# Service difficulty reports: N563WN
A list on [N563WN](https://openairdocs.org/aircraft/N563WN.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 5 · 221 reports
- [SDR SWAA2026101901367](https://openairdocs.org/sdr/SWAA2026101901367.md): Support Bracket · delaminated · Oct 14, 2026 · N563WN · Boeing 737752 · Trailing Edge Flaps
> RIGHT WING NR 8 FLAP FWD CANOE FAIRING FWD SUPPORT BRACKET RUBBER BOLT ISOLATOR IS DELAMINATED. REMOVED AND REPLACED R/H WING #8FLAP FWD CANOE FAIRING FITTING ASSY IAW AMM 20-50-11.
- [SDR SWAA2026101988531](https://openairdocs.org/sdr/SWAA2026101988531.md): Rope · out of position · Oct 14, 2026 · N563WN · Boeing 737752 · Emergency Equipment
> RIGHT OVERWING EXIT ROPE NEEDS TO BE RESTOWED. RESTOWED RT OVERWING EXIT ROPE IAW AMM 25-61-10-400-802.
- [SDR SWAA2026091458590](https://openairdocs.org/sdr/SWAA2026091458590.md): Battery Pack · inoperative · Sep 10, 2026 · N563WN · Boeing 737752 · Emergency Lighting
> FOUND AFT LT DOORWAY, RIGHT RT ESCAPE SLIDE & AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT M1673 LOCATION IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2026050495220](https://openairdocs.org/sdr/SWAA2026050495220.md): Spacer · missing · May 2, 2026 · N563WN · Boeing 737752 · Passenger Compartment Equipment
> SEAT 14F WILL NOT STAY IN UPRIGHT POSITION. SEAT BACK WILL STAY UPRIGHT WHEN NOT OCCUPAID;SEAT NOT USABLE. OK TO CONTINUE PER MEL 25-6-01 ALL 3 SEATS INOP 14 DEF. FOUND SEAT 14F TO BE MISSING SPACER; WASHER AND NUT ON THROUGH BOLT FOR BACK ASSEMBLY. REINST
- [SDR SWAA2026041789958](https://openairdocs.org/sdr/SWAA2026041789958.md): Lamp · inoperative · Apr 16, 2026 · N563WN · Boeing 737752 · Emergency Lighting
> RIGHT EXTERIOR SLIDE POSITION EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 3-51-04.
- [SDR SWAA2025112037086](https://openairdocs.org/sdr/SWAA2025112037086.md): Power Supply · inoperative · Nov 20, 2025 · N563WN · Boeing 737752 · Emergency Lighting
> MULTIPLE EMERGENCY LIGHTS INOPERATIVE. R & R POWER SUPPLY AT BS 727 LT IAW AMM 33-51-06. OP CHECKED GOOD.
- [SDR SWAA2025103129722](https://openairdocs.org/sdr/SWAA2025103129722.md): Bulb · inoperative · Oct 29, 2025 · N563WN · Boeing 737752 · Emergency Lighting
> CABIN EMERGENCY LIGHTS INOP AT SEATS 11D AND 17A. R&R CABIN EMERGENCY LIGHT BULBS ABOVE SEATS 11DEF AND 17ABC PER AMM 33-51-03.
- [SDR SWAA2025051571256](https://openairdocs.org/sdr/SWAA2025051571256.md): Flap Track · loose · May 8, 2025 · N563WN · Boeing 737752 · Trailing Edge Flaps
> RIGHT WING I/B AFT FLAP O/B TRACK LOWER ATTACHED BEARING LOOSE FROM TRACK.<[01] R AND R RIGHT WING I/B AFT FLAP O/B TRACK IN REF AMM 27-51-16;[02] CORRECTED MEASUREMENT -FAILURE TYPE REPAIR FROM MINOR TO MAJOR; ON BEHALF OF AMT.
- [SDR SWAA2025012890112](https://openairdocs.org/sdr/SWAA2025012890112.md): Engine · fire · Jan 27, 2025 · N563WN · Boeing 737752 · Engine (Turbine/Turboprop)
> COMPANY AIRCRAFT REPORTED A FIRE COMING OUT OF THE #2 ENGINE DURING. TAXI. RAN THE QRH FOR TAIL-PIPE FIRE AND IT WENT OUT.<[01] PERFORMED CONDITIONAL INSPECTION AMM#TASK 05-51-49. RAN ENGINE #2 PER AMM#71-00-00; TO FLUSH OUT OIL ACCUMULATED AT CENTER PLUG CAVI
- [SDR SWAA2025010682931](https://openairdocs.org/sdr/SWAA2025010682931.md): Bulb · failed · Jan 3, 2025 · N563WN · Boeing 737752 · Passenger Compartment Lighting
> FA REPORTS ACRID SMELL NEAR FWD GALLEY<[01] PERFORMED SMOKE/FUME CONDITIONAL INSPECTION PER AMM 05-51?56. FOUND BAD LIGHT BULB AND REPLACED REFERENCE LOG PAGE 2577464.
- [SDR SWAA2024120658459](https://openairdocs.org/sdr/SWAA2024120658459.md): Rib · cracked · Nov 10, 2024 · N563WN · Boeing 737752 · Horizontal Stabilizer Structure
> CRACK INSPAR RIB LOCATED STAB STA 120.30 LOWER CORD OUTBOARD SIDE OF THE FROM SPAR AT RT HORIZONTAL STABILIZER 2024-680457<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3015GOES00000 S/N 142811019 DUE DATE 23
- [SDR SWAA2024120571586](https://openairdocs.org/sdr/SWAA2024120571586.md): Angle · worn · Nov 3, 2024 · N563WN · Boeing 737752 · Wing Main, Frame Structure
> WEAR ON ANGLE LOCATED BS540 PLUS 9INCH AND RBL40 AT CENTER WING BOX 2024-680424<[01] ON STEP 5: TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X11290U021704; DUE DATE: 14 APR 25;[02] REPAIRED ANGLE LOCATED BS540 PLUS 9INCH AND RBL40 AT CENTER WING BO
- [SDR SWAA2024120555947](https://openairdocs.org/sdr/SWAA2024120555947.md): Web · corroded · Nov 2, 2024 · N563WN · Boeing 737752 · Cargo Compartments
> CORROSION WEB LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT 2024-680400<[01] REPLACED SHIELD WEB LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146A00
- [SDR SWAA2024120555956](https://openairdocs.org/sdr/SWAA2024120555956.md): Angle · cracked · Nov 2, 2024 · N563WN · Boeing 737752 · Fuselage Miscellaneous Structure
> CRACK ANGLE LOCATED BS540 AND LBL1 AT PASSENGER CABIN 2024-680405<[01] REPLACED ANGLE LOCATED BS540 AND LBL1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG:143A0060 SHEET:44 REV:4.
SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP
- [SDR SWAA2024120555957](https://openairdocs.org/sdr/SWAA2024120555957.md): Angle · cracked · Nov 2, 2024 · N563WN · Boeing 737752 · Fuselage Miscellaneous Structure
> CRACK ANGLE LOCATED BS540 AND RBL1 AT PASSENGER CABIN 2024-680407<[01] REPLACED ANGLE LOCATED BS540 AND RBL 24 TO LB0 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG:143A0060 SHEET:44 REV:4.
SEE INDIVIDUAL SIGN OFF BELOW;[02] CORR
- [SDR SWAA2024120555948](https://openairdocs.org/sdr/SWAA2024120555948.md): Stinger · cracked · Nov 2, 2024 · N563WN · Boeing 737752 · Fuselage Main, Longeron/Stringer
> CRACK STRINGER 23R LOCATED BS 540 AT FWD CARGO COMPARTMENT 2024-680397<[01] TOOL USED: UT EQUIPMENT. P/N: 45MG; S/N: 232017609; CAL DUE DATE: 08-OCT-25;[02] EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[03] REPAIRED STRINGER 23R LOCATED
- [SDR SWAA2024120555949](https://openairdocs.org/sdr/SWAA2024120555949.md): Stringer · cracked · Nov 2, 2024 · N563WN · Boeing 737752 · Fuselage Main, Longeron/Stringer
> CRACK STRINGER 25R LOCATED BS 540 AT FWD CARGO COMPARTMENT 2024-680398<[01] TOOL USED: UT EQUIPMENT. P/N: 45MG; S/N: 232017609; CAL DUE DATE: 08-OCT-25;[02] EQUIPMENT USED P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 11-MAR-25;[03] PERFORMED PERMANENT REPAIR
- [SDR SWAA2024120555950](https://openairdocs.org/sdr/SWAA2024120555950.md): Stringer · cracked · Nov 2, 2024 · N563WN · Boeing 737752 · Fuselage Main, Longeron/Stringer
> CRACK STRINGER 26L LOCATED BS 540 AT FWD CARGO COMPARTMENT 2024-680399<[01] TOOL USED: UT EQUIPMENT. P/N: 45MG; S/N: 232017609; CAL DUE DATE: 08-OCT-25;[02] TOOL USED: ET EQUIPMENT; P/N: NORTEC600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[03] REPAIRED STRIN
- [SDR SWAA2024120455953](https://openairdocs.org/sdr/SWAA2024120455953.md): Frame · cracked · Nov 2, 2024 · N563WN · Boeing 737752 · Fuselage Main, Frame
> CRACK FRAME LOCATED BS400 AND STR8L TO STR9L AT PASSENGER CABIN 2024-680403<[01] REPAIRED FRAME LOCATED BS400 AND STR8L TO STR9L AT PASSENGER CABIN IAW EA 24-153-03279-WIP1 AND EA 24-153-03279.
SEE INDIVIDUAL SIGN OFF BELLOW;[02] REPAIRED FRAME LOCATED BS4
- [SDR SWAA2024120455954](https://openairdocs.org/sdr/SWAA2024120455954.md): Frame · cracked · Nov 2, 2024 · N563WN · Boeing 737752 · Fuselage Main, Frame
> CRACK FRAME LOCATED BS380 AND STR8L TO STR9L AT PASSENGER CABIN 2024-680402<[01] REPAIRED FRAME LOCATED BS380 AND STR8L TO STR9L AT PASSENGER CABIN IAW EA 24-153-03257-WIP AND EA 24-153-03257.
SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPAIRED FRAME LOCATED BS380
- [SDR SWAA2024120455952](https://openairdocs.org/sdr/SWAA2024120455952.md): Frame · cracked · Nov 2, 2024 · N563WN · Boeing 737752 · Fuselage Main, Frame
> CRACK FRAME LOCATED BS440 AND STR8L TO STR9L AT PASSENGER CABIN 2024-680404<[01] PERFORM REPAIR FRAME LOCATED BS440 AND STR8L TO STR9L AT PASSENGER CABIN IAW EA 24-153-03262-WIP1 AND EA 24-153-03262
SEE INDIVIDUAL SIGN OFF BELOW.;[02] PERFORM REPAIR FRAME
- [SDR SWAA2024120555738](https://openairdocs.org/sdr/SWAA2024120555738.md): Structure · cracked · Nov 1, 2024 · N563WN · Boeing 737752 · Fuselage Miscellaneous Structure
> CRACK INNER CHORD LOCATED BS 303.9 AT LEVEL STR17L AT FWD GALLEY AREA 2024-680375<[01] REPLACED INNER CHORD LOC. BETWEEN BS 360 TO BS 377 LBL57 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND #DWG: 141A8110 SHEET: 11 REV:- #DWG: 142A0050 SHEET: 15 REV
- [SDR SWAA2024120455737](https://openairdocs.org/sdr/SWAA2024120455737.md): Web · cracked · Nov 1, 2024 · N563WN · Boeing 737752 · Fuselage Main, Structure
> CRACK ON WEB LOCATED BETWEEN BS 294.5 TO BS 303.9 AT LEVEL STR16L AT PASSENGER CABIN 2024-680374<[01] REPAIRED INTERCOSTAL WEB LOCATED BETWEEN BS 294.5 TO BS 303.9 AT LEVEL STR16L AT PASSENGER CABIN IAW EA 24-153-03103-WIP1 AND 24-153-03103.
SEE INDIVIDUAL
- [SDR SWAA2024120455736](https://openairdocs.org/sdr/SWAA2024120455736.md): Frame · cracked · Nov 1, 2024 · N563WN · Boeing 737752 · Fuselage Main, Frame
> CRACK ON FRAME LOCATED BS 259.5 AT LEVEL STR9R AT PASSENGER CABIN 2024-680373<[01] TOOL USED P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 14-APR-25.;[02] PERFORMED REPAIR ON FRAME LOC. BS259.5 AT PASSENGER CABIN BETWEEN STR 5R TO STR 12R IAW EA 24-153-031
- [SDR SWAA2024120655603](https://openairdocs.org/sdr/SWAA2024120655603.md): Rib · cracked · Oct 31, 2024 · N563WN · Boeing 737752 · Horizontal Stabilizer Structure
> CRACK INSPAR RIB LOCATED STAB STA120.30 STIFFENER 2 AT RT HORIZONTAL STABILIZER 2024-680368 CRACK INSPAR RIB LOCATED STAB STA120.30 STIFFENER 3 AT RT HORIZONTAL STABILIZER 2024-680369<[01] TOOL USED: ET EQUIPMENT; P/N: NORTEC600D; S/N: 60009161631; CAL DUE DATE:11-MAR-25;[02] TOOL USED: ET EQUIPMENT; P/N: NORTEC600D; S/N: 60007161486; CAL DUE DATE: 0
- [SDR SWAA2024120655604](https://openairdocs.org/sdr/SWAA2024120655604.md): Rib · cracked · Oct 31, 2024 · N563WN · Boeing 737752 · Horizontal Stabilizer Structure
> CRACK INSPAR RIB LOCATED STAB STA120.30 STIFFENER 4 AT RT HORIZONTAL STABILIZER 2024-680370<[01] TOOL USED: ET EQUIPMENT; P/N: NORTEC600D; S/N: 60009161631; CAL DUE DATE:11-MAR-25;[02] TOOL USED: ET EQUIPMENT; P/N NORTEC600D; S/N: 60007161486; CAL DUE DATE: 06
- [SDR SWAA2024120655329](https://openairdocs.org/sdr/SWAA2024120655329.md): Rail · corroded · Oct 31, 2024 · N563WN · Boeing 737752 · Wing Miscellaneous Structure
> CORROSION RAIL NUT PLATE LEADING EDGE LOCATED OFSS568 AT LT WING 2024-680357<[01] REPLACED RAIL NUT PLATE ON LEADING EDGE LOCATED OFSS568 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.
SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED COMPLETE TAS
- [SDR SWAA2024120654747](https://openairdocs.org/sdr/SWAA2024120654747.md): Panel · cracked · Oct 29, 2024 · N563WN · Boeing 737752 · Trailing Edge Flaps
> CRACK ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2024-680262<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: B20189443 DUE DATE: 06-MAR-25.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 25-JAN-25.;[03] TOOL USED: ULTRASONIC FLAW DETECTOR P/
- [SDR SWAA2024120554555](https://openairdocs.org/sdr/SWAA2024120554555.md): Angle · cracked · Oct 29, 2024 · N563WN · Boeing 737752 · Cargo Compartments
> CRACK ANGLE LOCATE BS 500A LBL 21 AND WL 156 FWD FACE POSITION AT FWD CARGO COMPARTMENT 2024-680252<[01] REPLACED ANGLE LOCATED BS 500A LBL 21 AND WL 156 FWD FACE POSITION AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02; DWG 143A7505
- [SDR SWAA2024120554556](https://openairdocs.org/sdr/SWAA2024120554556.md): Angle · cracked · Oct 29, 2024 · N563WN · Boeing 737752 · Cargo Compartments
> CRACK ANGLE LOCATE BS 500C RBL 21 AND WL 156 FWD FACE POSITION AT FWD CARGO COMPARTMENT 2024-680253<[01] REPLACED ANGLE LOCATE BS 500C RBL 21 AND WL 156 FWD FACE POSITION AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7505 SHEET:
- [SDR SWAA2024120554557](https://openairdocs.org/sdr/SWAA2024120554557.md): Angle · cracked · Oct 29, 2024 · N563WN · Boeing 737752 · Cargo Compartments
> CRACK ANGLE LOCATE BS 500C LBL 21 AND WL 156 FWD FACE POSITION AT FWD CARGO COMPARTMENT 2024-680254<[01] REPLACED ANGLE LOCATE BS 500C LBL 21 AND WL 156 FWD FACE POSITION AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 143A75
- [SDR SWAA2024120554553](https://openairdocs.org/sdr/SWAA2024120554553.md): Gusset · cracked · Oct 29, 2024 · N563WN · Boeing 737752 · Cargo Compartments
> CRACK GUSSET LOCATE BS 500D AND STR 19L FWD CARGO COMPARTMENT 2024-680255<[01] REPLACED GUSSET LOCATED BS 500D AND STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 DWG 143A7902-162 REV -. SEE INDIVIDUAL SIGNS OFF BELOW;[02] REPLACED GUS
- [SDR SWAA2024120554554](https://openairdocs.org/sdr/SWAA2024120554554.md): Angle · cracked · Oct 29, 2024 · N563WN · Boeing 737752 · Cargo Compartments
> CRACK ANGLE LOCATE BS 420 RBL 21 AND WL 156 FWD FACE POSITION AT FWD CARGO COMPARTMENT 2024-680256<[01] REPLACED ANGLE LOCATE BS 420 RBL 21 AND WL 156 FWD FACE POSITION AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG #143A1212 SHEE
- [SDR SWAA2024120554183](https://openairdocs.org/sdr/SWAA2024120554183.md): Panel · elongated · Oct 28, 2024 · N563WN · Boeing 737752 · Cargo Compartments
> ELONGATED HOLE BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT 2024-680136<[01] FABRICATED BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 STEP 1 F AND DWG 453A2510; SHEET 9; REV A MATERIAL USED P/N A31RG4W PO: 2024-142584 SEE INS
- [SDR SWAA2024120554184](https://openairdocs.org/sdr/SWAA2024120554184.md): Panel · cracked · Oct 28, 2024 · N563WN · Boeing 737752 · Cargo Compartments
> CRACK BULKHEAD PANEL 142NW AT AFT CARGO COMPARTMENT 2024-680138<[01] TOOL USED:CALIPER P/N: 500-197-30; S/N: A23217620; DUE DATE: 02-MAR-25.;[02] REPAIRED BULKHEAD PANEL 142NW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-00-200-806 PARAGRAPH 6.D (3) (D);
- [SDR SWAA2024120554385](https://openairdocs.org/sdr/SWAA2024120554385.md): Lens · missing · Oct 28, 2024 · N563WN · Boeing 737752 · Emergency Lighting
> MISSING LENS EMERGENCY LIGHT ON OVERHEAD STOWAGE BIN 8 RT SIDE AT PASSENGER CABIN (1EA) 2024-680235<[01] INSTALLED LENS EMERGENCY LIGHT ON OVERHEAD STOWAGE BIN 8 RT SIDE AT PASSENGER CABIN (1EA) I.A.W B737-700 AMM 33-51-03-960-801 STEP 2.D(3)(A) AND STEP 2.D(3
- [SDR SWAA2024120554066](https://openairdocs.org/sdr/SWAA2024120554066.md): Scuff Plate · cracked · Oct 28, 2024 · N563WN · Boeing 737752 · Cargo Compartments
> CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2024-680118<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30;S/N:B23399190;DUE DATE:04-MAR-25;[02] EQUIPMENT P/N XRP-3000; S/N 1753759; DUE DATE 07-DEC-24 WAS USED ON STEP 4;[03] REPAIRED SCUFF PLATE AFT CORNE
- [SDR SWAA2024101748479](https://openairdocs.org/sdr/SWAA2024101748479.md): Cover · loose · Oct 14, 2024 · N563WN · Boeing 737752 · Passenger/Crew Doors
> METAL PLATE ON FORWARD ENTRY DOOR HANDLE CAME OFF<[01] 05 - OK TO CONTINUE PER [MEL 25-10-01;NON-ESSENTIAL EQUIPMENT & FURNISHINGS (NEF) - LISTED]. WITH SP _1B________ AND AUTHORIZATION NUMBER _218736______;[02] INSTALLED AND SECURED COVER ON FWD ENTRY DOOR IN
- [SDR SWAA2024080923685](https://openairdocs.org/sdr/SWAA2024080923685.md): Spar Cap · corroded · Aug 7, 2024 · N563WN · Boeing 737752 · Horizontal Stabilizer, Spar/Rib
> RH HORIZONTAL STAB AFT UPPER SPAR CAP HAS EVIDENCE OF CORROSION INTERGRANULAR CORROSION AT STAB STATION 304.19 ENDING AT +10 AT BUTT LINE 254.66. SPAR CORD IS EXFOLIATED COMPLETELY THROUGH. DAMAGE MEASURES 10'X 1'. REFERENCE TTG8Q00V2E87 FOR ORIGINAL FAULT.
- [SDR SWAA2024080923988](https://openairdocs.org/sdr/SWAA2024080923988.md): Spar Cap · corroded · Aug 7, 2024 · N563WN · Boeing 737752 · Horizontal Stabilizer, Spar/Rib
> R/H HORIZONTAL STABILIZER AFT SPAR CAP HAS EVIDENCE OF CORROSION AT STAB BUT LINE 254.66.<[01] REPAIRED PER EA 24-155-02168. SPEED TAPE APPLIED.;[02] REPAIRED PER EA 24-155-02168. SPEED TAPE APPLIED. REF. TTG8Q00V2NFP;[03] VERIFIED MECHANIC REPAIRED PER EA 24-
- [SDR SWAA2024080823684](https://openairdocs.org/sdr/SWAA2024080823684.md): Spar Cap · corroded · Aug 7, 2024 · N563WN · Boeing 737752 · Horizontal Stabilizer, Spar/Rib
> R/H HORIZONTAL STABILIZER AFT SPAR CAP HAS EVIDENCE OF CORROSION AT STAB BUT LINE 254.66.<[01] REPAIRED PER EA 24-155-02168. SPEED TAPE APPLIED.;[02] REPAIRED PER EA 24-155-02168. SPEED TAPE APPLIED. REF. TTG8Q00V2NFP;[03] VERIFIED MECHANIC REPAIRED PER EA 24-
- [SDR SWAA2024080823242](https://openairdocs.org/sdr/SWAA2024080823242.md): Girt Bar · out of adjust · Aug 7, 2024 · N563WN · Boeing 737752 · Escape Slide
> CABIN - R1 DOOR ESCAPE SLIDE GIRT PULLED OUT OF SLIDE BOX.<[01] RE-PACKED CABIN R1 DOOR ESCAPE SLIDE GIRT REF AMM 25-66-01.
- [SDR SWAA2023110718750](https://openairdocs.org/sdr/SWAA2023110718750.md): Fan · failed · Nov 7, 2023 · N563WN · Boeing 737752 · Air Distribution Fan
> DURING CRUISE FLT ATT REPORTED ODOR OF SMOKE IN AFT CABIN. DECLARED EMERGENCY DIVERTED TO IND; ACCOMPLISHED QRH SMOKE CABIN ISOLATED SYSTEM LANDED UNEVENTFUL DID NOT HAVE OVER WEIGHT LANDING PLEASE CHECK 3 PHASE POWER AT FAN<[01] LP 2556329 AP 4232348 PERFORME
- [SDR SWAA2023073183712](https://openairdocs.org/sdr/SWAA2023073183712.md): Cover · missing · Jul 29, 2023 · N563WN · Boeing 737752 · Emergency Lighting
> AFT SERVICE DOOR EXIT COVER MISSING<[01] REPLACED MISSING EXIT COVER AFT SERVICE DOOR PER SIP; ALL CHECKS GOOD.
- [SDR SWAA2023033021806](https://openairdocs.org/sdr/SWAA2023033021806.md): Lens · broken · Mar 29, 2023 · N563WN · Boeing 737752 · Emergency Lighting
> FWD LOWER EMERGENCY EXIT INDICATOR LENS AT ROW 12DEF IS BROKEN<[01] REMOVED AND REPLACED FWD LOWER EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01.
- [SDR SWAA2022122083600](https://openairdocs.org/sdr/SWAA2022122083600.md): Girt Bar · loose · Dec 20, 2022 · N563WN · Boeing 737752 · Emergency Equipment
> FWD ENTRY DOOR SLIDE BAR HOLD CLIP LOOSE.<[01] RE SECURED FWD ENTRY DOOR GIRT BAR CLIP. REF AMM 25-66-01
- [SDR SWAA2022120979719](https://openairdocs.org/sdr/SWAA2022120979719.md): Battery Pack · inoperative · Dec 8, 2022 · N563WN · Boeing 737752 · Emergency Lighting
> INOP LOWER SIDEWALL PANEL BATTERY PACK EMERGENCY EXIT DOOR LH SIDE AT PASSENGER CABIN. REPLACED LOWER SIDEWALL PANEL BATTERY PACK EMERGENCY EXIT DOOR LH SIDE AT PASSENGER CABIN IAW AMM-33-51-06-960-805. TESTED OK.
- [SDR SWAA2022120175112](https://openairdocs.org/sdr/SWAA2022120175112.md): Angle · cracked · Nov 23, 2022 · N563WN · Boeing 737752 · Fuselage Miscellaneous Structure
> CRACKED ANGLE, BS 291.5 - 294.5 S17R. REPLACED THE ANGLE IAW SRM 51-40-02, AND DRAWING 141A8310, SHEET 1, REV D.
- [SDR SWAA2022120874183](https://openairdocs.org/sdr/SWAA2022120874183.md): Floor Support · cracked · Nov 21, 2022 · N563WN · Boeing 737752 · Fuselage Miscellaneous Structure
> CRACKED FLOOR SUPPORT BETWEEN BS 344 - 360, LBL11, WL208.1. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A5400, SHEET 46, REV A.
Next page: https://openairdocs.org/aircraft/N563WN/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 = 'N563WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```
This list as a web page: https://openairdocs.org/aircraft/N563WN/reports
---
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