# Service difficulty reports: N17126

A list on [N17126](https://openairdocs.org/aircraft/N17126.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 · 81 reports

- [SDR CALA2026101320350](https://openairdocs.org/sdr/CALA2026101320350.md): Access Panel · cracked · Oct 6, 2026 · N17126 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING INTERSPAR 2 EACH CRACKS NOTED WHILE ACCOMPLISHING EA5720-03647 (A) AT HOLES NR 6 & 27 AT PANEL ACCESS 643BB. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5720-03684 AND ST ENGINEERING EA757-5720-13-A4616 WITH NO DEVIATIONS. DIP REQUIR ED AS FOLL
- [SDR CALA2026100720169](https://openairdocs.org/sdr/CALA2026100720169.md): Fitting · cracked · Oct 2, 2026 · N17126 · Boeing 757224 · Nacelle/Pylon, Main Frame
  > NR 2 ENG PYLON NACELLE MID STRUCTURE BULKHEAD PP STA 174.30 RBL 9 WITH CRACK. ACCOMPISHED REPAIR ON #2 ENG PYLON MID-BULKHEAD FWD RH LOWE R-FLANGE IAW EC/RA#:5450-03163,VT EA#:757-5450-13-A4626.REF:NR#1 9168
- [SDR CALA2026100620124](https://openairdocs.org/sdr/CALA2026100620124.md): Skin · dented · Sep 29, 2026 · N17126 · Boeing 757224 · Fuselage Main, Plate/Skin
  > (SDR) UPON FURTHER EVALUATION OF DIP LOGPAGE 8690478, FOUND DISCREPANCY WITH DENT LOCATION. (VERIFY LOCATION AND CHECK DENT.) REF NRC 19069. SFR CW PARTIAL SKIN PANEL REPLACEMENT BETWEEN B.S. 590 TO 630 AND S-14L TO S-19L PERFORMED I.A.W B757-200 SRM 53-30-01
- [SDR CALA2026092919998](https://openairdocs.org/sdr/CALA2026092919998.md): Retainer · cracked · Sep 29, 2026 · N17126 · Boeing 757224 · Fuselage Main, Structure
  > RIGHT MLG WW, CUTOUT FWD SEAL RETAINER HAVE 2 CRACKS IN DIFFERENCE PLACES. REMOVED AND REPLACED THE SUPPORT CHANNEL AND SUPPORT BRACKET (4EA) AT RT MLG WW CUTOUT FWD SEAL RETAINER IAW SRM 51-40-05, AND 51-40-02. RESTORED SURFACE PROTECTION IAW SRM 51-20-01,
- [SDR CALA2026092819949](https://openairdocs.org/sdr/CALA2026092819949.md): Channel · cracked · Sep 27, 2026 · N17126 · Boeing 757224 · Fuselage Miscellaneous Structure
  > LH MLG WW AFT BULKHEAD THROUGH ACCESS PANEL 143XAL WEB CRACKED. REMOVED AND REINSTALLED THE LT SLIDE PRESS BOTTLE IAW AMM 25-6 5-00/201 AND ARMING THE OFF-WING ESCAPE SYS TO BE ACCOMPLISH ON N/R 19021. REMOVED AND REPLACED THE WEB CHANNEL IAW SRM 51-40-02 -0
- [SDR CALA2026092819913](https://openairdocs.org/sdr/CALA2026092819913.md): Support Channel · cracked · Sep 25, 2026 · N17126 · Boeing 757224 · Fuselage Miscellaneous Structure
  > LEFT WW CUTOUT, FWD SEAL RETAINER WAS CRACKED IN THE OTBD SIDE. REMOVED AND REPLACED THE SUPPORT CHANEL OF THE LT WW CUTOUT FWD SEAL RETAINER IAW SRM 51-40-05, & 51-40- 02, RESTORED SURFACE PROTECTION IAW SRM 51-20-05, & AMM 51-21-15.
- [SDR CALA2026092519822](https://openairdocs.org/sdr/CALA2026092519822.md): Skin · dented · Sep 24, 2026 · N17126 · Boeing 757224 · Emergency Exits
  > LEFT FWD OVERWING EXIT DOOR EXTERIOR SKIN UPPER AND SIDE EDGE FOUND TWO DENTS. REPAIRED THE LT FWD OVERWING EXIT DOOR IAW EC/RA 5222-01051 AND EA 757-5220-13-A4623.
- [SDR CALA2026092419784](https://openairdocs.org/sdr/CALA2026092419784.md): Support Bracket · corroded · Sep 23, 2026 · N17126 · Boeing 757224 · Fuselage Miscellaneous Structure
  > LEFT WW AFT BULKHEAD OTBD SUPPORT BRACKET THAT ATTACH ACCESS PANEL 143XAL, CORRODED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02.
- [SDR CALA2026083119054](https://openairdocs.org/sdr/CALA2026083119054.md): Wire · detached · Aug 27, 2026 · N17126 · Boeing 757224 · Emergency Lighting
  > UPON PERFORMING EMERGENCY LIGHT TEST, FOUND ROW 41 ABC EMERGENCY LIGHT BURNED OUT TRACED WIRE FOR EMERGENCY EXIT LIGHT, FOUND BLACK WIRE BROKEN BETWEEN SEAT TRACK SEE PIC FOR DETAILS AVIONICS REQUIRED PERFORMED SPLICE OF EMERGENCY LIGHT WIRE ROW 41 ABC IAW SWP
- [SDR CALA2026083119053](https://openairdocs.org/sdr/CALA2026083119053.md): Battery Pack · inoperative · Aug 26, 2026 · N17126 · Boeing 757224 · Emergency Lighting
  > DURING AIRCRAFT INTERIOR INSPECTION, FOUND EMERGENCY EXIT LIGHTS FROM ROW 32 TO ROW 41 INOPERATIVE. PERFORMED LIGHT TEST OF BATTERY PACKS M737 AND M736 AND FOUND THEM NOT TURNING ON, R & R BOTH BATTERY PACKS IAW AMM 33-51-07. OPS CHECKED OK.
- [SDR CALA2026081418636](https://openairdocs.org/sdr/CALA2026081418636.md): Wire · detached · Aug 11, 2026 · N17126 · Boeing 757224 · Light System Wiring
  > ASILE PATH EMERGENCY LIGHT AT 35C, BROKEN SEAT MOUNTED WHITE LIGHT INOP. SEAT LIGHTS FWD AND AFT OP CHECK GOOD. REQUEST MEL 3351H APPROVED COMPLIED WITH MEL. *DM8 ADDED TO MATERIAL LIST 1 EA 29-3326-3-0013 LIGHT, SEAT, WH IN CASE NEEDED. FOUND SEAT 36C EMERG
- [SDR CALA2026060316801](https://openairdocs.org/sdr/CALA2026060316801.md): Charger · no test · Jun 2, 2026 · N17126 · Boeing 757224 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - EMERGENCY SEATS FLOOR PATH LIGHTING FROM ROW 32 TRU 41 INOP REMOVED AND REPLACED POWER SUPPLY REF AMM 33-51-07. OPS CHK NORMAL.PARTS USED: 19-3351-3-0097, QTY:1
- [SDR CALA2026052216479](https://openairdocs.org/sdr/CALA2026052216479.md): Power Supply · inoperative · May 22, 2026 · N17126 · Boeing 757224 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILS. THIRD OVERHEAD BIN LIGHT DOESENT LIGHT UP, RELAMP DOES NO GOOD. AFT 9 INTERIOR SEAT MOUNTED ISLE LIGHTS DONT LIGHT UP. SUSPECT BAD BATTERY. SWAPPED TWO ELECTRICAL CONNECTORS (D80 & D78) IAW WDM 33-51-22-906 FOR EMERGENCY LIGHT BATT
- [SDR CALA2026032414806](https://openairdocs.org/sdr/CALA2026032414806.md): Charger · faulted · Mar 23, 2026 · N17126 · Boeing 757224 · Emergency Lighting
  > FROM ROWS 31 TO BACK EMERGENCY LIGHTS INOP EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - SWAPPED EMERGENCY LIGHT BATTERY ON ROWS 29 (M735)(M10954). NO HELP SUSPECT BAD BATTERY AT AFT GALLEY (M736/M737). REPLACED EMERGENCY LITE POWER SUPP
- [SDR CALA2026032414819](https://openairdocs.org/sdr/CALA2026032414819.md): Transmitter · faulted · Mar 22, 2026 · N17126 · Boeing 757224 · Engine Indicating System
  > ERRONEOUS ENG INDICATION ON NUN 2 ENG. EPR READ OVER 2.0. FUEL F LOW WAS 2000 LESS THAN NR 1. SPOKE WITH FLT CREW. PHOTO OF ENGINE 2 PARAMETERS WHILE IN FLIGHT. REMOVED AND REPLACED #2 ENG EPR TRANSMITTER AND P1 FLEXIBLE LINE FOR EPR TRANSMITTER. REF AMM 77-11
- [SDR CALA2026030614381](https://openairdocs.org/sdr/CALA2026030614381.md): Oven · odor · Mar 4, 2026 · N17126 · Boeing 757224 · Buffet/Galleys
  > MID GALLEY OVEN HAD A BURNING ODOR DURING USE. DEBRIEFED CREW AND WAS INFORMED THAT ODOR ONLY OCCURED DURING OVEN USE. OVEN DEACTIVATED AND PLACARDED MID GALLEY OVEN INOP PER NEF 2520P. R & R G21 OVEN IAW AMM 25-34-00-000-801. OPS CHECK OK. NEF REVERSED.
- [SDR CALA2026022514058](https://openairdocs.org/sdr/CALA2026022514058.md): Power Supply · inoperative · Feb 24, 2026 · N17126 · Boeing 757224 · Emergency Lighting
  > EMERGENCY AISLE LIGHTS ROWS 32-41 OUT. R & R M737 EMERGENCY LIGHT POWER SUPPLY, OPS CHECKED GOOD IAW AMM 33-51-07.
- [SDR CALA2026022614111](https://openairdocs.org/sdr/CALA2026022614111.md): Oven · overtemp · Feb 21, 2026 · N17126 · Boeing 757224 · Buffet/Galleys
  > FOUND AFT GALLEY NR 3 OVEN EXCESSIVELY OVERHEATED WITH THERMAL IMAGING. REMOVED OVEN TO INSPECT ELECTRICAL CONNENCTION AND FOUND NO DAMGE OR BURNING. PLACARDED AFT GALLEY NR 3 OVEN. CB PULLED MEL APPLIED PLACED ON NEF. PULLED AND COLLARED CIRCUIT BREAKER.
- [SDR CALA2025112011358](https://openairdocs.org/sdr/CALA2025112011358.md): Mechanism · out of adjust · Nov 18, 2025 · N17126 · Boeing 757224 · Passenger/Crew Doors
  > L2 BOARDING DOOR WILL NOT CLOSE KNUCKLE KNOCKER HANGS UP. OTHERWISE DOOR 2L OPERATES AND SLIDE ARMS NORMALLY. REQUEST MEL. DDP COMPLIED WITH. MEL APPROVED FOR KNUCKLE KNOCKER HANGS UP HANGS UP AT DOOR 2L. PLACED IN MEL. *DM* SEE AMM TASK 52-11-20-825-001 & 52-
- [SDR CALA2025081807875](https://openairdocs.org/sdr/CALA2025081807875.md): Battery Pack · inoperative · Aug 16, 2025 · N17126 · Boeing 757224 · Emergency Lighting
  > EMERGENCY PATH LIGHTING FROM ROW 32 AFT INOP. CORRECT EPL DRAWING IS BR2013-P-757CO-5 REV F. PER THE BRUCE DRAWING ROWS 32-41 ARE POWERED BY BATTERY PACK / CHARGER M736 LOCATED ABOVE THE G4 AFT GALLEY AND RECEIVES POWER THROUGH PIN 13 OF D78. ALSO, REFERENCE W
- [SDR CALA2025081807874](https://openairdocs.org/sdr/CALA2025081807874.md): Lamp · inoperative · Aug 16, 2025 · N17126 · Boeing 757224 · Emergency Lighting
  > LEFT SIDE EXTERIOR OVERWING (FORWARD POSITION) EMERGENCY LIGHT INOP RELAMPED REF WDM 33-00-01-1. OPS CHECK GOOD.
- [SDR CALA2025050204411](https://openairdocs.org/sdr/CALA2025050204411.md): Frame · dented · May 1, 2025 · N17126 · Boeing 757224 · Fuselage Main, Frame
  > (19-5310-1-2500) STR-AFT CARGO COMPT. L/SIDE FR1260 BTWN STRG 25 /26 HAS A DENT ON FEE FLANGE AREA DOT 34-005 SDR/SFR REPORTING ONLY REPAIR ON AFT CARGO COMPARTMENT STA 1260 STR 25LH WAS PERFORMED IAW WORK PER UAL EC/RA #5360-01947 AND VT MAE EA 757-5360-13-A3
- [SDR CALA2025050204410](https://openairdocs.org/sdr/CALA2025050204410.md): Floorbeam · cracked · Apr 30, 2025 · N17126 · Boeing 757224 · Fuselage Main, Floor Beam
  > (SDR)-(B757-53-3-0487) NOSE FWD FUSELAGE MAIN DECK FLOOR BEAM CH ANNEL STA 345 BL0 CRACKED. DOT 139-2 REF:124292 SDR/SFR REPORTING ONLY CLOSING FOR SDR REPORTING
- [SDR CALA2025050104392](https://openairdocs.org/sdr/CALA2025050104392.md): Support · cracked · Apr 30, 2025 · N17126 · Boeing 757224 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) AFT CARGO COMPARTMENT AREA WATER TANK HAS SUPPORT WITH CRACK BTW STA 1640 AND 1660 BL 0 AT CEILING PANEL (REMOVED AND REPLACED) SDR/SFR REPORTING ONLY REPAIRED WATER TANK SUPPORT IAW B757 SRM 57-70-11-0G-0 ON AFT CA RGO COMP BTW STA 1640 AND 166
- [SDR CALA2025050104391](https://openairdocs.org/sdr/CALA2025050104391.md): Access Panel · corroded · Apr 30, 2025 · N17126 · Boeing 757224 · Nacelle/Pylon, Plate/Skin
  > (SDR)-B757-54-3-0053 ENGINE # L/H NACELLE STRUT 433 FL ACCESS AR EA SHOWS LOWER NUT PLATE RIVETS LOOSE AND NUT PLATE SUPPORTY LIG HT CORROSION. DOT 75-029 HA-75. REF:123778 SDR/SFR REPORTING ONLY REMOVED PANEL 433FL AND SUPPORT PLATE IAW B757-200 SRM 51-40-02-
- [SDR CALA2025050104387](https://openairdocs.org/sdr/CALA2025050104387.md): Bracket · cracked · Apr 30, 2025 · N17126 · Boeing 757224 · Leading Edge Devices
  > LEFT WING #3 L.E. SLAT OUTBD LWR L.E. HAS A CRACKED BRACKET BELOW ANTI-ICE DUCT. DOT 5-001 SDR/SFR REPORTING ONLY REMOVED END RIB (BRACKET) AT SLAT #3 LH WING IAW B757-200 SRM 51 -40-02-06-0 AND INSTALLED NEW END RIB (BRACKET) IAW B757-200 SRM 51-40-02-06-0, R
- [SDR CALA2025050104376](https://openairdocs.org/sdr/CALA2025050104376.md): Door Frame · dented · Apr 29, 2025 · N17126 · Boeing 757224 · Fuselage Main, Structure
  > (SDR)-(B757-06-3-0274) DENT IN L/H APU DOOR FRAME STA 1896. DOT 140-074.REF:124179 SDR/SFR REPORTING REMOVED LONGERON LH SIDE IAW B757-200 SRM 51-40-02-0G-0, RECIEVE D NEW LONGERON PN:UA 148N8201-7 LOCATED AND DRILLED WEB IAW B757 -200 SRM 51-40-05 RESTORED SU
- [SDR CALA2025050104375](https://openairdocs.org/sdr/CALA2025050104375.md): Bracket · corroded · Apr 29, 2025 · N17126 · Boeing 757224 · Fuselage Miscellaneous Structure
  > (SDR)-EA 5210-03219-CORROSION ON BRACKET FWD POSITION ON CENTER SCUFF PLATE AREA DOOR 4R. NO DOT.REF:124363 SDR/SFR REPORTING ONLY REMOVED AND REPLACED HAT STIFFENER (BRACKET) ON FWD POSTION ON C NTER SCUFF PLATE AREA DOOR 4RH IAW SRM 51-40-02-0G-0 AND RESTORE
- [SDR CALA2025050104374](https://openairdocs.org/sdr/CALA2025050104374.md): Gate · cracked · Apr 28, 2025 · N17126 · Boeing 757224 · Passenger/Crew Doors
  > CRACK ON UPPER DOOR GATE, 1R DOOR. REMOVE AND REPLACED UPPER DOOR GATE ON 1R DOOR IAW B757 AMM 52-1 1-38-404-009 AND ADJUSTMENTS AND OPS CHECKS WAS GOOD TO SERVICE WC#: 124368.
- [SDR CALA2025042904311](https://openairdocs.org/sdr/CALA2025042904311.md): Support Bracket · cracked · Apr 26, 2025 · N17126 · Boeing 757224 · Wing Miscellaneous Structure
  > (SDR)B757-57-3-0369-RH WING UPPER WTB FAIRING 196AR, AFT BRACKET SUPPORT IS CRACKED SFR REPORTING ONLY REMOVED T-CHORD OUTER CRACKED I.A.W B757-200 SRM 51-40-02-0G-0 A ND RECEIVED T-CHORD OUTER NEW P/N UASRM 53-40-71-01-1-13 TRAVEL ER # T25/1808169 AND INSTAL
- [SDR CALA2025042904317](https://openairdocs.org/sdr/CALA2025042904317.md): Repair · not reported · Apr 25, 2025 · N17126 · Boeing 757224 · Fuselage Structure (General)
  > (B757-53-3-0478) VERIFIED APPLICABILITY, STR-AFT CARGO COMPT. ST A 1320 BTWN STRG 24/26 HAS FRAME REPAIR VERY CLOSE TO FACTORY SPLICE, REMOVED EXISTING REPAIR AND INSTALLED NEW REPAIR IN AFT PIT STA 1320 STR 24/26R IAW 757 SRM 53-00-07-2R-5 DETAIL III. MAJOR
- [SDR CALA2025041403786](https://openairdocs.org/sdr/CALA2025041403786.md): Skin · dented · Apr 8, 2025 · N17126 · Boeing 757224 · Fuselage Main, Plate/Skin
  > (SUPPORT TASK) DENT ON RH FUSELAGE SKIN AT STA1640 TO STA1661 BE TWEEN STGR V27RH AND STGR28 RH (EVALUATION) FOR SDR REPORTING. SFR CREATED FOR REPAIR. ACCOMPLISHED REPAIR ON FUSELAGE SKNI AT STA 1640-1660 S27R-S28R IAW B757-200 SRM 53-00-01-2R-7. THIS REPAIR
- [SDR CALA2025040803650](https://openairdocs.org/sdr/CALA2025040803650.md): Lens · cracked · Apr 8, 2025 · N17126 · Boeing 757224 · Emergency Lighting
  > (B757-53-3-0564) L/H FUSELAGE LIGHT LENS CRACKED AT AFT OVER WIN G HATCH DOT 140-065
- [SDR CALA2025022802522](https://openairdocs.org/sdr/CALA2025022802522.md): Transmission · faulted · Feb 26, 2025 · N17126 · Boeing 757224 · Trailing Edge Flap Actuator
  > WHEN GOING FROM FLAPS UP TO FLAPS 1 TE FLAP DISAGREE CAUTION MS G DISPLAYED AUDIBLE CLUNK FOUND INBOARD FLAP SEAL CAME LOOSE. PHOTOS ADDED OP CHECKED FLAP NORMAL SYSTEM, OPERATED NORMALLY NO FAULTS OR CLUNKS. NO HISTORY IN LAST 90 DAYS OF FLAP DISAGREE. RECOM
- [SDR CALA2025011301877](https://openairdocs.org/sdr/CALA2025011301877.md): Screen · detached · Jan 9, 2025 · N17126 · Boeing 757224 · Compressor Bleed Valve
  > PDA 2 DURING BSI OF E2 DISCOVERED LIBERATED ACOUSTIC ATTENUATOR SCREEN AT 9OCLOCK POSITION IMAGE UPDATE R/R E#2 ACOUSTI ATTENAUTOR SCREEN IAW AMM TASK 75-32-10-404-006-R00 NO DEFECTS NOTICED AT THIS TIME A/C OK FOR SERVICE.
- [SDR CALA2024072900301](https://openairdocs.org/sdr/CALA2024072900301.md): Limit Switch · faulty · Jul 25, 2024 · N17126 · Boeing 757224 · Stabilizer Control System
  > STAB TRIM CAUTIO ON CLMB OUT. AUTOPILOT CAUTION EICAS FOLLOWED 3 TIMESDEBRIEFED CREW AND WAS INFORMED THAT STAB TRIM CAUTION CAME ON PRIOR TO A/P ENGAGEMENT ON CLIMB. PERFORMED MCDP BITE IAW AMM 22-02 TASK 801; FOUND SEVERAL PREVIOUS FLIGHT LEGS A/P CAUTION ME
- [SDR CALA2024050701389](https://openairdocs.org/sdr/CALA2024050701389.md): Fuse · blown · May 7, 2024 · N17126 · Boeing 757224 · Emergency Lighting
  > EXIT/SALIDA EMERGENCY LIGHT INOP AT LAV S. VERIFIED OPS OF LIGHTS CHECKS GOOD. REMOVED AND REPLACED EMERGENCY LIGHT LAMPS REF AMM 33-51-10 REMOVED AND REPLACED FUSE ON M10919 REF AMM 33-51-07-962-071,
- [SDR CALA2023072802348](https://openairdocs.org/sdr/CALA2023072802348.md): Transmitter · unknown · Jul 25, 2023 · N17126 · Boeing 757224 · Stabilizer Position Indicating
  > UNSHEDULED STAB TRIM ILLUMINATED AT 65KNOTS ON T/O AND REJECT AT 75 KNOTS LOCKED FOR FIX. REF L/P 5266158 FOR WORK PERFORMED & CORRECTIVE ACTION. ALL OPS CKS GOOD, NO FAULTS AT THIS TIME. A/C OK TO CONTINUE. ADD EMP:U197565 REMOVED AND REPLACED LEFT AND RIG
- [SDR CALA2023070702192](https://openairdocs.org/sdr/CALA2023070702192.md): Module · faulty · Jul 4, 2023 · N17126 · Boeing 757224 · Flight Control System
  > ON TO UNSCHD STAB TRIM EICAS REJECTED TO AT APPROX 30KNTS REPLACED RIGHT LSTM IAW AMM 27-48-01-024-001 AND STAB POSITION MODULE BOARD M10410. PRFORMED OPS CHECK AMM27-41-00-501 & 27-48-00-501 & 27-48-03-424-009 ALL TEST PASSED. PARTS USED: 1435135,QTY:1 19-
- [SDR CALA2022101002761](https://openairdocs.org/sdr/CALA2022101002761.md): Fseu · faulty · Oct 10, 2022 · N17126 · Boeing 757224 · Trailing Flap Position Indicating System
  > TE FLAP DISAGREE. ALT LE AND TE FLAPS USED AND FLAP ISLN VAL MESSAGE APPEARED AT 20 DEGREE FLAP. REPLACED FSEU 1. NO HELP. RAN FLAPS UP AND DOWN HYDRAULICALLY AND FOUND STATUS MSG FLAP ISLN VAL.FOLLOWED FIM 27-51 FAULT TREE 818 AND REPLACED PRESSURE SWITCH ON
- [SDR CALA2022090702302](https://openairdocs.org/sdr/CALA2022090702302.md): None · worn · Sep 6, 2022 · N17126 · Boeing 737 · Powerplant System
  > TALKED TO INBOUND CAPT. HE STATED AT FL 360 (36000 FT), HIS ENG #1 PARAMETERS VARIED GREATLY FROM ENG #2. HIS PARAMETERS DID NOT RETURN TO NORMAL UNTIL FL 210 (21000 FT.) THE INBOUND CAPT GAVE ME THE FOLLOWING ENG PARAMETERS AT FL 360: ONE MORE PARAMETER. CAPT
- [SDR CALA2022071101706](https://openairdocs.org/sdr/CALA2022071101706.md): Repair · discovered · Jul 10, 2022 · N17126 · Boeing 757224 · Fuselage Main, Frame
  > 46 AFT CARGO COMPARTMENT FRAME INITIAL INSPECTION (RH SIDE) STA 1300 STR 26R EXISITING REPAIR 6" ABOVE AND 6" BELOW STR 26R. CONTACT ENGINEERING (SEE BAM N/R 792868) COMPLIED WITH EC/RA 5360-01656. SEE UPDATES IN BAM FOR ALL WORK ACCOMPLISHED. BAM N/R 7928
- [SDR CALA2022062201547](https://openairdocs.org/sdr/CALA2022062201547.md): Skin · gouged · Jun 20, 2022 · N17126 · Boeing 757200 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN, REPAIR DOUBLER AND SKIN LAP, AT S14L JUST FORWARD OF STA 1720, ARE GOUGED. AIRCRAFT FLIGHT CYCLES BUT BEFORE 44,000 TOTAL AIRCRAFT FLIGHT CYCLES....REF ORIGINAL L/P# 980227 AND HANGAR N/R# 674756 PLANNING TO CONTACT ENGINEERING FOR EC/RA 533
- [SDR CALA2022051301220](https://openairdocs.org/sdr/CALA2022051301220.md): Floorbeam · corroded · May 11, 2022 · N17126 · Boeing 757200 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM STA 377 AT L1 DOOR (MARKED)
- [SDR CALA2021100601811](https://openairdocs.org/sdr/CALA2021100601811.md): Warning Message · illuminated · Oct 6, 2021 · N17126 · Boeing 757224 · Trailing Edge Flap Control System
  > DURING APPCH FROM FLAPS UP TO FLAPS 1 TE FLAP DISAGREE EICAS MISSIONS AND ACCOMPL CORRECTIVE ACTION AS NECESSARY. SO FAR, THE LEFT WING MOST INBOARD FLAP TRANSMISSION #4 OVERLOAD IND IS POP PED. ABOVE LP IS CORRECT AND CONFIRMED THAT THE FLAP NEVER MOVED UPON
- [SDR CALA2021100601807](https://openairdocs.org/sdr/CALA2021100601807.md): Flap System · faulted · Oct 6, 2021 · N17126 · Boeing 757224 · Trailing Flap Position Indicating System
  > TE FLAP DISAGREE EICAS WHEN FLAP HANDLE MOVED TO FLAPS 1 POSIT ION. QRH PROCEDURE RUN PERFORMED OPS TEST OF TE FLAP SYSTEM REF AMM 27-51-00-715-001, LE AND TE FLAPS OPERATE NORMAL. PERFORMED BITE OF FSEU 1,2,AND 3. BITE SHOW NO FAULTS REF 27-51 FAULT TRE
- [SDR CALA2021100601777](https://openairdocs.org/sdr/CALA2021100601777.md): Actuator · tripped · Oct 3, 2021 · N17126 · Boeing 757224 · Trailing Edge Flap Actuator
  > LE SLAT DISAGREE DEBRIEF FROM CREW WHEN HE SELECTED FLAPS 1 THE FLAP INDICATOR RETURNED FLAPS TO NORMAL CONFIG AND PERFORMED FSEU BITE. ON CYCLED FLAPS UP AND DOWN SEVERAL TIMES WITH NO FAULTS. CHECKED STOPPED AT 1/2 AND A LEADING EDGE SLAT DISAGREE MSG CAME O
- [SDR CALA2019021700264](https://openairdocs.org/sdr/CALA2019021700264.md): Frame · dented · Feb 15, 2019 · N17126 · Boeing 757224 · Fuselage Main, Frame
  > B757-06-3-0230 DENT ON FWD CARGO FRAME UPPER FLANGE AT STA 660 ABOVE STR 22L. REF ST SAA N/R 0049127 FWD CARGO FRAME UPPER FLANGE DENT AT STA 660 STR 22L FOUND OUT OUT OF LIMITS, L=1.0, W=1.0, D=0.030, IAW SRM 53-00-07 FIG 101. CUT OUT DMG & ACC PERMANENT REPA
- [SDR CALA2019021700263](https://openairdocs.org/sdr/CALA2019021700263.md): Floorbeam · corroded · Feb 15, 2019 · N17126 · Boeing 757224 · Fuselage Main, Floor Beam
  > B757-53-3-0488 FLOOR BEAM AT STA 365.25 HAS A PREVIOUS REPAIR WI TH CORROSION FROM RBL 12 TO RBL 25 ON UPPER SURFACE. REF N /R 0049140 FOUND STA 365 FLOOR BEAN UPPER CHORD OUT OF LIMITS IAW B757-200 SRM 53-00-51 FIG 101 L=3.0 W=2.0 D=.015. REMOVED EXISTING REP
- [SDR CALA2018020900553](https://openairdocs.org/sdr/CALA2018020900553.md): Elt · no test · Feb 9, 2018 · N17126 · Boeing 757224 · Emergency Locator Beacon
  > AFT PORTABLE EMERGENCY LOCATOR TRANSMITTER FAILED BITE TEST. REMOVED AND REPLACED AFT PORTABLE ELT. BITE TEST PASSED IAW AMM 25-64-02.

Next page: https://openairdocs.org/aircraft/N17126/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 = 'N17126' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N17126/reports

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