

A list on [N8522P](https://openairdocs.org/aircraft/N8522P.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 · 113 reports

- [SDR SWAA2026100117202](https://openairdocs.org/sdr/SWAA2026100117202.md): Lamp · inoperative · Sep 23, 2026 · N8522P · Boeing 7378H4 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT AT AFT DOOR IS INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT AFT SERVICE DOOR AND PERFORMED A GOOD INSTALLATION TEST IAW AMM TASK 33-51-04-960-801. VERIFIED TASK C/W.
- [SDR SWAA2026081097690](https://openairdocs.org/sdr/SWAA2026081097690.md): Handle · loose · Aug 4, 2026 · N8522P · Boeing 7378H4 · Service Doors
  > R1 DOOR HANDLE LOOSE. TIGHTENED HARDWARE ON DOOR HANDLE IAW AMM 52-41-31. OPS CHKD GOOD.
- [SDR SWAA2026072841242](https://openairdocs.org/sdr/SWAA2026072841242.md): Lens · missing · Jul 24, 2026 · N8522P · Boeing 7378H4 · Emergency Lighting
  > EXIT SIGN OVERHEAD ISLE MISSING. INSTALLED FWD MIDDLE LENS COVER IAW AMM 33-51-01.
- [SDR SWAA2026041488322](https://openairdocs.org/sdr/SWAA2026041488322.md): Sign · damaged · Apr 11, 2026 · N8522P · Boeing 7378H4 · Emergency Lighting
  > EXIT ROW SIGN ABOVE AISLE MISSING THE FRONT PART. RECOVERED FRONT OF EXIT SIGN FROM OVERHEAD BIN. REINSTALLED PER AMM 33-51-00 OPS CHECKED NORMAL.
- [SDR SWAA2026021670482](https://openairdocs.org/sdr/SWAA2026021670482.md): Skin · cracked · Feb 13, 2026 · N8522P · Boeing 7378H4 · Service Doors
  > RAMP REPORTS GROUND POWER DOOR WAS OPEN ON ARRIVAL. CRACK FOUND ON FUSELAGE SIDE OF DOOR MATING SURFACE. DAMAGED AREA MEASURES 3.00 INCH BY 0.5 INCH. REMOVED DAMAGED SKIN IAW M-24-153-01825 & APPLIED SPEED TAPE. REF. TTG8Q01AEGUJ.
- [SDR SWAA2026020667928](https://openairdocs.org/sdr/SWAA2026020667928.md): Sign · unsecure · Feb 5, 2026 · N8522P · Boeing 7378H4 · Emergency Lighting
  > OVERHEAD EXIT SIGN NEEDS TO BE SECURED. SECURED THE COVER IAW SIP. NO DEFECTS NOTED.
- [SDR SWAA2026010956205](https://openairdocs.org/sdr/SWAA2026010956205.md): Battery Pack · inoperative · Dec 28, 2025 · N8522P · Boeing 7378H4 · Emergency Lighting
  > ALL EMERGENCY LIGHTS COMMON TO M1695 EMERGENCY BATTERY PACK INOPERATIVE. REMOVED THE EMERGENCY LIGHT BATTERY PACK M1695 AND INSTALLED SERVICEABLE BATTERY PACK, PERFORMED A GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805.
- [SDR SWAA2026011255864](https://openairdocs.org/sdr/SWAA2026011255864.md): Tee Fitting · cracked · Dec 27, 2025 · N8522P · Boeing 7378H4 · Aerodynamic Fairings
  > PANEL 195AL FWD SUPPORT TEE FITTING CRACKED AT LOWER END BS 520. REMOVED PANEL 195AL FOR ACCESS IAW AMM 53-51-21-000-802. REMOVED AND REPLACED WING TO-BODY FIRING SUPPORT FRAME BS 520 IAW SRM 51-40-02 AND DWG 116A3010 REV: B. CLOSED PANEL 195AL IAW AMM 53-51
- [SDR SWAA2026011253532](https://openairdocs.org/sdr/SWAA2026011253532.md): Battery Pack · no test · Dec 17, 2025 · N8522P · Boeing 7378H4 · Emergency Lighting
  > FUNCTIONAL CHECK ALL EMERGENCY LIGHTS, ALL EMERGENCY LIGHTS TEST GOOD LESS LIGHTS COMMON TO M1695 BATTERY PACK. IAW AMM 33-51-00-710-801.
- [SDR SWAA2025111735586](https://openairdocs.org/sdr/SWAA2025111735586.md): Flashlight · no test · Nov 15, 2025 · N8522P · Boeing 7378H4 · Emergency Equipment
  > AFT / CAPT SIDE I/B FLASHLIGHT WONT TEST. R & R AFT, INBD FLASHLIGHT IAW AMM 25-64-00. OPS CHECKED GOOD.
- [SDR SWAA2025111033651](https://openairdocs.org/sdr/SWAA2025111033651.md): Unknown · odor · Nov 8, 2025 · N8522P · Boeing 7378H4 · Air Distribution System
  > UNIDENTIFIED ODD SMELL AT FWD GALLEY. PERFORMED FUMES IN CABIN CONDITIONAL INSPECTION IAW AMM 05-51-56. NO DEFECTS FOUND.
- [SDR SWAA2025071190351](https://openairdocs.org/sdr/SWAA2025071190351.md): Light · loose · Jul 10, 2025 · N8522P · Boeing 7378H4 · Emergency Lighting
  > CREW REPORTS: FLOOR PROX. PHOTO. STRIP LOOSE AT ROWS 11-12. SECURED SAME. ALL GOOD. REF AMM 33-51-15
- [SDR SWAA2025032407691](https://openairdocs.org/sdr/SWAA2025032407691.md): Radome · cracked · Mar 19, 2025 · N8522P · Boeing 7378H4 · Aerodynamic Fairings
  > FOUND CRACK ON CENTER OF NOSE RADOME<[01] FOUND TO BE DAMAGE LIMITED TO EROSION BOOT. REPAIRED PER EA M-21-153-01060-REPREF;[02] FOUND TO BE DAMAGE LIMITED TO EROSION BOOT. REPAIRED PER EA M-21-153-01060-REPREF
- [SDR SWAA2025031907347](https://openairdocs.org/sdr/SWAA2025031907347.md): Sign · detached · Mar 19, 2025 · N8522P · Boeing 7378H4 · Emergency Lighting
  > FOUND EMERGENCY EXIT SIGN ON AFT PILOTS SIDE LAV DETACHED<[01] RESECURED AFT PILOTS SIDE EMERGENCY EXIT SIGN REF. AMM 33-51-01
- [SDR SWAA2025022800337](https://openairdocs.org/sdr/SWAA2025022800337.md): Flashlight · failed · Feb 26, 2025 · N8522P · Boeing 7378H4 · Emergency Equipment
  > CAPTAIN SIDE AFT FA FLASHLIGHT WILL NOT TEST<[01], REMOVED AND REPLACED FLASHLIGHT ASSY IAW M/M 25-64-00.
- [SDR SWAA2025022699501](https://openairdocs.org/sdr/SWAA2025022699501.md): Light · detached · Feb 24, 2025 · N8522P · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY FLOOR LIGHT TRACK COVER LIFTING IN ROW 12<[01] RESECURED TRACK AT ROW 12 AS NEEDED REF AMM 33-51-12
- [SDR SWAA2025022598075](https://openairdocs.org/sdr/SWAA2025022598075.md): Battery · inoperative · Feb 20, 2025 · N8522P · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1675 WILL NOT CHARGE <[01]. REMOVED & REPLACED BATTERY IAW AMM 33-51-06-960-805. OPS CHECK GOOD.; [02] AUDIT C/W.
- [SDR SWAA2025022598076](https://openairdocs.org/sdr/SWAA2025022598076.md): Battery · inoperative · Feb 20, 2025 · N8522P · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1676 WILL NOT CHARGE <[01]. REMOVED & REPLACED BATTERY IAW AMM 33-51-06-960-805. OPS CHECK GOOD.; [02] AUDIT C/W.
- [SDR SWAA2025022598077](https://openairdocs.org/sdr/SWAA2025022598077.md): Battery · inoperative · Feb 20, 2025 · N8522P · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1694 WILL NOT CHARGE <[01]. REMOVED & REPLACED BATTERY IAW AMM 33-51-06-960-805. OPS CHECK GOOD.; [02] AUDIT C/W.
- [SDR SWAA2025022598078](https://openairdocs.org/sdr/SWAA2025022598078.md): Battery · inoperative · Feb 20, 2025 · N8522P · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1670 WILL NOT CHARGE <[01]. REMOVED & REPLACED BATTERY IAW AMM 33-51-06-960-805. OPS CHECK GOOD.; [02] AUDIT C/W.
- [SDR SWAA2025022598079](https://openairdocs.org/sdr/SWAA2025022598079.md): Battery · inoperative · Feb 20, 2025 · N8522P · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1671 WILL NOT CHARGE <[01]. REMOVED & REPLACED BATTERY IAW AMM 33-51-06-960-805. OPS CHECK GOOD.; [02] AUDIT C/W.
- [SDR SWAA2025022593356](https://openairdocs.org/sdr/SWAA2025022593356.md): Scuff Plate · cracked · Feb 5, 2025 · N8522P · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE IS CRACKED <[01]. CRACKS ON FWD CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE WAS REPAIRED ON BACK SHOP WORK ORDER 46321/1400/0002 SERIAL NO: 9541388 SHOP WELD IAW SRM 53-30-15-2R-1; [02] VERIFIED ITEM 1 C/W.
- [SDR SWAA2025022593355](https://openairdocs.org/sdr/SWAA2025022593355.md): Scuff Plate · cracked · Feb 5, 2025 · N8522P · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE IS CRACKED <[01]. CRACK ON FWD CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE WAS REPAIRED ON BACK SHOP WORK ORDER 46321/1400/0001 SERIAL NO: 9541387 SHOP WELD IAW SRM 53-30-15-2R-1; [02] VERIFIED ITEM 1 C/W.
- [SDR SWAA2025022592219](https://openairdocs.org/sdr/SWAA2025022592219.md): Handle · broken · Feb 1, 2025 · N8522P · Boeing 7378H4 · Galley Doors
  > R2 DOOR; ASSIST HANDLE BROKEN. <[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)] ATAG: A293801 P/N: 65-5458-20N ATAG: A293797 P/N: 65-5458-21N ATAG: A80299 P/N: 65-5458-21N; [02]
- [SDR SWAA2025022591137](https://openairdocs.org/sdr/SWAA2025022591137.md): Wire · damaged · Jan 30, 2025 · N8522P · Boeing 7378H4 · Emergency Lighting
  > AFT CARGO PIT OVERWING ESCAPE GROUND LIGHT HAS DAMAGED WIRES W3142-0331-16 AND W3142-0353-16 AT STA 727F <[01]. SPLICED WIRES W3142-0331-16 AND W3142-0353-16 AT L547 IAW SWPM 20-30-12 AND WDM 33-51-13; OPS CHECK 33-51-06-960-805. OPS CHECK GOOD; [02] VERIFIE
- [SDR SWAA2025022599590](https://openairdocs.org/sdr/SWAA2025022599590.md): Wire · damaged · Jan 30, 2025 · N8522P · Boeing 7378H4 · Emergency Lighting
  > AFT CARGO PIT OVERWING ESCAPE GROUND LIGHT HAS DAMAGED WIRES W3142-0331-16 AND W3142-0353-16 AT STA 727F <[01]. SPLICED WIRES W3142-0331-16 AND W3142-0353-16 AT L547 IAW SWPM 20-30-12 AND WDM 33-51-13; OPS CHECK 33-51-06-960-805. OPS CHECK GOOD; [02] VERIFIE
- [SDR SWAA2025022590999](https://openairdocs.org/sdr/SWAA2025022590999.md): Floor Panel · pulled · Jan 29, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT#28 A-043 AFT CABIN FLOOR PANEL 241WF HAS PULLED FIBERS <[01]. REPAIRED IAW EA 25-153-00249 AND SRM 53-00-50-2R-1.;[ 02] C/W. AUDIT COMPLETE.
- [SDR SWAA2025022590993](https://openairdocs.org/sdr/SWAA2025022590993.md): Floor Panel · pulled · Jan 29, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT#36 A-043 AFT CABIN FLOOR PANEL 241ZF HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W. AUDIT COMPLETE.
- [SDR SWAA2025022590997](https://openairdocs.org/sdr/SWAA2025022590997.md): Floor Panel · pulled · Jan 29, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT#41 A-043 AFT CABIN FLOOR PANEL 241ABF HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W. AUDIT COMPLETE.
- [SDR SWAA2025022591005](https://openairdocs.org/sdr/SWAA2025022591005.md): Floor Panel · pulled · Jan 29, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT#42 A-043 AFT CABIN FLOOR PANEL 241AAF HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W. AUDIT COMPLETE.
- [SDR SWAA2025022591096](https://openairdocs.org/sdr/SWAA2025022591096.md): Floor Panel · corroded · Jan 29, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT L7-005: AFT CARGO FLOOR PANEL 140BF HAS CORROSION AT FASTENER HOLES<[01] EVALUATED CORROSION ON FLOOR PANEL 140BF WITH THE TOTAL ACCUMULATED DAMAGE LENGTH IS 32' WERE IS A MAXIMUM OF 20' ON ALLOWABLE DAMAGE; THEREFORE IS OUT OF LIMITS; MECHANICALLY MEASURE
- [SDR SWAA2025022591098](https://openairdocs.org/sdr/SWAA2025022591098.md): Floor Panel · pulled · Jan 29, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT L7-006: AFT CARGO FLOOR PANEL 140EF HAS CORROSION AT FASTENER HOLES<[01] FABRICATED NEW FLOOR PNL. 140EF IAW AMM 25-52-10-400-801;[02] VERIFIED STEP 1.<BR>AUDIT C/W
- [SDR SWAA2025022591099](https://openairdocs.org/sdr/SWAA2025022591099.md): Floor Panel · corroded · Jan 29, 2025 · N8522P · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > DOT L7-007: AFT CARGO FLOOR PANEL 140CF HAS CORROSION AT FASTENER HOLES <[01]. FABRICATED NEW FLOOR PNL 140CF I.A.W AMM 25-52-01-201-801; [02] AUDIT C/W.
- [SDR SWAA2025022190990](https://openairdocs.org/sdr/SWAA2025022190990.md): Floor Panel · pulled · Jan 29, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT#29 A-043 AFT CABIN FLOOR PANEL 241UF HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.'; [02] C/W AUDIT COMPLETE.; [03] C/W AUDIT COMPLETE.
- [SDR SWAA2025022191002](https://openairdocs.org/sdr/SWAA2025022191002.md): Floor Panel · pulled · Jan 29, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT#33 A-043 AFT CABIN FLOOR PANEL 242UF HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W AUDIT COMPLETE.
- [SDR SWAA2025022191003](https://openairdocs.org/sdr/SWAA2025022191003.md): Floor Panel · pulled · Jan 29, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT#34 A-043 AFT CABIN FLOOR PANEL 242D HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W AUDIT COMPLETE.
- [SDR SWAA2025022190992](https://openairdocs.org/sdr/SWAA2025022190992.md): Floor Panel · pulled · Jan 29, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT#35 A-043 AFT CABIN FLOOR PANEL 241XF HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W AUDIT COMPLETE.
- [SDR SWAA2025022190994](https://openairdocs.org/sdr/SWAA2025022190994.md): Floor Panel · pulled · Jan 29, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT#37 A-043 AFT CABIN FLOOR PANEL 241D HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W. AUDIT COMPLETE.
- [SDR SWAA2025022190998](https://openairdocs.org/sdr/SWAA2025022190998.md): Floor Panel · pulled · Jan 29, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT#43 A-043 AFT CABIN FLOOR PANEL 242F HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.'; [02] C/W; [03] C/W. AUDIT COMPLETE.
- [SDR SWAA2025022191006](https://openairdocs.org/sdr/SWAA2025022191006.md): Floor Panel · pulled · Jan 29, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT#44 A-043 AFT CABIN FLOOR PANEL 241F HAS PULLED FIBERS<[01] 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W. AUDIT COMPLETE.
- [SDR SWAA2025022690579](https://openairdocs.org/sdr/SWAA2025022690579.md): Seal · debonded · Jan 28, 2025 · N8522P · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > DOT A24-1 R/H HORIZONTAL STABILIZER; LOWER T/E SEAL 344BB FABRIC IS DISBONDED FROM BASE.<[01] REPLACED ON SITE - R/H HORIZONTAL STABILIZER LOWER T/E SEAL 344 BB IAW B737-800 SRM 51-40-02-0G-0;[02] ISSUED TAG: WN 49734;[03] CORRECTION OF ITEM 1-2:<BR><BR>REPLAC
- [SDR SWAA2025022690483](https://openairdocs.org/sdr/SWAA2025022690483.md): Winglet · corroded · Jan 28, 2025 · N8522P · Boeing 7378H4 · Wing Main, Frame Structure
  > DOT#26 A-043 LH WINGLET CORRODED ON AFT OTBD EDGE 10' FROM TOP EDGE<[01] AUDIT C/W
- [SDR SWAA2025022590480](https://openairdocs.org/sdr/SWAA2025022590480.md): Floor Panel · corroded · Jan 28, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT L7-004: FWD CARGO FLOOR PANEL 120BF HAS COOROSION AT FASTENER HOLES AND MULTIPLE DENTS <[01]. CORROSION AROUND SEVERAL FASTENER HOLES AND MULTIPLE LARGE DENTS. VERIFIED CORROSION AND DENTS ARE OUT OF LIMITS IAW SRM 53-00-53-1A-1. VERIFIED MATERIAL IAW SRM
- [SDR SWAA2025022590580](https://openairdocs.org/sdr/SWAA2025022590580.md): Seal · debonded · Jan 28, 2025 · N8522P · Boeing 7378H4 · Horizontal Stabilizer Structure
  > DOT A24-3 R/H HORIZONTAL STABILIZER; LOWER T/E SEAL 344DB FABRIC IS DISBONDED FROM BASE. <[01] RECEIVED NEW R/H HORIZONTAL STABILIZER; LOWER T/E SEAL 344DB FROM STORES. VERIFIED PN 185A1621-122 IAW B 737-800 AIPC 27-41-11-08. T/E SEAL 344 DB WILL BE INSTALLED
- [SDR SWAA2025022590581](https://openairdocs.org/sdr/SWAA2025022590581.md): Seal · debonded · Jan 28, 2025 · N8522P · Boeing 7378H4 · Horizontal Stabilizer Structure
  > DOT A24-2 R/H HORIZONTAL STABILIZER; LOWER T/E SEAL 344AB FABRIC IS DISBONDED FROM BASE. <[01] RECIEVED NEW R/H HORIZONTAL STABILIZER; LOWER T/E SEAL 344AB FROM STORES. VERIFIED PN 185A1621-110 IAW AIPC B 737-800 27-41-11-08. T/E SEAL 344 AB WILL BE INSTALLED
- [SDR SWAA2025022190479](https://openairdocs.org/sdr/SWAA2025022190479.md): Floor Panel · corroded · Jan 28, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT L7-003: FWD CARGO FLOOR PANEL 120CF HAS CORROSION AT FASTENER HOLES<[01] CORROSION ON FLOOR PANEL IS FOUND TO BE OUT OF LIMITS I.A.W. SRM 53-00-53-1A-1 MATERIAL VERIFICATION FOR ALUMINUM WITH P/N 2024-T3-071 SHEET AND ATAG A276640 I.A.W. AMM 25-52-10-400-8
- [SDR SWAA2025022090481](https://openairdocs.org/sdr/SWAA2025022090481.md): Floor Panel · corroded · Jan 28, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT L7-001: FWD CARGO FLOOR PANEL 120AF HAS COOROSION AT FASTENER HOLES<[01] VERIFIED LIMITS; 3' BETWEEN DAMAGE (ALLOWABLE DAMAGE IS MINIMUN OF 5' BETWEEN DAMAGE) THEREFORE IS FOUND OUT OF LIMITS I.A.W. SRM 53-00-53-1A-1<BR><BR>FABRICATED NEW FLOOR PANEL 120AF
- [SDR SWAA2025022090482](https://openairdocs.org/sdr/SWAA2025022090482.md): Floor Panel · corroded · Jan 28, 2025 · N8522P · Boeing 7378H4 · Fuselage Floor Panel
  > DOT L7-002: FWD CARGO FLOOR PANEL 120DF HAS COOROSION AT FASTENER HOLES AND MULTIPLE DENTS<[01] UPON FURTHER INVESTIGATION FOUND THERE TO BE MULTIPLE DENTS THAT ARE OUT OF LIMITS AND 46 INCHES OF CORROSION WITH MAX ALLOWED LENGTH OF CORROSION BEING 3 INCHES FO
- [SDR SWAA2025022090046](https://openairdocs.org/sdr/SWAA2025022090046.md): Angle · corroded · Jan 27, 2025 · N8522P · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > DOT#07 A-043 AFT CARGO COMPARTMENT LH Z ANGLE CORRODED STA 727D TO 727I+12' LBL 21 WL 156<[01] 04 - REPAIRED LH ZEE ANGLE BETWEEN STA 727D TO 727I+12' AT LBL 21 AND WL 156 PER [SRM 53-00-53-2R-5-B00308 (REPAIR 5 - CARGO COMPARTMENT SIDEPLATE REPAIR BETWEEN FLO
- [SDR SWAA2025022090051](https://openairdocs.org/sdr/SWAA2025022090051.md): Shield · corroded · Jan 27, 2025 · N8522P · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > DOT#09 A-043 AFT CARGO COMPARTMENT RH FWD SHIELD CORRODED ON TOP AND BOTTOM STA 767 TO 787 RBL 21 WL 156<[01] REMOVED AND REPLACED AFT CARGO RH FWD SHIELD I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 146A0081; SHEET 49; REV A.

Next page: https://openairdocs.org/aircraft/N8522P/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 = 'N8522P' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8522P/reports

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